diff --git "a/data.ndjson" "b/data.ndjson"
new file mode 100644--- /dev/null
+++ "b/data.ndjson"
@@ -0,0 +1,20381 @@
+[4.660344123840332, -4.534090518951416, "Satellite Image Capture Date March 30, 2022"]
+[1.358309268951416, 2.866987705230713, "Weather Station Record Temperature -11.8\u00baC"]
+[1.4310497045516968, 2.7544384002685547, "Weather Station Average High Temperatures in March Around -48\u00baC"]
+[-0.6952682137489319, 9.060954093933105, "Reference Frame Recognition Global Geodetic Reference Frame (GGRF)"]
+[1.2389103174209595, -2.327073097229004, "Geodetic Spherical Satellite Number of Satellites Smaller with respect to the ones of GNSS"]
+[1.5219515562057495, -3.1213018894195557, "Future Satellites Tracking Opportunities Several times per day"]
+[0.057232316583395004, 13.409958839416504, "Metrology System Component Quantity 2"]
+[0.022340575233101845, 13.42423152923584, "Metrology System Component Interchangeable Yes"]
+[0.022957628592848778, 13.421963691711426, "Metrology System Component Reliability Equally reliable"]
+[-3.5728821754455566, 4.398563861846924, "Spacecraft Launch Date June 13, 2012"]
+[-3.0859858989715576, 4.2586774826049805, "Spacecraft Launch Vehicle Pegasus-XL"]
+[-0.9510623812675476, 7.678762912750244, "Device Measurement Objective Measure the magnetic fluxes produced by Earth's magnetic field"]
+[-1.014470100402832, 7.782899856567383, "Device Operating Principle Change in electrical resistance experienced by a multilayer structure in the presence of a magnetic field"]
+[-1.037355661392212, 7.749382019042969, "Device Structure Composed of magnetic and non-magnetic films"]
+[-1.0239357948303223, 7.757257461547852, "Device Resistance Very high without an external magnetic field and a current applied perpendicular to the magnetization of the layers"]
+[-1.0134965181350708, 7.737900733947754, "Device Resistance Decreases in the presence of an external magnetic field perpendicular to the magnetization of the layers"]
+[-0.1565524935722351, 15.58780288696289, "Spectrometer Spectral Range 0.05 - 0.8 nm"]
+[-0.14758315682411194, 15.585911750793457, "Spectrometer Dynamic Range 10^-9 - 10^-3 W/m^2"]
+[-0.10892411321401596, 15.510515213012695, "Spectrometer SNR 1:1 over 10 minute average"]
+[-0.13266369700431824, 15.461962699890137, "Spectrometer Data Product Accuracy \u226420% over mission life"]
+[-0.10771258920431137, 15.531170845031738, "Spectrometer Cadence \u22643 s"]
+[-0.12269847095012665, 15.582439422607422, "Spectrometer Spectral Range 5 - 127 nm"]
+[-0.19473174214363098, 15.630414962768555, "Spectrometer Spectral Resolution From 5-35 nm: 10 nm bins, From 35-115 nm: 40 nm bins, Lyman-\u03b1 (121.6 nm): 10 nm (FWHM), 5-115 nm; 5 nm bins, 117-127 nm; 10 nm bin"]
+[-0.0897674486041069, 15.595380783081055, "Spectrometer SNR 1:1 over 10 minute average, > 20:1 over 10 minute average"]
+[-0.09378965198993683, 15.584844589233398, "Spectrometer Data Product Accuracy \u226420% over mission life, 18% over mission life"]
+[-0.09593286365270615, 15.535240173339844, "Spectrometer Cadence \u226430 s, 27 s"]
+[5.334449291229248, -4.360644817352295, "Satellite Launch Date Late January 2016"]
+[2.266209840774536, -1.5668268203735352, "Satellite Laser Terminal Type Autonomous state-of-the-art telescope"]
+[0.682248592376709, -1.3973097801208496, "Satellite Moving Target Distance Up to 45 000 km"]
+[2.4996843338012695, -2.55806303024292, "Satellite Laser Beam Capacity Up to 1.8 Gbit/s of user data"]
+[2.4975287914276123, -2.2142839431762695, "Satellite Radio Transmitter Type Ka-band"]
+[-0.36762869358062744, 15.626220703125, "FUV Imaging Spectrometer Spectral Range ~133\u2013165 nm"]
+[-0.34502488374710083, 15.598711967468262, "FUV Imaging Spectrometer Resolution 0.21, 0.35, or 2.16 nm"]
+[-0.3738399147987366, 15.58486557006836, "FUV Imaging Spectrometer Scanning Cadence ~15 min"]
+[-0.37185561656951904, 15.655472755432129, "FUV Imaging Spectrometer Spectral Dispersion 0.04 nm/pixel"]
+[-0.3682625889778137, 15.631734848022461, "FUV Imaging Spectrometer Brightness Unit R (1R = 1010 photons m-2 s-1 steradian-1)"]
+[4.646851539611816, -2.618204355239868, "Satellite Mission Duration Decade-long"]
+[2.815478801727295, -1.0385619401931763, "Satellite Purpose Study polar ice"]
+[2.137005090713501, -1.7674976587295532, "Satellite Study Area Antarctica"]
+[2.290858745574951, -1.4855672121047974, "Satellite Instrument Ice, Cloud and land Elevation Satellite-2"]
+[2.381368398666382, -1.5591151714324951, "Satellite Instrument Operation IceBridge"]
+[-2.1770646572113037, 6.653831958770752, "Flight Hardware Components AMS Experiment, AMS Payload Integration Hardware (PIH)"]
+[0.12377922236919403, 7.196624755859375, "Experiment Provider International AMS Collaboration led by the MIT (Massachusetts Institute of Technology)"]
+[-1.9817968606948853, 7.539074420928955, "Hardware Provider NASA/JSC (Johnson Space Center), Houston, TX, with the support of Lockheed Martin Space Operations (LMSO)"]
+[2.8855059146881104, 14.168157577514648, "Laser Instrument Operation Sends pulses of light to Earth"]
+[2.8574581146240234, 14.237278938293457, "Laser Instrument Timing Accuracy Within a billionth of a second"]
+[2.9110074043273926, 14.167708396911621, "Laser Instrument Laser Pulses More than 50 billion times"]
+[2.810600519180298, 14.216530799865723, "Laser Instrument Pulse Rate 10,000 pulses/s"]
+[2.826585292816162, 14.215426445007324, "Laser Instrument Photons Sent per Pulse 300 trillion"]
+[4.236832141876221, -2.563227653503418, "Satellite Contaminant Dissipation Time Fourteen days"]
+[-0.07951193302869797, 15.528292655944824, "Spectrometer Prototype Operation Duration 10 days"]
+[-0.023369167000055313, 15.510457038879395, "Spectrometer Prototype Observation Millions of helium nuclei, but no antihelium"]
+[-0.038752153515815735, 15.491145133972168, "Spectrometer Prototype Purpose Test particle physics technology in LEO"]
+[-0.059835441410541534, 15.534996032714844, "Spectrometer Prototype Magnet Quantity 10"]
+[-0.05490240454673767, 15.525622367858887, "Spectrometer Prototype Magnet Types Seven magnets for field calculation, leakage and dipole moment; Three full-size magnets for space qualification, destructive testing and flight"]
+[0.8950853943824768, 14.797050476074219, "Instrumentation Employing Teams Institute for Telecommunications in Portugal and the University of Stirling in Scotland"]
+[0.9068194031715393, 14.79814624786377, "Instrumentation Deployed Teams University of Leiden, the University of Oldenburg in Germany and the ITC Faculty of Geo-Information Science and Earth Observation of the University of Twente"]
+[-1.0368962287902832, 6.895968914031982, "Activity Performing Teams University of Alberta in Canada and the Technical University Delft in the Netherlands"]
+[-2.6528396606445312, 11.661107063293457, "Imager Telescope Type Off-axis"]
+[-2.6319096088409424, 11.718186378479004, "Imager Number of Detectors 216"]
+[-2.645690679550171, 11.678519248962402, "Imager Spectral Bands 14"]
+[-2.6137142181396484, 11.690240859985352, "Imager Calibration Full-path on-orbit"]
+[-2.5078227519989014, 4.33349609375, "Space Station Remote Manipulator System Operator JAXA astronaut Kimiya Yui"]
+[11.845503807067871, 5.305184364318848, "3U CubeSats Mass 5 kg"]
+[11.85825252532959, 5.300774574279785, "3U CubeSat Mass ~3 kg"]
+[11.886523246765137, 5.289100170135498, "3U CubeSat Mass 4 kg"]
+[2.8864259719848633, -1.7198452949523926, "Satellite Prime Developers Telespazio (Rome, Italy) and TAS (Thales Alenia Space)"]
+[16.565872192382812, 7.021846771240234, "Minisatellite Built by TUBITAK-UZAY and TAI (Turkish Aerospace Industries Inc.) consortium"]
+[16.606327056884766, 6.985049247741699, "Minisatellite Integration and Testing TAI's facilities"]
+[0.4541528820991516, 9.36517333984375, "Attitude Control System Control Coarse three-axis control of the spacecraft body"]
+[-1.7155544757843018, 8.825712203979492, "Fine Control System Control Small, rapid adjustments to the detector position to keep the target star stationary"]
+[-2.775803327560425, 4.1742167472839355, "Space Boundary Reconnection Lines Multiple"]
+[0.6572016477584839, 4.180673122406006, "Atmospheric Phenomenon East/West Extents Relatively small"]
+[-2.6476032733917236, 4.064297199249268, "Space Phenomenon Length A few RE or smaller"]
+[-2.568117380142212, 4.050161361694336, "Space Phenomenon Spatially Localized True"]
+[2.714076519012451, 14.395289421081543, "Optical Instrument Scattering Level Between 1 and 2 Rsun"]
+[2.6230742931365967, 14.331352233886719, "Optical Instrument Function Blocks the direct light from the external occulter"]
+[2.630080461502075, 14.32695484161377, "Optical Instrument Critical Parameter Micro-roughness of each surface"]
+[2.599091053009033, 22.31779670715332, "Instrument Stray Light Analyses Model ASAP model"]
+[1.6989468336105347, -1.5805810689926147, "Satellite Modes Usage Increase Quick ramp up"]
+[1.5604716539382935, -1.5073896646499634, "Satellite Mode Resolution 5 m"]
+[1.4171007871627808, -1.4762095212936401, "Satellite Mode Swath 125 km"]
+[4.0876994132995605, 13.92879867553711, "Laser Altimeter Ground Footprint 10 m"]
+[4.087247848510742, 13.927189826965332, "Laser Altimeter Repetition Rate 10 kHz"]
+[4.098663330078125, 13.929987907409668, "Laser Altimeter Laser Energy ~1 mJ"]
+[4.089817523956299, 13.92369270324707, "Laser Altimeter Number of Beams 9"]
+[4.119340896606445, 13.906403541564941, "Laser Altimeter Detector Pixels per Spot Multiple"]
+[4.090972423553467, 13.927692413330078, "Laser Altimeter Ground Footprint 10 m"]
+[1.7103251218795776, 6.921157360076904, "Communication Device Size 106 mm x 166 mm x 90 mm"]
+[1.6853917837142944, 6.924919128417969, "Communication Device Mass 1.6 kg"]
+[1.7471662759780884, 6.892823696136475, "Communication Device Downlink Rate Capability Up to 2 Mbit/s"]
+[1.7354155778884888, 6.896441459655762, "Communication Device Uplink Rate 100 kbit/s"]
+[2.4470536708831787, 22.23876190185547, "Instrument Low-Light Imaging Capability Collect low-light imaging data of the Earth during the nighttime period"]
+[2.059595823287964, 22.489988327026367, "Instrument Radiances Measurement Down to 10-9 W/cm2/sr"]
+[1.8408644199371338, 22.125892639160156, "Instrument Spatial Resolution 2.7 km"]
+[-2.3201189041137695, 9.133914947509766, "Electrical Power System Bus Voltage 70 V"]
+[-2.8535218238830566, 9.465455055236816, "Battery Discharge Regulator Bus Voltage 70 V"]
+[-2.2886621952056885, 7.407192230224609, "On-board Computer Protocol MIL STD 1553B"]
+[0.973641037940979, -4.427536487579346, "Satellite Mass 3 kg"]
+[1.6955819129943848, 6.95700740814209, "Communication Device Modulation QPSK"]
+[1.6991158723831177, 6.94780969619751, "Communication Device Error Correction RS (255, 223)"]
+[1.7268441915512085, 6.910304069519043, "Communication Device Transmission Rate 1.5 Mbit/s"]
+[1.674931526184082, 6.966784477233887, "Communication Device Modulation QPSK"]
+[1.6887078285217285, 6.957583904266357, "Communication Device Error Correction RS (255, 223)"]
+[1.6895617246627808, 6.9336700439453125, "Communication Device Transmission Rate 155 Mbit/s"]
+[3.47634220123291, 10.554698944091797, "Amplifier Output Power Unknown"]
+[3.4749045372009277, 10.55401611328125, "Amplifier Isolation Among Output Ports High performance"]
+[3.4761009216308594, 10.558640480041504, "Amplifier TWTA Traveling Wave Tube Amplifier"]
+[3.475696325302124, 10.553765296936035, "Amplifier Bandwidth 1.1 GHz"]
+[6.34124755859375, 7.3908915519714355, "Satellite Component Design Stiffness, strength and pointing requirements of the payload, sensors"]
+[6.322231292724609, 7.410899639129639, "Satellite Component Construction Sandwich construction with aluminum core and CFRP face skin"]
+[6.263063907623291, 7.349650859832764, "Satellite Component Interface Interface with the launch vehicle"]
+[6.264142036437988, 7.430774688720703, "Satellite Component Interface Interface for the propellant tank and reaction wheel deck"]
+[-1.9046252965927124, 8.154335021972656, "System Block Diagram Figure 16"]
+[5.111230850219727, -4.387979507446289, "Satellite Mission Date April 19-21, 2007"]
+[5.056012153625488, -4.636470794677734, "Satellite Workshop Date Oct. 13-15, 2008"]
+[-2.484358549118042, 12.570696830749512, "Spectral Imager Spectral Channels 9"]
+[-2.486496686935425, 12.573311805725098, "Spectral Imager Spectral Region 443 to 910 nm"]
+[-2.482095956802368, 12.56523609161377, "Spectral Imager Polarized Filters 3"]
+[-2.528221607208252, 12.599200248718262, "Spectral Imager Polarized Wavelengths 3"]
+[-2.48939847946167, 12.557732582092285, "Spectral Imager Image Sequence Acquisition Time 20 seconds"]
+[-4.496443748474121, 15.91183090209961, "Radar Technology APAA (Active Phased Array Antenna)"]
+[-4.467922210693359, 15.899083137512207, "Radar X-band Spatial resolution from 1 to 500 m"]
+[-4.521285533905029, 15.932875633239746, "Radar Swath Width 10 - 750 km"]
+[-2.984677314758301, 16.168289184570312, "Scatterometer Ku-band 25 x 25 km spatial resolution"]
+[-2.982954502105713, 16.170637130737305, "Scatterometer Swath 1800 km"]
+[1.2387287616729736, 10.903830528259277, "Scanner Channels 4"]
+[1.2325618267059326, 10.917177200317383, "Scanner Spatial Resolution 80 m"]
+[1.1946501731872559, 10.933119773864746, "Scanner Swath 800 km"]
+[1.253494381904602, 10.899698257446289, "Scanner Channels 8"]
+[1.308616280555725, 10.891093254089355, "Scanner Spatial Resolution 1 km"]
+[1.19673752784729, 10.945680618286133, "Scanner Swath 3000 km"]
+[2.765130043029785, 22.4174747467041, "Instrument Type Radiomet"]
+[1.39035964012146, -1.993509292602539, "Satellite Pointing Stability Best performance to date for spacecraft of its size"]
+[3.0834810733795166, -1.758535623550415, "Satellite Mission Status Operating on an extended mission"]
+[-10.264510154724121, 9.977684020996094, "Accelerometer Device Type Electrostatic"]
+[0.22007670998573303, 9.190285682678223, "Stabilization System Presentation Date June 21-23, 2010"]
+[0.11876743286848068, 9.136388778686523, "Stabilization System URL https://trs.jpl.nasa.gov/handle/2014/41635"]
+[2.6597559452056885, 5.391363143920898, "Emergency Beacon Location Accuracy About 20 km"]
+[2.661360263824463, 5.391097545623779, "Emergency Beacon Identification Not included"]
+[-9.95862865447998, 5.84322452545166, "Search and Rescue System Persons Rescued Over 27,000"]
+[2.434746503829956, -1.2369699478149414, "Satellite Experiment Investigate the effect of gravity on the reproductive spores of the fern, Ceratopteris richardii"]
+[-1.2800955772399902, 7.927680015563965, "Lab-on-a-chip devices Quantity 3"]
+[-1.364198923110962, 8.061843872070312, "Lab-on-a-chip devices Function Integrate the sensors that allow for real-time measurement of calcium signaling"]
+[6.345426082611084, 7.394150733947754, "Satellite Component Function Shields the cryogenic radiator from the warm Earth and all direct sun"]
+[-0.39128929376602173, 8.232380867004395, "Insulation Type Specialized"]
+[-1.212892770767212, 8.603386878967285, "Component Function Thermally conductive, yet structurally isolating"]
+[-0.8144496083259583, 8.734463691711426, "Heater Function Maintain a constant cryogenic detector temperature"]
+[-1.734283685684204, 8.854491233825684, "Control System Function Maintains thermal control of the focal planes when pointing the instrument at off-nadir ground targets"]
+[6.165323257446289, 7.573291301727295, "Satellite Component Quantity 3"]
+[3.51291561126709, 13.41666316986084, "Laser Transmitter Wavelength 532 nm"]
+[3.498525381088257, 13.401693344116211, "Laser Transmitter Pulse Width 1 ns"]
+[3.4818034172058105, 13.40632438659668, "Laser Transmitter Repetition Rate 10 kHz"]
+[3.4738659858703613, 13.396069526672363, "Laser Transmitter Beam Divergence 20 \u00b5rad"]
+[3.4947385787963867, 13.416364669799805, "Laser Transmitter Footprint Diameter 10 m"]
+[2.6370325088500977, 13.454033851623535, "Optical Element Beam Splitting Split the single transmit beam into 6 beams"]
+[-2.4448652267456055, 4.107824802398682, "Space Segment Signal Detection Emergency signals"]
+[2.6616930961608887, 5.389351844787598, "Beacon Alert Message Content Identification code"]
+[2.6432950496673584, 5.405632019042969, "Beacon Additional Feature 121.5 MHz homing transmitter"]
+[-3.01216459274292, 7.823081016540527, "Data Processor Development Company MDA (MacDonald Dettwiler)"]
+[-2.6483314037323, 11.473522186279297, "Image Size 100 km x 100 km"]
+[-2.7000584602355957, 11.445935249328613, "Image Required Tapes 6 magnetic tapes of 1600 BPI"]
+[1.5745058059692383, 2.3281288146972656, "Geostationary Operational Environmental Satellite Image Acquisition Date 18 August 2021"]
+[-0.04680789262056351, 4.492576599121094, "Hurricane Speed 15 miles (24 km) per hour"]
+[0.18163487315177917, 4.521942138671875, "Tropical Storm Landfall Location Florida Panhandle near Apalachicola"]
+[0.1934438943862915, 4.462719917297363, "Tropical Storm Sustained Winds 65 miles (105 km) per hour"]
+[-0.15016604959964752, 4.764945983886719, "Storm Location Offshore near the Bahamas"]
+[2.6703717708587646, -1.7435181140899658, "Satellite Constellation Operator Open Cosmos"]
+[5.214047908782959, -4.3349199295043945, "Satellite Launch Date 22 March 2021"]
+[2.8367209434509277, -2.4525458812713623, "Satellite Network Connection Type 5G IoT"]
+[-1.6183830499649048, 1.481981873512268, "Data Relay System Operation Period 2015 until 2021, with an option for extension until 2028"]
+[-1.6367944478988647, 1.500927448272705, "Data Relay System Partners ESA, Airbus DS, DLR, 50 companies in 13 European countries"]
+[-1.636414885520935, 1.5052520036697388, "Data Relay System Service Level Agreement Date 20 February 2015"]
+[2.6855828762054443, 21.66334342956543, "Observation Instrument Quantity 26 (24 normal cameras and 2 fast cameras)"]
+[1.4609763622283936, -2.417081356048584, "Satellite Orbit Lagrangian point L2 of the Sun-Earth system"]
+[4.173375606536865, -2.6298911571502686, "Satellite Long-Term Pointing Stability 3.85 days"]
+[1.40919029712677, -2.017732620239258, "Satellite Short-Term Pointing Stability 25 s"]
+[-1.1325644254684448, 4.4720869064331055, "Ground Stations Operation Frequency S-band"]
+[-1.2441229820251465, 4.412467956542969, "Ground Station Component Function Control the antenna"]
+[2.267920732498169, -2.0308988094329834, "Satellite Control Center Location S\u00e3o Jos\u00e9 dos Campos, Brazil"]
+[2.140573263168335, -1.9667136669158936, "Satellite Control Center Main Functions Orbit and attitude control, manoeuvre calculations, operational payload configuration, real-time monitoring of the satellite health"]
+[-3.1442251205444336, 1.9499913454055786, "Mars Sample Return Campaign Mission Type Multiple missions to the Red Planet to collect samples, launch them into space and return them safely to Earth"]
+[-2.1127021312713623, 4.313010215759277, "Space Stations Previous Projects International Space Station, Orion and the future Gateway around the Moon"]
+[2.7407174110412598, 12.527976036071777, "Multibeam System Survey Date April 20, 2012"]
+[2.6949303150177, 12.423561096191406, "Multibeam System Survey Date April 8, 2012"]
+[-0.9485366344451904, 6.389008045196533, "Survey System Survey Date April 11, 2012"]
+[1.8279848098754883, 22.24150848388672, "Instrument Image Resolution 0.7 m"]
+[1.7120648622512817, -1.78350031375885, "Satellite Geolocation Accuracy Not provided"]
+[1.3909037113189697, -3.0602617263793945, "Satellites Orbit Highly elliptical (600 x 60530 km)"]
+[1.4106510877609253, -3.1103708744049072, "Satellites Period About 19.7h"]
+[0.2802678346633911, 9.295794486999512, "Rotating Body Frames Alignment Parallel to each other"]
+[0.38864678144454956, 9.42009449005127, "Rotating Body Frames Orientation The corresponding x-axes are oriented along the relative motion line"]
+[-2.8050172328948975, 15.251859664916992, "Microwave Radiometer Mission Objective Investigate the use of microwave radiometers and to measure both wind speed and direction over the ocean"]
+[0.4804844856262207, 12.149547576904297, "Sensor Calibration Quality Extremely demanding"]
+[0.5074642300605774, 12.190800666809082, "Sensor Calibration Care Commensurate"]
+[-0.824073314666748, 12.60445499420166, "Radiation Area Monitors Quantity 6"]
+[-0.8264438509941101, 12.567282676696777, "Radiation Shielding Experiment Dosimeters Quantity 10"]
+[-0.8511662483215332, 12.489303588867188, "Battery-operated Independent Radiation Detector Parameter Active radiation monitor capable of time-resolved particle flux measurements"]
+[-3.5313870906829834, 4.3816423416137695, "Spacecraft Launch Date December 2014"]
+[-3.491649627685547, 4.36695671081543, "Spacecraft Return Date Sept. 1, 2015"]
+[-13.923437118530273, -2.139432907104492, "X-ray Telescope Energy Range 0.5-2 keV"]
+[-13.883410453796387, -2.242154121398926, "X-ray Telescope Number of X-ray Sources More than 18,000"]
+[-13.85734748840332, -2.223957061767578, "X-ray Telescope Number of X-ray Stars Most of the remainder X-ray stars"]
+[-13.852561950683594, -2.231816053390503, "X-ray Telescope Number of Clusters of Galaxies More then 400"]
+[-13.65527057647705, -2.2920804023742676, "X-ray Telescope Date of First X-ray Images 22 October 2019"]
+[-13.882394790649414, -2.2382006645202637, "X-ray Telescope Number of X-ray Telescope Modules 7"]
+[-13.862943649291992, -2.244248867034912, "X-ray Telescope Distance of Interacting Clusters of Galaxies About 800 million lightyears"]
+[1.3376798629760742, 5.351289749145508, "Spacecraft Bus Power Source Solar Panels"]
+[-3.0453059673309326, 4.396941661834717, "Spacecraft Data Storage Capacity 580 Gbits/day"]
+[-3.08042311668396, 4.3043341636657715, "Spacecraft Data Downlink Rate 220 Mbit/s"]
+[-3.039158821105957, 4.323497295379639, "Spacecraft Solar Panels 4"]
+[-3.0359842777252197, 4.343725204467773, "Spacecraft Solar Panels Power 1320 Watts"]
+[-3.0515189170837402, 4.2661614418029785, "Spacecraft Thrusters Four 22 N thrusters and eight 4.5 N thrusters"]
+[-3.016470432281494, 4.185435771942139, "Spacecraft Orbit Determination High-precision GPS receiver and laser ranging"]
+[3.0509212017059326, -1.6635479927062988, "Satellite Collaboration Partners Danish Technical University, University of Copenhagen, Aalborg University, Terma A/S, CRI, Copenhagen Optical Company, DDC International, Innovision, Per Udsen Co., Rescom, Ticra, DNSC, DMI, NASA, ESA, CNES, DLR, and more than 40 universities and research institutes"]
+[2.7408699989318848, -1.5200855731964111, "Satellite Image Credit DRSI"]
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+[-3.549692392349243, 14.274539947509766, "Radiometric Imager Full-polarimetric Capability Frequencies 10.7, 18.7, 37 GHz"]
+[-3.552363872528076, 14.249235153198242, "Radiometric Imager Width Swath >1000 km"]
+[-3.5764479637145996, 14.24047565460205, "Radiometric Imager Calibration On-board two-point"]
+[-3.5428781509399414, 14.275228500366211, "Radiometric Imager Frequency (GHz) 6.8/7.2"]
+[-3.5462639331817627, 14.26789665222168, "Radiometric Imager Bandwidth (MHz) 350"]
+[-3.5615577697753906, 14.267462730407715, "Radiometric Imager Polarisation V, H"]
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+[-3.5569896697998047, 14.244180679321289, "Radiometric Imager Spatial Resolution 53 x 31 km"]
+[-3.5367331504821777, 14.291028022766113, "Radiometric Imager Frequency (GHz) 10.7"]
+[-3.537238359451294, 14.28210163116455, "Radiometric Imager Bandwidth (MHz) 300"]
+[-3.5616514682769775, 14.275010108947754, "Radiometric Imager Radiometric Resolution (K) 0.4"]
+[-3.5555903911590576, 14.247820854187012, "Radiometric Imager Spatial Resolution 34 x 19 km"]
+[-3.536536693572998, 14.285706520080566, "Radiometric Imager Frequency (GHz) 19.1"]
+[-3.5475709438323975, 14.263701438903809, "Radiometric Imager Bandwidth (MHz) 750"]
+[-3.5451643466949463, 14.280149459838867, "Radiometric Imager Radiometric Resolution (K) 0.3"]
+[-3.5733232498168945, 14.24487590789795, "Radiometric Imager Spatial Resolution 19 x 11 km"]
+[-3.5589139461517334, 14.291489601135254, "Radiometric Imager Frequency (GHz) 23.8"]
+[-3.5595312118530273, 14.246861457824707, "Radiometric Imager Bandwidth (MHz) 500"]
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+[-3.5561397075653076, 14.248098373413086, "Radiometric Imager Spatial Resolution 15 x 9 km"]
+[-3.550212860107422, 14.269243240356445, "Radiometric Imager Frequency (GHz) 37.0"]
+[-3.562929391860962, 14.25876235961914, "Radiometric Imager Bandwidth (MHz) 2000"]
+[-3.543320655822754, 14.27790355682373, "Radiometric Imager Radiometric Resolution (K) 0.3"]
+[-3.561614513397217, 14.255867004394531, "Radiometric Imager Spatial Resolution 10 x 6 km"]
+[-3.554497718811035, 14.270197868347168, "Radiometric Imager Frequency (GHz) 90"]
+[-3.5478246212005615, 14.28050422668457, "Radiometric Imager Bandwidth (MHz) 2000"]
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+[-3.574071168899536, 14.238407135009766, "Radiometric Imager Spatial Resolution 4 x 2 km"]
+[0.16211634874343872, 7.202998161315918, "Experiment Size Requirement Fitting within 17.6 cm2"]
+[0.12449242919683456, 7.187677383422852, "Experiment Ceiling Height Requirement Less than 54 mm"]
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+[-3.373185396194458, 7.20050048828125, "Data Handling System On-board Data Storage 1 MB"]
+[-0.005109984427690506, 7.15423059463501, "Sample Oxygen Isotopic Composition Unknown"]
+[1.3765575885772705, -1.041789174079895, "Satellite Measurement Height of the ice surface"]
+[2.6248488426208496, -1.351720929145813, "Satellite Data Integration ICESat-2\u2019s predecessor, the original ICESat mission, as well as the European Space Agency\u2019s satellite dedicated to monitoring polar ice thickness, CryoSat-2"]
+[2.521761655807495, -1.167883038520813, "Satellite Data Use Update classical understanding of subglacial lakes in Antarctica"]
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+[-0.6315292716026306, 9.423722267150879, "Spacecraft Component Material Avcoat"]
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+[1.596588134765625, 2.2490665912628174, "Geostationary Satellite Data Download System Ka-band communications"]
+[2.182706832885742, 22.661184310913086, "Instrument Spectral Region 340-860 nm"]
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+[2.0974838733673096, 22.236547470092773, "Instrument Wide-Angle Video Camera Field of View 60\u00ba"]
+[-7.5528435707092285, 5.904947280883789, "Camera Field of View 10.7\u00ba x 14.0\u00ba"]
+[2.057753801345825, 22.595613479614258, "Instrument FWHM of the Filters 4, 4, 30, 30, 50 and 40 nm"]
+[-3.4555094242095947, 4.364141941070557, "Spacecraft Extra Flight Schedule 2010"]
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+[-2.1074931621551514, 4.307549953460693, "Space Station Research Benefits Benefits to humanity on Earth"]
+[2.7157320976257324, 22.25040626525879, "Instrument Testing Location Ocean Wave Facility"]
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+[-2.4093704223632812, 7.2738566398620605, "Onboard Computer Function Performs measurements of GNSS scintillations"]
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+[1.916619062423706, 10.720253944396973, "Imaging Device Sample Rate 25 seconds"]
+[-1.1437671184539795, 3.062859535217285, "Celestial Bodies Mass Accuracy 10%"]
+[-3.4650027751922607, 6.886031150817871, "Observation Data Precision 2%"]
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+[1.693381667137146, 6.913486003875732, "Communication Device Ground Station Contact Maintained"]
+[4.6879167556762695, -2.568467378616333, "Satellite Mission Duration 10 to 15 years"]
+[6.330593585968018, 7.407690525054932, "Satellite Component Manufacturer Honeywell"]
+[5.147043228149414, -4.379911422729492, "Satellite Loss Date January of this year"]
+[4.681297302246094, -2.57246732711792, "Satellite Expected Mission Duration 10 to 15 years"]
+[7.412738800048828, 12.546599388122559, "Satellite Instrument Image Acquisition Date December 19, 2018"]
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+[-6.715721607208252, 9.999499320983887, "Electromagnetic Waves Path Dependency Ionosphere Location"]
+[0.5084373354911804, 12.215489387512207, "Micro-sensor Size 30 mm x 50 mm"]
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+[-3.0525360107421875, 9.630562782287598, "Battery Voltage 24 V"]
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+[0.9573373794555664, -4.3930816650390625, "Satellite Mass 23.9 kg"]
+[4.946012020111084, -2.418351173400879, "Satellite Expected Lifetime 5 years"]
+[-1.5468865633010864, 12.841239929199219, "Solar Coronagraph Optical Performance Unknown"]
+[-1.5607010126113892, 12.848856925964355, "Solar Coronagraph Formation Flying Applied Unknown"]
+[6.356805324554443, 7.38180685043335, "Satellite Component Dimensions 1.34 x 1.34 x 3.2m"]
+[6.343977451324463, 7.407045364379883, "Satellite Component Power Source Six solar panels in two wings, with two Lithium-ion batteries"]
+[6.312803268432617, 7.418829441070557, "Satellite Component Communication System S-band TT&C (Telemetry, Tracking and Command) transceivers and X-band data downlink transmitters"]
+[-1.6012128591537476, 4.101718425750732, "Ground Segment Number of Ground Stations 3"]
+[-1.5807344913482666, 4.109930038452148, "Ground Segment Daily Downlink Time About 102 minutes"]
+[-1.1327499151229858, 4.474268913269043, "Ground Station Daily Downlink Time Approximately 93 minutes"]
+[-0.17387956380844116, 15.575089454650879, "Spectrometer Wavelength Calibration 1064 nm and 1532 nm"]
+[-0.10741528123617172, 15.5025634765625, "Spectrometer Mount Type Adjustable vernier kinematic mount with five degrees of freedom"]
+[-3.7951223850250244, 6.913243293762207, "Environmental Data Collection Design Life 3-5 years"]
+[4.6799139976501465, -2.605407476425171, "Satellite Operational Duration More than 22 years"]
+[0.08969226479530334, 11.653014183044434, "Environmental Monitoring Operational Date Fiscal Year 2024"]
+[-0.8307334780693054, 0.14657382667064667, "Satellite System Contract Type Predominantly fixed price"]
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+[-0.8240235447883606, 0.14459234476089478, "Satellite System Instrument Passive microwave imaging radiometer"]
+[-0.8232166171073914, 0.15851102769374847, "Satellite System ECP Sensor Hosted Government furnished"]
+[-1.9141913652420044, 14.874515533447266, "Radiometer Design Total-power radiometer"]
+[-1.9007631540298462, 14.859375953674316, "Radiometer Sensitivity Better sensitivity (factor 2) over a conventional Dicke-switched system"]
+[-1.9163404703140259, 14.892815589904785, "Radiometer Frequency Range 10-48 GHz"]
+[-1.8486216068267822, 14.831287384033203, "Radiometer Frequency Range 52-57, 91 and 183 GHz"]
+[-1.9100173711776733, 14.861753463745117, "Radiometer Polarization Vertical and horizontal"]
+[-1.9082634449005127, 14.8386869430542, "Radiometer Polarization Horizontal"]
+[-1.9204607009887695, 14.905021667480469, "Radiometer Number of Channels 29"]
+[-0.8362181186676025, 0.155246302485466, "Satellite System Purpose Provide accurate and timely meteorological forecasts"]
+[-0.7899072170257568, 0.1252266764640808, "Satellite System Forecasting Needs Civil and military"]
+[1.5817432403564453, -2.195791721343994, "Satellite Attitude Control 3-axis stabilized"]
+[2.0592260360717773, -2.603400945663452, "Satellite Reaction Wheels 4"]
+[1.5267003774642944, -2.3082821369171143, "Satellite Reaction Wheels Capacity 0.12 Nms"]
+[2.3342881202697754, -1.9606271982192993, "Satellite GPS Receiver Onboard location and time services"]
+[1.0984002351760864, -2.0673599243164062, "Satellite Body-pointing Capability \u00b130\u00ba in cross-track"]
+[-8.136198997497559, 8.828265190124512, "Electric Power Subsystem Solar Array Power 180 W (EOL)"]
+[-8.14125919342041, 8.827032089233398, "Electric Power Subsystem Battery Capacity 15 Ah"]
+[0.9831300377845764, -4.370682239532471, "Satellite Mass 120 kg"]
+[-1.6392544507980347, 9.687437057495117, "Propulsion Subsystem Propellant N2H4"]
+[-1.5853970050811768, 9.719430923461914, "Propulsion Subsystem Delta V 70 m/s"]
+[-4.481257915496826, 15.898895263671875, "Radar Interferometry Technique More sensitive to the motion of the ice"]
+[-3.443859338760376, 6.852782726287842, "Data Product Accuracy Improvement 10 times more accurate than any previous map"]
+[-3.438429594039917, 6.860653877258301, "Data Product Coverage Shows flows over 80% of the continent"]
+[-1.3790032863616943, 6.954411029815674, "Engineering Model Development Status Under development"]
+[-1.498070240020752, 7.047083854675293, "Engineering Model In-Orbit Demonstration Planned for 2010"]
+[3.706437349319458, 17.70534896850586, "Payload Electrical Interfaces Power, LRDL (Low Rate Data Link), HRDL (High Rate Data Link)"]
+[-5.214945316314697, 7.799371242523193, "Communication System Data Rate ~ 10 kbit/s"]
+[-5.22420072555542, 7.856645107269287, "Communication System Duty Cycle 55 - 90%"]
+[-5.20648717880249, 7.882573127746582, "Communication System Continuous Transmission 10 byte/s"]
+[-5.2619948387146, 7.9158935546875, "Communication System Command Path From the POCC to AMS-02"]
+[2.1757595539093018, 22.431884765625, "Instrument Sensitivity Greater than those carried by Ulysses in the 1990s"]
+[2.862035036087036, -1.2232273817062378, "Satellite Studies Objects outside our solar system, such as exploding stars and disks of hot gas accelerated by the gravity of massive black holes"]
+[2.6143269538879395, -1.4667705297470093, "Satellite Source of the X-rays By Juno"]
+[1.386596441268921, -2.5359275341033936, "Satellite Orbit type Sun synchronous"]
+[4.163773536682129, -3.008570671081543, "Satellite Local equator crossing time 13:00 \u00b1 0:15 hour"]
+[0.7642126083374023, -1.1772081851959229, "Satellite Altitude 613 km"]
+[4.120757579803467, -2.483966588973999, "Satellite Repeat cycle 6 days"]
+[1.146388053894043, -0.8258920907974243, "Satellite Spacecraft size (main body) 5.3 x 2.0 x 2.8 m"]
+[0.9507419466972351, -4.271507263183594, "Satellite Spacecraft mass < 2,000 kg"]
+[2.092449426651001, -0.5245112180709839, "Satellite Spacecraft power 5.0 kW"]
+[5.346092224121094, -4.46818733215332, "Satellite Launch date 29 October 2018"]
+[4.419705867767334, -3.383216619491577, "Satellite Launch time (UTC) 04:08:00"]
+[4.391372203826904, -3.3443796634674072, "Satellite Launch time (JST) 13:08:00"]
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+[1.900420904159546, 10.709443092346191, "Imaging Device Gating Time 1, 1/125, 1/250, 1/500, 1/1000 s"]
+[1.8966093063354492, 10.72200870513916, "Imaging Device Data Bit Depth 12 or 8 bit"]
+[1.9310921430587769, 10.705277442932129, "Imaging Device Nr. of Imaging Tiles per Record 1, 2 or 4"]
+[1.8676965236663818, 10.697552680969238, "Imaging Device Binning Modes 1 x 1, 1 x 2, 2 x 1, 2 x 2"]
+[1.9286435842514038, 10.73802661895752, "Imaging Device Data Block Length 0 to 134 MByte"]
+[1.9401051998138428, 10.731733322143555, "Imaging Device Gain 1 or 4"]
+[-5.379542350769043, 2.8441007137298584, "Imaging Telescope Energy Band 0.5-11 keV"]
+[-5.352456569671631, 2.8783059120178223, "Imaging Telescope Number of Observed Clusters of Galaxies Ten thousands"]
+[2.896522283554077, 22.468610763549805, "Instrument Provider RosKosmos (an IKI-led consortium)"]
+[2.884795904159546, 22.330575942993164, "Instrument Developer MPE Garching"]
+[1.4489197731018066, 5.390869140625, "Spacecraft Bus and Launch Provider Provider Roskosmos"]
+[-5.100259304046631, 7.696206092834473, "Communication Subsystem and Ground Station Support Provider Provider ESA"]
+[1.469614028930664, -2.391767978668213, "Satellite Orbit Initial sun-synchronous elliptical orbit, altitude 643 x 450 km, inclination of 98.3\u00ba"]
+[1.6112489700317383, -2.0404045581817627, "Satellite Attitude Mode SPM (Sun Pointing Mode)"]
+[1.8609914779663086, -1.9919832944869995, "Satellite Attitude Mode NM-Z"]
+[1.4480040073394775, -2.3945956230163574, "Satellite Orbit Circular orbit at an altitude of 393 km"]
+[3.518095016479492, 13.50417423248291, "Laser System Wavelength 532 nm"]
+[3.540719509124756, 13.447273254394531, "Laser System Pulse Rate 10,000 pulses per second"]
+[2.7961084842681885, 12.891965866088867, "Polarizing Beam Combiner Function Ensure primary and backup lasers head down the same path"]
+[2.790459632873535, 12.953189849853516, "Polarizing Beam Combiner Function Use a periscope to pick off a fraction of the laser light and direct it to the LSA"]
+[2.7717297077178955, 22.516027450561523, "Instrument Retrieval of Atmospheric Properties and Surface Bidirectional Reflectances Unknown"]
+[-3.111419200897217, 4.262951374053955, "Spacecraft Overall Responsibility Airbus"]
+[-3.83731746673584, 3.734502077102661, "Rover Launch Date July 2020"]
+[-3.8134491443634033, 3.7970125675201416, "Rover Landing Date February 2021"]
+[-3.8589322566986084, 3.714704751968384, "Rover Function Acquire Mars samples, cache them into sample tubes, and leave the tubes in one or more depots"]
+[-5.311848163604736, 7.5298848152160645, "Communication Protocol Data Format Analog voltages on the two analog channels"]
+[-5.249974250793457, 7.527276992797852, "Communication Protocol Data Packet Size Up to 255 bytes"]
+[-3.65649151802063, 7.649099349975586, "Data Recording Information Type Analog"]
+[-3.6877872943878174, 7.684488296508789, "Data Recording Information Type Analog"]
+[1.8753858804702759, -2.133206844329834, "Satellite Orbit Geostationary"]
+[2.0894253253936768, -1.4505571126937866, "Satellite Imaging Cadence Complete scan of each hemisphere every 15 minutes"]
+[0.5160537362098694, -1.4896390438079834, "Satellite Orbit Altitude 22,000 miles (35,786 km) above the Earth"]
+[-1.7217111587524414, 8.862447738647461, "Control System Cause of Failure Wrong routing and connection of the control lanes"]
+[-1.6961615085601807, 8.865335464477539, "Control System Effect of Failure Inversion of electrical connections, not detected through the different control steps and tests"]
+[-4.363367557525635, 0.19217684864997864, "GPS Module Reference Frame WGS84 Earth centered fixed frame"]
+[4.706991195678711, -2.5748841762542725, "Satellite Nominal Mission Lifetime 2 years"]
+[4.384822845458984, -2.721696615219116, "Satellite LEOP Duration Less than 2 days"]
+[4.504333019256592, -2.689885139465332, "Satellite Commissioning Duration About 2 months"]
+[4.635165214538574, -2.6150991916656494, "Satellite Nominal Operations Duration About 22 months"]
+[6.296670913696289, 7.443382263183594, "Satellite Component Size No bigger than the tip of a pinkie finger"]
+[6.235611915588379, 7.503225803375244, "Satellite Component Quantity 9"]
+[6.366979122161865, 7.3730926513671875, "Satellite Component Location Precise latitude, longitude, and elevation"]
+[6.223568439483643, 7.518304347991943, "Satellite Component Quantity 6"]
+[6.268368721008301, 7.473456859588623, "Satellite Component Intensity Much higher than normal"]
+[2.605536937713623, 12.164018630981445, "Beam Mode Coverage 90 km"]
+[2.6138553619384766, 12.184728622436523, "Beam Mode Incidence Angle Range 29-50\u00ba"]
+[2.6351613998413086, 12.197229385375977, "Beam Mode Image Single-pol (HH, VV, HV or VH)"]
+[2.6277379989624023, 12.187243461608887, "Beam Mode Swath Width At least 50 km"]
+[2.6211628913879395, 12.202425956726074, "Beam Mode Incidence Angle Range 30 -50\u00ba"]
+[2.6333253383636475, 12.19334888458252, "Beam Mode Image Single-pol (HH, VV, HV or VH)"]
+[0.6260950565338135, 9.305968284606934, "Attitude Control Subsystem Supplier Unknown Unknown"]
+[-1.2179458141326904, 6.179383754730225, "Telecommunications Subsystem Supplier Unknown Unknown"]
+[-1.4922446012496948, 13.408760070800781, "Solar Arrays Supplier Unknown Unknown"]
+[-8.12716293334961, 8.790449142456055, "Power subsystem and Batteries Supplier Unknown Unknown"]
+[-2.075991153717041, 6.636026859283447, "Flight computer Supplier Unknown Unknown"]
+[-2.0544943809509277, 6.239066123962402, "Focal Plane Supplier Unknown Unknown"]
+[-0.6522907614707947, 5.931536674499512, "Piezo Stage Supplier Unknown Unknown"]
+[-1.1126034259796143, 6.109957695007324, "Thermal hardware Supplier Unknown Unknown"]
+[-13.858725547790527, -2.1693508625030518, "X-ray Telescope Temperature Sensitivity More than 5.4 million degrees Fahrenheit"]
+[-13.878575325012207, -2.2216107845306396, "X-ray Telescope Temperature Sensitivity More than 3 million degrees Celsius"]
+[-13.869011878967285, -2.206275701522827, "X-ray Telescope X-ray Detection Range Higher end of the range"]
+[-13.863022804260254, -2.2419488430023193, "X-ray Telescope X-ray Source Sun, Jupiter"]
+[1.6860772371292114, 6.9516282081604, "Communication Device Table Entries 1440"]
+[1.703087329864502, 6.937474250793457, "Communication Device Table Switch Time 8 hours"]
+[1.6862238645553589, 6.952572345733643, "Communication Device Table Composition Time 8 hours"]
+[1.896806001663208, -2.124380588531494, "Satellite Orbit Geostationary"]
+[0.9800993800163269, -2.1434881687164307, "Satellite Position 82\u00b0 East, over the equator"]
+[8.955317497253418, 8.512242317199707, "Satellite Payload Control System Fully-automated operations engine"]
+[-0.16959333419799805, 11.065728187561035, "Monitoring and Control System Version Enhanced derivative of ESA's SCOS-2000 v3.1"]
+[-1.7463082075119019, 8.864649772644043, "Control System Function Supervise the complete cycle of telecommand uplink and execution, as well as reaction monitoring of telemetry"]
+[-1.6307092905044556, 14.734989166259766, "Photometer Wavelength 427.8nm and 630nm"]
+[-1.5998749732971191, 14.702139854431152, "Photometer Operation Nightside of the orbit"]
+[-0.7963244318962097, 11.626194953918457, "Detector Package Components Photomultiplier tube, high voltage power supply, and pulse amplitude discriminator electronics"]
+[-2.9856960773468018, 20.17962074279785, "Spectral Band Wavelength Range 0.45-0.49 \u00b5m"]
+[-3.0097591876983643, 20.160118103027344, "Spectral Band Center Wavelength 0.47 \u00b5m"]
+[-2.6056325435638428, 20.00696563720703, "Spectral Band Nominal IGFOV 1 km"]
+[-2.9833269119262695, 20.17168617248535, "Spectral Band Wavelength Range 0.59-0.69 \u00b5m"]
+[-2.9905998706817627, 20.176416397094727, "Spectral Band Center Wavelength 0.64 \u00b5m"]
+[-2.5931453704833984, 20.000791549682617, "Spectral Band Nominal IGFOV 0.5 km"]
+[-2.9754741191864014, 20.1700382232666, "Spectral Band Wavelength Range 0.846-0.885 \u00b5m"]
+[-2.9998276233673096, 20.178050994873047, "Spectral Band Center Wavelength 0.885 \u00b5m"]
+[-2.614572048187256, 20.0112247467041, "Spectral Band Nominal IGFOV 1 km"]
+[-2.9833598136901855, 20.187393188476562, "Spectral Band Wavelength Range 1.371-1.386 \u00b5m"]
+[-2.993421792984009, 20.17096519470215, "Spectral Band Center Wavelength 1.378 \u00b5m"]
+[-2.5949394702911377, 20.001388549804688, "Spectral Band Nominal IGFOV 2 km"]
+[-2.981729745864868, 20.1744327545166, "Spectral Band Wavelength Range 1.58-1.64 \u00b5m"]
+[-2.967313051223755, 20.16081428527832, "Spectral Band Center Wavelength 1.61 \u00b5m"]
+[-2.5911142826080322, 20.004133224487305, "Spectral Band Nominal IGFOV 1 km"]
+[-2.9833638668060303, 20.16969108581543, "Spectral Band Wavelength Range 2.225-2.275 \u00b5m"]
+[-2.9731364250183105, 20.198862075805664, "Spectral Band Center Wavelength 2.25 \u00b5m"]
+[-2.5894312858581543, 20.000957489013672, "Spectral Band Nominal IGFOV 2 km"]
+[-3.0166666507720947, 20.22097396850586, "Spectral Band Wavelength Range 3.80-4.00 \u00b5m"]
+[-3.0046212673187256, 20.18193244934082, "Spectral Band Center Wavelength 3.90 \u00b5m"]
+[-2.5948479175567627, 20.00176429748535, "Spectral Band Nominal IGFOV 2 km"]
+[-2.9742772579193115, 20.1866397857666, "Spectral Band Wavelength Range 5.77-6.6 \u00b5m"]
+[-2.9849653244018555, 20.17892837524414, "Spectral Band Center Wavelength 6.19 \u00b5m"]
+[-2.5989346504211426, 20.002857208251953, "Spectral Band Nominal IGFOV 2 km"]
+[-2.9392669200897217, 20.13660430908203, "Spectral Band Wavelength Range 6.75-7.15 \u00b5m"]
+[-2.9831838607788086, 20.197586059570312, "Spectral Band Center Wavelength 6.95 \u00b5m"]
+[-2.6031196117401123, 20.00551986694336, "Spectral Band Nominal IGFOV 2 km"]
+[-2.9478964805603027, 20.163997650146484, "Spectral Band Wavelength Range 7.24-7.44 \u00b5m"]
+[-2.994999885559082, 20.177175521850586, "Spectral Band Center Wavelength 7.34 \u00b5m"]
+[-2.5866217613220215, 19.99861717224121, "Spectral Band Nominal IGFOV 2 km"]
+[-2.9345178604125977, 20.231870651245117, "Spectral Band Wavelength Range 8.3-8.7 \u00b5m"]
+[-2.973010778427124, 20.160215377807617, "Spectral Band Center Wavelength 8.5 \u00b5m"]
+[-2.5872139930725098, 20.00140380859375, "Spectral Band Nominal IGFOV 2 km"]
+[-2.97377872467041, 20.184478759765625, "Spectral Band Wavelength Range 9.42-9.8 \u00b5m"]
+[-2.95550274848938, 20.152393341064453, "Spectral Band Center Wavelength 9.61 \u00b5m"]
+[-2.5986480712890625, 20.003662109375, "Spectral Band Nominal IGFOV 2 km"]
+[-2.956322193145752, 20.19562530517578, "Spectral Band Wavelength Range 10.1-10.6 \u00b5m"]
+[-2.9836809635162354, 20.160137176513672, "Spectral Band Center Wavelength 10.35 \u00b5m"]
+[-2.579774856567383, 19.995527267456055, "Spectral Band Nominal IGFOV 2 km"]
+[-2.924506187438965, 20.127756118774414, "Spectral Band Wavelength Range 10.8-11.6 \u00b5m"]
+[-2.991671562194824, 20.183509826660156, "Spectral Band Center Wavelength 11.2 \u00b5m"]
+[-2.5701684951782227, 20.034992218017578, "Spectral Band Nominal IGFOV 2 km"]
+[-2.936591148376465, 20.14188003540039, "Spectral Band Wavelength Range 11.8-12.8 \u00b5m"]
+[-3.146210193634033, 1.7069846391677856, "Satellite Mission Goal Demonstrate usefulness of space based sensing for refining orbital parameters of an orbiting object"]
+[-0.9441916346549988, -10.00124454498291, "Satellite Constellation Positional Error 1000 m"]
+[-0.9499239921569824, -10.00685977935791, "Satellite Constellation Number of Warnings About 10 per day"]
+[-0.9525427222251892, -10.001214027404785, "Satellite Constellation Number of Possible Conjunctions 1 in 10 days"]
+[-0.9769150614738464, -10.03890323638916, "Satellite Constellation Certainty Improvement Four orders of magnitude"]
+[-0.9571862816810608, -10.001803398132324, "Satellite Constellation Estimated Cost \u20ac 3.4 billion"]
+[-3.5553700923919678, 4.395816326141357, "Galileo Spacecraft Naming Ceremony Date Nov. 9, 2005"]
+[-0.9402301907539368, -10.008886337280273, "Satellite Constellation Operational Goal 2013"]
+[-0.14563727378845215, 9.032343864440918, "European Navigation Program Delay 3 years"]
+[-0.12117022275924683, 8.976508140563965, "European Navigation Program Number of Satellites 30"]
+[-0.14720194041728973, 9.065618515014648, "European Navigation Program Ground Segment Infrastructure Included"]
+[-1.664023518562317, 11.239099502563477, "Lidar Wavelengths 355, 532, and 1064 nm"]
+[-1.6729736328125, 11.232504844665527, "Lidar Operating Modes Six science modes"]
+[-1.6581028699874878, 11.236680030822754, "Lidar Lasers Two high repetition rate lasers"]
+[-1.664072871208191, 11.225711822509766, "Lidar IFOV Four"]
+[-13.8965482711792, -2.2321741580963135, "X-ray Telescope Optic Type Lobster-eye micropore optic"]
+[-13.891525268554688, -2.238637924194336, "X-ray Telescope Optic Size 4 x 4 cm"]
+[-13.84683609008789, -2.2413887977600098, "X-ray Telescope Micropore Array 20 x 20 \u00b5m square-hole micropores"]
+[-13.909687995910645, -2.267521381378174, "X-ray Telescope Optic Configuration Kirkpatrick/Baez system"]
+[1.2748539447784424, 5.326873779296875, "Spacecraft Bus Launch Mass 325 kg"]
+[1.4159404039382935, 5.388300895690918, "Spacecraft Bus Size (deployed) 3.9 m x 1.2 m x 1.5 m"]
+[-2.603874683380127, 9.619471549987793, "Power Source Power 400 W (EOL)"]
+[0.6297091245651245, 9.318336486816406, "Attitude Control Subsystem Pointing Accuracy 3.2 arcsec control, 2.7 arcsec knowledge"]
+[-5.197340965270996, 7.759710788726807, "Communication System Data Rate 100 Mbit/s"]
+[11.390673637390137, 5.60891056060791, "Corner Cube Retroreflectors Surface Quality Tolerances 1/10 wavelength for the three back faces, 1/8 wavelength for the front face, 1/4 exiting wavefront"]
+[11.26671314239502, 5.496876239776611, "Corner Cube Retroreflectors Quantity in Lot 10"]
+[2.8560311794281006, -1.476717472076416, "Satellite Earth Observation Mission First"]
+[2.0619094371795654, -1.5714749097824097, "Satellite Earth Magnetic Field Sensor COTS AMR magnetic sensor"]
+[7.194155216217041, 12.325695991516113, "Remote Sensing Instrument Purpose Provide measurements of atmospheric clouds and aerosols"]
+[7.202731609344482, 12.329726219177246, "Remote Sensing Instrument Information Type Range-resolved"]
+[-2.128877878189087, 4.303734302520752, "Space Station Orbit Passes over and along many of the primary aerosol transport paths within the atmosphere"]
+[-2.1476011276245117, 4.313811302185059, "Space Station Orbit Permits study of diurnal (day to night) changes due to the effects of aerosols and clouds in the atmosphere"]
+[-1.6166859865188599, 1.4789403676986694, "Data Relay System Feeder Link Antarctic Latitudes"]
+[-1.1171152591705322, 5.846761226654053, "Conference Date May 7-9, 2014"]
+[-0.8628390431404114, 6.1057024002075195, "Resource Address http://elib.dlr.de/89312"]
+[-6.674994468688965, 9.998207092285156, "Antenna Components 128 horn antennas, 128 high power amplifiers (HPAs), and a beam forming network (BFN) with 256 digital phase shifters (PSs)"]
+[3.474242925643921, 10.559857368469238, "Amplifiers Output Power 28 dBm"]
+[-1.7158088684082031, 8.863598823547363, "Control System Phase Control Interval 2 ms"]
+[-1.7465386390686035, 8.88459300994873, "Control System Beam Directions Eight spot beam directions for each beam"]
+[-1.7300828695297241, 8.879681587219238, "Control System Attenuator Control Compensate for gain variations due to temperature inputs"]
+[1.5155391693115234, 5.422050476074219, "Satellite Bus Attitude Control System Three-axis controlled, zero-momentum"]
+[1.5132766962051392, 5.4254150390625, "Satellite Bus Power Draw 290 W"]
+[1.5168075561523438, 5.431865692138672, "Satellite Bus Solar Array Power 415 W"]
+[1.5105221271514893, 5.4254255294799805, "Satellite Bus Reaction Wheels Four"]
+[1.7279220819473267, 6.8916168212890625, "Communication Device Antenna Diameter 0.7 m"]
+[1.7141231298446655, 6.920090675354004, "Communication Device Antenna Power 2 W"]
+[1.755712866783142, 6.879045486450195, "Communication Device Data Rate 100 Mbit/s"]
+[1.7776768207550049, 6.88034725189209, "Communication Device Data Downlink Intervals 4 hr intervals at each perigee"]
+[2.1071436405181885, 22.66651153564453, "Instrument Measurement Wavelengths 443 nm, 670 nm, 865 nm"]
+[2.476640462875366, 22.74524688720703, "Instrument Spectral Channels Eight"]
+[-0.6979342699050903, 12.404253005981445, "Monitor Purpose Interferometric Monitor for Greenhouse Gases"]
+[5.346901893615723, -4.443570613861084, "Satellite Launch Date November 19, 2016"]
+[1.9720107316970825, -2.173593521118164, "Satellite Orbit Type Geostationary"]
+[0.7192564010620117, -1.2062734365463257, "Satellite Altitude 35,786 km"]
+[0.8747643828392029, -2.0844552516937256, "Satellite Longitude 75\u00ba W"]
+[4.6613335609436035, -2.663086175918579, "Satellite Expected Service Period At least 22 years"]
+[-0.8640137910842896, 0.12903070449829102, "Satellite System Navigation Receiver Manufacturer RUAG Space"]
+[6.340866565704346, 7.404780864715576, "Satellite Component Accuracy Less than one meter"]
+[6.277485370635986, 7.458984375, "Satellite Component Manufacturer Location Vienna, Austria"]
+[-0.8565646409988403, 0.13566505908966064, "Satellite System Mission Objectives Address three critical SBEM gaps: ocean surface vector winds, tropical cyclone intensity, and LEO energetic charged particle characterization"]
+[-13.879278182983398, -2.244408130645752, "X-ray Telescope URL http://arxiv.org/PS_cache/arxiv/pdf/1001/1001.2502v2.pdf"]
+[-3.6650116443634033, 15.481757164001465, "Microwave Radar Instrument Frequency 13.995 GHz"]
+[-3.700535297393799, 15.516650199890137, "Microwave Radar Instrument Antenna Quantity 6"]
+[-3.6889591217041016, 15.50839614868164, "Microwave Radar Instrument Antenna Length 3 m"]
+[-3.660062551498413, 15.48640251159668, "Microwave Radar Instrument Swath Width 600 km"]
+[-3.745877504348755, 15.541569709777832, "Microwave Radar Instrument Gap Width 330 km"]
+[-3.7045583724975586, 15.518518447875977, "Microwave Radar Instrument Wind Speed Accuracy 2 m/s (rms)"]
+[-3.6925129890441895, 15.50336742401123, "Microwave Radar Instrument Wind Direction Accuracy 20\u00ba (rms)"]
+[-3.723623752593994, 15.5315580368042, "Microwave Radar Instrument Resolution 50 km"]
+[-3.7154898643493652, 15.523514747619629, "Microwave Radar Instrument Antenna Polarization 6 V, 2 H"]
+[-3.6824631690979004, 15.510716438293457, "Microwave Radar Instrument Antenna Beam Width 25\u00ba (3 dB broad beam) =0.42\u00ba (3 dB narrow beam)"]
+[-3.6736414432525635, 15.489500999450684, "Microwave Radar Instrument Mass 280 kg"]
+[-3.6480414867401123, 15.483916282653809, "Microwave Radar Instrument Power 240 W"]
+[-3.7129735946655273, 15.49777889251709, "Microwave Radar Instrument Data Rate 3.2 kbit/s"]
+[-3.6927332878112793, 15.5277099609375, "Microwave Radar Instrument Peak Transmit Power 110 W"]
+[-3.667381525039673, 15.480049133300781, "Microwave Radar Instrument Pulse Width 5 ms"]
+[-3.65604305267334, 15.495820045471191, "Microwave Radar Instrument PRF 62 Hz"]
+[11.214268684387207, 5.45587682723999, "CubeSat Mount Qualification Date April 24-25, 2013"]
+[11.29196834564209, 5.503782749176025, "CubeSat Mount Workshop Location Cal Poly State University, San Luis Obispo, CA, USA"]
+[11.256190299987793, 5.484195709228516, "CubeSat Mount URL http://www.cubesat.org/images/stories/workshop_media/DevelopersWorkshop2013/Maly_MoogCSA_ESPA-SUM.pdf"]
+[-1.1996392011642456, 7.502154350280762, "Speaker Presentation Date May 7-10, 2012"]
+[-1.2626687288284302, 7.552556037902832, "Speaker Conference Location El Segundo, CA, USA"]
+[-1.1300139427185059, 7.6199235916137695, "Speaker URL https://web.archive.org/web/20150423114038/http://www.responsivespace.com/Papers/RS2012/SPECIAL%20SPEAKERS/Dr.%20Peter%20Wegner/Dr.%20Peter%20Wegner.pdf"]
+[2.6232638359069824, 14.324209213256836, "Optical Instrument Field of View 24\u00ba x 24\u00ba"]
+[2.6275277137756348, 14.293933868408203, "Optical Instrument Entrance Pupil Diameter 10.5 cm"]
+[2.6304986476898193, 14.28235149383545, "Optical Instrument Focal Ratio f/1.4"]
+[2.635201930999756, 14.337358474731445, "Optical Instrument Wavelength Range 600 - 1000 nm"]
+[2.6197588443756104, 14.3128080368042, "Optical Instrument Ensquared Energy 50% within 15 x 15 \u00b5m"]
+[2.6462600231170654, 14.336167335510254, "Optical Instrument Ensquared Energy 90% within 60 x 60 \u00b5m"]
+[2.6756815910339355, -1.7551742792129517, "Satellite Platform ESPA (EELV Secondary Payload Adapter)"]
+[1.4009848833084106, -3.1140341758728027, "Satellites Type Small and medium free-flying"]
+[-1.8820455074310303, 7.244353771209717, "Platform First Flight Date March 9, 2007"]
+[-3.047846794128418, 4.301617622375488, "Spacecraft Deployment Attached to the ESPA ring"]
+[2.145698070526123, 22.340730667114258, "Instrument High-Temperature Calibration Source Temperature About 340 K"]
+[2.0173869132995605, 22.516334533691406, "Instrument Deep Space Radiant Temperature About 3 K"]
+[2.2113122940063477, 23.146677017211914, "Instrument Frequency Range 6.9-89 GHz"]
+[-5.213582992553711, 7.784929275512695, "Communication System Uplink Data Rate 4 kbit/s"]
+[-5.285104751586914, 7.750334739685059, "Communication System Downlink Data Rate Configurable between 3.5 \u2013 10 kbit/s"]
+[-5.213074207305908, 7.796233177185059, "Communication System Nominal Downlink Data Rate 5 kbit/s"]
+[-5.280317306518555, 7.952971935272217, "Communication System Antenna Type Monopoles with circular polarization"]
+[-5.222149848937988, 7.880004405975342, "Communication System Antenna Quantity 4"]
+[-5.303056240081787, 8.004402160644531, "Communication System Frequency Band UHF (435 MHz)"]
+[-5.248226165771484, 7.87930965423584, "Communication System Communication Protocols ECSS E 70, ECSS- E 41"]
+[-6.719848155975342, 9.988717079162598, "Antenna Center Frequency 5.405 GHz"]
+[-6.743014335632324, 10.01259994506836, "Antenna RF Bandwidth 11.6, 17.3, 30, 50, or 100 MHz"]
+[-6.7505316734313965, 10.005204200744629, "Antenna Transmitter Power (Peak) 1650 W (normal mode), 2280 W (ultra fine mode)"]
+[-6.791191101074219, 10.006444931030273, "Antenna Aperture Size 15 m x 1.37 m"]
+[-6.718714714050293, 9.987512588500977, "Antenna Type 2-D active phased array antenna"]
+[-6.730328559875488, 9.98034381866455, "Antenna Polarization Isolation \u226525 dB"]
+[-6.720291614532471, 9.995805740356445, "Antenna Imaging Mode Delay Time 10 ms"]
+[-6.74160099029541, 10.009161949157715, "Antenna X-band Downlink Margin 9 dB"]
+[-6.719804763793945, 9.982942581176758, "Antenna Data Rate (max) 105 Mbit/s"]
+[-6.723235130310059, 9.992189407348633, "Antenna Mass 750 kg"]
+[-7.396885871887207, 2.8680312633514404, "Cosmic Ray Detector Spectra Hardening Above 200 GV"]
+[-7.389862537384033, 2.8710391521453857, "Cosmic Ray Detector Rigidity Dependence Above 60 GV"]
+[-7.396186351776123, 2.8665637969970703, "Cosmic Ray Detector Boron-to-Carbon Ratio Study Conducted"]
+[-7.39239501953125, 2.871397018432617, "Cosmic Ray Detector Dark Matter Particles Possibility of Arising from"]
+[-2.772881507873535, 14.182303428649902, "Sounder Observation Modes China area mode, Mesoscale mode"]
+[-2.781940460205078, 14.193202018737793, "Sounder Temporal Resolution 55 minutes (China area mode), 30 minutes (Mesoscale mode)"]
+[-2.788529396057129, 14.198185920715332, "Sounder Coverage 4500 x 4500 km (China area mode), 1000 x 1000 km (Mesoscale mode)"]
+[-2.771599054336548, 14.186634063720703, "Sounder Detector Arrays 538 TIR channels and 375 MWIR channels"]
+[-2.778740167617798, 14.188913345336914, "Sounder Data Quantization 13 bit"]
+[-2.7835774421691895, 14.187322616577148, "Sounder Focal Plane Temperature Constantly low temperature"]
+[1.383882999420166, -1.886766791343689, "Satellite Pointing Stability 0.5 arcseconds RMS"]
+[4.200850486755371, -2.8031067848205566, "Satellite Observation Period 20 minutes"]
+[1.8439172506332397, -2.170379400253296, "Satellite Repeatability Stars positioned on the same pixels on each orbit"]
+[2.4487695693969727, -1.546857237815857, "Satellite Function Study exoplanets via the transit method"]
+[1.7965525388717651, -1.521746277809143, "Satellite X-ray Emission Brightness At least 10 times brighter than normal"]
+[2.741476058959961, -1.4134206771850586, "Satellite Follow-up Studies Performed quick follow-up studies"]
+[-0.8278154730796814, 3.0701990127563477, "Neutron Stars Radio Waves Can emit steady beams of radio waves"]
+[-0.7628405094146729, 3.148371458053589, "Neutron Stars Gamma Rays Have been known to release great bursts of gamma rays"]
+[-0.7328764200210571, 3.1203863620758057, "Neutron Stars X-rays Can emit X-rays"]
+[-2.976850748062134, 20.118452072143555, "Spectral Filter Assembly Number of Bands 10"]
+[-3.0236287117004395, 20.199155807495117, "Spectral Filter Assembly Wavelength Range 443 nm to 945 nm"]
+[-2.964171886444092, 20.16162109375, "Spectral Filter Assembly Number of Bands 3"]
+[-3.0070531368255615, 20.08807373046875, "Spectral Filter Assembly Wavelength Range 1375 nm to 2190 nm"]
+[-3.013277530670166, 20.170698165893555, "Spectral Bands Sampling 10 m bands"]
+[-0.8404382467269897, 11.594286918640137, "Detector Material HgCdTe"]
+[-0.8376903533935547, 11.616475105285645, "Detector Number of Bands 3"]
+[-2.9752414226531982, 20.095186233520508, "Spectral Bands Operation Mode TDI mode"]
+[1.3609950542449951, 10.605926513671875, "Imaging System Modulation Transfer Function (MTF) 9-10% at Nyquist"]
+[1.3667529821395874, 10.548487663269043, "Imaging System Signal-to-Noise Ratio >120 at a 15-degree sun elevation angle for a 15% reflective object"]
+[1.3597649335861206, 10.541495323181152, "Imaging System Positional Accuracy 5-meter CE90 for each individual image"]
+[1.3576587438583374, 10.550426483154297, "Imaging System Positional Accuracy 1-meter CE90 when suitable elevation data is available"]
+[-3.8439781665802, 3.7453572750091553, "Rover Launch Date July"]
+[-3.8549787998199463, 3.7144370079040527, "Rover Sampling System Coring drill and sample tubes"]
+[-3.86017107963562, 3.710181713104248, "Rover Sample Collection Method Cache rock and regolith samples in its collection tubes"]
+[-3.8526110649108887, 3.7206807136535645, "Rover Function Collect and deliver samples to Mars Ascent Vehicle"]
+[-3.174907922744751, 5.344998359680176, "Vehicle Function Launch the samples into orbit around Mars"]
+[-0.74982088804245, 1.4602813720703125, "Orbiter Function Rendezvous with the samples in orbit around Mars and take them in a highly secure containment capsule for return to Earth"]
+[3.1331703662872314, -1.9513367414474487, "Satellite Operational Status On all the time"]
+[4.096292495727539, 13.895694732666016, "Laser Altimeter Surface Elevation Measurement Unknown"]
+[4.095820426940918, 13.931012153625488, "Laser Altimeter Snow and Ice Thickness Measurement Unknown"]
+[4.0999884605407715, 13.936320304870605, "Laser Altimeter Sub-ice-shelf Bathymetry Measurement Unknown"]
+[-8.137645721435547, 8.826943397521973, "Electric Power Subsystem Solar Arrays Quantity 3"]
+[-8.137161254882812, 8.827203750610352, "Electric Power Subsystem Battery Packs Quantity 3"]
+[-2.6072936058044434, 9.625470161437988, "Power Source Power Output > 330 W"]
+[-3.721442937850952, 8.293900489807129, "Energy Storage Device Depth of Discharge Not exceed 20%"]
+[-3.6626017093658447, 8.309589385986328, "Energy Storage Device Lifetime 5 years"]
+[-3.6426267623901367, 8.359793663024902, "Energy Storage Device Nominal Capacity 14.4 Ah"]
+[-0.4373460114002228, 0.2173352986574173, "Satellite Navigation System Interferometry Concept Employed for orbit determination"]
+[-0.4077131152153015, 7.018760681152344, "Technique Advantages Time synchronization problem between the stations is effectively solved by using the same source of time and frequency; The transmission media errors included troposphere, ionosphere and solar plasma are approximately the same between the two tracking stations"]
+[0.4580361247062683, 9.369796752929688, "Attitude Control System Components Momentum wheel, horizon scanner, magnetic coils"]
+[1.1496814489364624, -0.8453068137168884, "Satellite Diameter 76 cm"]
+[1.1413941383361816, -0.9430053234100342, "Satellite Height 122 cm"]
+[1.0100258588790894, -4.376229763031006, "Satellite Mass 104 kg"]
+[-1.4280312061309814, 7.065216541290283, "Simulation Model Characteristics High luminosity and directed beams of photons"]
+[-1.5414032936096191, 7.002997875213623, "Simulation Model Photon Flow Direction At a right angle to the polar beams expected in a standard pulsar model"]
+[-3.084867238998413, 2.0435948371887207, "Space Mission Resolution of High-Energy X-ray Background 2 percent to 35 percent"]
+[-3.0928092002868652, 2.020777463912964, "Space Mission Principal Investigator Fiona Harrison"]
+[-3.1013669967651367, 1.9864611625671387, "Space Mission Resolution of High-Energy X-ray Background 35 percent"]
+[11.212810516357422, 5.469871997833252, "CubeSat Inflation System High torsion springs"]
+[11.25317096710205, 5.489606857299805, "CubeSat Inflatable Structure Shape Octahedron tensegrity"]
+[11.410747528076172, 5.6214799880981445, "CubeSat Gas Volume Minimal"]
+[11.3250093460083, 5.545317649841309, "CubeSat Sail Material Surface Area Reduction 25%"]
+[-3.590625762939453, 4.396444320678711, "Spacecraft Capture Date 17 Dec. 2017"]
+[-3.218677043914795, 4.306286811828613, "Spacecraft Capture Time 5:57 a.m. EST"]
+[-3.031975030899048, 4.232981204986572, "Spacecraft Distance from Space Station 10 meters"]
+[2.6515421867370605, 13.443777084350586, "Optical Component Function Reflects the beam towards the focal plane"]
+[1.9103530645370483, 10.718390464782715, "Imaging Device Function Captures images"]
+[2.6456069946289062, 13.462855339050293, "Optical Component Function Directs pointing maneuvers to the desired solar targets"]
+[0.34189292788505554, 9.205121040344238, "Stabilization System Function Provides jitter removal to < 0.1 arcsec rms"]
+[2.0089852809906006, -2.659487009048462, "Satellite Exoplanet Candidates 5000"]
+[-2.1779849529266357, 2.902406930923462, "Observatory Newly-Found Planets Unknown"]
+[-1.28871488571167, 6.178310394287109, "Organization News Date 2 December 2021"]
+[2.603545665740967, 14.264514923095703, "Optical Instrument Size 79 mm x 69 mm x 15 mm"]
+[2.669829845428467, 14.308343887329102, "Optical Instrument Mass Less than 120 g"]
+[2.623548984527588, 14.310161590576172, "Optical Instrument Power Consumption ~ 1.5 W"]
+[0.4721805453300476, 12.016097068786621, "Temperature Transducer Output Current proportional to the absolute temperature"]
+[2.6623754501342773, 13.608454704284668, "Fiber Bragg Gratings Quantity 2"]
+[2.648402452468872, 13.674237251281738, "Fiber Bragg Gratings Mounting Steel mounting with a cantilever"]
+[-0.03283041715621948, 9.333175659179688, "Pointing System Azimuth Rotation Speed Varies"]
+[1.5163692235946655, -2.1344852447509766, "Satellite Pointing Stability Required"]
+[-0.922844409942627, 6.428665637969971, "Author Documentation Observation of the Earth and Its Environment: Survey of Missions and Sensors"]
+[-0.8377047181129456, 6.132070541381836, "Website Contact Email eoportal@symbios.space"]
+[1.5201215744018555, 2.5219788551330566, "Geostationary Meteorological Satellite Number of Satellites 7"]
+[1.5275051593780518, 2.5101921558380127, "Geostationary Meteorological Satellite Operational Satellites 3"]
+[1.5159863233566284, 2.5137476921081543, "Geostationary Meteorological Satellite Mission Objectives Imagery, sounding, lightning mapping, and space environment monitoring"]
+[-3.643700122833252, 12.76180362701416, "Particle Detector Measurement Electron flux and positron flux"]
+[-3.6176676750183105, 12.750645637512207, "Particle Detector Energy Range 0.5 to 200 GeV"]
+[-3.6410951614379883, 12.76236629486084, "Particle Detector Flux Behavior Increases, levels out, increases again, tendency to decrease"]
+[-3.2553114891052246, 5.420533657073975, "Launch Vehicle Next Launch Schedule Q1 2021"]
+[-3.237338066101074, 5.434395790100098, "Launch Vehicle Return to Flight Schedule End Q1 2021"]
+[-3.287550449371338, 5.454096794128418, "Launch Vehicle Quality and Competitiveness On the market"]
+[-3.2270758152008057, 5.373389720916748, "Launch Vehicle Autonomy of Access to Space Europe"]
+[3.096236228942871, 22.812957763671875, "Instrument Mission Status Complete"]
+[3.7025256156921387, 22.97024154663086, "Instrument Launch Date 25 June 2019"]
+[3.6477320194244385, 22.963403701782227, "Instrument End of Life Date 31 May 2021"]
+[2.2092247009277344, -1.950323462486267, "Satellite Structural Thermal Model -"]
+[-1.3648364543914795, 13.16909122467041, "Solar Wind Concentrator Component Diameter 73 cm"]
+[-1.348487138748169, 13.147747039794922, "Solar Wind Concentrator Component Collecting Area 3500 cm2"]
+[-1.332464337348938, 13.143942832946777, "Solar Wind Concentrator Component Number of Wafers 55"]
+[-1.3464467525482178, 13.173558235168457, "Solar Wind Concentrator Component Wafer Material Silicon, aluminum, gold foils"]
+[-1.3401042222976685, 13.133376121520996, "Solar Wind Concentrator Component Wafer Thickness 0.5 mm"]
+[-1.3622174263000488, 13.145794868469238, "Solar Wind Concentrator Component Wafer Shape 10 cm (point-to-point) hexagonal"]
+[-1.3426364660263062, 13.151034355163574, "Solar Wind Concentrator Component Temperature < 200 K"]
+[-2.877579689025879, 3.892162561416626, "Sample Return Capsule Developer Lockheed Martin Astronautics"]
+[2.9104363918304443, 22.432212829589844, "Instrument Developer Los Alamos National Laboratory"]
+[2.7541749477386475, 22.415781021118164, "Instrument Cleanroom Class Class 10"]
+[-3.090625762939453, 2.438145160675049, "Mission Principal Investigator Donald Burnett"]
+[-3.10854172706604, 2.386688709259033, "Mission Science Co-Investigators Approximately 18"]
+[2.8193976879119873, -1.9538105726242065, "Satellite Sea Surface Salinity Measurement Unknown"]
+[-0.7836359739303589, 8.859258651733398, "Thermal Control System Design Changes Address thermal control issues detected on GOES-16 and -17"]
+[2.8292031288146973, 22.552532196044922, "Instrument Parts Issues Required the GOES-R Program to re-plan the GOES-T schedule"]
+[5.200113773345947, -4.3310747146606445, "Satellite Launch Date December 2021"]
+[1.5382698774337769, 2.4726781845092773, "Geostationary Weather Satellite Purpose Provide faster, more accurate data for tracking lightning, storm systems, wildfires, dense fog and other hazards"]
+[-1.3229347467422485, 9.180365562438965, "Engine Propellant Xenon"]
+[-1.3582309484481812, 9.190631866455078, "Engine Thrust 11.5~17mN"]
+[-1.400286316871643, 9.265337944030762, "Engine Mass Flow Rate 10.5 cm3/s"]
+[-1.3710805177688599, 9.246397018432617, "Engine Instrument Mass 43 kg"]
+[-1.3637419939041138, 9.227285385131836, "Engine Power Consumption <403 W @ 11.5 mN, <580W @ 17 mN"]
+[-1.3483469486236572, 9.20473861694336, "Engine Signal Interface RS422"]
+[-1.3788504600524902, 9.19576358795166, "Engine Propellant Mass 12 kg"]
+[-1.3414912223815918, 9.16606330871582, "Engine MEOP 15 MPa"]
+[-1.3551164865493774, 9.198933601379395, "Engine Proof Pressure >1.5 x MEOP"]
+[-1.3282698392868042, 9.218828201293945, "Engine Burst Pressure 2.0(tank), 2.5(valve), 4.0(tube etc.) x MEOP"]
+[-1.4023691415786743, 9.266637802124023, "Engine Leakage internal: <0.5 Pa m3/h(Ghe), external: <1x10 -7 Pa m3/s(Ghe)"]
+[5.0982255935668945, -4.3442583084106445, "Satellite Mission Date July 23-27, 2007"]
+[2.576514959335327, -3.917508125305176, "Satellite URL http://www.earthobservations.org/documents/cop/ag_gams/200707_01/gmes_sentinel2.pdf"]
+[-5.388034343719482, 2.777008533477783, "Telescope Aperture Diameter 80 mm"]
+[-5.422028541564941, 2.75638484954834, "Telescope Spatial Resolution 6 m"]
+[-5.393933296203613, 2.7849643230438232, "Telescope Field of View Up to 10 km"]
+[-5.384085655212402, 2.832581043243408, "Telescope Instrument Size (Folded) 100 mm x 100 mm x 60 mm"]
+[-5.383147716522217, 2.775334358215332, "Telescope Instrument Size (Unfolded) 100 mm x 100 mm x 210 mm"]
+[-5.372131824493408, 2.7898197174072266, "Telescope Instrument Mass < 0.5 kg"]
+[-5.393737316131592, 2.770204544067383, "Telescope Instrument Power < 0.5 W"]
+[-5.220269203186035, 7.835667610168457, "Communication System Antenna Size 11.3 m"]
+[-5.068794250488281, 8.042989730834961, "Communication System Components S-band transmitter feed, S-band receiver feed, X-band receiver feed, tracking system"]
+[2.5730690956115723, -1.2076743841171265, "Satellite Detector Type Absorption"]
+[5.005504608154297, -4.31095552444458, "Satellite Observation Date 2013 and 2014"]
+[2.4165682792663574, -1.4036235809326172, "Satellite Data Representation Orange circles"]
+[2.3996245861053467, -1.4519301652908325, "Satellite Data Representation Blue squares"]
+[-1.1746273040771484, 3.065985918045044, "Celestial Object Light Baseline Gray line"]
+[-1.5160547494888306, 16.90464973449707, "Altimeter Frequency 13.65 GHz"]
+[-1.50070321559906, 16.898544311523438, "Altimeter Measurement Accuracy 2.5 cm"]
+[-1.4957008361816406, 16.886985778808594, "Altimeter Mass 24 kg"]
+[-1.49203360080719, 16.884422302246094, "Altimeter Power 49W"]
+[1.9653325080871582, -1.6686687469482422, "Satellite Sound Impact 140 decibels (dB)"]
+[0.6034705638885498, -1.4589734077453613, "Satellite Orbit Altitude Around 500 km"]
+[0.7047144174575806, -1.4615191221237183, "Satellite Orbit Distance 220 km"]
+[-3.2394564151763916, 14.582596778869629, "Interferometric Synthetic Aperture Microwave Imager Component Unknown Unknown"]
+[-1.870412826538086, 14.843121528625488, "Radiometer Application Ocean salinity observation"]
+[-0.48076125979423523, 5.84005069732666, "Unknown Sea Surface Salinity Retrieval Unknown"]
+[0.5668371915817261, -1.5050363540649414, "Satellite Orbit Altitude 681 km"]
+[4.833302021026611, -2.4348304271698, "Satellite Mission Life 7 years"]
+[0.9375942945480347, -4.354269027709961, "Satellite Spacecraft Mass ~2000 kg"]
+[1.054262638092041, -1.4418824911117554, "Satellite GSD (Ground Sample Distance) 0.41 m (Pan) 1.65 m (MS)"]
+[1.0466697216033936, -1.378116488456726, "Satellite Swath Width 14.4 km"]
+[2.638354539871216, -2.639524221420288, "Satellite Data Rate 740 Mbit/s"]
+[11.200488090515137, 5.387515068054199, "CubeSat Deployer Quantity 9"]
+[11.20488452911377, 5.395776271820068, "CubeSat Deployer Quantity 3"]
+[11.217698097229004, 5.372261047363281, "CubeSat Deployer Quantity 2"]
+[11.101595878601074, 5.324494361877441, "CubeSat Deployer Quantity 1"]
+[-0.5329217314720154, 1.231323003768921, "Satellite Orbit Altitude 600 km"]
+[-0.5319193601608276, 1.232245922088623, "Satellite Orbit Inclination 97.8o"]
+[-0.5325610637664795, 1.2352908849716187, "Satellite Orbit LTDN 10:30 hours"]
+[3.1122140884399414, -1.865478754043579, "Satellite Mission Status Operating quite well"]
+[0.5366685390472412, 9.42158031463623, "Attitude Determination and Control System Status Nominal operation"]
+[-4.435091018676758, 12.132537841796875, "Magnetic Sensors Status Providing science data"]
+[2.1197354793548584, -0.9022656679153442, "Satellite Sensor Beam Modes 450 km wide ship detection optimized beam mode in the HH polarization channel, and a 530 km wide multi-purpose beam mode in the HH and HV polarization channels"]
+[-1.8900471925735474, 6.902693271636963, "Software Output Statistically probable Minimum Detectable Ship Length (MDSL) metric at a 90% confidence level"]
+[-1.8875340223312378, 6.8758864402771, "Software Input Relevant characteristics of a proposed SAR beam mode"]
+[-3.047746181488037, 4.283254146575928, "Spacecraft Platform BCP (Ball Configurable Platform)"]
+[-3.3275394439697266, 4.477461814880371, "Space Vehicle Launch Date January 2024"]
+[-3.207000494003296, 4.756860733032227, "Space Vehicle Launch Vehicle SpaceX Falcon 9"]
+[-3.183398962020874, 4.415792942047119, "Space Vehicle Orbit Sunsynchronous orbit, LEO"]
+[0.6979395151138306, 12.03928279876709, "Sensor Type Microwave Imager"]
+[-1.2134463787078857, 15.064009666442871, "Imaging multi-spectral radiometers (vis/IR) Measurement Domain Ocean, Land"]
+[-1.1939842700958252, 15.043811798095703, "Imaging multi-spectral radiometers (vis/IR) Measurement Domain Ocean, Land"]
+[0.39418455958366394, 12.054039001464844, "Lightning sensors Measurement Domain Atmosphere"]
+[-2.577216625213623, 4.1404008865356445, "Space environment Measurement Domain Gravity and Magnetic Fields"]
+[2.4531314373016357, 23.16619873046875, "Airborne Instrument Frequency L- and S-band"]
+[2.228508234024048, 23.158491134643555, "Instrument Frequency 1.4 GHz"]
+[1.6816034317016602, 22.017663955688477, "Instrument Footprint Diameter 124 km"]
+[-1.2647078037261963, 15.051652908325195, "Imaging Multispectral Radiometer Objective Detect high temperature thermal events (HTE) such as biomass burning and volcanic ash regions"]
+[16.626562118530273, 6.964343070983887, "Earth Observation minisatellite Manufacturer MBRSC (Mohammed Bin Rashid Space Center)"]
+[16.856618881225586, 6.849612236022949, "Philippine EO microsatellite Manufacturer Philippine DOST (Department of Science and Technology)"]
+[16.813486099243164, 6.878224849700928, "Technology demonstration microsatellite Mass 50 kg"]
+[11.397335052490234, 5.566815376281738, "CubeSat technology demonstration Manufacturer Aichi University of Technology, Japan"]
+[16.697608947753906, 6.921388149261475, "Technology demonstration minisatellite Mass 220 kg"]
+[-2.6508777141571045, 9.554301261901855, "Power Source Voltage High-voltage"]
+[1.2594879865646362, -2.116328477859497, "Satellite Plasma Density 109 to 1012 m-3"]
+[-2.6439294815063477, 9.586822509765625, "Power Source Potential Most negative potential"]
+[2.974677085876465, -1.9641114473342896, "Satellite Development Status Unknown"]
+[3.0798351764678955, -2.323533296585083, "Satellite Launch Date Unknown"]
+[2.655850648880005, 14.29019546508789, "Optical Instrument Orbital Altitude ~ 700 km"]
+[2.6231422424316406, 14.288761138916016, "Optical Instrument Photon Number Calculation Source radiance and its duration, the characteristics of the optics and the filter and the distance from the source to the satellite"]
+[1.8620083332061768, 10.68163776397705, "Imaging Device Quantum Efficiency Parameter Value"]
+[2.300968885421753, 22.659772872924805, "Instrument Spectral Regions Thermal infrared region (TIR), water vapour absorption bands (WV), and in the visible range (VIS)"]
+[2.0376179218292236, 22.581832885742188, "Instrument Spectral Range VIS 0.5 - 0.9 \u00b5m"]
+[2.030566930770874, 22.609018325805664, "Instrument Spectral Range WV 5.7 - 7.1 \u00b5m"]
+[2.048815965652466, 22.4754581451416, "Instrument Spectral Range TIR 10.5 - 12.5 \u00b5m"]
+[2.2047970294952393, 22.316829681396484, "Instrument Field of View (FOV) 18\u00b0"]
+[2.1983137130737305, 22.28882598876953, "Instrument IFOV (Instantaneous FOV) VIS 0.065 mrad"]
+[2.220775604248047, 22.382600784301758, "Instrument IFOV (Instantaneous FOV) WV and TIR 0.14 mrad"]
+[1.7791831493377686, 22.11614227294922, "Instrument Spatial Resolution at Nadir VIS 2.5 km"]
+[1.7972787618637085, 22.109766006469727, "Instrument Spatial Resolution at Nadir WV and TIR 5 km"]
+[2.1521215438842773, 22.66900634765625, "Instrument Time Standard Synchronisation Accuracy One nanosecond"]
+[1.972859501838684, 22.282772064208984, "Instrument Orbital Distance Measurement Accuracy Within 0.1 m"]
+[1.8443342447280884, 22.6987361907959, "Instrument Energy Range 42.9 - 300 KeV"]
+[2.1363775730133057, 22.512001037597656, "Instrument High Temporal Resolution 500 - 600 second averages"]
+[2.204956293106079, 22.576717376708984, "Instrument Low Temporal Resolution 30 minute averages"]
+[-4.482799053192139, 12.15013599395752, "Three-axis magnetometer sensor Principle Magneto-inductive"]
+[-4.491921424865723, 12.120955467224121, "Three-axis magnetometer sensor Sampling Coordination With pulsing by the magnetorquers"]
+[-4.493542194366455, 12.131157875061035, "Three-axis magnetometer sensor DC Measurements Uncertainty 14 nT"]
+[-4.493733882904053, 12.140743255615234, "Three-axis magnetometer sensor DC Measurements Uncertainty 0.05% of the field in CuPID's orbit"]
+[-4.488104343414307, 12.132009506225586, "Three-axis magnetometer sensor Calibration Process Subtracted off from the DC measurements"]
+[3.6424458026885986, 22.947534561157227, "Instrument Imaging Date Jan. 13, 2015"]
+[3.6923630237579346, 22.923847198486328, "Instrument Imaging Date Jan. 14, 2015"]
+[3.6942341327667236, 22.962656021118164, "Instrument First Image Date July 25, 2014"]
+[3.691408634185791, 22.951610565185547, "Instrument Imaging Date July 25, 2014"]
+[2.38873553276062, -2.073732852935791, "Satellite Subsystems Around 1400"]
+[2.1318538188934326, -2.4908628463745117, "Satellite Processors 300"]
+[-1.3475202322006226, 8.597094535827637, "Electronic Component Source Indigenous"]
+[-1.3212761878967285, 8.61934757232666, "Electronic Component Source Indigenous"]
+[-1.3266985416412354, 8.609628677368164, "Electronic Component Source Indigenous"]
+[-2.62274169921875, 9.336041450500488, "Power Supply Source Indigenous"]
+[-6.689495086669922, 9.957010269165039, "Antenna Source Indigenous"]
+[0.49657297134399414, 9.427844047546387, "Attitude Determination System Primary Attitude Determination Method"]
+[0.499117374420166, 9.455204010009766, "Attitude Determination System Redundant Attitude Determination Method"]
+[0.5107321739196777, 9.456602096557617, "Attitude Determination System Redundant Attitude Determination Method"]
+[0.5054567456245422, 9.358040809631348, "Attitude Control Control Authority Mechanism Baseline three axis control authority mechanism at all altitudes"]
+[0.49961057305336, 9.367409706115723, "Attitude Control Control Authority Mechanism Primary control authority and reaction wheel desaturation at low orbital altitudes"]
+[8.956947326660156, 8.512319564819336, "Satellite Payload Introduction Date 1992"]
+[5.332357406616211, -4.460043430328369, "Satellite Launch Date July 9, 1992"]
+[5.277029037475586, -4.510875225067139, "Satellite Launch Date Aug. 28, 2002"]
+[5.103419303894043, -4.5736985206604, "Satellite Operational Service Start Date Jan. 29, 2004"]
+[16.944387435913086, 6.777693748474121, "Microsatellite Deployment Orbit Altitude ~630 km"]
+[16.900278091430664, 6.8296685218811035, "Microsatellite Deployment Orbit Inclination 97.9\u00ba"]
+[16.893564224243164, 6.823507308959961, "Microsatellite LSDN 12:00 hours \u00b1 15 min"]
+[16.89596176147461, 6.827315807342529, "Microsatellite IOC Operation Period Altitude 250 km"]
+[16.865402221679688, 6.851199150085449, "Microsatellite IOC Operation Period LSDN 16:00 hours"]
+[3.1735830307006836, -1.5823149681091309, "Satellite Mission Lead MIT"]
+[2.895693063735962, -1.838836669921875, "Satellite Managed By NASA's Goddard Space Flight Center"]
+[2.4014506340026855, -1.2640715837478638, "Satellite Monitoring Method Capturing changes in stellar brightness"]
+[-0.34940314292907715, 3.7534940242767334, "Planet Size Jupiter-size"]
+[-0.3853827118873596, 3.779987096786499, "Planet Orbit Period 34 hours"]
+[1.1933262348175049, -4.028199672698975, "Satellite Alloy Density Close to 10,000 kg/m3"]
+[-0.34687554836273193, 8.185111999511719, "Materials Density 9,870 kg/m3, 9,900 kg/m3, 9,860 kg/m3"]
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+[-0.3641631603240967, 8.191661834716797, "Material Main Metal Percentage 45%"]
+[-0.3520517945289612, 8.196480751037598, "Material Main Metal Percentage 74%"]
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+[-0.3179778456687927, 8.150839805603027, "Material Composition 13% W"]
+[-0.28113752603530884, 8.11872673034668, "Material Composition 5% Mo and 11 W"]
+[3.705878734588623, 17.673429489135742, "Payload Launch Date January 10, 2015"]
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+[-3.373873710632324, 7.486956596374512, "Data Processing Processed Images Level 1 image, ortho-image, pan-sharpen image and DSM (Digital Surface Model)"]
+[0.45573925971984863, 9.369720458984375, "Attitude Control System Reaction Wheels 3-axis"]
+[-4.5847392082214355, -3.122016429901123, "Exoplanet Orbital Period 36 days"]
+[-4.560815811157227, -3.088585615158081, "Exoplanet Surface Temperature Around 300 degrees Fahrenheit (150\u00baC)"]
+[-4.565189361572266, -3.0784201622009277, "Exoplanet Size About three times the size of Earth"]
+[-4.519822597503662, -3.040977716445923, "Exoplanet Mass 23 times as massive as the Earth"]
+[2.9256086349487305, 22.71375274658203, "Instrument Package Unknown Unknown"]
+[4.868738174438477, -3.3538708686828613, "Satellite Operational Period Until December 1987"]
+[2.8366129398345947, -2.4813153743743896, "Satellite Frequency 121.5 MHz"]
+[2.8037972450256348, -2.47102952003479, "Satellite Frequency 406 MHz"]
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+[5.26052188873291, -4.432025909423828, "Navigational Satellite Launch Date June 30, 1982"]
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+[2.8224735260009766, -1.0728600025177002, "Satellite Purpose Forest Monitoring"]
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+[-0.7725278735160828, 8.800641059875488, "Thermal Protection System Temperature 2200\u00ba C"]
+[-2.8228468894958496, 3.8523075580596924, "Capsule Speed 32,000 km/h"]
+[-0.6062846183776855, 8.635290145874023, "Heat Shield Material Interlaminar Strength Relatively low"]
+[-0.3472713232040405, 8.158088684082031, "Material Production Method Woven using a newly developed version of a \"Jacquard loom\""]
+[-2.2787463665008545, 7.404012203216553, "On-Board Computer Functions Sensor electronics, command processing, telemetry and housekeeping, attitude and orbit control, thermal management"]
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+[0.6757581233978271, 12.253181457519531, "Light Sensor Number of Sensors 8"]
+[0.775419294834137, 12.235272407531738, "Light Sensor Group Organization 2 groups of 4 sensors"]
+[0.6984908580780029, 12.270734786987305, "Light Sensor Circle Radii 42 and 52 mm"]
+[0.7404292225837708, 12.294492721557617, "Light Sensor Measurement Principle Light received by this sensor evolves nearly linearly with the distance with the full umbra"]
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+[-2.5876312255859375, 9.680365562438965, "Energy Source Installation Date 20 June 2021"]
+[-2.573483943939209, 9.716700553894043, "Energy Source Unfurling Date 20 June 2021"]
+[-2.584662675857544, 9.675597190856934, "Energy Source Installation Date 16 June 2021"]
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+[-1.7464889287948608, 8.840007781982422, "Control System Number of Orbit Control Thrusters 2"]
+[-0.42561376094818115, 8.669259071350098, "Actuators Number 3"]
+[-1.6653937101364136, 11.22815990447998, "Lidar Application Determination of Local Slope on the Greenland Ice Sheet"]
+[-3.0908682346343994, 2.436398983001709, "Mission Date 12 Dec. 2017"]
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+[-2.0030529499053955, 8.057089805603027, "Service Themes Sealed soil (imperviousness), tree cover density, forest type, and grasslands"]
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+[4.124394416809082, -3.0091421604156494, "Satellite Local Equator Crossing Time 22:30 hours"]
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+[-3.153930902481079, 2.092196226119995, "Commercial Resupply Service Mission Launch Date 5 December 2018"]
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+[-5.267747402191162, 7.943717002868652, "Communication System Uplink Frequency Unknown"]
+[-5.289180755615234, 7.88789176940918, "Communication System Message Length Unknown"]
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+[-2.311889171600342, 5.066551685333252, "Debris \u0394V (cm/s) 2.0"]
+[-2.3377926349639893, 5.047898769378662, "Debris \u0394V (cm/s) 2.68/2.68"]
+[-2.3200690746307373, 5.062533855438232, "Debris \u0394V (cm/s) 0.39"]
+[-2.3299782276153564, 5.066682815551758, "Debris \u0394V (cm/s) 0.92"]
+[-2.294861078262329, 5.060243606567383, "Debris \u0394V (cm/s) 1.80"]
+[-2.3192248344421387, 5.071413993835449, "Debris \u0394V (cm/s) 0.71"]
+[-2.321476936340332, 5.059957504272461, "Debris \u0394V (cm/s) 0.67"]
+[5.341305732727051, -4.340409755706787, "Satellite Launch Date November 2014"]
+[3.034451961517334, -1.609460711479187, "Satellite Agency NEC Corporation and the Institute for Unmanned Space Experiment Free Flyer (USEF)"]
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+[-0.42978355288505554, 6.764435768127441, "Test Equipment Purpose Integrates the P/L Flight units on the flight Optical Bench"]
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+[0.6234945058822632, 12.041831016540527, "Sensor Tracked Gases Atmospheric carbon dioxide, carbon monoxide and methane"]
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+[-0.5573041439056396, 8.362860679626465, "Ice Shelf Thinning Rate About 16 feet (5 meters) per year"]
+[-0.6146298050880432, 8.40768051147461, "Ice Shelf Thinning Rate About 10 feet (3 meters) per year"]
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+[2.8825716972351074, -1.7874804735183716, "Satellite Design Special"]
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+[-9.911750793457031, 7.3986310958862305, "Mirror Distance to M4 10 \u00b5m"]
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+[-9.912059783935547, 7.3982462882995605, "Mirror Distance to Focal Plane 10 \u00b5m"]
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+[-9.899998664855957, 7.386079788208008, "Mirror Distance to Focal Plane 10 \u00b5m"]
+[-9.90627384185791, 7.393166542053223, "Mirror Tilt 100 \u00b5rad"]
+[-1.0006020069122314, 7.775060176849365, "Device Tilt 87 \u00b5rad"]
+[-0.3388284146785736, 8.173908233642578, "Material CTE Coefficient of Thermal Expansion"]
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+[3.3182411193847656, 0.4646337032318115, "Satellite Program Unknown Unknown"]
+[-3.143653154373169, 1.7409613132476807, "Satellite Mission Unknown Unknown"]
+[-1.3004869222640991, 4.433897972106934, "Ground Equipment Location On the ground"]
+[-1.2880717515945435, 4.4132981300354, "Ground Equipment Performance Degradation Small enough for a useful disaster support"]
+[-1.3197680711746216, 4.417437553405762, "Ground Equipment Frequency Bandwidth Smoothly increased as expected"]
+[-1.3089702129364014, 4.418308734893799, "Ground Equipment Accommodated Number of Users Increased in a disaster scenario"]
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+[-1.9098055362701416, 6.881728172302246, "Software Function Calculate attitude state vector"]
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+[-0.7867138385772705, 11.646942138671875, "Detector Readout Noise 130 \u00b5V rms"]
+[-0.8604323267936707, 11.652746200561523, "Detector Sample Rate 4.8MHz"]
+[-0.80741947889328, 11.637906074523926, "Detector Sensitivity Adjustment Through CVF (Charge to Voltage conversion Factor)"]
+[-0.8245164155960083, 11.605335235595703, "Detector Straylight Rejection High"]
+[6.172589302062988, 7.563374996185303, "Satellite Components Quantity 8"]
+[-1.3340799808502197, 6.279266357421875, "Team Members Quantity 21"]
+[-1.3379802703857422, 6.280943870544434, "Team Members Quantity 13"]
+[-1.014249563217163, 6.452329158782959, "Document Levels Spacecraft, Subsystem and Unit level"]
+[-1.135596752166748, 6.599409580230713, "Technical Requirement Document Level Spacecraft Level"]
+[-0.761465311050415, 8.631050109863281, "Cooler Temperature Achieves temperatures needed for IR detectors"]
+[-0.13905291259288788, 9.24600887298584, "Pointing Function Function Detects cloud-free areas and repoints scanner in real time"]
+[2.6731884479522705, 22.392940521240234, "Instrument Stability Highly accurate and stable"]
+[0.22301752865314484, 13.787259101867676, "Calibration Target Emissivity >995%"]
+[0.2297138273715973, 13.780652046203613, "Calibration Target Temperature Errors <100 mK"]
+[2.328158140182495, 22.666236877441406, "Instrument Performance Stable scanner performance over life"]
+[2.7064785957336426, 22.293954849243164, "Instrument Observation Types DAY, LIM, NI1, OCC"]
+[3.7265641689300537, 22.999122619628906, "Instrument Launch Date 25 January 2018"]
+[3.7111146450042725, 22.971752166748047, "Instrument Geostationary Orbit Reach Date June 2018"]
+[3.6532607078552246, 22.96939468383789, "Instrument Commissioning Period 4 September to early October"]
+[2.847411870956421, 22.95395851135254, "Instrument Planned Science Mission Duration Two years"]
+[5.391283988952637, -4.390915393829346, "Satellite Launch Date April 2018"]
+[4.559605598449707, -2.5992634296417236, "Satellite Sky Survey Time 2 years"]
+[4.328521251678467, -2.6672792434692383, "Satellite Sector Data Collection Time 27 days"]
+[-0.40566015243530273, 16.21225929260254, "Spectrograph Location Chile"]
+[-0.40917104482650757, 16.217613220214844, "Spectrograph Purpose Identifies exoplanets by their gravitational tug on their host stars"]
+[2.346263885498047, 11.914458274841309, "Operational Mode Energy Balance Positive"]
+[-1.0433470010757446, 7.740660667419434, "Device Mode Sun Point"]
+[-1.0659338235855103, 7.737629413604736, "Device Mode Cyclic on/off cycle"]
+[2.432495594024658, 11.982540130615234, "Operational Mode Energy Consumption More than Safe Mode"]
+[1.6849069595336914, 6.954887390136719, "Communication Device Number of Channels 2"]
+[1.7617599964141846, 6.8930983543396, "Communication Device Number of Channels 4"]
+[1.776130199432373, 6.860601425170898, "Communication Device Data Rate 300 Mbit/s"]
+[1.744935393333435, 6.887109279632568, "Communication Device Data Rate 450 Mbit/s"]
+[1.62934410572052, 6.987468719482422, "Communication Device Frequency 26 GHz"]
+[1.656019687652588, 6.9692158699035645, "Communication Device Bandwidth 450 MHz"]
+[1.7188588380813599, 6.9676737785339355, "Communication Device Bandwidth 900 MHz"]
+[1.6868022680282593, 6.955715656280518, "Communication Device Bandwidth 1800 MHz"]
+[1.7153948545455933, 6.927481174468994, "Communication Device Power > 51 dBW"]
+[1.7131437063217163, 6.943657875061035, "Communication Device Power < 800 W"]
+[-6.7637858390808105, 10.016128540039062, "Antenna Size 2.5 m"]
+[-5.24587869644165, 7.8871660232543945, "Communication System Type Redundancy"]
+[0.5978209376335144, 12.074023246765137, "Sensor Technology Magnetic sensors"]
+[-4.433521270751953, 12.129911422729492, "Magnetic Sensor Type 3-axis"]
+[1.590545654296875, 2.2848336696624756, "Geostationary Satellite Launch Mass 4850 kg"]
+[1.6081323623657227, 2.267909049987793, "Geostationary Satellite In-Orbit Mass 2750 kg"]
+[1.5945521593093872, 2.2764267921447754, "Geostationary Satellite S/C Size 2 m x 3 m x 8 m"]
+[-6.642177581787109, 9.942484855651855, "Antenna System Main Reflector Diameter 2.4 m"]
+[1.61037015914917, 2.270787239074707, "Geostationary Satellite Mission Design Life 5 years"]
+[-1.9671434164047241, 8.665082931518555, "Circuit Trigger Voltage across the inductor"]
+[-1.2372041940689087, 8.58459758758545, "Component Location Negative end of the high-voltage solar array and the end of the TJ arrays"]
+[-1.2162165641784668, 8.571542739868164, "Component Surface Treatment Completely covered with RTV adhesive"]
+[1.0455353260040283, -1.3795654773712158, "Satellite Ground-Track Control Within 150 m of nominal"]
+[1.7535197734832764, -1.1843026876449585, "Satellite XF Mode 5 m resolution, 125 km swath width"]
+[1.7376052141189575, -2.2392354011535645, "Satellite Definitive Orbits To be made available routinely for SAR data processing"]
+[1.9406250715255737, -1.4331899881362915, "Satellite Image Quality Stable and well within operating objectives"]
+[1.8357778787612915, -1.7973657846450806, "Satellite NRT Geolocation Accuracy Not provided"]
+[2.725464105606079, -3.2827913761138916, "Communication Satellite Mission Type Non-EO"]
+[2.8945415019989014, -3.3584370613098145, "Communication Satellite Launch Date 24 October 2021"]
+[2.8505942821502686, -3.3315811157226562, "Communication Satellite End of Life Date 24 October 2036"]
+[2.759892463684082, -3.280653715133667, "Communication Satellite Coverage Zone North, South and Central America, the Caribbean and the Atlantic Ocean"]
+[2.7149534225463867, -3.2192163467407227, "Communication Satellite Connectivity High-speed connectivity with a high degree of flexibility"]
+[-4.577250957489014, -3.1049623489379883, "Exoplanet Orbital Period 8.5 days"]
+[-4.543381214141846, -3.07084059715271, "Exoplanet Mass Less than 58 times Earth's mass"]
+[-4.579747200012207, -3.103830575942993, "Exoplanet Orbital Period 21 years"]
+[-4.601767063140869, -3.1245195865631104, "Exoplanet Orbital Period 3.3 years"]
+[4.239245414733887, -2.642042875289917, "Satellite Observation Period 27 days"]
+[2.3264987468719482, -1.6554964780807495, "Satellite Transit Recognition Usually, it takes at least two observed transits to recognize a planet's presence"]
+[5.274885654449463, -4.434010982513428, "Satellite Phase A Start Date October 2006"]
+[5.075106620788574, -4.4736552238464355, "Satellite PDR Date Fall of 2012"]
+[5.125274658203125, -4.264305114746094, "Satellite Phase CD/E1 Proposal Start Date Autumn 2013"]
+[0.5734333395957947, -1.4426064491271973, "Satellite Orbit Altitude > 2000 km"]
+[0.9093453288078308, -1.4591751098632812, "Satellite Geolocation Accuracy 2km"]
+[0.5226015448570251, -1.4723036289215088, "Satellite Orbit Altitude 36,786 km"]
+[0.46974268555641174, -1.524458408355713, "Satellite Orbit Altitude 2000 - 35,786 km"]
+[2.4438397884368896, -1.8119840621948242, "Satellite Geolocation Accuracy Unknown"]
+[1.9062566757202148, 8.608352661132812, "Subsystem Signal Generation Low power transmit signal pulses at C-band"]
+[-5.110321521759033, 8.29255199432373, "Signal Distribution Component Transmit Signal Distribution Distributes low power transmit signal pulses to each T/R module"]
+[-5.183090686798096, 8.328569412231445, "Signal Distribution Component Transmit Signal Distribution Distributes low power transmit signal pulses to T/R modules"]
+[-5.187337398529053, 8.296038627624512, "Signal Distribution Component Transmit Signal Distribution Distributes low power transmit signal pulses to T/R modules"]
+[-4.875809669494629, 8.335502624511719, "Signal Routing Component Signal Routing Routes the output signals from each of the combining networks to the two receiver channel inputs of the SE"]
+[-1.6159411668777466, 1.4871257543563843, "Data Relay System Data Down-link Directly to processing and archiving centers"]
+[-1.121058702468872, 4.491297721862793, "Ground Stations Data Reception Other data continues to be received"]
+[-3.5041401386260986, 6.8408026695251465, "Data Policy Access Full and open access to the data"]
+[-0.9664047956466675, 7.7915778160095215, "Device Cross Section Averaged around a circle at each velocity aberration"]
+[-1.021167278289795, 7.771008491516113, "Device Cross Section Per Unit Area Maximum at 1.1 inches"]
+[-0.9922186136245728, 7.7733988761901855, "Device Cross Section Per Unit Area Smallest change in range correction versus velocity aberration occurs at 1.0 inches"]
+[-1.0085117816925049, 7.808424472808838, "Device Size 1.0 inch"]
+[-1.2470594644546509, 8.651320457458496, "Canister Objective Demonstrate distributed, interactive and intelligent control approaches"]
+[1.4440131187438965, 10.867051124572754, "Scan Platforms Objective Measure Earth's atmospheric emissions, day and night glow, and aurora"]
+[1.4704962968826294, 10.80179214477539, "Scan Platforms Range 115 - 1,150 nautical miles"]
+[2.2833893299102783, 23.2467041015625, "Instrument Operation Frequency 1.41 GHz"]
+[2.491058111190796, 22.70656394958496, "Instrument Band L-band"]
+[2.6788642406463623, 23.650218963623047, "Instrument Bandwidth Not specified"]
+[2.6875085830688477, 23.705699920654297, "Instrument Operation Frequency Not specified"]
+[2.688457727432251, 23.70627212524414, "Instrument Operation Frequency Not specified"]
+[2.6877834796905518, 23.70692253112793, "Instrument Operation Frequency Not specified"]
+[2.689070224761963, 23.707805633544922, "Instrument Operation Frequency Not specified"]
+[2.6893060207366943, 23.709091186523438, "Instrument Operation Frequency Not specified"]
+[2.6890974044799805, 23.709169387817383, "Instrument Operation Frequency Not specified"]
+[2.6893491744995117, 23.70891761779785, "Instrument Operation Frequency Not specified"]
+[2.690185308456421, 23.710134506225586, "Instrument Operation Frequency Not specified"]
+[2.690345048904419, 23.711761474609375, "Instrument Operation Frequency Not specified"]
+[2.6974663734436035, 23.719369888305664, "Instrument Operation Frequency Not specified"]
+[2.693279981613159, 23.715803146362305, "Instrument Operation Frequency Not specified"]
+[2.6923623085021973, 23.714799880981445, "Instrument Operation Frequency Not specified"]
+[2.6947264671325684, 23.719154357910156, "Instrument Operation Frequency Not specified"]
+[2.6918258666992188, 23.716625213623047, "Instrument Operation Frequency Not specified"]
+[2.6917271614074707, 23.71844482421875, "Instrument Operation Frequency Not specified"]
+[2.693237543106079, 23.720138549804688, "Instrument Operation Frequency Not specified"]
+[2.6906182765960693, 23.720382690429688, "Instrument Operation Frequency Not specified"]
+[2.691256523132324, 23.718286514282227, "Instrument Operation Frequency Not specified"]
+[2.6914479732513428, 23.719562530517578, "Instrument Operation Frequency Not specified"]
+[2.6926040649414062, 23.726152420043945, "Instrument Operation Frequency Not specified"]
+[2.6899266242980957, 23.722888946533203, "Instrument Operation Frequency Not specified"]
+[2.687777519226074, 23.723369598388672, "Instrument Operation Frequency Not specified"]
+[2.6927175521850586, 23.731067657470703, "Instrument Operation Frequency Not specified"]
+[2.6937294006347656, 23.72688865661621, "Instrument Operation Frequency Not specified"]
+[2.7104878425598145, 23.744728088378906, "Instrument Operation Frequency Not specified"]
+[2.690354347229004, 23.728591918945312, "Instrument Operation Frequency Not specified"]
+[2.6877377033233643, 23.733430862426758, "Instrument Operation Frequency Not specified"]
+[2.6913795471191406, 23.725318908691406, "Instrument Operation Frequency Not specified"]
+[2.6913998126983643, 23.73248863220215, "Instrument Operation Frequency Not specified"]
+[2.673844337463379, 23.70648765563965, "Instrument Operation Frequency Not specified"]
+[2.6914453506469727, 23.727724075317383, "Instrument Operation Frequency Not specified"]
+[2.693695068359375, 23.73394012451172, "Instrument Operation Frequency Not specified"]
+[2.6920058727264404, 23.736848831176758, "Instrument Operation Frequency Not specified"]
+[2.6907236576080322, 23.7332820892334, "Instrument Operation Frequency Not specified"]
+[2.689488410949707, 23.72896957397461, "Instrument Operation Frequency Not specified"]
+[2.7048580646514893, 23.749961853027344, "Instrument Operation Frequency Not specified"]
+[2.683910369873047, 23.72783088684082, "Instrument Operation Frequency Not specified"]
+[2.6927273273468018, 23.729778289794922, "Instrument Operation Frequency Not specified"]
+[2.6891841888427734, 23.735090255737305, "Instrument Operation Frequency Not specified"]
+[2.6879868507385254, 23.73531723022461, "Instrument Operation Frequency Not specified"]
+[2.6887738704681396, 23.73525047302246, "Instrument Operation Frequency Not specified"]
+[2.690183401107788, 23.743757247924805, "Instrument Operation Frequency Not specified"]
+[2.688314914703369, 23.72730255126953, "Instrument Operation Frequency Not specified"]
+[2.6768105030059814, 23.751089096069336, "Instrument Operation Frequency Not specified"]
+[2.7156169414520264, 23.76143455505371, "Instrument Operation Frequency Not specified"]
+[2.69728422164917, 23.73903465270996, "Instrument Operation Frequency Not specified"]
+[2.7136828899383545, 23.76780128479004, "Instrument Operation Frequency Not specified"]
+[2.6943864822387695, 23.73670768737793, "Instrument Operation Frequency Not specified"]
+[-0.8266651034355164, 11.631768226623535, "Detector Spectral Range 11-17 \u03bcm"]
+[-0.8042925000190735, 8.759224891662598, "Cooling System Temperature 150 K"]
+[-0.8316186666488647, 11.608349800109863, "Detector Mounting Directly to the 55 K coldfinger of a 1 W tactical cooler"]
+[-0.7784497141838074, 8.621343612670898, "Cooler Power 1 W"]
+[-0.73857581615448, 8.579273223876953, "Cooler Temperature 55 K"]
+[2.6388731002807617, 14.324213981628418, "Optical Instrument Motion Synchronized with the filter wheel"]
+[2.657552719116211, 14.340570449829102, "Optical Instrument Number of IR spectral filters 18"]
+[2.656428098678589, 14.385965347290039, "Optical Instrument Revolution Time 100 ms"]
+[2.6673319339752197, 14.345097541809082, "Optical Instrument Steps to the next location Around 20 ms"]
+[2.62130069732666, 14.277613639831543, "Optical Instrument Sampling Independent of the filter-wheel position"]
+[0.2169427126646042, 13.787714958190918, "Calibration Instrument Uncertainty 5%"]
+[0.2258901298046112, 13.80385971069336, "Calibration Instrument Calibration Parts Absolute and relative radiometric calibrations"]
+[-1.5925626754760742, 4.10129976272583, "Ground Segment Locations La Crau test site (43.56\u00baN, 4.86\u00baE), Libya 1 (24.42\u00baN, 13.35\u00baE), Libya 2 (25.05\u00baN, 20.48\u00baE), Libya 3 (23.15\u00baN, 23.1\u00baE), Mauritania 2 (20.85\u00baN, 8.78\u00baW)"]
+[-5.032449245452881, 2.8952748775482178, "Space Telescope Observed Parts of X-ray Light Spectrum Low-energy"]
+[-5.026697635650635, 2.8960938453674316, "Space Telescope Observed Parts of X-ray Light Spectrum High-energy"]
+[-5.045639514923096, 2.895644187927246, "Space Telescope Observed Phenomenon Black hole winds blowing toward us"]
+[-5.004353046417236, 2.8878421783447266, "Space Telescope Detected Atoms Iron atoms"]
+[-5.0291571617126465, 2.885213851928711, "Space Telescope Observed Phenomenon Winds emanate from the black hole not in a beam, but in a nearly spherical fashion"]
+[2.8312103748321533, 22.23402976989746, "Instrument Design and Development MPE (Max-Planck-Institut f\u00fcr Extraterrestrik), Garching, Germany"]
+[2.881974935531616, 22.318254470825195, "Instrument Cooperating Institutions and Companies Institut f\u00fcr Astronomie und Astrophysik der Universit\u00e4t T\u00fcbingen (IAAT); Astrophysikalisches Institut Potsdam (AIP); Dr.-Remeis-Sternwarte, Bamberg; Hamburger Sternwarte; Space Research Institute (IKI), Moscow; Roskosmos, Moscow; Kayser-Threde GmbH, Munich; Carl Zeiss AG, Oberkochen; MLT (Media Lario Technologies), Italy"]
+[-0.4679233133792877, 0.20905384421348572, "Satellite Navigation System Selective Availability (SA) Removed on May 2, 2000"]
+[-0.4355795681476593, 0.20332685112953186, "Satellite Navigation System Signal Accuracy Highest\u2010possible"]
+[-0.4441989064216614, 0.20225633680820465, "Satellite Navigation System Source of Signal Error Ionospheric effects"]
+[2.8175880908966064, 13.70805835723877, "Optical Communications System Service Start Date Nov. 23, 2016"]
+[2.8232197761535645, -1.1416447162628174, "Satellite Purpose Observe other satellites and orbital debris"]
+[1.9260836839675903, -1.3980752229690552, "Satellite Optics Small aperture"]
+[2.2752785682678223, -2.374701976776123, "Satellite Cost Cheap"]
+[4.226655960083008, -2.9230809211730957, "Satellite Safe-hold Mode Activation Time 1:37 a.m. EDT"]
+[2.292964458465576, -1.5308623313903809, "Satellite Instrument Status Turned off"]
+[2.612858533859253, -1.839231014251709, "Satellite Backup Available"]
+[0.22710725665092468, 4.613461017608643, "Natural Disaster Wind Speed 140 mile/h (225 km/h)"]
+[0.28192925453186035, 12.199172019958496, "Lightning Data Sensor Data Use Long-term trending and climate understanding"]
+[-2.784252405166626, 4.260208606719971, "Space Environmental In Situ Suite Purpose Monitor the near-Earth particle and electromagnetic environment in real-time"]
+[-2.8751144409179688, 4.2781081199646, "Space Environmental In Situ Suite Monitored Particles Geomagnetically trapped electrons and protons; electrons, protons, and heavy ions of direct solar origin; and galactic background particles"]
+[4.063388347625732, 13.915175437927246, "Laser Altimeter Canister Components Laser transmitter, concave mirror/detector"]
+[-1.5012699365615845, 16.899856567382812, "Altimeter Support Cannister Components Control, telemetry, telecommand and power conditioning electronics"]
+[2.9153876304626465, 22.443103790283203, "Instrument Components 38 cm telescope, diode-pumped Nd:YAG laser transmitter, altimeter receiver electronics package, 250 MHz waveform digitizer"]
+[-5.210848331451416, 7.848711967468262, "Communication System Antenna Type Transmitting and receiving"]
+[-5.152358531951904, 7.911907196044922, "Communication System Beam Control Independently, flexibly and rapidly"]
+[-5.232272148132324, 7.881505489349365, "Communication System Communication Function SS-TDMA (Satellite Switched Time Division Multiple Access)"]
+[-5.210109710693359, 7.879213333129883, "Communication System Dimensions 1420 mm x 920 mm x 1500 mm"]
+[-5.246997833251953, 7.883313179016113, "Communication System Mass 183 kg"]
+[-5.210505962371826, 7.92855167388916, "Communication System Thermal Dissipation Function Self-controlled"]
+[1.0578384399414062, -1.0434707403182983, "Satellite Length Nearly the length of a football field"]
+[2.8492050170898438, -1.0723544359207153, "Satellite Purpose Advance understanding of the Van Allen radiation belts and their effect on spacecraft components"]
+[4.669098854064941, -2.57243013381958, "Satellite Expected Mission Duration At least a year"]
+[3.220109224319458, -1.7296010255813599, "Satellite Operation Phase Launch and Early Operations"]
+[1.7521686553955078, -1.3350006341934204, "Satellite Concentration Measurement Precision 4 ppm (CO2), 34 ppb (CH4)"]
+[4.11301326751709, -2.7950291633605957, "Satellite Observational Period 3 month - 1,000 km mesh (terrestrial region), 1 month - 500 km mesh (terrestrial region), 2,000 km mesh (ocean)"]
+[1.6087511777877808, -1.4173310995101929, "Satellite Estimation Accuracy of Flux Reduce the estimation error on the sub-continental scale to half compared with the one estimated using only ground observation data, Estimate the monthly net fluxes with the accuracy of \u00b1100%"]
+[1.1388351917266846, -0.9716286063194275, "Satellite Mesh Size 1,000 km (terrestrial region), 4,000 km (ocean)"]
+[2.812753200531006, -1.2330466508865356, "Satellite Mission Objectives Improve the understanding of the global carbon dioxide distribution and its contribution to climate change, and also monitor the carbon dioxide variation on seasonal time scales"]
+[3.2016773223876953, -1.7644689083099365, "Satellite Manufacturer Changchun Institute of Optics, Fine Mechanics and Physics/Chinese Academy of Sciences (CIOMP/CAS)"]
+[-0.782054603099823, 11.52808952331543, "Detector Unknown Unknown"]
+[-0.7765566110610962, 11.52566909790039, "Detector Unknown Unknown"]
+[-0.4656525254249573, 5.875720977783203, "Unknown Unknown Unknown"]
+[1.5079821348190308, 5.420375823974609, "Satellite Bus Dimensions 1.4 m x 1.1 m x 0.953 m"]
+[0.9454711079597473, -1.158160924911499, "Satellite Deployed Length About 7.5 m"]
+[1.5140316486358643, 5.425588607788086, "Satellite Bus Subsystems Structure and mechanism, thermal control, attitude and orbit control, power supply, TT&C, antenna, housekeeping and electrical subsystems"]
+[1.516095519065857, 5.424523830413818, "Satellite Bus Main Structure Aluminum honeycomb sandwich panels"]
+[2.3516931533813477, 22.652786254882812, "Instrument Detection Threshold Low"]
+[-1.057621955871582, 10.958070755004883, "CCD Ground Sample Distance (GSD) Approximately 8 km"]
+[-2.7693393230438232, 7.891322135925293, "Processor Adjustability Allows digital event detection algorithms and parameters to be more flexibly developed and optimized to operate reliably at the limits of instrument noise"]
+[1.4333276748657227, -1.161190152168274, "Satellite Resolution 1 meter"]
+[2.7902028560638428, -2.6357011795043945, "Satellite Video Frame Rate 1 frame per second"]
+[4.731068134307861, -2.4746487140655518, "Satellite Mission Life 3 years"]
+[0.7353332042694092, -1.1688952445983887, "Satellite Altitude 450 km"]
+[2.861811876296997, -1.8875483274459839, "Satellite Business Model Pay-per-picture"]
+[-1.6063727140426636, 14.730978965759277, "Photometer Wavelength 260 nm"]
+[-1.5946842432022095, 14.701883316040039, "Photometer Triggering Strategy Search the occurrence of a sharp peak inside each photometer waveform"]
+[1.995926022529602, 22.591960906982422, "Instrument Distance Between Optical and Electronics Modules 1m"]
+[-7.4860053062438965, 5.967630386352539, "MicroCamera-Unit Wavelength 762 nm for sprite and 777 nm for lightning"]
+[-7.481287002563477, 5.96160888671875, "MicroCamera-Unit Wavelength Bandwidth 10 nm FWHM"]
+[3.4874942302703857, 10.567510604858398, "High Power Amplifier Tx power 25 W"]
+[3.502567768096924, 10.582003593444824, "High Power Amplifier Operational frequency range 28 MHz - 85 MHz"]
+[3.490596055984497, 10.56932258605957, "High Power Amplifier Number of TRMs 80"]
+[3.4886398315429688, 10.568608283996582, "High Power Amplifier Efficiency 25%"]
+[3.4886655807495117, 10.571414947509766, "High Power Amplifier Noise figure 2.9 dB"]
+[3.4887001514434814, 10.571765899658203, "High Power Amplifier TRM size 203 mm x 117 mm x 23.5 mm"]
+[3.4935386180877686, 10.572343826293945, "High Power Amplifier TRM mass 675 g"]
+[-0.16394129395484924, 4.870385646820068, "Underwater Feature Depth 9 to 12 fathoms"]
+[-0.25040262937545776, 4.943520545959473, "Wind Speed 2.5 to 5 m/s"]
+[-0.29019084572792053, 5.023609161376953, "Wind Speed 0 to 2.5 m/s"]
+[3.7399940490722656, 17.710948944091797, "Payload Units CEM (Correlative Environment Monitor) and CCA (Central Carrier Assembly)"]
+[-1.26674485206604, 6.866090297698975, "Central Carrier Assembly Sub-Experiments CREDANCE (Cosmic Radiation Environment Dosimetry and Charging Experiment), DIME-1 (Dosimetry Inter-comparison and Miniaturization Experiment Board #1), DIME-2 (Dosimetry Inter-comparison and Miniaturization Experiment Board #2), ELDRS (Linear Enhanced Low Dose Rate Sensitivity), COTS-2 (Commercial Off the Shelf Technology)"]
+[-0.47323447465896606, 8.31983757019043, "Coating Purpose Release charges and prevent concentration of electric field"]
+[-0.4924502372741699, 8.358607292175293, "Coating Advantages Cost savings, does not require change in solar array design"]
+[-1.1516977548599243, 4.457072734832764, "Ground Station Equipment Quantity 1 computer rack"]
+[-1.150138020515442, 4.461421966552734, "Ground Station Antenna Quantity 2"]
+[-1.141979455947876, 4.499388694763184, "Ground Station Location NPS (Naval Postgraduate School), Monterey, CA"]
+[-1.1361725330352783, 4.477908611297607, "Ground Station Location USU (Utah State University), Logan, UT"]
+[-1.1193288564682007, 4.483269214630127, "Ground Station Location UH (University of Hawaii) at Manoa, HI"]
+[-1.1206320524215698, 4.525875568389893, "Ground Station Location AFIT (Air Force Institute of Technology), located on Wright-Patterson AFB, Ohio"]
+[0.8939933776855469, 14.79120922088623, "Instrumentation Antenna Type Parabolic cylinder reflector antenna"]
+[3.7286925315856934, 17.723115921020508, "Payload Configuration L-band scatterometer and different frequencies for radiometer"]
+[-6.725459575653076, 9.991455078125, "Antenna Frequency L/S/C"]
+[-6.6810503005981445, 9.942726135253906, "Antenna Type Deployable parabolic cylinder mesh reflector"]
+[-6.6389665603637695, 9.921710014343262, "Antenna Frequency L-band"]
+[1.9032282829284668, 10.721821784973145, "Imaging Device Payload Qualification Unknown"]
+[1.9077447652816772, 10.692667007446289, "Imaging Device Optical Performance Test Results Unknown"]
+[2.723726987838745, 22.118406295776367, "Instrument Imaging Earth\u2019s upper atmosphere"]
+[2.7288753986358643, 22.069623947143555, "Instrument Orbit Geostationary"]
+[2.9149317741394043, 22.45577621459961, "Instrument Project Manager LASP"]
+[2.866318464279175, 22.36576271057129, "Instrument Principal Investigator Richard Eastes of UCF"]
+[2.7200748920440674, 22.43115997314453, "Instrument Data Center Collect, process, and distribute the science data for the mission"]
+[1.4442429542541504, 2.727914571762085, "Meteorological Satellite Operation Start Date June 1986"]
+[1.4684537649154663, 2.6838560104370117, "Meteorological Satellite Owner EUMETSAT"]
+[-1.354000210762024, 6.178811550140381, "Organization Operational Mandate 1993"]
+[-1.3427400588989258, 6.178083896636963, "Organization Ground Segment Establishment Date 1995"]
+[-3.157879114151001, 1.7027941942214966, "Satellite Mission Data Continuity Maintaining data continuity from GRACE"]
+[-3.1559243202209473, 1.7099053859710693, "Satellite Mission Data Gap Minimizing any data gap after GRACE"]
+[-3.1540071964263916, 1.7163019180297852, "Satellite Mission Project Execution Location US"]
+[-3.2069947719573975, 1.703857660293579, "Satellite Mission Observation Date Oct. 7-25, 2019"]
+[-3.153752088546753, 1.6949235200881958, "Satellite Mission Ion Type Oxygen ions"]
+[-3.1342973709106445, 1.7093489170074463, "Satellite Mission Light Wavelength 135.6 nm"]
+[-3.2252414226531982, 1.7447290420532227, "Satellite Mission Data Release Date December 7, 2019"]
+[-3.1493537425994873, 1.721166968345642, "Satellite Mission Data Availability Through 11/30/2019"]
+[3.9879791736602783, -2.7769484519958496, "Satellite Orbit Completion 100,000th"]
+[5.015103816986084, -2.3411500453948975, "Satellite Designed Mission Life Three years"]
+[3.1602818965911865, -1.7477744817733765, "Satellite Manufacturer Lockheed Martin Space Systems"]
+[2.6755998134613037, -1.739877462387085, "Satellite Sensor Provider Northrop Grumman"]
+[2.3874082565307617, -1.9356236457824707, "Satellite Location Lockheed Martin facility near Moffett Field in Sunnyvale, California"]
+[3.178887367248535, -1.775983452796936, "Satellite Manufacturer Lockheed Martin"]
+[5.005857467651367, -4.412978649139404, "Satellite Measurement Date March 29, 2021"]
+[1.5328903198242188, -1.3262865543365479, "Satellite Wetness Percentile Varies"]
+[3.7206830978393555, -2.466063976287842, "Satellite Dry Condition Frequency 2 percent of the time (about once every 50 years)"]
+[4.942345142364502, -3.729487657546997, "Satellite Drought Period 2000-2018"]
+[2.3120017051696777, 22.12767791748047, "Instrument Parameter Atmosphere"]
+[-3.8752427101135254, 7.918905258178711, "Data Storage Total Capacity 7 Gbit"]
+[-3.8452022075653076, 7.975933074951172, "Data Storage Capacity for Pan Imagery 4 Gbit"]
+[-3.787376880645752, 7.903737545013428, "Data Storage Capacity for MS Imagery 3 Gbit"]
+[-3.8471086025238037, 7.891308307647705, "Data Storage Number of Pan Scenes 31"]
+[-3.825209379196167, 7.911167621612549, "Data Storage Number of MS Scenes 31"]
+[-2.564117431640625, 11.599058151245117, "Imagery Ground Area 30.7 km x 30.7 km"]
+[5.410117149353027, -4.40163516998291, "Satellite Launch Date August 2, 2017"]
+[2.0924391746520996, -2.6790757179260254, "Satellite Number of Satellites in Orbit 3"]
+[2.1139414310455322, -2.7276954650878906, "Satellite Planned Number of Satellites 10"]
+[-0.9495432376861572, 9.828376770019531, "Rocket Error Programming error in the upper stage"]
+[1.6931633949279785, 6.937392234802246, "Communication Device Performance Tuning Ongoing"]
+[5.287778377532959, -4.359114170074463, "Satellite Launch Date January 2016"]
+[2.5819039344787598, -2.392944812774658, "Satellite Data Transmission 1.7 petabytes"]
+[2.1620101928710938, -2.4971892833709717, "Satellite Optical Inter-satellite Links Almost 30,000"]
+[-1.6180846691131592, 1.4848406314849854, "Data Relay System Data Transmission Speed 1.8 Gbit/s"]
+[-1.6141780614852905, 4.0954766273498535, "Space and Ground Segment Objective Demonstrate a prototype secure CCSDS packet TM/TC system in an operational environment"]
+[-2.401817798614502, 4.1139936447143555, "Space Segment Components Number of switches, several electronic devices, and interfaces to the Sparc processor with the relevant software loaded"]
+[-1.5850492715835571, 4.120590686798096, "Ground Segment Components Telecommand and telemetry security layer software integrated into the primary STRV TM/TC processor workstation"]
+[-0.6487019658088684, 9.419028282165527, "Spacecraft Component Material Dielectric material (resin-glass)"]
+[-0.6521544456481934, 9.418289184570312, "Spacecraft Component Length 25 cm"]
+[-2.8495993614196777, 20.19240379333496, "Emission Line Wavelength 530.285 nm"]
+[2.045154333114624, 22.470918655395508, "Instrument Width 0.02 nm"]
+[-2.9089910984039307, 20.057159423828125, "Emission Line Width ~0.1 nm"]
+[-1.0263965129852295, 7.754525661468506, "Device Tilt Mechanically tilted"]
+[-1.7972848415374756, 12.173402786254883, "Infrared Camera System Objective Demonstrate and assess QWIP FPA uniformity, stability, and repeatability and responsivity in a space radiation environment"]
+[-1.378836989402771, 7.372750759124756, "Integrated Dewar Assembly Location Installed on the bottom side of the S/C deck"]
+[-1.2324409484863281, 8.25483226776123, "Integrated Dewar Assembly Components QWIP FPA, cryocooler, motherboard ROIC"]
+[0.11284442991018295, 7.163212776184082, "Experiment Operational Scenario Turned on every few days to collect and transfer data to the S/C for downlink transmission"]
+[-2.1860835552215576, 5.947978973388672, "Formation Flying Navigation Reference Frame Local Vertical Local Horizontal (LVLH)"]
+[-2.223426342010498, 5.8850321769714355, "Formation Flying Navigation Functions Collision risk detection, metrology data validity assessment, self-assessment of estimated position and velocity covariance, state estimation validity, navigation using alternative metrology, relative attitude computation, ancillary absolute orbit processing"]
+[-2.169250965118408, 5.93741512298584, "Formation Flying Guidance Reference Frame Local Vertical Local Horizontal (LVLH)"]
+[-2.18759822845459, 6.00299072265625, "Formation Flying Guidance Functions Computes the reference state, position, velocity and attitude; and feed forward action in case of forced continuous phases (formation acquisition, coronagraphy, formation flying maneuvers), and calculates the orbital maneuvers and application times and direction in case of impulsive maneuvers (perigee pass DTMs, CGC, Go to Safe, CAM)"]
+[-0.8050302267074585, 11.616130828857422, "Detector Quantum Efficiency ~85% (at 650 nm)"]
+[-0.8248071670532227, 11.589892387390137, "Detector Fill Factor 100%"]
+[-0.8016632199287415, 11.622081756591797, "Detector Frame Rate 230 frames/s"]
+[1.8027210235595703, 8.472793579101562, "Mission Data Handling Subsystem Components FPGA, mass memory and some peripheral components"]
+[-4.193515300750732, 8.782730102539062, "Signal Generator Doppler Frequency Shifts Setup Independent"]
+[-4.2326436042785645, 8.829339981079102, "Signal Generator Code Generators Four independent code generators for primary and secondary codes per unit"]
+[-4.214735507965088, 8.796027183532715, "Signal Generator Modulation Schemes AltBOC and CASM (Coherent Adaptive Subcarrier Modulation)"]
+[2.583068609237671, 22.166379928588867, "Instrument Data Focus Atmospheric, ocean, and land data"]
+[2.6576263904571533, 22.330705642700195, "Instrument Data Focus Near real-time lightning data"]
+[2.436504602432251, 22.799903869628906, "Instrument Number of Level 1b End-Products 8"]
+[0.7554826736450195, -1.1749730110168457, "Satellite Altitude About 490 km"]
+[0.5888471007347107, -1.4323453903198242, "Satellite Orbital Speed About 7.5 km/s"]
+[1.6177349090576172, -2.1450750827789307, "Satellite Orbit Near-polar"]
+[4.046787261962891, -2.743088722229004, "Satellite Orbital Period Once every 90 minutes"]
+[4.419835567474365, -2.6613049507141113, "Satellite Checkout Phase Duration 85 days"]
+[4.625171661376953, -2.7570555210113525, "Satellite First Science Data Release About seven months"]
+[5.107043743133545, -4.141402244567871, "Satellite Launch Date December 2029"]
+[0.5633320808410645, -1.4184105396270752, "Satellite Orbit Altitude 693 km"]
+[0.6848350167274475, -2.318507671356201, "Satellite Orbit Inclination 98.19\u00b0"]
+[4.140793323516846, -2.825119972229004, "Satellite Orbit Period 98.74 minutes"]
+[4.172234058380127, -2.472637891769409, "Satellite Repeat Cycle 12 days"]
+[-4.485829830169678, 15.934183120727539, "Radar Instrument Type C-band synthetic aperture radar"]
+[-4.50008487701416, 15.91590404510498, "Radar Operation Mode Transmit-receive or receive-only"]
+[-1.5652897357940674, 6.979979991912842, "Simulation Equipment Gravity Levels 0 and 1g"]
+[-0.27932336926460266, 6.924283981323242, "Investigation Purpose Simulating the high-energy, low gravity conditions that were present during formation of the early solar system"]
+[11.496885299682617, 5.694423198699951, "CubeSat Size 6U"]
+[11.521312713623047, 5.72357177734375, "CubeSat Size 3U"]
+[11.500701904296875, 5.714718341827393, "CubeSat Size 3U"]
+[11.512076377868652, 5.7229461669921875, "CubeSat Size 3U"]
+[16.82213592529297, 6.873649597167969, "Microsatellite Mass 56 kg"]
+[11.512176513671875, 5.717075824737549, "CubeSat Size 3U"]
+[16.817773818969727, 6.876986503601074, "Microsatellite Mass 37 kg"]
+[11.503814697265625, 5.709475040435791, "CubeSat Size 3U"]
+[11.485061645507812, 5.702528476715088, "CubeSat Size 6U"]
+[11.155187606811523, 5.268642425537109, "CubeSat Mass 5 kg"]
+[11.51921558380127, 5.733921527862549, "CubeSat Size 1U"]
+[16.80828094482422, 6.891211032867432, "Microsatellite Mass ~40 kg"]
+[0.03533947095274925, -2.017383337020874, "Satellite Operation Number of Orbits 2"]
+[-0.017721213400363922, -1.98261296749115, "Satellite Operation Operation Sequence Handover from FF to RVX at WP0, Reaching WP1 through a forced motion retreat maneuver, Reaching pre-perigee WP2 by non-drifting hop, Demonstration of perigee passage under Sun illumination until WP3"]
+[0.8203441500663757, -1.790929913520813, "Sun-synchronous Altitude 628km"]
+[1.136391520500183, -2.3816215991973877, "Sun-synchronous Inclination 97.9\u00ba"]
+[1.1183288097381592, -2.41048526763916, "Sun-synchronous Local Sun Time 12:00 \u00b1 15 min"]
+[1.1091384887695312, -2.377859354019165, "Sun-synchronous Revisit Time 14 days"]
+[1.0253653526306152, -4.324275016784668, "Satellite Mass 2120 kg"]
+[1.216986894607544, -0.7649180293083191, "Satellite Size 9.9 m (x) x 16.5 m (y) x 3.7 m (z)"]
+[2.077026844024658, -0.5064844489097595, "Satellite Power Generation 5.2 kW"]
+[-5.219405651092529, 7.895193099975586, "Communication System X-band 800 Mbit/s (16 QAM), 400/200 Mbit/s (QPSK)"]
+[-5.2527174949646, 7.924271583557129, "Communication System Ka-band 278 Mbit/s (QPSK)"]
+[1.8431495428085327, 22.188034057617188, "Instrument Spatial Resolution 48 x 48 mrad"]
+[2.083556890487671, 22.287532806396484, "Instrument Scan Angle 100\u00ba"]
+[1.674471139907837, 21.973968505859375, "Instrument Swath Width 3200 km"]
+[2.3789143562316895, 22.68400001525879, "Instrument Scan Time 6 seconds"]
+[2.069269895553589, 22.25522232055664, "Instrument IFOV 48 mrad x 48 mrad"]
+[2.135686159133911, 22.537546157836914, "Instrument Sampling Period 62.5 ms"]
+[2.0902304649353027, 22.2646541595459, "Instrument FOV 100\u00ba (3200 km)"]
+[2.351125955581665, 22.645103454589844, "Instrument Scan Period 6 s"]
+[2.228337287902832, 22.418926239013672, "Instrument Pixels per Scan 51"]
+[2.298555374145508, 22.58534812927246, "Instrument Useful Scan Time 3.18 s"]
+[1.9832569360733032, 22.580589294433594, "Instrument Dynamic Range (solar) up to 425 W m -2  sr -1"]
+[1.6811907291412354, 21.52442169189453, "Instrument Instrument Mass 40 kg"]
+[1.8530330657958984, 22.93735122680664, "Instrument Instrument Power 42 W (average)"]
+[1.8907309770584106, 22.624618530273438, "Instrument Dynamic Range (total) up to 500 W m -2  sr -1"]
+[1.744618535041809, 22.218408584594727, "Instrument Instrument Size 614 x 512 x 320 mm"]
+[2.096280336380005, -2.736022710800171, "Satellite Number of Satellites 2"]
+[2.0671818256378174, -2.703923463821411, "Satellite Number of Satellites 4"]
+[-0.9534875750541687, -10.00426959991455, "Satellite Constellation Number of Satellites 30"]
+[-0.9492388963699341, -10.007485389709473, "Satellite Constellation Orbital Planes Inclination 56\u00ba"]
+[-0.9546666741371155, -10.015366554260254, "Satellite Constellation Mean Altitude 23616 km"]
+[-0.9481410384178162, -10.006246566772461, "Satellite Constellation Orbital Period 5/3 revolutions/day"]
+[-0.9476179480552673, -10.006446838378906, "Satellite Constellation Ground Track Repeat ~ 10 days"]
+[-0.9476779103279114, -10.005899429321289, "Satellite Constellation Orbit Graveyard MEO (+ 300 km)"]
+[-3.1506309509277344, 1.707088828086853, "Satellite Mission Formation Resize 25 to 250 m"]
+[-3.0921289920806885, 1.7683542966842651, "Satellite Mission Formation Retarget -30\u00ba to +30\u00ba"]
+[1.7792716026306152, -2.2462990283966064, "Satellite Maneuver Objective Demonstrate operations foreseen from future formation flying missions"]
+[1.8563950061798096, -2.360337018966675, "Satellite Maneuver Objective Demonstrate service operation and move from point A to point B"]
+[-2.475980758666992, 12.566650390625, "Spectral Imager Spectral Channels 0.38, 0.67, 0.87, 1.375, and 1.64 \u00b5m"]
+[-2.487355947494507, 12.570881843566895, "Spectral Imager Spatial Resolution 0.5 km"]
+[-2.4999141693115234, 12.579876899719238, "Spectral Imager Swath Width 400 km"]
+[-2.429572105407715, 12.607956886291504, "Spectral Imager CO2 Measurement Accuracy 1 to 4 ppm"]
+[-2.4989817142486572, 12.578120231628418, "Spectral Imager Measurement Scales Regional (500 km x 500 km) and monthly"]
+[-1.8241899013519287, 8.303674697875977, "Sub-system Mounting Location In front of the instrument Tube, under the lid of the FDA (Front Door Assembly)"]
+[-1.8181334733963013, 8.19249439239502, "Sub-system Mounting Location In front of the instrument Tube"]
+[-1.818476676940918, 8.177796363830566, "Sub-system Mounting Location Under the lid of the FDA (Front Door Assembly)"]
+[-5.099397659301758, 2.867572784423828, "Space Telescope Parameter Unknown"]
+[-7.554020404815674, 5.896519184112549, "Fast Camera Parameter Unknown"]
+[-0.9901233315467834, 3.1294829845428467, "Astronomical Systems Time Delay About one-tenth of a second"]
+[-13.700770378112793, -2.0939810276031494, "X-ray Binary System Brightness Outburst June 2015"]
+[-13.707233428955078, -2.117063522338867, "X-ray Binary System Brightness Outburst Less than 1 percent of its maximum expected brightness"]
+[0.5974027514457703, 9.365278244018555, "Attitude Determination and Control Subsystems Components Sun sensors, magnetometers, rate gyro"]
+[-13.671928405761719, -2.30452561378479, "X-ray Telescope Launch Year 2012"]
+[-13.864788055419922, -2.2105376720428467, "X-ray Telescope X-ray Energy Detection Above 30,000 eV"]
+[4.912047386169434, -4.263387680053711, "Satellite X-ray Observations March 2014 and June 2016"]
+[-14.254265785217285, -2.4937744140625, "X-ray Telescope Principal Investigator Fiona Harrison"]
+[-14.214757919311523, -2.4619343280792236, "X-ray Telescope Principal Investigator Affiliation Caltech in Pasadena, California"]
+[6.37863302230835, 7.369607925415039, "Satellite Component Function Controls and monitors the payload of the satellite and many other subsystems"]
+[6.324354648590088, 7.412482261657715, "Satellite Component Composition Several layers of metal-evaporated polyimide film"]
+[6.354598522186279, 7.384771823883057, "Satellite Component Function Deliver additional heat protection"]
+[6.3605122566223145, 7.382083892822266, "Satellite Component Function Provides both the command and control of the spacecraft and the attitude and orbit control functions"]
+[5.293513298034668, -4.421134948730469, "Satellite Data Collection Start Date Early 2019"]
+[2.472726345062256, -1.1857017278671265, "Satellite Data Content Mexico coastline, mountains, trees, ocean waves, seafloor"]
+[2.5359582901000977, -1.1801506280899048, "Satellite Data Content Amery Ice Shelf, meltwater pooling on the surface of the ice shelf"]
+[-3.0079188346862793, 20.20668601989746, "Spectral Band Wavelength Range 0.50 \u00b1 0.2 - 0.70 \u00b1 0.2 \u00b5m"]
+[-2.9785072803497314, 20.1790714263916, "Spectral Band Wavelength Range 0.70 \u00b1 0.2 - 1.10 \u00b1 0.2 \u00b5m"]
+[-2.9901702404022217, 20.18987274169922, "Spectral Band Wavelength Range 1.60 \u00b10.50 - 1.80 \u00b1 0.50 \u00b5m"]
+[-2.9927496910095215, 20.19053077697754, "Spectral Band Wavelength Range 3.50 \u00b1 0.50 - 4.10 \u00b1 0.50 \u00b5m"]
+[-2.982527494430542, 20.182912826538086, "Spectral Band Wavelength Range 10.5 \u00b1 0.50 - 11.5 \u00b1 0.50 \u00b5m"]
+[-2.9774436950683594, 20.17818260192871, "Spectral Band Wavelength Range 11.5 \u00b1 0.50 - 12.5 \u00b1 0.50 \u00b5m"]
+[2.095120906829834, 22.225732803344727, "Instrument Plane Scanning Angle 108\u00ba, 54\u00ba"]
+[1.7481744289398193, 22.051069259643555, "Instrument Width 2800 km"]
+[2.0301828384399414, 22.425500869750977, "Instrument Resolution 1.2 +0.2 mrad"]
+[1.8316009044647217, 22.148012161254883, "Instrument Resolution 1 km"]
+[2.255855083465576, 22.722949981689453, "Instrument Signal-to-Noise Ratio \u2265 200, \u2265 100"]
+[2.1387674808502197, 22.490957260131836, "Instrument Measurement Error 10%"]
+[1.976914882659912, 22.469392776489258, "Instrument Temperature Range 213-313 K"]
+[2.102889060974121, 22.39303207397461, "Instrument Temperature Sensitivity \u2264 1 K \u2264 0.2 K \u2264 0.2 K"]
+[2.112779140472412, 22.501686096191406, "Instrument Measurement Error 0.5 K"]
+[2.5827431678771973, 22.573402404785156, "Instrument Data 10 bit"]
+[2.302602767944336, 22.944988250732422, "Instrument Rate 660 kbit/s"]
+[2.7824747562408447, 22.74552345275879, "Instrument Mode Continuous"]
+[1.5216915607452393, 21.228748321533203, "Instrument Mass \u2264 70 kg"]
+[2.697262763977051, 21.623498916625977, "Science Instrument Observation Capabilities POD (Precise Orbit Determination), GNSS-RO (GNSS Radio Occultation), Neutral Atmosphere, Ionosphere, and Scintillation, GNSS-R (GNSS Reflections)"]
+[2.7213006019592285, 21.581701278686523, "Science Instrument Tolerant to Total Ionizing Dose 40 kRad"]
+[2.7293715476989746, 21.650733947753906, "Science Instrument Processor Architecture Dual processor"]
+[2.731426477432251, 21.619009017944336, "Science Instrument SNR Higher than previous generation receivers"]
+[2.7242188453674316, 21.614511489868164, "Science Instrument Flexibility Greater to accommodate future requirements"]
+[-3.198436737060547, 1.734110713005066, "Satellite Mission Launch Date 2034"]
+[-3.1414284706115723, 1.7098133563995361, "Satellite Mission Satellite Quantity 3"]
+[-3.1386046409606934, 1.7043721675872803, "Satellite Mission Satellite Triangle Side Length Approx. 2.5 million kilometers"]
+[-3.1376142501831055, 1.696540117263794, "Satellite Mission Gravitational Wave Measurement Range 10 seconds to more than half a day"]
+[5.018622875213623, -4.511605262756348, "Satellite Presentation Date 05-05-2017"]
+[5.05521297454834, -4.424431324005127, "Satellite Publication Date 15 May, 2018"]
+[2.573201894760132, -3.895622491836548, "Satellite Abstract URL https://journals.aps.org/prl/abstract/10.1103/PhysRevLett.120.191103"]
+[4.088867664337158, 13.935052871704102, "Laser Altimeter System Function Measure melting ice sheets and investigate how this effects sea level rise, investigate changes in the mass of ice sheets and glaciers, estimate and study sea ice thickness, and measure the height of vegetation in forests and other ecosystems worldwide"]
+[4.113046646118164, 13.935478210449219, "Laser Altimeter System Manufacturer NASA"]
+[4.715625762939453, -2.6031293869018555, "Satellite Mission Duration Long-term"]
+[5.200620174407959, -4.071458339691162, "Satellite Discovery Year 2007"]
+[5.149341106414795, -2.2797598838806152, "Satellite Legacy 25 years"]
+[-0.5037065744400024, 6.858199596405029, "Research Topic Emphasis Ice Motion"]
+[1.5035899877548218, 5.426466464996338, "Small Satellite Bus SpaceWire Deterministic Implementation Unknown"]
+[2.9180099964141846, -2.0476763248443604, "Satellite ELEGANT Framework Unknown"]
+[5.254778861999512, -4.135242462158203, "Satellite Launch Date 2017"]
+[-0.9859955906867981, 9.856060028076172, "Rocket Launch Date 2017"]
+[-3.2631986141204834, 5.420164108276367, "Launch Vehicle Objective Demonstrate performance"]
+[3.3054747581481934, -2.6012020111083984, "Satellite Data Downlink Frequency Once per orbit"]
+[0.2566155195236206, 11.593594551086426, "Sensor System Data Output Modes L data, T data, TF data, LF data, TS, LS"]
+[0.24813000857830048, 11.565496444702148, "Sensor System Data Collection Infrared Fine resolution data (TF data) can be collected continuously, day and night. Visible fine (LF data) is collected during daytime only"]
+[2.9842026233673096, 22.7862606048584, "Instrument Bias Unknown"]
+[-0.8152405023574829, 0.16354309022426605, "Satellite System Orbit Calculation Technique Reduced-dynamic"]
+[2.404656410217285, -1.1154325008392334, "Satellite Data Radial Accuracy 2.5 cm"]
+[6.3441081047058105, 7.391242027282715, "Satellite Components Precision Unknown"]
+[0.6420475840568542, -1.4037607908248901, "Satellite Deep Space Flight Distance 40,000,000 km"]
+[1.3322120904922485, -1.0475822687149048, "Satellite Asteroid Flyby Resolution 3 m"]
+[0.8368770480155945, -1.3644373416900635, "Satellite Asteroid Flyby 1 km-level"]
+[2.724189519882202, -1.6269965171813965, "Satellite Lagrangian Point Feature Utilized"]
+[2.7784125804901123, -1.776423692703247, "Satellite Lagrangian Point Flyby Realized"]
+[2.148792266845703, -1.7536894083023071, "Satellite Observation Total solar eclipse"]
+[2.2858428955078125, -1.5188722610473633, "Satellite Observation Ionosphere response"]
+[0.6420596241950989, -1.6895548105239868, "Satellite Segment Number of LEOLUTs 53"]
+[0.7140758633613586, -1.6721402406692505, "Satellite Segment Number of GEOLUTs 23"]
+[0.7051604390144348, -1.8061550855636597, "Satellite Segment Number of MCCs 31"]
+[0.6822850108146667, -1.7129653692245483, "Satellite Segment Number of Operational Spacecraft 5"]
+[0.6945549249649048, -1.7926949262619019, "Satellite Segment Number of Operating Satellites 7"]
+[1.5994590520858765, 2.2850310802459717, "Geostationary Satellite Testing Position 167\u00baE"]
+[1.6173410415649414, 2.2630717754364014, "Geostationary Satellite Launch Year 2015"]
+[1.670391321182251, 2.2125823497772217, "Geostationary Satellite Launch Year 2015"]
+[1.6095401048660278, 2.271177053451538, "Geostationary Satellite Launch Year 2016"]
+[14.595510482788086, 7.744857311248779, "Nanosatellite Size Shoebox-sized"]
+[14.49123477935791, 7.724196434020996, "Nanosatellite Orbit Altitude Close to 6000 km"]
+[14.484180450439453, 7.6712422370910645, "Nanosatellite Sensor Complement Radiation-detection payloads from CERN, the European Council for Nuclear Research, Slovenian firm SkyLabs and ESA"]
+[1.467060923576355, -2.397205352783203, "Satellite Orbit Type Highly-elliptical Earth Orbit"]
+[0.7427348494529724, -1.5899869203567505, "Satellite Perigee 600 km"]
+[0.6433179974555969, -1.6710515022277832, "Satellite Apogee 60,530 km"]
+[0.7303000688552856, -2.275547981262207, "Satellite Inclination 59\u00ba"]
+[4.162127494812012, -2.8488261699676514, "Satellite Orbital Period 19 hr 38 minutes"]
+[-0.5211379528045654, 15.525794982910156, "Imaging Spectrometer Filter Wavelength Range 623-750 nm"]
+[-0.5243695378303528, 15.523978233337402, "Imaging Spectrometer Filter Wavelength 762 nm"]
+[-0.5073539614677429, 15.527560234069824, "Imaging Spectrometer Filter Wavelength 427.8 nm"]
+[-0.5090010166168213, 15.536986351013184, "Imaging Spectrometer Filter Wavelength 630 nm"]
+[-0.5209529399871826, 15.527060508728027, "Imaging Spectrometer Filter Wavelength 557.7 nm"]
+[-0.5003292560577393, 15.528730392456055, "Imaging Spectrometer Filter Wavelength Range 150-280 nm"]
+[-0.47995302081108093, 15.57168960571289, "Imaging Spectrometer Filter Wavelength Range 250-390 nm"]
+[-0.5077601671218872, 15.530341148376465, "Imaging Spectrometer Filter Wavelength 337.0 nm"]
+[-1.5883601903915405, 4.111196994781494, "Ground Segment Module Ability Provide accurate estimation of GIOVE and GPS orbits and clocks"]
+[-1.9437878131866455, 7.41829776763916, "On-board Device Performance Excellent frequency stability"]
+[-1.9510458707809448, 7.568685531616211, "On-board Device Predictability Errors at 100 minutes clearly below the nanosecond"]
+[-1.6067771911621094, 4.2021708488464355, "Ground Segment Module Compliance Feasible compliance to the Galileo requirements"]
+[3.4917995929718018, 13.413267135620117, "Laser Transmitter Continuous Operation 3 years"]
+[3.535799503326416, 13.355081558227539, "Laser Transmitter Laser Shot Count ~1 trillion"]
+[3.4692673683166504, 13.415214538574219, "Laser Transmitter Components Laser Optical Module (LOM) and Laser Electronics Module (LEM)"]
+[3.5179052352905273, 13.36412239074707, "Laser Transmitter Number of Units Three"]
+[3.5174484252929688, 13.386082649230957, "Laser Transmitter Spare Units One"]
+[1.868354320526123, -0.22998394072055817, "Radar Imaging Satellite Imaging Data High-resolution"]
+[1.8472100496292114, -0.21914295852184296, "Radar Imaging Satellite Operation Day or night, when skies are cloudy or clear"]
+[1.868399739265442, -0.23091226816177368, "Radar Imaging Satellite Location Cloudy tropical location like the Tonga archipelago"]
+[1.6563551425933838, -1.1901333332061768, "Satellite Image Resolution Sub-meter"]
+[2.1050894260406494, -1.5910989046096802, "Satellite Imaging Modes Single pass stereo"]
+[2.7750251293182373, -1.2136811017990112, "Satellite Applications Public safety, resource management, environmental monitoring, location-based services, intelligence and disaster monitoring"]
+[-5.368300437927246, 2.877185583114624, "Optical Telescope Purpose Capturing satellite streaks"]
+[1.430838704109192, 5.447666645050049, "Bus Manufacturer Boeing"]
+[-13.670586585998535, -2.319755792617798, "X-ray Telescope Launch Date 26 April 2019"]
+[-13.747241973876953, -2.2997043132781982, "X-ray Telescope Symposium Date June 16-19, 2014"]
+[-13.635153770446777, -2.402613878250122, "X-ray Telescope Progress Update Date 18 September 2018"]
+[3.125067710876465, -1.933681845664978, "Satellite Mission Status Operational"]
+[2.3767857551574707, -1.2361092567443848, "Satellite Data Tracking Ice Loss at the Poles"]
+[0.9827179312705994, -4.293869972229004, "Satellite Weight Measurement Midwestern Floods"]
+[-5.385767459869385, 2.8148655891418457, "Telescope Field of View (FOV) Energy-dependent"]
+[-5.464975357055664, 2.733830451965332, "Telescope Spectral Resolution 500 eV at energies below ~30 keV, 1.2 keV at the upper end of the energy range"]
+[-5.387632369995117, 2.780731201171875, "Telescope Temporal Resolution 2 \u00b5s"]
+[-5.376426696777344, 2.7732372283935547, "Telescope Intrinsic Temporal Resolution Better than 1 \u00b5s"]
+[-5.3606719970703125, 2.7450473308563232, "Telescope Target of Opportunity (ToO) Response Time Less than 24 hours"]
+[-5.309524059295654, 2.6921491622924805, "Telescope Average Turnaround Time Typically within 6 hours"]
+[-4.973212718963623, 9.784478187561035, "Receiver Frequency Range 3 kHz to 750 kHz"]
+[-4.761961936950684, 9.261615753173828, "Transmitter High Power Frequency Range 3 \u2013 50 kHz"]
+[-4.743427276611328, 9.2712984085083, "Transmitter High Power Output Up to 500 W"]
+[-4.695276260375977, 9.32287883758545, "Transmitter Low Power Frequency Range 50 \u2013 750 kHz"]
+[-4.72027063369751, 9.262667655944824, "Transmitter Low Power Output 1 W"]
+[1.9060413837432861, 22.72077751159668, "Instrument HST Measurement 100 \u2013 500 keV electrons"]
+[2.028806209564209, 22.469491958618164, "Instrument HST Geometric Factor 0.1 cm2 str"]
+[2.0424561500549316, 22.37962532043457, "Instrument HST Loss Cone 6.5\u00ba"]
+[2.15307354927063, 22.29839515686035, "Instrument FSH Pitch Angle Distribution 130\u00ba x 10\u00ba"]
+[1.9936772584915161, 22.561283111572266, "Instrument FSH Measurement 50 \u2013 700 keV electrons"]
+[2.135254383087158, 22.49496841430664, "Instrument FSH Measurement Interval 167 ms"]
+[7.270425796508789, 12.40684700012207, "Spacecraft Instruments Accuracy Requirement Good positional accuracy"]
+[-0.819996178150177, 0.16306838393211365, "Satellite System Daily Collection Capacity Enough to deliver a return on the investment"]
+[-1.6231192350387573, 9.704522132873535, "Electric Propulsion System Specific Impulse (Isp) 2,250 s"]
+[-1.6364741325378418, 9.672506332397461, "Electric Propulsion System Thrust 1.24 mN"]
+[-1.6380972862243652, 9.741329193115234, "Electric Propulsion System Power 70 W"]
+[-1.6400020122528076, 9.722908973693848, "Electric Propulsion System Propellant Iodine"]
+[11.262190818786621, 5.535810470581055, "CubeSat Deployment Date October 5, 2015"]
+[11.254440307617188, 5.47230863571167, "CubeSat Relative Motion About 1 m/s"]
+[11.315900802612305, 5.524998664855957, "CubeSat Main Payload SDR (Software Defined Radio)"]
+[6.35122537612915, 7.398308277130127, "Satellite Component Operation Type LCT time synchronization, On-orbit propagator, LCT alignment matrix, LCT park and unpark, Ka-band antenna steering pause"]
+[-2.020737648010254, 5.757300853729248, "Flight Operations Team Operation Type Telemetry verification"]
+[1.373395562171936, 7.054501056671143, "Communication Equipment Location Fairchild Air Force Base (FAFB), near Spokane, Washington, and Loring Air Force Base, Limestone, Maine"]
+[-3.2388880252838135, 7.300747394561768, "Data Processing Center Location Offutt Air Force Base, near Omaha, Nebraska"]
+[-1.7186516523361206, 6.6083807945251465, "Program Declassification Date March 1973"]
+[-3.6114799976348877, 7.656099319458008, "Compression Algorithm Implementation Wavelet transform with bit plane coding"]
+[-1.7827128171920776, 8.492677688598633, "Integrated Circuit Speed Up to 25 Mpixel/s"]
+[-3.614454984664917, 7.637890338897705, "Encryption Algorithm Key Size 128-bit"]
+[5.265728950500488, -4.464350700378418, "Satellite Launch Date June 2015"]
+[5.349490165710449, -4.455738544464111, "Satellite Launch Date March 2017"]
+[-2.845320701599121, 15.219141960144043, "Microwave Radiometer Frequency Eight"]
+[-2.8089380264282227, 15.23848819732666, "Microwave Radiometer Polarization Dual"]
+[-0.7489198446273804, 15.34302043914795, "VIS/IR Radiometer and Imaging Spectrometer Number of Channels 36"]
+[-3.8825666904449463, 15.743976593017578, "Active Microwave Radar Provider National Aeronautics and Space Administration/Jet Propulsion Laboratory (NASA/JPL)"]
+[3.04294490814209, -1.5677669048309326, "Satellite Development Program Participants Over 150 undergraduate students, 7 active graduate students, 7 faculty"]
+[5.059142112731934, -4.2932939529418945, "Satellite Mission Concept Review Completion Date Spring of 2021"]
+[2.901705026626587, -1.2164472341537476, "Satellite Scientific Goal Study Gamma-Ray Bursts (GRBs)"]
+[1.7513309717178345, -3.078115224838257, "Satellite Gamma-Ray Regime 50-500 keV"]
+[4.416321277618408, -2.675443649291992, "Satellite Afterglow Period Duration Hours to months"]
+[2.72279691696167, 21.65962028503418, "Scientific Instrument Data Capacity 6 TB"]
+[-3.5126516819000244, 6.806912422180176, "Data Resolution 7 m"]
+[-3.5077335834503174, 6.825671195983887, "Data Resolution Unknown"]
+[0.6464953422546387, 9.323958396911621, "Attitude Determination and Control Subsystem Attitude Control 3-axis stabilization"]
+[0.6404863595962524, 9.344583511352539, "Attitude Determination and Control Subsystem Attitude Sensing 3-axis magnetometer, a 3-axis gyroscope, 4 sun sensors, 2 ST (Star Trackers)"]
+[-0.9873570203781128, 7.837358474731445, "Positioning Device Function Orbital position information"]
+[3.4733269214630127, 13.44102668762207, "Laser Communications Network Ground Stations Redu (BE), Harwell (UK), Weilheim (DE), Matera (IT)"]
+[2.2310876846313477, -1.9433009624481201, "Satellite Test Location Munich"]
+[5.233097553253174, -3.836859703063965, "Satellite Launch Year 2019"]
+[5.257906436920166, -3.8647305965423584, "Satellite Launch Year 2016"]
+[0.8075628876686096, -1.7041006088256836, "Satellite Thruster Operation Within 20% of the apogee location, up to 10% on each side of apogee while above 52,000 km"]
+[1.2892624139785767, -1.9986039400100708, "Satellite Thruster Operation Below 1,600 km, which only represents 25 minutes of the 19.3-hour orbital period"]
+[2.0221259593963623, -1.481905460357666, "Satellite Battery Type Li-ion 18650s"]
+[2.1298129558563232, -2.7240653038024902, "Satellite Number of Batteries 16"]
+[5.0801849365234375, -2.3148553371429443, "Satellite Design Life 1 year"]
+[2.093017578125, -0.7089916467666626, "Satellite Power Source Solar panels and batteries"]
+[-0.6967114210128784, 3.26894211769104, "Star Sensor Degradation Commercial-grade CCD"]
+[2.4694910049438477, -1.273910641670227, "Satellite Data High precision scalar magnetic data"]
+[0.46592041850090027, 4.488193511962891, "Natural Phenomenon Wind Speed Increase 80 miles (130 km) per hour in one day"]
+[0.5601606965065002, 4.662493705749512, "Phenomenon Wind Speed Increase At least 35 miles (56 km) per hour within 24 hours"]
+[-0.04447885602712631, 4.625938892364502, "Hurricane Speed 2 miles per hour"]
+[6.202458381652832, 7.536215782165527, "Satellite Component Quantity 3"]
+[6.301181793212891, 7.431591033935547, "Satellite Component Thermal Control Cold-biased passively and actively controlled using heaters"]
+[-1.2671382427215576, 7.934733867645264, "Electronic Device Thermal Stability Requirement Change less than 0.1\u00ba C over 7 days"]
+[-1.273140549659729, 7.951536178588867, "Electronic Device Channels 4 (vertical, horizontal and the sum and difference which is equivalent polarization at \u00b145\u00ba)"]
+[-1.3552684783935547, 8.082923889160156, "Electronic Device Components Dicke switch, reference load, coupler to a noise diode"]
+[-6.692992210388184, 9.971470832824707, "Antenna Polarization Circular"]
+[-6.668854236602783, 9.934812545776367, "Antenna Type Dipole"]
+[-5.30263614654541, 8.014626502990723, "Communication System Uplink Frequency 145.848 MHz"]
+[-5.315699100494385, 8.022290229797363, "Communication System Downlink Frequency 436.450 MHz"]
+[-5.24525785446167, 7.7981109619140625, "Communication System Data Rates 9.6 kbit/s"]
+[2.1312029361724854, -2.522904872894287, "Satellite Dynamic Range 6 bits"]
+[1.6101683378219604, -1.5607149600982666, "Satellite Noise Level Relatively low"]
+[1.4996312856674194, -1.1561675071716309, "Satellite Triangulation Results 1-1.5 pixels"]
+[3.7402188777923584, -1.607102870941162, "Satellite Operation Status Nominal"]
+[2.250309467315674, -1.7157520055770874, "Satellite Calibration and Validation Lead Kelly Brunt"]
+[3.052809953689575, -1.5758298635482788, "Satellite Deputy Project Scientist Tom Neumann"]
+[2.9148921966552734, -1.92855703830719, "Satellite Campaign Team Four-person team"]
+[-3.280982255935669, 7.855058193206787, "Image Compressor, Mass Memory, Data Ciphering Unit Function Process, store and format multi-spectral video instrument data for the satellite downlink"]
+[-3.265331745147705, 7.903365612030029, "Image Compressor, Mass Memory, Data Ciphering Unit Technology NAND flash memory"]
+[-3.3312509059906006, 8.10958194732666, "Image Compressor, Mass Memory, Data Ciphering Unit Memory Capacity Various capacities"]
+[-3.25923752784729, 7.840022087097168, "Image Compressor, Mass Memory, Data Ciphering Unit Operation Start Date Since September 2012"]
+[2.508574962615967, -2.020017623901367, "Satellite CoReCi Unit Carried"]
+[3.723977565765381, 17.652620315551758, "Payload Interface Card SDRAM Mass Storage 10 GByte"]
+[3.7833313941955566, 17.625234603881836, "Payload Interface Card LVDS Serial Data Recording Port Speed 2 Mbit/s"]
+[3.7219581604003906, 17.659719467163086, "Payload Interface Card RS-422 Serial Interfaces Primary and redundant"]
+[3.709836006164551, 17.646799087524414, "Payload Interface Card Pulse Input Channels Primary and redundant"]
+[2.653346538543701, 14.479474067687988, "MultiSpectral Instrument Supplier Astrium Toulouse"]
+[3.229952335357666, -1.7756186723709106, "Satellite Manufacturer EADS-Astrium GmbH"]
+[3.2253682613372803, 2.3750524520874023, "Satellite Subsystem Power Requirement High"]
+[3.2234835624694824, 2.3748795986175537, "Satellite Subsystem Antenna Configuration Omnidirectional"]
+[3.2259867191314697, 2.369175434112549, "Satellite Subsystem Antenna Selection Autonomous and seamless"]
+[3.222905397415161, 2.374337911605835, "Satellite Subsystem Latency High"]
+[3.221846342086792, 2.37322735786438, "Satellite Subsystem Command Uplinks Can be uploaded in advance"]
+[-0.6680530905723572, 9.452729225158691, "Spacecraft Component Diameter 5 m"]
+[-0.6478701233863831, 9.435787200927734, "Spacecraft Component Thickness 4 cm"]
+[-0.36813849210739136, 8.186565399169922, "Ablative Material Erosion Roughly 20 percent"]
+[-0.6206107139587402, 9.419483184814453, "Spacecraft Component Removal Date Feb. 27, 2015"]
+[-0.6374799609184265, 9.427170753479004, "Spacecraft Component Test Article Water impact testing"]
+[-5.373724937438965, 2.8098790645599365, "Telescope Resolution 1 m GSD"]
+[-5.289763927459717, 2.738959312438965, "Telescope Orbital Altitude 550 km"]
+[-5.383129119873047, 2.775193214416504, "Telescope Aperture Diameter 50 cm"]
+[0.45926734805107117, 4.517158508300781, "Natural Phenomenon Minimum Extent 3.74 million km2 (1.44 million square miles)"]
+[0.4685457646846771, 4.534071922302246, "Natural Phenomenon Annual Minimum Date September 15, 2020"]
+[0.45477160811424255, 4.551635265350342, "Natural Phenomenon Extent Rank Second-lowest"]
+[1.5385324954986572, 21.250242233276367, "Instrument Mass 30 kg"]
+[1.6429063081741333, 23.198604583740234, "Instrument Power 40 W"]
+[2.350717782974243, 22.906845092773438, "Instrument Data Rates 7.2 kbit/s (X-band), 0.9 kbit/s (L-band)"]
+[1.6363282203674316, 22.18492317199707, "Instrument Envelope 76 cm x 30 cm x 37 cm"]
+[2.6839599609375, 22.2587833404541, "Instrument Thermal Control Active control , 2 zones"]
+[3.4943981170654297, 8.123311042785645, "X-Ray Sensor Function Monitors solar flares and helps predict solar proton events"]
+[1.5332942008972168, 21.240093231201172, "Instrument Mass 32 kg"]
+[2.018446445465088, 22.361928939819336, "Instrument Volume 0.8 m x 0.5 m x 0.25 m"]
+[1.623193621635437, 23.21573829650879, "Instrument Power Consumption 50 W"]
+[2.4619827270507812, 22.509029388427734, "Instrument Data Quantization 12 bit"]
+[2.286726236343384, 22.9246883392334, "Instrument Data Rate 883 kbit/s"]
+[1.8810555934906006, 22.014848709106445, "Instrument Observation Swath 2400 km"]
+[1.7657560110092163, 22.086946487426758, "Instrument Pixel Size at Nadir 6 km x 7 km"]
+[-0.047950033098459244, 9.26080322265625, "Guidance System Function Computes the S/C attitude reference based on the sun direction and relative position inputs"]
+[-0.03735750541090965, 9.265215873718262, "Guidance System Modes Boost Mode, Coast Mode, Forced Motion Mode"]
+[-1.668500304222107, 5.883021831512451, "Maneuver Reference Trajectory Constant relative range and with a direction that ensures the S/C are Sun aligned"]
+[4.191359043121338, -2.4819040298461914, "Satellite Revisit Time 5 days"]
+[2.5653860569000244, -2.215226888656616, "Satellite Range of Spectral Bands Unknown"]
+[2.8526687622070312, -1.2082092761993408, "Satellite Mission Purpose Monitor changes in plant health and growth"]
+[2.5187976360321045, -1.1455726623535156, "Satellite Glacier Monitoring Monitors changes in glacier mass, extents, trace area and length of glacier changes through time and derive surface velocity"]
+[-0.02388877049088478, 15.468655586242676, "Spectrometer Mass 3 kg"]
+[-0.1444711834192276, 15.461846351623535, "Spectrometer Size 180 mm x 110 mm x 230 mm"]
+[-0.1362791657447815, 15.552116394042969, "Spectrometer Spectral Range 8-12 \u00b5m"]
+[-0.13191720843315125, 15.515942573547363, "Spectrometer Spatial Resolution < 200 m @ 600 km altitude"]
+[-0.17293930053710938, 15.54369068145752, "Spectrometer Detector Type Uncooled infrared detector"]
+[-0.0932164415717125, 15.51226806640625, "Spectrometer Number of Pixels 640 x 480"]
+[-0.13118013739585876, 15.492717742919922, "Spectrometer FOV 12\u00ba x 9\u00ba"]
+[-0.11184435337781906, 15.529176712036133, "Spectrometer Exposure Time 33 ms"]
+[-0.09478958696126938, 15.573176383972168, "Spectrometer Dynamic Range 180 K - 400 K"]
+[-0.11006595194339752, 15.509758949279785, "Spectrometer NEDT 0.2 K@300 K"]
+[-0.1323670893907547, 15.52734661102295, "Spectrometer Temperature Accuracy <4 k (goal 2 K @ 300 K)"]
+[-1.6288485527038574, 12.206327438354492, "Infrared FPA Principle Detecting infrared energy as minute changes of the IR absorber temperature when infrared radiation id detected"]
+[5.255964756011963, -4.4774065017700195, "Satellite Launch Date May 24, 2014"]
+[4.406187057495117, -3.379833221435547, "Satellite Launch Time 03:05 UTC"]
+[16.794452667236328, 6.902134418487549, "Microsatellite Mass 43 kg"]
+[16.732444763183594, 6.956316947937012, "Microsatellite Mass ~ 50 kg"]
+[14.72085189819336, 7.80741024017334, "Nanosatellite Mass ~7 kg"]
+[-1.558454990386963, 12.8539457321167, "Solar Coronagraph Formation Flying Yes"]
+[-1.5554927587509155, 12.835865020751953, "Solar Coronagraph Stray Light Analysis Optimization"]
+[-1.56632399559021, 12.85439682006836, "Solar Coronagraph ICSO 2010 Presentation Date Oct. 4-8, 2010"]
+[-1.5614773035049438, 12.848668098449707, "Solar Coronagraph URL http://congrex.nl/ICSO/Papers/Session%209a/FCXNL-10A02-1987947-1-LANDINI_ICSO_PAPER.pdf"]
+[2.9873287677764893, 22.72317886352539, "Instrument Mission Status Operational (extended)"]
+[3.7168092727661133, 22.974123001098633, "Instrument Launch Date 21 November 2013"]
+[3.569810628890991, 22.902360916137695, "Instrument End of Life Date 31 December 2023"]
+[3.2006940841674805, -1.5449347496032715, "Satellite Mission Type EO"]
+[2.721576452255249, -1.122314691543579, "Satellite Objective Provide monitoring data to shipping line customers who are interested in the Arctic Sea ice state and the eventual use of the Arctic shipping routes"]
+[-2.2775120735168457, 11.128580093383789, "Digital Image Processing System Detection Threshold Unknown"]
+[-2.9034152030944824, 7.648558616638184, "Real Time Event Processor Sampling Rate 500 Hz"]
+[-3.1719183921813965, 7.484759330749512, "Real Time Event Processor Background Value Computation Exponential moving average with an adjustable time constant k"]
+[1.7005751132965088, 6.936941623687744, "Communication Device Transmission Speed 20 wpm"]
+[1.705337405204773, 6.932762145996094, "Communication Device Protocol AX.25"]
+[1.6910686492919922, 6.9484148025512695, "Communication Device Modulation FSK"]
+[1.6295843124389648, 7.004568099975586, "Communication Device Frequency Band UHF (437.375MHz)"]
+[1.661431908607483, 6.979732513427734, "Communication Device Frequency Band VHF (144 MHz)"]
+[-2.3065900802612305, 7.415306091308594, "Embedded Computer Size 71 mm(W) x 220.5 mm(D) x 177.5 mm (H)"]
+[-2.3634464740753174, 7.466160774230957, "Embedded Computer Mass 1.9 kg"]
+[-2.374309778213501, 7.4633049964904785, "Embedded Computer Power Consumption 14 W"]
+[-2.3025639057159424, 7.452323913574219, "Embedded Computer SpaceWire Interface Channels 8"]
+[-2.2707889080047607, 7.413651943206787, "Embedded Computer UART Interface Channels 2"]
+[2.5466136932373047, -1.627461314201355, "Satellite Earth environmental observation satellite Japanese (JAXA, formerly NASDA)"]
+[2.795158624649048, -1.2027904987335205, "Satellite Science Objectives Acquire data contributing to international global change research (carbon cycle and the water and energy cycle), as well as for applications in such fields as meteorology and fishery"]
+[2.6579177379608154, -1.8265538215637207, "Satellite Japanese Contribution to IEOS WCRP/GEWEX & CLIVAR, IGBP and GCOS"]
+[3.203716993331909, -1.785827875137329, "Satellite S/C Manufacturer Mitsubishi Corporation"]
+[5.146989345550537, -4.336873531341553, "Satellite Mission Start Date June 2004"]
+[5.112400054931641, -4.446339130401611, "Satellite International Image Distribution Contract Start Date June 2004"]
+[3.6926519870758057, 22.971765518188477, "Instrument First Observation Date 4 July 2004"]
+[0.5569684505462646, -1.4640719890594482, "Satellite Parking Orbit Altitude 723 km"]
+[0.5704373717308044, -1.437313199043274, "Satellite Mission Orbit Altitude 888 km"]
+[7.184023380279541, 12.30562973022461, "Remote Sensing Instrument First Image Taken Date 4 June 2004"]
+[2.5657315254211426, -2.056971788406372, "Satellite Navigation Message performance analysis and Signal In Space User Ranging Error (SISRE) characterization Unknown"]
+[0.7431225180625916, 12.049375534057617, "Sensor Station Multi-Receiver Unknown"]
+[1.5120025873184204, 5.424685001373291, "Satellite Bus Data Transfer S-band communications"]
+[1.508684515953064, 5.418899059295654, "Satellite Bus Data Transfer X-band communication"]
+[1.5146793127059937, 5.425558567047119, "Satellite Bus Data Rate 800 Mbit/s"]
+[-3.855537176132202, 3.715512990951538, "Rover Function Navigate, locate and collect the sample tubes"]
+[-3.1820414066314697, 5.359922409057617, "Vehicle Launch Date 2026"]
+[0.02356998808681965, 7.26740837097168, "Sample Container Transfer Method STA will transfer the sample tubes into the Orbiting Sample (OS)"]
+[2.2000513076782227, 13.401928901672363, "Optical Sensor Resolution High"]
+[2.1334519386291504, 13.334131240844727, "Optical Sensor Function Observation"]
+[-0.2876741886138916, 12.339472770690918, "Atomic Oxygen Monitor System Altitude 380 km"]
+[0.762470006942749, -1.1919982433319092, "Satellite Altitude 268 km"]
+[1.4060604572296143, -3.111928701400757, "Satellites Next Operations Phase Three-month period"]
+[0.9992209672927856, 0.8034635782241821, "Earth Observation Satellite Program Date June 4-8, 2012"]
+[-0.8658367991447449, 0.18320690095424652, "Satellite System Newsletter Date Q1 2011"]
+[-1.1565567255020142, 6.694859504699707, "Overview Presentation Forum Date December 12, 2010"]
+[-5.882424831390381, 16.006664276123047, "Synthetic Aperture Radar Reprogrammable Parameters Resolution, swath width, polarization"]
+[-5.751256465911865, 15.960168838500977, "SAR Sensor Modes Swath Width Wider than the original modes"]
+[-5.771154880523682, 15.987753868103027, "SAR Sensor Modes Polarization Quad-pol"]
+[-5.721317768096924, 15.979991912841797, "SAR Sensor Modes Resolution Good"]
+[-0.8702868819236755, 7.831310272216797, "Charge-Coupled Device Pixel Arrangement 516 x 512 pixels"]
+[-0.8876851797103882, 7.788318634033203, "Charge-Coupled Device Operating Temperature -10\u00baC"]
+[-5.104248523712158, 8.803558349609375, "Transmit Receive Antenna Module Performance Within 0.7 dB of theoretical projections"]
+[2.890359401702881, 21.94191551208496, "Instrument Purpose Monitor ocean and land surfaces, global atmospheric parameters, and obtain sea surface wind profiles"]
+[2.6968188285827637, 22.39988899230957, "Instrument Scanning Type Conical"]
+[2.245438575744629, 23.127113342285156, "Instrument Operating Frequencies 10.6, 18.7, 23.8, 31.5, 36.7, 42, 48, and 91.65 GHz, 52-57 GHz, 183.31 GHz"]
+[2.8341259956359863, 22.362607955932617, "Instrument Image Source Roskosmos, Roshydromet/Planeta"]
+[3.4341249465942383, 13.453001022338867, "Laser Communication Terminals Data Exchange Speed Up to 1800 Mbit/s"]
+[3.449814558029175, 13.42803955078125, "Laser Communication Terminals Data Transmission Speed 600 Mbit/s"]
+[-5.159046173095703, 8.976551055908203, "RF Link Data Rate Approximately 300 Mbit/s"]
+[-5.0261945724487305, 2.8635051250457764, "Space Telescope Launch Year 2009"]
+[-5.080110549926758, 2.8560473918914795, "Space Telescope Principal Investigator William Borucki"]
+[-5.0668840408325195, 2.8827505111694336, "Space Telescope Mission Status Retired"]
+[7.287246227264404, 12.40712833404541, "Satellite Instrument Image Size 17.4 degree diameter circle"]
+[7.285221576690674, 12.40982723236084, "Satellite Instrument Image Size 17.8 degree diameter circle"]
+[7.248117923736572, 12.447250366210938, "Satellite Instrument Image Size 17.8 degree diameter circle"]
+[7.244658946990967, 12.393306732177734, "Satellite Instrument Image Size 17.7 degree diameter circle"]
+[4.95531702041626, -2.3828964233398438, "Satellite Mission Design Life 12 months"]
+[1.631680965423584, -2.32613468170166, "Satellite Orbit Capability LEO, MEO"]
+[1.5016309022903442, -2.295938491821289, "Satellite Control 3-axis stabilized"]
+[0.9862005114555359, -4.354960918426514, "Satellite Payload Mass (max) 170 kg"]
+[0.9804255962371826, -4.360825538635254, "Satellite Bus Mass 180 kg"]
+[0.9937810897827148, -4.379371643066406, "Satellite Total Mass 600 kg"]
+[1.1752634048461914, -0.7726746201515198, "Satellite Stowed Dimensions 1.1 m x 0.8 m x 0.8 m"]
+[1.1608552932739258, -0.8314720988273621, "Satellite Deployed Dimensions 3.6 m x 2 m x 1.1 m"]
+[2.076558828353882, -0.5352820754051208, "Satellite Payload Power 350 W, 1.1 kW"]
+[2.0589754581451416, -0.5508299469947815, "Satellite Array Power 650 W, 790 W"]
+[1.7976094484329224, -1.539962649345398, "Satellite Battery Capacity 60 Ah"]
+[1.0721373558044434, -2.0741655826568604, "Satellite S/C Pointing 1.0\u00ba, 1.0\u00ba"]
+[0.8424813151359558, -2.2105016708374023, "Satellite Slew Rate 0.25 to 1.0\u00ba/s"]
+[2.6568384170532227, -2.5268311500549316, "Satellite RF Communications 2 kbit/s, 2 Mbit/s"]
+[2.5856761932373047, -2.0313022136688232, "Satellite Command & Data Handling 240 MIPS, 128 MB, 128 MB"]
+[2.6769020557403564, 14.372740745544434, "Optical Instrument Type Zeiss 1 m \u2205 Ritchey-Chr\u00e9tien/Coud\u00e9 telescope"]
+[2.647085189819336, 14.322646141052246, "Optical Instrument Mount Type English mount"]
+[-0.12984326481819153, 15.457988739013672, "Spectrometer Measurement Domain Carbon Dioxide detection"]
+[-0.18246521055698395, 15.52218246459961, "Spectrometer Measurement Category Near-infrared absorption of carbon dioxide and the molecular oxygen in reflected sunlight"]
+[-2.6383392810821533, 11.706506729125977, "Imager Measurement Category Cloud and aerosol interference errors from CarbonSpec\u2019s measurements"]
+[-3.249194383621216, 7.32275915145874, "Data Processing and Control Center Service Level Agreement Continuous payload utilization, up to 200 links per day and communication channel, over the expected lifetime of 15 years, with a targeted service availability of at least 99.6% over 60 days and an order reaction time well below one hour"]
+[-5.085841655731201, 7.052245140075684, "Link Management System Processing Automatic requests received from the MOC"]
+[-1.2668741941452026, 8.578352928161621, "Central Component Task Executing the automatized flight operations procedures"]
+[3.1434524059295654, -1.7828524112701416, "Satellite Manufacturer OHB System"]
+[5.387291431427002, -4.388439655303955, "Satellite Launch Date 6 August 2019"]
+[1.8513128757476807, -2.1793622970581055, "Satellite Orbit Geostationary"]
+[0.553602397441864, -1.4747127294540405, "Satellite Orbit Altitude 36,000 km"]
+[2.3561770915985107, -2.1365151405334473, "Satellite Engine Type Liquid apogee engine"]
+[4.989046573638916, -4.305909156799316, "Satellite Measurement Date December 7, 2020"]
+[1.5674018859863281, -1.369299292564392, "Satellite Wetness Percentile Varies"]
+[0.5035330653190613, 4.415506839752197, "Climate Phenomenon Effect on Southwest U.S. Tends to cause dry weather"]
+[0.4833056926727295, 4.381311416625977, "Climate Phenomenon Effect on Jet Stream Pushes the jet stream north and causes it to curve"]
+[0.7503681182861328, -4.175414562225342, "Satellite Mass at Launch ~4850 kg"]
+[0.9574368000030518, -4.347476959228516, "Satellite In-Orbit Dry Mass ~2750 kg"]
+[1.1832077503204346, -0.7265087366104126, "Satellite Size 2 m x 3 m x 8 m"]
+[2.088690757751465, -0.5104843378067017, "Satellite Power 5.2 kW"]
+[1.5977333784103394, -2.1974165439605713, "Satellite Attitude Control 3-axis stabilization (zero momentum control)"]
+[2.6899685859680176, -2.4145829677581787, "Satellite RF Frequency Ka-band"]
+[1.621495008468628, 6.9952712059021, "Communication Device RF Frequency Rx (uplink): 17.7-18.8 GHz Tx (downlink): 27.5-28.6 GHz"]
+[1.7097524404525757, 6.928961277008057, "Communication Device EIRP More than 67.9 dBW"]
+[1.7441281080245972, 6.896579265594482, "Communication Device G/T More than 16.9 dB/K"]
+[2.7393863201141357, -3.2321617603302, "Satellite Communication Regenerative Mode Uplink 1.5, 6, 24, 51, or 155 Mbit/s"]
+[2.7481184005737305, -3.241895914077759, "Satellite Communication Regenerative Mode Downlink 155 Mbit/s"]
+[2.755422353744507, -3.2283263206481934, "Satellite Communication Bent-pipe Mode Up to 1.2 Gbit/s"]
+[3.724721908569336, -1.6115443706512451, "Satellite Operation Status Nominal"]
+[5.134564399719238, -4.47159481048584, "Satellite SAR Imagery Collection Start Date July 1, 2012"]
+[2.3280160427093506, -1.7608158588409424, "Satellite Data Reception Location Shadnagar GS (Ground Station) of NRSC (National Remote Sensing Center)"]
+[2.21028208732605, -1.9881998300552368, "Satellite Test Download Location Troms\u00f8, Norway"]
+[-2.758668899536133, 15.258088111877441, "Microwave Radiometer Calibration Algorithm Version v2.0"]
+[-2.800616502761841, 15.250057220458984, "Microwave Radiometer Calibration Algorithm Version v2.2"]
+[-2.8320510387420654, 15.267219543457031, "Microwave Radiometer Bias Histograms Zero mean and of Gaussian shape"]
+[-2.8274447917938232, 15.232146263122559, "Microwave Radiometer Inter-beam Biases Negligible"]
+[-5.3798723220825195, 2.773702383041382, "Telescope Mirror Modules 7"]
+[-5.391315937042236, 2.7619435787200928, "Telescope On-axis Resolution 15 arc seconds HEW"]
+[-13.902534484863281, -2.1571247577667236, "X-ray Telescope Energy Range Up to 10 keV"]
+[6.309625148773193, 7.437620639801025, "Satellite Component Optimization Diameter 1.02 Rsun"]
+[6.336414337158203, 7.401328086853027, "Satellite Component Stray Light Source Diffraction by the EO (External Occulter) edge of the direct Sun light"]
+[-0.9118852615356445, 6.767146110534668, "Process Steps 1) Diffraction by the external occulter based on the Fresnel-Kirchhoff theory at the pupil and the primary objective level. 2) Propagation of the diffracted light in the instrument with ASAP"]
+[-3.0991463661193848, 4.260856628417969, "Spacecraft Development Status Final assembly and integration completed"]
+[-2.3637077808380127, 4.423410415649414, "Space Environment Testbeds Launch Date June 2019"]
+[-2.835721969604492, 4.248093128204346, "Space Environment Testbeds Mission Study how to better protect satellites in space"]
+[11.2960786819458, 5.504983425140381, "Cubesat Drift Speed Approximately 7.5m/s"]
+[11.17083740234375, 5.377793788909912, "Cubesat Lateral Deployable Booms 2 out of 4 deployed as planned"]
+[11.242258071899414, 5.488964080810547, "Cubesat Longitudinal Deployable Boom Deployed as planned"]
+[2.636183023452759, 22.170001983642578, "Instrument Data Retrieval Atmospheric and surface parameters"]
+[3.6905460357666016, 22.9677734375, "Instrument Conference Date 4-8 February 2013"]
+[3.0845494270324707, 22.488962173461914, "Instrument URL http://smsc.cnes.fr/IASI/PDF/conf3/10_04-Uspensky_Alexander.pdf"]
+[0.6302143931388855, 12.079520225524902, "Sensor Components Two particle telescopes"]
+[0.6628711819648743, 12.01924991607666, "Sensor Type Low size, weight and power sensor"]
+[0.5802662372589111, 11.99722957611084, "Sensor Purpose Provide a focused subset of space environmental data"]
+[-0.9493081569671631, 9.80341625213623, "Rocket Launch Date 17 October, 2019"]
+[5.117061138153076, -4.368026256561279, "Satellite Loss Date 15 May 2021"]
+[-3.0869717597961426, 2.4392528533935547, "Mission Date 9 December 2021"]
+[-3.087750196456909, 2.440683126449585, "Mission Date 2 April 2022"]
+[6.313798427581787, 7.429104804992676, "Satellite Component Length 80 meters"]
+[2.9328019618988037, -1.600267767906189, "Satellite Program Manager Jeffrey Christmas"]
+[5.092526912689209, -4.417407512664795, "Satellite Deployment Date 12 July 2019"]
+[2.2124428749084473, -1.9794656038284302, "Satellite Location Kirtland AFB, New Mexico"]
+[6.283523082733154, 7.457314491271973, "Satellite Component Size 205 mm x 125 mm x 200 mm"]
+[6.298792362213135, 7.430337905883789, "Satellite Component Mass ~ 2.5 kg"]
+[6.281176567077637, 7.458659648895264, "Satellite Component Power Consumption < 3.5 W"]
+[-1.914070725440979, 7.647337436676025, "PCB Function Driving the HVs of the photomultipliers, Driving the power supply of the calibration sources, Providing the necessary power lines (+5V, \u00b112 V) and switching them on and off, Acquiring (including data quantization) signals from the sensor"]
+[-0.8355681896209717, 3.1557157039642334, "Active Galactic Nucleus Luminosity More active than the larger galaxy's central black hole"]
+[-0.7964380979537964, 3.2548859119415283, "Dwarf Galaxy Black Hole Size Unknown"]
+[-0.8585886359214783, 3.278618335723877, "Spiral Galaxy Color in Image Greenish"]
+[3.493464231491089, 8.121509552001953, "X-ray Measurement Instrument Technology Silicon drift diode"]
+[3.486818790435791, 8.106411933898926, "X-ray Detector Size Barely bigger than an ant"]
+[3.634732961654663, 22.238388061523438, "Instrument Component Performance Measure the largest flares without saturation"]
+[6.08914852142334, 7.806578159332275, "SARSAT Repeater Band Coverage 121.5 MHz"]
+[6.0387864112854, 7.877535820007324, "SARSAT Processor Band Coverage 406 MHz"]
+[6.004195213317871, 7.8241047859191895, "SARSAT Processor Configuration SARP with memory"]
+[5.974912166595459, 7.866177558898926, "SARSAT Processor Configuration Improved SARP with memory"]
+[6.179358959197998, 7.646475791931152, "SARSAT Repeater Components Two dual-conversion receivers, two 4.0 W phase modulated L-band transmitters, two Power, Telemetry and Command (PTC) units"]
+[-0.09731867164373398, 13.58956527709961, "Measurement Device Scan Area 8 m x 4 m"]
+[-0.08614945411682129, 13.573441505432129, "Measurement Device Z-axis Scan Capability 20 cm"]
+[2.8922457695007324, 21.984209060668945, "Instrument Purpose Provide the plane information of the antenna plane"]
+[7.269267559051514, 12.404570579528809, "Satellite Instrument Parameter Value"]
+[0.6429551839828491, 4.220609664916992, "Atmospheric Phenomenon Movement Symmetrical"]
+[7.296551704406738, 12.426375389099121, "Satellite Instrument Data Collection 20 orbits"]
+[7.264865875244141, 12.38412094116211, "Satellite Instrument Data Downlink About 10-12% of the scans"]
+[7.347607135772705, 12.427397727966309, "Satellite Instrument Data Downlink About 70% of the data"]
+[-3.0881690979003906, 2.4252331256866455, "Mission Success Rate 80%"]
+[2.737480401992798, 13.762899398803711, "Optical System Function Simultaneously image receive aperture and steering mirror pivot plane onto the photodetector"]
+[2.7567386627197266, 13.76041316986084, "Optical System Requirement Small coupling of tilt into the length measurement"]
+[-2.6389811038970947, 11.694051742553711, "Photodetector Number of Pixels 4"]
+[2.7632694244384766, 13.741626739501953, "Optical System Main Cause of Residual Coupling Different spatial profile of the two beams and residual beam misalignments"]
+[1.7774461507797241, -0.5761153101921082, "Imaging Satellite Synoptic Coverage 6000 km2"]
+[1.8017874956130981, -0.5114102959632874, "Imaging Satellite NIIRS 5 or better"]
+[1.752418875694275, -0.4586114287376404, "Imaging Satellite Use Cases Disaster response, event preparation, defense"]
+[2.736792802810669, 13.650638580322266, "Optical Unit Unknown Unknown"]
+[-1.4891407489776611, 6.728684425354004, "Lens Assembly Unknown Unknown"]
+[-6.678890228271484, 9.962272644042969, "Antenna Function Ensure that the main transmissions in S-band are always directed towards the Earth"]
+[-5.536268711090088, 9.498072624206543, "Frequency Band Range 2098 - 2110 MHz"]
+[-5.487940311431885, 9.551446914672852, "Frequency Band Range 1675-1696 MHz"]
+[-5.524738311767578, 9.50840950012207, "Frequency Band Range 402.0-402.2 MHz"]
+[-13.869525909423828, -2.2235612869262695, "X-ray Telescope Purpose Detect highest-energy X-ray light in great detail"]
+[-13.863492965698242, -2.252131223678589, "X-ray Telescope Complements Telescopes that observe lower-energy X-ray light, such as XMM-Newton and NASA's Chandra X-ray Observatory"]
+[-1.1441799402236938, 3.084174871444702, "Celestial Object Mass Millions to billions times the mass of our sun"]
+[0.7021278142929077, -2.276005744934082, "Satellite Surface Solar Zenith Angle < 80\u00ba"]
+[4.198290824890137, -2.806255340576172, "Satellite Sunlit Phase Duration ~46 minutes"]
+[0.7738221287727356, -2.174354076385498, "Satellite Latitude Range -51\u00ba to 56\u00ba"]
+[0.7840465903282166, -2.2100436687469482, "Satellite Latitude Range -82\u00ba to 79\u00ba"]
+[1.9743388891220093, -1.675631046295166, "Satellite Sun-Glint Observation Mode Observation Mode"]
+[1.5131760835647583, -1.5548038482666016, "Satellite Instrument Boresight Within 5\u00ba of the principal plane"]
+[0.7345237731933594, -2.298630714416504, "Satellite Pitch Axis Attitude Change -60\u00ba~+60\u00ba"]
+[0.7533805966377258, -2.325103282928467, "Satellite Yaw Axis Attitude Change Approximately for 160\u00ba"]
+[0.7398107647895813, -2.2839200496673584, "Satellite Roll Angle About 20\u00b0"]
+[0.7891035079956055, -2.2654480934143066, "Satellite Maximum Yaw Axis Slew Rate 0.2\u00b0/s"]
+[2.9965765476226807, 22.496816635131836, "Instrument Manufacturer Neptec UK (NUK) and Neptec Design Group Canada (NDG)"]
+[3.3944296836853027, 13.475340843200684, "Laser Control Electronics Unit Components 980 nm continuous-wave laser diode and signal processing electronics"]
+[2.752711296081543, 13.652976989746094, "Optical Head Unit Manufacturer Micos"]
+[2.9358158111572266, 22.449010848999023, "Instrument Sub-Assemblies LCEU (Laser Control Electronics Unit), the OHU (Optical Head Unit), and the CCRR (Corner Cube Retroreflector)"]
+[6.312843322753906, 7.401175022125244, "Satellite Component Structure Provides structural support"]
+[-7.577755451202393, 5.878385543823242, "Cameras Quantity 24 normal and 2 fast cameras"]
+[-7.592078685760498, 5.868294715881348, "Cameras Function Provide optical imaging"]
+[2.0614113807678223, -2.408672571182251, "Satellite Emergency Maneuvers 2"]
+[3.7350761890411377, -1.6159173250198364, "Satellite Operation Status Nominal"]
+[2.013056516647339, -1.3777416944503784, "Satellite Imagery Quality Outstanding"]
+[4.501220703125, -2.6690731048583984, "Satellite Time on Orbit One year"]
+[0.32277238368988037, 10.545988082885742, "Vision-Based System Operating Modes Cooperative Mode, Non-cooperative Mode"]
+[-5.157007217407227, 2.8720078468322754, "micro-Advanced Stellar Compass Integration Integrated with the STR (Star Tracker) package"]
+[-5.09812068939209, 2.8615217208862305, "micro-Advanced Stellar Compass Function Output the relative state of the target spacecraft to be referenced in inertial coordinates"]
+[-0.11172770708799362, 15.538086891174316, "Spectrometer Band 1 Spectral Range 0.755 - 0.772 \u00b5m"]
+[-0.07787682861089706, 15.56583023071289, "Spectrometer Band 1 Wave Numbers 12,950 - 13,250"]
+[-0.13652034103870392, 15.553674697875977, "Spectrometer Band 1 Resolution 0.2 cm -1"]
+[-0.0902729406952858, 15.531692504882812, "Spectrometer Band 2 Spectral Range 1.563 - 1.695 \u00b5m"]
+[-0.11541090160608292, 15.540998458862305, "Spectrometer Band 2 Wave Numbers 5900 - 6400"]
+[-0.14647607505321503, 15.55062198638916, "Spectrometer Band 2 Resolution 0.2 cm -1"]
+[-0.12916839122772217, 15.55889892578125, "Spectrometer Band 3 Spectral Range 1.923 - 2.381 \u00b5m"]
+[-0.13085058331489563, 15.579042434692383, "Spectrometer Band 3 Wave Numbers 4200 - 5200"]
+[-0.13871440291404724, 15.550310134887695, "Spectrometer Band 3 Resolution 0.2 cm -1"]
+[-0.06437661498785019, 15.512605667114258, "Spectrometer Band 4 Spectral Range 5.56 - 8.45 \u00b5m"]
+[-0.09516962617635727, 15.565956115722656, "Spectrometer Band 4 Wave Numbers 1183 - 1800"]
+[-0.1354345977306366, 15.601537704467773, "Spectrometer Band 4 Resolution 0.2 cm -1"]
+[-0.1399797946214676, 15.568730354309082, "Spectrometer Band 5 Spectral Range 8.45 - 14.29 \u00b5m"]
+[-0.04498555138707161, 15.61251163482666, "Spectrometer Band 5 Wave Numbers 700 - 1183"]
+[-0.1319190263748169, 15.532238960266113, "Spectrometer Band 5 Resolution 0.2 cm -1"]
+[-0.4574536383152008, 6.832447528839111, "Investigation Equipment Centrifuge Provides a variable gravity environment"]
+[-0.6946358680725098, 6.730870723724365, "Study Purpose Studied cement solidification in microgravity"]
+[-0.3653618395328522, 8.166044235229492, "Material Use Second only to water in terms of use by humanity"]
+[-2.716916561126709, 8.753954887390137, "Module Function Holds the foam insert and slots for two MICS cement packets"]
+[4.090997695922852, 13.935701370239258, "Advanced Topographic Laser Altimeter System Acquisition Date October 19, 2018"]
+[5.3391852378845215, -4.362232208251953, "Satellite Launch Date 15 September 2018"]
+[2.5183091163635254, -1.713208556175232, "Satellite Highest-resolution laser altimeter Yes"]
+[1.2002441883087158, -1.0520472526550293, "Satellite Measurement Height of Earth\u2019s surfaces"]
+[-2.6384122371673584, 11.64614200592041, "Operational Land Imager Image Acquisition Date January 11, 2017"]
+[1.4182854890823364, -2.500908136367798, "Satellite Orbit Type Sun-synchronous"]
+[5.305070877075195, -4.352488040924072, "Satellite Launch Date 23.51962"]
+[5.324411869049072, -4.41155481338501, "Satellite Launch Date 23.8. 1962"]
+[5.373375415802002, -4.371228218078613, "Satellite Launch Date 19.2.19963"]
+[5.144872665405273, -4.427798748016357, "Satellite Reentry Date 26.12.1979"]
+[5.075248718261719, -4.421956539154053, "Satellite Publication Date 15 April 2019"]
+[1.7391948699951172, -2.102881908416748, "Satellite Waypoints Location Around the orbit"]
+[1.6673307418823242, -2.3058366775512695, "Satellite Maneuvers Transition to non-cooperative mode, Non-cooperative hop, Sun-aligned station-keeping maneuver"]
+[2.091007947921753, -1.602757453918457, "Satellite Inspection Cone Angle Limited to meet non-cooperative VBS constraints"]
+[-9.949740409851074, 5.856531143188477, "Search and Rescue Payload Frequency 406 MHz"]
+[-9.958770751953125, 5.8472723960876465, "Search and Rescue Payload Compatibility Full with existing and future 406 MHz beacons"]
+[-9.952801704406738, 5.853343486785889, "Search and Rescue Payload Detection and Location Global near-instantaneous"]
+[1.9017512798309326, -0.26929986476898193, "Satellite Radar Data Type Radar and visible satellite data"]
+[4.786421775817871, -4.483948707580566, "Satellite Image Date July 25, 2019"]
+[-0.7804001569747925, 5.098306179046631, "Location Earthquake Date Early July 2019"]
+[-3.1256983280181885, 4.9226555824279785, "Cargo Resupply Vehicle Cargo Capacity ~2360 kg"]
+[3.7038323879241943, 17.652708053588867, "Science Payload Unknown Unknown"]
+[-7.585625648498535, 5.902248382568359, "Camera Purpose Filming during four increments"]
+[-1.0546106100082397, 7.326550483703613, "Equipment Purpose Future spacewalks to prepare the station for the installation of the new international docking adapters"]
+[3.6998720169067383, 22.9666748046875, "Instrument First Image Capture Date 17 September 2018"]
+[5.471146583557129, -4.4058518409729, "Satellite Engagement Date 4 September 2018"]
+[2.6395328044891357, 5.409012317657471, "Emergency Beacon Frequency 406 MHz"]
+[2.6814124584198, 5.375053405761719, "Emergency Beacon Power 5 W"]
+[2.6621081829071045, 5.3909912109375, "Emergency Beacon GPS Capability Internal or external"]
+[2.6621580123901367, 5.390734672546387, "Emergency Beacon DF (Direction Finder) 406 MHz signal"]
+[4.682700157165527, -4.537293434143066, "Satellite Image Capture Date June 24, 2022"]
+[-0.44459691643714905, 5.057748317718506, "Lake Depth Around 6 m"]
+[-0.494368314743042, 5.152947425842285, "Strait Depth Around 6 m"]
+[-9.944012641906738, 5.8545026779174805, "Search and Rescue System Individuals Rescued 2156"]
+[-9.9522705078125, 5.853842735290527, "Search and Rescue System SAR Events 10385"]
+[2.6636135578155518, 5.389219284057617, "Beacon Quantity in Use 1600000"]
+[2.6730802059173584, 5.381136417388916, "Beacon Production Increase 6.3%"]
+[-2.7245469093322754, 8.673238754272461, "FFSW Module Function Plans, coordinates and manages the formation flying activities of the mission in an autonomous way"]
+[-2.7138421535491943, 8.709623336791992, "FFSW Module Function Coordinates the detection and flag processing coming from the different elements of the FFSW and provides alarms/warnings"]
+[-2.6843910217285156, 8.72498607635498, "FFSW Module Function Controls the relative state (position and attitude) of the formation"]
+[2.029863119125366, 22.64461326599121, "Instrument Wavelength 443 nm"]
+[2.2309584617614746, 22.789325714111328, "Instrument Bandwidth 20 nm"]
+[2.634408473968506, 22.44581413269043, "Instrument Polarization yes"]
+[2.07659649848938, 22.50743865966797, "Instrument Dynamic Range (Normalized Radiance) 0.05-0.22"]
+[2.416163444519043, 22.103336334228516, "Instrument Main Measurement Objective Ocean colour"]
+[1.9103214740753174, 10.721055030822754, "Imaging Device Size 636 pixels (939 pixels for the fast cameras)"]
+[-2.652461051940918, 11.54378604888916, "Image Data Transmission Method Raw data to ground or processed on-board"]
+[-2.5736074447631836, 11.50721549987793, "Image Data Transmission Method Transmitted to ground"]
+[5.329215049743652, -4.41038703918457, "Satellite Launch Date October 2018"]
+[2.8427441120147705, -1.3954477310180664, "Satellite Mission Greenhouse gas monitoring"]
+[8.517669677734375, 13.942791938781738, "Lidar Instrument Maximum Ground Spacing ~2 km at 20 km"]
+[8.518058776855469, 13.941670417785645, "Lidar Instrument Repetition Rate Variable (between 5 and 25 kHz)"]
+[8.514625549316406, 13.941412925720215, "Lidar Instrument Aircraft Speed ~200 m/s"]
+[8.518285751342773, 13.943113327026367, "Lidar Instrument Footprint Sampling ~2 m every ~4 cm along track"]
+[-5.022160053253174, 2.881314277648926, "Space Telescope Purpose Look for planets in orbit around nearby bright stars using the transit method"]
+[-4.567612648010254, -3.0778212547302246, "Exoplanet Size About 1.2 times as big around as Earth"]
+[-4.568900108337402, -3.0827479362487793, "Exoplanet Size 1.5 times as big around as Earth"]
+[-4.547428131103516, -3.1084296703338623, "Exoplanet Temperature 435 \u00b0C"]
+[-4.562819957733154, -3.0943844318389893, "Exoplanet Temperature 284 \u00b0C"]
+[-4.563537120819092, -3.0875635147094727, "Exoplanet Distance from Earth 33 light-years"]
+[3.4721832275390625, 10.554499626159668, "Amplifier Frequency Range 17.7 - 18.8 GHz"]
+[3.47898530960083, 10.555530548095703, "Amplifier Input Power Range -8 to -22 dBm/port"]
+[3.4814088344573975, 10.555853843688965, "Amplifier Total Output Power > 54.5 dBm (about 280 W)"]
+[3.4771041870117188, 10.552083969116211, "Amplifier Inter Port Isolation > 25 dB"]
+[3.4790992736816406, 10.555073738098145, "Amplifier Power Consumption < 1385 W"]
+[3.4767887592315674, 10.555084228515625, "Amplifier Number of TWTA 8"]
+[3.47356915473938, 10.557944297790527, "Amplifier TWTA Output Power 90 W max (saturation)"]
+[3.4693708419799805, 10.55858325958252, "Amplifier TWTA Output Power Nominal operation: 50 W (MPA operation in linear range)"]
+[3.483154535293579, 10.552838325500488, "Amplifier Gain Variable Range/Step Range: 0 to 3 dB Step: 0.5 dB"]
+[3.463188886642456, 10.554121971130371, "Amplifier Phase Variable Range/Step Range: 0 to 45\u00ba"]
+[3.4756903648376465, 10.554754257202148, "Amplifier Phase Variable Range/Step Range: 0 to 360\u00ba; Step: 90\u00ba"]
+[11.287422180175781, 5.580192565917969, "CubeSat Mission Duration 1 year"]
+[11.289826393127441, 5.554391860961914, "CubeSat Release Date October 2015"]
+[11.263616561889648, 5.488787651062012, "CubeSat Receiver Types ADS-B tracking signals, telecom satellite signals, X-band signals"]
+[11.2654390335083, 5.481476783752441, "CubeSat Receiver Reconfiguration Recorded the information in the aircraft signals needed by the UK Met Office"]
+[-5.918530464172363, 8.399214744567871, "Communication Channel Not Applicable Not Applicable"]
+[-5.9247894287109375, 8.383481979370117, "Communication Channel Center Frequency 50.3 GHz"]
+[-5.9009552001953125, 8.399531364440918, "Communication Channel Bandwidth/Passband 400 MHz"]
+[-5.984284400939941, 8.334647178649902, "Communication Channel Footprint 25.8 x 17.5 km"]
+[-5.9744038581848145, 8.361509323120117, "Communication Channel Polarization Horizontal"]
+[-5.908764839172363, 8.391792297363281, "Communication Channel NE\u0394T 0.4 K"]
+[-5.928389072418213, 8.38037395477295, "Communication Channel Center Frequency 52.8 GHz"]
+[-5.897419452667236, 8.39983081817627, "Communication Channel Bandwidth/Passband 400 MHz"]
+[-5.986690044403076, 8.339048385620117, "Communication Channel Footprint 25.8 x 17.5 km"]
+[-5.954921722412109, 8.383649826049805, "Communication Channel Polarization Horizontal"]
+[-5.91146993637085, 8.401727676391602, "Communication Channel NE\u0394T 0.4 K"]
+[-5.917797088623047, 8.372526168823242, "Communication Channel Center Frequency 53.596 GHz"]
+[-5.896026611328125, 8.395416259765625, "Communication Channel Bandwidth/Passband 400 MHz"]
+[-5.98733377456665, 8.338701248168945, "Communication Channel Footprint 25.8 x 17.5 km"]
+[-5.949507236480713, 8.390007019042969, "Communication Channel Polarization Horizontal"]
+[-5.9120073318481445, 8.395550727844238, "Communication Channel NE\u0394T 0.4 K"]
+[-5.969788074493408, 8.345911026000977, "Communication Channel Center Frequency 54.4 GHz"]
+[-5.898794174194336, 8.396289825439453, "Communication Channel Bandwidth/Passband 400 MHz"]
+[-6.004987716674805, 8.319903373718262, "Communication Channel Footprint 25.8 x 17.5 km"]
+[-5.956265449523926, 8.378233909606934, "Communication Channel Polarization Horizontal"]
+[-5.914395332336426, 8.405662536621094, "Communication Channel NE\u0394T 0.4 K"]
+[-5.9451751708984375, 8.383647918701172, "Communication Channel Center Frequency 55.5 GHz"]
+[-5.907641887664795, 8.39898681640625, "Communication Channel Bandwidth/Passband 400 MHz"]
+[-5.989276885986328, 8.337274551391602, "Communication Channel Footprint 25.8 x 17.5 km"]
+[-5.958756923675537, 8.397252082824707, "Communication Channel Polarization Horizontal"]
+[-5.893921375274658, 8.420713424682617, "Communication Channel NE\u0394T 0.4 K"]
+[-5.953374862670898, 8.411975860595703, "Communication Channel Center Frequency 57.29 GHz"]
+[-5.919734001159668, 8.403217315673828, "Communication Channel Bandwidth/Passband 350 MHz"]
+[-5.9893083572387695, 8.334214210510254, "Communication Channel Footprint 25.8 x 17.5 km"]
+[-5.9000468254089355, 8.390064239501953, "Communication Channel NE\u0394T 0.5 K"]
+[-5.945067882537842, 8.387551307678223, "Communication Channel Center Frequency 59.4 GHz"]
+[-5.932800769805908, 8.392797470092773, "Communication Channel Bandwidth/Passband 250 MHz"]
+[-5.990440368652344, 8.33204174041748, "Communication Channel Footprint 25.8 x 17.5 km"]
+[-5.8960089683532715, 8.393596649169922, "Communication Channel NE\u0394T 0.6 K"]
+[-5.934021949768066, 8.397300720214844, "Communication Channel Center Frequency 150.0 GHz"]
+[-5.875150203704834, 8.36661434173584, "Communication Channel Bandwidth/Passband 1500 MHz"]
+[-5.9873881340026855, 8.346016883850098, "Communication Channel Footprint 14.4 x 13.1 km"]
+[-3.0135231018066406, 4.277306079864502, "Spacecraft Maximum Orbit-Average Power Dissipation 24 W"]
+[-3.037825584411621, 4.292623043060303, "Spacecraft Operational Mode Safe Mode"]
+[-3.1367177963256836, 4.379263877868652, "Spacecraft Power Dissipation 24 W"]
+[-1.3839956521987915, 6.9207682609558105, "Model Purpose Evaluate surface treatments and other design decisions"]
+[1.8362149000167847, -1.5503058433532715, "Satellite Spectral Parameters LWIR: 700-1130 cm -1  (14.3-8.85 \u00b5m), S/MWIR :  1650-2250 cm -1  (6.06-4.44 \u00b5m), VIS: 0.55-0.75 \u00b5m"]
+[1.5134168863296509, -1.2334625720977783, "Satellite Spatial Resolution LWIR/S/MWIR : 16 km, VIS : 2 km"]
+[2.086028575897217, -1.7852305173873901, "Satellite Operational Mode China area: 5000 km x 5000 km, Mesoscale area: 1000 km x 1000 km"]
+[3.644752025604248, -2.494050979614258, "Satellite Temporal Resolution China area < 1 hr, Mesoscale area < \u00bd hr"]
+[1.6760108470916748, -1.7502286434173584, "Satellite Sensitivity LWIR: 0.5 -1.1 mW/m2 sr cm -1, S/MIR: 0.1-0.14 mW/m2 sr cm -1, VIS: S/N> 200(\u03c1=100%), LWIR: 0.3 mW/m2 sr cm -1, S/MIR: 0.06 mW/m2 sr cm -1"]
+[1.5361272096633911, -1.6151626110076904, "Satellite Calibration Accuracy 1.5 K (3\u03c3) radiation, 1.0 K (3\u03c3), 10 ppm (3\u03c3) spectrum, 5 ppm (3\u03c3)"]
+[2.4484615325927734, -2.0136513710021973, "Satellite Data Quantization 13 bit"]
+[0.6288773417472839, -1.492857575416565, "Satellite Orbit Altitude 720 km"]
+[0.7585297226905823, -2.242290496826172, "Satellite Orbit Inclination 98.1\u00ba"]
+[3.8492796421051025, -3.1618237495422363, "Satellite LTAN 9:20 hours"]
+[14.67971420288086, 7.813853740692139, "Nanosatellite Mass ~10 kg"]
+[14.68973445892334, 7.81871223449707, "Nanosatellite Mass 5.3 kg"]
+[16.801834106445312, 6.8921589851379395, "Microsatellite Mass ~44 kg"]
+[16.782306671142578, 6.911797046661377, "Microsatellite Mass 103 kg"]
+[16.823577880859375, 6.877090930938721, "Microsatellite Mass 117 kg"]
+[14.69089412689209, 7.8202290534973145, "Nanosatellite Mass 8 kg"]
+[-3.5353591442108154, 4.382646560668945, "Spacecraft Landing Date Dec. 5, 2014"]
+[-3.0824148654937744, 4.261822700500488, "Spacecraft URL http://www.nasa.gov/exploration/systems/mpcv/test_flight_2014.html#.UyqgYM52H5p"]
+[7.260275840759277, 12.427876472473145, "Satellite Instrument Centre Frequencies 6.925 GHz, 10.65 GHz, 18.7 GHz, 23.8 GHz, 36.5 GHz, 50.3 GHz, 52.8 GHz, 89.0A GHz, 89.0B GHz"]
+[7.265435695648193, 12.370930671691895, "Satellite Instrument Bandwidth 350 MHz, 100 MHz, 200 MHz, 400 MHz, 1000 MHz, 200 MHz, 400 MHz, 3000 MHz, 3000 MHz"]
+[7.293243408203125, 12.413795471191406, "Satellite Instrument Radiometric Resolution 0.34 K, 0.7 K, 0.7 K, 0.6 K, 0.7 K, 1.8 K, 1.6 K, 1.2 K, 1.2 K"]
+[7.289275646209717, 12.408186912536621, "Satellite Instrument Spatial Resolution 40x70 km, 27x46 km, 14x25 km, 17x29 km, 8x14 km, 6x10 km, 6x10 km, 3x6 km, 3x6 km"]
+[7.33061408996582, 12.45517349243164, "Satellite Instrument 3dB Beam Width 1.8\u00ba, 1.2\u00ba, 0.65\u00ba, 0.75\u00ba, 0.35\u00ba, 0.25\u00ba, 0.25\u00ba, 0.15\u00ba, 0.15\u00ba"]
+[7.295569896697998, 12.415983200073242, "Satellite Instrument Antenna Parabolic, Aperture Diameter = 2 m, Conical Scan"]
+[7.289693832397461, 12.402775764465332, "Satellite Instrument Incidence Angle 55\u00ba, 54.5\u00ba"]
+[7.2785325050354, 12.40151309967041, "Satellite Instrument Integration Time 2.5 ms, 1.2 ms"]
+[7.264577388763428, 12.382943153381348, "Satellite Instrument Polarization H/V (horizontal and vertical), H (vertical), H/V"]
+[7.288397789001465, 12.410510063171387, "Satellite Instrument Antenna Scan Rate 40 rpm (1.5 s/scan)"]
+[7.301061153411865, 12.40404224395752, "Satellite Instrument Cross-polarization Less than\u00d7-20 dB"]
+[7.283079147338867, 12.413100242614746, "Satellite Instrument Swath Width 1600 km"]
+[7.308392524719238, 12.384220123291016, "Satellite Instrument Dynamic Range 2.7 K to 340 K"]
+[7.28088903427124, 12.411666870117188, "Satellite Instrument Absolute Accuracy 1 K (1 sigma)"]
+[7.2345499992370605, 12.344155311584473, "Satellite Instrument A/D Quantization 12 bit, 10 bit"]
+[7.259576320648193, 12.373635292053223, "Satellite Instrument Data Rate 130 kbit/s"]
+[7.279000759124756, 12.390936851501465, "Satellite Instrument Mass 320 kg"]
+[7.278177738189697, 12.399077415466309, "Satellite Instrument Power 400 W"]
+[0.6386027336120605, -1.481534719467163, "Satellite Orbit Altitude 700 km"]
+[0.7916821837425232, -2.223005771636963, "Satellite Orbit Inclination 98\u00ba"]
+[1.3591662645339966, 7.073110580444336, "Communication Equipment Data Transfer Time About 2 minutes per day"]
+[1.3867430686950684, 7.053715705871582, "Communication Equipment Data Transfer Rate 9600 baud"]
+[2.642932176589966, -2.529419183731079, "Satellite Data Download Limit About 1Mb per day"]
+[0.59861159324646, -1.4547446966171265, "Satellite Orbit Altitude 550 km"]
+[-2.6736347675323486, 11.677450180053711, "Imager Field-of-View Wide"]
+[-2.625436782836914, 11.711584091186523, "Imager Purpose Make measurements of the Earth's space environment in soft X-rays"]
+[5.262753486633301, -4.027921676635742, "Satellite Launch Date 2016"]
+[3.3054542541503906, 0.41530153155326843, "Satellite Program Ownership NOAA"]
+[1.41298246383667, 2.6456706523895264, "Defense Weather Satellite System Procurement DoD"]
+[-2.3384175300598145, 7.347349166870117, "OnBoard Computer  "]
+[-8.139890670776367, 8.82898235321045, "Electrical Power Subsystem  "]
+[2.736015796661377, -2.8334507942199707, "Inter-Satellite Link  "]
+[-1.9371991157531738, 7.879304885864258, "Control Board  "]
+[-0.6483424305915833, 8.537632942199707, "Momentum Wheel  "]
+[-2.0201964378356934, 7.906968593597412, "AOCS  "]
+[-1.9506723880767822, 7.9558186531066895, "AOCS  "]
+[6.17019510269165, 7.572200298309326, "Satellite Component  "]
+[-3.6297237873077393, 12.755426406860352, "Particle Physics Detector Measurement Events 41 billion cosmic ray events"]
+[-3.6709084510803223, 12.723443984985352, "Particle Physics Detector Flux Measurement Smooth"]
+[-3.6153533458709717, 12.73198127746582, "Particle Physics Detector Spectral Index Single, constant"]
+[-3.639350652694702, 12.763370513916016, "Particle Physics Detector Positron Fraction Precision measurements"]
+[3.2626523971557617, -1.777381420135498, "Satellite Manufacturer GAIN (Galileo Industries S. A.)"]
+[2.7336010932922363, -2.0249109268188477, "Satellite Former Name GSTB-V2/B"]
+[3.9019315242767334, -2.819838762283325, "Satellite Clock Type Rubidium atomic clock"]
+[3.569335460662842, -2.824479103088379, "Satellite Clock Type Hydrogen-maser clock"]
+[2.605332136154175, -2.247349500656128, "Satellite Signal Transmission Two separate channels"]
+[2.6340906620025635, -2.2348177433013916, "Satellite Signal Transmission Three separate channels"]
+[-6.762448787689209, 9.954522132873535, "Electric Field Antenna Frequency Range DC to 3.3 MHz"]
+[-6.6800031661987305, 9.941489219665527, "Electric Field Antenna ULF Frequency Range 0 \u2013 64 Hz"]
+[-6.7264204025268555, 9.984396934509277, "Electric Field Antenna VLF Frequency Range Few Hz to 20 kHz"]
+[-3.1561853885650635, 7.622539043426514, "Data Processing Unit Components Electric field antenna, magnetic field antenna, Ion probe"]
+[2.1061387062072754, -1.261481761932373, "Satellite Imaging Satellite High-resolution optical imaging"]
+[-1.3418227434158325, 6.107724189758301, "Company Export License Refused by the German government"]
+[-1.3465158939361572, 6.066877365112305, "Company Export Approval Provided by the French government"]
+[3.319336414337158, 0.462796151638031, "Satellite Program Name Change FormoSat"]
+[-3.2508533000946045, 4.243315696716309, "Space Probe Nitrogen Variation Up to 38 percent"]
+[-3.2330875396728516, 4.240818977355957, "Space Probe Oxygen Variation Up to 7 percent"]
+[-0.604174792766571, 3.2314419746398926, "Star Nitrogen Enrichment Unknown"]
+[-0.6326253414154053, 3.2242989540100098, "Star Composition Unknown"]
+[2.630506992340088, 12.192551612854004, "Beam Mode Minimum Beam Mode Detectable Ship Length (MDSL) 25-95 m"]
+[2.6289074420928955, 12.187628746032715, "Beam Mode Minimum Beam Mode Detectable Ship Length (MDSL) 51-190 m"]
+[2.632134437561035, 12.19597339630127, "Beam Mode Minimum Beam Mode Detectable Ship Length (MDSL) 29-358 m"]
+[2.6297428607940674, 12.20525074005127, "Beam Mode Minimum Beam Mode Detectable Ship Length (MDSL) 61-639 m"]
+[-0.8155884146690369, 0.14509375393390656, "Satellite System Architecture Ground Mission Segment, GESS network, GIOVE Mission segment"]
+[-2.5722992420196533, 2.7540743350982666, "Ground Mission Segment Upgrade Year 2005"]
+[5.301029682159424, -4.45548152923584, "Satellite Signal Broadcast Start Date January 12, 2006"]
+[0.5321460962295532, -1.4869316816329956, "Satellite Orbit Altitude 684 km"]
+[0.9775221347808838, -1.3638544082641602, "Satellite Ground Surface Coverage 9,850,000 km2"]
+[2.4456348419189453, -1.8189374208450317, "Satellite Reconnaissance Missions Over 4800"]
+[1.848872184753418, -2.5033106803894043, "Satellite Orbits Completed 5344"]
+[3.0005595684051514, -2.7403318881988525, "Telecommunications Satellite Manufacturer Thales Alenia Space"]
+[2.7284231185913086, -3.164829730987549, "Military Communication Satellite Manufacturer Thales Alenia Space"]
+[4.14000129699707, -3.7337982654571533, "Telecommunications Satellite Launch Date 24 October 2021"]
+[3.7735629081726074, -3.3861470222473145, "Telecommunications Satellite Launch Time 02:10 UTC"]
+[2.9690940380096436, -2.8610527515411377, "Telecommunications Satellite Launch Vehicle Ariane 5 ECA"]
+[3.0137341022491455, -2.861785411834717, "Telecommunications Satellite Launch Site Launch Complex ELA-3 in Kourou"]
+[0.5054497122764587, 12.276898384094238, "Sensor Pan (panchromatic) 420-890 nm"]
+[2.6735079288482666, 14.251139640808105, "Optical Instrument Aperture 30 cm"]
+[0.5731046795845032, 12.139636039733887, "Sensor IFOV 3.68 \u00b5rad"]
+[0.633060097694397, 12.114503860473633, "Sensor IFOV 7.35 \u00b5rad"]
+[0.49204200506210327, 12.225042343139648, "Sensor Spatial Resolution 2.5 m"]
+[0.5274587273597717, 12.207719802856445, "Sensor Spatial Resolution 5 m"]
+[0.4968878924846649, 12.17054271697998, "Sensor Swath Width 20 km"]
+[0.47115859389305115, 12.211095809936523, "Sensor Swath Width 20 km"]
+[0.4639231562614441, 12.205172538757324, "Sensor MTF Pan: \u2265 8.0% @ Nyquist frequency"]
+[0.5662379264831543, 12.18508243560791, "Sensor MTF MS: \u2265 12.0% @ Nyquist frequency"]
+[0.6810862421989441, 12.070662498474121, "Sensor Data Quantization 8 bit"]
+[0.5449479222297668, 12.193443298339844, "Sensor Data Storage Capacity 64 Gbit"]
+[0.5487273335456848, 12.13654899597168, "Sensor Mass 38.7 kg"]
+[0.6569585204124451, 12.1373929977417, "Sensor Power 52.3 W (max), 14 W (standby)"]
+[0.4758283197879791, 12.271828651428223, "Sensor Physical Size Optics: \u00d8 420 mm x 755 mm, Electronics : 320 mm x 215 mm x165 (mm)"]
+[4.242741107940674, -2.5104830265045166, "Satellite Revisit Time 5 days"]
+[4.178704261779785, -2.483797311782837, "Satellite Revisit Time 10 days"]
+[1.1088470220565796, -1.372038722038269, "Satellite Swath Width 290 km"]
+[1.4847334623336792, -1.1303216218948364, "Satellite Spatial Resolution 10 m, 20 m, and 60 m"]
+[1.2113378047943115, -1.6046539545059204, "Satellite Geolocation Accuracy < 20 m"]
+[1.6866581439971924, -1.3477466106414795, "Satellite Radiometric Image Quality Very good"]
+[1.3835803270339966, -3.1002197265625, "Satellites Measurement Gravitational pull exerted by massive bodies such as ice sheets"]
+[1.3633416891098022, -3.1253738403320312, "Satellites Measurement Weight, or mass, of the object below"]
+[4.699039459228516, -4.5287346839904785, "Satellite Image Capture Date June 2020"]
+[4.669234275817871, -4.537918567657471, "Satellite Image Capture Date June 2022"]
+[-0.4471770226955414, 4.8791890144348145, "Island History Long history of eruptions"]
+[-0.4771709144115448, 4.910658359527588, "Island Age Between 12 and 20 million years"]
+[5.33265495300293, -4.444465160369873, "Satellite Launch Date Aug. 23, 1962"]
+[0.9946383833885193, -4.395780086517334, "Satellite Mass 91 kg"]
+[0.8426119089126587, -1.6531533002853394, "Satellite Orbit Perigee 578 km"]
+[0.7766097784042358, -1.6625866889953613, "Satellite Orbit Apogee 752 km"]
+[0.7211588025093079, -2.2485549449920654, "Satellite Orbit Inclination 98.5\u00ba"]
+[4.157721042633057, -2.81607723236084, "Satellite Orbit Period 98.1 min"]
+[5.3893818855285645, -4.504756927490234, "Satellite Launch Date Feb. 19, 1963"]
+[1.001670002937317, -4.422489643096924, "Satellite Mass 40 kg"]
+[1.0199040174484253, -1.7713627815246582, "Satellite Orbit Perigee 488 km"]
+[0.7261917591094971, -1.6365944147109985, "Satellite Orbit Apogee 810 km"]
+[0.7510557174682617, -2.270819664001465, "Satellite Orbit Inclination 100.5\u00ba"]
+[4.155834197998047, -2.8320627212524414, "Satellite Orbit Period 98.7 min"]
+[1.9621297121047974, -1.3416787385940552, "Satellite Laser Altimeter Measures the height of the first substance it hits"]
+[2.4344711303710938, -1.2093818187713623, "Satellite Open Water Detection Open water within a lead shows up in the satellite data as a very flat surface"]
+[2.4570772647857666, -1.1427805423736572, "Satellite Sea Ice Detection The comparatively textured surface of sea ice"]
+[4.936546325683594, -4.23918342590332, "Satellite Detection Period October 2019 through April 2020"]
+[3.5988574028015137, -2.528712272644043, "Satellite Data Filter Month"]
+[2.5323543548583984, -1.8471733331680298, "Satellite Next Step Building a statistical model"]
+[3.4611356258392334, 13.474605560302734, "Laser Stabilization System Material Zerodur or ULE"]
+[3.5160021781921387, 13.46272087097168, "Laser Stabilization System Thermal Expansion Coefficient 3 x 10-8/K"]
+[3.552116632461548, 13.461739540100098, "Laser Stabilization System Insulation Yes"]
+[5.26902961730957, -4.418403625488281, "Satellite Launch Date December 19, 2013"]
+[-3.1060094833374023, 2.3980791568756104, "Mission Purpose Provide precise characteristics of thousands of exoplanet systems"]
+[-5.449260711669922, 2.8752806186676025, "Telescope Component Glass Segmentation Unknown"]
+[-5.448158264160156, 2.8542282581329346, "Telescope Component Support Spiders Unknown"]
+[-5.517341613769531, 2.918757677078247, "Telescope Component Polyimide Thermal Shield Unknown"]
+[-5.509640216827393, 2.909247398376465, "Telescope Component Intermediate Mandrel (IM) Unknown"]
+[-5.471922874450684, 2.8775253295898438, "Telescope Component IM Glass Blue"]
+[-5.476579189300537, 2.901261806488037, "Telescope Component IM Spacers Light Blue"]
+[-5.442070960998535, 2.8712878227233887, "Telescope Component Spacers Gray"]
+[-5.471083164215088, 2.8445632457733154, "Telescope Component Sextants and Dodecants Unknown"]
+[-0.07895433157682419, 15.496296882629395, "Ion Spectrometer Field of View 26\u00ba starting along the spin axis by about 3\u00ba in azimuth"]
+[-0.07124145328998566, 15.48567008972168, "Ion Spectrometer Energy Steps 40 per spectrum"]
+[-0.02463080920279026, 15.427881240844727, "Ion Spectrometer Energy Range 200 eV/q to 25 keV/q"]
+[-0.07390604168176651, 15.519415855407715, "Ion Spectrometer Sky Circle Radius ~24\u00ba"]
+[-13.831482887268066, -2.1802189350128174, "X-ray Monitor Telescope Modules 5"]
+[-13.863380432128906, -2.208718776702881, "X-ray Monitor MCP Optics per Telescope Module Approximately 60"]
+[-13.8436918258667, -2.2063939571380615, "X-ray Monitor Source Transit Time 300-1800 s"]
+[-2.164334535598755, 2.8820202350616455, "Space Observatory Position Lagrange point L2 of the Sun-Earth system"]
+[2.068131685256958, -2.689650297164917, "Satellite Number of CubeSat Units 3"]
+[2.061856985092163, -2.6564784049987793, "Satellite Number of CubeSat Units 1 x 3"]
+[2.06911301612854, -2.6975765228271484, "Satellite Number of CubeSat Units 3"]
+[2.1107077598571777, -2.6701292991638184, "Satellite Number of CubeSat Units 1"]
+[2.0645766258239746, -2.7249372005462646, "Satellite Number of CubeSat Units 3"]
+[2.0945043563842773, -2.639000415802002, "Satellite Number of CubeSat Units 1"]
+[2.055168867111206, -2.7098140716552734, "Satellite Number of CubeSat Units 3"]
+[2.0985348224639893, -2.671243190765381, "Satellite Number of CubeSat Units 1"]
+[2.1109540462493896, -2.649832248687744, "Satellite Number of CubeSat Units 1"]
+[2.109163284301758, -2.6738533973693848, "Satellite Number of CubeSat Units 1"]
+[2.2478322982788086, 13.436914443969727, "Optical Sensor Telescope Type TMA (Three Mirror Anastigmat)"]
+[2.200505018234253, 13.39222240447998, "Optical Sensor Primary Mirror Material NTSIC (New Technology Silicon Carbide)"]
+[2.186086654663086, 13.412188529968262, "Optical Sensor SiC Strength Two to three times higher than a conventional sintered SiC"]
+[16.803144454956055, 6.89329719543457, "Microsatellite Mass 103 kg"]
+[16.890092849731445, 6.81976318359375, "Microsatellite Payload Earth imaging payload with panchromatic and multispectral cameras"]
+[1.0026994943618774, -4.406450271606445, "Satellite Mass 117 kg"]
+[2.5661768913269043, -1.7582676410675049, "Satellite Payload NAOMI (New AstroSat Optical Modular Instrument)"]
+[14.65501880645752, 7.788894176483154, "Nanosatellite Mass 8 kg"]
+[0.9067932963371277, 14.798882484436035, "Instrumentation Sensor Complement Unknown"]
+[0.9039454460144043, 14.795389175415039, "Instrumentation EVA Duration 6 hr 19 min"]
+[0.9045694470405579, 14.801105499267578, "Instrumentation Astronauts Andrew Feustel, Greg Chamitoff"]
+[0.9078769087791443, 14.800056457519531, "Instrumentation EVA Date May 20, 2011"]
+[0.9104055166244507, 14.797947883605957, "Instrumentation Image Credit NASA, ESA, Ref. 68"]
+[-1.455822467803955, 1.238412618637085, "Data Relay Satellite Data Relay Service Sentinel-1 and -2"]
+[1.6063705682754517, 2.2736093997955322, "Geostationary Satellite Data Relay Ka-band link"]
+[1.6299835443496704, 2.225698709487915, "Geostationary Satellite Downlink Encryption Planned"]
+[-1.4490225315093994, 1.2114264965057373, "Data Relay Satellite Bit Rates 600 Mbit/s and higher"]
+[-0.6351452469825745, 3.2057106494903564, "Star Type Mass 1.5-2.5 times the Sun\u2019s mass"]
+[-0.6386472582817078, 3.204658269882202, "Star Type Rotation Once or twice a day"]
+[-0.6372034549713135, 3.1860129833221436, "Star Type Difficulty of Pulsation Interpretation Complicated and difficult"]
+[0.3979117274284363, 12.39113712310791, "Sensor Centre Frequency 1.275 GHz"]
+[0.5140025615692139, 12.270197868347168, "Sensor Wavelength 23.5 cm"]
+[0.4027591645717621, 12.398381233215332, "Sensor System Bandwidth 19 MHz"]
+[0.5909358263015747, 12.164217948913574, "Sensor PRF 1464-1640 Hz"]
+[0.47951963543891907, 12.248526573181152, "Sensor Dimensions 10.74 m x 2.16 m"]
+[0.673782467842102, 12.034724235534668, "Sensor Look Angle 20\u00ba"]
+[0.4919934868812561, 12.221741676330566, "Sensor Ground Incidence Angle 23\u00ba\u00b13\u00ba cross track"]
+[0.6764237284660339, 12.033818244934082, "Sensor Type 1024-element passive microstrip-based arrays antenna, linearly polarized"]
+[0.4305279850959778, 12.308831214904785, "Sensor Pixel Size 25 m x 25 m"]
+[0.5149796009063721, 12.183676719665527, "Sensor Swath Width 100 km"]
+[0.5079715847969055, 12.207194328308105, "Sensor Transmitted Peak Power 1 kW"]
+[1.6916934251785278, 6.9541449546813965, "Communication Device Purpose Exchange data between the different elements of the constellation or network spacecrafts"]
+[1.696679711341858, 6.933261871337891, "Communication Device Requirements Lower latencies and transmission error rates"]
+[1.7009059190750122, 6.959723949432373, "Communication Device Operation Usually operate without any ground intervention"]
+[-5.367275714874268, 2.846673011779785, "Telescope Aperture 150 mm"]
+[-5.380950927734375, 2.8001887798309326, "Telescope FOV 1.38\u00ba"]
+[-5.431151866912842, 2.759974479675293, "Telescope IFOV 24 \u00b5rad"]
+[-5.368725299835205, 2.7778472900390625, "Telescope GSD 15 m"]
+[-5.375948905944824, 2.792029619216919, "Telescope Field of Incident Angle 0\u00ba to 0.69\u00ba"]
+[-5.335887908935547, 2.827784299850464, "Telescope Material CFRP (Carbon Fiber Reinforced Plastic)"]
+[-5.384191036224365, 2.806796073913574, "Telescope Primary Mirror Material Clearceram\u00ae of OHARA, Inc., Japan"]
+[-5.376724720001221, 2.785709857940674, "Telescope Secondary Mirror Material Fused silica"]
+[5.352975368499756, -4.412118434906006, "Satellite Launch Date December 28, 2005"]
+[5.030439376831055, -4.159605503082275, "Satellite End of Life Date November 24, 2021"]
+[3.2050039768218994, -1.537592887878418, "Satellite Mission Type Non-EO"]
+[3.0055713653564453, -1.5949079990386963, "Satellite Agency ESA"]
+[2.6116409301757812, -1.7528133392333984, "Satellite Overview GIOVE is the \"Galileo In-Orbit Validation Element\", a forerunner and technology demonstration project of the European Galileo constellation"]
+[5.265102386474609, -4.416958332061768, "Satellite Launch Date 6 November 2014"]
+[5.076853275299072, -4.108307838439941, "Satellite End of Life Date 6 November 2019"]
+[3.689626455307007, 22.964548110961914, "Instrument Completion Date Oct. 9, 2014"]
+[0.22379834949970245, 13.790018081665039, "Calibration Component Size 700 x 250 mm2"]
+[3.6132709980010986, 22.25999641418457, "Instrument Component Door Stability Stable without power supply"]
+[-1.2659833431243896, 7.537392616271973, "Launch Locking Device Function Provides a reliable launch locking device and allows after pin retraction the mechanism to rotate in both senses"]
+[0.5235766172409058, 9.437989234924316, "Attitude Determination and Control System Sensors Fine and coarse sun sensors, magnetometers, rate gyro"]
+[0.537217915058136, 9.41375732421875, "Attitude Determination and Control System Calibration Duration About one month"]
+[0.5439587235450745, 9.402586936950684, "Attitude Determination and Control System Attitude Control Performance Capable of periods of 1 degree pointing (1\u03c3)"]
+[0.5207515358924866, 9.425527572631836, "Attitude Determination and Control System Attitude Control Performance Suffers from worse performance when the orientation vectors (magnetic and sun) are close together or during the eclipse"]
+[-1.8497041463851929, 7.590803146362305, "Onboard Device Transmitter Frequencies 401.25 MHz, 2036.25 MHz"]
+[-1.324849247932434, 7.641421794891357, "Onboard Device Message Duration 0.8 seconds"]
+[-1.3610047101974487, 7.606499195098877, "Onboard Device Message Repeat Interval 10 seconds"]
+[2.5629875659942627, 5.351572513580322, "Ground Location Beacon Transmission Frequency Unknown"]
+[2.5887036323547363, 5.369504928588867, "Ground Location Beacon Transmission Interval Once, twice, or three times every minute"]
+[4.269680023193359, -2.8244471549987793, "Satellite Data Processing Time to Level 1 Image 13 minutes"]
+[4.300428867340088, -2.7479519844055176, "Satellite Ship Detection Information Availability 18 minutes"]
+[-2.0519766807556152, 7.946220874786377, "Service Ship Detection Data Processing Time 18 minutes"]
+[4.252954006195068, -2.802427291870117, "Satellite Data Transfer Time to Ground More than an hour"]
+[-1.980240821838379, 8.029948234558105, "Service Data Transfer Time from Satellite to Ground More than an hour"]
+[-3.1601290702819824, 5.352680683135986, "Vehicle Use Traverse along 88 degrees south"]
+[-3.0948424339294434, 2.434866428375244, "Mission Duration Late October to late November 2017"]
+[-3.0946102142333984, 2.404921531677246, "Mission Purpose Map the snow and ice of Antarctica"]
+[-3.0032010078430176, 4.299557685852051, "Spacecraft Platform Size 5.5 m in length, 6.6 m in height, and 2.8 m in width"]
+[-3.0529515743255615, 4.177540302276611, "Spacecraft Solar Array Size 8.9 m x 3.3 m"]
+[-2.9715261459350586, 4.318671226501465, "Spacecraft Subsystems Command and data handling, Attitude determination and control, Electrical power"]
+[-3.0477945804595947, 4.345745086669922, "Spacecraft Components Solar array, Three batteries"]
+[-7.347147464752197, 6.1198577880859375, "Camera System Bands Up to 760 nm"]
+[-7.378986835479736, 6.089946746826172, "Camera System Wavelength for Ozone Measurement Near 600 nm"]
+[-7.3671345710754395, 6.102156639099121, "Camera System Wavelength for Oxygen Absorption Measurement Near 760 nm"]
+[-7.377777576446533, 6.091989517211914, "Camera System Wavelength for Ozone Measurement 322 nm"]
+[-7.32901668548584, 6.142385959625244, "Camera System Wavelength for Pointing Information 350 nm"]
+[-1.8225622177124023, 14.961695671081543, "Imaging Radiometer Telescope Primary Aperture Diameter 400 mm"]
+[-1.7360223531723022, 14.980810165405273, "Imaging Radiometer Telescope Secondary Aperture Diameter 140 mm"]
+[-1.7902791500091553, 14.96394157409668, "Imaging Radiometer Telescope VIS Focal Length 3650 mm"]
+[-1.7935214042663574, 14.999075889587402, "Imaging Radiometer Telescope WV and IR Focal Length 535 mm"]
+[-1.7494850158691406, 15.043359756469727, "Imaging Radiometer HgCdTe Detectors Cooling Temperature 90 K"]
+[-1.8116012811660767, 14.960575103759766, "Imaging Radiometer Earth Disk Scanning Time 30 min"]
+[-1.8196474313735962, 14.976147651672363, "Imaging Radiometer Telescope Rotation Angle 1.25 x 10-4 radians"]
+[3.2166190147399902, 2.3748884201049805, "Satellite Management Subsystem Components Versatile onboard computer(SpaceCube2), Telemetry/Command interface module, SpaceWire router, Network data recorder, Standard middleware, Software development kit"]
+[-2.3385910987854004, 7.318341255187988, "Onboard Computer Type Versatile"]
+[-4.864519119262695, 8.131731986999512, "Communication Module Type Telemetry/Command interface module"]
+[1.489166498184204, 6.977462291717529, "Network Device Type SpaceWire router"]
+[-3.6580421924591064, 7.631469249725342, "Data Recorder Type Network data recorder"]
+[-1.9176853895187378, 6.882417678833008, "Software Type Standard middleware"]
+[-1.9279565811157227, 6.894789695739746, "Software Type Software development kit"]
+[11.062166213989258, 5.377439498901367, "CubeSat Space Telescope Pointing Error Arcsec-level"]
+[11.07487678527832, 5.383578777313232, "CubeSat Space Telescope Focal Plane Temperature Control Highly stable"]
+[11.03436279296875, 5.370935916900635, "CubeSat Space Telescope Objective Demonstrate new technologies for studying nearby stars"]
+[11.043959617614746, 5.3647565841674805, "CubeSat Space Telescope Function Stabilizes the position of a star image on the telescope detector"]
+[11.026479721069336, 5.363822937011719, "CubeSat Space Telescope Function Returns a star image to the same location on the telescope detector"]
+[11.0237455368042, 5.393064498901367, "CubeSat Space Telescope Function Holds the temperature of the telescope detector constant"]
+[10.949322700500488, 5.30820369720459, "CubeSat Space Telescope Function Downloads images of the star so that its brightness can be observed over time"]
+[-0.7826045155525208, 12.669441223144531, "Radiation Dose Rate Sensor Provider DERA"]
+[-0.4421652853488922, 8.63641357421875, "Cryocooler Vibration Suppression Experiment Provider BMDO"]
+[-0.3335787355899811, 8.602038383483887, "Cryocooler Vibration Suppression Experiment Objective To demonstrate and to qualify a new vibration suppressing design by employing piezo materials"]
+[-0.3725351393222809, 8.674468994140625, "Cryocooler Vibration Suppression Experiment Use To use these low-power flight piezo drivers and control systems in zero-g environments"]
+[1.449199914932251, 2.720181703567505, "Meteorological Satellite Orbit Polar"]
+[1.616015911102295, -2.322922945022583, "Military Satellite Orbit Polar"]
+[3.0926456451416016, -1.5813931226730347, "Satellite Management Air Force"]
+[1.7051128149032593, -2.2084834575653076, "Satellite Initial Orbit Control Atmospheric Drag"]
+[-2.7506790161132812, 7.913524150848389, "Processor Architecture i86"]
+[-2.4847190380096436, 11.16262149810791, "Image Processor Architecture AMD 2910 bit-slice"]
+[-2.4558358192443848, 11.172091484069824, "Image Processor Functions Flare detection, exposure evaluation, time averaging, spatial averaging, sub-field extraction, and JPEG compression"]
+[-3.179184675216675, 1.7256600856781006, "Satellite Mission Publication Year 2002"]
+[0.09587093442678452, 7.182554244995117, "Experiment URL http://www.crista.uni-wuppertal.de/campaigns/handbook/hb-iii.html"]
+[-0.7695034742355347, 10.996524810791016, "Observations Conference Proceedings Year 2001"]
+[-5.408018112182617, 2.8003337383270264, "Telescope Purpose Find exoplanets"]
+[-7.291547775268555, 2.869716167449951, "Gamma-ray Burst Discovery Date Oct. 16"]
+[-7.278581142425537, 2.8761818408966064, "Gamma-ray Burst Study Publication The Astrophysical Journal"]
+[-0.7482950091362, 11.540793418884277, "Detector Energy Range 2-15 keV"]
+[-0.8043795228004456, 11.582479476928711, "Detector Effective Area 17 cm2"]
+[-0.8447878360748291, 11.583672523498535, "Detector Field of View 3% sky"]
+[-0.8235335350036621, 11.627578735351562, "Detector Sensitive Range 2 keV \u2013 15 keV"]
+[-0.8867001533508301, 11.554210662841797, "Detector Mass 125 g"]
+[-0.8381646871566772, 11.598519325256348, "Detector Power 0.45 W"]
+[-0.8327769041061401, 11.612154960632324, "Detector Volume ~15.3 x 71 x 66 cm3"]
+[5.390465259552002, -4.515540599822998, "Satellite Launch Date Sept. 30, 2001"]
+[2.6220669746398926, -2.389503002166748, "Satellite Launch Vehicle Athena-1"]
+[2.7723886966705322, -2.349438428878784, "Satellite Launch Site Kodiak Launch Complex on Kodiak Island, Alaska"]
+[2.0974936485290527, -2.733299493789673, "Satellite Number of Satellites in Payload 4"]
+[2.5496418476104736, -1.9693238735198975, "Satellite Type Technology demonstration microsatellite of DoD/AFRL"]
+[2.4604668617248535, -1.80581533908844, "Satellite Type Prototype Communications Satellite"]
+[2.4905009269714355, -1.7409058809280396, "Satellite Type Stanford AudioPhonic Photographic IR Experiment"]
+[-0.8160724639892578, 11.602813720703125, "Detector Installation Date 2011"]
+[-0.8137423992156982, 11.5942964553833, "Detector Number of Instruments 7"]
+[-0.8250473737716675, 11.568345069885254, "Detector Mass 6918 kg"]
+[-0.7937262058258057, 11.58424186706543, "Detector Working Life Extended"]
+[-0.7365869283676147, 11.52224063873291, "Detector Cooling Pumps 3 out of 4 stopped working"]
+[-2.4236133098602295, 12.315326690673828, "Visible Wavelength Imager CCD Detector Electrim EDC-1000E"]
+[-2.3969781398773193, 12.383340835571289, "Visible Wavelength Imager Array Size 652 x 492 pixels"]
+[-2.431304693222046, 12.269041061401367, "Visible Wavelength Imager Pixel Size 7.4 \u00b5m"]
+[-2.3969478607177734, 12.363019943237305, "Visible Wavelength Imager Field of View 20\u00ba x 30\u00ba"]
+[-2.4299662113189697, 12.356575012207031, "Visible Wavelength Imager Ground Imagery Size 200 km x 150 km"]
+[-2.4477295875549316, 12.328225135803223, "Visible Wavelength Imager Resolution < 1 km"]
+[-3.163564682006836, 4.181321620941162, "Spacecraft Project Leadership Team of graduate students"]
+[-3.0794522762298584, 4.232765197753906, "Spacecraft Operations Concept Wavefront timing for sGRB detection"]
+[-2.9779155254364014, 4.177815914154053, "Spacecraft Orbit Type Highly eccentric orbit"]
+[-3.0914087295532227, 4.2701497077941895, "Spacecraft Deployment Orbit Super-synchronous"]
+[-3.0470921993255615, 4.322690963745117, "Spacecraft Thruster Small maneuvering thruster"]
+[-3.097742795944214, 4.190278053283691, "Spacecraft Baseline Orbital Parameters Shown in Table 2"]
+[1.4523431062698364, 7.004990100860596, "Communication Equipment Frequency Band X-band, S-band, L-band"]
+[-1.1382008790969849, 5.44506311416626, "Facility Location Fairmont, W.VA"]
+[-3.4924004077911377, 6.952359676361084, "Data Analysis Purpose Identify anomalies in the instrument data"]
+[4.680430889129639, -2.6576180458068848, "Satellite Operation Duration 13 Years (1992 to 2005)"]
+[0.8251755237579346, -1.1024831533432007, "Satellite Global Average Sea Level Rise 7 cm"]
+[5.323192119598389, -4.415804386138916, "Satellite Launch Date 1992"]
+[2.8742456436157227, -2.0859222412109375, "Satellite Soil Moisture Measurement Unknown"]
+[-0.4032343626022339, 5.131951332092285, "Reservoirs Storage Rate Just below 25 percent"]
+[-0.6018275618553162, 4.931153774261475, "Region Precipitation Difference About 38 percent less"]
+[-0.7230806946754456, 5.107639312744141, "Country Drought Level At least a moderate level"]
+[-0.6527858972549438, 5.0662407875061035, "Country Drought Level Extreme or exceptional"]
+[0.8738389015197754, 12.068161964416504, "Sensor Quantity 2"]
+[0.583115816116333, 12.02096939086914, "Sensor Function Deflect the ambient ions and to ionize neutrals"]
+[0.614804744720459, 11.953672409057617, "Sensor Function Can be utilized for ions or neutrals"]
+[-5.02662992477417, 7.955172061920166, "Communication Terminal Data Rate 5.6 Gbit/s"]
+[-5.009589195251465, 7.944008827209473, "Communication Terminal Link Distances About 5000 km"]
+[-5.015812873840332, 7.972784996032715, "Communication Terminal Data Stream 5.625 Gbit/s"]
+[-5.101875305175781, 7.986278057098389, "Communication Terminal User Data Rate 600 Mbit/s"]
+[5.254300117492676, -4.519831657409668, "Satellite Launch Date July 25, 2013"]
+[5.268810749053955, -4.422045707702637, "Satellite Launch Date Expected in 2014"]
+[3.704416513442993, 22.9709529876709, "Instrument Observation Date 2 July 2019"]
+[2.159576654434204, 22.407495498657227, "Instrument Brightness Reduction >80% around totality"]
+[2.129021644592285, 22.47098731994629, "Instrument \u03a3O/N2 Column Density Ratio Enhancement ~80% within the eclipse's totality"]
+[2.049762725830078, 22.528064727783203, "Instrument \u03a3O/N2 Column Density Ratio Enhancement ~7% after the eclipse passed"]
+[2.716038703918457, 22.427793502807617, "Instrument Type Multiple direction/polarisation radiometers"]
+[5.327999591827393, -4.442016124725342, "Satellite Launch Date 16 January 2003"]
+[5.137923717498779, -4.195484638214111, "Satellite End of Life Date 1 February 2003"]
+[2.081556797027588, -1.6840983629226685, "Satellite Mode Addition Spotlight mode, Five wider coverage stripmap modes, Two higher resolution ScanSAR modes for maritime surveillance, Extra wide swath 5 m resolution mode (Extra Fine)"]
+[1.9556533098220825, -1.7029708623886108, "Satellite Mode ScanSAR Wide mode"]
+[-0.804819643497467, 7.3084940910339355, "Electronic Device Testing Objective Measure and evaluate the effects of the high radiation environment on electronic devices"]
+[-3.286027431488037, 8.096372604370117, "Analog Neural Network VLSI Chips Architecture Special feed-forward \u201clearning\u201d architecture"]
+[-0.13066542148590088, 12.198312759399414, "Infrared Sensors Objective Determine if exposure of the HIP sensor to the complex spectrum of incident radiation might result in increased sensitivity"]
+[-1.1175568103790283, 7.847411155700684, "Electronic Device Objective Develop a small, low-cost, low-power SEU and TD (Total Dose) RADMON using standard CMOS processes"]
+[-13.958115577697754, -2.293656826019287, "X-ray Telescope Distance to Vela supernova 800 light-years"]
+[-0.7224528193473816, 2.9646811485290527, "Supernova Remnant Discovery Just 20 years ago"]
+[-0.7303539514541626, 2.9828317165374756, "Supernova Remnant Location Top right"]
+[1.2481145858764648, 10.911280632019043, "Scanner Purpose Ocean color and temperature scanning"]
+[-0.12697221338748932, 11.109284400939941, "Monitoring Program Reporting Date August 11, 2020"]
+[-0.0819535180926323, 11.155345916748047, "Monitoring Program Partners U.S. Department of Agriculture, the National Oceanic and Atmospheric Administration, and the University of Nebraska\u2013Lincoln"]
+[-0.07503277063369751, 11.195993423461914, "Monitoring Program Number of Observers More than 350 federal, state, and local observers"]
+[0.12000853568315506, 7.240592002868652, "ADR Experiment Deployment Date October"]
+[0.20044292509555817, 7.300266265869141, "ADR Experiment Technology 2D and 3D LiDaR (light detection and ranging)"]
+[0.0986209511756897, 7.25248384475708, "ADR Experiment Firing Speed 20 m/s"]
+[0.15428899228572845, 7.228209018707275, "ADR Experiment Purpose Cause the orbit of the spacecraft to rapidly decay"]
+[-0.9667260050773621, 9.828091621398926, "Rocket Height 42 m"]
+[-0.9600339531898499, 9.82858943939209, "Rocket Landing Location Autonomous spaceport drone ship"]
+[-0.9614934325218201, 9.82160472869873, "Rocket Landing Date Jan. 11, 2015"]
+[-0.9706456661224365, 9.811578750610352, "Rocket Landing Attempt Mostly successful"]
+[-0.9715360403060913, 9.825984954833984, "Rocket Landing Experiment Pinpoint soft landing of a rocket onto a miniscule platform at sea"]
+[2.6505210399627686, 5.397195816040039, "Emergency Beacon Frequency 406 MHz"]
+[2.668243885040283, 5.387273788452148, "Emergency Beacon Types Personal Locator Beacons (PLBs), Emergency Position Indicating Radio Beacons (EPIRBs), Emergency Locator Transmitters (ELTs)"]
+[5.298308372497559, -4.394386291503906, "Satellite Launch Date 26 Sept. 2016"]
+[14.258804321289062, 7.7957377433776855, "Nanosatellite Space Launch Date July 2016"]
+[-3.142040729522705, 1.7003250122070312, "Satellite Mission Duration Five hours"]
+[6.331509590148926, 7.407215118408203, "Satellite Component Information Source Herbert J. Kramer"]
+[6.367062091827393, 7.377460956573486, "Satellite Component Documentation Source Observation of the Earth and Its Environment: Survey of Missions and Sensors"]
+[6.364706993103027, 7.372385501861572, "Satellite Component Update Contact eoportal@symbios.space"]
+[-1.1071703433990479, 10.99081802368164, "Cloud Discrimination Device Observation Wavelengths 0.67 \u00b5m, 0.87 \u00b5m, 1.60 \u00b5m"]
+[-1.0210950374603271, 7.780970096588135, "Device Observation Direction Angles Forward- (+20\u00ba) and backward-looking (-20\u00ba)"]
+[-0.9888556003570557, 7.79027795791626, "Device Observation Direction Angles Nadir, \u00b126.1\u00ba, \u00b145.6\u00ba, \u00b160.0\u00b0 and \u00b170.5\u00ba forward and backward of the local vertical"]
+[2.7428956031799316, -1.3088425397872925, "Satellite Science Objectives Determine the cross- or macroscale spatial and temporal properties of magnetic reconnection"]
+[2.103858232498169, -1.8723918199539185, "Satellite Science Questions (1) Under what conditions is magnetopause reconnection spatially continuous versus discontinuous? (2) under what conditions is magnetopause reconnection temporally steady versus bursty?"]
+[-5.2183146476745605, 7.833069324493408, "Telecommunication Platform Financing Mainly financed by the Federal Office for Scientific, Technical and Cultural Affairs (OSTC) of Belgium, with a contribution from its German counterpart (DLR)"]
+[-5.229440212249756, 7.879530429840088, "Telecommunication Platform Development Contractor SAIT-Systems S. A. of Brussels"]
+[-5.266739368438721, 7.801558494567871, "Telecommunication Platform Operation Contract SAIT Systems has also a contract from ESA to operate LLMS/IRIS for a period of three years"]
+[-1.9083243608474731, 7.3076252937316895, "Computer Type Single powerful"]
+[-3.3614420890808105, 8.568449020385742, "Mass Memory Type Enhanced by a mass memory"]
+[-2.309997320175171, 8.13363265991211, "I/O Interface Type Implementing all I/O interfaces with the platform subsystems"]
+[0.9198153018951416, 9.196037292480469, "Attitude and Orbit Control System Fine Pointing Performance Fully achieved in the Science Observation Mode"]
+[0.9867867827415466, 9.162931442260742, "Attitude and Orbit Control System Sun Protection Always guaranteed"]
+[-1.9248974323272705, 6.8744001388549805, "Software Type Onboard software"]
+[-7.592397212982178, 5.865416526794434, "Camera Field-of-View 30\u00b0"]
+[-7.588736057281494, 5.862550735473633, "Camera Detector Size 1280 x 1024 pixels"]
+[-0.1872994601726532, 15.551657676696777, "Spectrometer Spectral Range 900 - 1700 nm"]
+[-0.13007588684558868, 15.561726570129395, "Spectrometer Spectral Resolution 6 nm"]
+[-0.11777723580598831, 15.597354888916016, "Spectrometer Spectral Range Extension Up to 2500 nm"]
+[-0.09692153334617615, 15.552081108093262, "Spectrometer Viewing Angle 0.1\u00b0"]
+[-0.07868921756744385, 15.51300048828125, "Spectrometer Integration Time 100 microseconds to 8 seconds"]
+[0.5880282521247864, -1.4861663579940796, "Satellite Orbit Altitude 635 km"]
+[0.6619453430175781, -2.2780327796936035, "Satellite Orbit Inclination 97.4\u00b0"]
+[-1.6809848546981812, 6.975024700164795, "Simulation Software Parameter Various"]
+[0.6624383926391602, 4.19026517868042, "Atmospheric Interaction Signal Type Distinct"]
+[-4.568035125732422, -3.081808090209961, "Exoplanet Star Type M dwarf"]
+[-4.568142890930176, -3.091555118560791, "Exoplanet Surface Type Ocean-covered, all-land"]
+[-0.6161657571792603, 6.262082576751709, "Event Date 16 October 2017"]
+[-0.8830145597457886, 6.430866241455078, "Article Published Date 28 March 2017"]
+[-0.9357316493988037, 6.483160018920898, "Article Published Date 5 March 2013"]
+[-0.8513288497924805, 11.62086296081543, "Detector Material Teledyne HgCdTe"]
+[-0.820797324180603, 11.610623359680176, "Detector Read-out Integrated Circuit GeoSnap"]
+[-0.833533763885498, 11.62692928314209, "Detector Pixel Resolution 2048 x 2048 pixels"]
+[-0.8145310282707214, 11.616837501525879, "Detector Temperature Requirement At or below 190 K"]
+[-0.8362767696380615, 0.16533729434013367, "Satellite System Partnership Duration More than 50 years"]
+[3.581733465194702, 13.862662315368652, "Laser Ranging Interferometer Distance Measurement Accuracy Up to 0.000001 mm"]
+[3.5786259174346924, 13.854630470275879, "Laser Ranging Interferometer Design Provider Max-Planck-Institute for Gravitational Physics (Albert-Einstein-Institute)"]
+[3.5913925170898438, 13.859718322753906, "Laser Ranging Interferometer Flight Hardware Provider STI (SpaceTech GmbH)"]
+[1.1637133359909058, -1.355729103088379, "Satellite Pair Formation Distance 144 m"]
+[1.2800960540771484, -1.3452244997024536, "Satellite Pair Minimum Formation Distance 25 m"]
+[1.2190905809402466, -1.3293495178222656, "Satellite Pair Maximum Formation Distance 250 m"]
+[0.26206091046333313, 11.570145606994629, "Sensor System Function Acquire formation and re-acquire it once per orbit"]
+[0.47561076283454895, 4.526332855224609, "Natural Phenomenon Annual Summer Minimum Date September 18, 2019"]
+[0.4931827485561371, 4.496713161468506, "Natural Phenomenon Summer Ice Extent Marked decreases in all seasons"]
+[0.47038793563842773, 4.5277533531188965, "Natural Phenomenon Impact Affects local ecosystems, regional and global weather patterns, and the circulation of the oceans"]
+[2.279423952102661, 22.87105941772461, "Instrument Window Channels 23.8, 31.4, 50.3, 89.0 GHz"]
+[2.222362518310547, 22.921337127685547, "Instrument Window Channels 19.4, 22.2, 37.0, 85.5 GHz"]
+[2.656846284866333, 22.47286605834961, "Instrument Polarization Mixed V & H (V only for 22.2)"]
+[2.292114734649658, 22.238300323486328, "Instrument Scan Geometry Cross-track \u00b148.33 \u00ba"]
+[2.2473831176757812, 22.287328720092773, "Instrument Scan Geometry Conical 45 \u00ba"]
+[2.041947364807129, 22.237686157226562, "Instrument Field of View (FOV) Varies with angle about 48 km at nadir about 150 km at limb"]
+[2.232028007507324, 22.465192794799805, "Instrument Field of View (FOV) Varies with frequency about 15 km at 85.5 GHz about 60 km at 19.4 GHz"]
+[1.6973692178726196, 21.96250343322754, "Instrument Swath Width About 2000 km"]
+[1.6840811967849731, 21.966548919677734, "Instrument Swath Width About 1400 km"]
+[-4.822577953338623, 9.269497871398926, "X-band Transmitter Bitrate Up to 100 Mbit"]
+[-4.813666343688965, 9.263083457946777, "X-band Transmitter Set Bitrate 3 Mbit"]
+[-6.737865447998047, 10.013720512390137, "Antenna Location +Y face of the satellite"]
+[-4.306795597076416, 7.380038738250732, "Data Receiver Function Provides the CCSDS data stream to the transmitter"]
+[-5.123867511749268, 7.985711574554443, "Communication System Operating Modes Searching, Tracking, Gyro-holding"]
+[-6.739475250244141, 10.059259414672852, "Antenna Operating Mode Description Open loop tracking mode for initial acquisition and re-acquisition"]
+[-6.659316539764404, 9.94994068145752, "Antenna Operating Mode Description Beacon is used to estimate the pointing error, which is then used to continuously steer the antenna back to the satellite"]
+[-6.70713996887207, 9.983229637145996, "Antenna Operating Mode Error Handling If the estimated pointing error is too large, the control system sends a command to mute the Tx"]
+[-6.731905937194824, 10.003410339355469, "Antenna Operating Mode Error Handling If the beacon strength suddenly drops, the control system sends a command to mute the Tx and switches to the gyro-holding mode"]
+[2.626176118850708, 14.309633255004883, "Optical Instrument Design f=1:4"]
+[2.6330206394195557, 14.309303283691406, "Optical Instrument Entrance Pupil Diameter 10.5 cm"]
+[2.6770083904266357, 14.345810890197754, "Optical Instrument Coating Antireflection"]
+[2.644117832183838, 14.31657600402832, "Optical Instrument Long-pass Filter Coating Cutoff at 600 nm"]
+[2.6720244884490967, 14.379168510437012, "Optical Instrument Red Limit 1000 nm"]
+[0.46029502153396606, 12.086454391479492, "Gas Flow Sensor Objective To demonstrate in space a gas flow control and sensing principle"]
+[0.5471146702766418, 12.09583854675293, "Gas Flow Sensor Measurement Principle Thermal technique to measure the flow rate of gas"]
+[-1.2353460788726807, 12.66094970703125, "Linear Concentrator Objective To measure the IV curves and to determine the pointing sensitivity of a new linear concentrator solar cell assembly"]
+[-2.203467607498169, 5.9315185546875, "Formation Flying System Purpose Maintain the satellites in the desired relative configuration"]
+[-1.7786757946014404, 8.835132598876953, "Control System Modes High accuracy inertial pointing, target pointing and safe sun pointing"]
+[2.653318166732788, 14.198554992675781, "Optical Bench Assembly Purpose Mount the metrology equipment of both the CSC (Coronagraph Spacecraft) and of the OSC (Occulter Spacecraft)"]
+[-7.545930862426758, 5.901270866394043, "RGB Camera Pointing Direction TANSO-FTS-2 viewing"]
+[1.8964697122573853, 22.223167419433594, "Instrument Spatial Resolution Higher than TANSO-CAI-2"]
+[2.711705207824707, 22.39610481262207, "Instrument Intelligent Pointing System Present"]
+[2.4000236988067627, 22.727306365966797, "Instrument Bands Near infrared (NIR, 0.87 \u00b5m) and shortwave infrared (SWIR, 1.60 \u00b5m)"]
+[2.5525076389312744, -1.461169719696045, "Satellite Cloud Discrimination Algorithm CLAUDIA (Cloud and Aerosol Unbiased Decision Intellectual Algorithm)"]
+[1.7588471174240112, 6.8740410804748535, "Communication Device Data Reception Capacity 1.8 Gbit/s"]
+[1.7548664808273315, 6.887439727783203, "Communication Device Data Handling Capacity Up to 300 Mbit/s"]
+[2.446126699447632, -1.7491775751113892, "Satellite AOCS Operational Modes MAS, MGT, MCO, MNO"]
+[1.4129596948623657, -1.7903954982757568, "Satellite MNO Pointing Performance 500 \u00b5rad"]
+[2.0270943641662598, -2.198641538619995, "Satellite Reaction Wheel Configuration Pyramid configuration"]
+[1.932059645652771, -2.1494009494781494, "Satellite Reaction Wheel Configuration Pyramid configuration"]
+[-1.7296826839447021, 8.829076766967773, "Control System Battery Configuration Two batteries connected in series"]
+[-1.711760401725769, 8.886366844177246, "Control System Battery Life More than 6 hours"]
+[-1.722464680671692, 8.842244148254395, "Control System Display Type OLED (Organic Light Emitting Diode)"]
+[-1.7735648155212402, 8.791293144226074, "Control System Data Interface USB"]
+[2.454998731613159, -1.762080430984497, "Satellite Design 3U CubeSat"]
+[2.014665126800537, -0.6389750242233276, "Satellite Solar Array Power Approximately 3 W"]
+[2.030421733856201, -0.610923707485199, "Satellite Solar Array Power About 60 percent more power than MicroMAS-1"]
+[2.6878130435943604, -2.350534200668335, "Satellite Radiometer Bands Near 90, 118, 183, and 206 GHz"]
+[1.6705199480056763, -1.1349397897720337, "Satellite Measurements Precipitation, temperature, and humidity"]
+[2.6900198459625244, -1.9711239337921143, "Satellite Signal-In-Space Test Activity Unknown"]
+[2.7238574028015137, -2.023829460144043, "Satellite Performance Assessment Unknown"]
+[-4.9390645027160645, 9.779302597045898, "Receiver Unknown Unknown"]
+[3.687882423400879, 22.946945190429688, "Instrument Installation Date 30 December 2017"]
+[-3.202658176422119, 4.630850791931152, "Cargo Spacecraft Installation Date 17 Dec. 2017"]
+[-3.0735208988189697, 4.6537861824035645, "Cargo Spacecraft Payload Mass 2205 kg"]
+[3.7202138900756836, 17.68630599975586, "Payload Compartment Combined Mass 645 kg"]
+[-6.646056652069092, 9.95594596862793, "Antenna Monitor, Control, and Test Subsystem Function Monitoring, control, and test functionality for the antenna control unit, receive elements, transmit elements, control ports of the switching system, RF switching, BITE (Built-In Test Equipment), environmental and fire suppression system monitoring, waveguide dehydrator, and other related equipment"]
+[-3.7928175926208496, 6.9059906005859375, "Data Collection System Function Data collection"]
+[-4.321436882019043, 7.3788886070251465, "High Rate information Transmission / Emergency Managers Weather Information Network Function High rate information transmission / Emergency managers weather information network"]
+[-5.836297988891602, 8.674485206604004, "GOES-R Rebroadcast Function Provide full resolution, calibrated, navigated, near-real-time direct broadcast data"]
+[-3.0200257301330566, 4.262151718139648, "Spacecraft Quantity 4 mid-inclination satellites"]
+[-2.9851415157318115, 4.341120719909668, "Spacecraft Quantity 2 sun-synchronous Legions"]
+[2.24714732170105, 22.284835815429688, "Instrument Measurement Changes in the solar extreme ultraviolet irradiance"]
+[2.7839207649230957, 22.29937744140625, "Instrument Impact Excess EUV radiation can result in radio blackouts of terrestrial high frequency communications at low latitudes"]
+[2.6834397315979004, 22.271486282348633, "Instrument Impact EUV flares also deposit large amounts of energy in Earth\u2019s upper atmosphere (thermosphere) causing it to expand into Low Earth Orbiting satellites"]
+[1.4272234439849854, 2.306990623474121, "Geostationary Lightning Mapper Mission Objective Measure from GEO the total lightning activity on a continuous basis over the Americas and portions of the adjoining oceans"]
+[1.4247474670410156, 2.343991279602051, "Geostationary Lightning Mapper Measurement Continuous measurements of lightning and ice-phase precipitation"]
+[5.225710868835449, -3.8175699710845947, "Satellite Launch Year 2018"]
+[5.184596538543701, -4.00142240524292, "Satellite Launch Year 2010"]
+[4.904073238372803, -4.211184501647949, "Satellite Measurement Period October 2018 to April 2019"]
+[1.9790313243865967, -1.250170111656189, "Satellite Measurement Comparison February/March 2019 ICESat-2 measurements with those calculated using ICESat in February/March 2008"]
+[2.645875930786133, 5.3900909423828125, "Distress Signal Beacon Signal Frequency 406 MHz"]
+[-9.95327377319336, 5.851807594299316, "Search and Rescue System Number of LEOSAR satellites 5"]
+[-9.955205917358398, 5.853757858276367, "Search and Rescue System Number of GEOSAR satellites 5"]
+[-9.981468200683594, 5.82538366317749, "Search and Rescue System Number of LEOLUTs 45"]
+[-9.972089767456055, 5.849102020263672, "Search and Rescue System Number of GEOLUTs 19"]
+[-9.954429626464844, 5.8533034324646, "Search and Rescue System Number of Mission Control Centers 29"]
+[2.689011335372925, 5.355672836303711, "Distress Signal Beacon Number in Use Over 600,000"]
+[2.652148485183716, 5.382943153381348, "Distress Signal Beacon Individuals Rescued More than 22,400"]
+[2.651249408721924, 5.384286403656006, "Distress Signal Beacon SAR Events Approximately 6,200"]
+[-1.6564699411392212, 9.590685844421387, "Ion Engine System Thrust 20 mN"]
+[-1.5696815252304077, 9.602065086364746, "Ion Thruster Lifetime 16,000 hours"]
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+[0.5400280952453613, 12.028746604919434, "Temperature Sensors Parameter Unknown"]
+[-0.6638180613517761, 9.452884674072266, "Spacecraft Component Diameter 5 m"]
+[-0.6461219787597656, 9.46861743927002, "Spacecraft Component Maximum Temperature 2200\u00ba C"]
+[-0.6330683827400208, 9.427149772644043, "Spacecraft Component Material Avcoat ablator"]
+[-0.532000720500946, 1.2241246700286865, "Satellite Orbit Altitude 500 km"]
+[-0.5282394289970398, 1.2314982414245605, "Satellite Orbit Inclination 40.5\u00ba"]
+[2.090836524963379, -2.808906316757202, "Satellite Number of Experiments 26"]
+[2.103189468383789, -2.707397937774658, "Satellite Number of Non-separating Components 2"]
+[2.180187940597534, -2.755554676055908, "Satellite Number of Missions 8"]
+[-0.9671504497528076, 9.846430778503418, "Rocket Original Manifest ELaNa-4 CubeSats"]
+[5.194594383239746, -4.374253749847412, "Satellite Data Collection Start Date December 11, 2018"]
+[2.536099433898926, -1.2418285608291626, "Satellite Data Collection Arctic and Antarctic sea ice"]
+[2.548421859741211, -1.161888837814331, "Satellite Data Collection Thin ice, thick ice, and features such as ice ridges"]
+[2.570920705795288, -1.234499216079712, "Satellite Data Collection Open water in the cracks between the ice floes, called leads"]
+[2.4690158367156982, -1.2206730842590332, "Satellite Data Collection Fresh ice is totally flat to within a couple centimeters"]
+[0.9916160106658936, 0.7823252081871033, "Earth Observation Satellite Orbit Altitude 504 \u00b1 2 km"]
+[1.014955759048462, 0.7644937038421631, "Earth Observation Satellite Orbit Inclination 97.42 \u00b10.1\u00ba"]
+[0.9750869870185852, 0.7447817325592041, "Earth Observation Satellite Orbit Eccentricity 0.00125\u00b10.0008"]
+[1.0022789239883423, 0.7870116829872131, "Earth Observation Satellite Local Time of Descending Node 11:00 hours \u00b1 15 min"]
+[-1.9847805500030518, 14.786697387695312, "Dicke Radiometer Frequency 23.8 GHz"]
+[-2.0359506607055664, 14.747265815734863, "Dicke Radiometer Bandwidth 500 MHz"]
+[-1.9856433868408203, 14.790563583374023, "Dicke Radiometer Polarization V"]
+[-2.0202367305755615, 14.775314331054688, "Dicke Radiometer Frequency 36.5 GHz"]
+[-2.042760133743286, 14.780540466308594, "Dicke Radiometer Bandwidth 1 GHz"]
+[-2.0131752490997314, 14.762097358703613, "Dicke Radiometer Polarization V and H"]
+[-2.02703595161438, 14.747232437133789, "Dicke Radiometer Resolution 40 km"]
+[-2.0271995067596436, 14.740937232971191, "Dicke Radiometer Swath Width 380 km"]
+[-2.007763624191284, 14.765490531921387, "Dicke Radiometer Resolution 50 km"]
+[-2.0475351810455322, 14.696324348449707, "Dicke Radiometer Sensitivity 0.5 K"]
+[-2.0302271842956543, 14.74760913848877, "Dicke Radiometer Incidence Angles 52\u00ba and 58\u00ba"]
+[-2.0506608486175537, 14.741403579711914, "Dicke Radiometer Brightness Temperature Stability 1 K"]
+[-2.0350236892700195, 14.717711448669434, "Dicke Radiometer Mass 99 kg"]
+[-2.105755090713501, 14.6652193069458, "Dicke Radiometer Power Consumption 96 W"]
+[2.641247034072876, -1.8976892232894897, "Satellite Type DIY"]
+[5.275904655456543, -4.408415794372559, "Satellite Launch Date 26 May 2016"]
+[5.277163505554199, -4.429804801940918, "Satellite Update Date 07 February 2018"]
+[1.1593056917190552, -0.7151711583137512, "Satellite Size 25 mm x 75 mm x 100 mm"]
+[0.9747278094291687, -4.371783256530762, "Satellite Mass 0.275 kg"]
+[2.3729841709136963, -1.6417454481124878, "Satellite Radio Battery operated, very low power"]
+[-1.2126905918121338, 8.603445053100586, "Component Length 32 m"]
+[-1.22773015499115, 8.609169006347656, "Component Number of MEMS RF switches 4"]
+[-1.2714165449142456, 8.606302261352539, "Component Charge Pump Voltage 100 V"]
+[-3.047755241394043, 7.677034854888916, "Central Processing Unit Model PIC16F877A"]
+[-2.483391523361206, 8.871493339538574, "Analog Digital Converters Number 5"]
+[-2.4551899433135986, 8.899188041687012, "Analog Digital Converters Resolution 8 bit"]
+[-2.441267490386963, 8.844321250915527, "Analog Digital Converters Measurement Range 0 - 4.096 V"]
+[-1.899395227432251, 8.76003360748291, "Circuit Number 2 (three redundant)"]
+[-2.6226882934570312, 9.325994491577148, "Power Supply Voltage 300 V"]
+[3.7318406105041504, 17.709760665893555, "Payload Total Mass 2,000 kg"]
+[3.7076668739318848, 17.682538986206055, "Payload Launch Date Jan. 16 -Feb. 1, 2003"]
+[3.736438512802124, 17.711599349975586, "Payload Orbit Altitude 275 km"]
+[3.721402883529663, 17.698753356933594, "Payload Orbit Inclination 39\u00ba"]
+[1.704180359840393, 6.9475860595703125, "Communication Device Function Receive information from, or transmit information to the satellite"]
+[1.6935467720031738, 6.948832988739014, "Communication Device Tasks Tracking of the satellite, Telemetry operations, Command operations, Data processing operations"]
+[-4.526601314544678, 12.065112113952637, "Magnetic Separator Spatial Extent Large or small"]
+[0.5251455903053284, 4.599858283996582, "Physical Phenomenon Duration More than 10 RE"]
+[0.4985024631023407, 4.557275772094727, "Physical Phenomenon Stability Stable and single"]
+[0.5017750263214111, 4.548896789550781, "Physical Phenomenon Continuity Continuous along the dayside boundary"]
+[5.327583312988281, -4.419782638549805, "Satellite Launch Date 15 September 2018"]
+[4.980236530303955, -4.296992301940918, "Satellite First Height Measurements 3 October"]
+[-3.0537848472595215, 2.4783473014831543, "Mission Start Date 2009"]
+[-3.1258151531219482, 2.3905386924743652, "Mission Purpose Maintain continuity of laser-altimetry measurements between NASA\u2019s ICESat missions"]
+[2.0398099422454834, -2.0964181423187256, "Satellite Orbit Track Not provided"]
+[2.1218910217285156, -1.747167706489563, "Satellite Wind and Temperature Observations Mode-S"]
+[3.1796560287475586, -1.896530032157898, "Satellite Functionality Status Operational"]
+[1.6892902851104736, -2.1160755157470703, "Satellite Attitude Manoeuvring Up to 7 target changes per orbit"]
+[2.260667324066162, -1.8891489505767822, "Satellite PI Gary S. E. Lagerloef of ESR (Earth & Space Research), Seattle, WA; Raul F. Colomb of CONAE, Argentina; Sandra Torrusio"]
+[2.3135862350463867, -1.8778505325317383, "Satellite Ground Station Location Cordoba, Argentina"]
+[2.3629610538482666, -1.9151819944381714, "Satellite Instrument Data Distribution Facility Location Buenos Aires, Argentina"]
+[2.6375820636749268, -1.7290633916854858, "Satellite Payload Contributions Italy, France, and Canada"]
+[-3.067383289337158, 4.267148971557617, "Spacecraft Instrumentation CONAE and NASA"]
+[-4.260123252868652, 0.4767051041126251, "Radio Occultation Project Presentation Date Dec. 5-7, 2012"]
+[2.0451138019561768, -2.80560302734375, "Satellite Quantity At least six"]
+[-3.6044955253601074, 6.985918998718262, "Data Platform Image Catalog Expanded"]
+[-0.9460707306861877, -10.002488136291504, "Satellite Constellation Roadmap Extends industry leadership well into the next decade"]
+[-14.187203407287598, -2.45497989654541, "X-ray Telescope Principal Investigator Nanda Rea"]
+[-14.115518569946289, -2.424530267715454, "X-ray Telescope Array Principal Investigator Nanda Rea"]
+[-0.7415005564689636, 3.146042585372925, "Neutron Star Distance from Earth 16,000 light-years"]
+[-0.6892484426498413, 3.138026714324951, "Neutron Star Age About 240 years old"]
+[1.4321142435073853, 2.7716410160064697, "Weather Satellite Launch Date April 1, 1960"]
+[1.4414348602294922, 2.781318426132202, "Weather Satellite Stabilization Spin stabilized to inertial space"]
+[1.4545197486877441, 2.74487566947937, "Weather Satellite View Only an oblique swath of the Earth's surface occasionally in each orbit"]
+[4.834049224853516, -3.049604654312134, "Satellite Development Time Not soon"]
+[2.7761237621307373, 22.383947372436523, "Instrument Type Earth radiation budget radiometers"]
+[2.8403501510620117, 22.328899383544922, "Instrument Type Earth radiation budget radiometers"]
+[2.329885721206665, 22.220928192138672, "Instrument Measurement Category Downwelling (Incoming) solar radiation at TOA"]
+[2.318514108657837, 22.19983673095703, "Instrument Measurement Category Downwelling (Incoming) solar radiation at TOA"]
+[2.801067590713501, -1.0367355346679688, "Satellite Purpose Track methane emissions"]
+[2.6983659267425537, -2.260916233062744, "Satellite Band Ka-band"]
+[2.1327950954437256, -2.5755038261413574, "Satellite User Beams Nearly 200"]
+[2.544879198074341, -2.0076744556427, "Satellite Processor Type Digital transparent processor (DTP)"]
+[2.746731996536255, -2.018545627593994, "Satellite Processor Generation Fifth-generation"]
+[2.554597854614258, -1.983540654182434, "Satellite Processor On-board processor"]
+[0.8308842182159424, 11.975052833557129, "Sensor Type Unknown"]
+[0.8282672166824341, 11.940570831298828, "Sensor Type Unknown"]
+[0.8196646571159363, 11.97617244720459, "Sensor Type Unknown"]
+[0.8284411430358887, 11.970121383666992, "Sensor Type Unknown"]
+[-4.345571517944336, 0.21574588119983673, "GPS Receiver Manufacturer NovAtel"]
+[-0.4556998908519745, 8.672727584838867, "Actuator Type Unknown"]
+[-0.45184797048568726, 8.670554161071777, "Actuator Type Unknown"]
+[-4.943192481994629, 9.77849006652832, "Receiver Manufacturer GomSpace"]
+[-5.464122295379639, 9.105463027954102, "Radio Module Type Software Defined Radio"]
+[-4.815373420715332, 9.289119720458984, "X-band Transmitter Model EWC27"]
+[5.076204299926758, -4.486127853393555, "Satellite Arrival Date 18 June 2019"]
+[2.1863362789154053, -2.454638719558716, "Satellite Successful Laser Links 20,000"]
+[5.09027099609375, -4.375437259674072, "Satellite Status Update Date 23 January 2019"]
+[1.829380989074707, 10.695700645446777, "Imaging Technology Compensation Methods Ground-based input of horizontal frequency data and altimetry data supplementary on board"]
+[1.7501845359802246, 10.674439430236816, "Imaging Technology Resolution 7 m"]
+[1.8057280778884888, 10.644279479980469, "Imaging Technology Resolution 1.3 m"]
+[-1.1660661697387695, 4.4447407722473145, "Ground Station Daily Capacity 5.4 TB/day"]
+[-1.1274760961532593, 4.469634532928467, "Ground Station Advanced Mode Daily Capacity 16.2 TB/day"]
+[-1.1486867666244507, 4.461681842803955, "Ground Station Daily Capacity 10.8 TB/day"]
+[-1.1334079504013062, 4.472748756408691, "Ground Station Advanced Mode Daily Capacity 32.4 TB/day"]
+[3.172760486602783, -1.9016743898391724, "Satellite Mission Status Operational (nominal)"]
+[5.357293605804443, -4.424651145935059, "Satellite Launch Date 17 May 2012"]
+[5.007267951965332, -4.065815448760986, "Satellite End of Life Date Operational as of December 2022"]
+[2.1084444522857666, -1.1609501838684082, "Satellite Measurement Category Multi-purpose imagery (ocean), Multi-purpose imagery (land)"]
+[2.2841193675994873, -1.5435394048690796, "Satellite Instrument Type Other, Communications, Data collection, Lightning sensors"]
+[-0.35657799243927, 3.8149142265319824, "Planet Age 40 million years"]
+[-0.6005135774612427, 3.226407766342163, "Star Star Spot Coverage Up to 40%"]
+[2.811758518218994, -1.085027813911438, "Satellite Purpose Find young stars like DS Tuc A"]
+[-1.1254273653030396, 4.488132476806641, "Ground Station Locations Matera (Italy), Maspalomas (Spain), Svalbard (Norway), Alaska (USA)"]
+[-3.269333600997925, 7.264148235321045, "Processing/Archiving Center Locations Farnborough (UK), Madrid (Spain)"]
+[3.7355692386627197, 17.69453239440918, "Payload Data Management Center Location ESA/ESRIN, Frascati, Italy"]
+[-3.3275601863861084, 7.443566799163818, "Data Processing Steps Radiometric corrections, Geometric corrections"]
+[-3.3423960208892822, 7.466658115386963, "Data Processing Steps Cloud screening, Atmospheric corrections, Geophysical variables retrieval algorithms"]
+[-3.381334066390991, 7.480930328369141, "Data Processing Function Spatio-temporal synthesis"]
+[-0.4036254584789276, 16.206253051757812, "Spectrograph Wavelength Range 80 - 170 nm"]
+[-0.4094253480434418, 16.219009399414062, "Spectrograph Resolution 1.5 nm"]
+[-0.40738415718078613, 16.240489959716797, "Spectrograph Viewing Altitude Approximately 50 km to 750 km"]
+[-0.4125262498855591, 16.22673797607422, "Spectrograph Instrument Type Low Resolution Airglow/Aurora Spectrograph"]
+[5.337334156036377, -4.498610019683838, "Satellite Launch Date Feb. 23, 1999"]
+[-3.5609548091888428, 4.396794319152832, "Spacecraft Launch Date Oct. 18, 2003"]
+[-7.355900764465332, 2.904355525970459, "Cosmic Ray Detector Magnetic Field Strength 4,000 times stronger than the Earth\u2019s own magnetic field"]
+[-7.394203186035156, 2.8719451427459717, "Cosmic Ray Detector Detector Type Particle physics detector containing a large, cryogenic superfluid helium superconducting magnet"]
+[-4.480888366699219, 12.104453086853027, "Superconducting Magnet Magnet Type Cryogenic superfluid helium superconducting magnet"]
+[-7.389226913452148, 2.8748998641967773, "Cosmic Ray Detector Sponsorship DOE"]
+[-7.398156642913818, 2.868328809738159, "Cosmic Ray Detector MOU Date September 20, 1995"]
+[2.8969974517822266, -1.86185622215271, "Satellite Operations Intensive, highly automated, intermittent TT&C pass operations"]
+[2.966013193130493, -1.702965497970581, "Satellite Approach for Operations Multi-mission"]
+[2.953470230102539, -1.698306679725647, "Satellite Mission Operations Day-to-day end-to-end system operations and maintenance of the satellite and ground segment"]
+[2.597491979598999, 21.924890518188477, "Instrument Function Monitor energetic particle populations and the spacecraft's radiation exposure"]
+[2.149488925933838, 22.211118698120117, "Instrument Measurement Intensity of energetic particles"]
+[2.8355064392089844, 22.119585037231445, "Instrument Diagnostic Identify when X-ray measurements may be contaminated from charged particles"]
+[2.9223148822784424, 22.401819229125977, "Instrument Design Custom designed for the mission"]
+[-3.084336757659912, 4.229724407196045, "Spacecraft Structure Type X50M"]
+[6.08600378036499, 7.653853893280029, "Satellite Component Quantity 2"]
+[6.1686906814575195, 7.5659003257751465, "Satellite Component Quantity 1"]
+[6.17206335067749, 7.561566352844238, "Satellite Component Quantity 1"]
+[6.19135046005249, 7.548051834106445, "Satellite Component Quantity 2"]
+[2.0468661785125732, -2.7970316410064697, "Satellite Quantity 2"]
+[6.093343257904053, 7.641108989715576, "Satellite Component Quantity 1"]
+[-5.225722312927246, 7.895599365234375, "Communication System Quantity 1"]
+[-0.10548968613147736, 9.213546752929688, "Navigation System Components LiDAR and 2D camera"]
+[-5.2603254318237305, 7.930822849273682, "Communication System Quantity 2"]
+[-5.220447540283203, 7.804426193237305, "Communication System Data Rate 38.4 kbit/s (low rate), 2-4 Mbit/s (high rate)"]
+[-3.270578384399414, 5.425097942352295, "Launch Vehicle Orbit Altitude ~650 km x 610 km"]
+[-3.270761251449585, 5.427058696746826, "Launch Vehicle Orbit Inclination 6\u00ba"]
+[-4.902584552764893, 2.7831544876098633, "Space Telescope Launch Date June 13, 2012"]
+[-5.002622604370117, 2.862539052963257, "Space Telescope Mission Duration 10 years"]
+[-5.023077011108398, 2.881457805633545, "Space Telescope Purpose Detects high-energy X-ray light and studies some of the most energetic objects and processes in the universe"]
+[2.549713373184204, 22.35053253173828, "Instrument Loop Heat Pipe Blockage Caused the instrument to overheat"]
+[5.347195625305176, -4.223250389099121, "Satellite Renaming Date After launch"]
+[4.67468786239624, -2.611799478530884, "Satellite Operational Role Transition Time Two weeks"]
+[1.395226001739502, -3.107585906982422, "Satellites Observation Area United States, Mexico, Central America, South America, the Caribbean and much of the Pacific and Atlantic Oceans"]
+[-1.3353393077850342, 6.2265238761901855, "Team Research Focus Develop new ways to help forecast the intensity of incoming hurricanes"]
+[-5.253077983856201, 7.888319969177246, "Communication System Concept of Operation Communication link sessions are planned and coordinated between the EDRS MOC and the user\u2019s MOC, making use of the visibility windows available between EDRS and the user satellites"]
+[-5.293266296386719, 7.886402130126953, "Communication System Data Transmission User data will be transmitted from LEO user satellites to either of the EDRS payloads (i.e., EDRS-A, EDRS-C) and relayed to the DGS and/or FLGS/B-FLGS on the ground"]
+[-5.196086883544922, 7.855656147003174, "Communication System Data Availability It will be made available through terrestrial network to the users\u2019 sites"]
+[-5.167849063873291, 7.963261604309082, "Communication System User Ground Stations The users can also operate their own user ground stations to receive directly the user data"]
+[-2.2066617012023926, 5.956910610198975, "Aircraft Flight Lines Proposed during the 2017 Antarctic Field Campaign of Operation IceBridge"]
+[2.203763246536255, -1.6017663478851318, "Satellite Laser Altimetry Mission Proceedings of the IEEE. Vol 98, No. 5, May 2010. Pages 735-751"]
+[14.469381332397461, 7.6596455574035645, "Nanosatellite Command and Data Handling System Function Communication with the ground, controls the solar panels, distributes power to the various components, and provides attitude control"]
+[14.481586456298828, 7.688455581665039, "Nanosatellite Command and Data Handling System Storage Non-volatile flash file-system consisting of two SD cards"]
+[14.244095802307129, 7.809061050415039, "Nanosatellite Launch Date Sept. 13, 2012"]
+[14.454062461853027, 7.682748794555664, "Nanosatellite Launch Vehicle Atlas-5-411"]
+[3.715764045715332, 17.673871994018555, "Primary Payload Organization National Reconnaissance Organization"]
+[-3.0902085304260254, 4.258304119110107, "Classified Spacecraft Organization NRO/MSD (Mission Support Directorate)"]
+[2.6223204135894775, 13.443370819091797, "Optical and Mechanical Components M1A (Primary Mirror Assembly), M2 A (Secondary Mirror Assembly), CLA (Correction Lens Assembly), the metering structure"]
+[-0.8539328575134277, 11.616738319396973, "Detector Type Linear"]
+[-3.3920094966888428, 8.174251556396484, "Signal Processor Output Digital Signals"]
+[-2.1550464630126953, 8.906807899475098, "Control Module Redundancy All the modules have redundancy except the optical part and the FPA"]
+[-0.8448129892349243, 8.902676582336426, "Temperature Control Module Function Provides temperature control management of the DMAC instrument"]
+[1.4372527599334717, -1.9101378917694092, "Satellite Polarimetric Accuracy Fluctuate seasonally"]
+[2.05197811126709, -1.4062550067901611, "Satellite Imaging Mode TOPS (Terrain Observation by Progressive Scans)"]
+[4.961113929748535, -4.52488374710083, "Satellite Interferogram Date March 17, 2014"]
+[2.0814054012298584, -0.6702532172203064, "Satellite Power Generation 300 V"]
+[2.0594379901885986, -0.6689745187759399, "Satellite Photovoltaic Power Generation 300 V"]
+[-3.193558931350708, 2.072239637374878, "Future Missions Power Requirement High-voltage photovoltaic generation"]
+[0.9884868264198303, -4.414259910583496, "Satellite Mass 39 kg"]
+[1.1081234216690063, -0.9070199728012085, "Satellite Diameter 47.5 cm"]
+[0.9675642251968384, -4.413746356964111, "Satellite Mass 91 kg"]
+[1.1463513374328613, -0.8357611298561096, "Satellite Diameter 94.5 cm"]
+[11.30331039428711, 5.553061008453369, "CubeSat Three-axis control accuracy 3\u00ba"]
+[11.487884521484375, 5.6881842613220215, "CubeSat Size 10 x 10 x 30 cm"]
+[11.25076961517334, 5.471391677856445, "CubeSat Orientation Control Spinning miniaturized \u2018reaction wheels' at varying speeds"]
+[11.436630249023438, 5.669705390930176, "CubeSat Mission Duration Six months"]
+[-7.195658206939697, 10.075516700744629, "Cassegrain antenna Diameter 0.65m"]
+[-7.155801296234131, 10.068907737731934, "Cassegrain antenna Tx frequency 28.05 GHz\u00b1550 MHz"]
+[-7.207038879394531, 10.07905101776123, "Cassegrain antenna Rx frequency 18.25 GHz\u00b1550 MHz"]
+[-7.256556510925293, 10.072623252868652, "Cassegrain antenna SSPA output power 20 W (linear) 40 W (saturated)"]
+[-7.210256099700928, 10.077046394348145, "Cassegrain antenna EIRP >55.0 dBW"]
+[-7.230607986450195, 10.078751564025879, "Cassegrain antenna G/T >13.5dB/K"]
+[-7.222850799560547, 10.079666137695312, "Cassegrain antenna Azimuth tracking 360\u00ba Continuous"]
+[-7.220535755157471, 10.080265045166016, "Cassegrain antenna Elevation 20\u00ba~90\u00ba"]
+[-7.273043632507324, 10.081605911254883, "Cassegrain antenna Cross elevation \u00b115\u00ba"]
+[-7.220844268798828, 10.077424049377441, "Cassegrain antenna Tracking accuracy <\u00b10.2\u00ba"]
+[-7.22805118560791, 10.076828956604004, "Cassegrain antenna Tracking acquisition <12 minute cold start <5 minute warm start <1 s for 60 s lost"]
+[-7.228989601135254, 10.080055236816406, "Cassegrain antenna Operating temperature -20\u00baC ~+40\u00baC"]
+[-7.177680015563965, 10.06726360321045, "Cassegrain antenna Power supply AC 90 V~120 V 50/60 Hz"]
+[-7.210366725921631, 10.07777214050293, "Cassegrain antenna Power consumption <1.5 KVA"]
+[-7.223635673522949, 10.078682899475098, "Cassegrain antenna Mass < 120 kg"]
+[-0.14670155942440033, 15.572468757629395, "Spectrometer Spectral Resolution Very high"]
+[-0.12217047810554504, 15.553154945373535, "Spectrometer Wavelength Range Wide"]
+[-4.561957359313965, -3.0876526832580566, "Exoplanet Mass Half the mass of Earth"]
+[-4.575083255767822, -3.100031614303589, "Exoplanet Orbital Period Approximately eight hours"]
+[-4.563686847686768, -3.0904147624969482, "Exoplanet Diameter Just over 9000 km"]
+[-4.563393592834473, -3.089123487472534, "Exoplanet Distance from Earth Just under 31 light years"]
+[-4.576894760131836, -3.103175163269043, "Exoplanet Orbital Period Only one-third of an Earth day"]
+[-4.502721786499023, 12.067023277282715, "Magnetic Field Strength 5 times weaker than the SCM"]
+[-0.6518647074699402, 11.716802597045898, "Silicon Tracker Detector Optimization Extend the lever arm of the tracking measurement"]
+[-0.652279257774353, 11.71692180633545, "Silicon Tracker Detector Function Measure smaller curvatures"]
+[2.389908790588379, 13.6409273147583, "Optics Coating Application First 7 groups"]
+[2.552471160888672, 13.512514114379883, "Optics Assembly Component Material Titanium"]
+[2.5979645252227783, 13.668651580810547, "Optics Assembly Component Material Glass and graphite"]
+[2.171788215637207, -2.6583704948425293, "Satellite Sensor Quantity 6"]
+[-1.237390398979187, 15.070443153381348, "Multi-spectral Radiometer Measurement Frequency Twice each day"]
+[-2.784933090209961, 15.272428512573242, "Imaging Microwave Radiometer Measurement Frequency Unknown"]
+[-2.673715114593506, 15.229031562805176, "Imaging Microwave Radiometer Applications Global measurements of air temperature profiles, humidity profiles and other atmospheric measurements"]
+[-2.806770086288452, 15.232614517211914, "Microwave Radiometer System Scan Mechanism Step-scan motion in the cross-track direction of \u00b1 40.5\u00ba"]
+[-2.7987828254699707, 15.244362831115723, "Microwave Radiometer System Observation Rate 7.5 scans/minute"]
+[-2.7670328617095947, 15.234557151794434, "Microwave Radiometer System Spatial Resolution About 48 km"]
+[-2.758514404296875, 15.264714241027832, "Microwave Radiometer System Swath Width About 1500 km"]
+[11.521980285644531, 5.753154277801514, "CubeSat Size 2U"]
+[2.8985979557037354, 21.980140686035156, "Instrument Purpose Detect X-ray pulses produced by coronal mass ejections"]
+[3.6258676052093506, 22.93157386779785, "Instrument Launch Year 2021"]
+[2.9228954315185547, 21.981355667114258, "Instrument Purpose Monitor space weather"]
+[0.11811648309230804, 9.146903991699219, "Coarse Pointing Assembly Azimuth Rotation Axis Perpendicular to the FUS baseplate"]
+[0.195078045129776, 9.219657897949219, "Coarse Pointing Assembly Elevation Rotation Axis Perpendicular to the azimuth rotation axis"]
+[-1.0436222553253174, 7.7808308601379395, "Device Optical Power Amplifier 5 W"]
+[-1.0311857461929321, 7.721519947052002, "Device Receiver Data Rate 1.8Gbit/s"]
+[-1.110403060913086, 7.823093414306641, "Device Service Life 15 years"]
+[2.1465554237365723, -0.9420647025108337, "Satellite Sensor Scan Rate 31.9 scans/min"]
+[2.1142020225524902, -0.9045732021331787, "Satellite Sensor Sampling Scheme 128 samples per scan for the 85 GHz channels, and 64 scene stations per two scans for the other channels"]
+[2.0786991119384766, -0.8719002604484558, "Satellite Sensor Footprint Sampling Every 25 km for the 19, 22, and 37 GHz channels, and every 12.5 km for the 85 GHz channel"]
+[1.2617474794387817, -0.8747394680976868, "Satellite Size Same as Starshine-1"]
+[0.9993675351142883, -4.3596272468566895, "Satellite Mass Same as Starshine-1"]
+[0.8158222436904907, -2.2431373596191406, "Satellite Spin System Rate 5\u00ba/s"]
+[0.5702730417251587, -1.4904645681381226, "Satellite Orbit Altitude 387 km"]
+[0.7420822381973267, -2.286970615386963, "Satellite Orbit Inclination 51.6\u00ba"]
+[1.682267665863037, 6.962610721588135, "Communication Device Frequency 401.65 MHz\u00b10.0405 MHz"]
+[1.7496453523635864, 6.8899688720703125, "Communication Device Bit Rate 400bit/s"]
+[1.6670502424240112, 6.967653751373291, "Communication Device Frequency 465.9875 MHz"]
+[1.76805579662323, 6.8748602867126465, "Communication Device Power over 5 W"]
+[1.7230383157730103, 6.856761932373047, "Communication Device Bit Rate 200 bit/s"]
+[-6.683459758758545, 9.953225135803223, "Antenna G/T over -36.6 dBk"]
+[-6.724315643310547, 9.993091583251953, "Antenna EIRP over 27.1 dBm"]
+[1.7576417922973633, 6.952354431152344, "Communication Device Manufacturer Tekever in Portugal"]
+[-1.9575690031051636, 7.365535736083984, "Software and Hardware Purpose Permit to autonomously perform, with the required strict accuracy, the maneuvers necessary for accomplishing mission scientific and technology demonstration goals, guaranteeing at the same time the mission safety"]
+[5.265377998352051, -4.358894348144531, "Satellite Launch Date Late 2020"]
+[1.0788146257400513, -1.035881519317627, "Satellite Length 150-m"]
+[2.751166820526123, -1.080015778541565, "Satellite Purpose Study the Sun\u2019s faint corona closer to the solar rim"]
+[-5.331019878387451, 7.8827314376831055, "Communication System Downlink Frequency X-band"]
+[-5.298627853393555, 7.976212978363037, "Communication System TT&C Frequency S-band"]
+[-1.4424077272415161, 1.2126357555389404, "Data Relay and Test Satellite Communication Link Frequency Ka-band for mission data and S-band for TT&C data"]
+[-3.589012861251831, 4.396739482879639, "Spacecraft Launch Date Dec. 14, 2002"]
+[-3.145914077758789, 4.303098678588867, "Spacecraft Launch Site TNSC (Tanegashima Space Center), Japan"]
+[0.6102005243301392, -1.3631677627563477, "Satellite Structure Length 6.85 m"]
+[0.6550832986831665, -1.5917243957519531, "Satellite Structure Battery Capacity 25.5 A hr"]
+[6.3992791175842285, 7.337672233581543, "Satellite Component Size 3 m x 4.9 m"]
+[0.5756149291992188, 12.012977600097656, "Sensor Function Provide detailed global measurements of the electron distribution in the Earth's ionosphere"]
+[-3.190812349319458, 14.616827964782715, "Microwave Imager Function Define the extent of sea ice and seastate conditions (wave height and patterns) on the world's oceans"]
+[5.834036350250244, 14.37387466430664, "Transponder Type Deep-Space"]
+[5.833952903747559, 14.376096725463867, "Transponder Manufacturer NASA/JPL"]
+[5.83437967300415, 14.375237464904785, "Transponder URL https://www.nasa.gov/sites/default/files/atoms/files/brochure_irisv2_201507.pdf"]
+[1.7259074449539185, 6.9266533851623535, "Communication Device Maximum Power Output 27 dBm (0.5 W)"]
+[1.7357428073883057, 6.895453929901123, "Communication Device Data Rate (Downlink) 32 kbit/s to 1 Mbit/s"]
+[1.773690104484558, 6.868988037109375, "Communication Device Data Rate (Uplink) 4 kbit/s"]
+[1.6391746997833252, 6.988619804382324, "Communication Device Frequency Allocations Amateur Satellite UHF-band or Space Research S-band"]
+[2.690568685531616, -2.4120724201202393, "Satellite Communication Configuration UHF in uplink and the S-band in downlink"]
+[-0.8282949924468994, 11.636040687561035, "Detector Signal Few tenths of a \u00b5W/m2"]
+[-2.5772650241851807, 9.304864883422852, "High Voltage Modules Voltage Output Several hundred volt"]
+[-2.7113516330718994, 8.765810012817383, "Module Gain Factors Four possible"]
+[-0.8461762070655823, 11.613420486450195, "Detector Fragile Component Special care will have to be paid in the choice of the model, or in its accommodation"]
+[-1.773250937461853, 8.319159507751465, "Mechanical System Status Currently under consideration"]
+[7.5103583335876465, 12.65093994140625, "Satellite Instrument Operational Date August 25, 2011"]
+[7.302443504333496, 12.450346946716309, "Satellite Instrument Salt Concentration Units Parts per thousand (grams of salt per kilogram of sea water)"]
+[7.364765167236328, 12.49609088897705, "Satellite Instrument Average Salinity About 35"]
+[1.154048204421997, -0.8557407259941101, "Satellite Width 2.3 m"]
+[-2.5468249320983887, 9.669880867004395, "Power Source Span 7.9 m"]
+[-2.847989797592163, 3.9295246601104736, "Capsule Diameter 1.5 m"]
+[-1.2159491777420044, 8.690460205078125, "Canister Diameter 0.97 m"]
+[-2.8447587490081787, 3.9184980392456055, "Capsule Height 1.31 m"]
+[1.0522830486297607, -4.418184757232666, "Satellite Mass 494 kg (dry mass), 636 kg (wet mass)"]
+[2.1000280380249023, -0.5659515261650085, "Satellite Power 202 W average (EOL), 254 W max"]
+[-1.5393483638763428, 9.610099792480469, "Propulsion Type Blowdown monopropellant (hydrazine) with helium pressurant"]
+[0.6829656958580017, 12.050381660461426, "Sensor Manufacturer Harris"]
+[5.364474296569824, -4.4469733238220215, "Satellite Launch Date 29 October 2018"]
+[5.4092559814453125, -4.438871383666992, "Satellite Launch Date 29 October 2018"]
+[1.0016052722930908, -4.393017292022705, "Satellite Total Mass 1980 kg"]
+[2.0779004096984863, -0.518920361995697, "Satellite Generated Power 2100 W"]
+[2.690995216369629, -2.701531171798706, "Satellite Data Rate 900 Mbit/s"]
+[4.994681358337402, -2.367070198059082, "Satellite Service Life 5 years"]
+[-3.9304027557373047, 15.636134147644043, "Imaging Microwave Radar Minimum Spatial Resolution 3 m"]
+[-3.9376509189605713, 15.664437294006348, "Imaging Microwave Radar Spotlight Mode Resolution 1 m x 3 m"]
+[-1.158733606338501, 15.102383613586426, "Multi-purpose Imaging Vis/IR Radiometer Function Measures land surface temperature and detects active fires"]
+[6.273859977722168, 7.4672441482543945, "Satellite Component Effective Energy Range 2 keV to 1 MeV"]
+[2.4013607501983643, 22.816993713378906, "Instrument Quantity 6"]
+[2.379209518432617, 22.620744705200195, "Instrument Quantity 5"]
+[-8.517967224121094, 13.681941032409668, "Parameter Value ~18%"]
+[-8.43478775024414, 13.696426391601562, "Parameter Value ~80%"]
+[1.1880062818527222, -0.8049420714378357, "Satellite Size 12U"]
+[4.664188385009766, -2.5843968391418457, "Satellite Duration 1 year science operation with an additional several months for maneuvering and decommissioning"]
+[7.3331475257873535, 12.458024024963379, "Satellite Instrument Power On Time Jan. 28, 7:23 p.m. EST"]
+[7.353993892669678, 12.478893280029297, "Satellite Instrument Power Off Time Jan. 28, 7:40 p.m. EST"]
+[1.844081997871399, -2.1752114295959473, "Satellite Orbit Geostationary"]
+[1.827152132987976, -2.15551495552063, "Satellite Orbit Geostationary"]
+[0.47532597184181213, 11.28273868560791, "Vision Based Sensor Mode Cooperative and non-cooperative"]
+[0.4688359797000885, 11.291105270385742, "Vision Based Sensor Far Range LOS Measure 2 DOF"]
+[0.4748915731906891, 11.20039176940918, "Vision Based Sensor Close Range Solution 3DOF translational solution or a full 6 DOF pose/translation solution"]
+[-1.7769806385040283, 8.82823371887207, "RVX Control Function Objectives Regulate the spacecraft translational and rotational states around the guidance reference; Compute commands for the spacecraft actuators, based on the processing of the control error"]
+[-1.511855959892273, 13.440195083618164, "Solar Array Arc Duration 3 hours"]
+[-1.1423567533493042, 11.764266967773438, "Array Biasing Step Occurs if arcs do not occur on the high-voltage array"]
+[-8.548590660095215, 13.677379608154297, "Comparator Output Voltage Repeats High/Low in periods of several microseconds (\u00b5s)"]
+[-1.9272544384002686, 8.096065521240234, "IC Output One pulse lasting one second"]
+[2.927743911743164, 22.40061378479004, "Instrument Components USO (Ultra Stable Oscillator), MWA (Microwave Assembly), horn, IPU (Instrument Processing Unit), SPU (Signal Processing Unit)"]
+[2.7183098793029785, 23.622150421142578, "Instrument Redundancy The IPU, SPU, KBR and ACC are internally redundant, and the ultra-stable oscillator (USO) is redundant"]
+[-4.606708526611328, 9.63160514831543, "Ultra Stable Oscillator Redundancy Redundant"]
+[-2.990751266479492, 4.222565174102783, "Spacecraft First Orbit Apogee Altitude 890 km"]
+[-2.963902473449707, 4.167689323425293, "Spacecraft First Orbit Perigee Altitude 200 km"]
+[-2.974386692047119, 4.151070594787598, "Spacecraft Second Orbit Apogee Altitude 5,808 km"]
+[-3.0022966861724854, 4.284546852111816, "Spacecraft Location of Inspection Naval Base San Diego Mole Pier"]
+[-2.991150379180908, 4.240799903869629, "Spacecraft Inspection Areas Back shell thermal protection system tiles, back shell thermal barriers, reaction control system thruster nozzles, base heat shield acreage, docking hatch thermal protection system blankets, docking hatch window, and crew module windows"]
+[-3.078845500946045, 4.178856372833252, "Spacecraft Assessment Tool Bumper 3 code and the ORDEM 3 orbital debris environment"]
+[-2.999758243560791, 4.2306365966796875, "Spacecraft Window Damage Assessment ORDEM 3 predicted 0.2 features of 0.3 mm and greater diameter"]
+[-3.1113500595092773, 4.243120193481445, "Spacecraft Heat Shield Avcoat"]
+[-3.017688035964966, 4.359481334686279, "Spacecraft Location of Heat Shield Extraction NASA/MSFC (Marshall Space Flight Center)"]
+[2.6871886253356934, 22.494937896728516, "Instrument Usable Cloud-Free Data Collection 20% to 46%"]
+[2.2111480236053467, 22.642183303833008, "Instrument Improvement Factor 2.3 times"]
+[2.2544071674346924, 22.609699249267578, "Instrument Expected Improvement Substantial"]
+[-1.2002145051956177, 8.61125373840332, "Component Shape Toroidal"]
+[-1.2327886819839478, 8.599679946899414, "Component Inner Diameter 1.1 m"]
+[-1.232956051826477, 8.616628646850586, "Component Outer Diameter 2.7 m"]
+[-1.215270757675171, 8.606353759765625, "Component Length of Central Cylinder 0.9 m"]
+[-4.488749027252197, 12.075398445129395, "Magnet Temperature 1.8 K"]
+[-0.803925096988678, 8.717865943908691, "Cooling Agent Volume 2500 l"]
+[-0.7811344861984253, 8.613740921020508, "Cooling Agent Boiling Throughout the lifetime of the experiment"]
+[-5.920557975769043, 16.004985809326172, "Synthetic Aperture Radar Frequency 5.35 GHz"]
+[-5.8924689292907715, 16.014707565307617, "Synthetic Aperture Radar Field of Regard 659 km"]
+[-5.888951301574707, 15.971748352050781, "Synthetic Aperture Radar Spatial Resolution 1 - 50 m"]
+[-5.9020233154296875, 15.992279052734375, "Synthetic Aperture Radar Swath Width 10 - 240 km"]
+[-5.873061180114746, 16.002758026123047, "Synthetic Aperture Radar Incidence Angle Coverage 12\u00b0- 55\u00b0"]
+[0.4656130373477936, -1.4842724800109863, "Satellite Orbit Altitude 536 km"]
+[0.7463821768760681, -2.2650017738342285, "Satellite Orbit Inclination 97.55\u00b0"]
+[3.8734514713287354, -3.1791930198669434, "Satellite LTAN 0600 and 1800 hours"]
+[1.0111863613128662, 0.7708306312561035, "Earth-observation satellite Data Relay Method Highly precise lasers"]
+[-1.6217528581619263, 1.4853588342666626, "Data Relay System Partnership ESA and Airbus"]
+[-1.622617483139038, 1.4800938367843628, "Data Relay System Investment German Space Administration DLR"]
+[0.7234100699424744, 11.958833694458008, "Sensor Mounting Location On the OSC"]
+[-3.216296911239624, 4.176792144775391, "Spacecraft Role Chaser spacecraft"]
+[-5.577187538146973, 7.040718078613281, "Communication Link Purpose Relay camera measurements"]
+[0.2873765230178833, 10.56352710723877, "Vision-Based System Information Source RVX (RendezVous Experiment)"]
+[0.13735556602478027, 7.16841983795166, "RendezVous Experiment Conduct Autonomously"]
+[2.4484925270080566, 22.83591079711914, "Instrument Number of Electrodes 3"]
+[2.540764570236206, 22.367063522338867, "Instrument Electrode Shape Spherical"]
+[1.8334437608718872, 22.227758407592773, "Instrument Debye Length 0.2 to 1 cm"]
+[1.8658795356750488, 22.21078109741211, "Instrument Probes Distance 10 cm"]
+[-2.6026611328125, 9.627552032470703, "Power Source Quantity 4 3U double sided solar panels and 1 additional 2U solar panel"]
+[-2.5864086151123047, 9.596966743469238, "Power Source Type UTJ (Ultra Triple Junction)"]
+[-2.5659685134887695, 9.644438743591309, "Power Source Average Power 9.1 W"]
+[-3.7416810989379883, 8.27641773223877, "Power Storage Capacity 30 W hr"]
+[-2.5046496391296387, 9.275158882141113, "Power Conditioning Output Voltages 3.3, 5 and 12 V"]
+[-2.1911542415618896, 6.9211907386779785, "Flight Computer Model PIC24"]
+[-2.2616324424743652, 6.934866428375244, "Flight Computer Type Salvo Real Time Operating System"]
+[-3.8997037410736084, 7.912806034088135, "Data Storage Usage Payload data storage"]
+[-0.9449418187141418, 9.819544792175293, "Rocket Payload Mass 10,264 kg"]
+[-0.9736632108688354, 9.510271072387695, "Rocket Component Extension Length 1.5 m"]
+[-0.8997225165367126, 11.663735389709473, "Detector-Collimator System Number of Systems 5"]
+[-0.9494078755378723, 11.72360897064209, "Detector-Collimator System Polar Angles 30o, 60o, 90o, 120o, and 150o"]
+[-0.8739340901374817, 11.672415733337402, "Detector-Collimator System Collimator Angle Nominal 10o full angle"]
+[-0.8840811848640442, 11.642848014831543, "Detector-Collimator System Energy Channels 5"]
+[-0.9173420071601868, 11.663742065429688, "Detector-Collimator System Energy Range 43 and 300 keV"]
+[-0.8933724164962769, 11.670210838317871, "Detector-Collimator System Full Energy and Azimuthal Coverage Time 100 seconds"]
+[-0.950117290019989, 11.723794937133789, "Detector-Collimator System Full Latitudinal Coverage Time 5 successive 100-second intervals"]
+[-0.3475455343723297, 13.432339668273926, "Error Detection System Function Looking for single-event upset errors in a known memory pattern in the memory of a test RAM"]
+[-3.8044722080230713, 6.93169641494751, "Data Collection System Field of View About 80o great circles of the arc of its subsatellite point"]
+[1.24370539188385, -0.9774343967437744, "Satellite Optic Diameter < 10 cm"]
+[0.6597821712493896, 12.081079483032227, "Sensor Maximum Distance to Targets Unknown"]
+[0.9100266098976135, -1.3675650358200073, "Satellite Maximum Separation < 100 km"]
+[0.6852816343307495, -1.4210070371627808, "Satellite Relative Tangential Velocity < 3 km/s"]
+[0.7276298403739929, -2.267814874649048, "Satellite Solar Separation Angle > 30\u00ba"]
+[0.7159884572029114, -2.301684617996216, "Satellite Earth Exclusion Angle 85\u00ba"]
+[0.7466921210289001, -2.296440839767456, "Satellite Lunar Exclusion Angle 1\u00ba"]
+[2.600123643875122, 22.445894241333008, "Instrument Signal Amplification Method Dynamic nuclear polarization process"]
+[-4.619925022125244, 9.635747909545898, "Oscillator Polarization Amplification Factor About 3000"]
+[-4.68237829208374, 9.593605041503906, "Oscillator RF Frequency Variable"]
+[-4.643882751464844, 9.685005187988281, "Oscillator Polarities Positive or negative"]
+[-5.254300594329834, 7.859814167022705, "Communication System Modulation OQPSK"]
+[-5.26176643371582, 7.864504814147949, "Communication System Coding Convolutional + RS"]
+[-5.2149553298950195, 7.7768635749816895, "Communication System Maximum Bit Rate 50 Mbit/s"]
+[-5.269980430603027, 7.994604587554932, "Communication System Maximum Spectral Width Smaller than 375 MHz"]
+[-4.56527853012085, 7.466775894165039, "Transmission System Frequency Band EESS X-band"]
+[-1.5087171792984009, 13.426066398620605, "Solar Array Open Circuit Voltage Approximately 7V"]
+[-1.494504451751709, 13.417268753051758, "Solar Array Number of Spherical Cell Modules 66"]
+[-1.4994522333145142, 13.446000099182129, "Solar Array Maximum Generation Voltage Approximately 900 V"]
+[-1.499917984008789, 13.415926933288574, "Solar Array Generation Voltage Regulation Up to 350 V"]
+[-0.543846070766449, 11.750727653503418, "Silicon Tracker Number of Sensors 2300"]
+[-0.4693302512168884, 11.803528785705566, "Silicon Tracker Position Resolution 8.5 \u00b5m"]
+[-0.5103194117546082, 11.822087287902832, "Silicon Tracker Total Instrumented Surface Area 6.45 m2"]
+[-0.5743700265884399, 11.730405807495117, "Silicon Tracker Readout Channels 196 k"]
+[0.24355725944042206, 9.773956298828125, "Alignment System Position Accuracy Better than 4 \u00b5m"]
+[-0.8428826928138733, 8.740974426269531, "Cooling System Purpose Evacuate the heat generated by the STD front-end electronics"]
+[-1.484636902809143, 9.567342758178711, "Hall Effect Thruster Power 200 W"]
+[-1.2974120378494263, 9.492622375488281, "Propellant Performance Similar to xenon (Xe)"]
+[-1.3189228773117065, 6.132111549377441, "Company EP Technologies Iodine-fueled HETs up to 10 kW power"]
+[-5.022511959075928, 7.85230016708374, "Command Control, Communications Segment Number of Satellite Operations Centers 2"]
+[-4.823705673217773, 7.797519207000732, "Command Control, Communications Segment Primary Satellite Operations Control Center Location Suitland, MD"]
+[-4.892437934875488, 7.807476997375488, "Command Control, Communications Segment Backup Environmental Satellite Operations Center Location SOC 81, Shriever (Falcon) AFB, Colorado Springs, CO"]
+[5.135244369506836, -4.4573259353637695, "Satellite Transfer Date December 23, 1999"]
+[2.8641581535339355, 22.023334503173828, "Instrument Purpose Detecting and measuring the energy of particles"]
+[1.1242482662200928, 13.197450637817383, "Modulation and Coding Type Offset Quadrature Phase Shift Keying"]
+[-8.407001495361328, 13.606303215026855, "Error Correction Parameters k=7, R= \u00bd"]
+[-8.415279388427734, 13.604879379272461, "Error Correction Parameters 255/223"]
+[1.129857063293457, 13.205881118774414, "Modulation and Coding Operation Locations Transmitter, Mass Memory, Processor"]
+[-5.443320274353027, 7.796682834625244, "Communication Type Continuous"]
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+[0.6075781583786011, 12.114291191101074, "Sensor Accuracy High"]
+[0.6523783802986145, 12.032597541809082, "Sensor Use Case Position-monitoring in PROBA-3"]
+[0.623675525188446, 12.01675796508789, "Sensor Use Case Monitoring the relative positions between craft in the constellation"]
+[0.6612878441810608, 11.984688758850098, "Sensor Use Case Monitoring the structural distortion before, during, and after deployment"]
+[2.2959115505218506, -1.2910503149032593, "Satellite Data Recording Conventional film"]
+[2.601011037826538, -1.305868148803711, "Satellite Data Return Film canisters were jettisoned and returned to Earth via parachute and recovered by aircraft"]
+[3.305436134338379, 0.4159698784351349, "Satellite Program Sensor Development Primary sensor and developing secondary sensor concepts"]
+[3.3234012126922607, 0.4595053791999817, "Satellite Program Secondary Sensor Complement Now flying on DMSP"]
+[2.2390449047088623, 22.594663619995117, "Instrument Imaging Wavelength Ultraviolet light"]
+[2.555713653564453, 22.76913833618164, "Instrument Cadence 30 min"]
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+[2.7156968116760254, 22.22008514404297, "Instrument Imaging Ionosphere"]
+[-13.939393043518066, -2.2280173301696777, "X-ray Telescope Map Accuracy Most accurate"]
+[-13.783348083496094, -2.3162431716918945, "X-ray Telescope First Light Date 22 October 2019"]
+[1.4542088508605957, 10.956829071044922, "ScanSAR Mode Swath 223 km"]
+[1.517797589302063, 10.917078018188477, "ScanSAR Mode Resolution 50 m"]
+[1.3901400566101074, 11.00384521484375, "ScanSAR Mode Swath 115 km"]
+[1.4644848108291626, 10.918744087219238, "ScanSAR Mode Resolution 25 m"]
+[2.409497022628784, 12.05034065246582, "High Resolution Sliding Spotlight Mode Ground Spot Size 10 km x 100 km"]
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+[-4.524750709533691, 12.110305786132812, "Magnetometer Development Date June 3, 2010"]
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+[2.744464874267578, 23.52216339111328, "Instrument Operational Life 12 months"]
+[2.431175947189331, 22.680492401123047, "Instrument Number of Images 90 in first 6 months"]
+[4.12872314453125, 13.967066764831543, "Laser Altimeter Measurement Accuracy About 10 vertical centimeters"]
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+[2.027801036834717, -1.336007833480835, "Satellite Data Type Tree Height"]
+[0.9729840159416199, -4.365438461303711, "Satellite Total Mass 100 kg"]
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+[1.145853877067566, -0.7663044333457947, "Satellite Size Cube with 700 mm length of each side"]
+[6.196983814239502, 7.525968074798584, "Satellite Component Mass 25 kg"]
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+[-2.5549142360687256, 9.438272476196289, "Power Distribution Voltage Regulated 28V \u00b1 2%"]
+[-2.354947805404663, 7.292472839355469, "Onboard Computers Type Military specification 31750a (dual-redundant silicon-on-sapphire)"]
+[-3.3499293327331543, 8.53512954711914, "Computer Memory Capacity 2 MByte per computer"]
+[2.7558717727661133, -3.245182514190674, "Satellite Communication Uplink S-band at 1 kbit/s"]
+[2.7240171432495117, -3.2114417552948, "Satellite Communication Downlink S-band at 10 kbit/s"]
+[1.4640989303588867, -2.215665340423584, "Satellite Control Spin Stabilized Control \u00b1 3\u00ba"]
+[1.3522499799728394, -2.2652652263641357, "Satellite Control Sun Aspect Angle 90\u00ba \u00b1 10\u00ba"]
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+[2.50822377204895, -1.1769018173217773, "Satellite Data Usage Hydrological variations monitoring"]
+[2.4765896797180176, -1.1325939893722534, "Satellite Data Usage Hydrological variations monitoring"]
+[-0.8471405506134033, 16.432247161865234, "Fourier Transform Spectrometer Objective Measure the density of greenhouse gases in the atmosphere"]
+[5.243317127227783, -3.7832460403442383, "Satellite Launch Year 2018"]
+[-0.8325011730194092, 16.424816131591797, "Fourier Transform Spectrometer Manufacturer Harris Corp. of Melbourne FL, USA"]
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+[4.643062114715576, -2.5754168033599854, "Satellite Duration of All Sky Survey 4 years"]
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+[4.744762897491455, -2.4928343296051025, "Satellite Follow-up Period 3 years"]
+[2.640174627304077, 5.404167175292969, "Radio Beacon Frequencies 150, 400 and 1067 MHz"]
+[2.6574127674102783, 5.392633438110352, "Radio Beacon Objective Observe ionospheric densities and irregularities"]
+[2.602430582046509, 21.90521240234375, "Instrument Function Provide on-orbit in-situ measurements"]
+[-7.396633625030518, 2.8690574169158936, "Cosmic Ray Detector Observation Date 11 January 2018"]
+[-7.394874095916748, 2.8688316345214844, "Cosmic Ray Detector Publication Date 11 January 2018"]
+[-1.9633030891418457, 15.081121444702148, "Radiometer and Polarimeter Measurement Multidirectional and polarised solar radiation reflected by the atmosphere and Earth\u2019s surface"]
+[-1.9361956119537354, 15.048516273498535, "Radiometer and Polarimeter Electromagnetic Spectrum Visible and near-infrared (VIS/NIR)"]
+[-5.902318000793457, 16.00800323486328, "Synthetic Aperture Radar Ground Resolution 25 x 6 m"]
+[-5.898000717163086, 16.000335693359375, "Synthetic Aperture Radar Wavelength 100-500 m"]
+[-5.892110824584961, 16.001619338989258, "Synthetic Aperture Radar Wave Direction 15\u00ba 360\u00ba"]
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+[-5.9168877601623535, 15.962983131408691, "Synthetic Aperture Radar Wind Speed 2-15 m/s"]
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+[0.10355205833911896, 7.200389862060547, "Experiment Critical Viscosity of Xenon-2 Unknown"]
+[2.72571063041687, 22.380929946899414, "Instruments Detection Capability Increases in signal levels when marine plastic waste is present"]
+[-6.711669445037842, 9.990063667297363, "Antenna Engineer Peter de Maagt"]
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+[2.6769707202911377, -1.588940978050232, "Satellite X-ray Emission Low level"]
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+[2.1619534492492676, -2.6373636722564697, "Satellite New Exoplanets Found 66"]
+[1.9903827905654907, -2.732938289642334, "Satellite Exoplanet Candidates Nearly 2,100"]
+[3.07265043258667, -1.703360915184021, "Satellite Project Scientist Patricia Boyd"]
+[3.560041904449463, 13.843353271484375, "Laser Ranging Interferometer Objective Measure the same range fluctuations as the KBR instrument, but with less noise, and provide precise measurements of the relative pointing of the satellites to each other"]
+[3.5734453201293945, 13.894979476928711, "Laser Ranging Interferometer Reliability Requirements Less stringent than the primary KBR instrument"]
+[3.592259168624878, 13.88122844696045, "Laser Ranging Interferometer Potential Future Use Primary instrument in future GRACE-type missions"]
+[7.51611852645874, 12.651111602783203, "Satellite Instrument Data Release Date 12 March 2019"]
+[7.293823719024658, 12.429969787597656, "Satellite Instrument URL https://gold.cs.ucf.edu"]
+[-1.3183624744415283, 6.239367961883545, "Manufacturer Telescopes, detectors and associated electronics Unknown"]
+[-0.9839679598808289, -9.960915565490723, "Satellite Constellation Launch Date 2021"]
+[-0.9431253671646118, -10.004729270935059, "Satellite Constellation Manufacturer Raytheon Space Systems"]
+[-0.954284131526947, -9.99609375, "Satellite Constellation Imager Manufacturer Raytheon Space Systems"]
+[-0.945330023765564, -10.008606910705566, "Satellite Constellation Imager Manufacturer Experience 45 years"]
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+[3.0514490604400635, -1.6580876111984253, "Satellite Collaboration Partner MBIE (Ministry of Business Innovation & Employment)"]
+[2.954401731491089, -1.5883945226669312, "Satellite Collaboration Partner EDF"]
+[4.988183498382568, -3.9591312408447266, "Satellite Data Release 1977"]
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+[2.981334686279297, -2.008359432220459, "Satellite Commercial Users 15 companies"]
+[2.833897829055786, -1.7704036235809326, "Satellite Commercial Results Improved forecasts lead to better routing of ships with substantial savings in operating costs"]
+[-1.7708511352539062, 8.626527786254883, "Control Electronics Function Control the Externally Occulted Solar Coronagraph Instrument"]
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+[-2.074540615081787, 12.609114646911621, "Solar Ultra Violet Imager Wavelength Range 9.4 nm - 30.4 nm"]
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+[-1.0822677612304688, 7.777968883514404, "Device Function Analyzing the bi-dimensional distribution of the spectral profiles of several coronal emission lines (CEL)"]
+[-2.7152247428894043, 4.1345367431640625, "Space System Separation -145 m"]
+[-1.918015718460083, 15.03773021697998, "Radiometer/Polarimeter CCD Detection Array 274 x 242 pixels"]
+[-1.8955633640289307, 15.079495429992676, "Radiometer/Polarimeter Optics Field-of-View \u00b1 51\u00ba cross-track and \u00b1 43\u00ba along-track"]
+[-1.986560583114624, 15.095431327819824, "Radiometer/Polarimeter Filters Spectral and polarized"]
+[-4.563742160797119, -3.0855064392089844, "Exoplanet Mission Unknown Unknown"]
+[-1.3253155946731567, 6.107149124145508, "Company Image Sensor Supplier Unknown"]
+[-4.556278705596924, -3.0575692653656006, "Exoplanet Mission Delivery Date 11 April 2019"]
+[-4.594326019287109, -3.041416645050049, "Exoplanet Mission Construction Start Date 4 October 2018"]
+[-4.555386543273926, -3.0688891410827637, "Exoplanet Mission Proposal Selection Date 25 April 2018"]
+[-5.47426700592041, 2.8147032260894775, "Telescope Primary Mirror Material SiC"]
+[-5.449399948120117, 2.7107632160186768, "Telescope Secondary Mirror Material SiC"]
+[-5.3993988037109375, 2.7879340648651123, "Telescope Tertiary Mirror Material SiC"]
+[-5.389862537384033, 2.8134403228759766, "Telescope Folding Mirror Material SiC"]
+[-5.396361827850342, 2.838862419128418, "Telescope Focal Plane Components Detectors, filters, front-end electronics"]
+[-5.451733589172363, 2.804722309112549, "Telescope Detection Chain Components Detectors, F2EM, MEV"]
+[-1.9503204822540283, 7.312072277069092, "Computer Data Storage Unknown"]
+[-1.9540061950683594, 7.304190635681152, "Computer Data Transmission Ku-band"]
+[0.16273652017116547, 7.137096405029297, "Experiment Downlink Bandwidth 2 Mbit/s"]
+[-1.9370291233062744, 7.333722114562988, "Computer Data Transmission HRDL"]
+[7.319736003875732, 12.449347496032715, "Satellite Instrument Cloud Discrimination Unknown"]
+[7.306874752044678, 12.429404258728027, "Satellite Instrument Support Vectors Unknown"]
+[0.11614621430635452, 14.488916397094727, "Reflectance Calibration Assembly Light Source Phosphor light source with peak emission over the TOMS wavelength range"]
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+[2.871187686920166, -1.295941948890686, "Satellite Mission Purpose Mapping differences in land cover, understanding the landscape, mapping how it is used, monitoring changes over time"]
+[-3.0166192054748535, 4.207389831542969, "Spacecraft Observation Region (Summer) Northern latitude range of 70-80\u00ba"]
+[-2.990380048751831, 4.176262378692627, "Spacecraft Observation Region (Winter) Northern latitude range of 40-50\u00ba"]
+[-2.9603075981140137, 4.149374485015869, "Spacecraft VNIR Imagery 500 km x 500 km with a spatial resolution of 500 m"]
+[-2.9363861083984375, 4.150455951690674, "Spacecraft Laser Wavelengths 1570 nm and 1556 nm"]
+[-5.355442047119141, 2.826289415359497, "Telescope URL http://airex.tksc.jaxa.jp/dr/prc/japan/contents/AA0064574157/64574157.pdf"]
+[-5.416982650756836, 2.811988115310669, "Telescope URL http://www.nustar.caltech.edu/uploads/files/helio_decadal_WP_10nov.pdf"]
+[-3.691405773162842, 7.071405410766602, "Data Archive Data Source International Best Track Archive for Climate Stewardship"]
+[2.533438205718994, -1.2838374376296997, "Satellite Data Source GOES 16 data from NOAA and the National Centers for Environmental Information (NCEI)"]
+[-3.4645707607269287, 6.81444787979126, "Visualization Data Source IBTrACS"]
+[5.19444465637207, -4.322691440582275, "Satellite Launch Date 16 September 2021"]
+[-3.0405805110931396, 4.417518615722656, "Ocean Vessel Landing Platform Falcon-9 rocket first stage"]
+[-0.978949785232544, 9.800202369689941, "Rocket Destination International Space Station"]
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+[3.766390800476074, 13.710877418518066, "Photon-counting laser altimeters Data Set Just a few dozen photons at most"]
+[1.3918371200561523, -1.1003965139389038, "Satellite Vegetation Height Accuracy 3\u2010m"]
+[1.4624814987182617, -1.2341318130493164, "Satellite Spatial Resolution 1 km"]
+[-1.5062434673309326, 16.900728225708008, "Altimeter Surface Acoustic Wave Generator Bandwidth 300 MHz"]
+[-1.5045241117477417, 16.90178108215332, "Altimeter Surface Acoustic Wave Generator Frequency 900 MHz"]
+[-1.5200153589248657, 16.9099063873291, "Altimeter Frequency Conversion 13.65 GHz"]
+[-1.5031816959381104, 16.9012451171875, "Altimeter Output Data Sea state and wind speed"]
+[-3.084744691848755, 4.273261070251465, "Spacecraft Purpose Carry the crew to space, provide emergency abort capability, sustain the crew during the space travel, and provide safe reentry from deep space return velocities"]
+[-3.060364007949829, 4.2533392906188965, "Spacecraft Capability Conduct regular in-space operations (rendezvous, docking, extravehicular activity) in conjunction with payloads delivered by the Space Launch System (SLS) for missions beyond LEO"]
+[-3.0908000469207764, 4.236619472503662, "Spacecraft Capability Be a backup system for International Space Station cargo and crew delivery"]
+[16.81838035583496, 6.892904758453369, "Microsatellite Mass About 44 kg"]
+[16.92873764038086, 6.790745258331299, "Microsatellite Orbit Duration About 3 years"]
+[16.872344970703125, 6.839396953582764, "Microsatellite Orbit Altitude About 450 km"]
+[2.487746238708496, 22.67498779296875, "Instrument Spectral Bands VIS and IR"]
+[2.3047783374786377, 22.65593719482422, "Instrument IR Channels 44 channels from 6.21-11.76 \u00b5m (850-1610 cm -1 ) with 0.1296 \u00b5m interval"]
+[2.401777744293213, 22.74649429321289, "Instrument IR Channels 22 channels from 3.0 - 5.7 \u00b5m (1754-3330 cm -1 )"]
+[2.33516788482666, 22.697595596313477, "Instrument IR Channels 22 channels from 12.78-12.85 \u00b5m (778.2-782.4 cm -1 ) with 0.2 cm -1  resolution"]
+[2.3149361610412598, 22.693239212036133, "Instrument VIS Channels 1024 channels from 0.753 - 0.784 \u00b5m with 0.1 nm FWHM resolution"]
+[2.6067428588867188, 14.281073570251465, "Optical Instrument Aperture Diameter 13 cm"]
+[-0.9403001666069031, 7.838930130004883, "Positioning Device Resolution 8 arcsec per pixel"]
+[2.296506643295288, 22.009784698486328, "Instrument IFOV 1 km (vertical) x 13 km (horizontal)"]
+[2.229813814163208, 22.155960083007812, "Instrument IFOV 1 km (vertical) x 21.7 km (horizontal)"]
+[2.2913007736206055, 22.044851303100586, "Instrument IFOV 1 km (vertical) x 2 km (horizontal)"]
+[2.290555715560913, 22.133544921875, "Instrument Observation Region Latitudinal zones 56\u00ba - 70\u00ba N and 63\u00ba - 88\u00ba S"]
+[2.311566114425659, 22.985919952392578, "Instrument Data Rate 453.7 kbit/s"]
+[2.652702569961548, 23.308027267456055, "Instrument Operation Time 12 minutes per occultation (limb observations)"]
+[1.4635123014450073, 21.174884796142578, "Instrument Mass < 138 kg"]
+[1.6566306352615356, 23.184717178344727, "Instrument Power < 120 W"]
+[1.6189364194869995, 22.158021926879883, "Instrument Size 950 mm x 1670 mm x 600 mm"]
+[2.351667642593384, -1.5899667739868164, "Satellite Mission Type Optical High Resolution"]
+[5.0904693603515625, -4.472790241241455, "Satellite Mission Date Oct. 15-16, 2007"]
+[-0.477981835603714, 5.867372035980225, "Unknown Size 10 cm x 10 cm x 8.2 cm"]
+[-0.48379603028297424, 5.823462009429932, "Unknown Mass 1 kg"]
+[-0.4653754234313965, 5.845692157745361, "Unknown Power Consumption <1.5 W"]
+[-0.5028553605079651, 5.8665690422058105, "Unknown Interface RS-422 or 1553B"]
+[-3.1348140239715576, 1.753649115562439, "Satellite Mission Formation Flying Unknown"]
+[-3.235727071762085, 1.7237385511398315, "Satellite Mission Participants Meeting Date March 13, 2008"]
+[2.1491897106170654, -1.756220817565918, "Satellite Mode Bent-pipe and Regenerative"]
+[2.6416118144989014, -2.6910934448242188, "Satellite Link Speed 1.2 Gbit/s"]
+[1.7678577899932861, -2.326359987258911, "Satellite Orbit Geostationary orbit (GEO) over the Pacific Ocean at 143\u00ba E longitude, altitude ~ 35,786 km"]
+[5.3215718269348145, -4.472710609436035, "Satellite Launch Date Feb. 23, 2008"]
+[5.061246395111084, -4.340334415435791, "Satellite End of Mission Date March 1, 2019"]
+[-5.410975933074951, 2.7574098110198975, "Telescope Envelope Dimensions \u00d8 1.3 m x 2.1 m"]
+[-5.412259578704834, 2.7558884620666504, "Telescope Mass < 80 kg"]
+[-5.355254173278809, 2.8304965496063232, "Telescope First Natural Frequency > 70 Hz"]
+[-5.390160083770752, 2.767324686050415, "Telescope Design Load 15 g per axis"]
+[-5.334402084350586, 2.7537522315979004, "Telescope In-orbit Environmental Temperatures -10\u00baC ~ +45\u00baC"]
+[-5.41909646987915, 2.7410202026367188, "Telescope Qualification Temperatures -15\u00baC ~ +55\u00baC"]
+[5.337532997131348, -4.441501140594482, "Satellite Launch Date 23 December 2017"]
+[4.430583953857422, -3.3713676929473877, "Satellite Launch Time (JST) 10:26:22"]
+[4.4086222648620605, -3.3989622592926025, "Satellite Launch Time (UTC) 01:26:22"]
+[-3.2585718631744385, 5.4141950607299805, "Launch Vehicle Launch Provider Mitsubishi Heavy Industries, Ltd."]
+[-3.271946430206299, 5.427028179168701, "Launch Vehicle Primary Payload GCOM-C1 spacecraft of JAXA"]
+[2.0537564754486084, -2.794886589050293, "Satellite Number of Satellites 2"]
+[3.5949110984802246, 13.858014106750488, "Laser Ranging Interferometer Manufacturer BATC (Ball Aerospace & Technologies Corporation)"]
+[-1.2403141260147095, 6.89827823638916, "Preliminary Design Review Date Jan. 20-24, 2014"]
+[-1.559527039527893, 12.820364952087402, "Coronagraph Detection Distance ~0.04 solar radii"]
+[-1.5558531284332275, 12.810506820678711, "Coronagraph Platforms Separation About 145 m"]
+[2.6705899238586426, -1.0317022800445557, "Satellite Monitoring Target Methane emissions"]
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+[-2.6538825035095215, 11.499920845031738, "Image Date 24 September 2020"]
+[-0.8777406811714172, 6.401500225067139, "Article Date 25 August 2020"]
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+[4.3559370040893555, -2.6694681644439697, "Satellite Time to Final Orbit About 60 days"]
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+[-0.9621933102607727, 7.656219482421875, "Device Objectives Unambiguous association of lightning with TLEs and TGFs, better understanding of the physical mechanisms behind them, variation in TLEs and TGFs"]
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+[-3.1119909286499023, 4.30405330657959, "Spacecraft Telemetry Downlink Speed 20 kbit/s"]
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+[-2.0943071842193604, 6.949124336242676, "Effort Data Combination Data from 13 NASA and ESA missions"]
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+[-3.6169402599334717, 12.748641967773438, "Particle Physics Detector Gamma-ray Energy Range Up to hundreds of GeV"]
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+[1.1875633001327515, -0.8199473023414612, "Satellite Thermal Capacity Very small"]
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+[3.375384569168091, -2.8452131748199463, "Satellite Total Hours 910.29"]
+[1.8210464715957642, -2.577061891555786, "Satellite Total Orbits 36836"]
+[2.227930784225464, -2.7414896488189697, "Satellite Total Hours 12405.95"]
+[-3.1324262619018555, 4.279208183288574, "Spacecraft Mission Status Planned"]
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+[-3.056161880493164, 4.279135704040527, "Spacecraft Sensor Complement Detection and characterization of terrestrial exoplanets around bright solar-type stars"]
+[4.67153787612915, -2.58893084526062, "Satellite Routine Flight Operations Duration At least 15 years"]
+[-1.794697642326355, 8.754437446594238, "Control Center Development Location DLR's GSOC"]
+[2.091120481491089, -2.7047033309936523, "Satellite Number of Receiver Antennas 4"]
+[2.510298490524292, -2.0415961742401123, "Satellite Assembly Platform SmallGEO platform"]
+[1.0197303295135498, 0.7326850891113281, "Earth Observation Satellite Payload Capacity Up to 50 kg"]
+[1.048203706741333, 0.7356330752372742, "Earth Observation Satellite Power Capacity Up to 50 W"]
+[1.0131884813308716, 0.7658610343933105, "Earth Observation Satellite Structure Size 60 cm x 60 cm x 100 cm"]
+[5.122138023376465, -4.428924560546875, "Satellite Data Release Date 19 October 2012"]
+[2.2765018939971924, -1.2447588443756104, "Satellite Imaging Products SAR data"]
+[2.2136991024017334, -1.9981224536895752, "Satellite Operational Modes Multiple"]
+[-9.952061653137207, 5.855570316314697, "Search and Rescue System URL http://poes.gsfc.nasa.gov/sarr-sarp.html"]
+[-9.95749282836914, 5.851944923400879, "Search and Rescue System Document C/S T.003, Issue 4, Oct.. 2008"]
+[-0.11823432892560959, 15.52918529510498, "Spectrometer Telescope Diameter 30 cm"]
+[-0.12698358297348022, 15.542049407958984, "Spectrometer Telescope Length 160 cm"]
+[-0.06847181916236877, 15.542891502380371, "Spectrometer Telescope Focal Length 8.66 m"]
+[-0.8661739230155945, 11.632320404052734, "Detector Array Dimensions 1024 x 1024"]
+[-0.9158667922019958, 11.699359893798828, "Detector Array Cooling Temperature -65\u00baC"]
+[-0.6343364715576172, 9.427035331726074, "Spacecraft Component Condition Excellent"]
+[-0.5644875764846802, 10.427972793579102, "Probe Component Function Protect the samples"]
+[-0.6462005972862244, 9.558927536010742, "Probe Component Function Allow solar wind particles to be deeply embedded within the material"]
+[-13.666094779968262, -2.280996799468994, "X-ray Telescope Observation Date 17 to 18 October 2019"]
+[-13.873669624328613, -2.1936302185058594, "X-ray Telescope Energy Bands Red, green and blue"]
+[-13.895454406738281, -2.2346582412719727, "X-ray Telescope Gas Temperature Tens of millions of degrees"]
+[-13.90433406829834, -2.275036573410034, "X-ray Telescope Observation Results Catalogues of millions of exotic celestial objects such as black holes, galaxy clusters, neutron stars, supernovae and active stars"]
+[1.5467751026153564, -2.0903608798980713, "Satellite Pointing Modes Heliocentric, Geocentric"]
+[0.8136765956878662, -2.2071428298950195, "Satellite Solar Array Rotation ~ 0.025 deg/sec"]
+[0.800155758857727, -2.271232843399048, "Satellite Maneuver Angle 30 deg"]
+[0.6295948624610901, 11.89561939239502, "Estimator Availability 98%"]
+[0.6711056232452393, 12.06135082244873, "Estimator Availability 66%"]
+[2.7781662940979004, 13.720731735229492, "Optical Device Mass 1.76 kg"]
+[6.349157810211182, 7.392361164093018, "Satellite Component Location S/C top deck"]
+[-1.1038886308670044, 5.430903434753418, "Facility Function Develop optical sensing, imaging, and propagation technologies"]
+[4.019438743591309, -2.54695725440979, "Satellite Formation Flying Operation Several hours"]
+[1.5418165922164917, -2.365558624267578, "Satellite Orbit Highly-elliptical Earth Orbit"]
+[2.4038712978363037, -1.9463579654693604, "Satellite GPS Measurement Availability Not available during Formation Flying operation periods"]
+[1.8539109230041504, -1.4228315353393555, "Satellite Metrology Sensor Suite Acquiring the formation and providing relative position determination with micrometric precision"]
+[1.4826152324676514, -2.2807457447052, "Satellite Sun Off-pointing Effect Thermo-elastic deformations"]
+[-3.8214516639709473, 6.856231689453125, "Data Collection Platform Data Transmission Frequency 1691, 1694.5 MHz"]
+[-3.7991745471954346, 6.853419303894043, "Data Collection Platform Time Slot 27 seconds"]
+[-3.845965623855591, 6.8782572746276855, "Data Collection Platform Bit Rate 12.5 kbit/s"]
+[-3.840524435043335, 6.857041835784912, "Data Collection Platform Transmission Slots per Hour 15"]
+[5.341185569763184, -4.43977689743042, "Satellite Launch Date July 19, 2000"]
+[1.4116315841674805, -2.4969305992126465, "Satellite Orbit Type Sun-synchronous circular orbit"]
+[0.5963050723075867, -1.4620064496994019, "Satellite Orbit Altitude 556 km"]
+[0.7152361869812012, -2.2650821208953857, "Satellite Orbit Inclination 97.3\u00ba"]
+[5.834219932556152, 14.37549877166748, "Transponder Mass 1.5 kg"]
+[2.65299916267395, -2.7121431827545166, "Satellite Uplink TT&C Data Rate 2 kbit/s"]
+[2.659742593765259, -2.7053327560424805, "Satellite Downlink TT&C Data Rate 20 kbit/s"]
+[2.663522243499756, -2.7111124992370605, "Satellite Payload Data Downlink Rate 1 Mbit/s"]
+[0.18110734224319458, 13.966362953186035, "Calibration Corner Reflector Thermal Control \u00b11\u00b0C"]
+[0.2208162248134613, 13.996400833129883, "Calibration Corner Reflector Dihedral Error Variation 0.05 arcsec"]
+[0.18949350714683533, 13.9630708694458, "Calibration Corner Reflector Temperature Reporting Thermistors on the CCRR will report the temperature of the CCRR in-flight"]
+[-1.929796576499939, 6.90730619430542, "Software Function Read the associated displacement error for that temperature from the look-up table, and subtract it from the displacement measurement"]
+[-3.326294183731079, 4.2488861083984375, "Spacecraft Mission Duration 36 days"]
+[-2.98592472076416, 4.481647491455078, "Spacecraft Payload Delivery More than 5,600 pounds of science and supplies"]
+[-1.3423515558242798, 6.101891994476318, "Company CubeSat Deployment Count 190"]
+[-1.3488857746124268, 6.099089622497559, "Company Small Satellite Deployment Count 228"]
+[-5.252871036529541, 7.896126747131348, "Communication System Type Fixed offset system with three beams"]
+[-5.206135272979736, 7.922806739807129, "Communication System Reflector Diameter 2.5 m"]
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+[-2.978938341140747, 16.148046493530273, "Scatterometer Frequency 1.26 GHz"]
+[-0.6284084916114807, 8.719029426574707, "Thermal Protection Material Filling Method Filled by hand"]
+[-3.151258707046509, 4.187935829162598, "Spacecraft Radiation Protection None beyond Earth's atmosphere and magnetic field"]
+[5.09307861328125, -4.377811908721924, "Satellite Discovery Date 24 June 2020"]
+[5.094064712524414, -4.39626932144165, "Satellite Discovery Date 24 June 2020"]
+[-0.6107041835784912, 3.2040047645568848, "Star Nature Volume 582"]
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+[-1.231601595878601, 15.086585998535156, "Imaging Multi-spectral Radiometer Instrument Type Imaging multi-spectral radiometers (vis/IR)"]
+[2.849133014678955, -2.00778865814209, "Satellite Main Payload Unknown"]
+[3.720078229904175, 17.686729431152344, "Payload Unknown Unknown"]
+[-0.5353817343711853, 5.881392955780029, "Unknown Funding Agency ASI (Italian Space Agency"]
+[2.7537899017333984, -1.8744944334030151, "Satellite Hosted Payload Unknown"]
+[3.714301824569702, 17.687023162841797, "Payload Selected by ESA Unknown"]
+[3.731107711791992, 17.702592849731445, "Payload Owner Avanti Communications (UK)"]
+[0.5392484664916992, -1.4576990604400635, "Satellite Orbit Altitude ~ 825 km"]
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+[3.881121873855591, -3.1724116802215576, "Satellite LTAN 9:30 hours"]
+[1.3470046520233154, -3.0447144508361816, "Satellites Orbit Altitude ~ 635 km"]
+[1.2860592603683472, -2.9918811321258545, "Satellites Orbit Inclination 98.8\u00ba"]
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+[3.0933218002319336, -1.5399459600448608, "Satellite Mission Partner Space Force"]
+[3.054011821746826, -1.6443655490875244, "Satellite Vice President and General Manager Mark Healy"]
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+[8.517094612121582, 13.942191123962402, "Lidar Instrument Data Availability Freely available"]
+[8.51632308959961, 13.9415922164917, "Lidar Instrument Funding Source International Space Station Program"]
+[8.517277717590332, 13.94187068939209, "Lidar Instrument Purpose Measure clouds and aerosols"]
+[8.51336669921875, 13.940879821777344, "Lidar Instrument Impact Enabled more accurate aerosol modeling and forecasting"]
+[-2.2608792781829834, 8.289215087890625, "Interface Module Configuration Capability Variable"]
+[1.1892445087432861, -2.071502685546875, "Satellite Body-pointing Event Monitoring Capability \u00b145\u00ba in any direction from nadir"]
+[0.4561730623245239, 9.365705490112305, "Attitude Control System Components RWA (Reaction Wheel Assembly), IRU (Inertial Reference Unit), STT (Star Trackers), GPSR (GPS Receiver) and the control S/W"]
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+[0.718138575553894, -2.306715488433838, "Satellite Inclination 97.84\u00b0"]
+[3.865948438644409, -3.152949810028076, "Satellite LTAN 1300 \u00b1 0015 hours"]
+[4.106292247772217, -2.4855751991271973, "Satellite Repeat Cycle 6 days"]
+[1.001311182975769, -4.380401134490967, "Satellite Mass About 1700 kg"]
+[2.071425199508667, -0.5581451058387756, "Satellite Power Generation 5kW"]
+[5.359842777252197, -2.1636905670166016, "Satellite Design Life Five years"]
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+[0.774897575378418, -2.2566447257995605, "Satellite Autonomous Rotation Angle Within 35\u00b0 of the sun"]
+[1.2471040487289429, -2.052431344985962, "Satellite Pointing Mode View the cusp from different perspectives"]
+[2.4146065711975098, -1.8841867446899414, "Satellite Avionics System Modular"]
+[2.3432323932647705, -1.600029468536377, "Satellite Science Instruments Built into the chassis"]
+[-0.46900463104248047, 13.731191635131836, "Dosimetry System Objective To record the space radiation environment absorbed dose behind various thin shields and to estimate the dose due to low energy electrons"]
+[-0.47985216975212097, 13.738212585449219, "Dosimetry System Components Four radiation sensitive dual MOSFETs"]
+[-0.8336272239685059, 12.593892097473145, "Radiation Sensor Dose Measurement Range Between rad and Mrad"]
+[-0.7741758227348328, 12.532254219055176, "Radiation Sensor Shield Each MOSFET has a unique shield covering the sensitive device"]
+[-4.555091381072998, 15.875101089477539, "Radar Mode Spotlight -"]
+[-4.504288673400879, 15.902458190917969, "Radar Mode Stripmap -"]
+[-4.5134196281433105, 15.914824485778809, "Radar Mode ScanSAR -"]
+[-4.505520343780518, 15.91189956665039, "Radar Mode Ultra-fine -"]
+[-4.518019199371338, 15.909388542175293, "Radar Mode High-sensitive -"]
+[10.909144401550293, 1.1386123895645142, "Radar Parameter 1257.5 MHz -"]
+[10.909158706665039, 1.1385513544082642, "Radar Parameter 1236.5 / 1278.5 MHz -"]
+[10.909586906433105, 1.1381633281707764, "Radar Parameter 8\u00ba to 70\u00ba -"]
+[10.909163475036621, 1.1386128664016724, "Radar Parameter 84 MHz -"]
+[10.909570693969727, 1.1383042335510254, "Radar Parameter 3 m (rg) x 1 m (az) -"]
+[10.909540176391602, 1.138296365737915, "Radar Parameter 25 km (rg) x 25 km (az) -"]
+[10.909947395324707, 1.138129472732544, "Radar Parameter SP -"]
+[10.919057846069336, 1.130263090133667, "Radar Parameter 800 Mbit/s -"]
+[10.910411834716797, 1.1377474069595337, "Radar Parameter -24 dB -"]
+[10.909106254577637, 1.1390362977981567, "Radar Parameter 25 dB -"]
+[10.907649040222168, 1.140613317489624, "Radar Parameter 20 dB -"]
+[-5.29523229598999, 7.560619831085205, "Communication Protocols Usage Successful"]
+[-5.291081428527832, 7.621221542358398, "Communication Protocol Packet Size ~ 425-475 bytes"]
+[-4.822643280029297, 7.850182056427002, "Telemetry System Packet Size Variable"]
+[-5.304321765899658, 7.500496864318848, "Communication Protocol Delivery One-way only path through NASA firewall"]
+[-5.301286697387695, 7.529138088226318, "Communication Protocol Flexibility Different telemetry packets delivered to various destinations based on onboard addressing decisions"]
+[0.9313903450965881, 0.9210984706878662, "Earth Observation Sensor Scan Pattern Conical at 45\u00ba from nadir"]
+[0.9170064330101013, 0.9403928518295288, "Earth Observation Sensor Field of Regard 144\u00ba"]
+[0.9399064779281616, 0.9122031331062317, "Earth Observation Sensor Angle of Incidence 53.1\u00ba"]
+[0.9483774304389954, 0.904817521572113, "Earth Observation Sensor Swath Width 1,700 km"]
+[0.900987982749939, 0.9525507688522339, "Earth Observation Sensor Data Channels 24"]
+[0.9547134041786194, 0.906541109085083, "Earth Observation Sensor Height Coverage Up to about 32 km"]
+[0.934267520904541, 0.9311248064041138, "Earth Observation Sensor Temperature Retrievals Extended up to about 80 km"]
+[2.39906907081604, -1.4345672130584717, "Satellite Object Observation AFSPC catalog"]
+[2.360502004623413, -1.5789308547973633, "Satellite Image Transmission Ground"]
+[1.5992823839187622, -2.025496244430542, "Satellite Orbital Parameter Refinement Reduce uncertainty in position estimation and improve accuracy of conjunction analysis"]
+[1.856840968132019, -1.7217350006103516, "Satellite Conjunction Analysis Higher level of confidence"]
+[2.35300874710083, -1.587446689605713, "Satellite Picture Taking Orbital debris"]
+[2.2675163745880127, -1.3633954524993896, "Satellite Sensor Type Spectrometer"]
+[2.2852561473846436, -1.8516570329666138, "Satellite Methane Detection Limit 2 parts per billion"]
+[0.8544269800186157, -1.4762165546417236, "Satellite View Path 200 kilometers"]
+[2.605597972869873, -1.1587860584259033, "Satellite Emission Source Detection Small emission sources over large areas"]
+[-3.325439691543579, 7.48416805267334, "Data Processing Power 0.65 W (average)"]
+[-3.338834762573242, 7.411438941955566, "Data Processing Data Storage Capacity 2GB"]
+[-3.342264413833618, 7.446962356567383, "Data Processing CMD Schedule Resolution 1 s"]
+[-3.3153269290924072, 7.4502482414245605, "Data Processing Max No of Sequences 300"]
+[-3.3425960540771484, 7.449976921081543, "Data Processing Max No of Commands 500"]
+[-3.3327507972717285, 7.450263977050781, "Data Processing Max No of Parameters 1500"]
+[-3.359161376953125, 7.438568115234375, "Data Processing Total Parameter Size 36 kB"]
+[-4.277265548706055, 7.396048069000244, "Data Transmission Bus SOH Rate 90 kB/min"]
+[-4.260371685028076, 7.3881754875183105, "Data Transmission Maximum Telemetry Rate Based on typical 1 minute snapshots with additional attitude control data saved at 1 Hz"]
+[-2.9432482719421387, 4.541041851043701, "Spacecraft Weight 5,291 pounds (2,400 kg)"]
+[-3.019883871078491, 4.276684761047363, "Spacecraft Size Roughly one-third the size of what the actual spacecraft would be"]
+[-3.032942533493042, 4.28659200668335, "Spacecraft Testing Method Dropping a prototype lander in a warehouse-like space at JPL"]
+[-2.9623584747314453, 4.450642108917236, "Spacecraft Payload Capacity Up to 200 kg"]
+[-1.6109468936920166, 9.699180603027344, "Propulsion System Manufacturer ENPULSION of Wiener Neustadt, Austria"]
+[-1.6111023426055908, 9.686972618103027, "Propulsion System Type Microsat propulsion technology"]
+[-1.051743984222412, 10.953078269958496, "CCD Device Spectral Ranges 0.5 - 0.6 \u00b5m, 0.6 - 0.7 \u00b5m, 0.8 - 0.9 \u00b5m"]
+[-1.0420342683792114, 10.990225791931152, "CCD Device Spatial Resolution 45 m x 33 m"]
+[-1.0542293787002563, 10.956929206848145, "CCD Device Swath 45 km"]
+[-1.0614311695098877, 10.939651489257812, "CCD Device Repeat Cycle 18 days"]
+[-1.0531100034713745, 10.94100570678711, "CCD Device Look Angle \u00b132\u00ba"]
+[-1.0512813329696655, 10.9741849899292, "CCD Device Scan Rate 200 lines/s"]
+[-1.0574222803115845, 10.936026573181152, "CCD Device Instrument Mass 60 kg"]
+[-1.2326409816741943, 6.544487476348877, "Natural and Human-Managed Average Seasonal Fluctuation 8.6 inches (0.22 m)"]
+[-1.328005313873291, 6.898848056793213, "Human-Managed Average Seasonal Fluctuation 34 inches (0.86 m)"]
+[-1.4557174444198608, 6.764071464538574, "Human-Managed Global Variability of Water Storage 57%"]
+[-1.3261715173721313, 6.740031719207764, "Human-Managed Vary the Most Middle East, southern Africa, and the western United States"]
+[-1.6148555278778076, 1.473658561706543, "Data Relay System Technology Laser"]
+[1.8703805208206177, -2.1566858291625977, "Satellite Orbit Geostationary"]
+[1.8548256158828735, -2.1525585651397705, "Satellite Orbit Geostationary"]
+[-3.0087006092071533, 4.216114044189453, "Spacecraft Altitude Below 1000 km"]
+[-1.1536089181900024, 4.464030742645264, "Ground Station Connection Permanent"]
+[6.371180534362793, 7.369226932525635, "Satellite Component Dimensions 3 x 13 m"]
+[-5.2598700523376465, 7.98622989654541, "Communication System Uplink Frequency 2.0 GHz"]
+[-5.305859565734863, 8.003984451293945, "Communication System Downlink Frequency 2.2 GHz"]
+[-3.643976926803589, 12.757962226867676, "Particle Detector Positron Count More than 400,000"]
+[-3.6460883617401123, 12.777450561523438, "Particle Detector Positron Fraction of Cosmic Ray Electrons Up to 10%"]
+[-1.1999304294586182, 3.1790976524353027, "Cosmic Entity Composition Unknown"]
+[2.6321029663085938, 13.45355224609375, "Optical Component Composition 30.7 nm aluminum and a 217.9 nm polyimide layer"]
+[-0.6840441823005676, 8.423340797424316, "Structural Component Mounting Optical element"]
+[-5.374881744384766, 2.786813974380493, "Telescope Structure Light Tightness Three-bounce"]
+[0.5334062576293945, 12.132272720336914, "Sensor Energy Channels 20 fixed energy channels between 30 eV and 30 keV"]
+[0.4848593473434448, 12.219572067260742, "Sensor Aperture Size About 20 x 10 (FWHM)"]
+[0.454172283411026, 12.003384590148926, "Sensor Low Energy Detector Channels 10 channels centered at 34, 49, 71, 101, 150, 218, 320, 460, 670, and 960 eV"]
+[0.4861280918121338, 12.22489070892334, "Sensor High Energy Detector Channels 10 channels centered at 1.0, 1.4, 2.1, 3.0, 4.4, 6.5, 9.5, 14.0, 20.5 and 29.5 KeV"]
+[0.563396692276001, 12.179387092590332, "Sensor Integration Time 0.09 s"]
+[0.5082827806472778, 12.176553726196289, "Sensor Data Volume Approximately 1 Mbyte per satellite"]
+[-0.3360215127468109, 4.918002605438232, "Ice Island Dimensions 7 kilometres by 12 kilometres"]
+[-0.44763457775115967, 4.925473690032959, "Ice Island Discovery Year 1946"]
+[-0.4098189175128937, 4.863653659820557, "Ice Island Tracking Duration Since 1946"]
+[4.8558173179626465, -4.207347869873047, "Satellite Imaging Period August 16 to October 6, 1978"]
+[0.7248538732528687, -1.400262475013733, "Satellite Travel Distance 157 km"]
+[4.429687023162842, -2.6218202114105225, "Satellite Travel Duration 61 days"]
+[-2.9888193607330322, 16.170515060424805, "Scatterometer Pulse Transmit Frequency 14.599 GHz"]
+[-2.985100746154785, 16.163103103637695, "Scatterometer Beam Width 500 km"]
+[-2.966312885284424, 16.155414581298828, "Scatterometer Swath Width 500 km"]
+[-2.9811313152313232, 16.157934188842773, "Scatterometer High Wind Swath Width 250 km"]
+[-2.98405122756958, 16.17303466796875, "Scatterometer Spatial Resolution 50 km"]
+[5.103491306304932, -4.009491443634033, "Satellite Launch Date 2028"]
+[5.058907508850098, -4.092750072479248, "Satellite End of Life Date 2035"]
+[2.053471088409424, -1.2644858360290527, "Satellite Measurement Domain Gravity and Magnetic Fields"]
+[2.7058603763580322, 22.376718521118164, "Instrument Type Imaging microwave radars"]
+[2.540652275085449, 13.86596965789795, "Large Uniform Light Source Calibration Parameter Signal to noise ratio, linearity, saturation and uniformity of radiometric response"]
+[2.572617530822754, 14.00022029876709, "Large Uniform Light Source Accuracy Absolute accuracy traceable to the NIST (National Institute of Standards and Technologies) or equivalent primary standards of radiance scale"]
+[-1.0004185438156128, 12.00246524810791, "Cold Ion Detector Collimator Half Angle 5.7\u00ba"]
+[-0.9752765893936157, 12.010046005249023, "Cold Ion Detector Electrostatic Energy Analyzer Passband DE/E = 0.14"]
+[-1.0353282690048218, 12.08353042602539, "Cold Ion Detector Microchannel Plate Detector Records the impact of the particles"]
+[-0.9611374139785767, 11.981987953186035, "Cold Ion Detector Length 120 mm"]
+[-0.9774795770645142, 11.98726749420166, "Cold Ion Detector Mass 180 g"]
+[-0.9869365692138672, 12.021014213562012, "Cold Ion Detector Alu Shielding Thickness 2 mm"]
+[-1.0000026226043701, 12.062253952026367, "Cold Ion Detector Minimum Energy Threshold Approximately 750 keV"]
+[2.752063751220703, 22.415267944335938, "Instrument Type Earth radiation budget radiometers, Space environment, Magnetic field, Other, Atmospheric chemistry, Communications, Data collection, Hyperspectral imagers, Gravity instruments"]
+[2.396211862564087, 22.097562789916992, "Instrument Measurement Category Atmospheric Temperature Fields"]
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+[-13.876322746276855, -2.2364144325256348, "X-ray Telescope Imaging Survey First ever true imaging survey of the sky in the hard band (2-8 keV)"]
+[-13.89272689819336, -2.2648510932922363, "X-ray Telescope Galaxy Cluster Detection Redshifts z > 1"]
+[2.668132781982422, 13.43300724029541, "Light-emission Mechanism Light Profile Varies"]
+[2.695195436477661, -1.761735200881958, "Satellite X-ray Detection Range Unknown"]
+[1.4793319702148438, -3.00866436958313, "Satellites Simultaneous Observations Conducted"]
+[5.0090227127075195, -4.340008735656738, "Satellite Observation Date 24 December 2018"]
+[1.8516596555709839, -2.028110980987549, "Satellite Path 135"]
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+[2.3018786907196045, -1.9071091413497925, "Satellite Beam Polarization HH+HV"]
+[-5.850457191467285, 16.04109764099121, "Synthetic Aperture Radar Frequency L-band"]
+[-5.8932414054870605, 16.022930145263672, "Synthetic Aperture Radar Observation Modes Spotlight, 3/6/10-m resolution stripmap, and ScanSAR"]
+[2.6453914642333984, 22.707799911499023, "Instrument Data Rate Unknown"]
+[2.56119966506958, 22.736392974853516, "Instrument Data Rate Unknown"]
+[2.5992166996002197, 22.72825813293457, "Instrument Data Rate Unknown"]
+[2.576478958129883, 22.74437141418457, "Instrument Data Rate Unknown"]
+[-1.83731210231781, 8.424318313598633, "Electronics Data Rate 4.0 Mbit/s"]
+[-4.320145130157471, 8.333815574645996, "Remote Terminal Unit Shutdown Cause Loss of onboard power regulation and spacecraft attitude stabilization"]
+[2.281763792037964, 11.941052436828613, "Mode Operation Neutralizer and main hollow-cathode heating PS-4 and PS-6 on, low level"]
+[2.337634801864624, 11.927010536193848, "Mode Operation Neutralizer hollow-cathode activation PS-6 on, high level"]
+[2.3790838718414307, 11.970237731933594, "Mode Operation Main hollow-cathode activation PS-4 on, high level"]
+[2.3503825664520264, 11.940323829650879, "Mode Operation Neutralizer discharge on PS-7 on"]
+[2.2981038093566895, 11.902122497558594, "Mode Operation Main hollow-cathode discharge and main discharge on PS-5 and PS-3 on"]
+[2.4130380153656006, 12.013461112976074, "Mode Operation All discharge on and beam on/off by command from orbit control system PS-3, PS-5 and PS-7 on and PS-1 on/off by command"]
+[2.397616147994995, 11.996970176696777, "Mode Operation Grid cleaning, short-circuit opening (function for failure) Not specified"]
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+[-2.5343565940856934, 8.245429039001465, "Fault Detection and Isolation System Performed under Ground Segment control Yes"]
+[-2.6044533252716064, 8.199535369873047, "Fault Detection and Isolation System FDIR considers all envisaged failures that may affect the safety of the RVX mission and all the SW failures of the RVX GNC Parameter Value"]
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+[-4.500395774841309, 7.750402450561523, "Telemetry and Command Assembly Microcontroller P89C51"]
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+[-8.127681732177734, 8.829489707946777, "Electric Power Subsystem Solar Cells Triple junction GaAs"]
+[-8.109607696533203, 8.796475410461426, "Electric Power Subsystem Battery Packs 2 Li-ion battery packs"]
+[-8.137602806091309, 8.825457572937012, "Electric Power Subsystem Power Output 20 W"]
+[-8.14084529876709, 8.825231552124023, "Electric Power Subsystem Output Voltages 5 V, 12 V, and 28 V"]
+[-1.0747032165527344, 7.718775749206543, "Device Backup Power Duration At least 24 hours"]
+[-6.714931488037109, 9.984086990356445, "Antenna Connection Robustness Robust"]
+[-1.1589678525924683, 4.453639030456543, "Ground Station Quantity 6"]
+[-1.1406594514846802, 4.469261169433594, "Ground Station Software CGA (Common Ground Architecture)"]
+[-1.9427266120910645, 6.95073127746582, "Software Operating System CentOS (Linux)"]
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+[6.757084369659424, 6.940054416656494, "Satellite Component Unknown Unknown"]
+[-1.42489492893219, 4.346357822418213, "Ground System Unknown Unknown"]
+[-0.9539178609848022, -10.003959655761719, "Satellite Constellation Number of Satellites 60"]
+[0.9517882466316223, 0.8712099194526672, "Earth Observation System URL http://www.blacksky.com/"]
+[-0.39401671290397644, -0.4175575375556946, "Satellite Deployment Platforms User High school, university level, professional researchers"]
+[-2.1210334300994873, 4.329092502593994, "Space Station Access Frequent"]
+[-2.170260429382324, 4.300330638885498, "Space Station Testbed Perfect testbed for those that are new to space and to those that have a long history in orbit"]
+[1.424384355545044, -1.8391309976577759, "Satellite Precision 1%"]
+[5.329360008239746, -4.440183162689209, "Satellite Launch Date December 21, 2016"]
+[2.665057420730591, -2.3682568073272705, "Satellite Launch Vehicle Chinese Long March 2D"]
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+[2.4376118183135986, -1.352432131767273, "Satellite Data Acquisition Regardless of light or weather conditions"]
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+[-3.255206346511841, 20.27349090576172, "Spectral Band SSD 20 m"]
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+[-3.291745185852051, 20.282665252685547, "Spectral Band SSD 10 m"]
+[-2.9721782207489014, 20.133228302001953, "Spectral Band Center Wavelength 865 nm"]
+[-3.271815061569214, 20.27904510498047, "Spectral Band SSD 20 m"]
+[-2.9390788078308105, 20.098413467407227, "Spectral Band Center Wavelength 940 nm"]
+[-3.2874085903167725, 20.285715103149414, "Spectral Band SSD 60 m"]
+[-2.9790220260620117, 20.112287521362305, "Spectral Band Center Wavelength 1375 nm"]
+[-3.2836122512817383, 20.283706665039062, "Spectral Band SSD 60 m"]
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+[-3.30846905708313, 20.292036056518555, "Spectral Band SSD 10 m"]
+[-2.978410243988037, 20.140918731689453, "Spectral Band Center Wavelength 560 nm"]
+[-3.2900023460388184, 20.284626007080078, "Spectral Band SSD 10 m"]
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+[-3.290388345718384, 20.283336639404297, "Spectral Band SSD 10 m"]
+[-2.9776692390441895, 20.13614273071289, "Spectral Band Center Wavelength 705 nm"]
+[-3.254842758178711, 20.26961326599121, "Spectral Band SSD 20 m"]
+[-2.99027943611145, 20.14621353149414, "Spectral Band Center Wavelength 740 nm"]
+[-3.2894647121429443, 20.290882110595703, "Spectral Band SSD 20 m"]
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+[-3.2516703605651855, 20.272817611694336, "Spectral Band SSD 20 m"]
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+[-3.3350698947906494, 20.296154022216797, "Spectral Band SSD 10 m"]
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+[-3.3121604919433594, 20.302364349365234, "Spectral Band SSD 20 m"]
+[-2.986111640930176, 20.140077590942383, "Spectral Band Center Wavelength 1610 nm"]
+[-3.237703800201416, 20.25595474243164, "Spectral Band SSD 20 m"]
+[-2.9920835494995117, 20.076786041259766, "Spectral Band Center Wavelength 2190 nm"]
+[-3.2945780754089355, 20.307863235473633, "Spectral Band SSD 20 m"]
+[2.432387113571167, 22.759933471679688, "Instrument Number of Channels 14"]
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+[2.9509284496307373, 22.46074676513672, "Instrument Manufacturer National Space Science Center of CAS"]
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+[-5.349547863006592, 2.75685453414917, "Telescope Image Blur Metrics FWHM (Full Width Half maximum), RMS (Root-Mean-of Squares)"]
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+[-1.0704054832458496, 7.738065242767334, "Device Detection Time Near-instantaneous"]
+[-3.791734457015991, 6.940942287445068, "Data Collection System Role Unknown"]
+[-13.877588272094727, -2.2418062686920166, "X-ray Telescope Discovery Large-scale bubbles in the halo of the Milky Way"]
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+[2.7429890632629395, 22.421939849853516, "Instrument Type Magnetic field"]
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+[2.724186897277832, 22.341238021850586, "Instrument Type Atmospheric temperature and humidity sounders"]
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+[16.95301628112793, 6.774901390075684, "Microsatellite Launch Time 20:30 UTC"]
+[-3.0161263942718506, 4.457164764404297, "Spacecraft Cargo Capacity 2625 kg"]
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+[7.289407730102539, 12.414922714233398, "Satellite Instrument Swath Width 24 km"]
+[7.280648708343506, 12.424126625061035, "Satellite Instrument S/C Body Pointing Capability \u00b145\u00ba in the roll and pitch axis"]
+[7.268056392669678, 12.385917663574219, "Satellite Instrument Optics Focal Length 2896 mm"]
+[7.291337966918945, 12.41220760345459, "Satellite Instrument Pupil Diameter 600 mm"]
+[7.290187835693359, 12.41747760772705, "Satellite Instrument Pan Pixels 12,000 pixels"]
+[7.269304275512695, 12.391423225402832, "Satellite Instrument MS Pixels 3,000 pixels"]
+[7.296681880950928, 12.41771411895752, "Satellite Instrument Integration Time 0.308 ms for PAN, 1.232 ms for MS"]
+[7.27022123336792, 12.382926940917969, "Satellite Instrument Processing Rate 10 Mpixel/s for PAN, 5 Mpixel/s for MS"]
+[7.278839111328125, 12.400588035583496, "Satellite Instrument Pixel Quantization 12 bit"]
+[7.2794060707092285, 12.404168128967285, "Satellite Instrument Data Compression Ratio 2.8 and 3.75 for PAN, 1.7 and 3.75 for MS"]
+[7.227627277374268, 12.349252700805664, "Satellite Instrument Instrument Mass 114 kg"]
+[7.2438201904296875, 12.358996391296387, "Satellite Instrument Power Consumption 161 W for imaging, 73 W for standby"]
+[1.6786384582519531, 6.956759929656982, "Communication Device Type Unknown"]
+[-1.4282704591751099, 4.350330829620361, "Ground System Status Unknown"]
+[2.961479425430298, -1.9860715866088867, "Satellite Mission Status Unknown"]
+[2.9240829944610596, -2.002983808517456, "Satellite Mission Status Unknown"]
+[-4.940959930419922, 9.767565727233887, "Receiver Frequency 37 GHz"]
+[6.253798007965088, 7.4875030517578125, "Satellite Component Size Scaled from the GMI RDA"]
+[6.297399997711182, 7.4424614906311035, "Satellite Component Size 1.8-m"]
+[-1.7596336603164673, 8.461181640625, "Electronics Prototype Built and tested by Ball"]
+[1.8577488660812378, -2.1454033851623535, "Satellite Orbit Modeled"]
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+[1.901483416557312, 10.7243070602417, "Imaging Device CCDs 4"]
+[1.9025845527648926, 10.71296501159668, "Imaging Device Pixels 4510 x 4510"]
+[1.8627766370773315, 10.813785552978516, "Imaging Device Mode Full frame mode"]
+[1.8590128421783447, 10.740479469299316, "Imaging Device Effective FoV 1037\u00ba x 1037\u00ba for the \u201cnormal\u201d cameras and 619\u00ba x 619\u00ba for each of the two \u201cfast\u201d cameras"]
+[1.8744453191757202, 10.74380874633789, "Imaging Device Purpose Star brightness measurements, fine guidance sensors, spectral band measurements"]
+[1.8946387767791748, 10.714628219604492, "Imaging Device Bandpass Filters Blue, Red"]
+[1.8948144912719727, 10.722651481628418, "Imaging Device Groups 4 groups of 6 cameras"]
+[1.8979535102844238, 10.726635932922363, "Imaging Device Group FoV All 6 cameras of each group have exactly the same FoV"]
+[1.930266261100769, 10.714966773986816, "Imaging Device Group Offset Angle 9.2\u00b0 from the PLM (Payload Module) +Z axis"]
+[-7.510256767272949, 5.939821243286133, "Camera Quantity 104"]
+[2.4676637649536133, 22.577239990234375, "Instrument Quantity 26 cameras and electronic units"]
+[5.083586692810059, -3.961254358291626, "Satellite Launch Year 2026"]
+[2.7854127883911133, -1.1349754333496094, "Satellite Purpose Find and study extrasolar planetary systems"]
+[4.675222873687744, -2.5871989727020264, "Satellite Mission Duration 5 years"]
+[4.629978179931641, -2.626269817352295, "Satellite Mission Duration 7 years"]
+[4.630082607269287, -2.615222454071045, "Satellite Mission Duration 7 years"]
+[4.665493965148926, -2.5883522033691406, "Satellite Mission Duration 7 years"]
+[4.678117275238037, -2.613147497177124, "Satellite Mission Duration 7 years"]
+[4.682135105133057, -2.5706992149353027, "Satellite Mission Duration 7 years"]
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+[7.30386209487915, 12.377252578735352, "Satellite Instrument Polarization 10.85 \u03bd, h"]
+[7.304267406463623, 12.384222030639648, "Satellite Instrument Bandwidth 500 MHz"]
+[7.2918500900268555, 12.413201332092285, "Satellite Instrument Sample Time 1.8 ms"]
+[7.280461311340332, 12.4042329788208, "Satellite Instrument Beam Width 1.06 \u00ba"]
+[7.253041744232178, 12.370490074157715, "Satellite Instrument 3 dB Footprint Size 38 x 23 km"]
+[7.294274806976318, 12.418656349182129, "Satellite Instrument Center Frequency 18\u03bd, 18h"]
+[7.302606582641602, 12.408944129943848, "Satellite Instrument Bandwidth 500 MHz"]
+[7.292690753936768, 12.408644676208496, "Satellite Instrument Sample Time 1.8 ms"]
+[7.28153657913208, 12.45770263671875, "Satellite Instrument Beam Width 0.66 \u00ba"]
+[7.251311302185059, 12.385191917419434, "Satellite Instrument 3 dB Footprint Size 23 x 15 km"]
+[7.261721611022949, 12.372946739196777, "Satellite Instrument Center Frequency 23\u03bd"]
+[7.285957336425781, 12.39354419708252, "Satellite Instrument Bandwidth 370 MHz"]
+[7.303402423858643, 12.396793365478516, "Satellite Instrument Sample Time 1.8 ms"]
+[7.285577774047852, 12.420112609863281, "Satellite Instrument Beam Width 0.58 \u00ba"]
+[7.22228479385376, 12.341033935546875, "Satellite Instrument 3 dB Footprint Size 21 x 13 km"]
+[7.202474594116211, 12.3282470703125, "Satellite Instrument Center Frequency 36.75 \u03bd, h"]
+[7.328297138214111, 12.396062850952148, "Satellite Instrument Bandwidth 500 MHz"]
+[7.209654808044434, 12.328359603881836, "Satellite Instrument Sample Time 1.8 ms"]
+[7.264366149902344, 12.438143730163574, "Satellite Instrument Beam Width 0.43 \u00ba"]
+[7.299741744995117, 12.434356689453125, "Satellite Instrument 3 dB Footprint Size 15 x 10 km"]
+[7.288367748260498, 12.412221908569336, "Satellite Instrument Center Frequency 37.3 \u03bd, h"]
+[7.317331790924072, 12.377190589904785, "Satellite Instrument Bandwidth <2500"]
+[7.309350490570068, 12.361115455627441, "Satellite Instrument Center Frequency 89 \u03bd, h"]
+[7.292119979858398, 12.409873008728027, "Satellite Instrument Bandwidth <6000"]
+[7.276498317718506, 12.414921760559082, "Satellite Instrument Beam Width 0.43 \u00ba"]
+[7.2368669509887695, 12.370635032653809, "Satellite Instrument 3 dB Footprint Size 15 x 10 km"]
+[-4.424516677856445, 15.955229759216309, "Radar Observing System Mission Start Date 29 October 2012"]
+[-4.4384589195251465, 15.906173706054688, "Radar Observing System URL https://www.d-copernicus.de/daten/satelliten/satelliten-details/news/rose-l-radar-observing-system-for-europe-l-band-sar/?tx_news_pi1%5Bcontroller%5D=News&tx_news_pi1%5Baction%5D=detail&cHash=a04a6343ad86edd934b7d33e53318699"]
+[2.711029291152954, -2.8017418384552, "Inter-Satellite Links Bit Error Rates Lower"]
+[2.701392650604248, -2.7292823791503906, "Inter-Satellite Links Latency Requirements Not compromised"]
+[-5.216008186340332, 7.5602641105651855, "Network Purpose Maximize coverage and throughput of each space platform"]
+[-0.95134437084198, -10.006900787353516, "Satellite Constellation Imagery Resolution 30 cm"]
+[-0.9104478359222412, -10.052380561828613, "Satellite Constellation Revisit Rate Over 15 times a day"]
+[-0.9482846856117249, -10.012541770935059, "Satellite Constellation Contract Value $35 million"]
+[-0.9464914798736572, -10.003816604614258, "Satellite Constellation Imagery Access Direct task and download 30 cm-class satellite imagery to its ground station"]
+[-0.9473378658294678, -10.002632141113281, "Satellite Constellation Orbit Types Sun-synchronous orbit and mid inclination orbit"]
+[-3.3426878452301025, 4.265892028808594, "Spacecraft Operational Lifetime More than 20 years"]
+[-0.4198836386203766, 14.521245002746582, "Imaging Instrument Focal Planes Two large visible near-infrared and shortwave infrared focal planes"]
+[-0.4111473858356476, 14.47162914276123, "Imaging Instrument Detectors 12 detectors"]
+[-0.40906888246536255, 14.515411376953125, "Imaging Instrument Pixels 450,000 pixels"]
+[-0.4229481518268585, 14.524698257446289, "Imaging Instrument Optomechanical Stability Extremely high"]
+[-0.4111174941062927, 14.521814346313477, "Imaging Instrument Material Silicon carbide ceramic"]
+[-1.9403631687164307, 8.446714401245117, "Monolithic Integrated Circuit Total Ionizing Dose Measurement Unknown"]
+[-1.0400930643081665, 7.6934990882873535, "Device Total Ionizing Dose Measurement Unknown"]
+[-1.0842658281326294, 7.654702663421631, "Devices Total Ionizing Dose Measurement Unknown"]
+[-1.8398419618606567, 8.787277221679688, "Controller Technology 0.35 micron, 3.3 V CMOS"]
+[-3.317225456237793, 8.484643936157227, "Memory Device Technology Unknown"]
+[-3.329134464263916, 8.503310203552246, "Memory Device Technology Unknown"]
+[-1.0556749105453491, 7.7354583740234375, "Device Technology 2 micron CMOS (Orbit) process"]
+[-4.518938064575195, 12.116429328918457, "Magnetometer Boom Length 8 m"]
+[-0.8227340579032898, 11.555804252624512, "Detectors Quantity 6"]
+[-6.7136945724487305, 9.980009078979492, "Antenna Mounting Location Upper right edge of the panel"]
+[4.655088901519775, -2.6462206840515137, "Satellite Operation Duration 15 years"]
+[1.882753849029541, -1.318806767463684, "Satellite Measurement Type Magnetic field intensity"]
+[2.2903077602386475, -1.4130069017410278, "Satellite Main Instruments CSC and Overhauser magnetometers"]
+[2.5006511211395264, -1.5853602886199951, "Satellite Star Camera Status Disabled"]
+[2.7730789184570312, -1.9940742254257202, "Satellite Telemetry Receiver Status Problematic"]
+[0.09775137156248093, 7.214751243591309, "Experiment Purpose Comparing the time at two or more laser-ranging sites"]
+[0.06995464116334915, 7.121375560760498, "Experiment Precision Better than 100 ps"]
+[0.12493698298931122, 7.172209739685059, "Experiment Accuracy 1.5 ns"]
+[-0.7299102544784546, 12.347834587097168, "Space Environment Monitor Device Type Monitor"]
+[1.725102186203003, -1.5585272312164307, "Satellite Sky Observation Swath 24-by-96-degree"]
+[-3.085793972015381, 2.0127596855163574, "Space Mission Distance Scale Each kiloparsec equal to 3,260 light-years"]
+[1.073042631149292, -1.5420076847076416, "Satellite Sky Survey 20000 light-years from the Sun"]
+[-5.007587909698486, 2.8630337715148926, "Space Telescope Operation Period 2006 to 2013"]
+[-3.107090473175049, 1.9878448247909546, "Space Missions Sky Survey Period 2009 to 2018"]
+[-0.6207686066627502, 8.636289596557617, "Cryocooler Detector Temperature Below 120 K"]
+[1.5628114938735962, 22.177820205688477, "Instrument Size 10 x 10 x 15 mm"]
+[1.6753789186477661, 23.169160842895508, "Instrument Power Subsystem Requirement 10-15 W"]
+[2.257986307144165, 22.338275909423828, "Instrument FOV 100 mrad (6\u00ba)"]
+[3.613614559173584, 22.251604080200195, "Instrument Component FOV Size 100 km"]
+[1.8306853771209717, 10.712515830993652, "Imaging Interval 2.7 s"]
+[-8.461079597473145, 13.736889839172363, "Variable Measurement Methods 4 ways"]
+[-8.448662757873535, 13.753118515014648, "Variable Measurement Methods 3 ways"]
+[-8.500921249389648, 13.708158493041992, "Variable Measurement Methods 2 ways"]
+[-8.498806953430176, 13.705129623413086, "Variable Measurement Methods 3 ways"]
+[1.7463420629501343, -0.36174535751342773, "Satellite Imaging Payload Imaging Capacity Doubles DigitalGlobe's capacity to capture multispectral and 30 cm imagery"]
+[1.7819801568984985, -0.3001583218574524, "Satellite Imaging Payload Imaging Capacity Triples to quadruples the company's capacity to image high-demand areas"]
+[-0.9100134968757629, -10.045119285583496, "Satellite Constellation Imaging Frequency Every 20 to 30 minutes"]
+[-3.073235511779785, 7.663122177124023, "Processing Unit Number of In/Out Ports About 130"]
+[-3.0874404907226562, 7.705409049987793, "Processing Unit Clock Frequency 20 MHz"]
+[-3.3085110187530518, 8.498594284057617, "Memory Capacity 32 Mbit"]
+[-2.036052703857422, 7.744834899902344, "Circuit Board Size 115 mm x 190 mm"]
+[2.07718563079834, 22.53417205810547, "Instrument Signal Photon Density Greater than 4 photons/m"]
+[1.9857689142227173, 22.56611442565918, "Instrument Signal Photon Density 3.4 photons per 70 cm"]
+[1.93498957157135, 22.622434616088867, "Instrument Signal Photon Density 3.9 photons per 70 cm"]
+[2.0068657398223877, 22.53614044189453, "Instrument Signal Photon Density 3.1 photons per 70 cm"]
+[1.91758394241333, 22.558340072631836, "Instrument Signal Photon Density 3.4 photons per 70 cm"]
+[0.8452057838439941, -1.127598762512207, "Satellite Bathymetry Measurement Depth Up to 25 meters"]
+[2.7668933868408203, -2.1829795837402344, "Satellite Surface Wave Frequency Unknown"]
+[2.7700376510620117, -2.0016510486602783, "Satellite Surface Wave Structure Unknown"]
+[1.232454776763916, 22.132240295410156, "Pushbroom instrument Spectral Range 0.4-2.4 \u00b5m (VNIR + SWIR)"]
+[1.1653627157211304, 22.089797973632812, "Pushbroom instrument Spatial Sampling Distance 10 m (VNIR), 20 m (SWIR), 60 m (3 bands)"]
+[1.1994609832763672, 22.11173439025879, "Pushbroom instrument Swath Width 290 km"]
+[1.1672629117965698, 22.089052200317383, "Pushbroom instrument Detector Technologies Monolithic Si (VNIR); hybrid HgCdTe CMOS (SWIR)"]
+[1.1905665397644043, 22.10318946838379, "Pushbroom instrument Detector Cooling Cooling of SWIR detector to < 210 K"]
+[1.1559284925460815, 22.086301803588867, "Pushbroom instrument Data Quantization 12 bit"]
+[1.1736910343170166, 22.066064834594727, "Pushbroom instrument Instrument Mass ~290 kg"]
+[1.1551055908203125, 22.08841323852539, "Pushbroom instrument Instrument Power < 266 W"]
+[1.1550424098968506, 22.08647346496582, "Pushbroom instrument Data Rate 450 Mbit/s after compression"]
+[5.149535655975342, -4.562526702880859, "Satellite Presentation Date Sept. 29 to Oct. 3, 2008"]
+[5.18594217300415, -4.495847702026367, "Satellite Conference Date June 24-28, 2002"]
+[5.098361968994141, -4.560438632965088, "Satellite Conference Date May 16-18, 2006"]
+[1.9021514654159546, 8.60500717163086, "Subsystem Alignment 100 \u00b5rad"]
+[1.8569080829620361, 8.639361381530762, "Subsystem Pointing Error Residual errors and offsets in the beam steering control loop and optics"]
+[1.9013046026229858, 8.611490249633789, "Subsystem Mirror Actuator Requirement Very linear and predictable mirror actuator, or an internal sensor within the actuator that yields an accurate representation of the actual mirror angle"]
+[-1.9203897714614868, 8.125353813171387, "System EW (3\u03c3) \u00b121 \u00b5rad"]
+[-0.1907626986503601, 13.608196258544922, "Error Measurement 0.47, 0.64, 0.865, and 1.61 \u00b5m channels \u00b116 \u00b5rad"]
+[-0.20919251441955566, 13.59670352935791, "Error Measurement 1.378, 2.25, 3.9, 6.185, 6.95, 7.34, 8.5, 9.61, 10.35, 11.2, 12.3, and 13.3 \u00b5m channels \u00b121 \u00b5rad"]
+[-0.18328092992305756, 13.609905242919922, "Error Measurement Any two pixels in a Frame \u00b121 \u00b5rad"]
+[-0.18057367205619812, 13.606218338012695, "Error Measurement  \u00b1 5.2 \u00b5rad"]
+[-0.1540183126926422, 13.631851196289062, "Error Measurement 2 km to 2 km, 1 km, 0.5 km (wavelength/detector dependent) \u00b1 6.3 \u00b5rad"]
+[-0.1607833206653595, 13.666778564453125, "Error Measurement 1 km to 1 km, 0.5 km (wavelength/detector dependent) \u00b1 5.2 \u00b5rad"]
+[0.725623369216919, -4.14552116394043, "Satellite Launch Mass ~2060 kg"]
+[2.0878050327301025, -0.4964122772216797, "Satellite Power ~1.1 kW"]
+[5.136163711547852, -2.292431354522705, "Satellite Nominal Design Life 7.7 years"]
+[-3.550419807434082, 4.373329162597656, "Spacecraft Launch Date Nov. 10, 2014"]
+[-3.111112117767334, 4.331828594207764, "Spacecraft Design Baseline design"]
+[-3.1713593006134033, 4.3163886070251465, "Spacecraft Rocket United Launch Alliance Atlas V rocket"]
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+[2.6231067180633545, 21.98522186279297, "Instrument Function Samples the energy distribution"]
+[2.6232664585113525, 22.326854705810547, "Instrument Data Output Raw data to obtain the neutral wind vector, the neutral temperature and the O and N2 densities"]
+[-3.0707905292510986, 4.289594650268555, "Spacecraft Nominal Generation Voltage 160 V"]
+[-3.0564281940460205, 4.361595630645752, "Spacecraft Transmission Voltage 120 V"]
+[-3.035857677459717, 4.321810245513916, "Spacecraft Required Voltage 300 - 400 V"]
+[-2.578023672103882, 4.24340295791626, "Space Environment Maximum Voltage 200 V"]
+[-2.9576117992401123, 4.427594184875488, "Spacecraft Voltage Limit 160 V"]
+[4.4127349853515625, -2.5378665924072266, "Satellite Mission Extension 2025 and beyond"]
+[-4.567180156707764, -3.0928127765655518, "Exoplanet Host Star Consumption Time Less than 1 million years"]
+[2.695451021194458, -1.6782679557800293, "Satellite Discoveries Three newly-discovered planets"]
+[2.049999713897705, -2.736457586288452, "Satellite Number of Confirmed Exoplanets 175"]
+[-0.3925264775753021, 14.537118911743164, "Imaging Instrument Modes Mode 3 and Mode 4"]
+[-0.41634541749954224, 14.519037246704102, "Imaging Instrument Mode 3 Imaging Frequency 1 FD image, 3 CONUS and 30 Mesoscale images, every 15 minutes"]
+[-0.4087235927581787, 14.520822525024414, "Imaging Instrument Mode 4 Imaging Frequency 30 Mesoscale images every 15 minutes as well as a Full Disk every 5 minutes"]
+[-0.4248916208744049, 14.53953742980957, "Imaging Instrument Full-disk Earth observation Frequency Within 15 minutes"]
+[-0.4319736659526825, 14.53475284576416, "Imaging Instrument CONUS Observation Frequency Every 5 minutes (goal of 1 minute)"]
+[-0.40223830938339233, 14.516448974609375, "Imaging Instrument Minimum Imagery Size 1000 km x 1000 km (nadir)"]
+[-1.5043413639068604, 16.901765823364258, "Altimeter Development Time 25 Years"]
+[2.2813973426818848, -1.130157709121704, "Satellite Project Radar Altimeter Information Not Provided"]
+[4.861551761627197, -2.402204990386963, "Satellite Project Development Time 25 Years"]
+[11.158062934875488, 5.228682994842529, "CubeSat Mass 1.2 kg"]
+[11.25638484954834, 5.512839317321777, "CubeSat Affiliation University of W\u00fcrzburg, Germany"]
+[11.267631530761719, 5.485598087310791, "CubeSat Affiliation Planet Labs Inc. (formerly Cosmogia Inc.), San Francisco, CA, USA"]
+[11.304347038269043, 5.522763729095459, "CubeSat Affiliation Argentina (sponsored by the Argentinian Ministry of Science, Technology and Productive Innovation)"]
+[-1.9760664701461792, 7.844668865203857, "Avionics Unit Affiliation Hartron-Arkos, Ukraine"]
+[-3.473738431930542, 6.964108943939209, "Data Structure Bit Size 64-bit"]
+[-2.4547252655029297, 11.07420825958252, "On-board Image Processing System Data Bandwidth 6 Mbit/s"]
+[1.8766230344772339, 10.717569351196289, "Imaging Device Frame Rate 500 frames/s"]
+[1.9315170049667358, 10.688735008239746, "Imaging Device Data Size 14 bit/pixel"]
+[1.8965617418289185, 10.71516227722168, "Imaging Device Raw Video Data Bandwidth 12.5 Gbit/s"]
+[-4.486049652099609, 15.913034439086914, "Radar Frequency 1257.5 MHz"]
+[-4.507381916046143, 15.900657653808594, "Radar Frequency Adjustment \u00b1 21 MHz"]
+[-4.470249176025391, 15.901142120361328, "Radar ScanSAR Mode Spatial Resolution 60 m"]
+[-4.494300842285156, 15.921807289123535, "Radar ScanSAR Mode Swath 490 km"]
+[-4.501084327697754, 15.88293743133545, "Radar Stripmap Mode Spatial Resolution 10 m, 6 m, and 3 m"]
+[-4.503402233123779, 15.922775268554688, "Radar Stripmap Mode Swath 70 km, 70 km, and 50 km"]
+[-4.483065128326416, 15.911291122436523, "Radar Spotlight Mode Spatial Resolution 1 m x 3 m"]
+[-4.499058246612549, 15.926078796386719, "Radar Spotlight Mode Swath 25 km x 25 km"]
+[0.6919940114021301, -2.3196542263031006, "Satellite Inclination 97.9\u00b0"]
+[0.7584269642829895, -1.1463836431503296, "Satellite Altitude 628 km"]
+[4.039185523986816, -2.8305797576904297, "Satellite Period 97 minutes"]
+[4.237530708312988, -2.5227365493774414, "Satellite Revisit Time 14 days"]
+[-0.5416678190231323, 15.584977149963379, "Spectrographic Imager Parameter Species Wavelength O + 834 \u00c5"]
+[-0.4080500304698944, 15.649303436279297, "Spectrographic Imager Parameter Species Wavelength O 911 \u00c5, 1304 \u00c5, 1356 \u00c5"]
+[-0.5714086890220642, 15.542675018310547, "Spectrographic Imager Parameter Species Wavelength O 989 \u00c5, 1304 \u00c5, 1356 \u00c5, 1641 \u00c5"]
+[-0.5545631647109985, 15.54171085357666, "Spectrographic Imager Parameter Species Wavelength N 2 1085 \u00c5 (N+), N 2 LBH bands"]
+[-0.47078704833984375, 15.575906753540039, "Spectrographic Imager Parameter Species Wavelength O 1356 \u00c5"]
+[-0.22714999318122864, 6.849478244781494, "Test Specimen Composition GaAs/InGaP/Ge multi-junction solar cells"]
+[-1.5008935928344727, 13.426467895507812, "Solar Array Connection Connected via the switches (MOSFET, for biasing) to the negative end of the high-voltage solar array"]
+[-1.5060374736785889, 13.429789543151855, "Solar Array Test Discharge test will be performed on each TJ array when the biasing switch is activated"]
+[-8.146522521972656, 8.827126502990723, "Electrical Power Subsystem Output Voltage 3.3 V and 5.0 V"]
+[-8.137670516967773, 8.828023910522461, "Electrical Power Subsystem Stored Energy 38 Wh"]
+[-3.091733694076538, 2.4083147048950195, "Mission Computer Function Stores mission-specific commands"]
+[-5.687158584594727, 9.214218139648438, "UHF Radio System Function Primary RF communications method"]
+[-4.2924370765686035, 0.21877487003803253, "GNSS Receiver Constellations GPS and GALILEO"]
+[-5.555413722991943, 9.368419647216797, "Radio Frequencies Data Download Rate 60 Mbit/s"]
+[-5.530775547027588, 9.394309043884277, "Radio Frequencies Uplink Rate 20 kbit/s"]
+[-5.6455769538879395, 9.362735748291016, "Radio Frequencies Downlink Rate 384 kbit/s"]
+[-5.358621597290039, 2.7844839096069336, "Telescope Use Photographing distant objects of the universe"]
+[-2.1561367511749268, 2.9057936668395996, "Observatory Discovery Date January 13, 2020"]
+[-2.1557703018188477, 2.9118030071258545, "Observatory Lead Scientist Max Planck Institute for Extraterrestrial Physics"]
+[7.309172630310059, 12.453933715820312, "Satellite Instrument Purpose Monitor ocean salinity features"]
+[7.291288375854492, 12.426214218139648, "Satellite Instrument Data Quality Impressive"]
+[-0.5655272603034973, 4.973427772521973, "Region Salinity High"]
+[-0.5217592716217041, 4.933387756347656, "Region Salinity Low"]
+[-0.47163158655166626, 5.112147331237793, "River Outflow Associated with low-salinity water"]
+[2.089226245880127, -1.6073321104049683, "Satellite Dual-receive aperture balance Some RADARSAT-2 modes (including Multi-Look Fine, Ultra-Fine and Spotlight) use dual receive apertures to double the effective pulse repetition frequency without needing to sacrifice swath width"]
+[1.0879333019256592, -2.1516361236572266, "Satellite Phase imbalances Can arise due to differences in component temperatures between wings, among other factors"]
+[-7.557858943939209, 5.894298553466797, "Camera Tracking Aid Usage Take images of stars"]
+[8.491719245910645, 15.222147941589355, "Camera Mount Usage Aid in taking astronaut photos"]
+[-1.1973187923431396, 3.1504156589508057, "Cosmic Object X-ray Luminosity About a million times brighter than the total light output of the Sun"]
+[-1.2080700397491455, 3.1442134380340576, "Cosmic Object Distance from Earth About 20,000 light-years"]
+[-1.2215288877487183, 3.148069143295288, "Cosmic Object Brightness Appears to be about 1,000 times dimmer than the minimum threshold to be considered a ULX"]
+[-1.238383412361145, 3.1567912101745605, "Cosmic Object X-ray Emission Confined within two cones of gas extending outward from opposite sides of the central object"]
+[-3.745380163192749, 6.9250054359436035, "Data Collection Data Processing NASA-funded scientists"]
+[-3.868068218231201, 7.958429336547852, "Data Storage Location National Snow and Ice Data Center"]
+[-0.9658925533294678, -9.986674308776855, "Satellite Constellation Number of Spacecraft 4"]
+[-0.9927483201026917, -10.051312446594238, "Satellite Constellation Frequency 121.5 MHz and 406 MHz"]
+[4.28097677230835, -2.927415609359741, "Satellite Configuration Time Delays Minutes to hours"]
+[-0.8148804306983948, 0.13631851971149445, "Satellite System Altitude < 1000 km"]
+[-1.3943220376968384, 4.351672172546387, "Ground System Component Function Status reporting, monitoring, configuration and asset management"]
+[-2.8212273120880127, 7.205183029174805, "Configuration Management System Function Manage the configuration of software builds, licenses, and database schema"]
+[-2.804448127746582, 7.11033821105957, "Configuration Management System Function Distribute software and database updates throughout the GS"]
+[-2.743367910385132, 7.099418640136719, "Configuration Management System Function Generate anomaly trouble tickets and support the prioritization, tracking, and resolution of anomalies"]
+[1.6813480854034424, 21.965660095214844, "Instrument Swath Width 17 m"]
+[2.019744634628296, 22.322233200073242, "Instrument Accuracy of Ice-Sheet Elevation Changes Measurement 4 mm per year"]
+[2.0900027751922607, 22.37660789489746, "Instrument Accuracy of Land Ice Surface Elevation Changes Measurement 0.25 m per year"]
+[2.0127322673797607, 22.27352523803711, "Instrument Accuracy of Land Ice Surface Elevation Changes Measurement 0.4 m/year"]
+[2.0213942527770996, 22.279090881347656, "Instrument Resolution of Winter and Summer Ice-Sheet Elevation Change 0.1 m"]
+[0.5906783938407898, -1.4584989547729492, "Satellite Orbit Altitude 496 km"]
+[0.7273297905921936, -2.1854419708251953, "Satellite Orbital Inclination 92\u00b0"]
+[4.108480453491211, -2.519280433654785, "Satellite Repeat Cycle 91 days"]
+[-5.0255632400512695, 2.883974552154541, "Space Telescope Deployment Sequence Launch configuration, solar array deployment, telescope deployment, in-orbit collimation"]
+[-1.5695550441741943, 12.85248851776123, "Solar Coronagraph Design and Development J.-Y. Plesseria, P. Levacher, W. Curdt, S. Vives, C. Guillon, A. Mazzoli, F. Rouesnel, A. Paschalis, N. Kranitis, A. Poulakidas, B. Fiethe, S. Shestov, S. Gunar, G. Capobianco, P. Lamy, P. Rochus, K. Tsinganos, S. Kuzin, P. Heinzel, S. Fineschi"]
+[0.7033424377441406, -1.1443299055099487, "Satellite Lowest Altitude 167.4 km"]
+[4.779439449310303, -3.272063732147217, "Satellite Mission Duration 23 December 2017 to 1 October 2019"]
+[0.5375964045524597, -1.4810752868652344, "Satellite Orbital Altitudes Seven different orbital altitudes"]
+[2.288776397705078, -2.058764934539795, "Satellite Engine Ion engine"]
+[2.4417576789855957, -2.145599365234375, "Satellite Engine Gas-jet thrusters"]
+[-0.9203841090202332, 9.86219310760498, "Rocket Booster Reuse Count Three times"]
+[-0.9653566479682922, 9.823094367980957, "Rocket First Stage Landing Location \"Just Read the Instructions\" droneship, Pacific Ocean"]
+[-0.5505361557006836, 1.1739294528961182, "Satellite Orbit Altitude 575 km"]
+[-0.5322242379188538, 1.23898184299469, "Satellite Orbit Inclination ~98\u00ba"]
+[-0.5336006879806519, 1.2342153787612915, "Satellite Orbit LTDN 10:30 hours"]
+[5.173437118530273, -4.352658271789551, "Satellite Global Data Release Date 28 May 2019"]
+[4.851096153259277, -4.486283302307129, "Satellite Image of the Day Date 29 January 2019"]
+[4.95290994644165, -4.456794738769531, "Satellite Image of the Day Date 12 December 2018"]
+[-1.7612446546554565, 5.302542686462402, "Mission Management Element Functional Areas Space-ground communications, Command generation, Telemetry (TT&C) processing, Mission operations, Product monitoring"]
+[1.5899407863616943, 6.999430179595947, "Communication Hardware Function Front-end for transmission and receipt of the RF signals"]
+[1.522609829902649, 7.008847236633301, "Communication Hardware Function Turns RF signals into information to be sent throughout the system"]
+[2.5812690258026123, -3.9241974353790283, "Satellite URL http://m.esa.int/Our_Activities/Observing_the_Earth/Copernicus/Sentinel-1/Satellites_shed_new_light_on_earthquakes"]
+[0.9467610716819763, 0.8763708472251892, "Earth Observation Program URL http://m.esa.int/Our_Activities/Observing_the_Earth/Copernicus"]
+[-1.3589743375778198, 6.175637245178223, "Organization URL https://www.jpl.nasa.gov/news/news.php?feature=6938&utm_source=iContact&"]
+[0.5254966020584106, -1.4450937509536743, "Satellite Orbit Altitude 685.1 km"]
+[0.7242187261581421, -2.2473623752593994, "Satellite Orbit Inclination 98.13\u00ba"]
+[4.12748384475708, -2.8467891216278076, "Satellite Orbit Period 98.5 minutes"]
+[3.8856096267700195, -3.1650426387786865, "Satellite LTAN 13:30 hours"]
+[3.1730709075927734, -1.9084794521331787, "Satellite Mission Status Fully operational in its 7th year of service"]
+[2.0783026218414307, -1.1703938245773315, "Satellite Imaging Capability High-resolution images of Earth's land cover"]
+[4.287088871002197, -2.4956347942352295, "Satellite Revisit Time Within three days"]
+[16.840126037597656, 6.871457099914551, "Microsatellite Observation Area Altitudes of 20 to 100 km over thunderstorms"]
+[4.948853015899658, -4.476477146148682, "Satellite Image Acquisition Date June 23, 2013"]
+[5.115980625152588, -4.503225326538086, "Satellite First Signal Reception Date Dec. 18, 2012"]
+[3.194694995880127, -0.29785987734794617, "Satellite Sensor Complement EOS-C (Earth Observation Satellite - Camera)"]
+[0.8575820326805115, 0.958892285823822, "International Terrestrial Reference Frame Release Date 18 July 2016"]
+[-0.9486464858055115, -10.008034706115723, "Satellite Constellation Geodetic Parameter Estimation Consistent"]
+[-3.6347343921661377, 4.432401657104492, "Spacecraft Launch Date October 1, 2010"]
+[-3.1236114501953125, 4.262280464172363, "Spacecraft Perigee 200 km"]
+[-3.1347641944885254, 4.240488052368164, "Spacecraft Apogee About 380,000 km"]
+[-3.017284393310547, 4.20620059967041, "Spacecraft Lunar Orbit 100 km above the moon's surface"]
+[-3.3416054248809814, 4.2630615234375, "Spacecraft Orbital Period Once every 118 minutes"]
+[-1.5589832067489624, 12.830435752868652, "Coronagraph Mission Date July 16-23, 2006"]
+[-1.5576452016830444, 12.826650619506836, "Coronagraph Mission Date July 16-23, 2006"]
+[-1.569867491722107, 12.80270767211914, "Coronagraph Mission Date July 16-23, 2006"]
+[-5.2132158279418945, 7.791904926300049, "Communication System Download Rate 100 Mbit/s"]
+[1.3710741996765137, 10.554219245910645, "Imaging System Wide Area Image Dimensions 100 km x 34 km"]
+[1.3442165851593018, 10.552787780761719, "Imaging System Stereo Image Dimensions 100 km x 20 km"]
+[-0.0818311795592308, 9.417394638061523, "Geo-location and Pointing System Accuracy Less than 1km"]
+[-3.837449550628662, 7.9390740394592285, "Data Storage Frame Capacity Up to 45 frames"]
+[-1.8606542348861694, 12.179295539855957, "Infrared Camera Spectral Range 0.8-1.7 \u00b5m"]
+[-1.8562676906585693, 12.166128158569336, "Infrared Camera Resolution 20 m"]
+[-0.8512738943099976, 3.1553893089294434, "Astronomical System Number of Stars 6"]
+[0.9516001343727112, -4.265334606170654, "Satellite Payload Capability About 360 kg"]
+[2.0932955741882324, -0.5188035368919373, "Satellite Power 3 kW"]
+[4.902651309967041, -2.432530641555786, "Satellite Lifetime 15 years"]
+[3.7250685691833496, 17.696144104003906, "Payload Manufacturer MDA Corporation (Canada)"]
+[3.684868335723877, 17.653345108032227, "Payload Manufacturer Tesat Spacecom (Backnang, Germany)"]
+[-3.182359218597412, 7.574706554412842, "Data Processing Unit Data Transmission Cadence Every 25 s"]
+[-3.156663656234741, 7.6163530349731445, "Data Processing Unit Pointing/Attitude Error Signal Cadence 2.5 s"]
+[-1.7144454717636108, 8.427943229675293, "Electronics Unit Quantity of N-DPUs 14"]
+[-1.6831268072128296, 8.420716285705566, "Electronics Unit Quantity of F-DPUs 2"]
+[-2.4430906772613525, 13.294507026672363, "Hyperspectral Camera Mass 2 kg"]
+[-2.438093662261963, 13.288265228271484, "Hyperspectral Camera Size 68 mm x 76 mm x 141 mm"]
+[-2.437506675720215, 13.304945945739746, "Hyperspectral Camera Power Consumption 1.5 W"]
+[-2.4503984451293945, 13.298957824707031, "Hyperspectral Camera Pointing Range > 5\u00ba /s"]
+[-2.440117120742798, 13.299504280090332, "Hyperspectral Camera Pointing Accuracy < 300 \u00b5rad (3\u03c3)"]
+[-2.44661808013916, 13.29526138305664, "Hyperspectral Camera Actuator Coreless DC motor"]
+[-2.440173387527466, 13.303133964538574, "Hyperspectral Camera Feedback Sensor 2D- PSD"]
+[-2.4564177989959717, 13.298641204833984, "Hyperspectral Camera Laser Diode 5mW laser diode (630 nm)"]
+[-2.4531021118164062, 13.291547775268555, "Hyperspectral Camera A/D Converter 14 bit"]
+[-2.437420129776001, 13.286552429199219, "Hyperspectral Camera Sensitivity 350 \u00b5rad/mV"]
+[-2.4511497020721436, 13.29410171508789, "Hyperspectral Camera Controller Microcomputer: 32bit RISC (SH2)"]
+[-0.7211492657661438, 3.2499709129333496, "Star Tracker Assembly Function Determines the orientation of the satellite by tracking it relative to the position of the stars"]
+[-5.476123809814453, 3.173769474029541, "Star Camera Assembly Quantity Three temperature controlled CCD star cameras"]
+[-1.2312041521072388, 7.113226890563965, "Center of Mass Trim Assembly Quantity Six (two per axis) MTMs (Mass Trim Mechanisms)"]
+[-3.0950911045074463, 2.4285569190979004, "Mission Definition Review Date July 2012"]
+[-0.6023974418640137, 9.009101867675781, "Coordinate System Definition Position of its alignment cube"]
+[0.2319856584072113, 13.788520812988281, "Calibration Reference Truth Data Position measurements by the laser tracker"]
+[0.23693014681339264, 13.791961669921875, "Calibration Reference Grid Positions Constructed to cover the field of view of FLLS"]
+[0.2272581309080124, 13.779735565185547, "Calibration Reference Translation Done using a set of high-accuracy translation stages"]
+[0.21583294868469238, 13.76962661743164, "Calibration Reference Mapping From the detector output at a given CCRR position to the corresponding position measurement from the laser tracker"]
+[2.4155263900756836, 22.74970054626465, "Instrument Lens Count 6"]
+[2.385725259780884, 22.733793258666992, "Instrument Spectrum Bands 5"]
+[2.103365182876587, 13.567543983459473, "Lens Wavelength 0.38 \u00b5m"]
+[2.1177456378936768, 13.574935913085938, "Lens Wavelength 0.87 \u00b5m and 0.67 \u00b5m @ 0\u00ba"]
+[2.134803295135498, 13.583967208862305, "Lens Wavelength 0.67 \u00b5m @ 60\u00ba&120\u00ba"]
+[2.129943370819092, 13.576455116271973, "Lens Wavelength 1.375 \u00b5m and 1.64 \u00b5m"]
+[2.106602668762207, 13.5686674118042, "Lens Wavelength 1.64 \u00b5m @ 60\u00ba"]
+[2.126636505126953, 13.57563304901123, "Lens Wavelength 1.64 \u00b5m @ 120\u00ba"]
+[3.1398425102233887, -2.2825284004211426, "Optical Satellite Manufacturer Airbus DS"]
+[5.126186847686768, -4.425829887390137, "Optical Satellite Launch Date Early March 2017"]
+[4.828279495239258, -4.331435203552246, "Optical Satellite Arrival Date at Kourou spaceport January 12, 2017"]
+[4.975528717041016, -4.316757678985596, "Optical Satellite Integration Completion Date July 29, 2021"]
+[-13.516106605529785, -2.035973072052002, "X-ray Observatory Data Wavelength 10 to 35 keV"]
+[-13.475334167480469, -2.036885976791382, "X-ray Observatory Science Operations Start Date August 1, 2012"]
+[-13.448692321777344, -1.9635072946548462, "X-ray Observatory Slew Rate Enhancement Factor of two"]
+[-13.484885215759277, -2.0256710052490234, "X-ray Observatory Phase E Duration Three months"]
+[-13.475541114807129, -2.0209856033325195, "X-ray Observatory Attitude Control Parameters Unknown"]
+[-2.2173800468444824, 5.919811725616455, "Aircraft Instruments Elevation-mapping lasers, ice-penetrating radars, optical and infrared cameras, gravimeters, magnetometers"]
+[2.8107104301452637, 22.389509201049805, "Instrument Team Lead Michael Studinger"]
+[2.842200517654419, 22.405168533325195, "Instrument Project Scientist Michael Studinger"]
+[0.6588106751441956, 9.321732521057129, "Attitude Determination and Control Subsystem Components 1 GPS receiver, 2 IMUs, 1 dual-FOV sun sensor, 5 coarse sun sensors, 3 magnetic torquers"]
+[-3.3403663635253906, 7.217418193817139, "Data Handling System Microcontroller Unit 100 MHz 8051 MCU"]
+[-3.3498377799987793, 7.22547721862793, "Data Handling System SD Card Capacity 2 GB"]
+[-8.13605785369873, 8.82719612121582, "Electrical Power Subsystem Solar Panels 5 GaAs panels"]
+[-8.160490989685059, 8.806001663208008, "Electrical Power Subsystem Peak Power 2.4 W"]
+[-8.131796836853027, 8.821206092834473, "Electrical Power Subsystem Battery Type Li-ion"]
+[-8.14601993560791, 8.82304573059082, "Electrical Power Subsystem Battery Capacity 2600 mAh"]
+[-5.2150983810424805, 7.7878336906433105, "Communication System Downlink Data Rate 9.6 kbit/s"]
+[-5.239477634429932, 7.777346134185791, "Communication System Uplink Data Rate 1.2 kbit/s"]
+[-5.289487838745117, 7.837921142578125, "Communication System Protocol AX.25 packet protocol"]
+[-1.3206629753112793, 3.213430404663086, "Astrophysical Phenomenon Cause Object with strong gravity accreting gas from a companion star"]
+[-1.574361801147461, 3.1853740215301514, "Astrophysical Parameter Definition Luminosity upper limit at which the radiation pressure balances the gravitational force"]
+[-1.2428836822509766, 3.1348888874053955, "Astrophysical Objects Model \"Accretion columns\" model where the infalling gas is guided by the pulsar's strong magnetic field so that it lands on the magnetic poles"]
+[0.12934720516204834, 7.175418376922607, "Experiment Date May 3-6, 2009"]
+[0.13358044624328613, 7.185861587524414, "Experiment Date Sept. 22-25, 2009"]
+[7.367431640625, 12.5014066696167, "Satellite Instrument Swath Width 170 km, 150 km, 120 km"]
+[7.269960880279541, 12.390584945678711, "Satellite Instrument Incidence Angle Range 20 to 45\u00ba"]
+[7.305515289306641, 12.430083274841309, "Satellite Instrument Image Types Single-pol (HH, VV, HV or VH) image or two dual-pol images (HH+HV or VV+VH)"]
+[-5.387331485748291, 2.774770975112915, "Telescope Purpose Look for previously unknown supernova remnants"]
+[-0.7290874123573303, 2.9875924587249756, "Supernova Remnant Diameter About 4.4 degrees"]
+[-0.7222871780395508, 2.969068765640259, "Supernova Remnant Area About 90 times bigger than the size of the full Moon"]
+[-0.7224946022033691, 2.97068452835083, "Supernova Remnant Location Very far off the galactic plane"]
+[-5.371240615844727, 2.782827138900757, "Telescope Purpose Confirm the nature of Hoinga"]
+[3.0205559730529785, -1.5869560241699219, "Satellite Mission In-orbit demonstrations of the GNC subsystem, the operations, the autonomy approach, and the VV"]
+[-1.942296028137207, 8.103078842163086, "System Update Cycle Allows for the propagation of the state when no measurements are available, while updating the state only when they are available"]
+[1.565829873085022, -2.3497188091278076, "Satellite Orbit Highly elliptical"]
+[2.423949956893921, -1.7217775583267212, "Satellite Technology RV technology, in particular with non-cooperative targets, with two satellites, in a highly elliptical orbit, using optical Navigation"]
+[-0.039103489369153976, 15.484505653381348, "Gamma-Ray Spectrometer Parameter Value"]
+[-3.5675315856933594, 12.785210609436035, "High-energy Solar Particle Detector Parameter Value"]
+[-1.2339979410171509, 12.920370101928711, "Solar Wind Ion Detector Parameter Value"]
+[-5.392720699310303, 2.7683920860290527, "Telescope Unknown Unknown"]
+[-5.385959625244141, 2.764686107635498, "Telescope Unknown Unknown"]
+[5.221644401550293, -4.001101493835449, "Satellite Launch Year 2006"]
+[5.1923441886901855, -3.9307079315185547, "Satellite Launch Year 2014"]
+[4.2065019607543945, -2.5021653175354004, "Satellite Revisit Time 46 days"]
+[4.22361421585083, -2.5133416652679443, "Satellite Revisit Time 14 days"]
+[0.7109388113021851, -2.283412218093872, "Satellite Incidence Angle 8-60\u00ba"]
+[0.7739704847335815, -2.199486255645752, "Satellite Incidence Angle 8-70\u00ba"]
+[1.458753228187561, -1.074758768081665, "Satellite Spatial Resolution - Strip map 10 m"]
+[1.4748224020004272, -1.1353565454483032, "Satellite Spatial Resolution - ScanSAR 100 m"]
+[1.4037383794784546, -1.1026884317398071, "Satellite Spatial Resolution - Strip map 3 m /6 m /10 m"]
+[1.463142991065979, -1.1355891227722168, "Satellite Spatial Resolution - ScanSAR 100 m"]
+[1.4614914655685425, -1.1106339693069458, "Satellite Spatial Resolution - Spotlight 1 m x 3 m"]
+[0.3095097243785858, 12.435114860534668, "Energetic Heavy Ion Sensor Objective Measure the proton, electron, and alpha particle fluxes at GEO"]
+[0.34647271037101746, 12.357998847961426, "Energetic Heavy Ion Sensor Incorporates ADIS (Angle Detecting Inclined Sensor)"]
+[-4.220767974853516, 12.26821517944336, "Magnetospheric Particle Sensor Sensor Type Three-axis vector magnetometer"]
+[-3.7588841915130615, 12.643860816955566, "Magnetospheric Particle Sensor Energy Range 30ev to 30kev"]
+[-3.8143229484558105, 12.593094825744629, "Magnetospheric Particle Sensor Monitor Medium and high energy protons and electrons"]
+[-0.7366377115249634, 12.360453605651855, "In Situ Ionospheric Plasma Monitoring System Conference Presentation Date Sept. 19-22, 2005"]
+[-0.9530308246612549, 6.483166217803955, "Documentation Publisher Springer Verlag"]
+[-1.5089130401611328, 16.905170440673828, "Altimeter Observation Oceanic currents, bathymetry, and waves"]
+[-2.9834349155426025, 16.16700553894043, "Scatterometer System Observation Ocean winds"]
+[-2.71852707862854, 15.28498649597168, "Scanning Multifrequency Microwave Radiometer Measurement Sea-surface temperature, wind speed, and liquid water"]
+[-5.879042625427246, 16.010040283203125, "Synthetic Aperture Radar Result Large-area maps of sea-ice movement in the Arctic"]
+[5.360818386077881, -4.472490310668945, "Satellite Launch Date 2 April 1998"]
+[4.992426872253418, -4.118955612182617, "Satellite End of Life Date 21 June 2010"]
+[-3.1488051414489746, 1.850183129310608, "Solar Mission Objective Study the three-dimensional magnetic structures of the sun"]
+[-3.177098512649536, 1.877423644065857, "Solar Mission Launch Date Feb. 14, 1980"]
+[-3.1490461826324463, 1.7972791194915771, "Solar Mission First US solar research satellite Since the Solar Maximum Mission"]
+[2.327326774597168, 22.498395919799805, "Instrument Radiance Channels 18 IR and one visible"]
+[1.7480921745300293, 22.0628662109375, "Instrument Footprint Area 10 km x 40 km"]
+[2.436021327972412, 22.22955894470215, "Instrument Footprint Positioning Anywhere in the FOR"]
+[1.777018427848816, 22.12677764892578, "Instrument Frame Size 640 km x 640 km"]
+[1.600821614265442, 22.17486572265625, "Instrument FOR Size 24\u00ba (E-W) x 19\u00ba (N-S)"]
+[2.5701045989990234, 22.818452835083008, "Instrument Sounding Time Almost three hours"]
+[3.0342659950256348, 22.799339294433594, "Instrument Unknown Unknown"]
+[3.7069356441497803, 17.677364349365234, "Payload Unknown Unknown"]
+[5.316020965576172, -4.415303707122803, "Satellite Launch Date June 23, 2015"]
+[5.296220779418945, -4.45353889465332, "Satellite Launch Date March 2017"]
+[0.5688657164573669, -1.4402384757995605, "Satellite Orbit Altitude 786 km"]
+[4.101269721984863, -3.1248011589050293, "Satellite Mean Local Solar Time 10:30"]
+[-2.477780342102051, 13.048849105834961, "Multispectral Imager Spectral Bands 13"]
+[-2.4678986072540283, 13.06467056274414, "Multispectral Imager Swath Width 290 km"]
+[-2.465599775314331, 13.064681053161621, "Multispectral Imager Spatial Resolution 10 m, 20 m, 60 m"]
+[-2.4737887382507324, 13.07688045501709, "Multispectral Imager Data Transmission X-band, laser link through EDRS"]
+[5.249446392059326, -2.23234224319458, "Satellite Design Life Seven years"]
+[0.966183602809906, -4.3117265701293945, "Satellite Fuel Capacity 123 kg"]
+[5.115128993988037, -4.295151710510254, "Satellite Mission Date April 2008"]
+[5.2046122550964355, -4.483006477355957, "Satellite Implementing Arrangement Date Sept. 11, 2008"]
+[-1.9144330024719238, 14.885282516479492, "Radiometer Operation One infrared detector, one water vapour detector and one pair of visible detectors will be in operation"]
+[-1.9176076650619507, 14.872675895690918, "Radiometer Detector Alignment The misalignment due to these displacements is corrected by central on-ground image processing before the images are distributed to users"]
+[-6.6516008377075195, 9.916274070739746, "Antennas Polarization Circular"]
+[-6.673620700836182, 9.941171646118164, "Antennas Polarization Same"]
+[-5.258481979370117, 7.86431884765625, "Communication System Modulation and Coding Impact on the bit rate, consumption, and implementation complexity"]
+[-5.2572174072265625, 7.921895503997803, "Communication System Architecture Not specified"]
+[2.586932897567749, 14.472772598266602, "Multi Spectral Instrument Hardware SiC"]
+[2.57448673248291, 14.423911094665527, "Multi Spectral Instrument Telescope Mirrors Manufacturing, testing and alignment"]
+[-3.0034515857696533, 7.74111270904541, "Central Processing Unit Voltage 300 V"]
+[-0.515346109867096, 11.328240394592285, "Monitoring Circuit Function Detects arc"]
+[-1.848556637763977, 8.732756614685059, "Circuit Function Counts the number of arcs"]
+[-3.0497336387634277, 7.691338539123535, "Central Processing Unit Function Recovers from malfunctions"]
+[-0.3349358141422272, 8.148354530334473, "Materials Function Mitigate arcing under a LEO plasma environment"]
+[6.3062238693237305, 7.4339494705200195, "Satellite Component Attachment Method Hinges"]
+[6.325545310974121, 7.412718296051025, "Satellite Component Attachment Method Support Rods"]
+[2.2515366077423096, -1.9890960454940796, "Satellite Configuration Open \u201cflower petal\u201d configuration"]
+[2.299884796142578, -1.8452942371368408, "Satellite Integration Method Soft-stacked"]
+[-1.4914860725402832, 13.414167404174805, "Solar Arrays Technology Roll up in a canister and then unfurl once in space"]
+[-1.492189884185791, 13.423726081848145, "Solar Arrays Manufacturer Deployable Space Systems"]
+[6.283184051513672, 7.455850124359131, "Satellite Component Power Generation 215 kW"]
+[-1.4835529327392578, 13.40641975402832, "Solar Arrays Power Generation 160 kW"]
+[2.7114522457122803, 22.482017517089844, "Instrument Descoped Yes"]
+[2.620755910873413, 13.427240371704102, "Optical Component Diameter 50 mm"]
+[2.5744967460632324, 13.426461219787598, "Optical Component Replaced by Lens objective (doublet)"]
+[-1.9257147312164307, 8.121912956237793, "System Mass Reduction About 30%"]
+[2.642568349838257, 13.45438289642334, "Optical Component Thermal Stability Relaxes the thermal stability requirements of the optical bench"]
+[-0.33633551001548767, 6.400991439819336, "Space Test Facility Exposure Orientations Ram, wake, zenith, and nadir"]
+[-3.0260090827941895, 4.425558567047119, "Spacecraft Cargo Capacity 2,630 kg"]
+[-3.01628041267395, 4.224379539489746, "Experimental Spacecraft Test Objectives Practice hitting an onboard target with a harpoon, jettison a small piggyback satellite and then try to bag it up with a net"]
+[-7.562744140625, 5.894082069396973, "Camera Data Collected 165 GB"]
+[-7.550069332122803, 5.893645286560059, "Camera Data Downlink Frequency Daily"]
+[-7.56060266494751, 5.8860650062561035, "Camera Number of All-Sky Maps 7"]
+[-7.53500509262085, 5.919398784637451, "Camera Combined Sensitivity Improvement Factor of 5"]
+[-7.558209419250488, 5.895959854125977, "Camera Number of Sources in Six Months 1 million"]
+[-1.5476330518722534, 12.834585189819336, "Coronagraph Design Evolution Not provided"]
+[-13.873786926269531, -2.1955926418304443, "X-ray Telescope Energy Range High-energy X-rays"]
+[-13.856904983520508, -2.165670871734619, "X-ray Telescope Energy Range Lower-energy X-rays"]
+[-0.7048879861831665, 2.966973304748535, "Supernova Remnant Distance from Earth 11,000 light-years"]
+[6.363708019256592, 7.3842692375183105, "Satellite Component Imaging Resolution 3m-100m"]
+[0.7656663060188293, -1.3004043102264404, "Satellite Field of Regard 150-500km"]
+[1.0068880319595337, -1.4295183420181274, "Satellite Ground Swath 20km-500km"]
+[0.7047099471092224, -1.156984806060791, "Satellite Altitude 798km"]
+[3.835667371749878, -3.091348171234131, "Satellite LTDN 6am"]
+[0.6800435185432434, -2.316624879837036, "Satellite Inclination 98.6\u00b0"]
+[4.041520118713379, -2.8499972820281982, "Satellite Period 100.7 minutes"]
+[5.323357105255127, -4.384064197540283, "Satellite Launch Date September 1997"]
+[0.691676914691925, -1.1825698614120483, "Satellite Altitude 35,786 km"]
+[0.8695680499076843, -2.099384307861328, "Satellite Longitude 57.5 \u00b0E"]
+[4.702772617340088, -2.5772366523742676, "Satellite Operational Duration 17 years"]
+[-2.2258236408233643, 8.177563667297363, "AOCS Interface Module Quantity 2"]
+[0.4672972857952118, 9.369795799255371, "Attitude Control Device Quantity 3"]
+[0.8743737936019897, 12.107444763183594, "Sensor Quantity 4"]
+[-4.49367618560791, 12.115187644958496, "Magnetometer Quantity 2"]
+[-0.5737650990486145, 8.520797729492188, "Reaction Wheels Quantity 4"]
+[-4.362430095672607, 0.19585837423801422, "GPS Receiver Quantity 1"]
+[-1.8521614074707031, 8.684920310974121, "Control Unit Quantity 1"]
+[-1.0739601850509644, 8.628599166870117, "Gyro Quantity 4"]
+[-2.273796558380127, 7.43057918548584, "On-Board Computer Quantity 2"]
+[-2.184812307357788, 7.575970649719238, "General Purpose Input/Output Board Quantity 1"]
+[-2.558372735977173, 9.266525268554688, "Power Module Quantity 3"]
+[-2.586779832839966, 9.291557312011719, "Power Module Quantity 3"]
+[-2.713965654373169, 9.469085693359375, "Power Generation Quantity 3"]
+[-3.0660908222198486, 9.635506629943848, "Battery Quantity 1"]
+[-5.166008949279785, 7.788796424865723, "Communication Bus Quantity 2"]
+[3.6539676189422607, 17.610620498657227, "Payload Power Supply Module Quantity 1"]
+[1.9074041843414307, 10.710981369018555, "Imaging Device Image Capture Time 5 and 8 p.m. local time (04:00 to 07:00 Universal Time)"]
+[1.8897862434387207, 10.72569751739502, "Imaging Device Image Capture Date January 15"]
+[-1.0105206966400146, 12.008526802062988, "Transition Radiation Detector Function Identify electrons and positrons"]
+[-2.3274967670440674, 15.090230941772461, "Electromagnetic CALorimeter Function Identify electrons and positrons"]
+[-0.5893410444259644, 11.732767105102539, "Silicon Tracker Detector Acceptance Matching ECAL"]
+[-2.3000309467315674, 13.030264854431152, "Multispectral Scanning Imaging System Imaging Capabilities Cloud cover, surface temperature, vegetation, snow and ice"]
+[-2.360734462738037, 13.105987548828125, "Multispectral Scanning Imaging System Imaging Capabilities Land and sea surfaces, and ice cover"]
+[-2.7794857025146484, 15.26351261138916, "Microwave Imaging/Sounding Microwave Radiometer Monitoring Capabilities Atmospheric temperature and humidity profiles, precipitation, sea-level wind speed and snow/ice coverage"]
+[0.7549640536308289, 0.9726402759552002, "Geophysical Monitoring System Komplex Monitoring Capabilities Space environment"]
+[-0.6357063055038452, 16.057390213012695, "Infrared Fourier Spectrometer-2 Monitoring Capabilities Atmospheric temperature and humidity profiles"]
+[-4.580913543701172, 15.914217948913574, "Onboard Radar Complex Imaging Capabilities Land and sea surface monitoring"]
+[-3.786367416381836, 6.962646961212158, "Data Collection System Data Collection In-situ data from Data Collection Platforms (DCPs) in the ground segment with location capability"]
+[-1.7868878841400146, 8.522416114807129, "Electronics Development and Integration Unknown"]
+[-0.8569082021713257, 11.53921127319336, "Detector RFI Mitigation Capability Unknown"]
+[2.643955707550049, 22.55157470703125, "Instrument Days of data collection 63.5"]
+[2.558438301086426, 22.567317962646484, "Instrument Days of data collection 91.0"]
+[2.608339309692383, 22.48960304260254, "Instrument Days of data collection 94.2"]
+[2.5568795204162598, 22.628482818603516, "Instrument Days of data collection 48.0"]
+[2.6978979110717773, 22.433616638183594, "Instrument Data Tapes 516 film reels"]
+[2.1733667850494385, -2.725358724594116, "Satellite Number of Workshops 13"]
+[2.0704660415649414, -2.7781221866607666, "Satellite Number of Colloquiums 2"]
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+[-2.5373446941375732, 8.238471984863281, "Failure Detection, Isolation and Recovery Design and Analysis Ongoing"]
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+[-0.5844590663909912, -0.15211181342601776, "Satellite Deployment System Largest Satellite Deployment 20 June 2018"]
+[5.117249011993408, -4.492676258087158, "Satellite Deployment Date 20 June 2018"]
+[2.692842483520508, 22.08407974243164, "Instrument Main Objective Improve the microphysical and radiative property characterization of clouds and aerosols"]
+[2.835151433944702, -1.3353095054626465, "Satellite Mission Objective Improve the microphysical and radiative property characterization of clouds and aerosols"]
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+[3.071293830871582, -1.4633971452713013, "Satellite Complementary Missions PARASOL (POLDER) complements CALIPSO (Lidar) and NASA's Aqua and Aura (MODIS, CERES) missions"]
+[-4.520439147949219, 15.920495986938477, "Radar Complementary Instrument PARASOL (POLDER) complements CALIPSO (Lidar) and NASA's Aqua and Aura (MODIS, CERES) missions, it also makes use of the CloudSat (CPR) radar data"]
+[11.235245704650879, 5.474876403808594, "CubeSat Component Angle Optimization"]
+[11.31476879119873, 5.469152927398682, "CubeSat Communications Snapshot URL: https://web.archive.org/web/20190716185147/http://mstl.atl.calpoly.edu/~bklofas/Presentations/DevelopersWorkshop2012/CHDC_Provost_CADRE.pdf"]
+[-4.4875311851501465, 15.911269187927246, "Radar Measurement Capability Measure methane emissions"]
+[-4.519652843475342, 15.945059776306152, "Radar Work Progress Analysed less than 0.14 per cent of the lakes in the Arctic"]
+[-4.531377792358398, 15.95226764678955, "Radar Future Plans Analyse Alaska, Canada and Greenland as well as eventually Russia"]
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+[-7.608399868011475, 5.927260398864746, "Cameras Quantity 3"]
+[-1.405386209487915, 7.960995674133301, "Unit Manufacturer Thales Alenia Space in Belgium"]
+[-1.229098916053772, 6.868770122528076, "Assembly Manufacturer Thales Alenia Space in Belgium"]
+[-7.543315887451172, 5.903095722198486, "Camera Manufacturer Thales Alenia Space in Switzerland"]
+[-1.1877671480178833, 6.824901580810547, "Assembly Manufacturer Thales Alenia Space in Spain"]
+[-1.4208943843841553, 8.069562911987305, "Unit Manufacturer Thales Alenia Space in Spain"]
+[5.834050178527832, 14.37497329711914, "Transponder Manufacturer Thales Alenia Space in Spain"]
+[-1.0561619997024536, 7.729966640472412, "Devices Manufacturer Leonardo"]
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+[-3.071270227432251, 4.231813907623291, "Spacecraft Landing Method Water"]
+[-3.5546369552612305, 4.381871223449707, "Spacecraft Launch Date 2017"]
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+[-4.5008721351623535, 15.925291061401367, "Radar Ability Penetrating vegetation such as forests"]
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+[-0.5012093782424927, 0.18156450986862183, "Global Navigation Satellite System Program Completion May 2003"]
+[-3.3757288455963135, 8.538618087768555, "Mass Memory System Technology NAND-Flash Storage"]
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+[5.3057661056518555, -4.462648391723633, "Satellite Launch Date 12 January 2018"]
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+[-5.842333793640137, 15.967982292175293, "Synthetic Aperture Radar Daily Data Acquisition Volume 800 GB"]
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+[2.2462968826293945, -1.304079294204712, "Satellite Detection Capability Ponds half the size of the Lincoln Memorial Reflecting Pool"]
+[2.026026487350464, -1.12901771068573, "Satellite Measurement Capability All of these lakes and reservoirs"]
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+[-1.2319320440292358, 8.588218688964844, "Component Expected Lifetime 3 years"]
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+[-0.9616424441337585, 13.103713035583496, "Solar Irradiance Sensor Operation Mode Follows the Sun from sunrise to its sunset, which occurs every 90 minutes"]
+[-1.0247001647949219, 13.109102249145508, "Solar Irradiance Sensor Contract Value Approximately $16.2 million"]
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+[-0.41425296664237976, 14.525949478149414, "Imaging Instrument Cadence ~30 min"]
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+[-4.975398063659668, 8.67896556854248, "Transmit/Receive Modules Number of Modules 512"]
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+[-4.985475063323975, 8.637077331542969, "Transmit/Receive Modules Number of Modules per Column 32"]
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+[0.44933584332466125, 4.524120330810547, "Natural Phenomenon Minimum Extent Area 3.74 million km2 (1.44 million square miles)"]
+[0.4916994571685791, 4.503798007965088, "Natural Phenomenon Satellite Record Start Year 1979"]
+[-0.3561212718486786, 12.211490631103516, "Thermal Infrared Sensor Image Type Land surface temperatures"]
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+[-5.406442642211914, 2.7842538356781006, "Telescope Detection Ability 7000 seconds"]
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+[-7.28386926651001, 2.8744146823883057, "Gamma Ray Burst Galaxy Light Travel Time 11.7 billion years"]
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+[6.745268821716309, 6.953360080718994, "Satellite Component Unknown Unknown"]
+[3.7355611324310303, 17.70994758605957, "Payload Receiver Type Geodetic grade COTS receiver"]
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+[0.49017518758773804, 9.555055618286133, "Attitude Sensor Performance Solid performance"]
+[3.7107958793640137, 17.69007682800293, "Payload Operation Successful delivery of GPS navigation fixes and raw measurements"]
+[-3.0279150009155273, 4.4175920486450195, "Spacecraft Service Module Unknown"]
+[-3.0632998943328857, 4.304923057556152, "Spacecraft Service Module Unknown"]
+[-3.0273194313049316, 4.287716865539551, "Spacecraft Service Module Unknown"]
+[-3.677180528640747, 8.038908958435059, "Solid State Recorder Commissioning Date April 27-28, 2012"]
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+[-0.6385332942008972, 9.450921058654785, "Spacecraft Component Control Speed 1500 rpm"]
+[-0.6205330491065979, 9.428354263305664, "Spacecraft Component Deployment Automatic"]
+[-0.6341047883033752, 9.45133113861084, "Spacecraft Component Deployment Automatic"]
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+[0.9910829663276672, -4.37500524520874, "Satellite Mass About 1700 kg"]
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+[-0.7745712399482727, 12.55394458770752, "Radiation Monitoring System Power Consumption 6.8 W"]
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+[-2.247263193130493, 6.266594886779785, "Focal Plane Operating Temperature -80\u00baC"]
+[-2.2836194038391113, 6.255433559417725, "Focal Plane Operating Temperature 20\u00baC"]
+[-0.8670974969863892, 11.606608390808105, "Detector Technology 0.35 \u00b5m CMOS technology"]
+[-0.8865258097648621, 11.515490531921387, "Detector Package Ceramic package"]
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+[0.22456642985343933, 13.786636352539062, "Calibration Device Interval 30 minutes"]
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+[0.2605946958065033, 13.7565279006958, "Calibration Signal Purpose Checking the stability of the amplifiers and of the data stream"]
+[-8.14322566986084, 8.831278800964355, "Electrical Power Subsystem Solar Panel Type Triple-junction solar cells"]
+[-8.135833740234375, 8.824875831604004, "Electrical Power Subsystem Solar Panel Conversion Efficiency 26.8%"]
+[-8.145284652709961, 8.822967529296875, "Electrical Power Subsystem Li-ion-polymer Battery Capacity 910 mAh"]
+[-8.14698314666748, 8.822020530700684, "Electrical Power Subsystem Battery Configuration 5 parallel sets of 2-series batteries"]
+[-2.2481629848480225, 9.045523643493652, "Power Control Unit Control Method PPT (Peak Power Tracking)"]
+[-2.2209348678588867, 9.006296157836914, "Power Control Unit Microprocessor 16 bit microprocessor (H8/3048F)"]
+[-1.421885371208191, 13.376357078552246, "Solar Cell Experiment Number of Cell Types 47"]
+[-1.3588804006576538, 13.32715129852295, "Solar Cell Experiment Sun Direction Tolerance 5\u00ba"]
+[-5.252642631530762, 7.618059158325195, "Space Communications Protocol Standards Objectives Demonstrate and test a full space implementation of the Space Communications Protocol Standards"]
+[-5.27766752243042, 7.654712200164795, "Space Communications Protocol Standards Services Spacecraft control and monitor data handling services based on and compatible with commercial Internet protocols"]
+[-1.941415548324585, 14.96387767791748, "Imaging Radiometer/Polarimeter Mass 32 kg"]
+[-1.904293417930603, 15.038128852844238, "Imaging Radiometer/Polarimeter Size 800 mm x 500 mm x 250 mm"]
+[-1.9055334329605103, 15.011228561401367, "Imaging Radiometer/Polarimeter Power Consumption 42 W"]
+[-13.913785934448242, -2.1301000118255615, "X-ray Telescope Energy Ranges 0.5 to 2 keV and 2 to 4 keV"]
+[-13.871106147766113, -2.129718065261841, "X-ray Telescope Energy Range 7 to 25 keV"]
+[-13.514052391052246, -2.0578644275665283, "X-ray Space Observatory Public Data Availability Aug. 29, 2013"]
+[-13.503803253173828, -2.056823492050171, "X-ray Space Observatories Collaboration Date Feb. 27, 2013"]
+[-1.5325756072998047, 13.456737518310547, "Solar Array Generation Voltage Unknown"]
+[-2.1765389442443848, 8.796401023864746, "Electrical System Potential Measurable"]
+[-3.0797131061553955, 4.158165454864502, "Spacecraft No Arcing Condition Monitoring Required"]
+[-2.151632070541382, 8.893111228942871, "Electrical System No Influence Condition Monitoring Required"]
+[-1.4803805351257324, 13.411284446716309, "Solar Arrays Arcing Detection Monitoring Required"]
+[-2.127403497695923, 8.882015228271484, "Electrical System CPU Recovery Time Unknown"]
+[-0.1775389313697815, 6.489078044891357, "Test Configuration Vacuum Chamber Dimensions 1.2 m in length and 1 m in diameter"]
+[-0.16443376243114471, 6.488292694091797, "Test Configuration Back Pressure 1 x 10-3 Pa"]
+[-0.16944117844104767, 6.5107102394104, "Test Configuration Plasma Density 1.3 x 1012 m-3"]
+[-0.17663194239139557, 6.511003017425537, "Test Configuration Electron Temperature 1.0 eV"]
+[4.6705780029296875, -2.5921294689178467, "Satellite Maximum Mission Duration About 2.5 years"]
+[3.255812168121338, -1.6543824672698975, "Satellite Operation Priority FF demonstration first, then science and finally experiments"]
+[-3.1434435844421387, 1.7292815446853638, "Satellite Mission Formation Flying Yes"]
+[-3.1534512042999268, 1.7192540168762207, "Satellite Mission Study Subject Sun\u2019s inner corona"]
+[-1.4300258159637451, 6.075662136077881, "Prime Contractor Overall Project Management Responsible"]
+[-1.2954760789871216, 6.190420627593994, "Contractor Avionics architecture Responsible"]
+[-1.3273227214813232, 6.163158893585205, "Contractor PLM structural engineering Responsible"]
+[-1.4984582662582397, 16.896827697753906, "Altimeter Ground Resolution 1-10 m"]
+[-1.5003024339675903, 16.89806365966797, "Altimeter Vertical Resolution Sub-meter"]
+[-1.5067640542984009, 16.898277282714844, "Altimeter Spatial Resolution Sub-kilometer"]
+[2.3333568572998047, 22.921512603759766, "Instrument Data Rate 5 Gbit/s"]
+[-3.0136055946350098, 7.771610736846924, "Data Processor Function Detects weak lightning flashes from the intense but slowly evolving background"]
+[-2.9600722789764404, 7.781957149505615, "Data Processor Function Averages the output from the focal plane over a number frames on a pixel-by-pixel basis to generate a background estimate"]
+[-3.0900731086730957, 7.790942668914795, "Data Processor Function Subtracts the average background estimate of each pixel from the current signal of the corresponding pixel"]
+[2.5257675647735596, 22.321971893310547, "Instrument Data Output Shot noise fluctuating about zero with occasional peaks due to lightning events"]
+[2.827237844467163, 22.479637145996094, "Instruments Characteristics and Calibration Unknown"]
+[1.539094090461731, 6.980640888214111, "Communication Technology Frequency Band X-band"]
+[-3.1167237758636475, 4.223535060882568, "Spacecraft Orbit Maneuvers More than 10"]
+[-3.3667850494384766, 4.2434258460998535, "Spacecraft Orbit Duration More than 2 years"]
+[-1.5650664567947388, 4.163790225982666, "Ground Segment Equipment Unknown Unknown"]
+[3.056941032409668, -1.5712802410125732, "Satellite Mission Operator MIT"]
+[-5.0290703773498535, 2.8657472133636475, "Space Telescope Retirement Date Jan. 30, 2020"]
+[2.52083158493042, -1.1856029033660889, "Satellite Data Usage Detecting pulsation patterns in young, rapidly rotating stars"]
+[2.7166268825531006, -1.4182169437408447, "Satellite Discovery Revolutionize scientists\u2019 ability to study details like the ages, sizes and compositions of stars"]
+[2.9420413970947266, -1.9934114217758179, "Satellite First Planets Unknown"]
+[2.9050445556640625, -2.070373296737671, "Satellite Far-flung Supernovae Unknown"]
+[-3.116403579711914, 2.2814176082611084, "Missions 1st-Light Data Unknown"]
+[-5.394901752471924, 2.8071577548980713, "Telescope FOV (Field of View) 4.6\u00ba x 4.6\u00ba"]
+[-5.426286697387695, 2.763960123062134, "Telescope Resolution < 0.22\u00ba"]
+[-5.342066764831543, 2.698732614517212, "Telescope Grasp (500 eV) 27.5 cm2 deg2"]
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+[-0.4511738717556, 14.264594078063965, "Microdosimeter Electron energy > 50 keV"]
+[-0.4378332197666168, 14.335529327392578, "Microdosimeter Ion energy > 1 MeV"]
+[-0.4548408091068268, 14.269976615905762, "Microdosimeter FOV 38\u00ba"]
+[-0.46132782101631165, 14.261947631835938, "Microdosimeter Electron energy > 50 keV"]
+[-0.43658870458602905, 14.29209041595459, "Microdosimeter Ion energy > 50 keV"]
+[-0.4328860342502594, 14.280055046081543, "Microdosimeter FOV 32\u00ba"]
+[-4.5049567222595215, 12.107085227966309, "Magnetometer Uncertainty \u00b114 nT"]
+[-4.506270885467529, 12.107641220092773, "Magnetometer Range \u00b1 100,000 nT"]
+[3.6405889987945557, 13.20761489868164, "Laser Operational Mode Science Mode 1"]
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+[-4.941251277923584, 9.768902778625488, "Receiver Wavelength 532 nm"]
+[-4.949311256408691, 9.777570724487305, "Receiver Detector Type Photon counting detectors"]
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+[2.62338924407959, 22.48276710510254, "Instrument Laser and Receiver Configurations Configuration 2a: 532 and 1064 nm narrow line width laser pulses, Configuration 2b: 355 nm laser pulses, Configuration 2c: Backup for laser 1"]
+[-4.504986763000488, 15.929884910583496, "Radar Swath Width 260 km"]
+[-6.783041954040527, 10.040865898132324, "Antenna Size 11m x 3,6m"]
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+[2.881378173828125, -1.2527670860290527, "Satellite Mission Environmental monitoring, land management, ocean monitoring"]
+[-1.4771806001663208, 9.567854881286621, "Liquid Apogee Motor Thrust 440 N"]
+[-1.5255396366119385, 9.595254898071289, "Liquid Apogee Motor Number of Thrusters 12"]
+[-1.4793896675109863, 9.553303718566895, "Liquid Apogee Motor Thruster Type 22 N bipropellant"]
+[-5.290799140930176, 7.967144012451172, "Communication System Bandwidth 30 MHz"]
+[-5.302402019500732, 8.016660690307617, "Communication System Frequency Range 4770 - 4800 MHz"]
+[-5.305383205413818, 7.996468544006348, "Communication System Antenna Type Omnidirectional antenna system for both up and down links and additional global horn for downlink"]
+[-0.11336810141801834, 13.594507217407227, "Measurement System Test Length 16 m"]
+[-0.44466641545295715, 6.7941179275512695, "Test Equipment Maximum Range 70 m"]
+[-0.42032793164253235, 6.783377647399902, "Test Equipment Longitudinal Movement Less than 1 m"]
+[-0.40158721804618835, 16.213809967041016, "Spectrograph Measurement OH distribution in the mesosphere and upper stratosphere"]
+[-0.4059649109840393, 16.19991683959961, "Spectrograph Measurement Nitric oxide"]
+[0.5616788268089294, 12.12317943572998, "Sensor Tracking Capability 0.5 arcdeg/s"]
+[0.47852209210395813, 12.239469528198242, "Sensor Centroidization Accuracy 0.1 camera pixels (3.5 arcsec)"]
+[0.4831094741821289, 12.232236862182617, "Sensor Absolute Calibration Accuracy 0.14 camera pixels (5 arcsec)"]
+[0.8049964904785156, 11.975510597229004, "Sensor Power Supply Unregulated 28 V"]
+[0.35308024287223816, 12.437883377075195, "Sensor Data Transmission Rate 10 Hz"]
+[0.5608695149421692, 12.166399002075195, "Sensor Power Consumption < 8 W"]
+[0.5953162908554077, 12.11991024017334, "Sensor Field of Operation 10 arcdeg"]
+[0.5265604853630066, 12.197688102722168, "Sensor Depth of Operation 5 m to 80 m"]
+[-1.595047116279602, 4.102877616882324, "Ground Segment Responsibilities All flight operations of the Sentinel-2 spacecraft including monitoring and control, execution of all platform activities and commanding of the payload schedules"]
+[-1.5858310461044312, 4.095327377319336, "Ground Segment Responsibilities Payload and downlink planning, data acquisition, processing, archiving and downstream distribution of the Sentinel-2 satellite data"]
+[-0.5623712539672852, 1.257637619972229, "Orbit Determination Tool Development and Testing Period Throughout 2014"]
+[-0.5685054659843445, 1.2589256763458252, "Orbit Determination Tool Incorporation Date End of 2014"]
+[-0.5673686861991882, 1.2664716243743896, "Orbit Determination Tool Function Generate definitive orbit files"]
+[-0.5641298294067383, 1.2644164562225342, "Orbit Determination Tool Reprocessed Data Entire mission orbit telemetry"]
+[6.336752891540527, 7.325361728668213, "Satellite Component Stability Low jitter"]
+[3.0601730346679688, -1.5284607410430908, "Satellite Mission Assurance Standards Class B"]
+[2.928126335144043, -1.6710573434829712, "Satellite Design Fully redundant"]
+[2.3515264987945557, -1.71635901927948, "Satellite Electronic Parts Rad-hard/tolerant level 1/2"]
+[1.561993956565857, -1.514704704284668, "Satellite Technology Readiness Level High"]
+[3.160881757736206, -1.77705979347229, "Satellite Manufacturing Cleanliness standards appropriate for optical payloads"]
+[2.426457643508911, -1.6216349601745605, "Satellite EMI/EMC Mitigations Integrated"]
+[-0.6392166614532471, 9.434416770935059, "Spacecraft Component Total Mass 3.25 kg"]
+[-0.6802858114242554, 9.387247085571289, "Spacecraft Component Steady-State Power 30W"]
+[-0.6695806980133057, 9.458882331848145, "Spacecraft Component Initial Heater Power 80 W"]
+[-1.2133604288101196, 8.9939603805542, "Tank Volume 100 cm3"]
+[-1.4699451923370361, 9.466922760009766, "Ion Thruster Type UK-10"]
+[-1.528639554977417, 9.574121475219727, "Ion Thruster Power Unknown"]
+[2.904205560684204, 21.9747314453125, "Instrument Purpose Study the salt content of ocean surface waters"]
+[1.9776040315628052, 22.219932556152344, "Instrument Measurement Depth Top 5 cm of the land"]
+[2.6547136306762695, 22.814626693725586, "Instrument Survey Time 8 days"]
+[2.6413636207580566, 22.217195510864258, "Instrument Survey Coverage Worldwide with gaps in mountainous or vegetated terrain"]
+[2.8738415241241455, 21.9287109375, "Instrument Purpose Help avoid a dangerous gap in Arctic sea ice data"]
+[5.3224663734436035, -4.441831588745117, "Satellite Launch Date April 2014"]
+[4.934844970703125, -4.324793338775635, "Satellite Cease Transmitting Weather Data August 4, 2017"]
+[1.9327075481414795, -1.9680055379867554, "Satellite Loss of Attitude Control Predicted to occur late next month"]
+[2.9806742668151855, -1.338327169418335, "Satellite Realignment A 1994 presidential directive realigned primary command and control of DMSP under the Department of Commerce\u2019s National Oceanic and Atmospheric Administration"]
+[-1.465583086013794, 4.3238091468811035, "Ground System Operation System Central-core system for the mission operation"]
+[-1.4328787326812744, 4.319852828979492, "Ground System Data Distribution Online or through a medium"]
+[-1.4421762228012085, 4.340828895568848, "Ground System Product Processing Processes AMSR and GLI 1km products on a semi-real-time basis"]
+[2.8973429203033447, 22.423479080200195, "Instruments Compatibility Space Plug and Play Compatible"]
+[3.641634941101074, 22.898157119750977, "Instruments Symposium Date April 8-12, 2013"]
+[2.673902750015259, 14.336600303649902, "Optical Instrument Lens System Spherical lenses"]
+[2.606064796447754, 14.308854103088379, "Optical Instrument Dispersing Element Direct vision prism, S-FPL53 and L-NBH54"]
+[2.6623411178588867, 14.375239372253418, "Optical Instrument Spectral Sampling Interval 1.2 nm to 16 nm"]
+[2.635225534439087, 14.355608940124512, "Optical Instrument Spectral Sensitivity Lower in the NIR band region than the visible band region"]
+[2.6631152629852295, 14.365744590759277, "Optical Instrument SNR Drops to rather low levels if a constant spectral sampling level is maintained"]
+[-4.461248874664307, 15.89754867553711, "Radar Resolution 1 m (Azimuth) x 0.67 m (Range)"]
+[-4.504984378814697, 15.928888320922852, "Radar Swath 10 km x 10 km"]
+[-4.453423023223877, 15.881514549255371, "Radar Resolution 3 m (Azimuth) x 2 m (Range)"]
+[-4.507167339324951, 15.928339958190918, "Radar Swath 25 km"]
+[-4.482974529266357, 15.915051460266113, "Radar Resolution 3 m (Azimuth) x 4 m (Range)"]
+[-4.539141654968262, 15.960188865661621, "Radar Swath 25 km"]
+[-4.538768768310547, 15.931497573852539, "Radar Resolution 21-23 m (Azimuth) x 8 m (Range)"]
+[-4.507949352264404, 15.932332038879395, "Radar Swath 115 km"]
+[-4.490978717803955, 15.905709266662598, "Radar Resolution 41-55 m (Azimuth) x 8 m (Range)"]
+[-4.510731220245361, 15.932198524475098, "Radar Swath 223 km"]
+[1.5124073028564453, 5.422999858856201, "Satellite Bus Variant GOES-R"]
+[-5.107305526733398, 7.822838306427002, "Communication Bus Type High-speed"]
+[5.295373439788818, -4.430230140686035, "Satellite Launch Date March 2018"]
+[5.160826683044434, -4.243436813354492, "Satellite Launch Date March 2022"]
+[1.8724769353866577, -1.9880309104919434, "Satellite Operational Position GOES-WEST at 137.2\u00b0 West"]
+[2.617501974105835, -2.02493953704834, "Satellite Expected Operational Position GOES-WEST"]
+[-3.4180212020874023, 7.109976291656494, "Data Analysis Center Affiliated Institutions MIT's Physics Department, Kavli Institute for Astrophysics and Space Research, the SAO (Smithsonian Astrophysical Observatory), and the NASA Ames Research Center"]
+[-3.639584541320801, 7.1649980545043945, "Data Archive Data Storage Raw and processed data"]
+[-1.2104289531707764, 3.088184356689453, "Astronomical Event Definition Occurrence when a planet passes in front of a star"]
+[-1.1871562004089355, 3.0337648391723633, "Celestial Object Brightness Dip Indicates the presence of a planet passing in front of it"]
+[-1.9157851934432983, 14.890707969665527, "Radiometer Channels 50.3, 52.8, 53.6, 91.665 (V and H polarization), 150, 183.3 \u00b1 1, 183.3 \u00b1 3, and 183.3 \u00b1 6.6 GHz"]
+[-1.9108957052230835, 14.870464324951172, "Radiometer Polarization Horizontally polarized (except for the two 91.665 GHz channels)"]
+[-1.8827204704284668, 14.827777862548828, "Radiometer Operation Provided SSMIS underflights during the March/April 2004 field campaign"]
+[1.732804298400879, -2.1129541397094727, "Satellite Orbit Position Geostationary"]
+[0.5241050720214844, -1.4722132682800293, "Satellite Orbit Altitude 35,786 kilometers"]
+[0.7081332802772522, 3.965623378753662, "Earth's Atmosphere Layer Altitude Range About 53 and 373 miles (85 and 600 km)"]
+[0.7022292017936707, 3.9629225730895996, "Earth's Atmosphere Layer Temperature Up to 2,700 \u00b0F (1,500 \u00b0C)"]
+[-1.4843494892120361, 13.42104434967041, "Solar Array Voltage 350 V"]
+[-1.5022298097610474, 13.427796363830566, "Solar Array Operation Time More than 50 hours"]
+[0.5864824652671814, 12.218466758728027, "Temperature Sensor Measurement Date After July 7, 2012"]
+[6.336887836456299, 7.382016181945801, "Satellite Panels Weight Difference The -X panel side is heavier than the +X panel side"]
+[0.6635082960128784, 9.325953483581543, "Attitude Determination and Control Subsystem Magnetorquer Coils Max. Magnetic Dipole 0.13 A m2"]
+[0.706745982170105, 9.3696870803833, "Attitude Determination and Control Subsystem Reaction Wheel 30 mNms"]
+[0.646608829498291, 9.328876495361328, "Attitude Determination and Control Subsystem Attitude Determination Accuracy \u00b110\u00ba"]
+[0.6513797044754028, 9.324241638183594, "Attitude Determination and Control Subsystem Pointing Stability \u00b11\u00ba"]
+[0.21168221533298492, 13.754152297973633, "Calibration Mechanism Selectable Positions Open (nominal), closed (testing) and X-ray source (calibration)"]
+[-3.1459639072418213, 7.614925861358643, "Data Processing Unit Frame Size 147,456 pixels"]
+[-3.223738670349121, 7.567062854766846, "Data Processing Unit Cycle Time 50 ms"]
+[-13.867505073547363, -2.2005865573883057, "X-ray Telescope Point Source Sensitivity ~30 times better than ROSAT (soft band 0.5-2 keV) and ~100 times better than HEAO/RXTE (hard band 2-10 keV)"]
+[3.6767547130584717, -2.5660502910614014, "Satellite Monitoring Frequency Every 24 days"]
+[1.6217354536056519, -1.5053530931472778, "Satellite Monitoring Area 3.8 million hectares"]
+[1.3561384677886963, -1.2961924076080322, "Satellite Detection Area 0.5 hectares"]
+[2.4637832641601562, -1.2415434122085571, "Satellite Surveillance Capabilities Global high-resolution surveillance"]
+[2.3814871311187744, -1.2948638200759888, "Satellite Data Acquisition Regardless of light or weather conditions"]
+[-13.896522521972656, -2.191153049468994, "X-ray Telescope Sensitivity Higher than previous survey missions"]
+[-13.850104331970215, -2.2077062129974365, "X-ray Telescope Number of Clusters of Galaxies Detected More than 100,000"]
+[-13.894189834594727, -2.248626947402954, "X-ray Telescope Number of Active Black Holes Detected Millions"]
+[-13.842937469482422, -2.2147912979125977, "X-ray Telescope Number of Isolated Neutron Stars Detected Unknown"]
+[-5.294646739959717, 2.7623565196990967, "Telescope Launch Vehicle Proton rocket"]
+[0.7329184412956238, -1.1991950273513794, "Satellite Re-entry Altitude 80 km"]
+[5.096092700958252, -4.45483922958374, "Satellite Re-entry Date Feb. 8, 2000"]
+[1.752726674079895, -2.0668861865997314, "Satellite Re-entry Location Atlantic Ocean off the coast of Brazil"]
+[2.0400030612945557, -2.078260660171509, "Satellite Tumbling Behavior Initially not as expected"]
+[3.497688055038452, -2.5908355712890625, "Satellite Flash Rate Once per 15 seconds to once or twice per pass"]
+[-1.929036021232605, 8.721601486206055, "Control Unit Class 20 mN"]
+[-1.4440819025039673, 9.520933151245117, "Thruster Class 20 mN"]
+[-1.3152638673782349, 9.426758766174316, "N/A N/A N/A"]
+[-1.2870386838912964, 9.417474746704102, "N/A N/A N/A"]
+[-5.216582775115967, 7.829169750213623, "Communication System Real-time Coverage 40\u201345% of the landmass"]
+[-5.242292881011963, 7.860838413238525, "Communication System Median Delivery Time Under 1 hour for high-priority imagery"]
+[-5.214126110076904, 7.846229553222656, "Communication System Fastest Delivery Time As fast as 11 minutes"]
+[-5.291345119476318, 7.844966888427734, "Communication System Imaging to Availability Time <1 minute"]
+[2.781359910964966, 23.036890029907227, "Instrument Operation Mode Low-voltage mode"]
+[1.6526628732681274, 23.20001983642578, "Instrument Power Requirement Low-power operation in the CubeSat"]
+[1.8424664735794067, 22.199996948242188, "Instrument Mass Resolution Enables mass resolution of the particles"]
+[0.5586209297180176, 12.064742088317871, "Sensor Omnidirectionality Ensured by the coils design"]
+[0.5214458703994751, 11.894726753234863, "Sensor Operational Environments Various environments, in particular for aeromagnetic surveys"]
+[0.6975023150444031, 11.962112426757812, "Sensor Design Evolutions Necessary to comply with the mass and power budgets allocated to the OVM"]
+[1.8998879194259644, 10.655335426330566, "Imaging Device Design Feature TDI (Time Delay Integration) method"]
+[1.9057773351669312, 10.712390899658203, "Imaging Device Imaging Solution Single lens and two angles of view in the same track"]
+[1.8729976415634155, 10.742137908935547, "Imaging Device Imaging Mode Pushbroom"]
+[1.8739314079284668, 10.675766944885254, "Imaging Device Data Volume Reduction Two-line pushbroom scheme"]
+[-0.7565133571624756, 1.3639682531356812, "Lunar Orbiter Launch Mass About 2480 kg"]
+[-0.7482306957244873, 1.3767497539520264, "Lunar Orbiter Fuel Mass 1300 kg"]
+[-0.8154848217964172, 1.430670976638794, "Lunar Orbiter Payload Mass 140 kg"]
+[-3.0677876472473145, 4.3308844566345215, "Spacecraft Number of Spaceships 2"]
+[-3.01542592048645, 4.307738304138184, "Spacecraft Number of Spaceships 2"]
+[-3.10113525390625, 4.661694526672363, "Resupply Ship Number of Spaceships 1"]
+[-3.069716453552246, 4.663244247436523, "Resupply Ship Number of Spaceships 1"]
+[-3.0803630352020264, 4.440650939941406, "Crew Ship Number of Spaceships 1"]
+[0.18783500790596008, 7.2462615966796875, "Science Experiment Subject Bobtail squid and bacteria"]
+[0.11595723778009415, 7.224530220031738, "Science Experiment Subject Cotton"]
+[0.14814265072345734, 7.2393598556518555, "Science Experiment Subject Tardigrades"]
+[0.4079940617084503, 4.55422306060791, "Geological Formation Subsidence Rate 0.3 meters per year"]
+[0.4100136160850525, 4.549938201904297, "Geological Formation Response Time to Pumping Takes a while to compress in response to the weight of land mass pressing down from above"]
+[0.36500051617622375, 4.584567546844482, "Geological Formation Response Time to Rain or Pumping Rises or falls more quickly in response to rain or pumping"]
+[2.8192942142486572, -2.522735834121704, "Satellite Frequency 406.05 MHz"]
+[0.7321943044662476, -1.4208316802978516, "Satellite Beacon Location Accuracy ~ 4 km"]
+[-4.469017028808594, 8.272560119628906, "Terminal Function Locates the beacons by Doppler processing"]
+[-4.524386882781982, 8.247188568115234, "Terminal Message Forwarding Forwards the located distress message to a nearby Mission Control Center (MCC)"]
+[-1.686176061630249, 6.9556355476379395, "Simulation Tool False Alarm Rate 2 per 3600 km along-track"]
+[-1.6658037900924683, 6.934544563293457, "Simulation Tool Detection Filter Constant False Alarm Rate (CFAR) filter using a K distribution"]
+[-1.6440393924713135, 6.958235263824463, "Simulation Tool Purpose Make useful relative comparisons between the existing RADARSAT-2 beam modes and these new beam modes"]
+[-3.6399059295654297, 12.754420280456543, "Particle Detector Inefficiency Requirement < 10-4"]
+[-3.6497325897216797, 12.752583503723145, "Particle Detector Task Reduce the trigger rate during periods of very large flux activity"]
+[-3.645686388015747, 12.769925117492676, "Particle Detector Response Time Requirement Fast"]
+[0.6448758840560913, 12.012563705444336, "Sensor Data Collection Start Date December 1, 2011"]
+[0.602152407169342, 12.179146766662598, "Sensor Data Collection Duration Four-months"]
+[0.5787566304206848, 12.185681343078613, "Sensor Salinity Measurement Units grams per kilogram"]
+[-1.6237801313400269, 6.980011463165283, "Geant4 Simulation Purpose Simulate GRB detection"]
+[-1.6269500255584717, 6.981719493865967, "Geant4 Simulation Purpose Simulate GRB detection"]
+[-0.8446856141090393, 11.585539817810059, "Detector Type Sodium Iodide (NaI)"]
+[1.819434404373169, -2.165977716445923, "Satellite Orbit Higher than Earth observation satellites"]
+[-0.8604902029037476, 0.13828319311141968, "Satellite System Connection Delay Up to 90 minutes"]
+[-0.8343543410301208, 0.15375542640686035, "Satellite System Information Transmission Quasi-real time"]
+[-7.394784927368164, 2.8706729412078857, "Cosmic Ray Detector Positron Fraction Measurement 0.5\u2013500 GeV"]
+[-7.395895004272461, 2.868649959564209, "Cosmic Ray Detector Publication Date Sept. 18, 2014"]
+[2.276080369949341, -1.8327888250350952, "Satellite Broadband Networking and Video Distribution Services Coverage Africa, Europe, the Middle East and Asia"]
+[2.440214157104492, -1.7205904722213745, "Satellite Function Second node in the European Data Relay System"]
+[2.5929884910583496, -1.7402435541152954, "Satellite Payload Hosted steerable Ka-band communications payload named HYLAS-3 for Avanti Communications"]
+[-3.283968687057495, 5.4577555656433105, "Launch Vehicle Payload Lift Performance to Geostationary Transfer Orbit Approximately 10,660 kg"]
+[2.832282304763794, -1.6096974611282349, "Satellite Salinity Measurement Mission Ongoing"]
+[5.012950420379639, -4.521842956542969, "Satellite Science Team Meeting Nov. 11-14, 2014"]
+[5.048046588897705, -4.564178466796875, "Satellite IGARSS Proceedings July 13-18, 2014"]
+[4.880777835845947, -4.384683132171631, "Satellite Soil Moisture Maps July 7, 2014"]
+[-2.8204119205474854, 8.951153755187988, "Conditioning and Amplifying Module Function Conditioning and amplifying the transmit chirp, hosting and distributing the instrument Ultra Stable Oscillator"]
+[-2.7034413814544678, 8.73841667175293, "Module Function Conditioning the radar echoes prior to injecting them in the DGRs"]
+[-1.961759090423584, 8.8264799118042, "Electromechanical Coaxial Switches Redundancy Concept 5 out of 6 redundancy concept is applied for the RXMs and DGRs"]
+[-1.8761870861053467, 8.131248474121094, "System Components Active Antenna Panels, Transmit Receive Modules (TRMs), Radio Frequency Distribution Network (RFDN), Mechanisms"]
+[0.5657399892807007, -1.4028193950653076, "Satellite Orbit Altitude ~400 km"]
+[0.7538058757781982, -2.239739418029785, "Satellite Orbit Inclination 51.6\u00ba"]
+[11.197138786315918, 5.3927459716796875, "CubeSat Deployer Deployment Time May 16, 2016"]
+[-2.7107300758361816, 4.275746822357178, "Space Station Module Deployment Time 10:05 UTC"]
+[-2.7454674243927, 4.30133056640625, "Space Station Module Deployment Time 14:40 UTC"]
+[5.833302974700928, 14.375462532043457, "Transponder Frequency 1544 MHz"]
+[5.835155963897705, 14.375178337097168, "Transponder Operation Independent GPS-III payload"]
+[-1.7829830646514893, 8.175481796264648, "Subsystems Management Responsibility NASA/ARC"]
+[6.3462347984313965, 7.386254787445068, "Satellite Component Design, Fabrication, and Testing Responsibility NASA Ames"]
+[0.44345375895500183, 4.541665077209473, "Natural Phenomenon Annual Minimum 2.6 million km2"]
+[0.48062992095947266, 4.513576030731201, "Natural Phenomenon 1981\u20132010 Average 2.8 million km2"]
+[0.45784884691238403, 4.534561634063721, "Natural Phenomenon Second-Lowest Minimum Extent Unknown"]
+[0.4640671908855438, 4.539721965789795, "Natural Phenomenon Energy Absorption 90 percent of the Sun\u2019s energy"]
+[0.4725431799888611, 4.540086269378662, "Natural Phenomenon Energy Reflection 80 percent of the Sun\u2019s energy"]
+[11.428929328918457, 5.657006740570068, "CubeSat Deployment Gap 3 hours plus"]
+[11.27643871307373, 5.509551048278809, "CubeSat TLE Availability Within 12 hours of deployment"]
+[11.250341415405273, 5.491588592529297, "CubeSat First Contact Attempt 22 November 2017 at 00:39 UTC"]
+[11.343965530395508, 5.581154823303223, "CubeSat Successful Contact Approximately 90 minutes later"]
+[-1.5061931610107422, 8.595267295837402, "Electronic Component Breakdown Voltage 356 V"]
+[6.317978382110596, 7.43919563293457, "Satellite Component Output Potential Fluctuates between 250 and 310 V"]
+[-2.883151054382324, 4.137763977050781, "Spacecraft Rotation Speed Less than 1\u00ba/s"]
+[-3.009056329727173, 4.226781368255615, "Spacecraft Minimum Resolution 1\u00ba/s"]
+[-3.1464293003082275, 4.252247333526611, "Spacecraft Attitude Data Sampling Rate 1 sample every 10 minutes"]
+[2.014543294906616, 22.304088592529297, "Instrument Measurement Interval 70 cm"]
+[1.9270799160003662, 22.316650390625, "Instrument Measurement Interval 170 m"]
+[2.4751482009887695, 22.755884170532227, "Instrument Number of Beams 6"]
+[5.371134281158447, -4.427245140075684, "Satellite Launch Date September 15th 2019"]
+[2.6321871280670166, -2.213902711868286, "Satellite Launch Location Vandenberg Air Force Base in California"]
+[2.3404932022094727, -1.4928408861160278, "Satellite Multispectral Data Parameter Value Unknown"]
+[-1.9219715595245361, 8.06773853302002, "Forecasting System Maturity Not Mature"]
+[2.2996184825897217, -0.936781108379364, "Satellite Remote Sensing Reality Becoming"]
+[-1.252798080444336, 6.819139003753662, "Technology Expertise Based on space technology"]
+[-4.425103664398193, 7.418036460876465, "Data Transmission System Uplink Frequency S-band"]
+[-4.3785481452941895, 7.354933261871338, "Data Transmission System Downlink Frequency L-band"]
+[-3.793823719024658, 6.957634925842285, "Data Collection System Data Transmission In-situ environmental sensor data"]
+[-3.789560317993164, 6.968814849853516, "Data Collection System Command Transmission GOES-R antennas at WCDAS"]
+[-2.7885658740997314, 15.26561164855957, "Microwave Radiometer Channels 7"]
+[-2.827794313430786, 15.24400806427002, "Microwave Radiometer Frequencies 4"]
+[-2.816218376159668, 15.241483688354492, "Microwave Radiometer Measurement Parameters Sea surface winds, rain rates, cloud water, precipitation, soil moisture, ice edge, and ice age"]
+[-2.813055992126465, 15.247413635253906, "Microwave Radiometer Swath Width 1400 km"]
+[2.0930120944976807, 22.650978088378906, "Instrument Wavelength Range 450-1000 nm"]
+[1.7906907796859741, 22.174081802368164, "Instrument Spatial Resolution Approximately 60 m"]
+[2.376549482345581, 23.212535858154297, "Instrument Frame Rate 500 Hz"]
+[1.9639737606048584, 22.243606567382812, "Instrument Detector Size 1084 x 1024 pixels"]
+[1.8900275230407715, 22.402191162109375, "Instrument Pixel Size 10.8 \u00b5m"]
+[-0.5348429083824158, 1.2285345792770386, "Satellite Orbit Longitude 75\u00ba W and 137\u00ba W (and possible 105\u00ba W for reduced operations)"]
+[-1.0058590173721313, 9.76763916015625, "Rocket Type EELV medium"]
+[-3.142550230026245, 2.2649142742156982, "Mission Parameter Year 2015"]
+[-0.9829400777816772, -9.97489070892334, "Satellite Constellation Number of Spacecraft 1 spacecraft cluster at each orbital slot"]
+[-8.532176971435547, 13.676870346069336, "Mission Parameter Value > 0.82"]
+[-3.1435484886169434, 2.3032710552215576, "Mission Parameter Years Data and products until year 2030"]
+[4.829741954803467, -2.4930856227874756, "Satellite Years 15 years (10 operational, after 5 years on-orbit spare)"]
+[-5.127858638763428, 7.876896381378174, "Communication System Data Rate Collect and transmit up to 100 Mbit/s"]
+[-5.30925989151001, 7.721807956695557, "Communication Function Data Rate Up to 31 Mbit/s"]
+[-3.0359461307525635, 2.4329993724823, "Mission Function Services Search & Rescue, Data Collection, Emergency Manager\u2019s Weather Information Network (EMWIN)"]
+[-2.6854357719421387, 4.333776473999023, "Space Station Module Source Tank Content Liquid methane"]
+[-2.6200807094573975, 4.333560466766357, "Space Station Module Receiver Tank Content Empty"]
+[-1.0188359022140503, 8.151480674743652, "Robotic Arm Number of Primary Tools 3"]
+[-7.5483551025390625, 5.9049787521362305, "Robotic Camera Purpose Monitor the process"]
+[-0.40690767765045166, 8.008662223815918, "Substance Boiling Point Extremely low"]
+[-0.37736883759498596, 7.930747032165527, "Substance Boil Off Occurs over time"]
+[-0.31689274311065674, 8.016222953796387, "Substance Behavior in Microgravity Bubbles don't rise to the top"]
+[2.1724181175231934, -1.7218949794769287, "Satellite Instrument Operation Modes Survey mode, Event mode"]
+[2.593493938446045, 23.182695388793945, "Instrument Memory Capacity Includes memory to store high resolution data for a time interval including the event detection time"]
+[-6.6983113288879395, 9.96696662902832, "Antenna Purpose Maintain a radio link between the two satellites"]
+[-6.713939189910889, 9.988197326660156, "Antenna Mission Maintain an artificial eclipse of the Sun"]
+[-0.9469603300094604, -10.01237964630127, "Satellite Constellation Resolution Less than one-meter"]
+[1.3600833415985107, -3.0622918605804443, "Satellites Imaging Resolution 35 cm at nadir, 50 cm on average"]
+[1.384271502494812, -3.1252288818359375, "Satellites Additional Features Infrared sensors, inter-satellite links, on-board data processing enabled by artificial intelligence"]
+[-1.3292349576950073, 6.111821174621582, "Company Third-Quarter Revenue $7.9 million"]
+[-1.3393771648406982, 6.094070911407471, "Company Third-Quarter Operating Loss $48.9 million"]
+[-1.3439151048660278, 6.111688137054443, "Company Cash on Balance Sheet $198 million"]
+[5.8331427574157715, 14.37584114074707, "Transponder Frequency Band X-band"]
+[-0.7174999117851257, 12.4178466796875, "Proton Monitor Manufacturer Thomson & Nielsen Electronics Ltd, Canada"]
+[-0.6804884672164917, 12.40099048614502, "Proton Monitor Objective To flight-prove a monitor which measures the upset rate due to high energy protons"]
+[-0.6983720064163208, 12.393303871154785, "Proton Monitor Components Dynamic RAM"]
+[-1.922538161277771, 6.8736042976379395, "Software Lines of Source Code 201,000"]
+[-1.9242151975631714, 6.84517765045166, "Software Development Time 2.4 years"]
+[-1.9205361604690552, 6.918490409851074, "Software Primary Modes Safe and Nominal"]
+[-5.426032543182373, 2.781026601791382, "Telescope Exposure Time More than 500 seconds"]
+[-5.37558126449585, 2.8419244289398193, "Telescope Energy Spectrum 0.3\u20130.6 keV, 0.6\u20131 keV, 1\u20132.3 keV"]
+[-0.7028700113296509, 2.9765026569366455, "Supernova Remnant Observable Time About 100,000 years"]
+[-6.729018211364746, 10.001477241516113, "Antenna Material CFRP (Carbon Fiber Reinforced Plastic)"]
+[-6.707522869110107, 9.989147186279297, "Antenna Beam-Pointing Positions 61"]
+[-6.74181604385376, 10.000434875488281, "Antenna Off-Nadir Intervals ~ 9 km"]
+[-6.756590843200684, 10.018671989440918, "Antenna Size 6 m x 1 m each"]
+[-6.721365928649902, 9.97757339477539, "Antenna Quantity 126"]
+[-6.7162394523620605, 9.993476867675781, "Antenna Implication Reduces the requirement of the number of beams by half"]
+[2.0256922245025635, -1.7208685874938965, "Satellite Operating Modes SAR operating modes, including Sliding Spotlight mode"]
+[2.5923473834991455, -1.1412912607192993, "Satellite Data Utilization Agriculture, Disaster Management and other ancillary applications related to oceanography, urban mapping, forest cover"]
+[2.2824623584747314, -1.2618448734283447, "Satellite Image Generation Hybrid Polarimetric SAR image generation"]
+[5.046143531799316, -3.967611312866211, "Satellite Launch Timeframe 2018-19"]
+[2.251323938369751, -2.087108850479126, "Satellite System Specifications Virtually the same as those of RISAT-1"]
+[3.5553975105285645, 13.505477905273438, "Laser System Wavelength 532.272 nm"]
+[2.6527366638183594, 12.29626178741455, "Beam Expander Beam Widening Factor More than four times"]
+[2.7710959911346436, 12.419892311096191, "Beam Expander Purpose Make the laser beam more than four times wider"]
+[2.5648326873779297, -1.7816191911697388, "Satellite Structure Material All-aluminum"]
+[1.1433004140853882, -0.8937564492225647, "Satellite Structure Length 0.82 m"]
+[2.447787046432495, -1.8910268545150757, "Satellite Subsystems EPS (Electrical Power Subsystem, C&DH (Command and Data Handling), communications, and an attitude determination and control subsystem"]
+[0.7872785329818726, 9.136569023132324, "Orbital Motion Compensation Mechanism Purpose Compensate for orbital motion during imaging"]
+[0.7587501406669617, 9.155673027038574, "Orbital Motion Compensation Mechanism Manufacturer ESA"]
+[0.6472182273864746, 9.178977966308594, "Orbital Motion Compensation Mechanism URL http://www.astrofein.com/astro-und-feinwerktechnik-adlershof/projekte/nightpod/"]
+[1.3290475606918335, -1.9314090013504028, "Satellite SIF Products Agreement Strong, higher than 0.73"]
+[2.499997615814209, -1.1100564002990723, "Satellite SIF Data Usage GPP modeling and global carbon flux estimations"]
+[5.219354629516602, -4.386250019073486, "Satellite First Global Carbon Dioxide Maps Production Date April 13, 2018"]
+[5.093084335327148, -4.269015312194824, "Satellite Global Carbon Dioxide Maps Data Collection Dates April and July 2017"]
+[2.6640384197235107, 5.388091087341309, "Beacon Transmission Power 5 W"]
+[2.663041830062866, 5.388108730316162, "Beacon Transmission Interval Approximately every 50 seconds"]
+[2.6375958919525146, 5.399867534637451, "Personal Locator Beacon Frequency 121.5 and 406 MHz"]
+[2.6451122760772705, 5.3954315185546875, "Personal Locator Beacon Authorization Date July 1, 2003"]
+[3.711099147796631, 17.717458724975586, "Payload Components Deployer, extension mechanism"]
+[3.728482484817505, 17.699932098388672, "Payload Mechanism Mechanical two stage ejector, extension mechanism with four booms rolled into a central distributor"]
+[2.660973310470581, -2.322922706604004, "Satellite Communication Type Broadband"]
+[-0.7950705289840698, 4.800542831420898, "Satellite Station Location Kesennuma and Higashimatsushima"]
+[-5.550847053527832, 7.067000865936279, "Communication Link Establishment Date March 15"]
+[-9.983915328979492, 5.881304740905762, "Search and Rescue System Orbit Mid-Earth"]
+[-9.952468872070312, 5.859279155731201, "Search and Rescue System URL http://searchandrescue.gsfc.nasa.gov/dass/groundsystem.html"]
+[-9.952197074890137, 5.858513832092285, "Search and Rescue System URL http://www.navnin.nl/NIN/Downloads/SARl.pdf"]
+[-9.918402671813965, 5.886420726776123, "Search and Rescue System URL http://tinyurl.com/k82lepc"]
+[-9.954026222229004, 5.856204032897949, "Search and Rescue System URL http://searchandrescue.gsfc.nasa.gov/dass/spacesegment.html"]
+[-9.955131530761719, 5.8543009757995605, "Search and Rescue System URL http://searchandrescue.gsfc.nasa.gov/dass/index.html"]
+[-0.1208580732345581, 15.563718795776367, "Spectrometer Spectral Range 303 - 714 cm -1 (3.3 - 14.7 \u00b5m)"]
+[-0.10777360945940018, 15.56326675415039, "Spectrometer Nr. of Samples Band 1: 1.6 x 10 5 ; band 2 & 3: 1.0 x 10 5"]
+[-0.20343180000782013, 15.604926109313965, "Spectrometer Spectral Resolution < 0.15 cm -1 (band 3); <0.25 cm -1 (band 2)"]
+[-0.13324464857578278, 15.621382713317871, "Spectrometer Measurement Stability < 0.43 K (band 3); <1.59 K (band 2), < 1.58 K (band 1)"]
+[-0.10461392998695374, 15.555281639099121, "Spectrometer Data Rate 882 kbit/s"]
+[-0.06102386862039566, 15.493414878845215, "Spectrometer Mass 130 kg"]
+[-0.13574351370334625, 15.582225799560547, "Spectrometer Power 150 W"]
+[-0.12220951914787292, 15.57071304321289, "Spectrometer Size 1150 mm x 930 mm x 650 mm"]
+[-4.584451675415039, 12.031499862670898, "Magnetometer Measurement Space environment magnetic field"]
+[-4.510498523712158, 12.104523658752441, "Magnetometer Resolution 0.016 nT"]
+[-4.499807834625244, 12.11638355255127, "Magnetometer Response Frequency 2.5 Hz"]
+[-4.587235450744629, 12.192376136779785, "Magnetometer Manufacturer Lockheed Martin"]
+[-4.492245674133301, 12.081771850585938, "Magnetometer Mounting Boom mounted on GOES-R"]
+[-5.4417643547058105, 2.8127100467681885, "Telescope Camera Height 80 cm"]
+[-5.41864538192749, 2.8555474281311035, "Telescope Camera Aperture 12 cm"]
+[-5.394935131072998, 2.847917079925537, "Telescope Camera Image Acquisition Frequency Every 25 seconds"]
+[-5.413456916809082, 2.8313560485839844, "Telescope Camera CCDs per Camera 4"]
+[-5.374557971954346, 2.872683048248291, "Telescope Camera Image Resolution 20.3 megapixels"]
+[-5.508100986480713, 3.004728078842163, "Telescope Camera Total Spacecraft Image Resolution 2.11 gigapixels"]
+[-3.6099722385406494, 7.051724910736084, "Data Fusion Platform Key Features Ease of use, Rapid revisit, Affordability"]
+[-0.9395381808280945, -10.012405395507812, "Satellite Constellation Revisit Rate Hourly"]
+[0.5686934590339661, -1.46550714969635, "Satellite Orbit Altitude 690 km"]
+[1.4511598348617554, -1.047788143157959, "Satellite Image Resolution ~2 m/pixel"]
+[1.1890581846237183, -1.2527154684066772, "Satellite Image Span 10 km x 3 km"]
+[2.5682272911071777, -2.2133948802948, "Satellite Signal Transmission Galileo spreading codes"]
+[-4.977100849151611, 9.801204681396484, "Receiver Reception Stability Stable"]
+[2.4972422122955322, -2.0537660121917725, "Satellite Signal Transmission L1+E5 or L1+E6"]
+[2.552635669708252, -2.0143344402313232, "Satellite Navigation Message Not representative from structure and contents viewpoint"]
+[-0.447190523147583, 0.20866307616233826, "Satellite Navigation System Agreement Date June 26, 2004"]
+[1.363763689994812, 10.544873237609863, "Imaging System Spectral Bands 6 bands in the Visible (VIS) and Infrared (IR)"]
+[1.3688286542892456, 10.558099746704102, "Imaging System Spatial Resolution 1 km"]
+[1.3478763103485107, 10.54002857208252, "Imaging System Swath Width 2800 km"]
+[-7.570271015167236, 5.8870368003845215, "Pushbroom Cameras Spectral Range Visible and near-infrared (VNIR)"]
+[-7.547317028045654, 5.910013675689697, "Pushbroom Cameras Spatial Resolution 60 - 120 m"]
+[-7.589107990264893, 5.867787837982178, "Pushbroom Cameras Swath Width 940 - 960 km"]
+[1.6283947229385376, 21.935354232788086, "Instrument Swath Width 1500 km"]
+[1.7419995069503784, 22.056161880493164, "Instrument Horizontal Spatial Resolution 16 - 198 km"]
+[1.8380647897720337, 22.10173797607422, "Instrument Vertical Spatial Resolution 1.5 - 7 km"]
+[1.6957064867019653, 21.992534637451172, "Instrument Swath Width 450 - 600 km"]
+[1.782626748085022, 22.1558837890625, "Instrument Spatial Resolution 400 - 1000 m"]
+[0.7242830991744995, -1.170228123664856, "Satellite Altitude 825 km"]
+[0.668855607509613, -2.3100526332855225, "Satellite Inclination 98.8\u00b0"]
+[4.008291721343994, -3.146895408630371, "Satellite Local Time on Ascending Node (LTAN) 0930 hours"]
+[3.987750768661499, -2.892760753631592, "Satellite Period 101.41 minutes"]
+[-0.7166162729263306, 3.174192428588867, "Neutron Star System X-ray Output Varies"]
+[-0.741218090057373, 3.18245267868042, "Neutron Star System Brightness Fluctuations Observed"]
+[1.9187570810317993, 10.715646743774414, "Imaging Device Field of View Overlapping"]
+[1.8831573724746704, 10.751322746276855, "Imaging Device Sample Rate 25 seconds"]
+[1.9091949462890625, 10.718348503112793, "Imaging Device Sample Frequency Every 2.5s"]
+[-2.9833991527557373, 4.2107062339782715, "Spacecraft Pointing Stability High"]
+[-3.3412461280822754, 4.225045680999756, "Spacecraft Observation Duration One to two years"]
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+[-3.159594774246216, 5.092309474945068, "Resupply Vehicle Departure from Space Station Unknown"]
+[-3.1582460403442383, 5.058518886566162, "Resupply Vehicle End of Mission Unknown"]
+[-3.8544225692749023, 3.7180047035217285, "Mars Rover Sample Tubes 43"]
+[-3.859469413757324, 3.716057777404785, "Rover Wheels Designed by engineers at NASA\u2019s Glenn Research Center in Cleveland, Ohio"]
+[-0.9584499001502991, 9.818066596984863, "Rocket Design Center NASA\u2019s Marshall Space Flight Center in Huntsville, Alabama"]
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+[14.545785903930664, 7.601583957672119, "Nanosatellite Water Ice Deposits Unknown"]
+[2.033752679824829, -1.5746910572052002, "Satellite Modes Standard, Wide, Low incidence, High incidence, Fine, ScanSAR wide, ScanSAR narrow"]
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+[1.5977033376693726, -1.1895204782485962, "Satellite Spatial Resolution 250-750 m, 250-650 m, 125-300 m, 750-1000 m, 525-750 m, 250-750 m, 300-720 m, 250-600 m, 400-600 m, 400-750 m, 400-550 m"]
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+[-0.9089815020561218, 12.227763175964355, "Surface Charging Monitor Measurement Potential"]
+[-0.9114178419113159, 12.15401840209961, "Surface Charging Monitor Composition Flour-polymer resin over a copper substrate"]
+[-0.946025013923645, 12.164433479309082, "Surface Charging Monitor Voltage 300 V"]
+[-0.9550268054008484, 12.098548889160156, "Surface Charging Monitor Potential 300 V"]
+[3.175438404083252, 22.968246459960938, "Instrument Status Fully functional"]
+[3.213992118835449, 22.998767852783203, "Instrument Status Fully functional"]
+[3.201016426086426, 22.97504997253418, "Instrument Status Fully functional"]
+[3.190216541290283, 22.976490020751953, "Instrument Status Fully functional"]
+[3.147622585296631, 22.899402618408203, "Instrument Status Functional with limitations"]
+[-1.1806297302246094, 7.778253078460693, "Device Status Functional"]
+[-1.079351782798767, 7.619654655456543, "Device Status Functional"]
+[-1.076216697692871, 7.7083210945129395, "Device Status Functional"]
+[-5.884287357330322, 16.007022857666016, "X-band Synthetic Aperture Radar Resolution Up to 400 m"]
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+[-4.5074357986450195, 15.925558090209961, "Radar Data Collection Ongoing"]
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+[-0.603361189365387, 6.178600311279297, "Event Date 1-5 October 2018"]
+[-0.9756342172622681, 6.618084907531738, "Paper URL https://iafastro.directory/iac/proceedings/IAC-18/IAC-18/C1/5/manuscripts/IAC-18,C1,5,10,x47313.pdf"]
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+[-9.954546928405762, 5.850736141204834, "Search and Rescue Concept Development Initiative LunaNet"]
+[-9.954962730407715, 5.850645065307617, "Search and Rescue Operations Year 2021"]
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+[-5.383735179901123, 2.794633626937866, "Telescope Capability Pinpointing the location of the radioactivity, creating maps"]
+[-5.447173118591309, 2.7108967304229736, "Telescope Capability Seeing high-energy X-ray light from the decay of titanium-44"]
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+[-0.3824007511138916, 6.4673004150390625, "Ground-based Test Bed Capability Receive the Galileo bands E6, E5a,b and L1 in full bandwidth"]
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+[8.49090576171875, 15.221566200256348, "Camera Mount Compatible Physical Lengths Unknown"]
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+[-0.8531370759010315, 12.682327270507812, "Radiation Monitor Objective To map the radiation environment of GTO with high temporal and spatial resolution at post-solar minimum conditions"]
+[-0.8879141807556152, 12.626039505004883, "Radiation Monitor Detected Particles Electrons, protons, and cosmic rays"]
+[-0.8483463525772095, 12.667129516601562, "Radiation Monitor Measurement Principle Examining the sizes of charge pulses generated by charged particles in silicon diodes polarized in reverse by a high voltage"]
+[-0.8244146704673767, 12.667847633361816, "Radiation Monitor Diode Configuration Two of the three diodes are in-line and operate in `coincidence'"]
+[-0.8602664470672607, 12.692394256591797, "Radiation Monitor Radiation Dose Measurement Measures the total radiation dose encountered by SREM itself and at different remote locations onboard the satellite, by using RADFETS"]
+[-2.9333512783050537, 4.237727642059326, "Spacecraft Controller Monitoring Function Spacecraft's status in telemetry as well as the state of the ground components"]
+[-1.0605827569961548, 7.672067642211914, "Device Monitoring Not specified"]
+[-1.9258224964141846, 14.885879516601562, "Radiometer System Integration Time 0.24 s"]
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+[3.5269968509674072, 13.695328712463379, "Laser Ranging System Wavelength Stability Excellent"]
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+[-4.509432315826416, 12.122244834899902, "Scalar Magnetometer Measurement Principle Proton magnetic resonance"]
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+[-4.508883476257324, 12.12363052368164, "Scalar Magnetometer Sampling Rate 1 Hz"]
+[-4.508594036102295, 12.126693725585938, "Scalar Magnetometer Deviation from Omni-directionality Less than 0.2 nT"]
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+[-1.9222875833511353, 14.870980262756348, "Radiometer Scan Components Cold reading, warm load reading, and the scene stations"]
+[-3.1796796321868896, 14.604207992553711, "Microwave Imager On-orbit reference standard for calibrating precipitation measurements Unknown"]
+[-2.9845404624938965, 4.353356838226318, "Spacecraft Based on the Ball Configurable Platform Proven, agile spacecraft with 50 years of on-orbit operations for affordable remote sensing applications"]
+[5.243747234344482, -4.028609752655029, "Satellite Launch Year 2011"]
+[5.291479587554932, -3.831602096557617, "Satellite Launch Year 2017"]
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+[11.26783275604248, 5.521108627319336, "CubeSat Mission Results Presentation Date August 6-11, 2016"]
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+[-0.4105689227581024, 5.066027641296387, "River Water Level 5 meters below normal"]
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+[5.187521457672119, -4.3602294921875, "Satellite Delayed Launch Date Mid-December 2013"]
+[-5.325287818908691, 7.530392169952393, "Communication Protocol Real-time telemetry delivery Yes"]
+[-5.292752742767334, 7.551237106323242, "Communication Protocol Reliable file transfer Yes"]
+[-5.288162708282471, 7.474747657775879, "Protocol Onboard clock synchronization Yes"]
+[-5.318224906921387, 7.518873691558838, "Communication Protocol Send UDP command packets to LPT over one-way uplink without Mobile IP or a two-way link Yes"]
+[-5.305144786834717, 7.525963306427002, "Communication Protocol Perform reliable file transfer over both two-way and one-way communication links Yes"]
+[0.014302932657301426, 13.546614646911621, "Acceleration Measurement Device Frequency Range Low"]
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+[-1.3922091722488403, 15.00017261505127, "Infrared Spectral Imaging Radiometer Device Type Radiometer"]
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+[-5.360045433044434, 2.9871649742126465, "Optical Telescope Assembly Lens Assembly Custom 5-element refractive design"]
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+[-0.07069797813892365, 7.602187633514404, "Nanopositioning Stage Model Modified version of the off-the-shelf P-733.2CD"]
+[1.613289475440979, 2.2582857608795166, "Geostationary Satellite Image Capture Time Around noon on August 20, 2020"]
+[0.4651973247528076, 4.5032453536987305, "Environmental Phenomenon Harmful Effects Degrade air quality, cause breathing and lung problems, contribute to heart disease and cancer"]
+[-2.937192916870117, 4.543899059295654, "Spacecraft Cargo Capacity 3,350 kg"]
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+[-2.2752559185028076, 2.833233118057251, "Spaceborne Gravitational Wave Observatory Number of Spacecraft 3"]
+[-2.2631144523620605, 2.866741418838501, "Spaceborne Gravitational Wave Observatory Spacecraft Separation 2.5 million kilometers"]
+[-2.2740862369537354, 2.8328943252563477, "Spaceborne Gravitational Wave Observatory Resolution Ten times smaller than an atom"]
+[-2.2622158527374268, 2.8367116451263428, "Spaceborne Gravitational Wave Observatory Feasibility Study Phase End Date January 2020"]
+[-4.229673385620117, 9.108695983886719, "Digital Chirp Generator Chirp Parameters 2-75 MHz"]
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+[-4.222918510437012, 9.115217208862305, "Digital Chirp Generator Amplitude 10 bit"]
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+[-4.257755279541016, 9.122400283813477, "Digital Chirp Generator Size 260 mm x 210 mm x 150 mm"]
+[-4.23293924331665, 9.11886215209961, "Digital Chirp Generator Mass 4 kg"]
+[-4.232707500457764, 9.110976219177246, "Digital Chirp Generator Power 4.5 W"]
+[-3.6253321170806885, 7.614728927612305, "Data Acquisition and Compression Subsystem ADC 8 I+8Q @ 20.8 - 250 MHz sampling rate"]
+[-3.640449047088623, 7.627749919891357, "Data Acquisition and Compression Subsystem Onboard Compression 2-6 bit BAQ"]
+[-3.6556057929992676, 7.6050944328308105, "Data Acquisition and Compression Subsystem Sensor Data Rate (max) 326 Mbit/s (6 bit BAQ), 1562 Mbit/s (3 bit BAQ)"]
+[-3.6271657943725586, 7.606115818023682, "Data Acquisition and Compression Subsystem Size 260 mm x 210 mm x 150 mm"]
+[-3.6298654079437256, 7.612644672393799, "Data Acquisition and Compression Subsystem Mass 4.6 kg"]
+[-3.6600077152252197, 7.612219333648682, "Data Acquisition and Compression Subsystem Power 27 W"]
+[3.725193738937378, 17.69582176208496, "Payload Controller Timing 2800-3700 Hz PRF (Pulse Repetition Frequency); 58-184 \u00b5s of data collection window"]
+[3.701955795288086, 17.667396545410156, "Payload Controller Interfaces MIL-STD-1553B @ 1 Mbit/s with bus BMU"]
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+[3.720858573913574, 17.7025146484375, "Payload Controller Power 15 W"]
+[-1.8946393728256226, 8.660714149475098, "Tile Digital Electronics No of Elevation Beams 126"]
+[-1.8893471956253052, 8.59646987915039, "Tile Digital Electronics TRM Phase/Amp Update Rate 18 \u00b5s @ PRF rate"]
+[-1.9178345203399658, 8.603087425231934, "Tile Digital Electronics Device Size 380 mm x 60 mm x 90 mm, 173 mm x 18.5 mm x 81 mm"]
+[-1.9188358783721924, 8.497188568115234, "Tile Digital Electronics Device Mass 2 kg, 0.2 kg"]
+[-1.9317353963851929, 8.592223167419434, "Tile Digital Electronics Device Power 3 W, 1.5 W"]
+[-5.695394039154053, 15.93873119354248, "Quicklook Processor/Near Real-time SAR Processor SAR Image Parameters Resolution: 1-12 m (ground range) x 1-48 m (azimuth)"]
+[-5.66335916519165, 15.912887573242188, "Quicklook Processor/Near Real-time SAR Processor Limited Swath 4096 range gates, 15-240 km in width"]
+[-5.729525566101074, 15.951191902160645, "Quicklook Processor/Near Real-time SAR Processor Full Swath 20 k range gates, 30-240 km in width"]
+[-5.682140827178955, 15.925546646118164, "Quicklook Processor/Near Real-time SAR Processor Throughput Real-time (QLP) to max 45 minutes (NRTP) per scene, 10-15 GFLOPS"]
+[-5.682196617126465, 15.930974006652832, "Quicklook Processor/Near Real-time SAR Processor Device Parameters 8-14 slot cPCI chassis, PE SBC, 96 Tiger SHARC DSP @ 250 MHz, 700 W, 20 kg"]
+[-2.2540485858917236, 2.8387818336486816, "Gravitational Wave Observatory Purpose Study gravitational waves produced by merging stellar mass black holes, supermassive black holes, white dwarfs, neutron stars, or small black holes"]
+[-2.262397050857544, 2.8368871212005615, "Gravitational Wave Observatory Hardware Test masses, measurement devices, lasers"]
+[-2.2723748683929443, 2.831284761428833, "Gravitational Wave Observatory Prototype Laser Delivery Date May, 2021"]
+[2.826390504837036, 14.245088577270508, "Laser Instrument Purpose Detect the telltale ripples in gravitational fields caused by the mergers of neutron stars, black holes, and supermassive black holes in space"]
+[1.4414443969726562, 2.760251760482788, "Weather Satellite Launch Date Unknown"]
+[1.451812982559204, 2.7570226192474365, "Weather Satellite URL https://en.wikipedia.org/wiki/Meteor-M_No.2-1"]
+[2.1013219356536865, -2.727973461151123, "Satellite Number of Satellites 2"]
+[-0.9539654850959778, -10.006266593933105, "Satellite Constellation Number of Satellites 72"]
+[-0.9748541712760925, -9.981430053710938, "Satellite Constellation Number of Planned In-Orbit Spares 3"]
+[-0.958652675151825, -9.99647331237793, "Satellite Constellation Number of Launches 7"]
+[11.152995109558105, 5.264415264129639, "CubeSat Mass 1 kg"]
+[11.087153434753418, 5.230030536651611, "CubeSat Mass 4 kg"]
+[11.17037296295166, 5.289667129516602, "CubeSat Mass 4.2 kg"]
+[0.7438087463378906, -1.2028297185897827, "Satellite Altitude 400 km"]
+[0.6898124814033508, -2.293729305267334, "Satellite Inclination 51.6\u00ba"]
+[-5.327576637268066, 8.010774612426758, "Communication System Frequency Band S-band"]
+[-5.218912124633789, 7.837181568145752, "Communication System Data Downlink Speed > 100 Mbit/s"]
+[-3.8667280673980713, 7.92876672744751, "Data Storage Capacity 8 GB + 32 GB of science data"]
+[0.7055894732475281, -4.138625144958496, "Satellite Launch Mass ~ 450 kg"]
+[5.295535564422607, -2.2047383785247803, "Satellite Design Life 5 years"]
+[4.910651683807373, -2.4275264739990234, "Satellite Goal Life 7 years"]
+[3.4878029823303223, 13.418155670166016, "Laser Transmitter Development Date July 23-27, 2018"]
+[-1.2982256412506104, 6.503395080566406, "Workshop Date May-June 2014"]
+[-2.1815950870513916, 5.88981819152832, "Flight Date 23 October 2018"]
+[-6.52215051651001, 9.882341384887695, "Multi-Antenna Receiver Purpose Test the signal array processing technology for mitigation and detection of radio interference in receivers of satellite navigation systems"]
+[-6.598202705383301, 9.889288902282715, "Multi-Antenna Receiver Technology Digital beamforming (DBF)"]
+[-6.487020015716553, 9.809521675109863, "Multi-Antenna Receiver Design Requirement Provides access to each part in the receiver to take appropriate counter measures against almost any kind of interference and jamming"]
+[3.712841272354126, 17.684343338012695, "Payload Location Nadir plate of the satellite close to the center of gravity"]
+[-0.8214511871337891, 12.644817352294922, "Radiation Environment Measurement Unit Location Outside, on the front panel"]
+[-0.7389928698539734, 8.8659029006958, "Thermal Control Subsystem Design Incorporates passive and active elements"]
+[-2.3163914680480957, 9.086922645568848, "Electrical Power System Manufacturer GER/NL/IT/USA"]
+[-2.363035202026367, 7.293636798858643, "Onboard Computer Manufacturer SWE"]
+[-1.6001243591308594, 8.83311653137207, "Reaction Control System Manufacturer UK"]
+[-3.3880083560943604, 8.551078796386719, "Mass Memory and Formatting Unit Manufacturer IT"]
+[2.6425585746765137, 13.93177604675293, "Optical Linescan System Resolution 2.77 km"]
+[2.612116575241089, 13.927607536315918, "Optical Linescan System Resolution 0.55 km"]
+[2.6081960201263428, 13.845483779907227, "Optical Linescan System Data Rate Decrease Factor of 25"]
+[2.6440842151641846, 13.94206714630127, "Optical Linescan System Sensing Capability View clouds by moonlight"]
+[2.6062586307525635, 13.861892700195312, "Optical Linescan System Sensing Capability Capture city lights and distinguish lights from fires"]
+[2.595648765563965, 13.895292282104492, "Optical Linescan System Viewing Capability Nighttime cloud viewing at a lower resolution than daytime visible fine-mode data"]
+[2.894902229309082, -1.5204477310180664, "Satellite Mission Description Aerotecnica Missili & Spazio, The Journal of Aerospace Science, Technology and Systems, Vol. 97, No.3 July-September 2018, pp 135-144"]
+[1.2463269233703613, -2.283433675765991, "Geodetic Satellite Thermal-optical design for one millimeter accuracy Advances in Space Research, Volume 65, Issue 10, 2020, Pages 2276-2289"]
+[-6.70722770690918, 10.660826683044434, "Retroreflector Array Transfer Function Not specified"]
+[1.585817813873291, 2.32112455368042, "Geostationary Operational Environmental Satellite Operation Agency NOAA"]
+[1.592777132987976, 2.288731098175049, "Geostationary Operational Environmental Satellite Image Acquisition Date September 14, 2020"]
+[0.4707496762275696, 4.519369125366211, "Natural Phenomenon Likelihood to Stall Increasing due to global warming signals"]
+[0.45195311307907104, 4.525965690612793, "Natural Phenomenon Acres Burned More than 300,000 acres (1,200 km2)"]
+[7.361281394958496, 12.46704387664795, "Satellite Instrument Problem Unknown"]
+[1.5495238304138184, 2.435835123062134, "Geostationary Weather Satellite Operational Role Start Date Unknown"]
+[0.6347945332527161, 4.2299981117248535, "Atmospheric Phenomenon Lead Time 10 minutes or more"]
+[-1.3497670888900757, 6.9752655029296875, "3D Model Derivative Datasets Digital Surface Model (DSM), Digital Terrain Model (DTM), and 3D Vectors"]
+[-3.4646544456481934, 6.856754302978516, "Information Source Use Cases 5G signal propagation, autonomous vehicles, smart cities and internet of things (IoT), guided munitions and disaster response planning and mitigation"]
+[-13.861815452575684, -2.2429935932159424, "X-ray Telescope Function Identify black holes and neutron stars"]
+[-1.171688437461853, 3.0637800693511963, "Celestial Objects Size Typically only the size of a large city"]
+[-1.1663700342178345, 3.0641863346099854, "Celestial Objects Weight A teaspoon of one would weigh about a billion tons on Earth"]
+[-1.1670178174972534, 3.071352481842041, "Celestial Object Energy Beams with the energy of 10 million Suns"]
+[2.1262471675872803, -0.9780263900756836, "Satellite Sensor Data Collection Frequency Every 10-15 minutes"]
+[1.8630293607711792, -2.1753437519073486, "Satellite Orbit Geostationary"]
+[-1.59121835231781, 9.30070972442627, "Carbon Sink Function Draws carbon out of the atmosphere and stores it in plant matter or the soil"]
+[2.6245603561401367, -1.3678730726242065, "Satellite Data Source Exoplanet discovery"]
+[-5.319376468658447, 2.8409814834594727, "Telescope Data Source Exoplanet discovery"]
+[-0.7648082375526428, 3.1895079612731934, "Star System Planet Size About as large as Neptune"]
+[-0.7426502108573914, 3.20432710647583, "Star System Planet Orbit Just over a week"]
+[-13.979901313781738, -2.289872407913208, "X-ray Telescope Image Detail High"]
+[-13.876267433166504, -2.1263985633850098, "X-ray Telescope Energy Range 20 to 40 keV"]
+[-5.286168575286865, 2.8613975048065186, "Infrared Telescope Background Picture Captured in infrared light"]
+[-13.905845642089844, -2.2295479774475098, "X-ray Telescope Mission ESA"]
+[-3.847541332244873, 15.716615676879883, "Active Microwave Radar Look Angle 40\u00ba and 46\u00ba from nadir"]
+[-3.8680858612060547, 15.713770866394043, "Active Microwave Radar Antenna Diameter 1 m"]
+[-3.84548282623291, 15.710630416870117, "Active Microwave Radar Operating Frequency 13.402 GHz"]
+[-3.890247344970703, 15.74045181274414, "Active Microwave Radar Wind Speed Measurement Range 3-20 m/s"]
+[-3.8911948204040527, 15.731672286987305, "Active Microwave Radar Wind Speed Measurement Accuracy 2 m/s"]
+[-3.858872413635254, 15.719799041748047, "Active Microwave Radar Wind Vector Direction Accuracy 20\u00ba"]
+[-3.8658244609832764, 15.719194412231445, "Active Microwave Radar Antenna Rotation Speed 18 rpm"]
+[-3.873507261276245, 15.710920333862305, "Active Microwave Radar Data Swath Continuous 1800 km swath, centred about nadir"]
+[-3.850515127182007, 15.731836318969727, "Active Microwave Radar Spatial Resolution 50 km"]
+[-3.8599278926849365, 15.71980094909668, "Active Microwave Radar IFOV \u00b152\u00ba from nadir"]
+[-3.858015775680542, 15.7232027053833, "Active Microwave Radar Mass 205 kg"]
+[-3.8550240993499756, 15.720519065856934, "Active Microwave Radar Power 250 W"]
+[-3.852849006652832, 15.719707489013672, "Active Microwave Radar Duty Cycle 100%"]
+[-3.8603365421295166, 15.722550392150879, "Active Microwave Radar Average Data Rate 40 kbit/s"]
+[-3.8606317043304443, 15.715362548828125, "Active Microwave Radar Thermal Operating Range 5-40\u00baC"]
+[-3.8616881370544434, 15.725606918334961, "Active Microwave Radar Pointing Knowledge 500 arcseconds"]
+[-3.578596353530884, 4.4088873863220215, "Spacecraft Berthing Date November 19, 2018"]
+[-1.3446654081344604, 6.111173629760742, "Company Triple-Altitude Delivery Yes"]
+[0.9594718813896179, -1.501051664352417, "Satellite Target Stars Distance Less than 300 light-years"]
+[1.8984920978546143, -1.520827293395996, "Satellite Target Stars Brightness 30-100 times brighter than those surveyed by the Kepler satellite"]
+[2.268510103225708, -1.5185821056365967, "Satellite Follow-up Observations Spectroscopy"]
+[2.330883026123047, -1.4364477396011353, "Satellite Follow-up Observations Study of the absorption and emission of light"]
+[2.2347476482391357, -1.4242900609970093, "Satellite Follow-up Observations Refine Measurements of Planet Masses, Sizes, Densities, and Atmospheric Properties"]
+[0.1192045733332634, 7.223804950714111, "Experiment Operation June 1998"]
+[0.11032726615667343, 7.190260410308838, "Experiment Operation On the International Space Station (ISS)"]
+[3.7138912677764893, 17.706069946289062, "Payload Operations and Control Center Duration Five years renewable"]
+[-1.5917962789535522, 5.433722019195557, "Science Operations Center Duration Five years renewable"]
+[0.1500183641910553, 7.214751243591309, "Experiment Collaboration 15 Countries, 44 Institutes and 600 Physicists"]
+[2.6906583309173584, 22.41472625732422, "Instrument Detector Type Teledyne H1RG HgCdTe FPA"]
+[2.6684741973876953, 22.40610122680664, "Instrument Detector Assembly JDSU LVF (Linear Variable Filter)"]
+[-0.6482152342796326, 8.592324256896973, "Cryocooler Cold Finger Temperature \u2264 115 K"]
+[8.514152526855469, 13.940630912780762, "Lidar Instrument Aerosol Types Dust, dust mixtures, smoke, marine aerosols"]
+[8.509125709533691, 13.937295913696289, "Lidar Instrument Aerosol Typing Algorithm CALIOP instrument aerosol typing algorithm"]
+[8.516681671142578, 13.942451477050781, "Lidar Instrument Observation Date February 18, 2016"]
+[-0.11384512484073639, 15.542468070983887, "Spectrometer Function Broadband spectral determination of composition and distribution of volatiles"]
+[-0.07564682513475418, 15.55900764465332, "Spectrometer Function Spectral determination of major minerals"]
+[-0.08770348876714706, 15.540218353271484, "Spectrometer Function Understanding of current dynamics of volatile sources, sinks, and processes"]
+[2.57552170753479, 14.20376205444336, "Optical Instrument Primary Mirror Diameter 30 cm"]
+[2.6335198879241943, 14.319989204406738, "Optical Instrument Image Stabilization \u00b10.1 arcsec"]
+[2.6368672847747803, 14.310370445251465, "Optical Instrument Effective Focal Length 8.66 m"]
+[2.6410694122314453, 14.317413330078125, "Optical Instrument Offset Pointing Disk center \u00b11\u00ba"]
+[2.6284313201904297, 14.301321983337402, "Optical Instrument FOV 8.5 x 8.5 arcmin"]
+[1.8770136833190918, 10.732613563537598, "Imaging Device Read-out Time 2.1 s"]
+[1.8952012062072754, 10.721013069152832, "Imaging Device Size 1024 x 1024 pixels"]
+[2.64528226852417, 14.33083438873291, "Optical Instrument Average Data Rate 3.6 Gbit/day"]
+[1.901248812675476, 10.707462310791016, "Imaging Device Pixel Size 21 x 21 \u00b5m (0.5 x 0.5 arcsec)"]
+[2.636549472808838, 14.25818920135498, "Optical Instrument Dimensions 37 x 37 x 188 cm"]
+[-0.4876224100589752, 5.8540496826171875, "Unknown Quantization 12 bit"]
+[-0.4744725525379181, 5.838961124420166, "Unknown Mass 51 kg"]
+[6.431480884552002, 7.309410572052002, "Satellite Component Issue Occasional sticking at anomalous alignment position"]
+[6.336474418640137, 7.3955206871032715, "Satellite Component Issue Slippage when the moving mirror vibrated"]
+[6.2471022605896, 7.491230487823486, "Satellite Component Issue Insufficient gain leading to induced vibration"]
+[6.414523124694824, 7.325186252593994, "Satellite Component Adjustment Related to the slippage margin"]
+[3.4915616512298584, 8.123581886291504, "X-ray Detector Energy Range 5-79 keV"]
+[3.491598606109619, 8.120043754577637, "X-ray Detector Angular Resolution (HPD) 45 arcsec"]
+[3.496950387954712, 8.12090015411377, "X-ray Detector Angular Resolution (FWHM) 9.5 arcsec"]
+[3.4958889484405518, 8.117387771606445, "X-ray Detector FOV (50% resp.) at 10 keV 10 arcmin"]
+[3.4844377040863037, 8.13319206237793, "X-ray Detector Sensitivity (6 - 10 keV) 2 x 10 -15  erg/cm 2 /s"]
+[3.492152452468872, 8.125103950500488, "X-ray Detector Background in HPD (10 - 30 keV) 6:8 x 10 -4  cts/s"]
+[3.497201919555664, 8.119280815124512, "X-ray Detector Spectral Resolution (FWHM) 500 eV at 10 keV, 1.2 keV at 80 keV"]
+[3.4840798377990723, 8.136110305786133, "X-ray Detector Strong source (> 10\u03c3) positioning 1.5 arcsec (1\u03c3)"]
+[3.4941487312316895, 8.118976593017578, "X-ray Detector Temporal Resolution 2 \u00b5s"]
+[3.494786262512207, 8.122628211975098, "X-ray Detector Target of Opportunity (ToO) response < 24 hours"]
+[0.2258003056049347, 13.633691787719727, "Calibration and Shutter Mechanism Dimensions ~ 80 cm x 30 cm"]
+[0.25557127594947815, 13.677515983581543, "Calibration and Shutter Mechanism Close Position Angle 0\u00ba"]
+[0.27986639738082886, 13.600945472717285, "Calibration and Shutter Mechanism Open Position Angle 63\u00ba"]
+[0.2181345671415329, 13.677590370178223, "Calibration and Shutter Mechanism Calibration Mode Position Angle 55\u00ba"]
+[2.801377058029175, 22.51349639892578, "Instrument System AMS-02"]
+[2.8575427532196045, 23.389204025268555, "Instrument URL http://www.srl.utu.fi/AuxDOC/kocharov/ICRC2009/pdf/icrc1064.pdf"]
+[3.0688068866729736, 22.496829986572266, "Instrument URL http://accms04.physik.rwth-aachen.de/~schael/AMS_Talks_files/07-Schael-Veto-klein.pdf"]
+[3.099649667739868, 22.528919219970703, "Instrument URL http://ams.cern.ch/AMS/Reports/TIMOct05/TOF/03_ACC_Wallraff.ppt"]
+[-0.7395148277282715, 12.368678092956543, "Proton Monitor Purpose Measure the effect of protons on photodiodes and LEDs"]
+[-0.7374576330184937, 12.385345458984375, "Proton Monitor Components Photodiodes and LEDs"]
+[-2.648937940597534, 11.69084358215332, "Imager Spatial Resolution Twice the current GOES Imagers"]
+[-2.638453960418701, 11.688095092773438, "Imager Coverage Rate Six times the current GOES Imagers"]
+[-2.6409876346588135, 11.677277565002441, "Imager Number of Spectral Channels More than three times the current GOES Imagers"]
+[-2.635251522064209, 11.664388656616211, "Imager Temporal Resolution More than five times the current GOES Imagers"]
+[-2.6498405933380127, 11.677972793579102, "Imager Number of Pixels Four times the current GOES Imagers"]
+[-2.9741368293762207, 4.337435245513916, "Spacecraft Pointing System Coarse pointing control, two-stage fine pointing control"]
+[-2.9867053031921387, 4.308976173400879, "Spacecraft Pointing Ability Coarse pointing control"]
+[-2.9700822830200195, 4.251345634460449, "Spacecraft Pointing Ability Two-stage fine pointing control"]
+[-3.0267539024353027, 4.257650852203369, "Spacecraft Unit of Measure Arcseconds"]
+[1.0221327543258667, 0.7683071494102478, "Earth Observation Satellite Launch Year 1979"]
+[0.4541810154914856, 4.535566329956055, "Natural Phenomenon Minimum Extent One of the lowest extents of the satellite record"]
+[0.4777549207210541, 4.518758296966553, "Natural Phenomenon Refreezing Rate Did not see its typical rate of refreezing in 2020"]
+[0.4679955840110779, 4.529050827026367, "Natural Phenomenon Extent in October 2020 The lowest on record for any October"]
+[2.891000270843506, 22.02849769592285, "Instrument Purpose Image the solar corona and help detect and characterize CMEs"]
+[2.478400707244873, 22.802221298217773, "Instrument Image Delivery Time Within 30 minutes of acquisition"]
+[2.6162009239196777, 22.659988403320312, "Instrument Number of Images per CME At least two"]
+[2.8561840057373047, 22.80877685546875, "Instrument Operating Capability During intense solar storms and flares"]
+[6.330937385559082, 7.411218166351318, "Satellite Component Antenna Type Electronically despun S-band antenna"]
+[6.320243835449219, 7.418267250061035, "Satellite Component Antenna Type UHF receive antenna"]
+[6.327264308929443, 7.411309719085693, "Satellite Component Antenna Type S-band toroidal pattern transmit antenna"]
+[-7.549679279327393, 5.851428508758545, "Camera Filter Bandwidth 10 nm FWHM"]
+[-7.565170764923096, 5.887709140777588, "Camera Filter Center 762 nm"]
+[-7.551699161529541, 5.884592533111572, "Camera Filter Bandwidth 10 nm FWHM"]
+[-7.569309711456299, 5.871852874755859, "Camera Filter Center 777 nm"]
+[2.195389747619629, -2.576467514038086, "Satellite Years in Orbit 3"]
+[4.597505569458008, -2.5867536067962646, "Satellite Routine Phase Operations 3 years"]
+[2.6393229961395264, -1.9529229402542114, "Satellite System and Operations Performance Met and surpassed system requirements"]
+[2.9725430011749268, -1.7570970058441162, "Satellite Maintenance Policy Adopted early in development"]
+[-0.6968900561332703, 12.396400451660156, "Monitor Mission Objective Space Weather monitoring and forecasting"]
+[11.236848831176758, 5.514986515045166, "CubeSat Launch Date 17 August 2021"]
+[11.21970272064209, 5.535253524780273, "CubeSat End of Life Date Operational as of February 2023"]
+[-0.6767534613609314, 12.402507781982422, "Monitor Technology Highly miniaturized"]
+[5.127387046813965, -4.1463518142700195, "Satellite Launch Date Late 2021"]
+[4.206871509552002, -2.502974510192871, "Satellite Revisit Time 12 days"]
+[5.371127128601074, -4.3755035400390625, "Satellite Launch Date September 2018"]
+[1.2688454389572144, -0.9619503617286682, "Satellite Measurements More than 2 billion in its first week"]
+[0.37659159302711487, 12.414852142333984, "Sensor Frequency 1.413 GHz"]
+[0.42237985134124756, 12.345277786254883, "Sensor Frequency 1.26 GHz"]
+[6.317313194274902, 7.423666477203369, "Satellite Component Aperture Diameter 2.5 m"]
+[1.5197627544403076, 21.23273468017578, "Instrument Mass 375 kg"]
+[1.6961501836776733, 23.178617477416992, "Instrument Power 375 W duty cycle, 50 W standby"]
+[0.4633868634700775, 12.168903350830078, "Sensor Antenna Beams 3 antenna beams at \u03b8 = 25.8\u00ba, 33.8\u00ba, 40.3\u00ba incidence angles with respect to nadir (to shadow side of orbit)"]
+[0.384855717420578, 12.315378189086914, "Sensor Footprint Size 76 km x 94 km, 84 km x 120 km, 96 km x 156 km"]
+[0.5879907608032227, 12.146279335021973, "Sensor NEDT, 12 s integration 0.05 K"]
+[0.596707820892334, 12.1051664352417, "Sensor Stability 0.12 K"]
+[0.5863130688667297, 12.135587692260742, "Sensor Calibration Stability for 7 days 0.13 dB"]
+[1.1523016691207886, -2.1038734912872314, "Satellite Knowledge 0.1\u00ba"]
+[3.594289779663086, -2.545403003692627, "Satellite Frequency Once per month"]
+[2.1196701526641846, -1.7563691139221191, "Satellite Modes ON, Standby, Survival"]
+[-5.421870231628418, 2.834332227706909, "Imaging Telescope Goal Provide high spatial resolution imaging"]
+[-0.933251142501831, -10.02509880065918, "Satellite Constellation Number of Microsatellites 60"]
+[-0.9460952877998352, -10.006916046142578, "Satellite Constellation Microsatellite Lifetime 4 years"]
+[1.730241060256958, 6.902999401092529, "Communication Device Thickness 7 mm"]
+[1.6920936107635498, 6.933506488800049, "Communication Device Dimensions 73.5 x 73.5 m x 6.8 mm"]
+[1.6966191530227661, 6.947076320648193, "Communication Device Qualification Tests Temperature cycling, vibration, thermal vacuum"]
+[-3.59572696685791, 12.74499225616455, "Particle Detector Energy Range 60 to 500 GeV"]
+[-3.598625659942627, 12.726768493652344, "Particle Detector Energy Range Above 8 GeV"]
+[-3.63260817527771, 12.75670051574707, "Particle Detector Mass of Dark Matter ~1 TeV"]
+[-0.0834108218550682, 13.586697578430176, "Measurement Technique Purpose Measuring with high sensitivity the angle between two wavefronts in a laser interferometer"]
+[6.324919700622559, 7.403186798095703, "Satellite Component Purpose To serve the feedback signal in the LRI"]
+[1.0971579551696777, -0.6368045806884766, "Satellite Dimensions 68.6 cm x 89 cm x 89 cm"]
+[1.1396689414978027, -0.7214757800102234, "Satellite Payload Envelope Size 61 cm x 61 cm x 46 cm"]
+[1.0423924922943115, -2.1776692867279053, "Satellite Attitude Knowledge/Control 0.15\u00ba/0.18\u00ba"]
+[0.4248388409614563, 4.560723304748535, "Natural Phenomenon Maximum Extent Date March 9, 2018"]
+[0.47538450360298157, 4.526864051818848, "Natural Phenomenon Average Concentration At least 15 percent"]
+[0.45752835273742676, 4.528594017028809, "Natural Phenomenon February Extent 13.95 million km2"]
+[0.4669942259788513, 4.5135273933410645, "Natural Phenomenon February Extent Deviation 1.35 million km2 below the 1981\u20132010 average"]
+[-3.220216751098633, 1.7159360647201538, "Satellite Mission Launch Date July 31, 2015"]
+[-3.1133222579956055, 1.7138532400131226, "Satellite Mission URL http://www.nasa-usa.de/mission_pages/sunearth/missions/mission_gold.html"]
+[-13.69978141784668, -2.3045201301574707, "X-ray Telescope Launch Date July 13, 2019"]
+[-13.898433685302734, -2.2497992515563965, "X-ray Telescope Orbit Halo orbit around the L2 point"]
+[-13.827468872070312, -2.2749178409576416, "X-ray Telescope Survey Sensitivity Unprecedented"]
+[-13.836474418640137, -2.2134151458740234, "X-ray Telescope Spectral Resolution Unprecedented"]
+[-13.889302253723145, -2.2361834049224854, "X-ray Telescope Angular Resolution Unprecedented"]
+[3.1267642974853516, -2.347041130065918, "Satellite Launch Date Unknown"]
+[2.568479061126709, -3.93876051902771, "Satellite URL https://tinyurl.com/y8f8qhrb"]
+[2.5785346031188965, -3.911179542541504, "Satellite URL https://blog.maxar.com/earth-intelligence/2020/enhancing-national-security-missions-with-worldview-legion"]
+[5.094026565551758, -4.519961357116699, "Satellite Conference Date August 1-6, 2020"]
+[2.5776751041412354, -3.914619207382202, "Satellite URL https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4709&context=smallsat"]
+[-1.717200756072998, 4.464969158172607, "Landing System Deployment Speed 32 km/h"]
+[-1.6683100461959839, 4.456427574157715, "Landing System Number of Drogue Parachutes 2"]
+[-1.6069583892822266, 4.464817047119141, "Landing System Number of Main Parachutes 3"]
+[-1.611488938331604, 4.343583583831787, "Landing System Coverage Area Almost an entire football field"]
+[-4.727725505828857, 7.579070091247559, "Data Reception System Antenna Systems Quantity 4"]
+[-4.695924282073975, 7.556079864501953, "Data Reception System Antenna Systems Length 7.5 m"]
+[-4.725313663482666, 7.596742153167725, "Data Reception System Antenna Polarization Dual"]
+[-4.72791051864624, 7.589978218078613, "Data Reception System Frequency S-band and X-band"]
+[-4.714632511138916, 7.583789825439453, "Data Reception System Telemetry Data Frequency 70 MHz"]
+[-1.2286884784698486, 9.016207695007324, "Gas Wavelength 2.738 \u00b5m"]
+[-0.2936675548553467, 8.099271774291992, "Liquid Wavelength 3.106 \u00b5m"]
+[-0.2828432619571686, 8.035382270812988, "Liquid Wavelength 2.903 \u00b5m"]
+[-0.30922403931617737, 8.068940162658691, "Liquid Wavelength 1.4 \u00b5m"]
+[-0.2821522653102875, 8.073305130004883, "Liquid Wavelength 1.9 \u00b5m"]
+[-0.8800486326217651, 12.317571640014648, "Ion Wavelength 2.7-2.8 \u00b5m"]
+[-0.9018612504005432, 12.458426475524902, "Ion Wavelength 2.81 \u00b5m"]
+[-2.905148983001709, 19.990676879882812, "Molecule Wavelength 2.2-2.3 \u00b5m"]
+[-2.9312222003936768, 20.065248489379883, "Molecule Wavelength 3.6 \u00b5m"]
+[-0.2925928831100464, 8.180530548095703, "Solid Wavelength 1.5 \u00b5m"]
+[-0.28308814764022827, 8.134492874145508, "Solid Wavelength 2 \u00b5m"]
+[-0.3501615524291992, 8.131213188171387, "Solid Wavelength 2.9 \u00b5m"]
+[0.26452940702438354, 8.174293518066406, "Crystal Wavelength 0.95-1 \u00b5m"]
+[0.2500961124897003, 8.16971206665039, "Crystal Wavelength 1 \u00b5m"]
+[0.23852194845676422, 8.162559509277344, "Crystal Wavelength 2 \u00b5m"]
+[0.23539862036705017, 8.167584419250488, "Crystal Wavelength 2 \u00b5m"]
+[0.27587857842445374, 8.157848358154297, "Crystal Wavelength 1 \u00b5m"]
+[0.2914970815181732, 8.177889823913574, "Crystal Wavelength 2.35 \u00b5m"]
+[0.270367830991745, 8.172574043273926, "Crystal Wavelength 2.5 \u00b5m"]
+[0.2660702168941498, 8.166446685791016, "Crystal Wavelength 3 \u00b5m"]
+[0.3052387237548828, 8.17184829711914, "Crystal Wavelength 3-3.5 \u00b5m"]
+[-0.968198835849762, 13.107332229614258, "Solar Irradiance Sensor Purpose Provide total and spectral solar irradiance measurements"]
+[-1.2677850723266602, 13.231127738952637, "Solar Radiation and Climate Experiment Launch Year 2003"]
+[-1.0231037139892578, 13.136000633239746, "Total Solar Irradiance Calibration Transfer Experiment Launch Year November 2013"]
+[3.309629201889038, 0.42995208501815796, "Air Force Space Test Program Satellite Design Life 2-3 years"]
+[0.9934892058372498, -4.392910957336426, "Satellite Mass 1858 kg"]
+[0.5437119603157043, -1.4851397275924683, "Satellite Orbit Altitude 536 km"]
+[0.7193945050239563, -2.2778799533843994, "Satellite Orbit Inclination 97.552\u00ba"]
+[4.154666900634766, -2.8129987716674805, "Satellite Orbit Period 95.49 minutes"]
+[3.8709468841552734, -3.1409032344818115, "Satellite LTAN 6 hours and 18 hours"]
+[4.225754261016846, -2.5103254318237305, "Satellite Revisit Period 25 days"]
+[4.144597053527832, -2.4808809757232666, "Satellite Inner Cycle in the CRS Mode 12 days"]
+[1.7070080041885376, -2.2263636589050293, "Satellite Maneuver Type DTM (Direct Transfer Maneuvers)"]
+[1.6948033571243286, -2.2580294609069824, "Satellite Maneuver Type Acquisition maneuvers"]
+[1.7519969940185547, -2.2104105949401855, "Satellite Maneuver Type Formation flying demonstration maneuvers and Sun corona observation"]
+[-3.259481430053711, 5.429177761077881, "Launch Vehicle Launch Date April 26, 2012"]
+[-3.263716459274292, 5.409425258636475, "Launch Vehicle Solid Propellant Quantity 12 tons"]
+[-3.2548937797546387, 5.439241886138916, "Launch Vehicle Number of Strap-on Motors 6"]
+[-3.2546167373657227, 5.415921688079834, "Launch Vehicle Version PSLV-XL"]
+[-3.2586660385131836, 5.447151184082031, "Launch Vehicle Launch Pad FLP (First Launch Pad) of SDSC"]
+[2.8659462928771973, 22.444801330566406, "Instrument Team Lead Michael Studinger"]
+[0.7458698153495789, -1.1530159711837769, "Satellite Average Elevation 1500 to 1750 meters"]
+[-0.7319926619529724, 5.322962760925293, "Castle Historical Use Home and stronghold for Vlad Tepe\u015f"]
+[-0.7442628741264343, 5.236712455749512, "Castle Historical Use Often cited as Vlad\u2019s home and as the inspiration for Stoker\u2019s gothic novel"]
+[1.2304188013076782, 2.7648749351501465, "Thermospheric Density Model Publication Date 18-21 August 2008"]
+[0.6592099070549011, 3.6677052974700928, "Thermosphere Model Publication Date 2015"]
+[5.193195819854736, -4.418588161468506, "Satellite Operational Update Date 1 June 2018"]
+[-5.780240535736084, 15.536531448364258, "Ultra Small Aperture Terminal Antenna Diameter 0.65 m"]
+[-5.785135746002197, 15.530564308166504, "Ultra Small Aperture Terminal SSPA Power 20 W"]
+[-5.787078380584717, 15.510269165039062, "Very Small Aperture Terminal Antenna Diameter 1.2 m"]
+[-5.781525135040283, 15.508142471313477, "Very Small Aperture Terminal SSPA Power 40 W"]
+[-6.670891761779785, 9.942267417907715, "Antennas Types MBAs (Multi-Beam Antennas) and APAAs (Active Phased Array Antennas)"]
+[-5.243483543395996, 7.990378379821777, "Communications Subsystems Repeater Modes Regenerative repeater mode and bent-pipe repeater mode"]
+[-0.9788352251052856, 7.693454742431641, "Device Mass 547 g"]
+[-1.0358119010925293, 7.780290126800537, "Device Power ~3 W TX, ~2.8 W RX, ~7.8 W Duplex"]
+[-1.0077234506607056, 7.759554862976074, "Device Volume ~175.1 cm 3"]
+[-1.008782982826233, 7.710667133331299, "Device Mass 129 g"]
+[-1.0200761556625366, 7.759997367858887, "Device Power 3.48 W"]
+[-0.9968822002410889, 7.742682933807373, "Device Volume ~35.4 cm 3"]
+[-1.0549492835998535, 7.771666049957275, "Device Processing Power 9 DMIPS/MHz (peak, 4 Cortex A53)"]
+[-1.4197171926498413, 9.485392570495605, "Propellant Quantity 6.38 kg"]
+[-1.3720762729644775, 9.552409172058105, "Propellant Reserved Quantity 3.9 kg"]
+[5.156645774841309, -4.118584156036377, "Satellite End of Service End of 2016 or possibly 1st quarter of 2017"]
+[-6.766498565673828, 10.016216278076172, "Antenna Panels Dimensions 2.2m x 3.6m"]
+[-4.494508266448975, 15.921646118164062, "Radar Component Quantity 60"]
+[-4.021678447723389, 8.544642448425293, "Cables and Divider/Combiners Function Route the RF signal"]
+[-5.803322792053223, 16.016368865966797, "SAR Antenna Deployment Function Deploy the SAR antenna after launch"]
+[2.788667678833008, -3.2944211959838867, "Communication Satellite Link Disaster Countermeasure Activities"]
+[2.7589802742004395, -3.3328449726104736, "Communication Satellite Outline Unknown"]
+[2.5538690090179443, -1.2618643045425415, "Satellite Marine Pollution Monitoring Capability ISTOP (Integrated Satellite Tracking of Pollution)"]
+[2.4945297241210938, -1.3628628253936768, "Satellite Marine Winds Monitoring Capability SAR derived marine winds"]
+[0.7927554845809937, -1.2855833768844604, "Satellite Ship Detection Range 1000 nautical miles from Canada's coasts"]
+[2.074481725692749, -2.771355390548706, "Satellite Number of Scenes Annually Up to 10,000"]
+[2.0906412601470947, -1.2707315683364868, "Satellite Daily SAR Imaging Requirement All required daily SAR imaging"]
+[-0.7428997159004211, 0.10923360288143158, "Distress Alerting Satellite System Space Segment Host GPS-III satellites"]
+[-0.7715511322021484, 0.1387103945016861, "Distress Alerting Satellite System Transponder Frequency 1544-1545 MHz"]
+[-1.8961244821548462, 8.11800765991211, "Trigger System Unknown Unknown"]
+[-0.798846423625946, 11.545036315917969, "Detector Unknown Unknown"]
+[2.9714510440826416, 22.883506774902344, "Instrument Power Status On"]
+[2.7173449993133545, 22.450258255004883, "Instrument Data Transmission Ongoing"]
+[-1.0012400150299072, 8.16616153717041, "Robotic Arm Capture Time 10:54 UTC"]
+[-1.0450820922851562, 8.123734474182129, "Robotic Arm Capture Date Jan 12, 2015"]
+[-0.8301634192466736, 3.241377353668213, "Active Galaxy Distance 570 million light-years"]
+[-5.354369163513184, 2.791045904159546, "Robotic Telescope Network Number of Telescopes 20"]
+[-0.8953977823257446, 3.036670684814453, "Active Galaxy Constellation Pictor"]
+[-5.8825578689575195, 15.996733665466309, "Synthetic Aperture Radar Boresight Orientation 20\u00ba from the vertical direction"]
+[-5.881190776824951, 15.993149757385254, "Synthetic Aperture Radar Antenna Beamwidth (Elevation) 6.2\u00ba"]
+[-5.883396148681641, 15.989392280578613, "Synthetic Aperture Radar Antenna Beamwidth (Azimuth) 1\u00ba"]
+[-5.86151123046875, 16.0091609954834, "Synthetic Aperture Radar Footprint 100 km x 15 km (3 dB contour)"]
+[-5.880878448486328, 16.00813865661621, "Synthetic Aperture Radar Swath Extends from 290 km to 390 km to the right of the S/C ground track"]
+[-5.914608001708984, 16.009523391723633, "Synthetic Aperture Radar Data Link Frequency 2.265 GHz"]
+[2.3109524250030518, -1.8243603706359863, "Satellite Laser Ready to fly"]
+[-5.262698173522949, 7.974610328674316, "Telecommunications System Relay In Orbit"]
+[-2.6294965744018555, 11.701095581054688, "Imager Detects Radiation upwelling from the Earth at specific wavelengths"]
+[-1.4428619146347046, 7.231759548187256, "Method Estimates Cloud top height, cloud thickness, cloud optical depth"]
+[-1.7445188760757446, 7.402054786682129, "Method Inputs ABI sensor data from GOES-R satellites, ambient temperature, relative humidity at the ground"]
+[3.7365810871124268, 17.71588706970215, "Payload Operating Frequency 406 MHz"]
+[3.680586099624634, 17.73299217224121, "Payload Uplink Band Extended C-band"]
+[3.734628200531006, 17.7030086517334, "Payload Downlink Band UHF band"]
+[3.730501413345337, 17.715913772583008, "Payload Data Transmission Destination INMCC (Indian Mission Control Center), located at ISTRAC (ISRO Telemetry, Tracking and Command Network), Bangalore"]
+[0.571478545665741, -1.5015126466751099, "Satellite Orbit Altitude 1336 km"]
+[0.8121088743209839, -2.058032274246216, "Satellite Longitude Spacing 1.4\u00ba"]
+[1.364335298538208, -1.6765395402908325, "Satellite Relative Bias Accuracy 1.6 mm"]
+[0.8804528117179871, -1.1178414821624756, "Satellite Sea-Level Anomaly Over 10 cm"]
+[0.9228491187095642, -1.162527322769165, "Satellite El Ni\u00f1o Anomaly More than 20 cm"]
+[14.419794082641602, 7.71388578414917, "Nanosatellite Mission Duration 1 year"]
+[14.448932647705078, 7.675225257873535, "Nanosatellite Platform Standard CubeSat"]
+[14.47868824005127, 7.694642543792725, "Nanosatellite Attitude Control Required for the operation of an imaging camera"]
+[2.452255964279175, -1.4229055643081665, "Satellite Data Processing Levels Standard products, Value added products"]
+[2.5343191623687744, -1.8800584077835083, "Satellite Ground Segment Location MOX (Mission Operations Complex) of ISTRAC (ISRO Telemetry, Tracking and Command Network), Bangalore"]
+[2.629241466522217, -1.8453823328018188, "Satellite Ground Segment Operation SAR payload operations"]
+[2.6768393516540527, -2.1240732669830322, "Satellite Ground Segment Communication Various mission computers and associated mission software and communication links"]
+[0.5623900294303894, -1.3957363367080688, "Satellite Orbit Altitude 802.9 km"]
+[0.7276133298873901, -2.2683486938476562, "Satellite Orbit Inclination 98.62\u00ba"]
+[4.130092144012451, -2.773388385772705, "Satellite Orbit Period 101 minutes"]
+[4.181623458862305, -2.4946563243865967, "Satellite Recurrent Period 4 days"]
+[4.129873275756836, -3.0595016479492188, "Satellite Local Sun Time 10:30 AM \u00b115 minutes"]
+[4.678936958312988, -2.587637186050415, "Satellite Mission Duration 10 months"]
+[5.131692886352539, -4.453894138336182, "Satellite Communication Experiment Date March 28 to 30, 2003"]
+[5.110721588134766, -4.479527473449707, "Satellite Communication Experiment Date Feb. 19, 2003"]
+[0.1247723400592804, 15.710491180419922, "Alpha Magnetic Spectrometer Antiproton Flux Accuracy 1%"]
+[0.12843267619609833, 15.722344398498535, "Alpha Magnetic Spectrometer Positron Fraction Measurement Up to 500 GeV"]
+[0.16764579713344574, 15.741216659545898, "Alpha Magnetic Spectrometer Potential Servicing Future spacewalk"]
+[0.16878537833690643, 15.743167877197266, "Alpha Magnetic Spectrometer Payload Condition Good"]
+[2.7166736125946045, -1.402807354927063, "Satellite Objective Study macroscale properties of dayside magnetopause reconnection"]
+[2.1308088302612305, -1.273935079574585, "Satellite Imaging Spatial and temporal ion dispersion signatures in the magnetospheric cusps"]
+[2.5108702182769775, -1.3491523265838623, "Satellite X-ray Generation Soft X rays imaged by the spacecraft"]
+[3.0672123432159424, -1.6492986679077148, "Satellite Principal Investigator Brian Walsh"]
+[-1.0759687423706055, 7.784533500671387, "Device Operation Operate the CCDs of the two fast cameras"]
+[-1.031768798828125, 7.72838020324707, "Device CCD Readout Interval 2.5 s"]
+[-1.0313507318496704, 7.780754566192627, "Device AFE Type Integrated analog front-end (AFE) electronics"]
+[-1.0324171781539917, 7.719709396362305, "Device AFE Type Non-integrated 16-bit AFE"]
+[-1.0331273078918457, 7.748160362243652, "Device Synchronization Signal Frequency 50 MHz"]
+[-1.1486265659332275, 4.457544326782227, "Ground Station Antenna Diameter 11 m"]
+[-1.1342854499816895, 4.484164714813232, "Ground Station Antenna Diameter 3.4 m"]
+[-5.186921119689941, 7.798989772796631, "Communication System Data Rate Considerable increase for nanosatellites"]
+[-2.0007107257843018, 8.077862739562988, "System Purpose Assess where crops need less or more water"]
+[2.4865224361419678, -1.376232385635376, "Satellite Data Source Satellite gravimetry data"]
+[-0.8347833752632141, 8.479090690612793, "Filter Wheel Assembly Number of Positions 6"]
+[-0.8544671535491943, 8.58126449584961, "Filter Wheel Assembly Motor Type Stepper motor / gear box with reduced backlash"]
+[-7.567350387573242, 5.864475250244141, "Shutter Mechanism Location Close to the intermediate focus"]
+[-7.574633598327637, 5.918284893035889, "Shutter Mechanism Type Mechanical shutter, under form of a blade"]
+[2.664433002471924, 14.352428436279297, "Optical Instrument Full Angle 2\u00ba"]
+[2.609144687652588, 14.26951789855957, "Optical Instrument Resolution 25 km"]
+[2.6363115310668945, 14.33409595489502, "Optical Instrument Wavelength 427.8 nm"]
+[2.6145992279052734, 14.317764282226562, "Optical Instrument Bandwidth 5.0 nm"]
+[2.622715473175049, 14.297857284545898, "Optical Instrument Diameter 1.27 cm"]
+[2.6448423862457275, 14.34135913848877, "Optical Instrument Integration Time 1.0 s"]
+[2.62890362739563, 14.343234062194824, "Optical Instrument Sensitivity 5 counts/s/Rayleigh"]
+[2.7001869678497314, 14.397575378417969, "Optical Instrument Maximum Count 500,000"]
+[-1.6004395484924316, 9.659818649291992, "Propulsion System Use Reduce the mass of satellites"]
+[3.7157557010650635, 17.719514846801758, "Payload Data Transmission Interval Every half hour"]
+[3.7138900756835938, 17.690658569335938, "Payload Mission Life 15 years"]
+[3.71935772895813, 17.691614151000977, "Payload Data Transmission Transmit data from a geostationary orbit"]
+[5.144594669342041, -4.230928897857666, "Satellite Mission Start Date April 15, 2019"]
+[-4.551129341125488, -3.087470054626465, "Exoplanet Diameter 89% of Earth\u2019s diameter"]
+[-0.627123236656189, 3.2498724460601807, "Star Type K-type"]
+[-0.6050861477851868, 3.2207860946655273, "Star Mass About 70% of the Sun\u2019s mass"]
+[-4.57517671585083, -3.1015865802764893, "Exoplanet Orbital Period Just under eight days"]
+[-4.560657978057861, -3.0876305103302, "Exoplanet Surface Temperature Perhaps as high as 800\u00ba F (427 \u00baC)"]
+[1.9074726104736328, 10.72457504272461, "Imaging Device Multispectral Imagery Resolution 50 cm"]
+[1.8918689489364624, 10.706748008728027, "Imaging Device Panchromatic Imagery Resolution 30 cm"]
+[1.9554259777069092, -1.1414873600006104, "Satellite Capacity to Collect Imagery 30 cm and multi-spectral"]
+[3.718165397644043, -2.554154872894287, "Satellite Imaging Frequency Every 20 to 30 minutes"]
+[-13.890469551086426, -2.2323238849639893, "X-ray Telescope Data Color Green"]
+[-2.1758501529693604, 2.899061679840088, "Space Observatory Measurement Black hole's spin rate"]
+[-2.177527666091919, 2.879303455352783, "Space Observatory X-ray Emission Models Clouds of dust and gas partially block the X-ray light, emission is reflected off the inner edge of the accretion disk"]
+[2.3906280994415283, -1.5474101305007935, "Satellite Laser Tests Preparing"]
+[5.0649824142456055, -4.19374418258667, "Satellite Technical Status Summary Sept. 1, 2016"]
+[2.9866392612457275, -1.8668303489685059, "Satellite Status Updates Ongoing"]
+[-5.416126251220703, 2.835253953933716, "Telescope Clear Aperture 165 mm"]
+[1.869855523109436, 10.735651016235352, "Imaging Device f/3.4 Number (Spatial) Unknown"]
+[1.9057899713516235, 10.71774673461914, "Imaging Device f/5.3 Number (Spectral) Unknown"]
+[-0.8454083204269409, 11.61977767944336, "Detector Resolution 1024 x 1024"]
+[-0.8133871555328369, 11.628652572631836, "Detector Readout Capability 12 bit full-frame at up to 120 frames/s"]
+[-3.3507089614868164, 7.161150932312012, "Data-Handling System Operating Modes 512 x 512, 512 x 1024, and 1024 x 1024"]
+[16.89031982421875, 6.815080642700195, "Microsatellite Mission Purpose Study of transient event energetic mechanisms that generate transient luminous emissions and gamma ray flashes in the terrestrial atmosphere above the thunderstorm areas"]
+[16.963960647583008, 6.744080543518066, "Microsatellite Phase B Start Year 2009"]
+[16.957977294921875, 6.755219459533691, "Microsatellite PDR Date June 2009"]
+[16.950706481933594, 6.75917387008667, "Microsatellite CNES Board Approval Date Dec. 9, 2010"]
+[16.975082397460938, 6.7389936447143555, "Microsatellite CDR Completion Date April 2013"]
+[2.6807212829589844, -2.0614638328552246, "Satellite Thermal Forces Minimization Unknown"]
+[3.1207237243652344, -2.369614839553833, "Satellite Launch Date Unknown"]
+[-0.38690268993377686, 15.93905258178711, "Imaging Spectrograph Mass 37 kg"]
+[-0.3899824321269989, 16.04804229736328, "Imaging Spectrograph Power Consumption 72 W"]
+[-0.40203383564949036, 15.987574577331543, "Imaging Spectrograph Size 40 x 30 x 70 cm"]
+[-0.3934171199798584, 16.01229476928711, "Imaging Spectrograph Data Rate ~6 Mbit/s"]
+[2.612978458404541, 14.250335693359375, "Optical Instrument Focal Length 150 mm"]
+[2.643531560897827, 14.267026901245117, "Optical Instrument Entrance Pupil Size 30 mm x 30 mm"]
+[0.5493188500404358, -1.4269518852233887, "Satellite Orbit Altitude 693 km"]
+[0.6304723024368286, -2.3115618228912354, "Satellite Orbit Inclination 98.19\u00b0"]
+[4.0871992111206055, -2.833214521408081, "Satellite Orbit Period 98.74 minutes"]
+[4.116189479827881, -2.4635002613067627, "Satellite Repeat Cycle 12 days"]
+[0.9142095446586609, -1.2924693822860718, "Satellite Formation Distance (Cross-track) 200 - 500 m"]
+[0.7748123407363892, -1.3253178596496582, "Satellite Formation Distance (Stereo) 350 km"]
+[-0.9328620433807373, 13.106460571289062, "Solar Energy Sensor Purpose Measures the total amount of solar energy input to Earth as well as the distribution of the Sun's energy input across a wide range of wavelengths"]
+[-0.8650665879249573, 12.839420318603516, "Total Irradiance Monitor Data Collection Start Date January 11th"]
+[-0.8938851356506348, 12.918915748596191, "Total Irradiance Monitor Measurement Record Extends a 40-year measurement of the Sun's total energy to Earth"]
+[-0.8911962509155273, 13.052265167236328, "Spectral Irradiance Monitor Data Collection Start Date March 4th"]
+[-0.9115405082702637, 13.024909973144531, "Spectral Irradiance Monitor Measurement Record Extends a 15-year record of spectral irradiance measurements"]
+[-1.9082181453704834, 6.898189067840576, "Software Suite Capabilities Translation and transmission of commands; uplink of files; downlink of telemetry, log messages, and files; automation of each listed capability through a TCL API"]
+[-1.971893310546875, 7.003018856048584, "Viewer Software Functions Plot and analyze spacecraft health and safety telemetry as a function of time, view GDS logs, view raw file and telemetry downlink, and create command products to downlink telemetry"]
+[-2.0002734661102295, 6.960215091705322, "Viewer Software Export Formats PNG, JPEG, CSV, JSON, tab-delimited"]
+[3.7285823822021484, 17.66359519958496, "Payload On-board Satellite RISAT-1"]
+[2.7318384647369385, 22.335071563720703, "Instrument Location Goddard Space Flight Center in Greenbelt, MD"]
+[2.7716000080108643, 22.430591583251953, "Instrument Host SES-14, a commercial communications satellite"]
+[3.2006592750549316, -1.8029497861862183, "Satellite Manufacturer Airbus"]
+[2.7623274326324463, -1.7284913063049316, "Satellite Operator SES, a Luxembourg-based satellite operator"]
+[-0.36041703820228577, 3.792551040649414, "Planet UV Light Absorption Absorbs UV light from the Sun and re-emits it to space"]
+[-2.8730478286743164, 15.264556884765625, "Microwave Water Vapor Profiler Channel Nr. 1-7"]
+[-2.9290499687194824, 15.209440231323242, "Microwave Water Vapor Profiler Frequency (GHz) 50.5, 53.2, 54.35, 54.9, 58.4, 58.825, 59.4"]
+[-2.864572525024414, 15.224458694458008, "Microwave Water Vapor Profiler Peaking altitude (km) 0, 2, 6, 10, 30, 16, 22"]
+[-2.8942294120788574, 15.218894958496094, "Microwave Water Vapor Profiler NEDT (K) 0.6, 0.4, 0.4, 0.4, 0.5, 0.4, 0.4"]
+[-1.5773601531982422, 4.124569416046143, "Ground Segment System Targeted Localization Accuracy Less than 10 m (CE90)"]
+[-1.5689141750335693, 4.144513130187988, "Ground Segment System Approach Star tracker calibration, estimate of optical sensor directional alignment and precise attitude determined value processing"]
+[-1.559371829032898, 4.155213356018066, "Ground Segment System Evaluation Method GCPs (Ground Control Points) prepared for the calibration will be used as true value"]
+[2.919727087020874, -1.3804947137832642, "Satellite Mission Capability Tropical coral reef mapping and coral bleaching detection"]
+[0.5829591155052185, 12.025315284729004, "Sensor Launch Schedule Late 2020 and early 2021"]
+[0.6658011078834534, 12.055381774902344, "Sensor Testing Timeline Within 12 months of launch"]
+[1.731433391571045, 6.90462064743042, "Communications Device Performance Data Transfer Successful"]
+[1.6963602304458618, 6.947436332702637, "Communications Device Function Demonstrate communications links"]
+[1.6851482391357422, 6.9824066162109375, "Communications Device Impact Enable newer, smaller, lighter, and more complex spacecraft"]
+[0.09431348741054535, 7.2312703132629395, "Experiment Components Electronics stack, three S-band antennas, one L-band antenna"]
+[0.1126275435090065, 7.166327476501465, "Experiment Forward Link Frequency 2106.40625 MHz"]
+[0.13517160713672638, 7.189062118530273, "Experiment Return Link Frequency 2287.5 MHz"]
+[0.1329321265220642, 7.195537090301514, "Experiment Antenna Operation Prohibited"]
+[-1.1520754098892212, 4.458980560302734, "Ground Station Quantity 4"]
+[-1.1393401622772217, 4.477476596832275, "Ground Station Purpose Telemetry, Tracking and Control (TT&C)"]
+[-3.3123891353607178, 7.358097553253174, "Data Processing System Activities Coordinated planning of the mission subsystems, automated and recurrent planning of the satellite observations, systematic acquisition and safeguarding of all spacecraft acquired data, recurrent calibration of the instrument, automated product circulation across PDGS distributed archives, long-term archiving of all mission data"]
+[-3.355891466140747, 7.424010753631592, "Data Processing System Quantity 1"]
+[1.913454532623291, -2.2063026428222656, "Satellite Orbit Type Geostationary"]
+[0.7324174642562866, -1.1894140243530273, "Satellite Altitude ~35,786 km"]
+[4.177570819854736, -2.849242925643921, "Satellite Scan Time 160 minutes"]
+[4.2451276779174805, -2.805138111114502, "Satellite India Scan Time ~40 minutes"]
+[3.7315163612365723, -1.6122848987579346, "Satellite Operation Status Nominal"]
+[2.2065062522888184, -2.6323840618133545, "Satellite Years on Orbit Two"]
+[2.0445363521575928, -2.661942481994629, "Satellite Number of Indian Meteorological Satellites Three"]
+[-0.9571715593338013, 9.816938400268555, "Rocket Launch Date Dec. 6, 2015"]
+[-3.0892786979675293, 2.421804904937744, "Mission Overview URL http://www.nasa.gov/sites/default/files/atoms/files/orbital_atk_crs-4_mission_overview-2.pdf"]
+[-3.2095041275024414, 5.201204776763916, "Cargo Launch Date Dec. 6, 2015"]
+[-2.0491037368774414, 8.984575271606445, "Electro-mechanical system Tracking Device Accommodates commercial optical cameras"]
+[-1.9695276021957397, 9.067109107971191, "Electro-mechanical system Compensation Accuracy Arcsecond"]
+[-2.016984462738037, 8.995699882507324, "Electro-mechanical system Axes 4"]
+[-1.990657925605774, 9.112464904785156, "Electro-mechanical system Usage Align to ISS local nadir direction, keep desired target steady in the camera's FOV, manually point at off-track targets"]
+[1.4219862222671509, -1.569967269897461, "Satellite Accuracy Improvement mm-level"]
+[2.149031162261963, -1.4050910472869873, "Satellite Data Improvement Order of magnitude"]
+[1.7432993650436401, -1.8139889240264893, "Satellite Improvement of EOP 17%"]
+[1.8670724630355835, -1.8490597009658813, "Satellite Improvement of EOP 21%"]
+[-1.8714430332183838, 15.023985862731934, "Imaging Radiometer/Polarimeter Detector Array 2-D"]
+[-1.9174926280975342, 15.04746150970459, "Imaging Radiometer/Polarimeter Sensor Matrix CCD sensor (242 x 548 photoelements, the pixels are binned one by two, resulting in 242 x 274 sensitive areas)"]
+[-1.904483675956726, 15.037544250488281, "Imaging Radiometer/Polarimeter Focal Length 3.57 mm"]
+[-1.9153809547424316, 15.030643463134766, "Imaging Radiometer/Polarimeter Field of View \u00b143\u00ba along-track"]
+[-1.9056289196014404, 15.035725593566895, "Imaging Radiometer/Polarimeter Field of View \u00b151\u00ba across-track"]
+[-1.915299892425537, 15.041088104248047, "Imaging Radiometer/Polarimeter Field of View \u00b157\u00ba diagonal"]
+[-1.895288109779358, 14.974693298339844, "Imaging Radiometer/Polarimeter Mass 33 kg"]
+[-1.9032403230667114, 15.040153503417969, "Imaging Radiometer/Polarimeter Power 42 W"]
+[0.12399964779615402, 7.193658828735352, "Experiment Cooling Pump Failure Unknown"]
+[0.11782746762037277, 7.186106204986572, "Experiment Longevity Unknown"]
+[-0.13960987329483032, 15.569070816040039, "Spectrometer Spectral Coverage 3-12.85 \u00b5m and 753-784 nm"]
+[-0.1085890606045723, 15.474393844604492, "Spectrometer Spatial Coverage 10 - 60 km"]
+[-0.15086103975772858, 15.437353134155273, "Spectrometer Vertical Resolution 1 km"]
+[-0.06091374531388283, 15.477249145507812, "Spectrometer Observation Accuracy 5% (1% for ozone)"]
+[14.475540161132812, 7.721662521362305, "Nanosatellite Orbit Altitude ~680 km"]
+[14.464853286743164, 7.716423034667969, "Nanosatellite Orbit Inclination 98.19\u00ba"]
+[14.468249320983887, 7.695785045623779, "Nanosatellite LTAN 13:30 hours"]
+[14.342896461486816, 7.766637802124023, "Nanosatellite Anomaly Duration One month"]
+[14.446142196655273, 7.755427837371826, "Nanosatellite Beacon Signal Currently transmitting"]
+[-5.119007587432861, 7.747074604034424, "Communications Bus Data Rate 1.23 Gbit/s"]
+[-3.6487293243408203, 8.07303524017334, "Solid State Drive Write Speed Up to 1.6 Gbit/s"]
+[-2.441174268722534, 13.243834495544434, "Hyperspectral Image Volume ~150-600 MByte"]
+[-0.8511030077934265, 11.613627433776855, "Detector Board Data Stream 1.23 Gbit/s"]
+[0.6634869575500488, 9.29921817779541, "Attitude Determination and Control Subsystem Pointing or Orientation Time Less than 24 hours"]
+[0.6212508082389832, 9.341655731201172, "Attitude Determination and Control Subsystem Self-Position Accuracy < 50 m"]
+[0.680860161781311, 9.328909873962402, "Attitude Determination and Control Subsystem Maximum Slew Rate 3\u00ba/s"]
+[0.6738688349723816, 9.314078330993652, "Attitude Determination and Control Subsystem Ideal Slew Rate 0.25\u00ba/s"]
+[0.6426560282707214, 9.334668159484863, "Attitude Determination and Control Subsystem STARE Pointing Stability 0.052\u00ba/s"]
+[0.6383689045906067, 9.332355499267578, "Attitude Determination and Control Subsystem STARE Smear Rate 0.02\u00ba/s"]
+[-0.9172192811965942, 6.484192371368408, "Documentation Author Herbert J. Kramer"]
+[-0.9878721833229065, 6.513285160064697, "Documentation Publisher Springer Verlag"]
+[-0.9573037028312683, 6.439175605773926, "Documentation Edition 4th"]
+[-0.8604665398597717, 6.136007785797119, "Website Contact Email eoportal@symbios.space"]
+[-0.9884154200553894, 6.241735935211182, "Copyright Year 2024"]
+[2.146118640899658, -1.8080376386642456, "Satellite Observation Target L 98-59"]
+[-0.3629094064235687, 3.783810615539551, "Planet Orbital Period 2.25 days"]
+[-0.3784447908401489, 3.7862672805786133, "Planet Orbital Period 3.7 days"]
+[-0.38121697306632996, 3.765671730041504, "Planet Orbital Period 7.5 days"]
+[-0.38590651750564575, 3.758073091506958, "Planet Energy Received from Star 22 times the amount of energy Earth receives from the Sun"]
+[-0.3716840147972107, 3.7757132053375244, "Planet Energy Received from Star 11 times as much radiation as Earth"]
+[-0.3926703631877899, 3.7630791664123535, "Planet Energy Received from Star 4 times the radiant energy as Earth"]
+[-0.3958691656589508, 3.7840778827667236, "Planet Habitable Zone None"]
+[-0.36799511313438416, 3.7871696949005127, "Planet Venus Zone Range of stellar distances where a planet with an initial Earth-like atmosphere could experience a runaway greenhouse effect"]
+[2.6975555419921875, -1.5198142528533936, "Satellite Goal Build a catalog of small, rocky planets on short orbits around very bright, nearby stars for atmospheric study by NASA's upcoming James Webb Space Telescope"]
+[1.3785945177078247, -1.3926677703857422, "Satellite Frame-Dragging Measurement Accuracy About 2 x 10-3"]
+[0.6593484878540039, -1.4437618255615234, "Satellite Equivalence Principle Test Range About 12,300 km"]
+[2.8197014331817627, -1.0905158519744873, "Satellite Purpose Test alternative theories of gravitation versus General Relativity"]
+[2.8472983837127686, -2.0173146724700928, "Satellite In-Orbit Validation Element Unknown"]
+[2.7679243087768555, -1.8799097537994385, "Satellite Navigation System Unknown"]
+[-13.48922348022461, -2.031100034713745, "X-ray Space Observatory Mast Length 10-m"]
+[-13.494781494140625, -2.0363056659698486, "X-ray Space Observatory Optics Modules Two identical"]
+[-13.488607406616211, -2.0295464992523193, "X-ray Space Observatory Mission Operations Center UC Berkeley"]
+[-13.479859352111816, -2.0275979042053223, "X-ray Space Observatory Outreach Program Location Sonoma State University, Rohnert Park, Calif"]
+[-13.485812187194824, -2.0194642543792725, "X-ray Space Observatory Managed by Goddard"]
+[2.701036214828491, 22.39374351501465, "Instrument Type Imaging multi-spectral radiometers (vis/IR)"]
+[2.71734356880188, 22.415666580200195, "Instrument Type Passive Synthetic Aperture Radar"]
+[2.8276851177215576, 22.384796142578125, "Instrument Type Multiview Thermal-Infared"]
+[-1.1687049865722656, 4.50238561630249, "Earth Station Location Higashimatsushima"]
+[-5.308712482452393, 7.961644649505615, "Communication System Connection Period March 20 to April 5"]
+[-5.222764015197754, 7.894143581390381, "Communication System Importance Extremely important due to the difficulty in obtaining information on the disaster in stricken areas"]
+[7.267031669616699, 12.435260772705078, "Space Weather Instrument Purpose Better space weather forecasts"]
+[-5.306706428527832, 3.0650782585144043, "Telescope Array Mission Date May 13, 2013"]
+[-5.326376914978027, 3.1854052543640137, "Telescope Array DOI 10.1088/0004-637X/770/2/103"]
+[3.0668325424194336, -1.9017634391784668, "Satellite Operational Phase Start of the operational phase"]
+[2.388292074203491, -1.5096213817596436, "Satellite VBN Demonstration Capturing images of DSAT-3 from various distances and over large duration"]
+[1.7083723545074463, -2.2686550617218018, "Satellite Maneuvers Types Radial (R-bar) or velocity (V-bar) burns"]
+[-0.5187408924102783, 1.217092752456665, "Satellite Trajectory Type Possible trajectory combining different maneuvers"]
+[0.995640218257904, -4.327917575836182, "Satellite Satellite Mass 15 kg"]
+[0.9864979386329651, -4.283317565917969, "Satellite Satellite Mass 350 kg"]
+[2.6890995502471924, -1.2026116847991943, "Satellite Focus Detecting methane rather than carbon dioxide"]
+[5.108889102935791, -4.009159088134766, "Satellite Launch Date Late 2022 or early 2023"]
+[-2.0556039810180664, 12.112196922302246, "Infrared Imager Mass 23 kg"]
+[-2.0061638355255127, 12.11713981628418, "Infrared Imager Power Consumption < 60 W"]
+[-2.039491891860962, 12.143281936645508, "Infrared Imager Aperture 200 mm"]
+[-2.0043411254882812, 12.136372566223145, "Infrared Imager Filter Wheel 6 filters"]
+[-1.9755975008010864, 12.159011840820312, "Infrared Imager FPA Two staggered CMT arrays, each of size 2 x 512 elements"]
+[-2.035761594772339, 12.146252632141113, "Infrared Imager Cryocooler Stirling cycle cryocooler"]
+[-1.9580384492874146, 12.138256072998047, "Infrared Imager Operating Temperature 80 K"]
+[-1.9753650426864624, 12.150985717773438, "Infrared Imager Telescope Structure Carbon fiber composite"]
+[6.279794216156006, 7.449645519256592, "Satellite Component Mass 37.5 kg"]
+[2.32053279876709, 13.64515495300293, "Optics Focal Length 10.15 m"]
+[2.3565220832824707, 13.677083015441895, "Optics Shell Radii 51 - 191 mm"]
+[2.3575093746185303, 13.654637336730957, "Optics Graze Angles 1.3 - 4.7 mrad"]
+[2.3185153007507324, 13.644721984863281, "Optics Mirror Thickness 0.21 mm"]
+[2.353456735610962, 13.651931762695312, "Optics Total Shells per Module 130"]
+[2.3512794971466064, 13.66049575805664, "Optics Total Mirror Segments 4680"]
+[2.339703321456909, 13.651862144470215, "Optics Multilayer Thickness (layer 1-89) ~0.7 \u00b5m"]
+[2.335588216781616, 13.642045021057129, "Optics Multilayer Thickness (layer 90-133) W/Si"]
+[2.3932247161865234, 13.675302505493164, "Optics Composite Structure D263 glass; DS-4 graphite; F131 epoxy"]
+[11.802988052368164, 5.318253993988037, "6U CubeSat Mass 12 kg"]
+[11.80935001373291, 5.307868480682373, "6U CubeSat Objective Test miniature telescope components"]
+[11.805139541625977, 5.312704563140869, "6U CubeSat Prime Mission Duration 90 days"]
+[4.613847732543945, -2.606513738632202, "Satellite Mission Duration 2 years"]
+[-4.566668510437012, -3.092559576034546, "Exoplanet Age 40 million years"]
+[-4.577442646026611, -3.105041980743408, "Exoplanet Orbital Period 8 days"]
+[4.885951042175293, -4.477863311767578, "Satellite Image Acquisition Date April 13, 2016"]
+[-0.6858118772506714, 5.496245861053467, "Bridge Location Gulf crossing Izmit Bay"]
+[2.220221996307373, 22.248104095458984, "Instrument Measurement Flux of atomic oxygen (AO)"]
+[1.8057304620742798, 22.124788284301758, "Instrument Altitude Around 600km"]
+[0.6839702725410461, 12.02388858795166, "Sensor Objective Characterize the debris and micrometeoroid environment of GTO"]
+[0.4599400758743286, 12.20254135131836, "Sensor Measurement Type Calibrated passive radiometric measurements at multiple microwave frequencies"]
+[0.4907354414463043, 12.14892292022705, "Sensor Data Output Ocean Surface Vector Winds (OSVW), Tropical Cyclone Intensity (TCI) and additional EDRs"]
+[0.4842813313007355, 12.126485824584961, "Sensor Measurement Type In-situ space weather measurements, ECP flux and warnings"]
+[-3.5914604663848877, 4.4167609214782715, "Spacecraft Retirement Date June 2010"]
+[-3.544799327850342, 4.396221160888672, "Spacecraft Last Observation Date June 21, 2010"]
+[-3.3632023334503174, 4.234333038330078, "Spacecraft Mission Duration 12 years"]
+[-5.343179225921631, 2.734647274017334, "Telescope Magnification Five times"]
+[-1.5341802835464478, 13.130242347717285, "Solar Phenomenon Description The bright, reticulated pattern observed in many EUV images of solar active regions"]
+[-3.0618202686309814, 4.36583137512207, "Spacecraft Mass Unknown"]
+[-3.0914065837860107, 2.412782669067383, "Mission Total IPS Mass 3700 kg"]
+[16.57147979736328, 7.028998851776123, "Minisatellite Mass ~180 kg"]
+[16.84369659423828, 6.857020378112793, "Microsatellite Mass 86 kg"]
+[16.8087100982666, 6.882131576538086, "Microsatellite Mass 70 kg"]
+[16.80031394958496, 6.895483493804932, "Microsatellite Mass 71 kg"]
+[14.683658599853516, 7.817709445953369, "Nanosatellite Mass 5 kg"]
+[14.690173149108887, 7.829293251037598, "Nanosatellite Mass ~ 4 kg"]
+[5.174567699432373, -4.309974670410156, "Satellite Launch Date 22 June 2020"]
+[2.5952706336975098, -3.9044950008392334, "Satellite URL https://www.nasa.gov/feature/goddard/2020/nasa-s-tess-enables-breakthrough-study-of-perplexing-stellar-pulsations"]
+[-1.5449351072311401, 4.146359443664551, "Ground Segment Element Function Provides the planning and satellite command, control functions and the maintenance of the satellite systems"]
+[-1.5344305038452148, 4.149895668029785, "Ground Segment Element Function Provides data reception and storage processes of KOMPSAT-3 spatial data and allows for the distribution of imagery products to end-users"]
+[1.8900188207626343, 8.598100662231445, "Subsystem Function User Interface"]
+[1.8982808589935303, 8.609994888305664, "Subsystem Function Image Collection Planning"]
+[1.8896912336349487, 8.613765716552734, "Subsystem Function Direct Ingestion"]
+[1.8982057571411133, 8.604809761047363, "Subsystem Function Product Management"]
+[-4.332144737243652, 0.2418615221977234, "GPS Occultation Receiver Measurement Atmospheric temperature and humidity profiles"]
+[-4.287667751312256, 0.2923034131526947, "GPS Occultation Receiver Measurement Electron density profiles in the ionosphere"]
+[-4.330960273742676, 0.246092289686203, "GPS Occultation Receiver Measurement Total Electron Count"]
+[-4.327052593231201, 0.25287026166915894, "GPS Occultation Receiver Measurement POD"]
+[-4.315742492675781, 0.25649967789649963, "GPS Occultation Receiver Components GPS receiver for RO (Radio Occultation), Velocity & anti-velocity antenna assembly, POD (Precise Orbit Determination) antenna, RF cables"]
+[1.4853153228759766, -2.4678900241851807, "Satellite Orbit Sun-synchronous LEO"]
+[2.3101963996887207, -1.193272352218628, "Satellite Imagery Panchromatic and multispectral"]
+[1.1692043542861938, -0.7804180979728699, "Satellite Bus Dimensions 1.2 m in diameter and 1.35 m in height"]
+[2.3712968826293945, -2.073287010192871, "Satellite Bus Structure Deck-and-longeron type"]
+[1.4404501914978027, 2.769057273864746, "Weather Satellite Launch Time 4:38 p.m. EST"]
+[1.436648964881897, 2.7612733840942383, "Weather Satellite Launch Date 1 March 2022"]
+[1.4477126598358154, 2.753237247467041, "Weather Satellite Solar Arrays Deployment Time 8:28 p.m. EST"]
+[-0.8827024102210999, 7.971885681152344, "Ranging Device Band K-Band"]
+[-0.790400505065918, 8.169021606445312, "Ranging Device Purpose Measure Earth's gravity field"]
+[2.9200949668884277, 22.51524543762207, "Instrument Manufacturer L3Harris"]
+[2.822988510131836, 22.359893798828125, "Instrument Problem Blockages in its radiator by FOD (Foreign Object Debris)"]
+[5.0521159172058105, -4.385785102844238, "Satellite Arrival Date November 10, 2021"]
+[5.114467620849609, -4.038693904876709, "Satellite Launch Date Early 2022"]
+[5.124261379241943, -4.044992446899414, "Satellite Operational Date Early 2023"]
+[14.612312316894531, 7.591889381408691, "Nanosatellite Mission Type EO"]
+[14.24219799041748, 7.8215107917785645, "Nanosatellite Launch Date 18 April 2014"]
+[14.262063980102539, 7.7925004959106445, "Nanosatellite End of Life Date 4 Jun 2014"]
+[14.568120002746582, 7.574154853820801, "Nanosatellite Size 3U CubeSat"]
+[5.341583251953125, -4.439737796783447, "Satellite Launch Date to ISS 5 December 2019"]
+[5.094313144683838, -4.390740871429443, "Satellite Deployment Date from Cygnus Early February 2020"]
+[1.0475478172302246, -1.1143702268600464, "Satellite Antenna Booms Length 80-meter and 16-meter"]
+[4.509908199310303, -2.699064254760742, "Satellite Experiment Duration About another six months"]
+[3.159231662750244, -1.6368749141693115, "Satellite Mission Director Lt. Col. James Caldwell"]
+[2.905052900314331, -1.538408875465393, "Satellite Radiation Belt Remediation (RBR) effort Leader Dr. Michael Starks"]
+[0.9092368483543396, 14.798864364624023, "Instrumentation Function Capture test results"]
+[0.9112530946731567, 14.79820728302002, "Instrumentation Performance Worked well throughout the entire flight"]
+[0.8962486386299133, 14.794142723083496, "Instrumentation Power Cycle Sequences Executed as planned"]
+[0.9059381484985352, 14.815829277038574, "Instrumentation Data Acquisition Functioned correctly throughout the mission"]
+[0.908948540687561, 14.805106163024902, "Instrumentation Data Recording Redundantly recorded all data as planned"]
+[2.276487112045288, 22.675518035888672, "Instrument Data Format Repeat 100 ms"]
+[1.5161125659942627, 21.23336410522461, "Instrument Total Mass ~145 kg"]
+[2.9397809505462646, 22.378366470336914, "Instrument Components EO (Electro-Optics) module, telescope, scan assembly, filter wheel, cooler, detectors, electronics packages"]
+[2.723978042602539, 22.638477325439453, "Instrument Magnet Configuration Permanent"]
+[-2.1221230030059814, 4.312310218811035, "Space Station Orbit Altitude ~400 km"]
+[-2.094759464263916, 4.323375701904297, "Space Station Orbit Inclination 51.6\u00ba"]
+[-2.130784511566162, 4.31351375579834, "Space Station Attitude Torque Equilibrium Attitude (TEA)"]
+[0.9054355025291443, 14.798233032226562, "Instrumentation Measurement Alternative magnetic field in the low and medium frequency ranges"]
+[0.8845625519752502, 14.795473098754883, "Instrumentation Frequency Range DC-20 kHz"]
+[0.9106295108795166, 14.808219909667969, "Instrumentation Frequency Range 10 Hz-20 kHz"]
+[0.8994264602661133, 14.794252395629883, "Instrumentation Frequency Range 100 kHz - 30 MHz"]
+[0.5976602435112, -1.463037133216858, "Satellite Orbit Altitude ~670 km"]
+[0.7323951125144958, -2.2567343711853027, "Satellite Orbit Inclination 98.23\u00ba"]
+[4.147672176361084, -2.798675775527954, "Satellite Orbit Period 98 minutes"]
+[3.8964040279388428, -3.064154863357544, "Satellite LTDN 21:30 hours"]
+[5.316857814788818, -4.458061695098877, "Satellite Launch Date July 12, 2010"]
+[2.7784478664398193, -2.2683987617492676, "Satellite Launch Site Satish Dhawan Space Centre (SDSC) SHAR, Sriharikota, India"]
+[5.250341892242432, -4.154241561889648, "Satellite Scheduled Launch Year 2014"]
+[0.09874239563941956, 7.161577224731445, "Experiment Unknown Unknown"]
+[0.8417865037918091, 11.98453140258789, "Sensor Unknown Unknown"]
+[-6.764499664306641, 10.025936126708984, "Antenna Size 2 m x 2 m"]
+[-6.758659839630127, 10.015235900878906, "Antenna Tile Size 1 m x 1 m"]
+[-6.713167190551758, 10.028575897216797, "Antenna Linear Array Length 1 m"]
+[-6.734212875366211, 9.998746871948242, "Antenna Number of Microstrip Patches per Array 20"]
+[-6.759457588195801, 10.044151306152344, "Antenna Number of Dual Polarized Linear Arrays per Tile 24"]
+[-0.7339205741882324, 8.583832740783691, "Inflatable Mechanism Deployment Length 1 m"]
+[-1.0245901346206665, 7.7071638107299805, "Devices Deorbit Time Within 25 years"]
+[-1.0675461292266846, 7.673591613769531, "Devices Trackable Yes"]
+[-1.0233631134033203, 7.703888893127441, "Devices Contribution to Debris Not contribute to the production of further debris in space"]
+[1.0030994415283203, -4.4208831787109375, "Satellite Mass 10 kg"]
+[2.8420369625091553, -1.0951977968215942, "Satellite Purpose Monitor nearby stars for orbiting exoplanets"]
+[-3.797306776046753, 6.936617374420166, "Data Collection System Number of Data Collection Platforms 19,000"]
+[-3.796334981918335, 6.9410176277160645, "Data Collection System Number of User-Platform Channels 433"]
+[2.6019840240478516, 21.98125457763672, "Instrument Function Provide accurate and higher resolution meteorological observations"]
+[2.5912322998046875, 21.930843353271484, "Instrument Function Measure temperature and humidity profiles"]
+[-0.6290168762207031, 8.531377792358398, "Cryocooler Performance Unknown"]
+[-0.6172839403152466, 8.568138122558594, "Cryocooler Performance Unknown"]
+[3.629305601119995, 22.23558235168457, "Instrument Component Spectral Ranges 4.3 to 5.15 \u00b5m and 5.4 to 6.0 \u00b5m"]
+[1.7918258905410767, 22.160480499267578, "Instrument Ground Resolution 35 m"]
+[1.8272428512573242, 22.054201126098633, "Instrument Ground Swath 15 km"]
+[0.1487521231174469, 7.168827056884766, "Experiment Objective To map the ionospheric electron densities in the satellite's orbital plane and to study the evolution of 1-100 km sized low latitude irregularities using radio/optical tomography techniques"]
+[0.11951020359992981, 7.197259426116943, "Experiment Components Three-frequency radio-beacon, antenna and an UV photometer"]
+[0.1440536230802536, 7.193039894104004, "Experiment Function Determine integrated ionospheric densities near the satellite orbit plane"]
+[2.109308958053589, -1.4475351572036743, "Satellite Atmospheric Density Comparison NRLMSISE-00 has more than +20% bias, JB2008 and DTM2013 correspond well with the SLATS data"]
+[2.93235445022583, -1.7134664058685303, "Satellite Revision Decision Revise the NDO to cut off the future fuel of RCS"]
+[2.655381917953491, -1.625024676322937, "Satellite Data Access Full and open"]
+[1.4272247552871704, -3.123389959335327, "Satellites Replacement Date Unknown"]
+[5.385351181030273, -4.466092109680176, "Satellite Launch Date December, 2007"]
+[5.183116912841797, -4.268416404724121, "Satellite Scheduled Operational Date 2010/11"]
+[-1.3060377836227417, 6.2310991287231445, "Working Group First Meeting Date December 8, 2010"]
+[1.1495269536972046, -0.8396012783050537, "Satellite Diameter 424 mm"]
+[0.9043242931365967, -4.286416530609131, "Satellite Payload Mass at Liftoff 296 kg"]
+[1.5716484785079956, -2.3541018962860107, "Satellite Orbit Type Circular MEO"]
+[0.5455331206321716, -1.480049967765808, "Satellite Orbit Altitude 5893 km"]
+[0.9463794827461243, -2.2876927852630615, "Satellite Orbit Eccentricity 0-0.0025"]
+[0.7106158137321472, -2.3063504695892334, "Satellite Orbit Inclination 70.16\u00ba"]
+[-3.0064282417297363, 7.027406215667725, "Command and Data Handling Model Proton P400K-SGMII-2-PCI104S-SD"]
+[-3.0301618576049805, 7.0294060707092285, "Command and Data Handling Processor Freescale advanced 45 nm dual-core microprocessor"]
+[-2.9968841075897217, 6.994242191314697, "Command and Data Handling Radiation Hardened Yes"]
+[-2.9900944232940674, 7.01691198348999, "Command and Data Handling Power Low"]
+[0.8003992438316345, 4.0814337730407715, "Atmospheric Measurement Temperature Accuracy 4 K at 1000 mb"]
+[0.7957773208618164, 4.070827484130859, "Atmospheric Measurement Temperature Accuracy 3 K at 850 mb"]
+[0.7962747812271118, 4.074467658996582, "Atmospheric Measurement Temperature Accuracy 1 K at 700-10 mb"]
+[0.8016771674156189, 4.081493854522705, "Atmospheric Measurement Humidity Accuracy Specific humidity 1.5 grams/kg or \u00b1 20 percent over clear sky or ocean"]
+[0.7942669987678528, 4.0833940505981445, "Atmospheric Measurement Rain Rate Accuracy 5 mm/h"]
+[0.829302966594696, 4.053796768188477, "Atmospheric Measurement Cloud Water Accuracy 0.10 kg m -2"]
+[0.8104490041732788, 4.0677080154418945, "Atmospheric Measurement Soil Moisture Accuracy \u00b1 10%"]
+[0.808634340763092, 4.06217622756958, "Atmospheric Measurement Ice Edge and Snow Edge Accuracy \u00b1 3 cm, \u00b1 2.5 K"]
+[-13.876220703125, -2.1581790447235107, "X-ray Telescope Energy Band 5 - 79 keV"]
+[-13.837207794189453, -2.28713321685791, "X-ray Telescope Focal Length 10.15 m"]
+[-13.875773429870605, -2.2643511295318604, "X-ray Telescope Optics Depth-graded multilayer coated grazing incidence optics"]
+[1.6432684659957886, -1.1612871885299683, "Satellite Measurement Around the clock"]
+[-2.197255849838257, 5.927244186401367, "Aircraft Collaboration ESA\u2019s CryoSat-2 and the European Union\u2019s Sentinel-3 satellites"]
+[-3.0893640518188477, 2.4334185123443604, "Mission Collaboration International Thwaites Glacier Collaboration"]
+[-2.6558847427368164, 11.668835639953613, "Imager Type Pushbroom"]
+[-2.672612428665161, 11.659165382385254, "Imager Manufacturer EADS Astrium SAS, France"]
+[-2.650801658630371, 11.671957969665527, "Imager Components Camera, IPU (Instrument Processing Unit), optical subassembly, secondary structure, FPA (Focal Plane Assembly), Korsch telescope, video electronics, sequencer, DC/DC converter, compression cards"]
+[-2.658719539642334, 11.679656028747559, "Imager Telescope Material SiC (Silicon Carbide)"]
+[-2.677957773208618, 11.684442520141602, "Imager IPU Components Video electronics, sequencer, DC/DC converter, compression cards"]
+[0.6840754151344299, 10.975333213806152, "Imaging Sensor Spatial Resolution Unknown"]
+[0.6977327466011047, 10.991833686828613, "Imaging Sensor Spatial Resolution Unknown"]
+[2.2394182682037354, -2.543872356414795, "Satellite Spectral Bands 13"]
+[1.4349510669708252, -1.1214792728424072, "Satellite Spatial Resolutions 10 to 60 m"]
+[-1.0609689950942993, 7.699305534362793, "Device Activation Automatic after a crash"]
+[-0.8603386282920837, 0.1741812825202942, "Satellite System Operational Year 1985"]
+[5.382448673248291, -4.407351016998291, "Satellite Launch Date Feb. 26, 1987"]
+[-3.3374857902526855, 7.4473114013671875, "Data Processing Responsible Organization Jet Propulsion Laboratory"]
+[-3.3225455284118652, 7.448724269866943, "Data Processing Responsible Organization Goddard Space Flight Center"]
+[-3.328110933303833, 7.441949367523193, "Data Processing Responsible Organization Navy Fleet Numerical Weather Central"]
+[-3.3383967876434326, 7.441908836364746, "Data Processing Responsible Organizations NOAA National Environmental Satellite Data and Information Service and Jet Propulsion Laboratory Pilot Ocean Data System"]
+[0.8017343282699585, -2.1461849212646484, "Satellite Latitude Coverage -56\u00b0 to 84\u00b0"]
+[5.341525554656982, -4.446218967437744, "Satellite Launch Date March 7, 2017"]
+[4.2478346824646, -2.825761079788208, "Satellite Separation Time 57 min 57 seconds"]
+[2.2451374530792236, -2.0188236236572266, "Satellite Solar Panel Deployment Complete"]
+[4.664342880249023, -2.940357208251953, "Satellite Expected Operations Start Three to four months after launch"]
+[2.7449495792388916, -3.2415802478790283, "Satellite Communication Technology Transmission Speed 3.2 Gbit/s"]
+[2.7367489337921143, -3.198746919631958, "Satellite Communication Technology Internet Access Disparities Reduction Verified"]
+[2.718897819519043, -3.126403331756592, "Satellite Communication Technology Emergency Communications Testing Verified"]
+[5.12880802154541, -4.2237868309021, "Satellite Mission Operation Start Date 2010"]
+[5.1389546394348145, -4.161323070526123, "Satellite Mission Operation Start Date 2008"]
+[-5.384702205657959, 2.861513614654541, "Ultraviolet Spectrography Telescope Objective Study extended sources of EUV bands"]
+[-5.262165069580078, 2.876718282699585, "Ultraviolet Spectrography Telescope Data Provided Jovian system EUV data"]
+[-3.115647792816162, 1.7527496814727783, "Satellite Mission Redundancy Approach Cold redundancy and use radiation-hardened qualified components"]
+[-3.174793243408203, 1.7557610273361206, "Satellite Mission Design Material Plastic"]
+[-3.176589012145996, 1.6999434232711792, "Satellite Mission Purpose of Models Visualize orientation and explain the mission easily"]
+[0.4715067148208618, 9.371025085449219, "Attitude Control Quantity 4"]
+[0.5026324987411499, 9.418218612670898, "Attitude Determination Quantity 3"]
+[0.4777088463306427, 9.362886428833008, "Attitude Control Usage Safe modes"]
+[1.0475947856903076, 9.137412071228027, "Attitude and Orbit Control Subsystem Configuration Presented in Table 2"]
+[0.5854230523109436, 9.190836906433105, "Reaction Control Subsystem Thrusters 9 of 11 N"]
+[-5.2429633140563965, 8.1985445022583, "RF Communications System TC Demodulation Scheme PSK (Phase Shift Keying)/PCM (Pulse Code Modulation)"]
+[-5.261484622955322, 8.072161674499512, "RF Communications System Date Rate 4 kbit/s"]
+[2.632552146911621, 13.441534042358398, "Optical Component Function Blocks stray light from the Moon and the Earth limb"]
+[-0.772430419921875, 8.824345588684082, "Thermal Control Device Construction Pyrolytic graphite film for the flexible section and aluminum terminals on each end"]
+[-1.7819229364395142, 8.43321704864502, "Electronics Manufacturer Ecliptic Enterprises"]
+[-1.7750203609466553, 8.44526195526123, "Electronics Function Powering, configuring, and reading pixel data from the imager"]
+[0.676882803440094, 11.873358726501465, "Sensors Purpose Assess space weather"]
+[3.6605191230773926, 22.952133178710938, "Instrument Conference Date Jan. 30- Feb. 2, 2006"]
+[-6.6777215003967285, 9.976731300354004, "Receiver and Antenna Connection Commercial Rubidium clock"]
+[-6.650838375091553, 9.949848175048828, "Receiver and Antenna Location IEN (Istituto Elettrotecnico Nazionale), Torino, Italy"]
+[-6.648975372314453, 9.922757148742676, "Receiver and Antenna Time Reference IEN time"]
+[1.1204413175582886, -0.842870831489563, "Satellite Outer Diameter 47.5 cm"]
+[1.034550666809082, -4.42712926864624, "Satellite Mass 39 kg"]
+[2.0540518760681152, -2.7092480659484863, "Satellite Number of Mirrors 878"]
+[6.3074798583984375, 7.431850910186768, "Satellite Component Number of Mirrors 499"]
+[6.290316581726074, 7.448182106018066, "Satellite Component Number of Mirrors 399"]
+[-8.490066528320312, 13.668582916259766, "Parameter Requirement Value 100"]
+[-8.559245109558105, 13.606928825378418, "Parameter Requirement Value 8%(PAN) 12%(MS)"]
+[-8.511125564575195, 13.688092231750488, "Parameter Requirement Value 0.7 m(PAN), 2.8 m(MS)"]
+[-8.55191707611084, 13.750439643859863, "Parameter Requirement Value 1.2 km"]
+[-8.506067276000977, 13.686074256896973, "Parameter Requirement Value 70 m CE90"]
+[-8.511018753051758, 13.67420768737793, "Parameter Validated Value 13%(PAN), 19%(MS)"]
+[-8.535774230957031, 13.668940544128418, "Parameter Requirement Value 0.5pixel RMS (MS)"]
+[-8.506416320800781, 13.661816596984863, "Parameter Requirement Value 3.5 m CE90 (Horizontal)"]
+[1.0560938119888306, -2.1064629554748535, "Satellite Attitude Accuracy 0.4\u00ba in roll and pitch, 0.5\u00ba in yaw"]
+[0.7102553844451904, -4.135659217834473, "Satellite Launch Mass 442 kg"]
+[0.9560155868530273, -4.348418235778809, "Satellite Dry Mass 429 kg"]
+[5.293904781341553, -2.205716848373413, "Satellite Design Life 5 years"]
+[-0.9328945279121399, -10.024004936218262, "Satellite Constellation Revisit Rate Up to 40 times in a day"]
+[1.8227208852767944, -0.5966219902038574, "Earth-imaging Satellites Quantity 18"]
+[1.7041382789611816, -0.6375590562820435, "Earth-imaging Satellites Size About the size of a mini-fridge"]
+[1.774801254272461, 8.442940711975098, "Data Handling Subsystem Processor 32 bit RISC processor (Renesas Technology, SH-4, 300 MIPS)"]
+[-5.240518093109131, 7.869119644165039, "Communication System Modulation BPSK (Binary Phase Shift Keying)"]
+[-5.193238258361816, 7.77908182144165, "Communication System Data Rate 10 Mbit/s"]
+[-5.216490745544434, 7.921029090881348, "Communication System Output Power 200 mW"]
+[0.1272972971200943, 13.208370208740234, "Metrology Sensor Commissioning Sequence Relative GPS sensors, CLS, FLLS"]
+[0.580524206161499, 12.145834922790527, "Coarse Lateral Sensor Commissioning Approach Incremental"]
+[-5.353888988494873, 7.832648754119873, "Communications Instrument Type Communications"]
+[-1.1614426374435425, 15.104540824890137, "Imaging multi-spectral radiometers (vis/IR) Instrument Type Imaging multi-spectral radiometers (vis/IR)"]
+[-2.9819495677948, 16.15528678894043, "Scatterometers Instrument Type Scatterometers"]
+[0.818997859954834, 4.0919013023376465, "Atmospheric chemistry Instrument Type Atmospheric chemistry"]
+[-1.3058243989944458, 15.0994873046875, "Imaging multi-spectral radiometers (passive microwave) Instrument Type Imaging multi-spectral radiometers (passive microwave)"]
+[2.741787910461426, -3.2501633167266846, "Satellite Communication System Internet Connection Speed 155 Mbit/s"]
+[2.6833503246307373, -3.1919162273406982, "Satellite Communication System Residential User Terminal Diameter 45 cm"]
+[2.7226643562316895, -3.237839460372925, "Satellite Communication System Business Terminal Diameter 5 m"]
+[-6.986296653747559, 11.2051362991333, "Active Phased Array Antenna Function First hopping spot beam antenna"]
+[-6.962590217590332, 11.143415451049805, "Active Phased Array Antenna Performance Working well"]
+[-3.375380516052246, 4.380088806152344, "Resupply Spacecraft Launch Date 17 November 2018"]
+[-3.3752028942108154, 4.412150859832764, "Resupply Spacecraft End of Life Date 25 February 2019"]
+[-3.269744873046875, 5.431775093078613, "Launch Vehicle Liftoff Time 04:01:22 EST (09:01:22 UTC)"]
+[1.7928465604782104, 22.086923599243164, "Instrument Atmospheric Volume Footprint 100 km x 100 km"]
+[1.6732521057128906, 22.185314178466797, "Instrument HMDA Window Size 40 cm"]
+[2.487464666366577, 22.750694274902344, "Instrument Hitchhiker Video Interface Units (HVIUs) 2"]
+[2.8223211765289307, 22.288471221923828, "Instrument Digital VCR (Video Cassette Recorder) Data Recording System"]
+[-2.9537694454193115, 20.18631935119629, "Spectral Band Wavelength Range 365-408 nm"]
+[-2.956605911254883, 20.165611267089844, "Spectral Band SNR 260"]
+[-2.5630109310150146, 19.96809196472168, "Spectral Band FOV 400 km x 0.5 km"]
+[-2.8731918334960938, 20.261018753051758, "Spectral Band Number of Pixels 1600"]
+[-2.9719324111938477, 20.15991973876953, "Spectral Band Wavelength Range 660-685 nm"]
+[-3.0057883262634277, 20.190601348876953, "Spectral Band SNR 160"]
+[-2.9751296043395996, 20.139802932739258, "Spectral Band Polarization Angle 0/60/120 \u00ba"]
+[-2.9069485664367676, 20.220935821533203, "Spectral Band Number of Pixels 1600"]
+[-2.9810850620269775, 20.159149169921875, "Spectral Band Wavelength Range 862-877 nm"]
+[-2.966693878173828, 20.187509536743164, "Spectral Band SNR 400"]
+[-2.888277292251587, 20.241764068603516, "Spectral Band Number of Pixels 1600"]
+[-2.949481725692749, 20.180423736572266, "Spectral Band Wavelength Range 1360-1390 nm"]
+[-3.0513904094696045, 20.19240379333496, "Spectral Band SNR 180"]
+[-3.0307793617248535, 20.208337783813477, "Spectral Band Number of Pixels 800"]
+[-2.9744601249694824, 20.17023468017578, "Spectral Band Wavelength Range 1628-1654 nm"]
+[-2.9777348041534424, 20.174480438232422, "Spectral Band SNR 110"]
+[-2.976663589477539, 20.141254425048828, "Spectral Band Polarization Angle 0/60/120 \u00ba"]
+[-3.0857975482940674, 20.251523971557617, "Spectral Band Number of Pixels 800"]
+[3.6922624111175537, -2.0712544918060303, "Satellite Data Collection 25 years"]
+[-4.478745937347412, 15.904251098632812, "Radar Technique Precision Up to two orders of magnitude better than speckle tracking"]
+[-0.9376051425933838, 7.645223617553711, "Product Ice Movement Resolution 20 cm/year in speed and 5 degrees in annual flow direction"]
+[0.48013541102409363, 9.370073318481445, "Attitude Software Performance Solid"]
+[-1.935670018196106, 7.545978546142578, "Operating System Functionality Turns the torquers off while reading from the magnetometer"]
+[0.7086514830589294, 11.932845115661621, "Sensors Processing Algorithm Logic added to improve performance"]
+[-0.4953809380531311, 8.644987106323242, "Actuators Functionality Apply counter dipoles"]
+[0.46310675144195557, 9.663741111755371, "Extended Kalman Filter Performance Good to around 1.5\u00ba in sunlight"]
+[2.8663554191589355, 21.97918128967285, "Instrument Purpose Accurate monitoring of Transient Luminous Event in the upper atmosphere"]
+[0.05767593905329704, 15.337214469909668, "Electron Spectrometer Purpose Measure electrons"]
+[1.0090941190719604, -4.291154861450195, "Satellite Per spacecraft mass 2500 kg"]
+[-0.8372719287872314, 0.1296432912349701, "Satellite System Number of satellites per system 6"]
+[2.203763961791992, -2.6790242195129395, "Satellite Total system cost $850 million"]
+[-0.8353369832038879, 0.15044304728507996, "Satellite System Total system cost $600 million"]
+[1.3943586349487305, -1.0569549798965454, "Satellite Nadir resolution 31 cm"]
+[-0.8247061967849731, 0.1574491262435913, "Satellite System Nadir resolution 29 cm"]
+[2.2287046909332275, -2.3559224605560303, "Satellite Daily system capacity 1x"]
+[-0.8353028297424316, 0.1498745232820511, "Satellite System Daily system capacity 3x"]
+[-3.0234944820404053, 4.412647724151611, "Spacecraft Wet Mass 300 kg"]
+[-2.9533114433288574, 4.27871036529541, "Spacecraft Size 985 mm x 1440 mm x 1238 mm"]
+[-3.0199646949768066, 4.244011402130127, "Spacecraft Solar Panel Layout Asymmetric solar sail concept"]
+[-3.0458498001098633, 4.2376275062561035, "Spacecraft Thruster Type Monopropellant"]
+[5.261902332305908, -3.9854931831359863, "Satellite Launch Date 2018"]
+[0.6857085824012756, 12.027676582336426, "Sensor Manufacturer ITT Exelis of Rochester, N.Y."]
+[0.6681758761405945, 12.015033721923828, "Sensor Type Thermal and Near-Infrared Sensor for carbon Observation-Fourier Transform Spectrometer"]
+[0.7340067028999329, 12.021108627319336, "Sensor Manufacturer Harris Corp."]
+[0.6991986632347107, 12.024490356445312, "Sensor Location Melbourne FL USA"]
+[-1.0612412691116333, 7.800483703613281, "Device Polarization Modes Single (HH/VV/HV), dual (HH + HV=VV + VH), quad (HH + HV + VV + VH), and compact polarimetry (Tx: oriented 45\u00ba or circular, Rx: H or V)"]
+[-5.870426177978516, 15.98620891571045, "Synthetic Aperture Radar CP Mode Polarization Linear polarization oriented at 45\u00ba or circular (LHCP or RHCP)"]
+[-5.864351272583008, 15.986284255981445, "Synthetic Aperture Radar CP Mode Polarization Selectable by command"]
+[2.0264248847961426, 22.21156120300293, "Instrument Field of View Very large"]
+[2.094815492630005, 22.397829055786133, "Instrument Telescope Sensitivity 1 m-class"]
+[-7.515979766845703, 5.940418720245361, "Camera Cadence 25 seconds"]
+[-7.5821332931518555, 5.9069952964782715, "Camera Star Magnitude Fainter than mV = 8"]
+[-7.585638523101807, 5.8666887283325195, "Camera Cadence 2.5 seconds"]
+[-7.57610559463501, 5.877918243408203, "Camera Star Magnitude Range 4 to 8"]
+[-5.344356536865234, 2.9205379486083984, "Telescope Optical Unit Number of Lenses 6"]
+[2.450000762939453, 22.75554847717285, "Instrument Number of Normal Cameras 24"]
+[2.5081965923309326, 22.75348663330078, "Instrument Number of Fast Cameras 2"]
+[1.824283480644226, 22.11212158203125, "Instrument Footprint 1 km x 1 km"]
+[2.5204434394836426, 22.592512130737305, "Instrument Scan Capability None"]
+[2.81705379486084, 22.319414138793945, "Instrument Control 3-axis"]
+[3.0125772953033447, 22.465757369995117, "Instrument Manufacturer Thoth Technology Inc."]
+[2.7327818870544434, 22.265172958374023, "Instrument Location York University, Toronto, Canada"]
+[2.5194365978240967, 22.098634719848633, "Instrument Measurement Objective Collect information on orbital debris"]
+[2.078399896621704, 22.47468376159668, "Instrument Time of Impact Resolution 0.1 s"]
+[1.7051517963409424, 22.169921875, "Instrument Detector Size 4 cm x 8 cm"]
+[2.845184803009033, 22.380285263061523, "Instrument Impact Event Record Storage S/C control unit"]
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+[-3.042543888092041, 7.023874282836914, "Command and Data Handling System Processor Innoflight CFC-300"]
+[-3.1048409938812256, 7.067440986633301, "Command and Data Handling System Data Storage Capacity 13.4 GB"]
+[-3.0339198112487793, 7.018139362335205, "Command and Data Handling System Data Storage Duration More than 28 days"]
+[-3.0490758419036865, 7.028299331665039, "Command and Data Handling System Health Monitoring Temperature, battery voltage"]
+[-3.0409960746765137, 7.013548851013184, "Command and Data Handling System Ground Contact Reset Full reset after a prolonged period without ground contact"]
+[0.9349678158760071, -4.270066738128662, "Satellite RCS Fuel Capacity 34.3 kg"]
+[0.7450538873672485, -1.188698649406433, "Satellite Altitude Descent From 393 km to 270 km"]
+[-2.1940174102783203, 6.004642963409424, "Flight Dynamics System Interference Analysis Frequency Daily"]
+[1.8711621761322021, -2.2085232734680176, "Satellite Collision Avoidance ISS Orbit"]
+[-1.8909273147583008, 14.858811378479004, "Radiometer Device Type Differential absolute radiometer"]
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+[-1.891511082649231, 14.867406845092773, "Radiometer Apertures per Channel 2"]
+[2.712118148803711, 23.216140747070312, "Instrument Communication General Orbiter services, including power control, command, and telemetry"]
+[2.8758280277252197, 22.93509864807129, "Instrument Operation Remote POCC (Payload Operations and Control Center)"]
+[0.1363116204738617, 7.200904846191406, "Experiment Start Time 16:52 on Nov. 28, 2012 (UT)"]
+[0.19723960757255554, 7.2361555099487305, "Experiment End Time 17:52 Nov. 28, 2012 (UT)"]
+[0.09084029495716095, 7.1476898193359375, "Experiment Data Collection Interval 1 minute"]
+[2.0406932830810547, -1.215259075164795, "Satellite Imaging Capability Full continental coverage of Antarctica"]
+[2.4361562728881836, -1.284333348274231, "Satellite Data Capture From the South Pole to the coast"]
+[2.836642265319824, -1.5069581270217896, "Satellite Image Credit NASA/JPL, UCI, ESA, CSA, JAXA"]
+[-2.0935797691345215, 7.687349319458008, "Computer System Operating System RTOS based on TRON"]
+[-2.3601574897766113, 7.395077228546143, "Real-Time Operating System Usage About 60% of the RTOS implementations in the embedded equipment market"]
+[-1.870434284210205, 6.981826305389404, "Development Environment Platform Eclipse-based embedded software integrated development environment"]
+[1.5213725566864014, -2.29229998588562, "Satellite Stabilization Three-axis"]
+[5.3398518562316895, -4.466728687286377, "Satellite Launch Date Fall of 1974"]
+[1.2792203426361084, -1.9841952323913574, "Satellite Pointing Accuracy Greater"]
+[2.088660717010498, -2.4704489707946777, "Satellite Cost Increased"]
+[-2.3695130348205566, 11.874361038208008, "Cloud and Aerosol Polarization Imager Measurement Channels 5"]
+[-2.3074471950531006, 11.926493644714355, "Cloud and Aerosol Polarization Imager Effective for sensors with few channels True"]
+[-3.0243756771087646, 4.277858734130859, "Spacecraft Primary Objective Testing of the spacecraft launch, orbital, reentry, and recovery systems"]
+[-3.2211756706237793, 5.195470809936523, "Exploration Vehicle Design Purpose Carrying crew to space, providing emergency launch abort capabilities, sustaining the crew during space travel, and providing reentry from deep space return velocities"]
+[16.653457641601562, 6.9434051513671875, "Communications Minisatellite Mission 168 kg"]
+[16.795408248901367, 6.902231216430664, "Microsatellite Mass ~100 kg"]
+[16.83108139038086, 6.87267541885376, "Microsatellite Mass 11 kg"]
+[16.80970573425293, 6.887020111083984, "Microsatellite Mass 100 kg"]
+[11.886574745178223, 5.280668258666992, "3U CubeSat Mass 3.5 kg"]
+[11.768129348754883, 5.391268730163574, "1U and 2U CubeSats Mission Technology demonstration"]
+[11.887762069702148, 5.28626823425293, "3U CubeSat Mass 4 kg"]
+[11.885252952575684, 5.287073612213135, "3U CubeSat Mass 4 kg"]
+[11.841833114624023, 5.326998710632324, "3U CubeSat Mission Measure the global magnetic field and radiation"]
+[-7.5634074211120605, 5.898525238037109, "Camera Imaging Bands One panchromatic and four multispectral (MS)"]
+[2.746746301651001, 13.754682540893555, "Electro-Optical Subsystem Components Telescope, FPA (Focal Plane Assembly), SPM (Signal Processing Module)"]
+[3.7670061588287354, 17.72445297241211, "Payload Management Subsystem Components TPM (Thermal & Power Module), MCM (Mass storage and Control Module)"]
+[16.80558967590332, 6.888899326324463, "Microsatellite Mass 100 kg"]
+[-2.1615052223205566, 5.5035200119018555, "Deployment System Unknown Unknown"]
+[-2.3738677501678467, 5.021280288696289, "Artificial Debris Targets Quantity Two"]
+[16.894628524780273, 6.821526527404785, "Microsatellite Technologies for Debris Removal Net capture, harpoon capture, vision-based navigation"]
+[-1.6732221841812134, 11.232940673828125, "Lidar Wavelengths 1064, 532, 355 nm"]
+[-1.675731897354126, 11.228816032409668, "Lidar Depolarization Measurements At all wavelengths"]
+[-1.6860270500183105, 11.240480422973633, "Lidar Primary Objective Continue the CALIPSO aerosol and cloud profile data record"]
+[-1.6499618291854858, 11.214112281799316, "Lidar Secondary Objective Support operational applications such as air quality and special event monitoring"]
+[-1.6856237649917603, 11.231831550598145, "Lidar Mission Goals Extend CALIPSO data record, Improve operational aerosol forecasting programs"]
+[-3.0019047260284424, 4.302200794219971, "Spacecraft Pointing Constraints Stringent"]
+[-3.0351927280426025, 4.270489692687988, "Spacecraft \u0394V Control Reasonable Margins"]
+[-3.0536725521087646, 4.3090643882751465, "Spacecraft Safety Needs to be ensured throughout the whole RVX mission"]
+[-3.0215985774993896, 4.1960859298706055, "Spacecraft Trajectory Profile Highly elliptical orbit"]
+[-3.0899605751037598, 4.172298431396484, "Spacecraft Mission Constraints Sun pointing attitude and Sun-aligned configuration"]
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+[2.8850202560424805, 22.057111740112305, "Instrument Purpose Space weather monitoring"]
+[3.173719882965088, 22.472318649291992, "Instrument URL http://www.goes-r.gov/spacesegment/suvi.html"]
+[-0.41431084275245667, 14.508188247680664, "Imaging Instrument Spatial Resolution 2-8 m"]
+[-0.4151581823825836, 14.495428085327148, "Imaging Instrument Spatial Resolution 16 m"]
+[-0.4150198996067047, 14.513496398925781, "Imaging Instrument Spatial Resolution 55 m"]
+[-0.4154494106769562, 14.518486022949219, "Imaging Instrument Swath Width 92 km"]
+[-0.41917479038238525, 14.523137092590332, "Imaging Instrument Swath Width 95 km"]
+[-0.4380808174610138, 14.555000305175781, "Imaging Instrument Swath Width 684 km"]
+[-8.475552558898926, 13.702054977416992, "Parameter Range of measurements 3-4"]
+[-8.5325345993042, 13.660679817199707, "Parameter Error \u00b11.0 K"]
+[-8.502922058105469, 13.703359603881836, "Parameter Range of measurements 20%"]
+[-8.528231620788574, 13.686293601989746, "Parameter Error \u00b12 m/s"]
+[-8.501976013183594, 13.707662582397461, "Parameter Range of measurements 16 km"]
+[-8.486076354980469, 13.724835395812988, "Parameter Range of measurements Up to 45 km"]
+[-8.494357109069824, 13.69179630279541, "Parameter Range of measurements 0-5 g/cm2"]
+[-8.56776237487793, 13.661417961120605, "Parameter Error \u00b11.5 K"]
+[-8.525583267211914, 13.67284107208252, "Parameter Error \u00b10.25 g/cm2"]
+[-8.455140113830566, 13.704303741455078, "Parameter Range of measurements 0-5 kg/m2"]
+[-8.524039268493652, 13.66956901550293, "Parameter Error \u00b10.2 kg/cm2"]
+[-8.525304794311523, 13.680595397949219, "Parameter Error \u00b13.0 K"]
+[-8.505807876586914, 13.698949813842773, "Parameter Range of measurements 0-25 mm/h"]
+[-8.538801193237305, 13.668404579162598, "Parameter Error \u00b15.0 mm/h"]
+[-8.51824951171875, 13.741272926330566, "Parameter Range of measurements Up to 1.5 m"]
+[-8.553589820861816, 13.65537166595459, "Parameter Error \u00b10.2 m"]
+[-8.46119499206543, 13.733380317687988, "Parameter Range of measurements Up to 16 km"]
+[-7.50726842880249, 5.948037624359131, "Camera Module Proton Shield Material Copper"]
+[-7.5088090896606445, 5.935432434082031, "Camera Module Power Line Voltage +27 V"]
+[-3.592233419418335, 7.331675052642822, "Data Acquisition System ADCs Resolution 14 bit"]
+[-3.410325765609741, 8.040007591247559, "Digital Signal Processor Data Transmission Energy, position and time information"]
+[1.8755803108215332, -0.23547114431858063, "Radar Imaging Satellite Launch Date April 2012"]
+[1.8723267316818237, -0.19516120851039886, "Radar Imaging Satellite End of Service Date March 2017"]
+[1.8667597770690918, -0.24230439960956573, "Radar Imaging Satellite Mission Purpose Utilise all-weather, day-and-night SAR (Synthetic Aperture Radar) for applications in agriculture, geology, flood monitoring, and more"]
+[1.7945765256881714, -2.0357508659362793, "Satellite Meteorological Program European meteorological program in GEO (Geostationary Orbit)"]
+[4.980669975280762, -3.781674861907959, "Satellite Initiated 1972"]
+[3.0326449871063232, -1.6172183752059937, "Satellite Predecessor Organization ESRO (European Space Research Organization)"]
+[4.792408466339111, -3.7307140827178955, "Satellite Proposal Acceptance 1972"]
+[0.8981379866600037, 14.789674758911133, "Instrumentation Science Objectives Address the questions listed"]
+[0.9014959931373596, 14.80443000793457, "Instrumentation Consortium European Institutes and Industries from Belgium, Czech Republic, France, Germany, Greece, Italy, Luxembourg, Russia, and the UK"]
+[2.7349088191986084, 22.39646339416504, "Instrument Type Scatterometers"]
+[2.6750619411468506, 22.399391174316406, "Instrument Type Imaging multi-spectral radiometers (passive microwave)"]
+[-0.4128464460372925, 14.522814750671387, "Imaging Instrument Cadence 30-minute"]
+[4.844456672668457, -3.633868932723999, "Satellite Launch Schedule 24 to 36 months from satellite contract to launch"]
+[2.9646921157836914, -1.8284674882888794, "Satellite Operator Launches Per Year 3 to 4 missions"]
+[-13.525116920471191, -2.0382192134857178, "X-ray Survey Band 1/4 keV"]
+[2.4988601207733154, 22.823381423950195, "Instrument Response Time Minutes"]
+[-0.5527654886245728, 8.131220817565918, "Structures Handling Must be handled differently"]
+[5.3591628074646, -2.165670156478882, "Satellite Design Life 6 years"]
+[2.225421905517578, -1.264878511428833, "Satellite Image Capture More than 10,000 images of the globe"]
+[2.797142744064331, -1.3310023546218872, "Satellite Image Distribution To government agencies, educational institutions, and commercial use"]
+[-1.8835515975952148, 14.852913856506348, "Radiometer Instrument Type Multiple direction/polarisation radiometers"]
+[-1.883484125137329, 14.864889144897461, "Radiometer Instrument Type Multiple direction/polarisation radiometers"]
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+[-0.5230067372322083, 1.2517399787902832, "Precision orbit Instrument Type Precision orbit"]
+[-3.611682891845703, 7.1428704261779785, "Data Delivery System Data Usage Atmospheric temperature profiles, cloud top height and temperature, sea surface temperature, specific humidity profiles, integrated water vapor measurements, cloud cover maps, land surface temperature, horizontal winds, total column ozone, and cloud type discrimination"]
+[0.16940148174762726, 11.962409973144531, "Lightning Detection Sensor Purpose Observe regional lightning activity in China"]
+[0.30340105295181274, 12.042848587036133, "Lightning Detection Sensor Products Forecasting and warning of convection precipitation, and studying of Earth's electric field"]
+[-0.04635905474424362, 15.607236862182617, "Spectrometer Usage Confirm the existence of the three planets"]
+[-4.533700942993164, -3.059080123901367, "Exoplanets Mass Between 0.5 and 1.7 times Jupiter\u2019s mass"]
+[-4.551553249359131, -3.067809820175171, "Exoplanets Size Slightly smaller to more than 1.6 times the size of Jupiter"]
+[-4.56207275390625, -3.091020345687866, "Exoplanets Density From styrofoam-like to three times denser than water"]
+[0.5553389191627502, -1.4174609184265137, "Satellite Orbit Altitude Same altitude"]
+[1.5186102390289307, -2.3243062496185303, "Satellite Orbit Pole to pole"]
+[3.444061756134033, -2.5594489574432373, "Satellite Orbit Frequency About 15 times a day"]
+[0.845905601978302, -1.390122890472412, "Satellite Distance Between Satellites Varies ever so slightly depending on the mass of Earth\u2019s surface below"]
+[-2.124999523162842, 5.4933953285217285, "Deployment System Size 15-inch"]
+[-6.703741550445557, 9.972341537475586, "Communication Antennas Quantity 4"]
+[-0.1344110667705536, 9.06744384765625, "Navigation Equipment Quantity 2"]
+[-1.6063652038574219, 9.668418884277344, "Propulsion System Total Impulse 1000 Newton-seconds"]
+[-1.6065367460250854, 9.669867515563965, "Propulsion System Maximum Thrust 1 Newton"]
+[-1.6134834289550781, 9.65589714050293, "Propulsion System Total Impulse 6000 Newton-seconds"]
+[-1.6143046617507935, 9.682944297790527, "Propulsion System Maximum Thrust 350 micronewtons"]
+[-3.3388283252716064, 7.508922100067139, "Data Processing Algorithm Function Remove non-lightning events from the data stream"]
+[-3.3086981773376465, 7.515946388244629, "Data Processing Algorithm Function Identify flashes by reviewing the remaining events"]
+[-3.284750461578369, 7.499117851257324, "Data Processing Algorithm Function Remove events not caused by lightning, including radiation hits and glint from Sun on the ocean"]
+[-3.344804286956787, 7.4463887214660645, "Data Processing Algorithm Function Rely on the fact that true lightning events are coherent in time and space, whereas noise events are not"]
+[0.5634025931358337, -1.5170248746871948, "Satellite Orbit Altitude 35786 km"]
+[0.7905310392379761, -2.1138083934783936, "Satellite Orbit Longitude 104.7\u00ba E"]
+[1.46833336353302, 2.6560513973236084, "GEO Weather Satellite Launch Date June 02, 2021"]
+[1.480909824371338, 2.653571128845215, "GEO Weather Satellite Launch Time 17:29 UTC"]
+[1.487968921661377, 2.6388816833496094, "GEO Weather Satellite Mass ~5300 kg"]
+[1.5095335245132446, 2.5728514194488525, "GEO Weather Satellite Orbit Altitude 35786 km"]
+[1.4926633834838867, 2.566251277923584, "GEO Weather Satellite Orbit Longitude 123.5\u00ba E"]
+[-6.680757522583008, 9.94360637664795, "Antenna Function Reception of uplinked command stream"]
+[-1.1404229402542114, 6.902315139770508, "Assembly Receiver Receives uplinked command stream"]
+[1.8984975814819336, 8.605610847473145, "Subsystem Battery Capacity 66 Ah"]
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+[1.8971545696258545, 8.608237266540527, "Subsystem Solar Array Placement On the top and side exterior surface of the satellites"]
+[2.5466294288635254, -2.117274284362793, "Satellite Signal Transmission L1 and E5"]
+[-2.5872223377227783, 7.970727443695068, "Clock Configuration Driven by the RAFS Flight Model 4 (RAFS FM4)"]
+[-4.9370856285095215, 9.784958839416504, "Receiver Number of Galileo Channels 7"]
+[-4.920137882232666, 9.750877380371094, "Receiver Frequency Band L1 1574.42 MHz"]
+[-4.938931941986084, 9.749963760375977, "Receiver Frequency Band E5a 1176.45 MHz"]
+[-4.9522929191589355, 9.753403663635254, "Receiver Frequency Band E5b 1207.14 MHz"]
+[-4.9300947189331055, 9.742753028869629, "Receiver Frequency Band E5a+b (AltBOC) 1191.795 MHz"]
+[11.808812141418457, 5.303831100463867, "6U CubeSat Mission Type Non-EO"]
+[11.773025512695312, 5.345077037811279, "6U CubeSat Launch Date 27 Sept 2021"]
+[11.805745124816895, 5.304588317871094, "6U CubeSat Science Objectives Answer fundamental questions in plasma physics and space weather"]
+[0.7268301844596863, 11.96142578125, "Sensors Data Processing Daily images"]
+[0.7386149764060974, 11.983552932739258, "Sensors Grid Cell Area Roughly 25 km by 25 km (15 miles by 15 miles)"]
+[0.7500777244567871, 11.968881607055664, "Sensors Minimum Sea Ice Coverage 15 percent of the water"]
+[0.4734402000904083, 4.529182434082031, "Natural Phenomenon Maximum Extent Decline Roughly 13 percent per decade"]
+[0.43862366676330566, 4.551109313964844, "Natural Phenomenon Minimum Extent Decline About 2.7 percent per decade"]
+[-0.16334187984466553, 15.575274467468262, "Spectrometer Band Wavelength 135.6 nm"]
+[0.04610953852534294, 15.448627471923828, "Spectrometer Launch Year 2018"]
+[-0.12022112309932709, 15.562273025512695, "Spectrometer Mission Purpose Ionosphere observations"]
+[-0.09816890209913254, 15.524828910827637, "Spectrometer Data Visualization March 2019"]
+[7.26667594909668, 12.407211303710938, "Satellite Instrument Measurement Type Arctic sea ice extent"]
+[7.462451934814453, 12.577081680297852, "Satellite Instrument Measurement Date September 18, 2019"]
+[-0.1298535019159317, 13.617095947265625, "Measurement Definition Total area in which the ice concentration is at least 15 percent"]
+[5.035056114196777, -4.357285022735596, "Satellite Operational Date Feb. 5, 2014"]
+[2.5796897411346436, -3.896275520324707, "Satellite URL http://www.imd.gov.in/section/satmet/dynamic/insat_3d.htm"]
+[2.549952983856201, -1.7598295211791992, "Satellite Initial Products http://www.isro.org/pdf/insat-3d-imager.pdf"]
+[-13.601158142089844, -2.096290349960327, "X-ray Observatory Energy Range (Red) 300 to 1,000 electron volts (eV)"]
+[-13.516796112060547, -2.035038948059082, "X-ray Observatory Energy Range (Green) 1,000 to 3,000 eV"]
+[-13.494308471679688, -2.022510528564453, "X-ray Observatory Energy Range (Blue) 3,000 to 10,000 eV"]
+[-6.533357620239258, 10.062418937683105, "Electromagnetic Radiation Energy Range About 2 to 3 eV"]
+[-13.502374649047852, -2.0285110473632812, "X-ray Observatory Energy Range Three times higher than Chandra detects"]
+[2.626093626022339, 14.313274383544922, "Optical Instrument Diffraction Pattern Precision \u00b11%"]
+[-1.1654597520828247, 3.049696922302246, "Celestial Object Description Finite set of non-coherent source points"]
+[-1.1870779991149902, 3.0627851486206055, "Celestial Object Intensity Variations Neglected"]
+[-0.40428054332733154, 16.212026596069336, "Spectrograph Wavelength Range 132 to 162 nm"]
+[-0.40687841176986694, 16.208707809448242, "Spectrograph Entrance Slit Widths 0.2 mm and 0.4 mm"]
+[-0.41230258345603943, 16.195083618164062, "Spectrograph Spectral Resolutions 0.2 nm and 0.4 nm"]
+[-1.0791387557983398, 5.551366329193115, "Facility Concept Compactness, self-automation, high speed, user oriented"]
+[-1.0954499244689941, 5.434629440307617, "Facility Function Monitoring and control of orbit and attitude of the satellite, planning and management of the satellite bus operation plan, reception and management of imaging plan, processing of the image data and storage and management of the product"]
+[0.758762001991272, -1.5302271842956543, "Satellite Super-Synchronous Deployment Perigee 185 km"]
+[0.6722936034202576, -1.5860438346862793, "Satellite Super-Synchronous Deployment Apogee 60,000 km"]
+[0.8380671143531799, -1.7022967338562012, "Satellite Science Target Orbit Perigee 300 km"]
+[0.6833672523498535, -1.58039128780365, "Satellite Science Target Orbit Apogee 60,000 km"]
+[0.7331374287605286, -2.300488233566284, "Satellite Science Target Orbit Inclination >27\u00ba"]
+[-1.6900895833969116, 5.8968610763549805, "Maneuver Total \u0394V 40 m/s"]
+[-1.638466238975525, 5.956092357635498, "Maneuver Total propellant used 9 g"]
+[-1.6929144859313965, 5.882748603820801, "Maneuver Total \u0394V 85 m/s"]
+[-1.6762845516204834, 5.903899192810059, "Maneuver Total propellant used 28.6 g"]
+[-1.6961607933044434, 5.869471549987793, "Maneuver Total \u0394V 55 m/s"]
+[-1.6553212404251099, 5.906244277954102, "Maneuver Total propellant used 23 g"]
+[-0.41991233825683594, 14.516870498657227, "Imaging Instrument Mesoscale Image Collection Interval 30 seconds"]
+[-0.42295604944229126, 14.520806312561035, "Imaging Instrument CONUS Image Collection Interval 5-minute (300-second)"]
+[-0.39811545610427856, 14.485998153686523, "Imaging Instrument Full Disk Swath Collection Interval 30 seconds"]
+[-13.855619430541992, -2.205052614212036, "X-ray Telescope Throughput Unknown"]
+[-13.871499061584473, -2.2248878479003906, "X-ray Telescope Data Telemetry Time and position information of every photon measured by the MCP"]
+[-13.880894660949707, -2.2321174144744873, "X-ray Telescope Imaging Rate Hundreds of counts/s over the FOV"]
+[-5.130155563354492, 8.949153900146484, "RF Module Peak Power 10 W"]
+[-5.143962383270264, 8.943800926208496, "RF Module Duty Cycle ~ 7%"]
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+[1.3943476676940918, -3.079951047897339, "Satellites Number of Satellites 2"]
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+[0.95960533618927, 0.8297536373138428, "Earth Observation Company Constellation Expansion From 12 to 14 high-resolution satellites"]
+[0.9567739367485046, 0.8436298370361328, "Earth Observation Company Daily Revisit Rate 8 to 10 times a day"]
+[3.4802844524383545, 10.554336547851562, "Amplifier Ports 8"]
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+[-4.427553176879883, 7.5755815505981445, "Constant Bit Rate Elevation Threshold 20\u00b0"]
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+[-4.440072536468506, 7.572023868560791, "Variable Bit Rate Transition Time Percentage 5% with 3-bit rates"]
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+[0.4816102683544159, 4.52997350692749, "Natural Phenomenon Decline Start Date 4 February 2020"]
+[-5.32568883895874, 3.0892624855041504, "Telescope Array Energy Band 5 - 80 keV"]
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+[-2.983834981918335, 4.4555768966674805, "Spacecraft Cargo Capacity Over 1630 kg"]
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+[3.7331531047821045, -1.6094672679901123, "Satellite Operation Status Nominal"]
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+[0.6308114528656006, 12.033675193786621, "Sensor Purpose Laser long-path absorption measurements of atmospheric trace species"]
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+[5.246655464172363, -4.05657958984375, "Satellite Launch Date 2018"]
+[-3.096806049346924, 2.421393394470215, "SweepSAR Mission Launch Date 2020"]
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+[2.955225944519043, -1.4532526731491089, "Satellite Mission Biomolecule-detection"]
+[3.0040946006774902, -1.3448885679244995, "Satellite Mission Growing plants in microgravity"]
+[2.9547860622406006, -1.3940995931625366, "Satellite Mission Understand phenomena related to Earth's auroras"]
+[2.930931568145752, -1.4458807706832886, "Satellite Mission Study the effects of radiation on electronic systems"]
+[2.948974370956421, -1.4110108613967896, "Satellite Mission Study the effects of radiation on electronic systems"]
+[2.904616594314575, -2.0230400562286377, "Satellite Mission Unknown"]
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+[1.9172461032867432, 10.731282234191895, "Imaging Device Total FOV 2300 square degrees"]
+[1.907432198524475, 10.727987289428711, "Imaging Device Sector Observation Time 27 days"]
+[1.9211218357086182, 10.729654312133789, "Imaging Device Pole Observation Time More than 80 days"]
+[1.9270237684249878, 10.7062406539917, "Imaging Device Ecliptic Pole Observation Time More than 300 days"]
+[-3.1736817359924316, 1.7554433345794678, "Satellite Mission Launch Year 2002"]
+[-3.1944966316223145, 1.7277566194534302, "Satellite Mission Decommission Year October 2017"]
+[-3.22163724899292, 1.7706164121627808, "Satellite Mission Launch Year May 2018"]
+[-3.1676716804504395, 1.7061305046081543, "Satellite Mission Data Continuity Continuation of GRACE data record"]
+[-3.1623921394348145, 1.6826924085617065, "Satellite Mission Data Consistency Consistent with GRACE data"]
+[-3.2900021076202393, 7.4571757316589355, "Data Processing Section Responsibilities Planning, data acquisition, processing and distribution of the G\u00f6kt\u00fcrk-2 satellite data"]
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+[-7.5605573654174805, 5.895096778869629, "Camera Optical Alignment Ground pixel radiance can be co-registered in bands 1 and 2 at the same time"]
+[-0.21011212468147278, 14.82036018371582, "Ozone Measurement Instrument Date April 25, 2006"]
+[-0.17347107827663422, 14.912826538085938, "Ozone Measurement Instrument URL http://earthobservatory.nasa.gov/Features/SOLSE/"]
+[-3.092020034790039, 7.6567702293396, "Processing Unit Interface CAN bus"]
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+[3.5182151794433594, 13.500106811523438, "Laser System Testing Range 140 m"]
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+[3.517387866973877, 13.493842124938965, "Laser System Range-dependent Biases Dimensionless"]
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+[0.7411789298057556, -2.181004762649536, "Satellite Angular Field of View 6 degrees"]
+[3.6221306324005127, -2.563234329223633, "Satellite Data Transmission Frequency Every 13.5 days"]
+[1.60258150100708, -2.1063497066497803, "Satellite Closest Approach to Earth Once per orbit"]
+[5.106256008148193, -4.254331111907959, "Satellite Start of Science Operations July 25, 2018"]
+[2.6970837116241455, -1.6236463785171509, "Satellite Expected Discovery New planets"]
+[-1.425689697265625, 4.359296798706055, "Ground-based Frame Rate More than 10,000 frames/s"]
+[-2.8333864212036133, 4.094109535217285, "Space-based Frame Rate 30 frames/s"]
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+[-2.6344406604766846, 4.006690502166748, "Space-based Resolution 1 km"]
+[-2.7351644039154053, 4.062525749206543, "Space-based Distance Range A few km to ~50 km"]
+[-0.12702666223049164, 15.547935485839844, "Spectrometer Wavelengths 1.61 \u00b5m, 2.06 \u00b5m, 0.76 \u00b5m"]
+[-0.1332220584154129, 15.567777633666992, "Spectrometer Resolving Power Near 21,000 in the A-band, near 12,000 in the CO2 bands"]
+[-0.06580480933189392, 15.450764656066895, "Spectrometer Footprint Size ~2 km x 2 km"]
+[-0.12519414722919464, 15.486228942871094, "Spectrometer Swath Width 20 km"]
+[2.2790117263793945, -1.1643288135528564, "Imagery Satellites Launch Partner SpaceX"]
+[-1.9154051542282104, 6.902576923370361, "Software Function Create photo-realistic, 3D accurate data models overnight"]
+[3.213430643081665, -1.7509876489639282, "Satellite Manufacturer Reorganization Date February"]
+[-0.9292338490486145, -10.01937484741211, "Constellation Funding Status Fully able to fund"]
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+[1.1720385551452637, -0.7858476638793945, "Satellite Dimensions 0.4 x 0.46 x 0.84 m"]
+[1.032289981842041, -4.356444358825684, "Satellite Mass 56 kg"]
+[0.5808871388435364, -1.4590400457382202, "Satellite Orbit Altitude Approximately 430 km"]
+[0.7060392498970032, -2.2729339599609375, "Satellite Orbit Inclination 42\u00b0"]
+[4.117825508117676, -2.840703248977661, "Satellite Orbit Period 90.00 min"]
+[-1.5667719841003418, 4.126375675201416, "Ground Segment Element Function Mission planning and satellite command, control"]
+[-1.5519423484802246, 4.135615348815918, "Ground Segment Element Function Receive and store KOMPSAT-3 data, support to collection planning, generate standard and value added imagery products, and distribute imagery products to users"]
+[1.3513182401657104, 10.55449390411377, "Image Reception and Processing Station Subsystems UIS (User Interface Subsystem), ICPS (Image Collection Planning Subsystem), DIS (Direct Ingestion Subsystem), PMS (Product Management Subsystem)"]
+[5.037163734436035, -4.55999231338501, "Satellite Conference Presentation Date Aug. 4-9, 2018"]
+[-4.382753849029541, 7.366661071777344, "Data Transmission System URL https://www.airbus.com/en/products-services/defence/connectivity/space-data-highway"]
+[-0.9548400044441223, -9.985830307006836, "Satellite Constellation Expected Orbit Date 2022"]
+[-9.950888633728027, 5.854599475860596, "Search and Rescue System Services FLS (Forward Link Service), RLS (Return Link Service)"]
+[-5.415993690490723, 7.094207286834717, "Return Link Service Function Provide the user in distress with a confirmation that its call for help has been received and that aid is underway"]
+[-7.391470432281494, 2.873116970062256, "Cosmic Ray Detector Helium Events 3.7 billion"]
+[-7.39572286605835, 2.8698649406433105, "Cosmic Ray Detector Antihelium Candidate Rate Approximately one per year"]
+[-7.394143581390381, 2.871691942214966, "Cosmic Ray Detector Antihelium Candidate to Helium Rejection One in a billion"]
+[-7.395637035369873, 2.871025800704956, "Cosmic Ray Detector Cosmic Ray Events More than 90 billion"]
+[-7.394615173339844, 2.872692108154297, "Cosmic Ray Detector Antiproton Events 3.49 x 105"]
+[-7.394007682800293, 2.870105743408203, "Cosmic Ray Detector Proton Events 2.42 x 109"]
+[-1.0310055017471313, 7.712534427642822, "Devices Accuracy Equivalent at high energies, 10% difference at low energies"]
+[-1.112496256828308, 7.779644966125488, "Device Number of CRs collected in 10 years Greater than the number of CRs that could be collected in the SCM scenario"]
+[-1.0876598358154297, 7.685641288757324, "Device Number of positrons collected Expected to be a factor 2 to 6 greater to the SCM configuration"]
+[-3.0960612297058105, 2.4154951572418213, "Mission Purpose Measure the primordial form of oxygen in the solar wind"]
+[0.4483296573162079, 4.505361557006836, "Natural Phenomenon Content Primordial form of oxygen"]
+[0.5116663575172424, 4.5233917236328125, "Natural Phenomenon Purpose Give insight into birth of solar system"]
+[-3.294010639190674, 7.476935863494873, "Data Processing Targeted Processing Time Less than one hour from image acquisition"]
+[-3.295456647872925, 7.500189781188965, "Data Processing Level Processing Time 42 s"]
+[-3.2865679264068604, 7.483974933624268, "Data Processing Level Processing Time 60 s"]
+[-3.30745267868042, 7.467029094696045, "Data Processing Level Processing Time 60 s"]
+[-3.32896089553833, 7.445051670074463, "Data Processing Level Processing Time 90 s"]
+[-3.2567384243011475, 7.417847156524658, "Data Processing Level Processing Time 180 s"]
+[-5.256854057312012, 9.282766342163086, "Repeater Frequency Bands 121.5 MHz and 406.05 MHz"]
+[-5.3266682624816895, 9.069884300231934, "Repeater Downlink Frequency 1544.5 MHz"]
+[-2.743685007095337, 7.904242992401123, "Processor Frequency 406.025 MHz"]
+[-2.759540557861328, 7.8944244384765625, "Processor Output 2400 bit/s bit stream"]
+[2.789135456085205, -2.4556586742401123, "Satellite Frequency Bands 121.5 MHz and 406 MHz"]
+[-1.733389139175415, 6.603694915771484, "Program Satellite Types LEOSAR, GEOSAR, MEOSAR"]
+[-1.7423783540725708, 6.614600658416748, "Program Ground Segment Components Local User Terminals (LUTs), Mission Control Centres (MCCs), Rescue Coordination Centres (RCCs)"]
+[-1.7224462032318115, 6.6425652503967285, "Program Payload Types SARR (Search and Rescue Relay) payloads, SARP (Search and Rescue Processing) payloads"]
+[6.323966026306152, 7.412944316864014, "Satellite Component Operation Schedule 4 days of operation and 10 days of standby"]
+[7.4589409828186035, 12.587565422058105, "Satellite Instrument Initial Checkout Date Between September 20 and October 10, 1996"]
+[7.513742446899414, 12.635337829589844, "Satellite Instrument First Observation Date October 10, 1996"]
+[2.065568208694458, -2.748427152633667, "Satellite Number of Stars Observed 400,000"]
+[2.04533052444458, -2.7409160137176514, "Satellite Number of Stars Identified in Catalog 1,822"]
+[2.0829737186431885, -2.764251232147217, "Satellite Number of Stars with Potential Earth-like Planets 408"]
+[1.922752022743225, -2.5181610584259033, "Satellite Number of Stars in Habitable Zone 1,822"]
+[-1.1939945220947266, 3.094329357147217, "Astronomical Concept Definition The area around a star at which water can be liquid on a rocky planet's surface"]
+[3.6840085983276367, 17.614511489868164, "Scientific Payload Unknown Unknown"]
+[3.669325351715088, 17.616552352905273, "Scientific Payload Unknown Unknown"]
+[3.6619443893432617, 17.609668731689453, "Scientific Payload Unknown Unknown"]
+[3.692772150039673, 17.64183235168457, "Scientific Payload Unknown Unknown"]
+[0.9931548237800598, 9.164979934692383, "Attitude Control and Orbit Correction Design and Prototyping Date Nov./Dec. 2002"]
+[-1.0973565578460693, 5.777715682983398, "UniSat-2 Conference Date March 9-16, 2002"]
+[1.4278961420059204, -1.4969085454940796, "Satellite Measurement Accuracy Within one micron (1 \u00b5m)"]
+[1.0281096696853638, -4.419355392456055, "Satellite Mass Measurement Unit Gigatons (Gt)"]
+[0.6669604182243347, -1.249382734298706, "Satellite Sea Level Rise Calculation 1000 gigatons of land ice into the ocean raises global sea level by 2.8 millimeters"]
+[2.881321907043457, 22.82132339477539, "Instrument Operation Mode Nominal"]
+[3.680232524871826, 22.96426010131836, "Instrument Operation Date 12-14 December 2018"]
+[1.6160508394241333, -2.228921890258789, "Satellite Attitude Control System Status Steady state"]
+[4.6318840980529785, -3.1572022438049316, "Satellite Next Operations Phase Examination Approximately in the next 2.5-month period"]
+[3.7098512649536133, 22.97810173034668, "Instrument Delivery Date June 13, 2018"]
+[2.5705902576446533, -1.2426550388336182, "Satellite Data Collection Freshwater from the surface of the ice shelf into the ocean below within three days"]
+[2.5746524333953857, -1.8842236995697021, "Satellite Ground Track Exactly repeating"]
+[2.2905113697052, -1.4548333883285522, "Satellite Laser Beams Can show the dramatic change in the terrain before and after the lake drained"]
+[0.23778128623962402, 11.615828514099121, "Sensor System Thermal Coupling Common opticalbench that thermally couples both sensors"]
+[-1.8142476081848145, 8.375174522399902, "Electronics Box Number of Boards 7"]
+[-1.765479564666748, 8.42630672454834, "Electronics Box Board Types Bus interface board, Solid state data recorder, Digital board, LED and heater control board, 2 x focal plane bias boards, Low-voltage power supply board"]
+[-1.5012880563735962, 14.929274559020996, "Visible and Infrared Radiometer Data Collection Mode Pushbroom"]
+[1.9467915296554565, -1.7113488912582397, "Satellite Observation Modes Nadir mode, Sun-glint mode, Sun glint track, Principle plane track, Target mode, Surface target track, Multi angles for one target"]
+[0.7207742929458618, -4.156890392303467, "Satellite Launch Mass 2060 kg"]
+[1.1641377210617065, -0.7914178967475891, "Satellite Size 2.4 m x 1.6 m x 1.5 m"]
+[0.9625613689422607, -4.3403801918029785, "Satellite Dry Mass 958.5 kg"]
+[-2.2900993824005127, 9.134199142456055, "Power System Power 1164 W"]
+[-3.6919260025024414, 8.327472686767578, "Energy Storage Capacity 18 Ah"]
+[0.5043520331382751, 9.3826322555542, "Attitude Control System Design Momentum-biased 3-axis stabilized spacecraft"]
+[-1.642305850982666, 9.698995590209961, "Propulsion System LAM Thrust 440 N"]
+[-1.6042861938476562, 9.67650032043457, "Propulsion System Thrusters Twelve 22 N"]
+[-5.439510822296143, 7.808608531951904, "Communication Size 0.9 m and 1.0 m"]
+[-3.151715040206909, 1.713462471961975, "Satellite Mission Design Life 7.7 years"]
+[-0.4187627136707306, 6.738066673278809, "Test Equipment Purpose Vision-based sensor system testing"]
+[-0.45380324125289917, 6.785928249359131, "Test Equipment Function Moved the LED target along a pre-programmed pattern"]
+[0.252483069896698, 11.575758934020996, "Sensor System Developer Technical University of Denmark (DTU)"]
+[0.25073477625846863, 11.550769805908203, "Sensor System Testing Support Supported the testing remotely"]
+[4.764145374298096, -4.489758014678955, "Satellite Image Capture Date Dec. 14, 2015"]
+[4.936738014221191, -4.5103631019592285, "Satellite Geolocation Accuracy Evaluation Date May 4-8, 2015"]
+[-1.3401644229888916, 6.091936111450195, "CEO & Managing Director Affiliation SI (Satrec Initiative Co. Ltd.)"]
+[-5.252834796905518, 2.722358226776123, "Telescope Observation Date April 29, 2015"]
+[-0.7330776453018188, 3.1409692764282227, "Stellar Zombie Description Pulsars are the collapsed remains of stars that exploded in supernova blasts. They can spin extremely fast and send out intense beams of radiation"]
+[-0.7279311418533325, 3.159939765930176, "Stellar Corpse Description White dwarfs are the collapsed, burned-out remains of stars not massive enough to explode in supernovae"]
+[-0.8437725305557251, 3.1611125469207764, "Stellar Corpse Description Small black holes that slowly feed off their companion stars, radiating X-rays as material plummets down into their bottomless pits"]
+[2.8348958492279053, 22.056406021118164, "Instrument Purpose Measure geophysical data related to the Earth's environment"]
+[2.9382681846618652, 22.222190856933594, "Instrument Affiliation Developed by NASDA, flown on NASA's Aqua mission"]
+[3.0554111003875732, -1.638598084449768, "Satellite Mission Phase Science Commissioning"]
+[3.0420327186584473, -1.556329369544983, "Satellite Mission Phase Science Operations"]
+[-5.251912593841553, 7.838090419769287, "Communication System Communication Distance 40-50 k km from Earth"]
+[-5.276371479034424, 7.804144382476807, "Communication System Provider KSAT (Kongsberg Satellite Services AS) and the Near-Earth Network (NEN)"]
+[1.020544171333313, 0.7746606469154358, "Earth Observation Satellite Sensing Amazon Seasonality Unknown"]
+[1.0240763425827026, 0.7719113230705261, "Earth Observation Satellite Capturing Shadows from a Solar Eclipse Unknown"]
+[0.4637649655342102, 9.371804237365723, "Attitude Control System Type Ball bearing"]
+[0.13854078948497772, 7.214544296264648, "Experiment Purpose Repeat the formation maneuvers controlling the relative spacecraft position and attitude only with the thrusters"]
+[-2.5197176933288574, 8.232629776000977, "Failure Detection, Isolation and Recovery System Design Principle Lowest-level isolation and recovery is attempted first"]
+[-2.5372378826141357, 8.166194915771484, "Failure Detection, Isolation and Recovery System Recovery Levels L0: Action None (Unit Level Local recovery), L1:Unit/Function Recovery (Recovery by FDIR), L2: Unit/Function Reconfiguration (Unit substitution by FDIR), L3: OBC / System Recovery (Safe orbit entered & System Mode to MANUAL), L4: CAM (Drifting orbit entered & System Mode to MANUAL)"]
+[7.2824320793151855, 12.41141414642334, "Satellite Instrument Total Irradiance Monitor (TIM) and the Spectral Irradiance Monitor (SIM) Upgraded versions of those flying on the SORCE mission"]
+[7.284381866455078, 12.413972854614258, "Satellite Instrument Orbit Non-sun-synchronous, inclined at 51.6\u00b0 at an altitude of 407 km and a period of 93 minutes"]
+[-0.6640756726264954, 12.411635398864746, "Monitor Number of Configurations 7"]
+[-0.6387173533439636, 12.449594497680664, "Monitor Measurement Frequency 15 measurements per day"]
+[-0.7193875908851624, 12.428668975830078, "Monitor Estimated Uncertainties Around 160 ppm"]
+[5.3194169998168945, -4.28996467590332, "Satellite Launch Date 2008"]
+[1.5124118328094482, -1.6309946775436401, "Satellite Service Area Almost one third of Earth's surface"]
+[2.7063231468200684, -3.2425451278686523, "Satellite Communication Device Types HDR-VSAT and SA-VSAT"]
+[-0.5951669216156006, -0.12438361346721649, "Satellite Deployment System Presentation Date February 17, 2015"]
+[-2.547168731689453, 4.623384475708008, "Space Cleanup System Presentation Date 5 April 2018"]
+[-3.052090644836426, 4.251043796539307, "Spacecraft Drag-free control concept Uses free-floating test masses sheltered inside each spacecraft as reference points for the measurement"]
+[-2.2893338203430176, 2.7690200805664062, "Ground-based observatories Gravitational wave detections Captured four dozen mergers"]
+[-5.012820243835449, 2.8881094455718994, "Space Telescope First multimessenger observation Picked up the first such multimessenger observation just seconds after LIGO detected a merger of two neutron stars through gravitational waves"]
+[14.512092590332031, 7.667038917541504, "Nanosatellite Form Factor 3U CubeSat"]
+[14.51067066192627, 7.677046298980713, "Nanosatellite Components Radio, batteries, attitude control unit, solar panels"]
+[14.449377059936523, 7.661447048187256, "Nanosatellite Solar Panel Configuration Double-deployed in cross-axis direction and two single deployed in axial direction"]
+[1.6130315065383911, 2.2522847652435303, "Geostationary Communications Satellite Operating Bands C- and Ku-bands"]
+[1.6364952325820923, 2.2529568672180176, "Geostationary Communications Satellite Propulsion Electric propulsion"]
+[1.6138341426849365, 2.2536628246307373, "Geostationary Communications Satellite Platform Eurostar E3000 EOR"]
+[-0.6056641340255737, 10.852465629577637, "Robotic Probe Launch Date October 1, 2010"]
+[-0.5625572204589844, 10.834476470947266, "Robotic Probe End of Life Date 2029"]
+[-0.554763674736023, 10.913983345031738, "Robotic Probe Mission Goal Collect high-resolution imagery of possible lunar landing sites"]
+[7.273038864135742, 12.391582489013672, "Satellite Instrument RMSE 5.34m(L1.1) / 6.73 m (L2.1)"]
+[7.201141834259033, 12.270476341247559, "Satellite Instrument NESZ (F/H/U) HH 1.31"]
+[7.2536396980285645, 12.376291275024414, "Satellite Instrument VV/HH VV+HH phase (deg) 1.0143"]
+[7.32804536819458, 12.458301544189453, "Satellite Instrument Spotlight High resolution 3 m"]
+[7.265209674835205, 12.431852340698242, "Satellite Instrument PSLR (azimuth) -16.20"]
+[7.26270866394043, 12.386487007141113, "Satellite Instrument Azimuth Range 23~14(mean:20)"]
+[2.303316354751587, -1.517509937286377, "Satellite Instrument Observations"]
+[-0.9460759162902832, 6.759494304656982, "Process Rate of Increase Up to two times higher than previous estimates"]
+[-0.9370505213737488, 6.7721476554870605, "Process Increase About 10% since 2003"]
+[11.294254302978516, 5.537240982055664, "CubeSats Operational Lifespan Around six months"]
+[11.511066436767578, 5.7168426513671875, "CubeSat Size 1U"]
+[11.49766731262207, 5.719194412231445, "CubeSat Size 3U"]
+[0.5163882374763489, -1.4980777502059937, "Satellite Orbit Altitude 628.6 km"]
+[0.6919804215431213, -2.2700979709625244, "Satellite Orbit Inclination 97.9\u00ba"]
+[0.9949630498886108, -4.388082981109619, "Satellite Mass 70 kg"]
+[11.48927116394043, 5.682336330413818, "CubeSat Size 1U"]
+[16.82428550720215, 6.876714706420898, "Microsatellite Mass 35 kg"]
+[16.783559799194336, 6.921021938323975, "Microsatellite Mass ~40 kg"]
+[-3.065390110015869, 4.190252304077148, "Spacecraft Emergency Abort Capability Yes"]
+[-3.1272149085998535, 4.253499984741211, "Spacecraft Crew Sustainment Yes"]
+[-3.128676652908325, 4.213253974914551, "Spacecraft Safe Reentry Capability Yes"]
+[-3.0918800830841064, 2.442746639251709, "Mission Launch Date December 2014"]
+[-3.2430734634399414, 5.355831623077393, "Space Launch System Launch Vehicle Orion's launch vehicle of choice"]
+[-0.08883212506771088, 15.550640106201172, "Spectrometer Parameter Value"]
+[-0.07198785245418549, 15.576591491699219, "Spectrometer Parameter Value"]
+[2.3165783882141113, 22.29673957824707, "Instrument Parameter Value"]
+[2.350705146789551, 22.47780990600586, "Instruments Parameter Value"]
+[-1.6135458946228027, 9.682515144348145, "Propulsion System Design and Test Complete"]
+[0.2606269121170044, 11.953388214111328, "Pollution Monitor Instrument Overview Not Applicable"]
+[4.962543487548828, -4.368103504180908, "Satellite Observation Date 22 November 2019"]
+[2.579805612564087, -3.9295337200164795, "Satellite URL https://doi.org/10.3847/2041-8213/ab564d"]
+[-0.9203033447265625, -10.03003978729248, "Satellite Constellation Mission Type EO"]
+[-0.9820911884307861, -9.97374153137207, "Satellite Constellation Number of Operational Satellites 62"]
+[2.870070695877075, -1.5163720846176147, "Satellite Probes Black Hole Jet Mystery"]
+[-5.87160062789917, 16.011009216308594, "Synthetic Aperture Radar Frequency of Operation C-band"]
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+[5.236563205718994, -4.305453777313232, "Satellite Peak Vegetation Growth Month April and May"]
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+[0.9480103850364685, 10.440803527832031, "3D Mapping Data Volume 110-petabyte"]
+[3.3047871589660645, -2.485832452774048, "Satellite Imagery Refresh Rate Unprecedented speed in the industry"]
+[-1.7335814237594604, 6.622171401977539, "Map Use Great for positional location and relative distance from one feature to another"]
+[1.1664906740188599, -0.8194245100021362, "Satellite Size Range 80% the size of Earth to comparable to or exceeding the sizes of Jupiter and Saturn"]
+[1.1512175798416138, -0.8345271348953247, "Satellite Planet Size Smaller in size than Neptune, but larger than Earth"]
+[-5.383340358734131, 2.7801530361175537, "Telescope Purpose Study other aspects of exoplanets, like the presence and composition of any atmosphere"]
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+[-4.6715216636657715, 9.023119926452637, "Transceiver Protocol Tests Mobile IP, NTP, UDP, MDP, FTP, SCP, SSH, IP"]
+[-4.694413185119629, 9.038358688354492, "Transceiver Data Flow Architecture Standard IP protocols and HDLC data framing"]
+[-4.694072246551514, 9.045190811157227, "Transceiver Communications GN/SN (Ground Network/Space Network), GPS Tracking and Orbit Determination, Internet Protocol (IP), Range Safety"]
+[2.8605844974517822, 21.978639602661133, "Instrument Purpose Calculate the performance of the radar systems and create simulated radar images"]
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+[1.3093552589416504, -1.8902322053909302, "Satellite General Relativistic Effect Test Frame-dragging"]
+[3.2522263526916504, 13.476644515991211, "Optical Communication Terminal Transmit Power 2.2 W"]
+[2.8421592712402344, 13.76877212524414, "Optical Communication Terminal Telescope Aperture 135 mm"]
+[-5.5726470947265625, 7.06083869934082, "Communication Link Data Rate 2.8 Gbit/s (1.8 Gbit/s user data)"]
+[-5.575214385986328, 7.051333904266357, "Communication Link Data Rate 600 Mbit/s"]
+[-4.288139343261719, 0.22301515936851501, "GNSS Receiver Supported Signals GPS, Galileo, CDMA GLONASS, Compass"]
+[-4.247187614440918, 0.2656528055667877, "GNSS Receiver Development Location Moog Broad Reach (formerly Broad Reach Engineering)"]
+[-4.28312873840332, 0.2309664636850357, "GNSS Receiver Intended Missions FormoSat-7/COSMIC-2, DESDynI, ICESat-2, Jason-CS, SWOT, DSAC, GRACE-FO, other NASA/NOAA missions"]
+[0.8775947690010071, -2.199739694595337, "Satellite Orbit Position 67.1\u00ba W above the equator"]
+[-2.261603593826294, 6.184030532836914, "Aviation Connectivity Solution Wi-Fi Connection Always-on high-speed"]
+[-2.209669589996338, 6.087857246398926, "Aviation Connectivity Solution Coverage Entire Americas and North Atlantic Corridor"]
+[-0.236286923289299, 15.437170028686523, "Hyperspectral Spectrometer Spectral Sampling Rate Unknown"]
+[-0.14591290056705475, 15.458212852478027, "Hyperspectral Spectrometer Range of CO2 Absorption Bands Unknown"]
+[-0.49203139543533325, 15.422953605651855, "Hyper-spectral Measurements Surface Pressure Retrieval Algorithm Unknown"]
+[7.306668758392334, 12.44894790649414, "Satellite Instrument Methane Retrieval Algorithm EOF-based regression algorithm"]
+[1.057887315750122, 0.7123245596885681, "Satellite Observation Single-Angle Polarization Reflectance Sensitivity Analysis Unknown"]
+[-1.4184165000915527, 3.273343801498413, "Astrophysical Project Unknown Unknown"]
+[-0.7422040104866028, 6.235342979431152, "URL N/A N/A"]
+[-2.5767626762390137, 9.600273132324219, "Power Source Type Li-Ion"]
+[-2.6348438262939453, 9.519819259643555, "Power Regulation Voltage 28 V"]
+[-1.4222899675369263, 13.359570503234863, "Solar Cells Type Triple-junction GaAs"]
+[-2.2647266387939453, 7.400807857513428, "On-board Computer Manufacturer Qinetiq Space"]
+[-1.2105870246887207, 8.602217674255371, "Component Material CFRP and aluminum core"]
+[-1.2202379703521729, 8.592018127441406, "Component Fittings Titanium"]
+[4.8306193351745605, -4.372015476226807, "Satellite Soil Moisture Measurement Date August 10, 2020"]
+[1.5668628215789795, -1.3485987186431885, "Satellite Wetness Percentile Varies"]
+[3.8078620433807373, -2.5094828605651855, "Satellite Dry Conditions Frequency Once every 50 years"]
+[-0.8149181008338928, 5.215008735656738, "City Record Days Above 110\u00b0F 34"]
+[-0.7433273196220398, 5.103704929351807, "City Last Measurable Rainfall Date Mid-April"]
+[-0.7830604910850525, 5.167688369750977, "City Summer Rainfall 0.05 inches"]
+[-3.5275144577026367, 6.800074100494385, "Population Data Version 4"]
+[0.9311996698379517, 10.825125694274902, "Image Quality Equation Version 5"]
+[-0.9693546295166016, 6.523604393005371, "Document Year 2019"]
+[2.36641788482666, -1.9164049625396729, "Satellite Ground Segment Location Redu (in Belgium)"]
+[2.3427276611328125, -2.0459728240966797, "Satellite Ground Station Location Santa-Maria in the Azores (in Portugal)"]
+[0.7035526037216187, 10.984931945800781, "Imaging Sensor Spatial Resolution 6.8 km"]
+[0.6529625654220581, 11.014886856079102, "Imaging Sensor Sensor Size 400 x 300 x 2"]
+[0.6722375750541687, 11.001399993896484, "Imaging Sensor Wavelength 777.4 nm"]
+[0.7010694146156311, 10.960314750671387, "Imaging Sensor Detection Efficiency >90%"]
+[0.722096860408783, 11.050829887390137, "Imaging Sensor False-alarm Ratio < 10%"]
+[0.7379515171051025, 10.985015869140625, "Imaging Sensor Dynamic Range > 100"]
+[-3.612680435180664, 12.741623878479004, "Particle Detector Energy Range 1-165 MeV"]
+[-3.5936808586120605, 12.744830131530762, "Particle Detector Energy Range 0.4 - 4 MeV"]
+[-4.503946304321289, 12.12476634979248, "Flux Gate Magnetometer Dynamic Range \u00b10.01 to \u00b1600 nT"]
+[-4.490344524383545, 12.12842082977295, "Flux Gate Magnetometer Resolution \u00b10.06 @ maximum of the dynamics"]
+[-13.934178352355957, -2.121034622192383, "X-ray Telescope Energy Region 6-11 keV"]
+[-13.869175910949707, -2.2275502681732178, "X-ray Telescope Sensitivity 3 x 10-13 erg s-1 cm-2 keV-1"]
+[-13.923535346984863, -2.163882255554199, "X-ray Telescope NH Parameter \u2265 3 x 1023 cm-2"]
+[-13.930213928222656, -2.148585319519043, "X-ray Telescope T Parameter \u2265 4 keV"]
+[-13.90577220916748, -2.147843599319458, "X-ray Telescope Energy Up to30 keV"]
+[4.638975620269775, -4.582066059112549, "Satellite Image Capture Date 19 January 2022"]
+[0.5089655518531799, 4.12365198135376, "Source of Methane Plumes Detection Date June 9, 2022"]
+[-0.08810511231422424, 15.362696647644043, "Source of Methane Plumes Monitoring Capability Systematic monitoring of emissions"]
+[-4.448026657104492, 15.902438163757324, "Radar Electronics Role Industry Role in ISRO's current and future Microwave Remote Sensing Payloads"]
+[-4.476500511169434, 15.907258987426758, "Radar Electronics Presentation Date Sept. 29 to Oct. 3, 2008"]
+[-4.47191047668457, 15.904170989990234, "Radar Electronics URL http://www.nrsc.gov.in/assets/pdf/kr.pdf"]
+[5.345426082611084, -4.448491096496582, "Satellite Launch Date March 1995"]
+[2.04948353767395, -2.778139352798462, "Satellite Number of Orbits More than 100,000"]
+[2.516124963760376, -2.0599091053009033, "Satellite Series DMSP-5D2"]
+[5.459950923919678, -4.349822044372559, "Satellite Launch Date 1997"]
+[2.021312952041626, -2.919436454772949, "Satellite Debris Quantity Over 100 pieces"]
+[2.020904779434204, -2.6670005321502686, "Satellite Small Fragments Quantity More than 50,000"]
+[2.6753828525543213, 22.126928329467773, "Instrument Objective Global and regional cloud cover mapping, SST (Sea Surface Temperature), and LST (Land Surface Temperature)"]
+[2.1608493328094482, 22.733707427978516, "Instrument Spectral Bands Six bands in the VIS and IR spectral regions"]
+[1.8310884237289429, 22.140380859375, "Instrument Spatial Resolution 1 km"]
+[2.7595274448394775, -1.1459814310073853, "Satellite Purpose Study the ionosphere"]
+[0.5051619410514832, 4.559889316558838, "Natural Phenomenon Shape Not specified"]
+[0.45277002453804016, 4.534884929656982, "Natural Phenomenon Location Just north and south of the equator"]
+[0.6898903250694275, 4.078315258026123, "Atmospheric Layer Purpose Study its changes"]
+[-3.1853256225585938, 1.741246223449707, "Satellite Mission Presentation Date June 9-13, 2003"]
+[-3.145442008972168, 1.707364797592163, "Satellite Mission Presentation Location Versailles, France"]
+[-3.2031710147857666, 1.7382991313934326, "Satellite Mission Presentation Date 2003"]
+[-5.41216516494751, 2.757504463195801, "Telescope Survey Duration 6 months"]
+[-5.351039886474609, 2.7609870433807373, "Telescope Uniform Exposure About 150-200 seconds"]
+[-5.439910888671875, 2.821479558944702, "Telescope Energy Measurement Accuracy 2% - 6%"]
+[-5.429576873779297, 2.746321678161621, "Telescope Image Resolution About 10\u201d"]
+[-5.294522285461426, 2.7940759658813477, "Telescope Dynamic Range More than one billion"]
+[2.3301942348480225, 22.199670791625977, "Instrument Parameter Detected Changes in saltiness"]
+[-2.8176116943359375, 15.250125885009766, "Microwave Radiometer Status Operating nominally"]
+[-7.49636697769165, 5.971675872802734, "High Sensitivity Camera Status Operating nominally"]
+[-3.7815823554992676, 6.980923652648926, "Data Collection System Status Operating nominally"]
+[-1.9128234386444092, 14.506424903869629, "Radio Occultation Sounder for Atmosphere Status Operating nominally"]
+[2.936809539794922, 23.34629249572754, "Instrument Status Operating nominally"]
+[-0.25044918060302734, 12.218317985534668, "New Infrared Sensor Technology Status Still in the commissioning phase"]
+[2.6784515380859375, 22.132326126098633, "Instrument Primary Objective Provide significantly improved temperature soundings"]
+[3.7109920978546143, 22.979787826538086, "Instrument Launch Date May 13, 1998"]
+[3.1185524463653564, 22.788286209106445, "Instrument Product Availability Since 1973"]
+[-4.936831474304199, 9.760488510131836, "Receiver Frequency L1 1575.42 MHz"]
+[-4.956926345825195, 9.76904296875, "Receiver Frequency L2 1227.6 MHz"]
+[-4.948451995849609, 9.787922859191895, "Receiver Purpose Measure TEC of the ionosphere and density measurements of the troposphere"]
+[16.8702449798584, 6.848783493041992, "Microsatellite Grabber Demonstrate capture"]
+[-3.0856587886810303, 2.3885133266448975, "Mission Proposed Launch Year 2023"]
+[-3.099457025527954, 2.387181043624878, "Mission Launch Date Q3 2016"]
+[-3.0927646160125732, 2.437300443649292, "Mission Altitude <400km"]
+[-3.1019275188446045, 2.4114887714385986, "Mission Orbital Residence Times <3 years"]
+[-0.9445239305496216, 9.836718559265137, "Rocket Inclination 20 degrees"]
+[-0.9235875606536865, 9.866667747497559, "Rocket Targeted Inclination 3 degrees"]
+[-0.9453946352005005, 9.801210403442383, "Rocket Apogee and Perigee Attitudes 249 x 45,234 km"]
+[-3.0965256690979004, 4.27049446105957, "Spacecraft Final Orbital Positions Unknown"]
+[-1.4260070323944092, 6.017221450805664, "Committee Chair Toni Tolker-Nielsen"]
+[-1.3563259840011597, 6.118228912353516, "Committee Submission Date Thursday, February 22, 2018"]
+[-1.0956193208694458, 7.724343299865723, "Device Operation Mode Periodic on/off to save energy"]
+[-1.0859631299972534, 7.766921043395996, "Device Operation Mode Continuous when they detect some requests or when they need to transmit their data"]
+[-1.9124932289123535, 6.897294044494629, "Software Components CAN drivers, TTC drivers, the operating system kernel, ADCS software, and the application software"]
+[-0.7755106091499329, 8.896148681640625, "Thermal Control Subsystem Control Method Passive thermal control is implemented based in the selection of materials, internal arrangement and paints or MLI (Multi-Layered Insulation)"]
+[2.743825674057007, -3.266385316848755, "Communication Satellite Data Rate 1.2 Gbit/s"]
+[2.7595980167388916, -3.309452533721924, "Communication Satellite Antenna Diameter 2.4m"]
+[2.7736599445343018, -3.3133914470672607, "Communication Satellite Amplifier Output Approximately 280 W"]
+[2.7970337867736816, -3.324857711791992, "Communication Satellite Orbit Geostationary"]
+[2.767848014831543, -3.296470880508423, "Communication Satellite Communication Technology Laser"]
+[2.764923095703125, -3.2618749141693115, "Communication Satellite Communication Delay Up to 90 minutes"]
+[2.845181703567505, -3.355642318725586, "Communication Satellite Service Start Date November 2016"]
+[0.11252819001674652, 7.181593894958496, "Dark Matter Experiment Mission Duration 12 years"]
+[0.09233573079109192, 7.227561950683594, "Dark Matter Experiment Mass 8.5 ton"]
+[0.10180302709341049, 7.201366424560547, "Dark Matter Experiment Number of Cosmic Rays Tracked More than 69 billion"]
+[0.05942905694246292, 7.220961570739746, "Dark Matter Experiment Arrival Date August 19, 2015"]
+[-1.5160223245620728, 13.451693534851074, "Solar Array Voltage 300 V"]
+[-1.4935322999954224, 13.453962326049805, "Solar Array Size 122 mm x 214 mm"]
+[-1.471659541130066, 13.40317153930664, "Solar Array Mass 186 g"]
+[-0.4770559072494507, 8.071019172668457, "Adhesive Thermal Environment -100 to +70\u00baC"]
+[0.06741295754909515, 7.356781959533691, "Adhesive Test Cycles 15 cycles"]
+[-3.498274326324463, 6.821343421936035, "Data Type Spacecraft health and safety information (engineering telemetry) and raw instrument data"]
+[-1.122097373008728, 4.477943420410156, "Ground Station Function Maneuver planning and scheduling for routine operations as well as special operations such as station keeping, annual yaw flips, and engineering or science investigations outside of normal operations"]
+[7.281622886657715, 12.411352157592773, "Satellite Instrument Sea Surface Temperature Product Algorithm Unknown"]
+[7.296969890594482, 12.423256874084473, "Satellite Instrument Calibration Unknown"]
+[7.317636966705322, 12.451318740844727, "Satellite Instrument URL http://www.eorc.jaxa.jp/en/hatoyama/etc/images/adeos_first/octs_ir_e3.html"]
+[7.319186210632324, 12.407309532165527, "Satellite Instrument Operation Mode Moon observation"]
+[-1.5635991096496582, 4.154752731323242, "Ground Segment System Based on FY (Feng Yun) satellite series of China"]
+[-1.3265981674194336, 4.399734020233154, "Ground Monitoring Network Number of Instruments 6"]
+[-3.2653403282165527, 7.344605445861816, "Data Processing System Function XCO2 retrieval based on the observation data, and for the provision of CO2 data products"]
+[-2.93652081489563, 4.1988372802734375, "Spacecraft Yaw Axis Slew 180\u00ba in five minutes"]
+[-3.0384490489959717, 4.26106071472168, "Spacecraft Principle-plane Nadir Observation Scanning the ground targets with the instrument boresight within 5\u00ba of the principal plane"]
+[-3.028064489364624, 4.210420608520508, "Spacecraft Principle-plane Nadir Observation Slowly slews for about 160\u00ba around the yaw axis"]
+[2.5714046955108643, -2.36454439163208, "Satellite Signal Modulation MBOC waveform"]
+[2.5947110652923584, -2.417041063308716, "Satellite Signal Modulation MBOC waveform"]
+[2.6510329246520996, -2.3295843601226807, "Satellite Signal Transmission MBOC modulation scheme standard"]
+[-0.18836025893688202, 15.516263008117676, "Spectrometer Spectral Bands 5"]
+[-0.030471140518784523, 15.409114837646484, "Spectrometer Measured Gases CO2, CH4, CO"]
+[-0.05123221501708031, 15.475431442260742, "Spectrometer Prime Contractor Mitsubishi Electric Corporation"]
+[-1.478882074356079, 7.004784107208252, "Engineering Qualification Model Test Standards MIL-STD-461E, ECSS-E-10-03A"]
+[2.767103433609009, 13.698875427246094, "Electro-Optical Unit Purpose Test its performance and to verify its optomechanical design against dynamic loads"]
+[-1.0493642091751099, 7.223125457763672, "Equipment Selection Basis Needs of several systems"]
+[-3.1423702239990234, 4.3385114669799805, "Coronagraph SpaceCraft Role Chaser"]
+[-3.1252431869506836, 4.105304718017578, "Occulter SpaceCraft Role Target"]
+[-3.0906665325164795, 3.9447414875030518, "Occulter SpaceCraft Occulting Disk Size 1.4 m"]
+[-1.5663613080978394, 12.80593204498291, "Coronagraph SpaceCraft Coronagraph Instrument Observation of Sun\u2019s corona during artificial eclipse"]
+[2.6687331199645996, 5.388209342956543, "Emergency Beacons Lifesaving Yes"]
+[-9.95315933227539, 5.854330062866211, "Search and Rescue System Meeting Date 06 \u2013 10 July 2015"]
+[-0.9169074892997742, 0.2353268712759018, "Satellite System Contribution Date June 18, 2015"]
+[-0.20851731300354004, 15.066729545593262, "Ozone Limb Sounding Experiment URL http://library01.gsfc.nasa.gov/host/hitchhiker/solse_2.html"]
+[0.1291600912809372, 7.101920127868652, "Critical Viscosity of Xenon Experiment URL http://library01.gsfc.nasa.gov/host/hitchhiker/cvx_2.html"]
+[0.5318565368652344, -1.491699457168579, "Satellite Orbit Altitude 20,000-23,000 km"]
+[4.164583683013916, -2.7500603199005127, "Satellite Orbital Period About 12 hours"]
+[3.7302000522613525, 17.711185455322266, "Payload Doppler Shift Smaller for 406 MHz beacons"]
+[-5.249890327453613, 7.529817581176758, "Network Start Date About 2010 onwards"]
+[1.4646718502044678, -1.078370213508606, "Satellite Resolution 2.5 m"]
+[-3.274855375289917, 5.424232006072998, "Launch Vehicle Injection Orbit Lower Than Target Orbit 33 km"]
+[-3.271462917327881, 5.435102939605713, "Launch Vehicle Inclination Difference 0.1\u00ba"]
+[4.2575178146362305, -2.5284478664398193, "Satellite Operation Phase Duration 7 days"]
+[3.1283371448516846, -2.255755662918091, "Satellite Operation Phase Number of OCMs 14"]
+[0.21578359603881836, 10.191699028015137, "Image Navigation and Registration System Operation Ground-based real time image navigation process"]
+[0.19273222982883453, 10.22731876373291, "Image Navigation and Registration System Update Frequency Daily"]
+[2.8324227333068848, 22.39790153503418, "Instrument Attitude Information Source Spacecraft"]
+[2.7921159267425537, 22.187999725341797, "Instrument Image Navigation and Registration Process Ground processing"]
+[2.8593335151672363, 22.70315933227539, "Instrument Operation Earth scene collection"]
+[11.25854778289795, 5.493709087371826, "CubeSat Pointing Stability 5 arcsecond RMS"]
+[11.284552574157715, 5.486446857452393, "CubeSat Pointing Repeatability 1 arcsecond RMS"]
+[-8.292160987854004, 13.785467147827148, "Point Spread Function Size Must be balanced against the increase in other noise sources such as read noise and dark current"]
+[-5.332260608673096, 2.727982521057129, "Telescope Mirror Modules Seven identical Wolter-1 mirror modules"]
+[-5.50034761428833, 2.7993433475494385, "Telescope Detector System Based on the successful XMM-Newton pn-CCD technology"]
+[-5.387577056884766, 2.788031816482544, "Telescope X-ray Sources Discovered More than 1 million"]
+[-5.3065643310546875, 2.6737608909606934, "Telescope Surveys Eight surveys"]
+[-5.364880561828613, 2.7779629230499268, "Telescope Data Release First public release of eROSITA data"]
+[-6.991860866546631, 11.215742111206055, "Phased Array Antenna Number of Elements 64"]
+[-6.720210075378418, 9.982653617858887, "Antenna Component Isolation Better than -25 dB"]
+[3.469486713409424, 10.561370849609375, "Amplifiers Type Monolithic Microwave Integrated Circuit"]
+[2.300361156463623, -1.2077884674072266, "Satellite SAR Imagery Vessel Detection Applications"]
+[2.5993659496307373, -1.1974490880966187, "Satellite Remote Sensing Ocean, Sea Ice, and Large Water Regions"]
+[2.7024357318878174, -1.3571778535842896, "Satellite Documentation Observation of the Earth and Its Environment: Survey of Missions and Sensors"]
+[2.965029001235962, 22.453567504882812, "Instruments Manufacturer University of Colorado Laboratory for Atmospheric and Space Physics"]
+[1.965741515159607, -3.1052868366241455, "Satellite Contract Amount $18,044,280"]
+[4.2936553955078125, -2.7326014041900635, "Satellite Period of Performance Ending with on-orbit acceptance by the government"]
+[-1.0630887746810913, 7.661494731903076, "Device Manufacturer NASA Jet Propulsion Laboratory"]
+[5.22228479385376, -4.301100730895996, "Satellite Launch Date December 2017"]
+[3.176952838897705, -2.373246192932129, "Satellite Launch Date Unknown"]
+[1.7620506286621094, 6.862934112548828, "Communication Device Data Rates 50kb to 66MHz"]
+[-5.210094928741455, 7.789604187011719, "Communication Service Information Rate 256 kbit/s"]
+[-5.163906574249268, 7.855698585510254, "Communication Service Information Stream Live stream of weather and other critical information"]
+[-5.195971488952637, 7.830806255340576, "Communication Service Data Processed mission data"]
+[-1.8428903818130493, 14.307682037353516, "Shortwave Infrared Spectral Range 800-1700 nm"]
+[-1.9239157438278198, 14.255694389343262, "Shortwave Infrared Spectral Resolution 20 m"]
+[0.24981652200222015, 11.575324058532715, "Sensor System MTF ~ 40%"]
+[0.2758180797100067, 11.594237327575684, "Sensor System Focus Distance 850 mm"]
+[0.2386104166507721, 11.540510177612305, "Sensor System Local Memory 128 MB"]
+[0.25136274099349976, 11.559849739074707, "Sensor System Radiometric Resolution 8 bit"]
+[0.24427150189876556, 11.54773235321045, "Sensor System Data Transmission 25MHz LVDS, 100 MHz SpaceWire, Real-time LVDS"]
+[0.2719489634037018, 11.591184616088867, "Sensor System Swath Width 15 km"]
+[1.3718491792678833, 10.552900314331055, "Imaging System Integration and Testing Date June 14-16, 2007"]
+[2.5788204669952393, -3.9270520210266113, "Satellite URL https://en.wikipedia.org/wiki/RASAT"]
+[16.950620651245117, 6.784776210784912, "Microsatellite Program Theme Education and hands-on experience of students and faculty in the field of aerospace engineering"]
+[-1.1402066946029663, 4.473259925842285, "Amateur Ground Station Location University of Rome"]
+[-0.8768890500068665, 0.20091411471366882, "Satellite System Components CI (Coronagraph Instrument), OD (Occulter Disk), metrological sensors"]
+[2.5797436237335205, 13.533052444458008, "Coronagraph Optical Box Components Optics, detector, radiator, FDA (Front Door Assembly), FWA (Filter Wheel Assembly), SHM (Shutter Mechanism)"]
+[0.7102033495903015, 12.033466339111328, "Shadow Position Sensor Mounting Location COB"]
+[-4.295071601867676, 0.34623634815216064, "Occulter Position Sensor Emitter Mounting Location Center of the Occulter Disk"]
+[1.6638048887252808, -1.5932267904281616, "Satellite Mode Purpose Orientation of the satellite in the direction of the Sun, with a slow rotation around the X-axis for thermal reasons"]
+[1.6324392557144165, -1.534483790397644, "Satellite Mode Purpose Transition from acquisition or safe-hold mode (MAS) to normal mode (MNO)"]
+[1.5744247436523438, -1.521773338317871, "Satellite Mode Control Requirement Satellite pointing requires knowing the orbit position"]
+[2.5648746490478516, -1.3380297422409058, "Satellite Data Distribution Real-time weather data"]
+[2.488844871520996, -1.2409472465515137, "Satellite Data Distribution Geophysical data"]
+[2.8684680461883545, -1.3683634996414185, "Satellite User Agencies NOAA, Navy, Coast Guard, Geological Survey, NSF"]
+[-7.338011741638184, 6.132436275482178, "Camera System Purpose Crew Earth Observations"]
+[-7.3524017333984375, 6.1190185546875, "Camera System Data Images of natural and human-made events on Earth"]
+[-7.316379070281982, 6.160238265991211, "Camera System Data Atmospheric phenomena"]
+[-7.3104448318481445, 6.16195011138916, "Camera System Data Events such as storms, floods, fires and volcanic eruptions"]
+[-7.320484161376953, 6.154473304748535, "Camera System Data Images of Earth at night"]
+[-13.74258804321289, -2.2262322902679443, "X-ray Telescope Survey Duration 8 December 2019 till 10 June 2020"]
+[-13.910218238830566, -2.1419780254364014, "X-ray Telescope Energy Range 4\u201312 kiloelectron volt (keV)"]
+[-2.1597847938537598, 2.862408399581909, "Space Observatory Launch Date 13 July 2019"]
+[-13.850994110107422, -2.226710796356201, "X-ray Telescope Survey Frequency Eight all-sky surveys for the next four years"]
+[2.4114835262298584, -1.6004751920700073, "Satellite Instrument Cameras"]
+[2.4340009689331055, -1.5607733726501465, "Satellite Instrument Cameras"]
+[2.4256269931793213, -1.5640631914138794, "Satellite Instrument Cameras"]
+[2.355633497238159, -1.5392930507659912, "Satellite Instrument Cameras"]
+[2.3659918308258057, -1.5534424781799316, "Satellite Instrument Cameras"]
+[-0.26801061630249023, 10.21566390991211, "Tracking System Tracking Location Utah Test and Training Range (UTTR)"]
+[-2.867586374282837, 3.901150941848755, "Capsule Landing Hard landing in the Utah desert"]
+[-2.8363919258117676, 3.887779951095581, "Capsule Damage The damage to SRC wasn't as severe as initially expected"]
+[-0.9622606635093689, 13.095314025878906, "Solar Irradiance Sensor Shipment Date 4 Aug. 2017"]
+[-1.0005887746810913, 13.126933097839355, "Solar Irradiance Sensor Project Overview Date Nov. 10-13, 2015"]
+[0.9336262345314026, -2.3019745349884033, "Satellite Elastic Modulus > 200 GPa"]
+[1.8473472595214844, -2.594350576400757, "Satellite Yield Strength > 500 MPa"]
+[-0.3295725882053375, 8.176653861999512, "Material Young Modulus ~130 GPa"]
+[-0.33525362610816956, 8.179091453552246, "Material Admissible Yield 400 MPa"]
+[-3.0064594745635986, 4.223458766937256, "Spacecraft Journey Distance 3,300 miles above Earth"]
+[-3.085932731628418, 4.16370964050293, "Spacecraft Road Trip Distance 2,700 miles"]
+[-3.4113411903381348, 4.267472743988037, "Spacecraft Flight Test Duration 4.5 hours"]
+[-3.128152370452881, 4.21165657043457, "Spacecraft Next Flight Exploration Mission-1"]
+[-3.204968214035034, 4.304810523986816, "Spacecraft Next Flight Type Uncrewed"]
+[-3.29132342338562, 8.780278205871582, "Memory Module Mass 14 Kg"]
+[-3.3040475845336914, 8.754185676574707, "Memory Module Storage Density Factor of 8"]
+[-3.2818634510040283, 8.78520679473877, "Memory Module Number of Modules Reduced"]
+[-3.289414882659912, 8.783061981201172, "Memory Module Mass and Volume Decline accordingly"]
+[0.9654982089996338, -4.37392520904541, "Satellite Mass 155 kg"]
+[16.78404426574707, 6.9095258712768555, "Microsatellite Mass ~22 kg"]
+[16.633888244628906, 6.971030235290527, "Minisatellite Mass 181 kg"]
+[11.106595039367676, 5.207383632659912, "CubeSats Mass 5 kg each"]
+[16.825742721557617, 6.874330043792725, "Microsatellites Mass 13.4 kg each"]
+[-3.1548757553100586, 1.720129132270813, "Satellite Mission Satellite Separation Millions of kilometers"]
+[-3.0979833602905273, 1.6619532108306885, "Satellite Mission Measurement Method Lasers"]
+[-3.133720874786377, 1.7240207195281982, "Satellite Mission Gravitational Wave Detection Yes"]
+[-3.1581082344055176, 1.6946394443511963, "Satellite Mission Image Credit AEI/MM/exozet; GW simulation: NASA/C. Henze"]
+[2.8096120357513428, -2.0372767448425293, "Satellite Debris Containment Bags Unknown"]
+[2.850583076477051, -1.3465615510940552, "Satellite Use Artificial debris targets"]
+[-3.0695652961730957, 2.387359380722046, "Mission Operations Center SSTL\u2019s MOC (Mission Operations Centre) in Guildford"]
+[-3.0836634635925293, 2.4524850845336914, "Mission Ground Station SSTL\u2019s MOC (Mission Operations Centre) in Guildford"]
+[-0.20465630292892456, 6.500045299530029, "Test Bench Operation Independent of COSPAS-SARSAT system"]
+[-0.23304383456707, 6.584662914276123, "Test Bench Interface LUT-to-MCC and nodal-MCC -to-RLSP"]
+[-4.500204086303711, 12.129088401794434, "Fluxgate Magnetometer Measurement Rate 12 readings/s"]
+[-4.537980556488037, 12.096783638000488, "Fluxgate Magnetometer X Axis Reporting Rate 10 readings/s"]
+[-4.506577014923096, 12.125667572021484, "Fluxgate Magnetometer Measurement Range \u00b165535 nT"]
+[-4.533169746398926, 12.15231704711914, "Fluxgate Magnetometer Resolution 2 nT"]
+[-4.509652614593506, 12.12897777557373, "Fluxgate Magnetometer X Axis Alignment Downward and aligned to local vertical within 0.01 degree"]
+[-4.476114749908447, 12.15904712677002, "Fluxgate Magnetometer Y Axis Alignment Parallel to the velocity vector for spacecraft with ascending node in the afternoon/evening sector"]
+[-4.504180908203125, 12.12531566619873, "Fluxgate Magnetometer Z Axis Alignment Away from the solar panel and anti-parallel to the orbit normal vector"]
+[0.22097541391849518, 7.10934591293335, "Experiment Purpose Testing general relativity"]
+[0.20654161274433136, 7.256513595581055, "Experiment Mission Date 21-25 October 2019"]
+[2.811837673187256, 22.451398849487305, "Instrument Type Precision orbit"]
+[5.227265357971191, -4.25462007522583, "Satellite Launch Date 13 July 2022"]
+[5.041428089141846, -4.0785932540893555, "Satellite End of Life Date March 2062"]
+[-8.140485763549805, 8.827657699584961, "Electrical Power Subsystem Solar Cell Type Triple junction solar cells (GaInP 2 /GaAs/Ge)"]
+[-8.115241050720215, 8.819095611572266, "Electrical Power Subsystem Solar Cell Efficiency 26.8%"]
+[-8.163124084472656, 8.814879417419434, "Electrical Power Subsystem Power Generation ~50-100 W"]
+[-8.148545265197754, 8.81226921081543, "Electrical Power Subsystem Battery Type Lithium Ion Polymer"]
+[-8.144680976867676, 8.826579093933105, "Electrical Power Subsystem Battery Nominal Voltage 7.4 V"]
+[-8.145853042602539, 8.824183464050293, "Electrical Power Subsystem Battery Nominal Capacity 4.55Ah"]
+[-8.151236534118652, 8.816574096679688, "Electrical Power Subsystem Battery Predicted Cycle Life 20000"]
+[-2.1884407997131348, 8.968619346618652, "Power Control Unit Microprocessor 16 bit Microprocessor (H8/3048F)"]
+[0.6456298828125, 9.352109909057617, "Attitude Control Subsystem Extendible Boom Length 3 m"]
+[0.6594488620758057, 9.304780006408691, "Attitude Control Subsystem Attitude Accuracy \u00b12\u00ba"]
+[0.6319671273231506, 9.319233894348145, "Attitude Control Subsystem Attitude Stability 0.03\u00ba/s"]
+[1.7816965579986572, 8.444461822509766, "Command & Data Handling Subsystem CPU 32 bit RISC, MPU (SH4)"]
+[1.7747098207473755, 8.43766975402832, "Command & Data Handling Subsystem Data Recorder Capacity >30 GByte"]
+[-5.143974781036377, 7.9795637130737305, "Communication Subsystem Downlink Ku-band transmitter at 10 Mbit/s, BPSK modulation, 0.2 W output"]
+[-5.1527180671691895, 7.966615676879883, "Communication Subsystem Uplink VHF at 9.6 kbit/s, frequency = 155 MHz, bandwidth = 16 kHz"]
+[-5.233244895935059, 7.578098297119141, "Protocol Stack Capability Aggregate telecommand and telemetry data into recognizable files and transport them end-to-end through the data networks"]
+[-5.275251388549805, 7.62824821472168, "Protocol Stack Optional Data Protection Mechanism Assure end-to-end security and integrity of message exchange"]
+[4.097702980041504, 13.938530921936035, "Laser Altimeter System Function Sends pulses of laser light toward Earth\u2019s ice, land, and water surfaces and derives height from the amount of time it takes for photons to bounce back"]
+[0.795939564704895, -1.1765871047973633, "Satellite Bathymetry Mapping Depth 26 meters (85 feet)"]
+[0.8660814166069031, -1.0540680885314941, "Satellite Bathymetry Mapping Depth 26 meters"]
+[1.389156699180603, 10.565200805664062, "Imaging System Target Distance \u2264 300 km"]
+[1.340811848640442, 10.539960861206055, "Imaging System Target Speed \u2264 3 km/s"]
+[1.367032527923584, 10.551247596740723, "Imaging System Number of Pixels 1280 x 1024"]
+[1.3602474927902222, 10.552037239074707, "Imaging System Focal Length 225 mm"]
+[1.3580844402313232, 10.559170722961426, "Imaging System FOV 2.08\u00ba x 1.67\u00ba"]
+[1.342849612236023, 10.523298263549805, "Imaging System Pixel Size 6.7"]
+[1.383244276046753, 10.551506996154785, "Imaging System Readout Resolution 8 bit"]
+[1.3529177904129028, 10.540146827697754, "Imaging System Exposure Time 1 s"]
+[1.3434067964553833, 10.542521476745605, "Imaging System Aperture Diameter 85 mm"]
+[1.3840328454971313, 10.536596298217773, "Imaging System Instrument Size < 9.75 cm x 9.75 cm x 15 cm"]
+[1.3606277704238892, 10.535989761352539, "Imaging System Instrument Mass < 1.83 kg"]
+[1.3505250215530396, 10.54105281829834, "Imaging System Output Data Rate < 50 kbit/s"]
+[0.49790677428245544, 9.44431209564209, "Angle to Position Converter Angular Accuracy Requirement 5 arcsec"]
+[-0.7890478372573853, 11.625226020812988, "HAS Detector Pixel Count 1024 x 1024"]
+[-0.7607423663139343, 11.558120727539062, "HAS Detector Pixel Size 18 \u00b5m"]
+[-0.8703392148017883, 11.621108055114746, "Detection System Operating Wavelength Around 980 nm"]
+[1.5247247219085693, 5.407646656036377, "Satellite Bus Length ~ 21 m"]
+[1.511507272720337, 5.425004005432129, "Satellite Bus Maximum Diameter 1.5 m"]
+[1.0130043029785156, -4.351715564727783, "Satellite Mass Nearly 2300 kg"]
+[0.717404842376709, 11.976032257080078, "Sensor Operation Mode Uncooperative"]
+[-2.993584156036377, 4.059423446655273, "Spacecraft Maneuver Requirement Relative trajectory that does not advance towards or retreats away from the target over multiple orbits"]
+[0.07077717781066895, 7.113368511199951, "Experiment Demonstration Requirement Non-cooperative forced motion maneuvers in closed-loop GNC, including hold, approach, retreat, and target inspection maneuvers"]
+[0.011066257953643799, 7.2378129959106445, "Experiments Requirement Totally complementary, without duplicating effort and results"]
+[0.14747625589370728, 7.177246570587158, "Experiment Requirement Not imply major constraints or hardware changes in the PROBA-3 baseline"]
+[-8.089330673217773, 11.684991836547852, "CCD Array Imager Pixel Count 1372 x 1300 pixels"]
+[-8.090270042419434, 11.694995880126953, "CCD Array Imager Pixel Size 30 x 30 \u00b5m"]
+[-8.089841842651367, 11.686031341552734, "CCD Array Imager Spectral Wavelength 777.4 nm"]
+[-8.088046073913574, 11.685693740844727, "CCD Array Imager Lens Focal Length 134 mm"]
+[-8.089476585388184, 11.686408042907715, "CCD Array Imager Lens FOV \u00b18\u00ba"]
+[-8.09119701385498, 11.687185287475586, "CCD Array Imager Ground Sample Distance 8-14 km"]
+[-8.09192943572998, 11.686822891235352, "CCD Array Imager Threshold < 4.0 J m -2  sr -1"]
+[-8.08780288696289, 11.685507774353027, "CCD Array Imager Flash Efficiency 80%"]
+[-8.090761184692383, 11.686614990234375, "CCD Array Imager Event Rate 1 x 10  -5  s -1"]
+[-8.090703964233398, 11.686508178710938, "CCD Array Imager SNR 6"]
+[-8.091324806213379, 11.687649726867676, "CCD Array Imager Dynamic Range > 100"]
+[-8.090912818908691, 11.686600685119629, "CCD Array Imager Detection Efficiency > 90% of total events"]
+[-8.089320182800293, 11.685182571411133, "CCD Array Imager False Alarm Rate <5% of total events"]
+[-8.091316223144531, 11.686675071716309, "CCD Array Imager Measurement Accuracy Location: 1 pixel; intensity: 10%; time tag at frame rate"]
+[-8.090984344482422, 11.686501502990723, "CCD Array Imager Temporal Resolution 2 ms"]
+[-8.086719512939453, 11.686057090759277, "CCD Array Imager Instrument Mass 125 kg"]
+[-8.088852882385254, 11.684341430664062, "CCD Array Imager Instrument Power 290 W"]
+[-8.09145450592041, 11.687329292297363, "CCD Array Imager Data Rate 7.7 Mbit/s"]
+[-8.088916778564453, 11.687448501586914, "CCD Array Imager Modulation PCM"]
+[-8.089774131774902, 11.685107231140137, "CCD Array Imager Quantization 14 bit"]
+[11.817906379699707, 5.311888694763184, "6U CubeSats Manufacturer Hiber Global"]
+[11.836921691894531, 5.331718921661377, "3U CubeSat Objectives Demonstrate a cross-link from LEO to MUOS WCDMA in GEO"]
+[16.80805015563965, 6.88565731048584, "X-band SAR microsatellite Mass ~ 80 kg"]
+[11.73669719696045, 5.392367362976074, "1U CubeSat Educational Mission Irvine Public School Foundation"]
+[11.82858943939209, 5.304327011108398, "6U Cubesat Mass ~8kg"]
+[11.660858154296875, 5.407459735870361, "1U CubeSat Purpose Carry a UHF/VHF amateur radio"]
+[16.810184478759766, 6.891846656799316, "Microsatellite Mass <100 kg"]
+[11.623396873474121, 5.511497974395752, "1U CubeSat Purpose Use of an amateur radio for communication"]
+[11.809507369995117, 5.316608428955078, "6U CubeSat Mass 11 kg"]
+[-5.307437896728516, 2.7732183933258057, "Telescope Mirror Modules 7"]
+[-5.422821998596191, 2.7301366329193115, "Telescope Mirror Shells 54"]
+[-5.375189781188965, 2.7943336963653564, "Telescope X-ray Cameras 7"]
+[-5.39213228225708, 2.765355348587036, "Telescope Manufacturer Russia"]
+[-1.8486988544464111, 7.254456043243408, "Platform Manufacturer Russia"]
+[-3.2596824169158936, 4.258144855499268, "Spacecraft Assembly and Testing Time Around nine months"]
+[-5.3764567375183105, 2.801083564758301, "Telescope Integration Location MPE integration Lab"]
+[-13.868963241577148, -2.2605903148651123, "X-ray telescope Mirror Assemblies 8"]
+[-13.865346908569336, -2.265578031539917, "X-ray telescope Camera Assemblies Unknown"]
+[-13.882908821105957, -2.213510751724243, "X-ray telescope MA-CA pairs 7"]
+[-2.7684433460235596, 7.8269524574279785, "Microprocessor Maximum Event Processing Rate 400 cps"]
+[-3.346292734146118, 7.374710559844971, "Data Processing System Pulse Pileup Threshold ~ 105 cps"]
+[-3.30177640914917, 7.393215179443359, "Data Processing System Maximum Source Flux Count Rate 104 cps"]
+[-3.375797986984253, 7.395532131195068, "Data Processing System Nominal Faint-Source Count Rate Dead Time < 2%"]
+[-1.9363553524017334, 8.11910629272461, "System Services Network fabric, consolidated storage, database services, enterprise service bus"]
+[-5.2461161613464355, 7.513444900512695, "Network Type IP (Internet-Protocol)-based"]
+[-3.808741569519043, 8.017783164978027, "Storage Function Enable short-term and long-term storage within the GS"]
+[-2.035123348236084, 8.03205680847168, "Service Function Enable element-level databases through the use of relational database clusters"]
+[-2.0778350830078125, 8.022865295410156, "Service Function Support a common set of message exchanges for both intra-and inter-element communication"]
+[-2.1123969554901123, 5.5032806396484375, "Deployment System Quantity 6 units"]
+[1.0094270706176758, -4.404910087585449, "Satellite Mass 3.5 kg"]
+[0.5904137492179871, -1.4742037057876587, "Satellite Orbit Altitude 635 km"]
+[0.7150030732154846, -2.2739224433898926, "Satellite Orbit Inclination 97.4\u00ba"]
+[4.193614959716797, -3.043344259262085, "Satellite Equatorial Crossing Time 9:30 hours"]
+[2.6683919429779053, -2.6985936164855957, "Satellite Data Rate 1 Mbit/s"]
+[0.03029930219054222, 13.43642520904541, "Metrology Element Measurement Accuracy 7.5 cm"]
+[0.470907062292099, 12.228214263916016, "Sensor Measurement Accuracy \u00b113 m @ 150 m (lateral)"]
+[0.4970611035823822, 12.216328620910645, "Sensor Measurement Accuracy 1 mm @150 m (lateral)"]
+[0.5288844108581543, 12.224510192871094, "Sensor Measurement Accuracy \u00b120.5 mm (lateral)"]
+[0.4798227548599243, 12.282491683959961, "Sensor Measurement Accuracy 21 \u00b5m (lateral)"]
+[0.5664802193641663, 12.175006866455078, "Sensor Measurement Accuracy 30 \u00b5m (longitudinal)"]
+[-0.5751665830612183, 1.2566548585891724, "Orbit Inclination Mid-inclination"]
+[-0.5940250158309937, 1.291363000869751, "Orbit Local Time of Imaging Varies"]
+[-0.6067031025886536, 1.2878782749176025, "Orbit Blackouts Multi-day periods when it is only in view of that geography during local nighttime"]
+[-5.322688579559326, 2.886619806289673, "Scanning Telescope Design Cassegrain"]
+[-5.322605609893799, 2.9327876567840576, "Scanning Telescope Clear Aperture 20.3 cm"]
+[-5.319753170013428, 2.8726770877838135, "Scanning Telescope Effective Collecting Area 185 cm2"]
+[-5.248000144958496, 2.9244325160980225, "Scanning Telescope Effective Focal Length 122 cm"]
+[-5.311440944671631, 2.9138545989990234, "Scanning Telescope Scan Angle \u00b156.25\u00ba"]
+[-5.288715362548828, 2.905729293823242, "Scanning Telescope Swath Width on the Ground 2960 km"]
+[-5.339759349822998, 2.8832199573516846, "Scanning Telescope Bandpass 0.5 - 0.85 \u00b5m"]
+[-1.2629339694976807, 13.302695274353027, "Solar Cell Measurement System Objective Measure the current and voltage characteristics of the solar cells under varies aspect angles to the sun to generate voltage-current (IV) curve traces twice per orbit"]
+[-1.2144081592559814, 13.279109001159668, "Solar Cell Measurement System Components 22 triple-junction cells, two commercial dual-junction control cells, analog cell measurement circuitry, data converters, microcontroller, FPGA, n-channel MOSFET transistor, amplifier, tolerance resistor"]
+[-1.2677899599075317, 13.288065910339355, "Solar Cell Measurement System Design Radiation-hardened system"]
+[-1.2588468790054321, 13.298003196716309, "Solar Cell Measurement System FPGA Redundancy Triple Modular Redundant (TMR)"]
+[-1.264849305152893, 13.33034896850586, "Solar Cell Measurement System Analog Circuit Design Uses an n-channel MOSFET transistor, amplifier and tolerance resistor to create the voltage-controlled current sink"]
+[7.334850788116455, 12.462757110595703, "Satellite Instrument Global Coverage Monthly"]
+[7.274204254150391, 12.386656761169434, "Satellite Instrument Data Product Grid 150 km"]
+[7.2862019538879395, 12.418400764465332, "Satellite Instrument Accuracy < 0.2 psu"]
+[7.293239593505859, 12.39752197265625, "Satellite Instrument Calibration Stability Requirement 0.15 K over two days"]
+[7.25301456451416, 12.414141654968262, "Satellite Instrument Imaging Concept 3-beam pushbroom"]
+[1.967391014099121, 22.083864212036133, "Instrument East-West Step 10 km"]
+[1.9152605533599854, 22.063674926757812, "Instrument East-West Block 640 km"]
+[1.8938133716583252, 22.099010467529297, "Instrument North-South Step 40 km"]
+[1.8844422101974487, 22.118867874145508, "Instrument North-South Block 640 km"]
+[-1.8297041654586792, 14.772401809692383, "Meter Manufacturer TREK Inc."]
+[-1.825735330581665, 14.76996898651123, "Meter Type Contact type"]
+[-1.867964267730713, 14.813132286071777, "Meter Input Impedance Extremely large"]
+[0.5901197195053101, 12.010961532592773, "Sensor Purpose Detecting the micro-debris impact on the surface of HORYU-2"]
+[3.722904920578003, 17.696491241455078, "Payload Operation Period 6 months"]
+[3.72247576713562, 17.697216033935547, "Payload Operation Period 6 months"]
+[-3.216357946395874, 4.272120952606201, "Spacecraft Operation Goal 1 year"]
+[-3.012096643447876, 4.236180782318115, "Spacecraft Mission Type Non-EO"]
+[-3.5611560344696045, 4.395001411437988, "Spacecraft Launch Date 5 Dec 2014"]
+[-3.071397066116333, 4.335549831390381, "Spacecraft Mission Status Unknown"]
+[-3.1295297145843506, 4.275936603546143, "Spacecraft Test Flight Uncrewed"]
+[3.048975706100464, -1.9879835844039917, "Satellite Deployment Status Working splendidly"]
+[1.473909616470337, -2.387974500656128, "Satellite Orbit 505 km sun-synchronous type"]
+[1.4983805418014526, -2.347196578979492, "Satellite Orbit Polar orbit of 365 km height"]
+[2.8025383949279785, 22.405025482177734, "Instrument Type Total-power passive microwave radiometer/scatterometer"]
+[1.9656985998153687, 22.981050491333008, "Instrument Form Factor 1U"]
+[-0.09270427376031876, 13.573173522949219, "Measurement System Modulation Frequencies 500 MHz, 100 MHz, 0.5 MHz"]
+[-0.09553345292806625, 13.55136489868164, "Measurement System Translation Range 15 m"]
+[-0.09235183894634247, 13.566709518432617, "Measurement System Translation Intervals 0.5 m"]
+[-0.09935036301612854, 13.584297180175781, "Measurement System Movement Direction +X direction and then back again along the same path in the -X direction"]
+[14.235867500305176, 7.812687873840332, "Nanosatellite Launch Date March 22, 2021"]
+[14.416814804077148, 7.729249954223633, "Nanosatellite Launch Time 7:07:12 am (CET)"]
+[14.339784622192383, 7.745929718017578, "Nanosatellite Launch Site Baikonur Cosmodrome, Kazakhstan"]
+[14.536282539367676, 7.617640495300293, "Nanosatellite Purpose Monitor the flow of rivers and water reserves, monitor and protect wildlife, receive weather data, monitor soil movements, monitor livestock and crops"]
+[2.7908504009246826, -1.4821314811706543, "Satellite Image Credit GRACE-FO Team"]
+[-0.10599341988563538, 11.210275650024414, "Monitoring System Land Area in Drought More than 93 percent of the land area in Utah, Colorado, Nevada, and New Mexico"]
+[-0.05482158437371254, 11.238734245300293, "Monitoring System Severe Drought Percentage 69 percent of Utah, as is 61 percent of Colorado"]
+[-3.192469358444214, 1.7472809553146362, "Satellite Mission Launch Date Unknown"]
+[-0.9484673738479614, 9.813608169555664, "Rocket Launch Date Unknown"]
+[5.264233112335205, -4.407046318054199, "Satellite Launch Date 27 October, 2017"]
+[5.32255744934082, -4.481945991516113, "Satellite Launch Date 27 October, 2017"]
+[-1.050087809562683, 6.717421054840088, "Research and Development Workshop Date Oct. 24-25, 2013"]
+[-2.5990588665008545, 9.611673355102539, "Power Source Average Power 12.3 W"]
+[-2.588963508605957, 9.619486808776855, "Power Source Efficiency 16%"]
+[-3.0903680324554443, 9.647740364074707, "Battery Capacity 4 Ah"]
+[1.77206552028656, 8.440570831298828, "Command and Data Handling Subsystem Microprocessor Rabbit 3000 8-bit"]
+[1.7759485244750977, 8.440810203552246, "Command and Data Handling Subsystem Microprocessor Clock Speed 29.4 MHz"]
+[1.7742801904678345, 8.441030502319336, "Command and Data Handling Subsystem A/D Converter 11 bit 8 channel (or 12 bit 4 channel if used in differential mode)"]
+[0.9662643671035767, -4.392210483551025, "Satellite Mass 12 kg"]
+[-5.197007179260254, 7.762028217315674, "Communication System Data Rate 9.6 kbit/s"]
+[-5.298861980438232, 8.105856895446777, "Communication System Uplink Frequency VHF (145 MHz)"]
+[-5.27274751663208, 8.00209903717041, "Communication System Downlink Frequency UHF (436 MHz)"]
+[-1.9099198579788208, 14.855250358581543, "Radiometer Observation Purpose Soil moisture and sea salinity"]
+[-3.195894479751587, 14.582465171813965, "Microwave Imager Observation Purpose Geophysical parameters of the land, ocean and atmosphere"]
+[-3.235288619995117, 16.246253967285156, "Radar Scatterometer Observation Purpose Snow water equivalence and freeze/thaw"]
+[-5.393869876861572, 2.7599258422851562, "Telescope Sensitivity Enough to detect the most distant clusters of galaxies in the Universe"]
+[-5.338267803192139, 2.741206169128418, "Telescope Integration Time About one day"]
+[-5.3804097175598145, 2.7837531566619873, "Telescope Distance of A3391/3395 system About 800 million lightyears"]
+[-5.4682769775390625, 2.8102033138275146, "Telescope Image Content Distribution of the diffuse hot gas, supernova remnants, foreground stars, distant Active Galactic Nuclei"]
+[2.319347381591797, -2.2298316955566406, "Satellite Laser Communication Terminals Multiple"]
+[2.5418689250946045, -2.165086269378662, "Satellite Communication Link Geostationary relay satellite of the SpaceDataHighway"]
+[2.198880910873413, -2.029979705810547, "Satellite Communication Network Geostationary orbit"]
+[-8.53309440612793, 13.673125267028809, "Parameter Measurement 5.28 million km2"]
+[-8.56006908416748, 13.740180969238281, "Parameter Measurement 2.04 million square miles"]
+[-8.509724617004395, 13.664441108703613, "Parameter Comparison 3.07 million km2 (1.19 million square miles) lower than the 1981-2010 average extent"]
+[-8.515196800231934, 13.684886932373047, "Parameter Date October 2020"]
+[-8.56510066986084, 13.742239952087402, "Parameter Time Period 1981-2010"]
+[5.3773956298828125, -4.3914594650268555, "Satellite Launch Date June 29, 1982"]
+[5.169586181640625, -4.429807186126709, "Satellite Decommissioned Date March 1988"]
+[0.5114715099334717, -1.4907726049423218, "Satellite Orbit Altitude 989 x1082 km"]
+[0.7308530807495117, -2.2729125022888184, "Satellite Orbit Inclination 83\u00ba"]
+[5.372472763061523, -4.468373775482178, "Satellite Launch Date Mar. 28, 1983"]
+[5.272355079650879, -4.265982627868652, "Satellite Decommissioned Date Dec. 1985"]
+[0.5650986433029175, -1.4348969459533691, "Satellite Orbit Altitude 801 x 826 km"]
+[0.754248321056366, -2.2297770977020264, "Satellite Orbit Inclination 98.2\u00ba"]
+[5.3735833168029785, -4.463618278503418, "Satellite Launch Date Feb. 26, 1987"]
+[5.389293670654297, -4.31422758102417, "Satellite Decommissioned Date April 1, 2003"]
+[0.7488561272621155, -2.168518304824829, "Satellite Orbit Longitude 155\u00ba E"]
+[5.285911560058594, -4.464026927947998, "Satellite Launch Date July 9, 1992"]
+[5.247897148132324, -4.181735038757324, "Satellite Decommissioned Date 2001"]
+[0.831229031085968, -2.1928136348724365, "Satellite Orbit Longitude 93.5\u00ba E"]
+[5.251578330993652, -4.483113765716553, "Satellite Launch Date Oct. 31, 1994"]
+[5.16055965423584, -4.295356750488281, "Satellite Mission End Date Nov. 2000"]
+[0.7210525870323181, -2.1453359127044678, "Satellite Orbit Longitude 76.5\u00ba E"]
+[5.265686511993408, -4.486667156219482, "Satellite Launch Date Feb. 26, 2011"]
+[0.6587262749671936, -1.5184627771377563, "Satellite Orbit Altitude 19,000 km"]
+[5.352971076965332, -4.521721363067627, "Satellite Launch Date Oct. 12, 2012"]
+[0.5231269001960754, -1.4693864583969116, "Satellite Orbit Altitude 23,222 km"]
+[-0.8152762055397034, 0.13822269439697266, "Satellite System Mission Prime Ball Aerospace"]
+[-0.8310290575027466, 0.1425304263830185, "Satellite System Mission Design Next-generation environmental satellite system for the Department of Defense (DoD)"]
+[-0.8411675095558167, 0.16207733750343323, "Satellite System Predecessor Suomi National Polar-orbiting Partnership (Suomi NPP), Joint Polar Satellite System (JPSS)-1, and the Global Precipitation Measurement (GPM) Microwave Imager (GMI) sensor"]
+[1.804001808166504, 22.088163375854492, "Instrument Scan Altitude 160 to 48 km"]
+[2.428492784500122, 22.71225929260254, "Instrument Scan Time 72 to 202 seconds"]
+[0.12016679346561432, 7.185770511627197, "Experiment Unknown Unknown"]
+[-0.4078650176525116, 14.510947227478027, "Imaging Instrument FOV Support Mode 0.5 km resolution, 1 km resolution, 2 km resolution"]
+[-0.41841253638267517, 14.522961616516113, "Imaging Instrument Full Disk Diameter 17.76\u00ba"]
+[-0.44585633277893066, 14.511785507202148, "Imaging Instrument CONUS Height 4.8129\u00ba"]
+[-0.41898399591445923, 14.519148826599121, "Imaging Instrument CONUS Width 8.0215\u00ba"]
+[-0.4179844260215759, 14.523306846618652, "Imaging Instrument Meso Height/Width 1.6043\u00ba"]
+[-0.6603121161460876, 8.590134620666504, "Cryocooler Cooling Power 53 K and 183 K"]
+[4.170352458953857, -2.9536211490631104, "Satellite Orbit Time 13:30 hours"]
+[4.185447692871094, -2.5074079036712646, "Satellite Revisit Period Shorter than 16 days"]
+[4.1910929679870605, -2.898343324661255, "Satellite Equator Crossing Time Deviation Shorter than 15 minutes"]
+[2.1255595684051514, -1.67596435546875, "Satellite Observation Types Nadir observations, sun-glint observations, and target observations"]
+[1.5062705278396606, -1.7197775840759277, "Satellite Spectrometric Calibration Accuracy Absolute accuracy of 5%, and a relative accuracy of 3%"]
+[1.6411900520324707, -1.420028805732727, "Satellite Localization Accuracy Better than one pixel"]
+[4.190617084503174, -2.8496768474578857, "Satellite Data Transmission Time Within eight hours"]
+[4.680841445922852, -2.5985071659088135, "Satellite Operation Time At least three years"]
+[-0.19804814457893372, 9.060885429382324, "Navigation Device Precision Autonomous"]
+[-1.6091270446777344, 9.678317070007324, "Propulsion System Class 20 mN"]
+[1.689982295036316, 6.962738513946533, "Communication Device Function Transmit instructions for on-board programming and time-tagging information"]
+[7.275431156158447, 12.425230979919434, "Satellite Instrument Application All-weather global tracking, ground-beacon positioning, estimate of the total content of ionospheric free electrons"]
+[2.5037028789520264, -1.26117742061615, "Satellite Data Products Sea surface topography, Significant wave height, Surface wind speed, Ocean tides, Vertically integrated atmospheric water vapor, Vertically integrated ionospheric electron content"]
+[-2.0340325832366943, 12.626358032226562, "Solar UV Imager Installation Date September"]
+[-13.675519943237305, -2.0934882164001465, "Extreme ultraviolet and X-ray Irradiance Sensors Delivery Date September"]
+[5.175759315490723, -4.370453834533691, "Satellite Thermal Vacuum Testing Start Date July 1"]
+[5.098824501037598, -4.401772975921631, "Satellite Thermal Vacuum Testing End Date August 24"]
+[0.6893395781517029, -2.24519681930542, "Satellite Maximum Temperature 87\u00baC"]
+[0.6960912346839905, -2.221829891204834, "Satellite Minimum Temperature -55\u00baC"]
+[11.177145957946777, 5.255828380584717, "CubeSat Mass ~4 kg"]
+[11.15926742553711, 5.279501438140869, "CubeSat Mass ~4 kg"]
+[11.083635330200195, 5.248485565185547, "CubeSat Mass Unknown"]
+[11.083625793457031, 5.253634452819824, "CubeSat Mass Unknown"]
+[16.79681396484375, 6.899919033050537, "Microsatellite Mass ~22 kg"]
+[0.7219276428222656, -4.144406795501709, "Satellite Launch Mass 1515 kg"]
+[5.153443813323975, -2.287262201309204, "Satellite Design Life 3 years for Aquarius and 5 years for the SAC-D instruments"]
+[0.9865922331809998, -4.323462009429932, "Satellite Bus Mass 800 kg"]
+[0.9439198970794678, -4.304516315460205, "Satellite Aquarius Assembly Mass 375 kg"]
+[1.0001953840255737, -4.333000183105469, "Satellite Other SAC-D Instruments Mass 275 kg"]
+[0.14333409070968628, 7.204564094543457, "Experiment Mass 0.7 kg"]
+[0.1619965136051178, 7.230157375335693, "Experiment Power Requirement 1.5 W"]
+[-3.329697608947754, 7.1963276863098145, "Data Handling System Objective Establish a plug-and play space experiment brokering system"]
+[-3.3635573387145996, 4.463160037994385, "Space Technology Research Vehicle-2 Launch Date June 7, 2000"]
+[-3.3189096450805664, 4.431030750274658, "Space Test Research Vehicle-1d Launch Date Nov. 16, 2000"]
+[14.587862014770508, 7.714449882507324, "Nanosatellite Dimensions 10 cm x 10 cm x 34 cm"]
+[14.668956756591797, 7.803641319274902, "Nanosatellite Mass About 3.5 kg"]
+[-2.5904064178466797, 9.615350723266602, "Power Source Average Power 4 W"]
+[-3.714561939239502, 8.328149795532227, "Energy Storage Capacity 4.8 Ah"]
+[-2.3904709815979004, 9.185489654541016, "Power Bus Voltage 4.0 V"]
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+[-1.603324294090271, 9.686929702758789, "Propulsion System Thrust Orientation Major-axis spin inducing"]
+[0.6488469243049622, 9.330550193786621, "Attitude Determination and Control Subsystem Wheel Type 30 mNms wheel"]
+[0.6597680449485779, 9.331341743469238, "Attitude Determination and Control Subsystem Wheel Design Custom (scalable) motor design"]
+[0.667517900466919, 9.331707000732422, "Attitude Determination and Control Subsystem Wheel Enclosure Does not require a pressurised enclosure"]
+[2.5152175426483154, -1.6984220743179321, "Satellite Imaging Instruments Unknown"]
+[3.128678798675537, -2.37083101272583, "Satellite Launch Date Unknown"]
+[2.953583002090454, -1.9638917446136475, "Satellite Mission Status Unknown"]
+[-13.913236618041992, -2.1656436920166016, "X-ray Telescope Energy Range 5 to 30 keV"]
+[-13.793665885925293, -2.196181535720825, "X-ray Telescope Field of View 0.3\u00ba x 0.3\u00ba, 36' diameter"]
+[-13.886714935302734, -2.20444393157959, "X-ray Telescope Angular Resolution HPD~ 30\u201d on-axis at 8 keV"]
+[-13.92152214050293, -2.248561382293701, "X-ray Telescope Mirror Modules 7"]
+[-13.903817176818848, -2.257746934890747, "X-ray Telescope Mirror Shells per Module 28"]
+[-2.48236083984375, 12.565790176391602, "Spectral Imager Spectral Band Centers 8.55, 10.8 and 11.8m"]
+[-2.466114044189453, 12.553955078125, "Spectral Imager Broad-band Window 7 to 13 \u00b5m"]
+[-2.4957661628723145, 12.555126190185547, "Spectral Imager NEDT System Sensitivity Performance 0.1 K"]
+[-2.4819347858428955, 12.554707527160645, "Spectral Imager Spatial Resolution 250 m"]
+[-2.4755654335021973, 12.565756797790527, "Spectral Imager Image Swath-Width 85 km"]
+[-0.5723057389259338, 15.516057968139648, "Imaging Spectrometer Spectral Resolution 0.018 nm"]
+[-0.5142360925674438, 15.478049278259277, "Imaging Spectrometer Wavelength Region 190 nm to 320 nm"]
+[-0.4112044870853424, 15.516777992248535, "Imaging Spectrometer Altitude Region for OH 38 to 90 km"]
+[-0.4469449818134308, 15.530658721923828, "Imaging Spectrometer Altitude Region for NO 48 to 160 km"]
+[-0.4714415669441223, 15.507558822631836, "Imaging Spectrometer Vertical Resolution 2 km"]
+[-0.4982761740684509, 15.514612197875977, "Imaging Spectrometer Down-track Resolution 8\u00ba - 12\u00ba"]
+[6.377817630767822, 7.361004829406738, "Satellite Component Deployment Included in Launch and early operations"]
+[-3.108978271484375, 2.1624560356140137, "Mission Phase Start Main observation periods for GRB events"]
+[-3.124699831008911, 2.1747653484344482, "Mission Phase Duration Within two months"]
+[2.7869679927825928, -2.8479108810424805, "Inter-Satellite Link Realtime Data Exchange Required"]
+[2.6807610988616943, -2.7636191844940186, "Inter-Satellite Link Latency Critical for formation flying missions"]
+[2.7623536586761475, -2.77315092086792, "Inter-Satellite Link Reliability Critical"]
+[-4.51858377456665, 7.826733589172363, "Tracking, Telemetry, and Command Data Reliability Lower criticality compared to ISL"]
+[0.12493296712636948, 7.1872100830078125, "Experiment Purpose Atmospheric occultation experiments"]
+[-0.12197478115558624, 15.507325172424316, "Spectrometer Purpose Detect greenhouse gases"]
+[0.625562846660614, 9.32632064819336, "Attitude Control Subsystem Type Momentum-bias"]
+[-5.294582843780518, 7.897372245788574, "Communications System Type Experimental"]
+[-1.914291262626648, 7.286362648010254, "Computer Type Custom"]
+[-1.622045636177063, 9.675888061523438, "Propulsion System Type Miniature"]
+[2.2675411701202393, 22.599872589111328, "Instrument Quantity > 170000"]
+[2.3063437938690186, 22.551742553710938, "Instrument Quantity 50-100 thousand galaxy clusters and groups"]
+[2.8546319007873535, 22.055625915527344, "Instrument Purpose Study the physics of galactic X-ray source populations, like pre-main sequence stars, supernova remnants and X-ray binaries"]
+[3.898911714553833, 8.977023124694824, "Space Shuttle Accident Date Feb. 1, 2003"]
+[0.13170617818832397, 7.180408954620361, "Experiment Final Mission Report Date March 20, 2003"]
+[0.12309279292821884, 7.203165531158447, "Experiment Web Source No longer available"]
+[2.2281172275543213, -1.803431510925293, "Satellite Antenna Test Location CATR (Compact Antenna Test Range) at Airbus in Ottobrunn Germany"]
+[2.7969071865081787, -2.3100032806396484, "Satellite Launch Site Kourou in French Guiana"]
+[-1.6203429698944092, 1.4875397682189941, "Data Relay System Purpose Relay data between satellites in low orbit and Earth via satellites in geostationary orbit"]
+[-1.6211614608764648, 1.485492467880249, "Data Relay System Technology Laser communication technology"]
+[3.6622562408447266, 17.636966705322266, "Payload Deployment Date 4 March 2019"]
+[3.732734203338623, 17.69899559020996, "Payload Deployment Status Partial"]
+[3.7346463203430176, 17.708621978759766, "Payload Indicators of Successful Demonstration Increase in the decay rate of the mothercraft, changes in the outputs pattern of the solar panels, increase in the brightness of the satellite from ground observations"]
+[2.3577849864959717, 22.13236427307129, "Instrument Measures Surface elevation"]
+[2.8414146900177, 21.947040557861328, "Instrument Purpose Study ice layers and Antarctica\u2019s bedrock"]
+[2.8830275535583496, 21.95346450805664, "Instrument Purpose Collect color images of the ice surface"]
+[2.881352663040161, 21.965410232543945, "Instrument Purpose Read surface temperatures of sea and land ice"]
+[2.8193588256835938, 22.05297088623047, "Instrument Purpose Takes measurements over hundreds of wavelengths"]
+[2.8788747787475586, 21.980056762695312, "Instrument Purpose Map the seafloor underneath the ice shelves"]
+[5.117912769317627, -4.437595844268799, "Satellite Mission Date Aug. 13-21, 2011"]
+[-0.9158443212509155, 6.451876640319824, "Author Documentation Observation of the Earth and Its Environment: Survey of Missions and Sensors"]
+[-0.8505115509033203, 6.132011413574219, "Website Contact Email eoportal@symbios.space"]
+[-2.6149861812591553, 9.62179183959961, "Power Source Quantity 5 parallel strings of 4 series connected"]
+[-2.6007280349731445, 9.610897064208984, "Power Source Quantity 3 parallel of 3 series"]
+[1.7445240020751953, 6.899713516235352, "Communication Device Transmission Power ~1W"]
+[1.6613484621047974, 6.971564292907715, "Communication Device Frequency Uplink = 145 MHz, downlink = 437.375 MHz"]
+[1.7504982948303223, 6.881805419921875, "Communication Device Data Transmission Rates FM communication = 1200 bit/s, CW communication (beacon) = 20 wpm"]
+[-1.7414782047271729, 8.843217849731445, "Control System Type Passive control via permanent magnet and hysteresis dumper"]
+[-1.9392825365066528, 8.121071815490723, "System Type Passive thermal control on the external surfaces"]
+[-0.9698480367660522, 7.939690589904785, "Monitoring Devices Types Solar cell voltage & current, Battery voltage & current, Temperature (panel inside x 6, radio, battery x 3), Angular velocity"]
+[0.09386058151721954, 7.196619987487793, "Experiments Quantity 2"]
+[0.09922562539577484, 7.192025184631348, "Experiments Quantity 5"]
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+[2.075363874435425, 22.535900115966797, "Instrument Sensitivity (NE\u0394T) Infrared Channel 4 K with a scene at 185 K, 1 K with a scene at 300 K"]
+[2.1546032428741455, 22.565670013427734, "Instrument Dynamic Range Visible Channel 65 - 10,000 fL (scene brightness)"]
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+[2.376389503479004, 22.745939254760742, "Instrument Scan Rate 48 rpm"]
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+[7.263908386230469, 12.397275924682617, "Satellite Instrument Manufacturer Harris Corp."]
+[7.313661575317383, 12.44560718536377, "Satellite Instrument Inclusion Plan On all future satellites"]
+[5.150757789611816, -4.04362678527832, "Satellite Launch Date 2021 or 2022"]
+[7.41113805770874, 12.468486785888672, "Satellite Instrument Build Timeline Approximately two years"]
+[7.285820960998535, 12.423548698425293, "Satellite Instrument Manufacturer Harris Corp."]
+[-7.533792018890381, 5.927958011627197, "CCD Camera Frame Rate 180 frames/s"]
+[-7.497368335723877, 5.958671569824219, "CCD Camera Resolution 512 x 80 pixels"]
+[-7.529386520385742, 5.927616596221924, "CCD Camera Field of View 20\u00ba x 3.15\u00ba"]
+[-0.24296174943447113, 15.696738243103027, "Spectrophotometer Modes of Operation Sprite continuous mode, sprite burst mode, auroral mode"]
+[-0.24699248373508453, 15.615556716918945, "Spectrophotometer Data Storage Separate 128 MByte memory"]
+[-0.27060267329216003, 15.605639457702637, "Spectrophotometer Data Downlink S-band"]
+[-0.2544618248939514, 15.61968994140625, "Spectrophotometer Total Data Volume About 1 Gbit/day"]
+[-2.1598193645477295, 6.527969837188721, "Flight Software Version 7.1.0"]
+[-1.931959867477417, 6.9233717918396, "Software Upgrade Yes"]
+[2.2511000633239746, -1.6895664930343628, "Satellite Photo Figure 3"]
+[2.346134901046753, -1.410513162612915, "Satellite Illustration Figure 4"]
+[2.964038133621216, -2.050736427307129, "Satellite Dragsail Deployment After DSAT-3 deploys a dragsail"]
+[-7.584733009338379, 5.916196823120117, "Cameras Data Collection As long as LOS (Line-Of-Sight) is maintained"]
+[-3.507274866104126, 6.831479549407959, "Data Download Method During ground contact windows"]
+[-1.9112573862075806, 6.912038326263428, "Software Function Provide \u2018ground truth\u2019 data against which the navigation algorithms will be compared for validation and performance assessment"]
+[0.6079453825950623, 12.02456283569336, "Gas Sensors Mounting Three flexures and an adapter ring"]
+[0.671532392501831, 11.993948936462402, "Sensor Assembly Design Athermalised optical design"]
+[-0.69287109375, 8.159770011901855, "Enclosure Material Aluminium honeycomb"]
+[-0.8579041957855225, 7.718975067138672, "Enclosure Mounting Four corner flexures"]
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+[1.819227695465088, -3.0396876335144043, "Satellite Possible Potential Rate 195"]
+[2.9573962688446045, -2.0341482162475586, "Satellite Development Status Unknown"]
+[3.1324069499969482, -2.364208459854126, "Satellite Launch Date Unknown"]
+[4.564524173736572, -2.664048433303833, "Satellite Observation Duration More than 11 years"]
+[-5.876660346984863, 16.014942169189453, "Synthetic Aperture Radar Frequency Band L-band"]
+[3.1828267574310303, -1.7921448945999146, "Satellite Manufacturer Mitsubishi Electric Corporation"]
+[3.062370777130127, -1.6682060956954956, "Satellite Contractor JAXA (Japan Aerospace and Exploration Agency)"]
+[6.1774582862854, 7.562123775482178, "Satellite Component Quantity 2"]
+[6.158929347991943, 7.577225685119629, "Satellite Component Quantity 1"]
+[6.1697187423706055, 7.564643859863281, "Satellite Component Quantity 2"]
+[6.187242031097412, 7.5518646240234375, "Satellite Component Quantity 2"]
+[6.202927112579346, 7.533050537109375, "Satellite Component Quantity 2"]
+[6.165257453918457, 7.579172134399414, "Satellite Component Quantity 1"]
+[6.134354114532471, 7.600511074066162, "Satellite Component Quantity 1"]
+[6.175648212432861, 7.562963962554932, "Satellite Component Quantity 2"]
+[-5.8259148597717285, 15.758865356445312, "Aperture Synthesis Technology Antenna Size Large"]
+[-1.9160261154174805, 14.923064231872559, "1D Interferometric Radiometer Antenna 6 x 9 m parabolic cylinder mesh reflector"]
+[-1.8263401985168457, 14.94011402130127, "1D Interferometric Radiometer Feed Array Tri-frequency patch feed array"]
+[-5.532309532165527, 9.5047607421875, "Frequency Band Along-track resolution 35 km"]
+[-5.531786918640137, 9.505104064941406, "Frequency Band Along-track resolution 20 km"]
+[-5.51226806640625, 9.511143684387207, "Frequency Band Along-track resolution 10 km"]
+[-5.532800197601318, 9.499716758728027, "Frequency Band Cross-track resolution 35-75 km"]
+[-5.534262180328369, 9.506217956542969, "Frequency Band Cross-track resolution 20-45 km"]
+[-5.539894104003906, 9.502897262573242, "Frequency Band Cross-track resolution 15-30 km"]
+[-5.532304763793945, 9.506967544555664, "Frequency Band Radiometric resolution 0.2 K"]
+[-5.535175800323486, 9.504097938537598, "Frequency Band Radiometric resolution 1.5 K"]
+[-5.527235507965088, 9.493525505065918, "Frequency Band Radiometric resolution 0.6 K"]
+[-5.524829864501953, 9.515106201171875, "Frequency Band FOV 1000 km"]
+[-5.535188674926758, 9.481008529663086, "Frequency Band FOV 1000 km"]
+[-5.5265583992004395, 9.515034675598145, "Frequency Band FOV 1000 km"]
+[2.6157259941101074, -1.849328875541687, "Satellite Platform NEXTAR"]
+[2.5121796131134033, -1.7507612705230713, "Satellite Architecture New system Architecture for Observation"]
+[-2.448728561401367, 13.19509220123291, "Hyperspectral Imager Manufacturer Kestrel Corporation of Albuquerque, NM, and the Florida Institute of Technology, Melbourne, FL"]
+[-2.4391820430755615, 13.181105613708496, "Hyperspectral Imager Objective Demonstrate spaceborne hyperspectral imaging technologies"]
+[-2.445542573928833, 13.183833122253418, "Hyperspectral Imager Advantage Can record the full spectra without any time delay and can decouple the spatial and spectral signatures"]
+[-5.913751602172852, 16.027860641479492, "Synthetic Aperture Radar Mass 147 kg"]
+[-5.883474349975586, 16.009828567504883, "Synthetic Aperture Radar Power Consumption 216 W"]
+[-5.862544059753418, 16.03139877319336, "Synthetic Aperture Radar Peak Power 1000 W"]
+[-5.8698225021362305, 16.01140022277832, "Synthetic Aperture Radar Operation Time 10 minutes per orbit"]
+[-2.7131330966949463, 15.292486190795898, "Scanning Multichannel Microwave Radiometer Device Type Radiometer"]
+[1.5702557563781738, 2.349273920059204, "Geostationary Operational Environmental Satellite Image Acquisition Date October 25"]
+[-0.7665113806724548, 5.155846118927002, "Location 48-hour Total Precipitation 16.55 inches"]
+[-0.7483243346214294, 5.186182975769043, "Location Precipitation on October 24 4.02 inches"]
+[-0.7630537152290344, 5.115035057067871, "Location 24-hour Total Precipitation on October 24-25 10.4 inches"]
+[-0.8108481764793396, 5.065971851348877, "Location 24-hour Total Precipitation on October 24-25 5.44 inches"]
+[-0.5668401122093201, 4.9604034423828125, "Region High Surf Warnings Swells of 16 to 24 feet"]
+[-3.0112340450286865, 4.232207298278809, "Spacecraft Image Credit NSPO"]
+[1.3963099718093872, 5.454512596130371, "Bus Image Credit NSPO"]
+[-1.9169752597808838, 14.84946060180664, "Radiometer Band Centers 3.8 \u00b5m (MWIR), 10.85 \u00b5m and 11.85 \u00b5m (TIR)"]
+[-1.9036976099014282, 14.851215362548828, "Radiometer Resolution 350 m"]
+[-1.9209342002868652, 14.889432907104492, "Radiometer Field of Regard 1064 km"]
+[-1.8810863494873047, 14.848679542541504, "Radiometer Field of View \u00b137.8\u00ba"]
+[-1.8913935422897339, 14.870567321777344, "Radiometer Temperature Range MWIR: 300-700 K and TIR: 250-500 K"]
+[-1.8714189529418945, 14.859665870666504, "Radiometer NEDT Better than 0.5 K at 400 K in the MWIR range and better than 0.4 K at 300 K in the TIR range"]
+[-1.8830443620681763, 14.890880584716797, "Radiometer Focal Plane Array 512 x 3 pixel microbolometer focal plane array (FPA)"]
+[-1.6188483238220215, 9.666726112365723, "Propulsion System Propellant Mass 120 kg"]
+[-3.3070545196533203, 4.23724365234375, "Spacecraft Design Life 7 years"]
+[-5.17645263671875, 7.839650630950928, "Communication System X-band Data Downlink 560 Mbit/s"]
+[-5.275059223175049, 7.8059306144714355, "Communication System S-band Uplink Data Link 64 kbit/s"]
+[-5.254975318908691, 7.895455837249756, "Communication System S-band Downlink Data Link 2 Mbit/s"]
+[-3.840115547180176, 7.961480617523193, "Data Storage Capacity 2.4 Tbit"]
+[-1.4881941080093384, 13.418081283569336, "Solar Arrays Installation Date Summer 2021"]
+[-1.7036323547363281, 8.221576690673828, "Legacy Unit Purpose Provide critical sparing support for the water production capability for the environmental control and life support system (ECLSS)"]
+[-2.0351381301879883, 8.741270065307617, "Emergency Air Supply System Support Duration Up to one hour"]
+[-1.904349684715271, 8.847249031066895, "Control Module Purpose Cosmonaut remote-control docking of Russian spacecraft"]
+[-0.9532203078269958, 8.536623001098633, "Filter Assembly Purpose Remove iodine from water consumed by the crew during nominal operations"]
+[-1.2321025133132935, 9.097245216369629, "Air Tanks Purpose Support gas resupply for routine cabin repress activities on-orbit"]
+[3.7130932807922363, 17.69207000732422, "Cold Stowage Capability Purpose Support expanded payload operations"]
+[-7.395533084869385, 2.8680593967437744, "Cosmic Ray Detector Mission Duration Since 2011"]
+[-7.389590740203857, 2.870482921600342, "Cosmic Ray Detector Number of Particles Recorded Over 140 billion particles"]
+[-7.39754056930542, 2.8697452545166016, "Cosmic Ray Detector Data Collection Upgrade Needed"]
+[-0.42076635360717773, 14.515743255615234, "Imaging Instrument Prime Contractor Airbus DS (former EADS Astrium SAS)"]
+[-0.8115622997283936, 11.599724769592285, "Detector Manufacturer Airbus DS-ISAE-e2v"]
+[-0.8236161470413208, 11.594620704650879, "Detector Manufacturer Sofradir"]
+[-3.3502144813537598, 7.4822564125061035, "Data Processing Compression Type Lossy compression based on wavelet transform"]
+[-3.485105276107788, 6.841806411743164, "Data Digitization 12 bit"]
+[2.8532235622406006, 22.016826629638672, "Instrument Mechanism Purpose Prevent the instrument from direct viewing of the sun in orbit and from contamination during launch"]
+[2.070253610610962, 22.529369354248047, "Instrument Performance Average 16.3 minutes"]
+[2.1982903480529785, 22.576967239379883, "Instrument Performance Peak 31 minutes"]
+[16.894311904907227, 6.825756072998047, "Microsatellite Design Four aluminum sandwich \u201ctrays\u201d assembled and kept together by four aluminum columns"]
+[16.868549346923828, 6.847930908203125, "Microsatellite Tray Dimensions 150 mm side with an overall height of 250 mm"]
+[-2.7774736881256104, 8.055183410644531, "Embedded microprocessor system module Microprocessor Rabbit 3000 8-bit microprocessor"]
+[-2.8393075466156006, 8.108736038208008, "Embedded microprocessor system module Microprocessor Clock Speed 29.4 MHz"]
+[-2.7737107276916504, 8.099937438964844, "Embedded microprocessor system module A/D Converter 11-bit 8-channel (or 12-bit 4-channel if used in differential mode)"]
+[-2.9699060916900635, 8.280522346496582, "Embedded microprocessor system module Flash Memory 512 kB"]
+[-3.0013160705566406, 8.349858283996582, "Embedded microprocessor system module Static RAM 512 kM"]
+[0.9507796764373779, 0.8506636619567871, "Earth Science Capability URL http://cats.gsfc.nasa.gov/index.html"]
+[-4.753054141998291, 9.259993553161621, "Transmitter Data Rate Up to 100 Mbit/s"]
+[-1.131822943687439, 7.326186656951904, "Equipment Compatibility Fully CCSDS compatible with ranging and coherent transmission capabilities"]
+[4.683979511260986, -4.551758766174316, "Satellite Image Capture Date 25 January 2022"]
+[4.656269073486328, -4.552246570587158, "Satellite Image Capture Date 20 January 2022"]
+[4.686637878417969, -4.565820217132568, "Satellite Image Capture Date January 28, 2022"]
+[-2.0735156536102295, 7.358531951904297, "Operating System Type Multithreaded"]
+[14.525386810302734, 7.68828010559082, "Nanosatellite Configuration Triple-cube"]
+[14.487295150756836, 7.70814323425293, "Nanosatellite Propulsion System Custom cold-gas"]
+[14.52751636505127, 7.715166091918945, "Nanosatellite Reaction Wheel 30 mNms"]
+[14.49787712097168, 7.690132141113281, "Nanosatellite GPS Receiver Commercially available"]
+[-5.245038986206055, 7.854296684265137, "Communications System Uplink Rate 125 bit/s"]
+[-5.282627582550049, 8.026589393615723, "Communications System Uplink Frequency 2.025-2.12 GHz"]
+[-5.206862926483154, 7.835513114929199, "Communications System Downlink Rate 1 kbit/s"]
+[-5.197299957275391, 8.023054122924805, "Communications System Downlink Frequency 2.2-2.3 GHz"]
+[-2.3328676223754883, 7.448713302612305, "Single Board Computer Processor Type PowerPC 750FX"]
+[-2.315433979034424, 7.403774738311768, "Single Board Computer Processor Configuration Triple-modular redundant"]
+[-2.318368673324585, 7.413712978363037, "Single Board Computer MIPS 1500"]
+[-2.306015729904175, 7.397228240966797, "Single Board Computer Radiation Susceptibility 1 uncorrected processor upset every 128 years"]
+[-2.434185743331909, 8.045490264892578, "Network Interface Card Number of Bidirectional Serial Ports 9"]
+[-2.3942196369171143, 8.074755668640137, "Network Interface Card Number of Unidirectional Serial Ports 1"]
+[-2.3679723739624023, 8.107379913330078, "Network Interface Card Serial Port Hardware Layer RS-422"]
+[-2.387812852859497, 8.095247268676758, "Network Interface Card Bidirectional Port Protocol UART (Universal Asynchronous Receiver/Transmitter)"]
+[-2.392462968826294, 8.064619064331055, "Network Interface Card Bidirectional Port Baud Rates 9600 to 115,200 baud"]
+[-2.37390398979187, 8.082188606262207, "Network Interface Card Unidirectional Port Protocol Clock, data, and enable"]
+[-2.41469144821167, 8.066080093383789, "Network Interface Card Unidirectional Port Data Rate 40 kbit/s"]
+[-2.7504210472106934, 11.536162376403809, "Pushbroom Imager Lens Focal Length 50.8 mm"]
+[-2.7346832752227783, 11.55412769317627, "Pushbroom Imager Lens Optical Diameter 70 mm"]
+[-2.7593891620635986, 11.518597602844238, "Pushbroom Imager Cross Track Full FOV Approximately 15\u00ba"]
+[-2.749305486679077, 11.520709991455078, "Pushbroom Imager Data Storage Two standard Exabyte-8505c 8mm tape recorders"]
+[-2.7619338035583496, 11.513992309570312, "Pushbroom Imager Blackbody Calibration Target Included"]
+[-0.832225501537323, 11.593639373779297, "Detector Data Transmission Rate 4 Mbit/s"]
+[-0.8408411741256714, 11.649962425231934, "Detector Health and Status Data Transmission Rate 1 kbit/s"]
+[2.8762564659118652, -2.0258781909942627, "Satellite Mission Results and Anomaly Investigation Unknown"]
+[2.6991968154907227, -1.96410071849823, "Satellite Testing and On-orbit Performance Unknown"]
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+[2.451201915740967, 22.729150772094727, "Instrument Antenna Quantity 1"]
+[2.657170534133911, 22.465538024902344, "Instrument Antenna Type Directive velocity antenna"]
+[2.411871910095215, 22.764925003051758, "Instrument Antenna Quantity 1"]
+[2.7780823707580566, 22.58002281188965, "Instrument Communication Interface MIL-STD-1553"]
+[2.612706422805786, 22.886940002441406, "Instrument Processor ADSP 21020"]
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+[2.7545487880706787, 23.283952713012695, "Instrument Operation Receives L1 C/A, L1 P(Y) and L2 P(Y) signals from GPS satellites"]
+[2.7810568809509277, 22.869163513183594, "Instrument Operation Performs position, time and velocity calculation based on a least square algorithm"]
+[2.884969472885132, 22.701522827148438, "Instrument Operation Provides observable data for each GPS satellite in lock"]
+[-0.10860832780599594, 13.605019569396973, "Measurement Configuration Horizontal and Vertical Direction Illustrated"]
+[-0.12129680067300797, 13.596695899963379, "Measurement Configuration FFOV (Forward FOV), AFOV (Aft FOV), LSFOV (Left Side FOV), RSFOV (Right Side FOV) Legend"]
+[1.3769817352294922, -1.240700125694275, "Satellite Ephemeris Accuracy 50-70 cm"]
+[1.7714109420776367, -1.4580180644989014, "Satellite Ephemeris Goal Submeter accuracy for the vertical component"]
+[2.748521327972412, -1.8304696083068848, "Satellite Ephemeris Improvement Expected"]
+[2.1645965576171875, -1.6356006860733032, "Satellite Ephemeris Accuracy Improvement Expected"]
+[2.7100462913513184, -1.4894884824752808, "Satellite Discovery Transiting Super-Earth in the pi Mensae System"]
+[4.97649621963501, -4.325369834899902, "Satellite Publication Date 30 November 2018"]
+[-3.116554021835327, 1.7619820833206177, "Satellite Mission Launch Provider ISC (International Space Company) Kosmotras"]
+[-3.1066174507141113, 1.7067103385925293, "Satellite Mission Launch Vehicle Dnepr rocket"]
+[-3.1428160667419434, 1.7380841970443726, "Satellite Mission New Launch Vehicle Falcon-9 rocket"]
+[-0.9711210131645203, 9.814377784729004, "Rocket Factors for Selection Reliability, cost, availability, and capability of lifting the satellite to its desired orbit"]
+[2.793170928955078, -1.1989086866378784, "Satellite Purpose Find the second Earth"]
+[-0.18902687728405, 6.845866680145264, "Test Date 01 June 2022"]
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+[5.075270175933838, -4.320672988891602, "Satellite Science Operations Start Date Mid-June"]
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+[-1.4811985492706299, 9.520591735839844, "Thruster Group N/A N/A"]
+[-5.314879417419434, 7.299772262573242, "Connection N/A N/A"]
+[-1.4203619956970215, 8.829299926757812, "Valve N/A N/A"]
+[-1.1935633420944214, 9.194332122802734, "Tank N/A N/A"]
+[-2.2340242862701416, 8.174710273742676, "Interface N/A N/A"]
+[-1.9327397346496582, 8.717082023620605, "Control Unit N/A N/A"]
+[-2.6286144256591797, 9.582151412963867, "Power N/A N/A"]
+[3.781308174133301, -2.748295783996582, "Satellite N/A N/A"]
+[-1.8916990756988525, 6.884693622589111, "Software N/A N/A"]
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+[0.52508544921875, 12.205825805664062, "Sensor Deployment Velocity 5 cm/s"]
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+[-6.747674465179443, 10.012845039367676, "Antenna Azimuth Resolution 1 m / 3 m / 6 m / 10 m / 100 m"]
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+[-0.9530262351036072, 6.466731548309326, "Product Guide Definition Unknown"]
+[-3.087697744369507, 6.784894943237305, "Product Distribution Function Provide data and products to the appropriate entities"]
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+[-3.355088710784912, 4.242042541503906, "Spacecraft Collection Mode Duration 2 years"]
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+[0.6194266676902771, -1.4720288515090942, "Satellite Expected Distance from Earth in 2029 7 million km"]
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+[-7.5850419998168945, 5.914095401763916, "Camera Type CCD (Charge Coupled Device)"]
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+[2.1603705883026123, -1.333294153213501, "Satellite Image Capture Solar corona\u2014including the region that is 10 times the Sun\u2019s angular diameter"]
+[2.7966272830963135, -1.2360222339630127, "Satellite Purpose Provision of satellite connectivity to \u201cinternet-of-things\u201d (IOT) devices"]
+[2.797337532043457, -1.1819725036621094, "Satellite Purpose Tryout of technology for the precise orbit insertion of small satellites of CubeSat format"]
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+[2.209153652191162, 22.03487205505371, "Instrument Across-Track Slope Calculated"]
+[2.0916194915771484, 22.336280822753906, "Instrument Temperature Range Below -20\u00ba Fahrenheit (-29\u00baC)"]
+[1.7724040746688843, 22.082839965820312, "Instrument Distance from Other People A hundred miles"]
+[-0.8600729703903198, 11.645909309387207, "Detector Sensitivity AC component of the signal"]
+[2.6895594596862793, 23.649566650390625, "Chopper Chopping Frequency 10 Hz"]
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+[-0.8323490619659424, 11.643038749694824, "Detector Wavelength Range 0.2 - 4 \u00b5m"]
+[-0.7803301215171814, 11.682845115661621, "Detector Wavelength Range 0.2 - 50 \u00b5m"]
+[-0.8590360283851624, 11.64286994934082, "Detector Wavelength Range 10.5 - 12.5 \u00b5m"]
+[-3.6509501934051514, 12.750860214233398, "Particle Detector Antiproton Background Rejection Close to 1 in a million"]
+[-3.6364212036132812, 12.755354881286621, "Particle Detector Antiproton Sample 349,000 antiprotons"]
+[-3.6310675144195557, 12.752197265625, "Particle Detector Antiprotons with Energies Above 100 Billion Electron Volts 2200"]
+[-3.636118173599243, 12.761198043823242, "Particle Detector Proton Flux Accuracy 1%"]
+[-3.622077465057373, 12.757237434387207, "Particle Detector Proton Flux 300 million protons"]
+[-3.635490655899048, 12.759151458740234, "Particle Detector Number of Instruments 7"]
+[-3.6345372200012207, 12.760963439941406, "Particle Detector Studied Nuclei Helium, lithium, carbon, oxygen and heavier nuclei up to iron"]
+[-3.644444465637207, 12.756935119628906, "Particle Detector Helium Flux Second most abundant cosmic ray"]
+[-3.6515448093414307, 12.778411865234375, "Particle Detector Lithium Flux Behaves similarly to protons and helium"]
+[1.8678574562072754, 22.166946411132812, "Instrument Ground Spacing ~85 m"]
+[1.843247413635254, 22.156776428222656, "Instrument Ground Spacing ~85 m"]
+[2.2643678188323975, 22.08930778503418, "Instrument Across-Track Slope Calculated"]
+[2.2601330280303955, 22.066930770874023, "Instrument Across-Track Slope Calculated"]
+[1.3880378007888794, 2.307933807373047, "Lightning Mapper Detection Efficiency 80%"]
+[1.3727316856384277, 2.312533378601074, "Lightning Mapper Operation 24 hours"]
+[1.390099048614502, 2.3079111576080322, "Lightning Mapper Frame Rate 500 frames/s"]
+[5.2533087730407715, -4.443859577178955, "Satellite Launch Date Oct. 28, 2014"]
+[0.7345829606056213, 12.004404067993164, "Sensor Type Line scanning"]
+[-0.8304004669189453, 11.607501029968262, "Detector Sensitivity Highly sensitive"]
+[-3.078033208847046, 4.186013698577881, "Spacecraft Stabilization Three axes"]
+[-3.089174509048462, 4.267664432525635, "Spacecraft Scanning Always \"looked down\""]
+[1.1732897758483887, -1.8682078123092651, "Satellite Relative Maneuver Precision Millimeter and fraction-of-a-degree"]
+[1.0127969980239868, -1.2148158550262451, "Satellite Formation Distance 150 m"]
+[4.41827392578125, -2.6731481552124023, "Satellite Monitoring Duration 27 days"]
+[-0.6135133504867554, 3.230607509613037, "Star Mass Roughly 40% of the Sun\u2019s mass"]
+[-0.6182821989059448, 3.2234930992126465, "Star Size Roughly 40% of the Sun\u2019s size"]
+[-0.5868893265724182, 3.1979429721832275, "Star Surface Temperature About half its surface temperature"]
+[-0.39093512296676636, 3.76086688041687, "Planet Size About the size of Earth"]
+[-0.4100487232208252, 3.7447292804718018, "Planet Transit No flares from the star"]
+[-1.1761549711227417, 15.098745346069336, "Imaging multi-spectral radiometers Instrument Type Imaging multi-spectral radiometers (vis/IR)"]
+[3.158411979675293, -1.5440512895584106, "Satellite Mission Type EO"]
+[3.012540578842163, -1.7115269899368286, "Satellite Agency ROSKOSMOS"]
+[5.304259777069092, -4.483249664306641, "Satellite Launch Date 26 Aug 2005"]
+[5.074825286865234, -4.123016357421875, "Satellite End of Life Date 21 Jan 2008"]
+[-3.2680389881134033, 5.411683082580566, "Launch Vehicle Orbit Sun-synchronous orbit, altitude altitude = 700 km, inclination = 98.25\u00ba"]
+[4.660470485687256, -2.6030995845794678, "Satellite Mission Duration Initially projected for a mission duration of three years"]
+[5.058001518249512, -2.3467516899108887, "Satellite Retirement Retired after operating for 11 years"]
+[2.2508466243743896, -1.3704195022583008, "Satellite Images Taken 13,362 images"]
+[1.5235888957977295, -2.4225616455078125, "Satellite Orbits 58,726 orbits"]
+[2.6216061115264893, 13.485899925231934, "Optical Components Quantity 7"]
+[-0.8253266215324402, 11.644170761108398, "Semiconductor CdTe double-sided strip detectors Energy Resolution About 10% above 10 keV"]
+[-0.8214275240898132, 11.618556022644043, "Semiconductor CdTe double-sided strip detectors Timing Capabilities Yes"]
+[-13.955162048339844, -2.2343597412109375, "X-ray Telescope Manufacturer ART-XC consortium"]
+[-13.710450172424316, -2.292954444885254, "X-ray Telescope Agreement Date Aug. 18, 2009"]
+[2.498751401901245, -1.5880510807037354, "Satellite Discovery Tool Exoplanets"]
+[-5.340003490447998, 2.7875800132751465, "Telescope Discovery Tool Exoplanets"]
+[-4.565536022186279, -3.0858371257781982, "Exoplanet Size Jupiter-size"]
+[-4.5895586013793945, -3.119874954223633, "Exoplanet Orbit Period Every day and a half"]
+[-4.5862860679626465, -3.1132097244262695, "Exoplanet Orbit Shape Elliptical"]
+[-4.586921691894531, -3.1158039569854736, "Exoplanet Orbit Stability Unstable"]
+[-0.7067187428474426, 3.2439301013946533, "Red Dwarfs Gravitational Influence Less likely"]
+[-13.66865348815918, -2.3211803436279297, "X-ray Telescope Launch Date 13 July 2019"]
+[-13.88266658782959, -2.2527360916137695, "X-ray Telescope Journey Distance 1.5 million kilometers"]
+[-13.916341781616211, -2.2796082496643066, "X-ray Telescope Target Orbit Lagrange point (L2)"]
+[-13.686846733093262, -2.3089518547058105, "X-ray Telescope Commissioning Phase Completion Date October 13"]
+[-13.799545288085938, -2.2754199504852295, "X-ray Telescope Prime Phase Duration Four years"]
+[-2.1484615802764893, 2.905881881713867, "Observatory Separation Date Unknown"]
+[4.406789302825928, -2.6848204135894775, "Satellite Observation Duration 27 days"]
+[3.7331762313842773, -2.5671849250793457, "Satellite Image Frequency Every 30 minutes"]
+[3.8051657676696777, -2.6051666736602783, "Satellite Snapshot Frequency Every two minutes"]
+[-0.6493292450904846, 3.184868335723877, "Star Type Pulsation Patterns Regular"]
+[-0.6377210021018982, 3.192084550857544, "Star Type Number of Identified Stars 60"]
+[-4.452795505523682, 9.426133155822754, "Animal Tracking System Receiver Signal Frequency 145.860 MHz"]
+[-0.3367292284965515, 10.474325180053711, "Animal Tracking System Receiver Mission Life 1 year"]
+[-0.2609095275402069, 10.760364532470703, "Animal Tracking Terminal Type GPS-In"]
+[-0.25329670310020447, 10.760480880737305, "Animal Tracking Terminal Type GPS-Ex"]
+[-0.27195683121681213, 14.029240608215332, "Electric Plasma Probe Objective Measure electron density and temperature in the upper atmosphere"]
+[2.3802287578582764, -1.9897092580795288, "Satellite Launch Box Purpose 1 Protect spacecraft during shipping, launch, and handling aboard the ISS"]
+[2.6561195850372314, -1.812805414199829, "Satellite Launch Box Purpose 2 Protect astronauts from protrusions and sharp edges during handling aboard the ISS"]
+[-2.849588394165039, 5.009265899658203, "Shipping Container Wrapping Foam"]
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+[0.8050448894500732, 4.063482761383057, "Atmospheric Measurement Definition Amount of water in a column of the atmosphere if all the water vapor in that column were condensed into liquid"]
+[-3.409390449523926, 7.284595012664795, "Data Assimilation System Data Source Satellite data and mathematical representations of physical processes"]
+[-5.000345706939697, 8.158958435058594, "Communication Module Size 25 mm x 15 mm x 14 mm"]
+[-5.016080856323242, 8.161352157592773, "Communication Module Mass 8 gram"]
+[-5.037164211273193, 8.10744857788086, "Communication Module Power Consumption 50 mW"]
+[-1.1094807386398315, 7.787909507751465, "Emitter Quantity Duplicated in every module"]
+[-4.940184593200684, 9.775886535644531, "Receiver Quantity Two"]
+[-1.2099659442901611, 4.426220417022705, "Ground Station Component Diameter 10 m"]
+[-1.251125693321228, 4.407543182373047, "Ground Station Component Diameter 11.28 m"]
+[-1.2035404443740845, 4.434054851531982, "Ground Station Component Recording Capacity Up to 160 Mbit/s"]
+[6.276248931884766, 7.466879367828369, "Satellite Component Spectral Bands Green (520-600 nm), red (630-690 nm), near infrared (770-900 nm)"]
+[6.351368427276611, 7.392627239227295, "Satellite Component Field of View 21.0 by 14.9 degrees"]
+[6.3399338722229, 7.404575824737549, "Satellite Component Swath Width 220 Kilometres"]
+[6.316160202026367, 7.427610874176025, "Satellite Component Resolution 22 metres"]
+[0.4944304823875427, 10.936385154724121, "Image Sensor Resolution 10000 by 7096 pixels"]
+[0.5246098637580872, 10.93000316619873, "Image Sensor Pixel Size 3.1 \u03bcm x 3.1 \u03bcm"]
+[0.5141328573226929, 10.921796798706055, "Image Sensor Analog Outputs 8"]
+[0.5013163089752197, 10.949432373046875, "Image Sensor Analog Output Frequency 30MHz"]
+[0.5051654577255249, 10.92381763458252, "Image Sensor Frame Rate 0.5 frames per second"]
+[0.49325117468833923, 10.922911643981934, "Image Sensor Bit Depth 12-bit"]
+[1.5384975671768188, 21.259944915771484, "Instrument Mass 2.4 kg"]
+[1.60287606716156, 23.23341178894043, "Instrument Power Consumption 2.5 W"]
+[1.6495496034622192, 22.214231491088867, "Instrument Size 281 mm x 155 mm x 71 mm"]
+[1.5330461263656616, 21.25383758544922, "Instrument Mass 2 kg"]
+[1.6424169540405273, 22.17630958557129, "Instrument Size 116 mm x 202 mm x 90 mm"]
+[0.12345655262470245, 7.194779396057129, "Student Experiment Module Number of Experiments 10"]
+[-3.6084024906158447, 12.751994132995605, "Particle Physics Technology Application Manned Interplanetary Flight"]
+[-3.6226656436920166, 12.762703895568848, "Particle Physics Technology URL http://ams.cern.ch/AMS/ETB/Appendix%20A-AMSonISS_Technology_Applications_Interplanetary.pdf"]
+[-2.620145559310913, 9.609365463256836, "Power Source Power Output 200 W"]
+[-2.5763463973999023, 9.652803421020508, "Power Source Cell Efficiency 26%"]
+[-2.586404323577881, 9.637093544006348, "Power Source Articulation Mechanism Resolution 1/64\u00ba"]
+[-3.7021737098693848, 8.332535743713379, "Energy Storage Capacity 15 Ah"]
+[-2.376230001449585, 7.310885429382324, "Onboard Computer Processor transputer T805 @ 20 MHz"]
+[-2.333406448364258, 7.32550048828125, "Onboard Computer Processing Capacity 2 MIPS"]
+[-2.3619892597198486, 7.300083637237549, "Onboard Computer Radiation Hardened 15 krad, SEL and SEU immune"]
+[-2.411391258239746, 7.337162971496582, "Onboard Computer Power Consumption 6 W max"]
+[-2.3608312606811523, 7.310459613800049, "Onboard Computer Mass 3 kg"]
+[2.5362071990966797, -1.9375600814819336, "Satellite Onboard Computers Mil Std 1750A, (dual-redundant)"]
+[2.4278206825256348, -2.571599245071411, "Satellite Onboard Computers RAM 128 kByte"]
+[3.01326584815979, -1.7947343587875366, "Satellite Operating System (kernel) Developed by the Mitre Corporation"]
+[2.539038896560669, -2.5986289978027344, "Satellite Operating System (kernel) RAM 120 kByte"]
+[-3.1604669094085693, 1.7195903062820435, "Satellite Mission Operator DLR/GSOC"]
+[-3.124864101409912, 1.7249393463134766, "Satellite Mission Operation Duration More than 10 years"]
+[-3.137782335281372, 1.685462474822998, "Satellite Mission Monitoring Capability Mass motions in the Earth system with unprecedented accuracy and temporal resolution"]
+[1.2503559589385986, -1.2670230865478516, "Small Satellite Capabilities Microwave Atmospheric Remote Sensing"]
+[11.270329475402832, 5.509326934814453, "CubeSat URL https://tropics.ll.mit.edu/CMS/tropics/The-MicroMAS-2-Cubesat"]
+[0.2371223270893097, 13.78671932220459, "Calibration System Calibration Distance 7 m and 70 m"]
+[0.2614123821258545, 13.768630027770996, "Calibration System Test Location RAL Space, in Harwell, UK"]
+[2.6916327476501465, 22.20281410217285, "Instrument Applications Monitoring displacement between satellites in constellation, measuring structural distortion before, during, and after deployment of large-scale structures, and fine-tuning positioning of telecommunication satellite antennas"]
+[5.032660961151123, -4.346620082855225, "Satellite Discovery Date January 27, 2021"]
+[-0.7486806511878967, 3.1656334400177, "Six-Star System Distance from Earth About 1,900 light-years"]
+[-0.7160775065422058, 3.184211254119873, "Binary Stars Orbital Period Roughly every day and a half"]
+[-0.7208489775657654, 3.1910805702209473, "Binary Stars Orbital Period About every four years"]
+[-0.7400787472724915, 3.1390256881713867, "Binary Stars Orbital Period About every eight days"]
+[11.486030578613281, 5.705694675445557, "CubeSat Size 2U"]
+[11.231234550476074, 5.470043659210205, "CubeSat Panel Deployment Cross Shape"]
+[11.216532707214355, 5.467499256134033, "CubeSat Momentum Wheel Activated just before leaving the platform"]
+[11.245933532714844, 5.465020656585693, "CubeSat Debris-Capture Materials Bag or net"]
+[11.241551399230957, 5.474409580230713, "CubeSat Camera Internally mounted"]
+[11.147028923034668, 5.342364311218262, "CubeSat LEDs Light up the impact space"]
+[14.25981616973877, 7.7966389656066895, "Nanosatellite Launch Date Aug. 14, 2017"]
+[14.471819877624512, 7.728917598724365, "Nanosatellite Orbit Altitude ~400 km"]
+[16.77892303466797, 6.9145121574401855, "Microsatellite Mass ~50 kg"]
+[-5.401071071624756, 2.803748607635498, "Telescope Resolution (Pan/MS) 1.5 m / 6 m"]
+[-5.394052028656006, 2.7995645999908447, "Telescope FOV (Field of View) 1,87\u00ba"]
+[-5.416380882263184, 2.822983741760254, "Telescope Swath width (550 km orbital altitude) 12-18 km with 8-12 kpixel"]
+[-5.403613090515137, 2.7475762367248535, "Telescope Payload mass < 20 kg electronics inclusive"]
+[-5.453894138336182, 2.736600160598755, "Telescope Instrument size 400 x 400 x 250 mm folded 400 x 400 x 1000 mm unfolded"]
+[-5.407342433929443, 2.7901580333709717, "Telescope Pointing accuracy 2 arcmin"]
+[-5.37125301361084, 2.7305169105529785, "Telescope Jitter performance 0.185 arcmin/s"]
+[-5.470339775085449, 2.6960201263427734, "Telescope Data downlink 10-50Mbit/s"]
+[-5.445821762084961, 2.790558338165283, "Telescope Power consumption 20 W average 50 W peak including downlink"]
+[0.840046226978302, -1.6068812608718872, "Satellite Array Arm Length About a million miles"]
+[1.284891963005066, -1.740435004234314, "Satellite Array Gravitational Wave Sources Ultra-compact binaries, supermassive black hole mergers, extreme mass ratio inspirals"]
+[1.2364808320999146, -1.8527965545654297, "Satellite Array Gravitational Wave Spectrum Broad range of astrophysical sources"]
+[6.376214504241943, 7.364048957824707, "Satellite Component Manufacturer Airbus (UK)"]
+[6.2441253662109375, 7.493971824645996, "Satellite Component Manufacturer Airbus (Germany)"]
+[6.3532867431640625, 7.3826422691345215, "Satellite Component Manufacturer Surrey Space Centre (UK)"]
+[-3.1951122283935547, 4.608415126800537, "Cargo Spacecraft Arrival Date April 4, 2018"]
+[-3.093459129333496, 4.628853797912598, "Cargo Spacecraft Cargo Weight More than 2630 kg"]
+[2.818462610244751, -2.519437551498413, "Satellite Downlink Frequency 2222.5 MHz"]
+[2.6318163871765137, -2.672353982925415, "Satellite RDS Data Rate 88.75 kbit/s unencoded, 177.5 kbit/s encoded"]
+[2.796795129776001, -2.498791456222534, "Satellite UHF RDS Transmission Frequencies 400.328 MHz, 400.822 MHz"]
+[0.7228777408599854, -4.13826322555542, "Satellite Launch Mass 1154 kg"]
+[0.706653356552124, -4.129821300506592, "Satellite Launch Mass 1230 kg"]
+[2.5009231567382812, 22.66569709777832, "Instrument Polarization States 4"]
+[0.7775641679763794, 12.297630310058594, "Ortho-Mode Transducer Function Separate horizontal and vertical polarization components"]
+[-1.0742733478546143, 7.758308410644531, "Device Function Synthesize \u00b145\u00ba polarized channels"]
+[2.1915335655212402, 22.30231285095215, "Instrument Measurement Stoke's parameters at Ka-band"]
+[2.2209577560424805, 22.172874450683594, "Instrument Measurement Water vapor content of the atmosphere"]
+[-4.317301273345947, 7.373725414276123, "Web Server Supported Services Catalog query, receiving acquisition coverage"]
+[1.294021725654602, -1.5367940664291382, "Satellite Geolocation Accuracy < 10 m"]
+[1.465172529220581, -1.8240320682525635, "Satellite Swath Positions 31"]
+[0.6942135691642761, -2.2911505699157715, "Satellite Incidence 20\u00ba - 49\u00ba"]
+[1.9982463121414185, -1.686161994934082, "Satellite Observation Modes Five new observation modes"]
+[0.9320263266563416, 0.88702791929245, "Earth Observation Programme New Name Copernicus"]
+[0.9368060827255249, 0.881435215473175, "Earth Observation Programme Announcement Date December 11, 2012"]
+[0.9069362282752991, 0.9096322655677795, "Earth Observation Programme Vice-President Antonio Tajani"]
+[0.9243600368499756, 0.9008159041404724, "Earth Observation Programme Catalyst Nicolaus Copernicus"]
+[11.27592945098877, 5.491381645202637, "CubeSat Payload L-band reconfigurable software-defined radio"]
+[11.289838790893555, 5.4959001541137695, "CubeSat Third-party Payload Miniaturized high data rate X-band transmitter"]
+[11.276329040527344, 5.513351917266846, "CubeSat Deployment ISS (International Space Station)"]
+[1.5078239440917969, -1.6640347242355347, "Satellite Monitoring Region 24-by-96-degree"]
+[4.39617919921875, -2.6956300735473633, "Satellite Monitoring Duration 27 days"]
+[-4.567948818206787, -3.0826101303100586, "Exoplanet Size Around 80% Earth\u2019s size"]
+[-4.567818641662598, -3.079835891723633, "Exoplanet Size Around 1.4 times Earth\u2019s size"]
+[-4.571273326873779, -3.0865297317504883, "Exoplanet Size Around 1.6 times Earth\u2019s size"]
+[2.5347952842712402, 22.683048248291016, "Instrument Channel Nr. 1, 2, 3, 4, 5, 6, 7"]
+[2.1925086975097656, 23.08365821838379, "Instrument Center Frequency (GHz) 19.35, 19.35, 22.235, 37.0, 37.0, 85.0, 85.0"]
+[1.9843446016311646, 22.604602813720703, "Instrument Center Wavelength 1.55 cm, 1.55 cm, 1.35 cm, 0.81 cm, 0.81 cm, 0.35 cm, 0.35 cm"]
+[1.80270254611969, 22.114234924316406, "Instrument Footprint (km) 68.9 x 44.3, 69.7 x 43.7, 59.7 x 39.6, 35.4 x 29.2, 37.2 x 28.7, 15.7 x 13.9, 15.7 x 13.9"]
+[2.5962119102478027, 22.477699279785156, "Instrument Polarization Vertical, Horizontal"]
+[2.094813585281372, 22.530813217163086, "Instrument NEDT (K) 0.45, 0.42, 0.73, 0.37, 0.38, 0.69, 0.73"]
+[-0.8241146802902222, 8.877912521362305, "Temperature Control System Zones 2"]
+[-0.8123135566711426, 8.89520263671875, "Temperature Control System Frequency 20 Hz"]
+[-1.9905601739883423, 8.9110689163208, "Motor Control Module Motors Filter Wheel Assembly stepper motor, Front Door Assembly main motor, SHM (Shutter Mechanism)"]
+[2.1878867149353027, 22.592540740966797, "Instrument Spectral Range Advanced Visible and Near-Infrared (AVNIR)"]
+[-1.8833361864089966, 14.861364364624023, "Whiskbroom Radiometer Measurement Ocean colour and sea surface temperature"]
+[-2.9903922080993652, 16.176340103149414, "Scatterometer Measurement Wind speeds over bodies of water"]
+[-0.10219809412956238, 15.534201622009277, "Spectrometer Measurement Earth's ozone layer composition"]
+[2.236283302307129, 22.196962356567383, "Instrument Measurement Earth\u2019s Reflectance"]
+[-0.08679092675447464, 15.524595260620117, "Spectrometer Measurement Upper atmosphere\u2019s gaseous composition"]
+[0.14475366473197937, 7.185205459594727, "Experiment Function Reflecting a transmitted laser beam back down to a designated ground station"]
+[-0.6935462355613708, 12.381908416748047, "Monitor Function Map greenhouse gas ratios on a global scale"]
+[-3.2210090160369873, 1.7157649993896484, "Satellite Mission In-Orbit Commissioning Completion Date 23 August 2018"]
+[-3.1454532146453857, 1.7046403884887695, "Satellite Mission Space Debris Capture Successful"]
+[-3.190920352935791, 4.240304470062256, "Spacecraft Mode Activation Time 30 minutes"]
+[-3.1125786304473877, 4.217389106750488, "Spacecraft Mode Activation Immediate pass-through from Initial Mode"]
+[-3.084652900695801, 4.180025100708008, "Spacecraft Mode Action Flight computer powers off"]
+[-3.116081714630127, 4.217410087585449, "Spacecraft Mode Action All subsystems besides the EPS power off"]
+[-0.8698086738586426, 11.472697257995605, "Gamma-ray Detector Purpose Detection of GRB events at apogee arc above the VAB"]
+[1.4073911905288696, -2.4940736293792725, "Satellite Orbit Type Super-synchronous"]
+[4.587655067443848, -2.643944263458252, "Satellite Expected Duration 18 months"]
+[7.274932861328125, 12.406681060791016, "Satellite Instrument Thermosphere Temperature Increase Over 160 \u00b0F (90 \u00b0C)"]
+[7.19614315032959, 12.505666732788086, "Satellite Instrument Heat Dependence on Time of Day Stronger effect in the morning hours compared to that in the afternoon"]
+[7.246029376983643, 12.376681327819824, "Satellite Instrument Impact of Minor Geomagnetic Activity Can have an impact"]
+[-4.9399566650390625, 2.827385902404785, "Astro-mapper Unknown Unknown"]
+[-4.918537616729736, 2.815443277359009, "Astro-mapper Unknown Unknown"]
+[2.038618564605713, -2.7500722408294678, "Satellite Number of Exoplanet Candidates Over 5,000"]
+[5.215770721435547, -3.8410139083862305, "Satellite Mission Start Year 2018"]
+[1.8224133253097534, -1.9013539552688599, "Satellite Extended Mission Observation Area Northern Hemisphere and ecliptic plane"]
+[5.044239521026611, -4.179561614990234, "Satellite Third Year of Mission July 2020 to June 2021"]
+[-2.7702527046203613, 7.89951753616333, "Processor Data Processing GMTI processing"]
+[-2.7813303470611572, 7.893287658691406, "Processor Data Processing Toggle mode data processing and waveform diversity processing"]
+[-2.7574989795684814, 7.92763090133667, "Processor Antenna Three-antenna"]
+[2.6191418170928955, -1.541095495223999, "Satellite Data Distribution Commercial basis"]
+[-1.7187750339508057, 6.6233649253845215, "Program Data Access Research and testing purposes"]
+[-5.288071632385254, 7.837178707122803, "Communication System Sequence Not provided"]
+[-2.8294055461883545, 8.035383224487305, "Clock Output Signals 10 MHz frequency and 1 pulse per second (1 PPS)"]
+[1.5994915962219238, -1.4443082809448242, "Satellite Service Horizontal Accuracy 4 m"]
+[1.3576444387435913, -1.437341570854187, "Satellite Service Vertical Accuracy 8 m"]
+[2.328932285308838, -1.923151969909668, "Satellite Service Availability > 99.5%"]
+[-0.8705713152885437, 5.034543037414551, "Stations Manufacturer Indra Espacio"]
+[1.3297772407531738, -1.3283929824829102, "Satellite Measurement Precision Few inches"]
+[2.3424572944641113, -1.5778186321258545, "Satellite Device Type Laser altimeter system"]
+[1.5051270723342896, -1.2349863052368164, "Satellite Parameter Measured Elevation changes"]
+[1.3348296880722046, -1.3316893577575684, "Satellite Measurement Precision Few inches"]
+[1.3656200170516968, -1.3045191764831543, "Satellite Measurement Precision Few inches"]
+[2.395390033721924, 22.110353469848633, "Weather Instrument Image Capture Time As often as every 30 seconds"]
+[2.3571603298187256, 22.145280838012695, "Weather Instrument Image Scanning Time 5 minutes"]
+[2.377788782119751, 22.080183029174805, "Weather Instrument Number of Built Units 7"]
+[6.332942962646484, 7.410573482513428, "Satellite Component Data Processing Process 60 times more data than today\u2019s GOES satellites"]
+[1.1014378070831299, -1.7973010540008545, "Satellite Attitude Sensor Provider CREST (Canada)"]
+[1.351911187171936, -1.6426124572753906, "Satellite Attitude Sensor Objective To demonstrate the capabilities of a new type of infrared Earth sensor over a range of altitudes from LEO to GEO in a harsh radiation environment on a slow-spinning satellite"]
+[-0.2901751697063446, 7.344933986663818, "Sparc Microprocessor Experiment-2 RAM 4 MByte"]
+[-0.14800399541854858, 7.262666702270508, "Sparc Microprocessor Experiment-2 EEPROM 2 MByte"]
+[1.6899800300598145, -1.9294615983963013, "Satellite Polarization Modes Fully polarimetric quad-polarization (quad-pol)"]
+[-1.5919511318206787, 4.101518154144287, "Ground Segment Purpose Perform image measurement and payload characterization work"]
+[-1.9216996431350708, 6.909622669219971, "Software Purpose Analysis of data and generation of calibration information"]
+[-1.9035089015960693, 7.348097324371338, "Platform Overall Dimensions 620 x 620 x 780 mm"]
+[-1.8262532949447632, 7.380609035491943, "Platform Total Mass 150 kg"]
+[-1.8724123239517212, 7.298717498779297, "Platform Overall Dimensions 550 x 550 x 760 mm"]
+[-1.9125728607177734, 7.332796573638916, "Platform Mass Approximately 100 kg"]
+[1.7775087356567383, 22.099781036376953, "Instrument Inter-satellite Distance 25 m to 250 m"]
+[-2.9260663986206055, 4.166501045227051, "Spacecraft Movement Range \u00b125 mm along the Z and Y axes"]
+[2.774623155593872, 13.688682556152344, "Optical Device Displacement Observation Twice the actual beam displacement"]
+[2.7644786834716797, 13.692296981811523, "Optical Device Impervious to Tilt of the Spacecraft Up to a certain angle"]
+[-1.6314537525177002, 9.702910423278809, "Satellite Propulsion System Propellant Water"]
+[-1.6460446119308472, 9.727264404296875, "Satellite Propulsion System Customization Available"]
+[-1.6151351928710938, 9.703347206115723, "Satellite Propulsion System Scalability Available"]
+[-1.6068722009658813, 9.713685989379883, "Satellite Propulsion System Integration Easy"]
+[-1.646689772605896, 9.720769882202148, "Satellite Propulsion System Affordability Available"]
+[6.295364856719971, 7.435940265655518, "Satellite Component Mass 800 - 900 kg"]
+[3.7336361408233643, 17.717777252197266, "Payload Mass 250 - 300 kg"]
+[3.7336573600769043, 17.701658248901367, "Payload Mass 200 - 250 kg"]
+[3.766524076461792, 17.733057022094727, "Payload Mass Approximately 100 kg"]
+[-4.3831586837768555, 7.372570037841797, "Data Transmission System Instantaneous Data Rate 27 Mbps"]
+[-4.3841938972473145, 7.3643798828125, "Data Transmission System Daily Data Volume 291.6GB"]
+[-4.361839294433594, 7.366772174835205, "Data Transmission System Downlink Data Rate 750 Mbps"]
+[-4.326836109161377, 7.235004425048828, "Data Downlink System Daily Downlink Time About 102 minutes"]
+[-4.323450565338135, 7.214860439300537, "Data Downlink System Daily Downlink Time About 93 minutes"]
+[2.7331652641296387, 22.194915771484375, "Instrument Pointing Nadir-pointing"]
+[2.2892205715179443, 22.20745086669922, "Instrument Measurement UV radiation from the Earth's atmosphere and ionosphere"]
+[2.30493426322937, 22.20684051513672, "Instrument Measurement Visible radiation (airglow and terrestrial albedo)"]
+[2.9702816009521484, 22.380779266357422, "Instrument Components SIS (Scanning Imaging Spectrometer), NPS (Nadir-looking Photometer System), Support module"]
+[2.524449348449707, -1.1692668199539185, "Satellite Observation Applications Emergency response, land monitoring, disaster management"]
+[2.1764395236968994, -1.2279354333877563, "Satellite Imaging Capabilities Urban land use and land-cover maps, forest areas monitoring, agricultural areas discrimination and classification, vegetation cover maps and crop identification, fire risk areas mapping, flood monitoring, land-cover change and snow cover maps"]
+[0.487539678812027, 12.261761665344238, "Sensor Pixel Size 600 \u00b5m"]
+[0.48828819394111633, 12.244500160217285, "Sensor Plate Scale 12.300/pixel"]
+[0.5075364112854004, 12.145858764648438, "Sensor Total Subtended FOV 13 arcmin on a side"]
+[0.39580267667770386, 12.303925514221191, "Sensor Pixel Format 32 x 32"]
+[0.6057167649269104, 12.201894760131836, "Sensor Threshold 2.5 keV"]
+[0.5560359358787537, 12.172547340393066, "Sensor Maximum Processing Rate 400 events/s"]
+[0.5577558279037476, 12.171774864196777, "Sensor Maximum Flux Measurement Rate 10 4  s -1"]
+[0.49335941672325134, 12.2162504196167, "Sensor Time Resolution 2 \u00b5s"]
+[0.7033478617668152, 12.115007400512695, "Sensor Dead Time Fraction 2%"]
+[3.5976622104644775, 13.301761627197266, "Laser Wavelength Accuracy Requirement Less than 3 x 10-7"]
+[3.607450008392334, 13.265177726745605, "Laser Thermal Expansion Coefficient Less than \u00b1 5 x 10-8/K"]
+[2.0629453659057617, 22.56640625, "Instrument Wavelength Range 3.3 \u00b5m to 14 \u00b5m"]
+[-0.809913158416748, 11.598991394042969, "Detector Nonlinearity Temperature Higher than 280 K"]
+[-0.39980489015579224, 16.028610229492188, "Imaging Spectrograph Manufacturer JHU/APL"]
+[-0.4168868064880371, 16.060461044311523, "Imaging Spectrograph Observation Scheme Not provided"]
+[4.573594093322754, -2.5818731784820557, "Satellite In-Orbit Performance 2 years"]
+[2.122358798980713, -0.8072177171707153, "Remote Sensing Satellite In-Orbit Results 6 years"]
+[-5.357095718383789, 2.7731471061706543, "Telescope Calibration First light pictures"]
+[2.2776694297790527, -2.0944488048553467, "Satellite Solar Arrays Deployed"]
+[2.9066171646118164, 22.37602996826172, "Instrument Team Caltech, Columbia University, DTU (Danish Technical University), LLNL (Lawrence Livermore National Laboratory),NASA/GSFC (Goddard Space Flight Center), and UCB (University of California, Berkeley)"]
+[-0.7567232847213745, 3.1905734539031982, "Sextuple Star System Inner Quadruple Orbit Period Every four years or so"]
+[-0.7449104189872742, 3.1854729652404785, "Sextuple Star System Outer Binary Orbit Period Roughly every 2,000 years"]
+[2.0509793758392334, -2.789473056793213, "Satellite Number of Stars Observed Around 80 million"]
+[2.0474021434783936, -2.7448041439056396, "Satellite Number of Eclipsing Binaries Candidates 450,000"]
+[-1.4033336639404297, 9.38987922668457, "Geyser Jet of Boiling Water Height High in the air"]
+[2.670048475265503, 14.309566497802734, "Optical Instrument Number of Filter Windows 18"]
+[2.67948317527771, 14.413496017456055, "Optical Instrument Rotation Speed 600 rpm"]
+[2.6515631675720215, 14.339815139770508, "Optical Instrument Rotation Time 100 ms"]
+[2.646042585372925, 14.350406646728516, "Optical Instrument Temperature 213K"]
+[-0.7911590933799744, 8.864225387573242, "Thermal Control System Temperature Stability \u00b11 K"]
+[0.9290186166763306, 0.9058759808540344, "Earth-monitoring Project Leader Nemani"]
+[-1.3812659978866577, 4.374552249908447, "Ground-based Network Measures Forest canopy fluxes of carbon dioxide and other key environmental variables"]
+[7.2927117347717285, 12.427102088928223, "Satellite Instrument Type Advanced instrument"]
+[-0.9562723636627197, -10.004341125488281, "Satellite Constellation Number of Satellites Not announced"]
+[-0.951549232006073, -10.001436233520508, "Satellite Constellation Projected Price Tag $600 million"]
+[1.9079035520553589, 10.726452827453613, "Imaging Device Image Capture Date Dec. 14, 2020"]
+[1.916006326675415, 10.718132972717285, "Imaging Device Image Capture Location Chile and Argentina"]
+[2.6649558544158936, -1.6380444765090942, "Satellite Operation Captured images of the shadow of the Moon crossing the face of Earth"]
+[1.646652102470398, -2.2556843757629395, "Satellite Spin Rate One revolution in 37.5 seconds"]
+[1.1649932861328125, -0.7937193512916565, "Satellite Platform Size 1.7 m diameter x 0.5 m height"]
+[1.0910965204238892, -1.0502498149871826, "Satellite Deployed Length 7.9 m"]
+[2.0892040729522705, -0.5743775963783264, "Satellite Power 202 W (EOL)"]
+[1.9067789316177368, -1.327775478363037, "Satellite Battery Capacity 448 Whr at 100% SOC and 313 Whr at 70% SOC"]
+[3.224351406097412, 2.378169059753418, "Satellite Subsystem Processor RAD 6000"]
+[3.2212412357330322, 2.3736894130706787, "Satellite Subsystem Propellant Monopropellant hydrazine (78 kg)"]
+[0.9687320590019226, -4.403238773345947, "Satellite Mass 494 kg"]
+[0.7232055068016052, -4.151055335998535, "Satellite Launch Mass 636 kg"]
+[-4.565432548522949, -3.088472843170166, "Exoplanets Formation Hypotheses Disk interaction, Gravity of other planets"]
+[-4.569186210632324, -3.0917751789093018, "Exoplanet Proximity to Star Close"]
+[-3.848787307739258, 7.930459499359131, "Data Storage Storage Capacity 1 Gbit"]
+[-5.289578437805176, 7.971999168395996, "Communication System Uplink Frequency S-band"]
+[-5.21730375289917, 7.7805938720703125, "Communication System Uplink Data Rate 15 kbit/s"]
+[-5.223237037658691, 7.804667949676514, "Communication System Downlink Data Rate 120 bit/s"]
+[-3.8171186447143555, 6.94124174118042, "Data Collection System Data Rate <1 kbit/s"]
+[-5.162790298461914, 7.991846561431885, "Communication System Transponders 2"]
+[-5.230551242828369, 7.876031875610352, "Communication System LGA (Low Gain patch Antennas) 4"]
+[-5.233728885650635, 7.902091979980469, "Communication System MGA (Medium Gain Antenna) 1"]
+[-1.3631566762924194, 3.2055439949035645, "Astrophysical Phenomenon Brightness Hundreds of times brighter than the Eddington luminosity"]
+[-1.2974306344985962, 3.1964643001556396, "Astrophysical Material Shock Front Formation Yes"]
+[-3.607924699783325, 12.72495174407959, "Particles Direction Out the sides of the column"]
+[5.254908084869385, -4.0287275314331055, "Satellite Launch Date 2018"]
+[2.323038101196289, -1.460808515548706, "Satellite Instrument Earth-observing laser instrument"]
+[2.6390552520751953, -1.4518769979476929, "Satellite Data Center NASA National Snow and Ice Data Center Distributed Active Archive Center (NSIDC DAAC)"]
+[2.850790023803711, -1.0307375192642212, "Satellite Purpose Investigate why and how much of the frozen parts of our world are changing as a result of climate change"]
+[-0.9031808972358704, 13.02015209197998, "Spectral Irradiance Monitor Operation Start Date March 2018"]
+[-0.8682953119277954, 12.936288833618164, "Spectral Irradiance Monitor Monitoring Frequency Every 12 h"]
+[-0.8973227739334106, 13.01396369934082, "Spectral Irradiance Monitor Accuracy uc < 0.25%"]
+[-0.9196850657463074, 13.04680347442627, "Spectral Irradiance Monitor Wavelength Range 200\u20132400 nm"]
+[-3.252610683441162, 7.450679302215576, "Data Handling Unit Components IPC (Image Processing Computer), Proton 400 k single board computer, 192 GB SSB (Solid-State Buffer) cards, analog I/O power switch board, power supply board"]
+[-2.779982566833496, 7.467527866363525, "Field Programmable Gate Arrays Quantity 2"]
+[-3.8518495559692383, 7.948721885681152, "Data Storage Capacity 192 GB"]
+[-1.939743995666504, 7.323150634765625, "Computer Function Responsible for commanding, communicating with the spacecraft master avionics unit, and interfacing with the Ka-band transmitter"]
+[-2.402209997177124, 9.115060806274414, "Power Switch Board Function Control instrument power"]
+[2.276515483856201, 22.13630485534668, "Instrument Measurement Principle Sending pulses of light from the satellite to Earth\u2019s surface and measuring how long it takes individual photons to return to the sensor"]
+[-0.3938436508178711, 5.128257751464844, "Reservoir Water Level Change Dropped 5.53 feet (1.69 meters) between March and June"]
+[-0.40596428513526917, 5.112657070159912, "Reservoir Highest Water Level June 2019"]
+[5.0311102867126465, -4.321857452392578, "Satellite Publication Date 9 December 2020"]
+[-1.3138387203216553, 6.103153228759766, "Company Article Date 27 October 2020"]
+[5.058361053466797, -3.601945638656616, "Satellite Operation Period 2002 to 2017"]
+[5.2614426612854, -3.7670199871063232, "Satellite Launch Year 2018"]
+[1.416659951210022, -3.1137442588806152, "Satellites Data Collection Period 17 years"]
+[1.4035217761993408, -3.1182072162628174, "Satellites Purpose Track changes in ice sheets, water stored on land, and variations in ocean mass"]
+[1.390383005142212, -3.1143276691436768, "Satellites Method Tease out the gravitational signal associated with the movement of water by evapotranspiration"]
+[1.7105231285095215, -2.2798945903778076, "Satellite Maneuver Design Strategy Non-drifting injection"]
+[2.8097808361053467, -2.589646577835083, "Satellite Maneuver Safety Period At least 5 days"]
+[2.049999952316284, -1.9876478910446167, "Satellite Thermal Constraint Compliance required"]
+[1.3897234201431274, -2.1404144763946533, "Satellite Attitude Profile Sun-pointing"]
+[5.834619045257568, 14.375449180603027, "Transponder Function Detects beacon signals"]
+[2.6620142459869385, 5.3875813484191895, "Beacon Function Sends location data through GOES to the SAR network"]
+[2.9748141765594482, -1.6402722597122192, "Satellite Support and Maintenance Provider NASA's SAR team"]
+[-0.4143095910549164, 14.511332511901855, "Imaging Instrument Capabilities Significantly Increased"]
+[5.457276344299316, -4.361140251159668, "Satellite Launch Date 28 March 2018"]
+[5.171962261199951, -4.515964984893799, "Satellite Arrival Date Feb. 15, 2018"]
+[1.51908278465271, -2.343559503555298, "Satellite Orbit Type Highly elliptical"]
+[1.9690067768096924, -2.1047606468200684, "Satellite Solar Panels On its Sun-facing side"]
+[2.3294529914855957, -1.479994535446167, "Satellite Camera A set of cameras"]
+[2.3215725421905518, -1.5633023977279663, "Satellite Camera Looking out for pulsing LEDs on the Coronagraph"]
+[-13.93794059753418, -2.2802393436431885, "X-ray Telescope Image Color Magenta"]
+[-13.874659538269043, -2.2387351989746094, "X-ray Telescope Image Location Center of our Milky Way galaxy"]
+[-13.89808177947998, -2.2552573680877686, "X-ray Telescope Image Credit NASA/JPL, Caltech"]
+[-0.49864816665649414, 5.844067573547363, "Unknown Unknown Unknown"]
+[-0.9888805747032166, 7.682608127593994, "Device Size 370 mm x 350 mm x 130 mm (width x depth x height)"]
+[-1.0163451433181763, 7.761089324951172, "Device Mass 5.5 kg"]
+[-1.0336108207702637, 7.732309341430664, "Device Size 235 mm x 205 mm x 85 mm (width x depth x height)"]
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+[-1.0379481315612793, 7.759215831756592, "Device Cooling Power 2.27 W at 53.0 K"]
+[-0.9836612939834595, 7.795137882232666, "Device Cooling Power 5.14 W at 183.1 K"]
+[3.7276837825775146, 17.70938491821289, "Payload Digital Technology Elements Advanced"]
+[-1.829437255859375, 8.732321739196777, "Controller Architecture Unknown"]
+[3.118150234222412, -1.608699083328247, "Satellite Mission Lead Caltech"]
+[3.0456225872039795, -1.5619293451309204, "Satellite Mission Manager JPL for NASA's Science Mission Directorate"]
+[3.0508387088775635, -1.7061960697174072, "Satellite Development Partners Danish Technical University and the Italian Space Agency (ASI)"]
+[3.0720133781433105, -1.7449883222579956, "Satellite Builder Orbital Sciences Corp."]
+[3.06350040435791, -1.6457514762878418, "Satellite Mission Operations Center University of California Berkeley"]
+[2.5471174716949463, -1.3483326435089111, "Satellite Data Archive NASA's High Energy Astrophysics Science Archive Research Center"]
+[-0.16276408731937408, 11.718481063842773, "Indicator Function Indicate the power status of the main power line and of single battery low-voltage"]
+[0.3444176912307739, 11.767351150512695, "Safety Feature Voltage Threshold Below the security margin set by the ISS safety policy"]
+[-1.2613954544067383, 8.585884094238281, "Component Speed Not specified"]
+[-1.286728024482727, 8.592020034790039, "Component Full Swap Angle Not specified"]
+[-1.1983739137649536, 8.6001615524292, "Component Function Provides containment for inadvertent flame and shatters"]
+[2.7082371711730957, 14.316981315612793, "Optical Instrument Quantity 26"]
+[0.5090122222900391, 10.923965454101562, "Image Sensor Quantity 104"]
+[0.5054850578308105, 10.916730880737305, "Image Sensor Pixel Count 4510 x 4510"]
+[5.086348056793213, -3.9349489212036133, "Satellite Launch Date 2026"]
+[4.681784152984619, -2.613506317138672, "Satellite Mission Duration 4 \u00bd years"]
+[4.712657928466797, -2.4396300315856934, "Satellite Potential Mission Extension 4 years"]
+[-1.3508480787277222, 6.117574691772461, "Company CCD Delivery Mid March"]
+[-1.337923526763916, 6.124522686004639, "Company Remaining CCD Delivery Before the end of 2020"]
+[2.7538020610809326, 22.487180709838867, "Instrument Onboard Storage Lost in August 2008"]
+[0.5616433620452881, 12.067456245422363, "Sensor Affected by Solar intrusions into the warm load, and thermal emission from the reflector"]
+[-3.5519487857818604, 4.389891624450684, "Spacecraft On-orbit Checkout Completion Date Jan. 29, 2007"]
+[-3.5153417587280273, 4.418330669403076, "Spacecraft On-orbit Checkout Completion Date Nov. 20, 2003"]
+[-13.864457130432129, -2.2681193351745605, "X-Ray Telescope URL https://www.jpl.nasa.gov/news/news.php?release=2017-088"]
+[-13.865846633911133, -2.246788263320923, "X-Ray Telescope URL https://www.nasa.gov/feature/jpl/andromedas-bright-x-ray-mystery-solved-by-nustar"]
+[-3.1696927547454834, 4.295374393463135, "Spacecraft Purpose Launch astronauts into space, perform multiple long distance/long duration space missions, and then return the astronauts safely back to Earth"]
+[-3.0530176162719727, 4.272145748138428, "Spacecraft Designation MPCV (Multi-Purpose Crew Vehicle)"]
+[1.0000157356262207, -4.389924049377441, "Satellite Mass 383 kg"]
+[1.1699588298797607, -0.7966459393501282, "Satellite Size 2.5 m x 5.2 m x 0.9 m"]
+[4.865319728851318, -2.452319860458374, "Satellite Mission Life ~2 years or longer"]
+[-1.6042799949645996, 9.672391891479492, "Propulsion System Thrust 10-28 mN"]
+[-1.6164216995239258, 9.672600746154785, "Propulsion System Isp ~2000 s"]
+[-1.6310611963272095, 9.69482707977295, "Propulsion System Electric Power 370 W @ 10 mN"]
+[-1.5134543180465698, 9.562198638916016, "Propulsion System Fuel Mass 10 kg (Xenon)"]
+[-1.613312840461731, 9.678475379943848, "Propulsion System Thrust 1 N x 4 engines"]
+[-1.613466739654541, 9.68127155303955, "Propulsion System Isp ~ 200 s"]
+[-1.5997573137283325, 9.709946632385254, "Propulsion System Fuel Mass 34 kg (N 2 H 4 )"]
+[5.347343444824219, -4.42708683013916, "Satellite Launch Date December 18, 2017"]
+[2.5863237380981445, -2.1622657775878906, "Satellite Launch Location Kennedy Space Center in Florida"]
+[2.6601436138153076, -2.3798630237579346, "Satellite Launch Vehicle Dragon capsule on board the SpaceX CRS-14 resupply mission"]
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+[2.2667596340179443, -2.124140977859497, "Satellite Configuration 20 satellites"]
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+[4.094085216522217, -2.4802706241607666, "Satellite Image Revisit Time One to four-day"]
+[1.4895652532577515, -1.095476746559143, "Satellite Image Resolution 2.5-meter"]
+[-2.496351480484009, 11.142897605895996, "Image Data Processor Integration Time 22.5 s"]
+[-2.4722321033477783, 11.157084465026855, "Image Data Processor Readout Time ~2.5 s"]
+[-2.4903998374938965, 11.174298286437988, "Image Data Processor Readout Interval 6.25 s"]
+[2.115072727203369, -0.6826807260513306, "Satellite Power Source Ancillary Electronics Units (AEUs)"]
+[2.773707866668701, -1.6480580568313599, "Satellite ICUs Two ICUs used in cold redundancy"]
+[-5.414554595947266, 2.836855888366699, "Imaging Telescope Aperture 24 cm diameter"]
+[-5.364291667938232, 2.795788288116455, "Imaging Telescope Payload Mass < 10 kg"]
+[-5.393982410430908, 2.886265516281128, "Imaging Telescope Resolution 0.9-1.1 m"]
+[-5.412671089172363, 2.8182616233825684, "Imaging Telescope Sensor Capabilities Staring, Motion, Imagery/ Video, Low Light"]
+[-5.350520610809326, 3.035614013671875, "Imaging Telescope Bands Visible Pan / Color"]
+[-1.5095815658569336, 13.439457893371582, "Solar Array Length 60-foot-long"]
+[-1.508620262145996, 13.441205978393555, "Solar Array Quantity 2"]
+[-3.155876398086548, 4.290154933929443, "Astronaut Total Spacewalking Time 52 hours and 43 minutes"]
+[-3.1946449279785156, 4.335757255554199, "Astronaut Total Spacewalking Time 26 hours and 15 minutes"]
+[2.655092716217041, 22.267900466918945, "Instrument Magnetic Field Intense and quite uniform field perpendicular to the vertical axis"]
+[2.076678514480591, 22.53221321105957, "Instrument Dipole Moment Negligible"]
+[2.674859046936035, 22.14000701904297, "Instrument Safety Regulations Compliance Fringe magnetic fields on the ISS"]
+[2.7637124061584473, 22.223466873168945, "Instrument Test Location CERN"]
+[2.7047741413116455, 22.24444007873535, "Instrument Test Location ESA/ESTEC in Noordwijk, The Netherlands"]
+[2.7201576232910156, 22.25416374206543, "Instrument Test Location KSC (Kennedy Space Center) in Florida"]
+[6.33424186706543, 7.410423278808594, "Satellite Component Field of View 8 km x 8 km"]
+[-1.688730001449585, 8.835746765136719, "Control System Parallelism Maintenance Within 1.9 x 10-4 degrees"]
+[-1.7172385454177856, 8.840137481689453, "Control System Return Time 3 seconds"]
+[-1.7229994535446167, 8.851311683654785, "Control System Alignment Bias Offset angle of the moving mirror"]
+[-1.5005508661270142, 16.897361755371094, "Altimeter Mean Sea Surface Topography Data"]
+[-1.5014108419418335, 16.895875930786133, "Altimeter Map of Surface Gravity and Earthquakes Data"]
+[-1.5058397054672241, 16.90833282470703, "Altimeter Marine Geoid Data"]
+[2.1396329402923584, 22.295503616333008, "Instrument Pointing Accuracy 2 / 20 arcsec (x, y / z)"]
+[2.2309560775756836, 23.094940185546875, "Instrument Attitude Data Update Frequency 0.3 Hz"]
+[1.5194939374923706, 21.232446670532227, "Instrument Mass 4 kg"]
+[1.6216797828674316, 23.223329544067383, "Instrument Power Consumption 11.2 W"]
+[1.577602744102478, 22.201396942138672, "Instrument Size 37 cm x 23 cm x 23 cm"]
+[-2.6745667457580566, 9.540745735168457, "Power Source Power 2 kW (BOL)"]
+[-2.6042752265930176, 9.658463478088379, "Power Source Area 23 m2"]
+[-2.607860565185547, 9.631614685058594, "Power Source Span 14 m"]
+[-2.983170747756958, 4.455633163452148, "Spacecraft Launch Mass 2778 kg"]
+[-3.325965166091919, 4.24324369430542, "Spacecraft Design Life 5 years"]
+[-2.8241968154907227, 4.697473049163818, "Spacecraft Payload Mass ~1200 kg"]
+[-9.955211639404297, 5.854879856109619, "Search And Rescue Processor Installation On all early spacecraft in the COSPAS as well as in the SARSAT series"]
+[-9.951866149902344, 5.855062484741211, "Search And Rescue Processor Support Both long and short messages"]
+[-9.956072807312012, 5.852057933807373, "Search And Rescue Processor Introduction On the MetOp-A spacecraft of EUMETSAT (launch October 19, 2006)"]
+[0.49257925152778625, 9.379518508911133, "Attitude Control Technology Features Star tracker, sun sensor, inertial measurement unit (IMU), magnetometer, reaction wheels, torque rods, and processor"]
+[0.5001593232154846, 9.375605583190918, "Attitude Control Technology Flight Software Capabilities Autonomously detumbling the spacecraft, searching for the sun, maintaining a sun-pointed coarse attitude, slew to an inertial attitude, maintain 3-axis pointing with relatively high precision over long durations"]
+[-2.268280506134033, 7.210151195526123, "Flight Computer Processor Virtex 4FX FPGA with an embedded PowerPC processor running Linux"]
+[1.7789433002471924, 8.444803237915039, "Command & Data Handling Subsystem Processor Sharp LH79520 ARM microprocessor"]
+[1.7717502117156982, 8.434199333190918, "Command & Data Handling Subsystem FPGA Xilinx XCV100"]
+[1.1365526914596558, -0.8013624548912048, "Satellite Size 50 cm in diameter and 93 cm in height"]
+[0.9723562598228455, -4.346686840057373, "Satellite Mass 86 kg"]
+[4.778289794921875, -2.4390389919281006, "Satellite Mission Life Two years (min)"]
+[2.109010934829712, -2.7458696365356445, "Satellite Number of Satellites 7"]
+[2.4564149379730225, -2.014536142349243, "Satellite Designations FengYun-4A through -4G"]
+[6.755715370178223, 6.942015647888184, "Satellite Component Unknown Unknown"]
+[6.752204895019531, 6.946098327636719, "Satellite Component Unknown Unknown"]
+[0.7550018429756165, -1.202110767364502, "Satellite Altitude ~200 km"]
+[1.594690203666687, -2.194288730621338, "Satellite Orbit Type Super Low Altitude"]
+[1.7151875495910645, -1.934187412261963, "Satellite Altitude Control System Ion engine system"]
+[-1.4677765369415283, 9.534010887145996, "Thruster Travel Time to Destination About three months"]
+[14.241479873657227, 7.810891151428223, "Nanosatellite Launch Date 2021"]
+[14.598268508911133, 7.591349124908447, "Nanosatellite Mission Prospect, locate, and estimate size and composition of water ice deposits on the Moon"]
+[3.6218583583831787, 13.266271591186523, "Laser Beam Accuracy \u2264 130 \u00b5m"]
+[3.6443355083465576, 13.2208833694458, "Laser Mass ~ 1.5 kg"]
+[3.6142115592956543, 13.251751899719238, "Laser Sun Exclusion Angle < 15\u00ba"]
+[-0.5864859223365784, 11.760360717773438, "Optical Detector Centroiding Error ~ 50 \u00b5m"]
+[-0.7197906374931335, 11.744330406188965, "Optical Detector Translation ~ 25 \u00b5m"]
+[-0.6059600710868835, 11.756525039672852, "Optical Detector Positioning Stability ~ 80 \u00b5m"]
+[3.6324124336242676, 13.24541187286377, "Laser Update Rate 100 Hz"]
+[3.6429011821746826, 13.23684310913086, "Laser Operating Range ~ 6 mm"]
+[-3.092750072479248, 2.427828550338745, "Mission Purpose Demonstrate Orion structural integrity, thermal protection systems, jettison separation of the launch abort system tower, on orbit energy and guidance capability, re-entry crew module control, separation from the service module, parachute and landing separation events"]
+[-2.116591691970825, 7.681392192840576, "Avionics Software Load About 50% of the entire software load that is required for crewed flight on EM-2"]
+[-0.7053608298301697, 8.921335220336914, "Heat Shield Purpose Protect the crew for re-entry velocities that are higher than any human spacecraft in history"]
+[-2.0809202194213867, 7.668241500854492, "Circuit Board Purpose Collects information on the frequency of single event effects and how to mitigate them, especially in specialized computer chips"]
+[-0.4863041639328003, 13.82486343383789, "Dosimetry Intercomparison and Miniaturization Experiment Number of Boards 2"]
+[-0.5721392631530762, 13.909599304199219, "Dosimetry Intercomparison and Miniaturization Experiment Ways to Measure Space Radiation 6"]
+[-0.6886693835258484, 12.532341003417969, "Enhanced Low Dose Rate Sensitivity Purpose Study the ELDRS effect"]
+[-0.712673544883728, 12.550655364990234, "Enhanced Low Dose Rate Sensitivity Number of Boards 1"]
+[-0.8852730393409729, 5.039562225341797, "Station Location INRiM, Turin Italy"]
+[-0.8678968548774719, 5.041646480560303, "Station Location Kiruna Sweden"]
+[-0.8731401562690735, 5.025195121765137, "Station Location Kourou French Guyana"]
+[-0.8601731657981873, 5.0514116287231445, "Station Location La Plata Argentina"]
+[-0.8475494384765625, 5.041118621826172, "Station Location Malindi Kenya"]
+[-0.8800551891326904, 5.056151866912842, "Station Location Mizusawa Japan"]
+[-0.8688583970069885, 5.042088985443115, "Station Location New Norcia Australia"]
+[-0.8785293102264404, 5.055079460144043, "Station Location ESA/ESTEC, Noordwijk The Netherlands"]
+[-0.8713912963867188, 5.029361248016357, "Station Location Dunedin New Zealand"]
+[-0.8815933465957642, 5.024544715881348, "Station Location Tahiti French Polynesia"]
+[-0.9076402187347412, 5.023895740509033, "Station Location USNO, Washington USA"]
+[-0.8908752202987671, 5.036320686340332, "Station Location Vesleskarvet Antarctica"]
+[-0.844626784324646, 5.026023864746094, "Station Location Wuhan China"]
+[2.3842597007751465, -1.6296967267990112, "Satellite Product Line High Resolution Small and Micro Satellites"]
+[4.988450050354004, -3.7485053539276123, "Satellite Program Overview 1 year from launch"]
+[0.45196202397346497, 4.5062971115112305, "Natural Phenomenon Maximum Extent 14.42 million km2 (5.57 million square miles)"]
+[0.4631860852241516, 4.5391387939453125, "Natural Phenomenon Minimum Extent Unknown"]
+[0.6339693665504456, 4.20685338973999, "Atmospheric Phenomenon Effect Trapped cold air in the Arctic"]
+[-9.954475402832031, 5.854232311248779, "Search and Rescue System Frequency 406 MHz"]
+[-1.15250825881958, 4.484005451202393, "Ground Facilities Function Process the satellite signal"]
+[1.6120810508728027, 2.2631094455718994, "Geostationary Satellites Quantity 2"]
+[1.6082332134246826, 2.2681002616882324, "Geostationary Satellite Quantity 1"]
+[1.6089510917663574, 2.2671287059783936, "Geostationary Satellite Quantity 1"]
+[0.6168655157089233, 12.059060096740723, "Sensor Development Date Sept. 29 to Oct. 3, 2008"]
+[0.6473249197006226, 12.021939277648926, "Sensor Publication Date Nov. 2008"]
+[2.1012625694274902, -2.619765281677246, "Satellite Solar Array Paddles Two"]
+[2.0753378868103027, -2.521057367324829, "Satellite Solar Array Paddle One"]
+[2.447068929672241, -1.939614176750183, "Satellite Radar L-band radio waves"]
+[2.1880042552948, -2.0894088745117188, "Satellite Configuration 12-sided cylinder with body-mounted solar cells on all cylinder sides"]
+[0.5992119908332825, 9.340262413024902, "Attitude Control Subsystem Attitude Sensing 3-axis magnetometer and a solar panel current algorithm"]
+[0.09965295344591141, 11.248323440551758, "Gyroscope Accuracy Range \u00b15\u00ba/s"]
+[0.09951724857091904, 11.349027633666992, "Gyroscope Power Consumption < 80 mA at \u00b15 V for each gyro"]
+[-3.0805246829986572, 9.652281761169434, "Battery Capacity 225 Whr"]
+[-3.0846753120422363, 9.635433197021484, "Battery Full Charge Voltage 29.4 V"]
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+[-5.248486042022705, 7.892608165740967, "Communication System Function Broadband for Africa"]
+[1.3716492652893066, 7.055917263031006, "Communication Equipment Manufacturer MDA Corp. of Canada"]
+[3.164454460144043, -1.7712571620941162, "Satellite Prime Contractor Airbus"]
+[3.0511720180511475, -1.7064602375030518, "Satellite Lead Investor Germany"]
+[3.1968748569488525, -1.5359725952148438, "Satellite Mission Lead MIT in Cambridge, Massachusetts"]
+[3.0936970710754395, -1.6268703937530518, "Satellite Mission Manager NASA's Goddard Space Flight Center"]
+[-0.3891560435295105, 3.776846408843994, "Planet Type Hot"]
+[-0.3780064582824707, 3.7651500701904297, "Planet Orbit Very close, nearly polar orbit around a rapidly rotating star"]
+[2.6235737800598145, 14.30031967163086, "Optical Instrument Beam Diameter Not specified"]
+[2.622224807739258, 14.292953491210938, "Optical Instrument Wavefront Planarity Not specified"]
+[2.6395394802093506, 14.305388450622559, "Optical Instrument Steering Range Relative to the S/C"]
+[-0.041994646191596985, 9.32425308227539, "Pointing System Performance \u00b1300 \u00b5rad"]
+[-1.2977094650268555, 6.90604305267334, "Design Used Alternative design"]
+[2.7665343284606934, -1.9256991147994995, "Satellite Operational Yes"]
+[2.7947564125061035, -1.9387961626052856, "Satellite Operational Yes"]
+[-3.0846457481384277, 4.278162956237793, "Spacecraft Operation and Control Brazil, China"]
+[-1.597774624824524, 4.105544090270996, "Ground Segment Function Control the satellites and achieve the objectives of its remote sensing missions"]
+[-1.1395517587661743, 4.4689812660217285, "Ground Stations Data Acquisition Raw data from the CBERS data collection system in the S-band"]
+[-1.8108576536178589, 8.810808181762695, "Control Center Function Receive a variety of satellite information"]
+[2.1167445182800293, 22.374732971191406, "Instrument Accuracy \u00b1 1 m"]
+[1.8334602117538452, 22.164297103881836, "Instrument Resolution Around 100 km"]
+[2.7661149501800537, 22.12484359741211, "Instrument Application Detailed maps of the marine geoid"]
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+[0.6921245455741882, -1.1759449243545532, "Satellite Mean Altitude 798 km"]
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+[4.056766033172607, -2.452045440673828, "Satellite Repeat Cycle 24 days (343 orbits)"]
+[0.7760146856307983, -1.4721448421478271, "Satellite Ground-Track Repeatability \u00b1 5 km (with a goal of \u00b11 km)"]
+[-0.18939423561096191, 12.353026390075684, "Proton Sensor Objective Measure the solar and galactic protons found in the Earth's magnetosphere"]
+[-3.1803860664367676, 7.591707229614258, "Data Processing Unit Function Process data from SEISS"]
+[-4.527628421783447, 12.146547317504883, "Magnetometer Function Measure magnetic fields"]
+[-2.6482388973236084, 11.681693077087402, "Imager Integration Completion Date Jan. 12, 2015"]
+[1.3922306299209595, 2.312676429748535, "Lightning Mapper Development and Testing Completion Date Oct. 9, 2014"]
+[2.112546920776367, -2.7118475437164307, "Satellite System Module Electronics Boxes More than 70"]
+[5.20927095413208, -4.441280364990234, "Satellite Instrument Installation Start Date July 30, 2014"]
+[-1.0623542070388794, 6.717442989349365, "Review Date July 22\u201324, 2014"]
+[-13.693771362304688, -2.297785997390747, "X-ray Telescope Data Capture Date February 19, 2014"]
+[-13.87684440612793, -2.236069679260254, "X-ray Telescope Supernova Remnant Name Cassiopeia A (Cas A)"]
+[4.897231101989746, -2.4642622470855713, "Satellite Build Cycle 24-36 months"]
+[-0.4970155656337738, 5.850322723388672, "Unknown Contract Date with Raytheon January 2018"]
+[-0.4547600746154785, 5.851462364196777, "Unknown Critical Design Review (CDR) Late 2018"]
+[5.135242938995361, -3.980205535888672, "Satellite First Launch Early 2021"]
+[-1.4846813678741455, 13.416284561157227, "Solar Array Efficiency Degraded over time"]
+[-1.4891072511672974, 13.417710304260254, "Solar Array Power Generation 215 kW"]
+[-1.5215998888015747, 13.446633338928223, "Solar Array Length 63 feet"]
+[-1.521574854850769, 13.446734428405762, "Solar Array Width 20 feet"]
+[-1.4914565086364746, 13.421104431152344, "Solar Array Mounting Plugs into the station\u2019s power channels and rotary joints"]
+[-1.7145737409591675, 5.367038726806641, "Mission Operations Control Centre Host University of Auckland\u2019s Te P\u016bnaha \u0100tea-Auckland Space Institute"]
+[-0.5174157619476318, 15.525552749633789, "Airborne Imaging Spectrometer Funding Environmental Defense Fund (EDF) and private philanthropy"]
+[1.3162094354629517, -1.1836111545562744, "Small Satellite Intended Measurement Scales Regional (100s of km) and fine scales (< 1 km)"]
+[2.6513352394104004, 22.59367561340332, "Instrument Team Leader Changxiang Yan"]
+[2.8051323890686035, 22.25384521484375, "Instrument Team Leader Zhongdong Yang"]
+[-0.9160065054893494, 6.762964248657227, "Process Team Leader Liu Yi"]
+[-0.9031169414520264, 6.761444568634033, "Process Team Leader Liu Yi"]
+[-0.8927451968193054, 6.7939043045043945, "Process Team Leader Xiangjun Tian"]
+[-0.909323513507843, 6.75726318359375, "Process Team Leader Chengcai Li"]
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+[3.3220603466033936, 0.2945023477077484, "Satellite Development Programme Number of Satellites Sold 16"]
+[3.3242027759552, 0.20934616029262543, "Satellite Development Programme Return on Investment Predicted to be more than 20 times"]
+[0.6867760419845581, 12.065260887145996, "Pressure Transducer Manufacturer Bradford Engineering"]
+[0.6837713122367859, 12.111950874328613, "Pressure Transducer Sponsor NIVR"]
+[-3.0850143432617188, 9.652233123779297, "Battery Mass Comparison Half the mass of a conventional nickel-cadmium battery"]
+[-0.3471854031085968, 6.60292911529541, "Electronics TestBed Manufacturer AFRL, Kirtland AFB, NM"]
+[-0.33270326256752014, 6.614631175994873, "Electronics TestBed Sponsor BMDO"]
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+[11.826626777648926, 5.335886001586914, "3U CubeSat Orbit MEO (~5900 km)"]
+[11.78709888458252, 5.367286205291748, "1U CubeSat Orbit LEO (~ 500 km)"]
+[11.858346939086914, 5.325811862945557, "3U CubeSat Orbit LEO (~ 500 km)"]
+[11.845580101013184, 5.331732749938965, "3U CubeSat Orbit LEO (~ 500 km)"]
+[11.841326713562012, 5.324471473693848, "3U CubeSat Orbit MEO (~ 5900 km)"]
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+[1.031169056892395, -4.438115119934082, "Satellite Mass 4 kg"]
+[3.731497287750244, 17.700902938842773, "Payload Volume Requirement Nearly a full 1U"]
+[0.6855801343917847, 9.312812805175781, "Attitude Determination and Control Subsystem Pointing Requirement 1\u00ba"]
+[0.6752355098724365, 9.35008430480957, "Attitude Determination and Control Subsystem Determination Requirement 0.5\u00ba"]
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+[2.296593427658081, -1.4009162187576294, "Satellite SAR Image Over La Reunion Island and its coastal area"]
+[2.396848440170288, -1.5948655605316162, "Satellite SAR Image Over La Reunion Island"]
+[4.473202705383301, -2.672358751296997, "Satellite Orbit Duration 1 month"]
+[0.9232262372970581, -2.182858467102051, "Satellite Final Position 9\u00b0E, over Europe"]
+[-5.264259338378906, 7.834695339202881, "Communication System Delivery Time Within 18 minutes"]
+[-5.408173561096191, 2.75899076461792, "Telescope Aperture 50 cm"]
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+[-3.092545986175537, 1.6888424158096313, "Satellite Mission Mass Requirement 220 kg"]
+[-3.086474657058716, 1.7651563882827759, "Satellite Mission Thermal Control Power Requirement 50 W"]
+[-3.081847667694092, 1.7255054712295532, "Satellite Mission Attitude Control Power Requirement 70 W"]
+[-3.0986084938049316, 1.7640105485916138, "Satellite Mission Power Supply Power Requirement 50 W"]
+[-3.047697067260742, 1.8230417966842651, "Satellite Mission TC/TM Power Requirement 25 W"]
+[-3.0673017501831055, 1.8130403757095337, "Satellite Mission Housekeeping Power Requirement 25 W"]
+[-3.1060779094696045, 1.7472041845321655, "Satellite Mission Data Transfer Power Requirement 30 W"]
+[-3.1131999492645264, 1.7491106986999512, "Satellite Mission Platform Total Power Requirement 250 W"]
+[-3.087386131286621, 1.7907592058181763, "Satellite Mission IMI Power Requirement 250 W"]
+[-3.1174120903015137, 1.7295500040054321, "Satellite Mission PMI Power Requirement 250 W"]
+[-3.1212668418884277, 1.7611056566238403, "Satellite Mission DFPSCAT Power Requirement 800 W"]
+[-3.107301950454712, 1.7442553043365479, "Satellite Mission Payload Total Power Requirement 1300 W"]
+[1.9859888553619385, 21.995838165283203, "Instrument Swath Large"]
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+[0.5541732907295227, -1.5053868293762207, "Satellite Orbit Altitude 526 km"]
+[4.185945510864258, -2.8033392429351807, "Satellite Orbit Period 100 minutes"]
+[-5.371488094329834, 2.797672748565674, "Telescope Imaging Capability High-energy X-rays"]
+[-5.390929698944092, 2.7935097217559814, "Telescope Ability to Capture Nanoflares Potential"]
+[-1.1110560894012451, 3.074687957763672, "Celestial Body Surface Temperature 6,000 degrees Celsius"]
+[-1.1518092155456543, 3.073395013809204, "Celestial Body Corona Temperature On average 1 million degrees Celsius"]
+[1.7097753286361694, 6.9255595207214355, "Communication Devices Quantity More than 50 billion globally"]
+[3.1677935123443604, -1.745652198791504, "Satellite IoT Company Investment Raised 10 million euros ($11.4 million)"]
+[-1.3375494480133057, 6.054510593414307, "Global Technology Company Ownership Stake Approximately 10.5%"]
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+[1.3476687669754028, 10.549070358276367, "Imaging System Pan Image Detector Size 4096 pixels x 4096 lines"]
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+[1.4113503694534302, -1.9380708932876587, "Satellite General Relativistic Effect Test Frame-dragging"]
+[1.384251356124878, -1.9291703701019287, "Satellite General Relativistic Effect Test Frame-dragging"]
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+[-3.0701904296875, 4.305525779724121, "Spacecraft Function Provide emergency abort during the launch ascent phase, sustain the crew during space travel, and provide safe reentry from deep space return velocities"]
+[-2.9210832118988037, 4.462540626525879, "Spacecraft Module Function Fuel and propel the Orion spacecraft in space"]
+[-2.9296419620513916, 4.4569268226623535, "Spacecraft Module Function Contain the in-space propulsion capability for orbital transfer, attitude control, and high-altitude ascent aborts"]
+[3.0096426010131836, -1.6179202795028687, "Satellite Mission Name Transiting Exoplanet Survey Satellite"]
+[2.74869966506958, -1.2393580675125122, "Satellite Purpose Discovering new Earths and Super-Earths in the solar neighborhood"]
+[-3.0937750339508057, 4.275694847106934, "Spacecraft Manufacturer Lockheed Martin"]
+[-3.082592487335205, 4.362115383148193, "Spacecraft Crew Capacity 2\u20136 astronauts"]
+[-3.171194314956665, 4.38455057144165, "Spacecraft Purpose Crewed missions to the Moon, asteroids and Mars"]
+[-2.1638190746307373, 5.95322322845459, "Test Flight Launch Date December 5, 2014"]
+[0.5342637300491333, -1.4612115621566772, "Satellite Orbit Altitude 9.5 km under the A-train"]
+[2.0696959495544434, -1.901389241218567, "Satellite Availability Near 90%"]
+[5.135746479034424, -4.421631813049316, "Satellite Deorbiting Date Autumn of 2013"]
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+[-1.1014595031738281, 4.494162082672119, "Ground Stations Network Global"]
+[-4.274794578552246, 7.385849952697754, "Data Transfer Method Direct downlink to users"]
+[-4.2297539710998535, 7.422539710998535, "Data Transfer Method Relay via satellite"]
+[-6.778215408325195, 10.02707290649414, "Antenna Dimensions 6.29 m x 2.09 m x 0.220 m"]
+[6.265394687652588, 7.405600547790527, "Satellite Component Mass 290 kg"]
+[-8.148039817810059, 8.830445289611816, "Electrical Power Subsystem Design Conditions 6 hour and 18 hour orbit illumination, large power requirement of the SAR payload, solar eclipse conditions during the summer solstice"]
+[-2.3469879627227783, 9.184975624084473, "Power System Power Output ~1000 W at the beginning of the mission, varying throughout the mission to ~ 700 W"]
+[-2.389533519744873, 9.198973655700684, "Power System Average On-Orbit Power About 700 W"]
+[6.31856632232666, 7.424915313720703, "Satellite Component Area 14.5 m2"]
+[-0.3790757954120636, 16.169397354125977, "Camera/Spectrograph Mission Apollo 16"]
+[-3.187796115875244, 1.7320635318756104, "Satellite Mission Level 2 Data Release Date June 3, 2019"]
+[-3.2477810382843018, 1.7550171613693237, "Satellite Mission Level 1C Data Availability March 12, 2019"]
+[2.7306785583496094, -1.2385398149490356, "Satellite General Objective Study the Earth's atmosphere"]
+[2.6607000827789307, -1.3778984546661377, "Satellite Specific Interest Role of clouds and aerosols in climate mechanisms"]
+[1.375098466873169, -1.451671838760376, "Satellite Measurement Accuracy Within a fraction of an inch"]
+[2.692859172821045, 21.929359436035156, "Instrument Function Times how long it takes light to travel to Earth\u2019s surface and back"]
+[2.6826910972595215, -1.636458158493042, "Satellite Data Processing Location NASA Goddard"]
+[2.619603157043457, -1.4421131610870361, "Satellite Data Products Availability Now available for free from the National Snow and Ice Data Center"]
+[1.4388359785079956, 2.755492687225342, "Weather Satellite Launch Date March 1"]
+[1.4793721437454224, 2.712756872177124, "Weather Satellite Orbital Location 137\u00ba west"]
+[1.4400506019592285, 2.7590856552124023, "Weather Satellite Launch Vehicle Atlas 5"]
+[-3.2867870330810547, 5.440693378448486, "Launch Vehicle Payload Fairing Diameter Five-meter"]
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+[-4.365196228027344, 0.19537602365016937, "GPS Receiver Operating Frequency 1227.6 MHz and 1575.4 MHz"]
+[-4.362856864929199, 0.19876298308372498, "GPS Receiver Mass 28 kg"]
+[-4.36663818359375, 0.1920422911643982, "GPS Receiver Power Consumption 29 W"]
+[-4.35769510269165, 0.19594399631023407, "GPS Receiver Altitude Accuracy < 10 cm"]
+[-1.5065042972564697, 16.899656295776367, "Altimeter Type Single-Frequency Solid-State"]
+[-1.7240177392959595, 6.610156536102295, "Program Objective Removing a large ESA-owned object from space"]
+[-0.6548191905021667, 6.736098289489746, "Study Phase 0 Analysis of a mission that could remove very heavy debris from orbit"]
+[-0.6492690443992615, 6.726373195648193, "Study Objective Remote maintenance of geostationary telecommunications satellites using a robotic arm"]
+[-0.6453889608383179, 6.756073474884033, "Study Objective ADR mission scenarios"]
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+[3.3246448040008545, 0.46361371874809265, "Satellite Program Data Declassification Date March 1973"]
+[3.321779727935791, 0.4591161906719208, "Satellite Program Constellation Two near-polar, sun-synchronous satellites"]
+[3.319075345993042, 0.43997424840927124, "Satellite Program Mission Provide global visible and infrared cloud data and other specialized meteorological, oceanographic and solar-geophysical data in support of world wide Department of Defense (DoD) operations"]
+[1.77149498462677, 22.209577560424805, "Instrument Pixel Spacing 300 m"]
+[4.564874172210693, -2.6806607246398926, "Satellite Routine Phase Operations Duration Over three years"]
+[2.050764322280884, -1.9499768018722534, "Satellite Availability Requirement Above 97%"]
+[2.1220905780792236, -1.4964299201965332, "Satellite Image Acquisition Success Rate Maintained at a high level"]
+[2.582381248474121, 14.278453826904297, "Optical Instrument Calibration Measurement Dark Earth, X-ray point sources"]
+[-0.4751030504703522, 5.84379768371582, "Unknown Types Cosmic X-ray, near-Earth extreme ultraviolet, instrument background"]
+[14.461170196533203, 7.6772966384887695, "Nanosatellite Mission Focus Attitude control, RF sensing, and high-speed data downlink"]
+[14.265079498291016, 7.795441150665283, "Nanosatellite Development Start Date June 2014"]
+[14.253453254699707, 7.798752307891846, "Nanosatellite Flight Model Delivery Date One year later"]
+[14.430085182189941, 7.698721885681152, "Nanosatellite Development Standards ESA-tailored ECSS (European Cooperation for Space Standards) engineering standards and product/quality assurance requirements"]
+[11.291707992553711, 5.539382457733154, "CubeSat Pointing Error Arcsec-level"]
+[11.236252784729004, 5.4813079833984375, "CubeSat Focal Plane Temperature Control Highly stable"]
+[0.9755440950393677, -4.363553047180176, "Satellite Mass 125 kg"]
+[1.1515021324157715, -0.7243406772613525, "Satellite Size 60 x 60 x 130 cm"]
+[5.291325569152832, -2.2072932720184326, "Satellite Design Life 5 years"]
+[1.5556623935699463, -1.2295852899551392, "Satellite Resolution 2.5m for the panchromatic band, and a 10 m for the four multispectral bands"]
+[1.1746623516082764, -1.4971425533294678, "Satellite Swath 17.5 km"]
+[1.7560659646987915, -2.012052059173584, "Satellite Attitude Determination Three gyroscopes and a star tracker"]
+[-1.6662288904190063, 11.233366012573242, "Lidar Function Sends pulses of laser light toward Earth and precisely times each photon\u2019s round-trip journey as it bounces off a surface and returns to the sensor"]
+[-0.09062189608812332, 4.97722053527832, "Iceberg Height About 35 meters (100 feet) above sea level"]
+[-0.08651970326900482, 4.996984958648682, "Iceberg Thickness About 280 meters"]
+[2.8899035453796387, 21.992904663085938, "Instrument Purpose Atmosphere and Ocean observation"]
+[2.3135790824890137, 22.700641632080078, "Instrument Quantity +49"]
+[-7.513587951660156, 5.944325923919678, "Electro Optical Camera Resolution 6.6 m (Pan)"]
+[-7.530881404876709, 5.919614791870117, "Electro Optical Camera Swath Width 17 km"]
+[-2.4789199829101562, 13.113364219665527, "Multispectral Camera Resolution 1 m (Pan)"]
+[-2.465057373046875, 13.133515357971191, "Multispectral Camera Swath Width 15 km"]
+[1.0513747930526733, 10.753841400146484, "Advanced Earth Imaging Sensor System Resolution 4 m (4 x MS)"]
+[0.8894796967506409, 10.793949127197266, "Advanced Earth Imaging Sensor System Swath Width 15 km"]
+[-5.255259990692139, 15.880156517028809, "Corea SAR Instrument Resolution 0.7 m (Pan)"]
+[-5.251452445983887, 15.879191398620605, "Corea SAR Instrument Swath Width 16.8 km"]
+[-5.234293460845947, 15.883819580078125, "Corea SAR Instrument Resolution 2.8 m (4 x MS)"]
+[-5.264153003692627, 15.86704158782959, "Corea SAR Instrument Swath Width 16.8 km"]
+[-5.254117488861084, 15.877652168273926, "Corea SAR Instrument Resolution 1 m"]
+[-5.255005836486816, 15.877260208129883, "Corea SAR Instrument Swath Width 5 km"]
+[-5.251314163208008, 15.879759788513184, "Corea SAR Instrument Resolution 3 m"]
+[-5.215865612030029, 15.872322082519531, "Corea SAR Instrument Swath Width 30 km"]
+[-5.222220420837402, 15.875736236572266, "Corea SAR Instrument Resolution 20 m"]
+[-5.247129440307617, 15.879793167114258, "Corea SAR Instrument Swath Width 100 km"]
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+[0.5413100719451904, -1.4456281661987305, "Satellite Orbital Altitude 685 km"]
+[0.5445447564125061, -1.4525518417358398, "Satellite Orbital Altitude 685 km"]
+[0.563952624797821, -1.4709089994430542, "Satellite Orbital Altitude 550 km"]
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+[3.856766700744629, -3.2085940837860107, "Satellite LTAN 10:50 hours"]
+[3.877737045288086, -3.169848680496216, "Satellite LTAN 13:30 hours"]
+[3.8771705627441406, -3.199094533920288, "Satellite LTAN 6:00 hours"]
+[5.1332268714904785, -2.2834246158599854, "Satellite Design Life 3 years"]
+[5.12583065032959, -2.2855987548828125, "Satellite Design Life 3 years"]
+[5.13250207901001, -2.2880804538726807, "Satellite Design Life 4 years"]
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+[2.088046073913574, -0.49173396825790405, "Satellite Power 1.3 kW"]
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+[1.3175151348114014, -1.9243885278701782, "Satellite Polarimetric Observations At multiple incidence angles"]
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+[4.467586517333984, -2.584376096725464, "Satellite Data Collection Period 40 years"]
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+[0.49015727639198303, 4.506781578063965, "Natural Phenomenon Trend About a week later per decade"]
+[0.47086116671562195, 4.522973537445068, "Natural Phenomenon Trend Nearly one month later since the start of the satellite record in 1979"]
+[0.5151459574699402, 12.199764251708984, "Sensor Field of View 12km"]
+[0.5918607115745544, 12.149109840393066, "Sensor Detection Threshold ~100 parts per billion (ppb)"]
+[0.45348218083381653, 12.299467086791992, "Sensor Pixel Size Tens of meters"]
+[0.9180765151977539, -1.3706371784210205, "Satellite Field of View 12km"]
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+[-3.0963168144226074, 2.415266275405884, "Mission Duration 11 years"]
+[-3.0980029106140137, 2.4228155612945557, "Mission Data Size Hundreds of terabytes"]
+[5.354287147521973, -4.384056568145752, "Satellite Launch Date November 2018"]
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+[-5.8563971519470215, 15.979618072509766, "Synthetic Aperture Radar FRS-2 Resolution 6 m x 4 m (Az x Range)"]
+[-5.924200534820557, 16.040184020996094, "Synthetic Aperture Radar FRS-2 Swath 25 km"]
+[-5.89893913269043, 16.003604888916016, "Synthetic Aperture Radar MRS Resolution 25 m x 8 m (Az x Range)"]
+[-5.889106750488281, 16.012163162231445, "Synthetic Aperture Radar MRS Swath 115 km"]
+[-5.878215789794922, 15.992228507995605, "Synthetic Aperture Radar CRS Resolution 50 m x 8 m (Az x Range)"]
+[-5.929892063140869, 16.049345016479492, "Synthetic Aperture Radar CRS Swath 223 km"]
+[-5.886817455291748, 15.969742774963379, "Synthetic Aperture Radar HRS Resolution < 2 m"]
+[-5.938584327697754, 15.947086334228516, "Synthetic Aperture Radar HRS Spotlight Target 10 km (azimuth) x 10 km (ground range)"]
+[-2.514390468597412, 13.013810157775879, "Multispectral Pushbroom Imager Data Requirements Disaster and emergency response, environment, mapping, urban planning, landcover, geology, coastal zone monitoring, ecosystem, and water resource management"]
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+[2.3118011951446533, 22.77247428894043, "Instrument Bandwidth (\u00c5) 1700"]
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+[2.067244291305542, 22.427576065063477, "Instrument Solar Temp. Range 3.6 - 3.8"]
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+[2.6572141647338867, 13.434943199157715, "Diffractive Optic Element Number of Beams 6"]
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+[-3.0452194213867188, 2.4776065349578857, "Mission Launch Date December 2014"]
+[-1.3158564567565918, 6.134174346923828, "Company URL http://blogs.nasa.gov/spacex/wp-content/uploads"]
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+[2.0579705238342285, -2.727994203567505, "Satellite Number of Pulsating Red Giants Identified More than 158,000"]
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+[-0.15904276072978973, 15.5765380859375, "Spectrometer Spectral Coverage 1024 visible channels in the range of 0.753 - 0.784 \u00b5m"]
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+[1.0120635032653809, -4.376951217651367, "Satellite Payload Mass ~1,250 kg"]
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+[0.9420702457427979, -2.0950241088867188, "Satellite Angular Drift Rate 0.0005\u00ba/s"]
+[3.125722885131836, -1.4564675092697144, "Satellite Educational Mission Provide educational opportunities with academic engagement for students on an actual aerospace system"]
+[3.084864616394043, -1.4781150817871094, "Satellite Educational Mission Develop in-house engineering solutions for ABEX lead by student design teams"]
+[3.124279260635376, -1.44219172000885, "Satellite Educational Mission Provide graduate students with early-career leadership roles in the project and system management roles"]
+[3.18277907371521, -1.56303071975708, "Satellite Educational Mission Facilitate continuous engagement with ASGC universities in the engineering and management of the project"]
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+[5.345005512237549, -4.5024094581604, "Satellite Launch Date Jun 13, 2012"]
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+[16.987285614013672, 6.7315144538879395, "Microsatellite Project Date Dec. 5-9, 2005"]
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+[-2.948075771331787, 4.2984299659729, "Tiny Spacecraft Printed Circuit Board Area 3.5 by 3.5 cm"]
+[-2.9706778526306152, 4.378518104553223, "Tiny Spacecraft Printed Circuit Board Thickness A few millimeters"]
+[-2.927563190460205, 4.289175987243652, "Tiny Spacecraft Printed Circuit Board Mass A few grams"]
+[-1.3686233758926392, 13.24619197845459, "Solar Wind Collector Accelerator Grid Voltage -8 kV"]
+[-1.2688475847244263, 13.14013671875, "Solar Wind Collector Collector Arrays Deployed from the SRC (Sample Return Capsule) which faces the sun"]
+[2.6042001247406006, 21.864023208618164, "Instrument Function Monitor solar wind"]
+[-2.067415714263916, 14.976051330566406, "Integrated L-band radiometers and scatterometer Objectives Understanding ocean circulation, global water cycle and climate interaction. Soil moisture measurements over Argentina"]
+[-2.100677013397217, 14.95958423614502, "Integrated L-band radiometers and scatterometer Frequency 1..413 GHz"]
+[-1.9855895042419434, 14.917756080627441, "Integrated L-band radiometers and scatterometer Beam Resolution Three beams: 76 km x 94 km, 84 km x 120 km, 96 km x 156 km"]
+[-1.869402289390564, 14.868103981018066, "Radiometer Parameters Precipitation rate, wind speed, sea ice concentration, water vapor, clouds"]
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+[-1.8743889331817627, 14.903196334838867, "Radiometer Polarization H+V"]
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+[-2.479909896850586, 14.079002380371094, "Infrared Sounder Objectives Hot spot events, SST (Sea Surface Temperature) measurements"]
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+[-2.5069873332977295, 14.111490249633789, "Infrared Sounder Swath 180 km"]
+[-7.516345977783203, 5.949467182159424, "High Sensitivity Camera Objectives Urban lights, electric storms, polar regions, snow cover"]
+[-7.525326251983643, 5.941026210784912, "High Sensitivity Camera Wavelength 0.45 - 0.9 \u00b5m"]
+[-7.5198163986206055, 5.951753616333008, "High Sensitivity Camera Swath 700 km"]
+[-3.8469700813293457, 6.914571762084961, "Data Collection System Uplink Frequency 401.55 MHz"]
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+[-4.3168206214904785, 0.25308191776275635, "GPS Occultation System Vertical Resolution 300 m"]
+[-0.5134337544441223, 7.156426429748535, "Technology Demonstration Package Objectives Position, velocity and time determination, inertial angular velocity"]
+[-0.48689979314804077, 7.162939071655273, "Technology Demonstration Package GPS Receiver Resolution 20 m"]
+[-0.5296099185943604, 7.152764320373535, "Technology Demonstration Package Inertial Reference Unit Resolution 1 m/s"]
+[-0.456424742937088, 7.157973289489746, "Technology Demonstration Package ARW 0.008\u00ba/sqrt h"]
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+[-0.9475292563438416, 4.89711332321167, "Remote Tracking Station Location Kaena Point, HI"]
+[-0.9915806651115417, 4.893424034118652, "Remote Tracking Station Location New Boston, NH"]
+[-0.9990867376327515, 4.834528923034668, "Remote Tracking Station Location Thule, Greenland"]
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+[-2.987170696258545, 4.185303211212158, "Spacecraft Solar panel pointing -Xs points to the sun, Ys is parallel to Earth equator plane"]
+[-1.8705884218215942, 14.852007865905762, "Radiometer System Overview Unknown"]
+[-1.622011423110962, 1.4859470129013062, "Data Relay System Data Transmission Few TB (terabyte) of data every day"]
+[-1.6215636730194092, 1.4837918281555176, "Data Relay System Service Provision Copernicus program"]
+[-1.607295036315918, 1.4632123708724976, "Data Relay System Technology Optical and Ka-band"]
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+[7.248186111450195, 12.370575904846191, "Satellite Instrument Swath Width 80 km"]
+[7.296651840209961, 12.420578956604004, "Satellite Instrument Ground Resolution 700 m"]
+[7.267285346984863, 12.397151947021484, "Satellite Instrument Swath Width 1400 km"]
+[7.28920316696167, 12.411249160766602, "Satellite Instrument Antennas 6"]
+[7.2382493019104, 12.350685119628906, "Satellite Instrument Frequency 13.995 GHz"]
+[7.278680324554443, 12.397211074829102, "Satellite Instrument Swath Width 600 m"]
+[7.282069683074951, 12.411471366882324, "Satellite Instrument Spectral Bands 6"]
+[7.2752838134765625, 12.401810646057129, "Satellite Instrument Frequency Range 308.6 nm to 360 nm"]
+[7.257964134216309, 12.386174201965332, "Satellite Instrument Channels 15"]
+[7.279626369476318, 12.406688690185547, "Satellite Instrument Beam Dimensions 1440 km x 2200 km"]
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+[7.276613235473633, 12.397497177124023, "Satellite Instrument Visible Channels 1024"]
+[7.263731479644775, 12.387887001037598, "Satellite Instrument Infrared Bands 3"]
+[7.355465888977051, 12.48116683959961, "Satellite Instrument Spectral Resolution 0.1 cm-1"]
+[1.4526954889297485, -2.4957492351531982, "Satellite Orbit Type Sun-synchronous polar descending"]
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+[6.1723833084106445, 7.569681644439697, "Satellite Component Parameter Value"]
+[-1.112898588180542, 8.271350860595703, "Semiconductor Thickness 100 \u00b5m"]
+[-1.0306028127670288, 11.09046745300293, "CCD-80 Thickness 100 \u00b5m"]
+[-1.0306963920593262, 11.07574462890625, "CCD-80 Quantum Efficiency Improvement Over 20% at 1000 nm"]
+[-1.181183099746704, 8.386528968811035, "Semiconductor Quantity 16"]
+[-2.129009962081909, 7.777251243591309, "Avionics System Structure Card-frame with backplane interconnections"]
+[-2.5552897453308105, 9.258541107177734, "Power Distribution Module Module Type Unknown"]
+[-2.9026715755462646, 9.293696403503418, "Battery Charge Module Module Type Unknown"]
+[-4.792994499206543, 9.320391654968262, "S-band Transmitter/Receiver Module Type Unknown"]
+[3.7466259002685547, 17.669960021972656, "Payload Interface Unit Module Type Unknown"]
+[-2.727170705795288, 8.759442329406738, "Module Module Type Unknown"]
+[0.5438112020492554, 9.423781394958496, "Attitude Determination and Control System Module Type Unknown"]
+[11.135132789611816, 5.252121448516846, "CubeSat Mass 3 kg"]
+[11.490094184875488, 5.716950416564941, "CubeSat Size 2U"]
+[11.538200378417969, 5.7444939613342285, "CubeSat Size 1U"]
+[11.136493682861328, 5.239762306213379, "CubeSat Mass 2 kg"]
+[16.6054744720459, 6.988070487976074, "Minisatellite Mass 138 kg"]
+[-2.784379005432129, 8.019892692565918, "Atomic Clock Stability 100 times more stable than today\u2019s best navigation clocks"]
+[2.6203107833862305, 22.161701202392578, "Instrument Observation Nitric Oxide in the Mesosphere and Lower Thermosphere"]
+[-3.4224929809570312, 4.371146202087402, "Spacecraft Publication Year 1996"]
+[-3.4283204078674316, 4.348013401031494, "Spacecraft Publication Year 1997"]
+[-3.637566089630127, 12.759998321533203, "Particle Detector Antiproton to proton ratio Measured"]
+[-3.644243001937866, 12.756052017211914, "Particle Detector Proton Flux Characteristically different from all the existing experimental results"]
+[-3.5430104732513428, 12.667335510253906, "Particle Detector Helium Flux Exhibits nearly identical and equally unexpected behavior as the proton flux"]
+[-3.6406869888305664, 12.760043144226074, "Particle Detector Positron Fraction, Antiproton/Proton Ratio, Electron Flux, Positron Flux, Proton Flux, Helium Flux, and other nuclei fluxes Provide precise and unexpected information"]
+[-5.286775588989258, 2.734156847000122, "Telescope Observation Date 18 to 19 October 2019"]
+[-5.389212131500244, 2.746163845062256, "Telescope Image Content LMC (Large Magellanic Cloud)"]
+[-5.337737083435059, 2.8011577129364014, "Telescope Image Content A3391/3395 system of interacting clusters of galaxies"]
+[-5.336532115936279, 2.7093262672424316, "Telescope Survey Duration 4 years"]
+[-2.9488251209259033, 4.229752063751221, "Spacecraft Image Resolution 10 m per pixel"]
+[-3.1105899810791016, 4.221220016479492, "Spacecraft Mission Objective Obtain important technical data for future deep-space exploration"]
+[-3.5315568447113037, 4.353390216827393, "Spacecraft Departure Date from L2 April 15, 2012"]
+[-3.498678684234619, 4.36984395980835, "Spacecraft Map of the Moon's Surface Observation Period October 2010 and May 2011"]
+[7.3105926513671875, 12.429530143737793, "Satellite Instrument Azimuth Extent Up to 100 km"]
+[7.311212539672852, 12.433542251586914, "Satellite Instrument Range Looks Up to 2"]
+[7.282884120941162, 12.407397270202637, "Satellite Instrument Antenna Beam Pointing Switches electronically in the elevation direction"]
+[7.218294143676758, 12.34016227722168, "Satellite Instrument Antenna Roll-Tilting \u00b136\u00ba"]
+[7.222528457641602, 12.354462623596191, "Satellite Instrument Elevation Beam Width 2.2\u00ba -1.5\u00ba"]
+[7.321744441986084, 12.444759368896484, "Satellite Instrument Off-Nadir Distance 107 km"]
+[7.309002876281738, 12.428631782531738, "Satellite Instrument Off-Nadir Look Angle 11.5-49.5\u00ba"]
+[-2.7192981243133545, 7.180211544036865, "Command and Control Segment Function Operating and monitoring the Aquarius Instrument's health"]
+[-2.6651971340179443, 7.245449542999268, "Command and Control Segment Coordination Coordinates with the Aquarius Science Team and the SAC-D Operations personnel"]
+[-0.12326551973819733, 6.394264221191406, "Testbed Verification Each Aquarius instrument command activity, nominal or contingency, is verified using the Aquarius testbed"]
+[-13.69659423828125, -2.3140759468078613, "X-ray Telescope Launch Date June 13, 2012"]
+[-14.010865211486816, -2.3240787982940674, "X-ray Telescope Mission Operations Center University of California, Berkeley"]
+[-13.865748405456543, -2.2296364307403564, "X-ray Telescope Official Data Archive NASA's High Energy Astrophysics Science Archive Research Center"]
+[0.4478767514228821, 4.554961204528809, "Natural Phenomenon X-ray Light Production Low-energy X-ray light"]
+[2.192218065261841, -1.9697908163070679, "Satellite Naming Italian word for \"Jupiter\""]
+[-5.341344356536865, 2.739753484725952, "Telescope Discovery Date January 7, 1610"]
+[-1.591528296470642, 4.118966579437256, "Ground Segment Name Galileo System Test Bed"]
+[-1.5417687892913818, 4.186025619506836, "Experimental Ground Segment Name Galileo System Test Bed-V1"]
+[-2.3690590858459473, 4.035207271575928, "Experimental Space Segment Name Galileo System Test Bed-V2"]
+[2.6512224674224854, -2.5886499881744385, "Satellite Data Communication Speed 1.2 Gbit/s"]
+[-10.264015197753906, 9.977762222290039, "Accelerometer Development Status Delivered in December 2015"]
+[-10.264490127563477, 9.975947380065918, "Accelerometer CDR Date September 2014"]
+[-10.264887809753418, 9.976253509521484, "Accelerometer EM Build Year 2013"]
+[-10.264184951782227, 9.97797966003418, "Accelerometer Delivery Date September 2015"]
+[-10.262887001037598, 9.979326248168945, "Accelerometer Launch Date August 2017"]
+[-3.649634838104248, 12.750635147094727, "Particle Detector Purpose Studies charged particles and nuclei in the cosmos"]
+[-3.6028659343719482, 12.79560375213623, "Particle Detector Data Accuracy ~1%"]
+[-3.6225836277008057, 12.73228931427002, "Particle Detector Data Collected More than 90 billion cosmic rays"]
+[-3.5914299488067627, 12.79598617553711, "Particle Detector Cosmic Rays Energy Up to multi-TeV"]
+[-3.6312499046325684, 12.753039360046387, "Particle Detector Observed Particles Electrons, protons, positrons and antiprotons"]
+[5.3199615478515625, -4.531101226806641, "Satellite Launch Date 29 July, 2009"]
+[2.4194319248199463, -1.9860186576843262, "Satellite Replacement DubaiSat-2"]
+[5.35471773147583, -4.486682891845703, "Satellite Launch Date 21 November, 2013"]
+[2.7275242805480957, 21.62922477722168, "Scientific Instrument Function Supports and measures the fern spore ion channel activity"]
+[2.6638071537017822, 21.668886184692383, "Scientific Instrument Quantity Three"]
+[2.7382266521453857, 21.6348934173584, "Scientific Instrument Type BioCDs"]
+[-4.363648414611816, 0.19425256550312042, "GPS Receiver Function Determine position, velocity and time using GPS signals"]
+[-4.339667320251465, 0.2194913774728775, "GPS Receiver Frequency Bands L1 and L2"]
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+[-3.1035232543945312, 14.728464126586914, "Microwave Sounder Data Volume 1.5 MByte per satellite"]
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+[3.481290817260742, 13.405187606811523, "Laser Communication Terminal Design One-unit"]
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+[-1.0479190349578857, 7.7112507820129395, "Device Operation Tailored to the operation in a LCT under harsh environmental conditions outside the spacecraft in GEO"]
+[-1.013782262802124, 7.759749889373779, "Device Potential Applications High precision, long life space instruments"]
+[-5.358549118041992, 2.717698574066162, "Telescope Operation Duration 4 years"]
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+[-3.237790822982788, 1.698509931564331, "Satellite Mission 9th Science Meeting Date 11-14 November 2014"]
+[-3.1896281242370605, 1.71005380153656, "Satellite Mission NASA Senior Review 2015"]
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+[-1.028900384902954, 9.08796215057373, "Thermal Vacuum Chamber Test Duration Weeks at a time"]
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+[-10.265497207641602, 9.975783348083496, "Accelerometer Instrument Family GRADIO accelerometer models composing the three axis gravity gradiometer of the GOCE mission of ESA"]
+[-7.374699115753174, 2.8918297290802, "Cosmic Ray Detector Energy Range 0.5 to 350 GeV"]
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+[3.4845211505889893, 13.85102367401123, "Laser Interferometer Development Joint US-German development with additional contributions from Australia"]
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+[0.1641189306974411, 7.217433929443359, "Science Experiment Objective Perform refractive radio occultation measurements of Earth's atmosphere"]
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+[4.715851783752441, -4.536599159240723, "Satellite Image Capture Date 20 January"]
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+[2.3933892250061035, -1.4834721088409424, "Satellite Data Capture 15TB per day"]
+[1.1613725423812866, -1.3139952421188354, "Satellite Coverage Area 25 million km\u00b2"]
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+[2.527702569961548, -1.757416009902954, "Satellite Payloads Optical communication system; and a high-performance payload data processor"]
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+[6.308011531829834, 7.45531702041626, "Satellite Component Power Buses 3.8, 5, 8 and 12 Volts"]
+[1.687880039215088, 6.961756229400635, "Communication Device Ground Command Acceptance Yes"]
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+[7.314422130584717, 12.450764656066895, "Satellite Instrument Manufacturer LASP (Laboratory for Atmospheric and Space Physics) at the University of Colorado, Boulder, CO"]
+[7.291159629821777, 12.422774314880371, "Satellite Instrument Principal Investigator Richard Eastes"]
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+[-1.242125153541565, 8.571687698364258, "Component Integration GNSS (Global Navigation Satellite Systems) constellations"]
+[-5.092666149139404, 9.178755760192871, "Radiobeacon Device Type Maritime"]
+[-5.094808578491211, 9.16809368133545, "Radiobeacon Device Type Aviation"]
+[-5.074435234069824, 9.262107849121094, "Radiobeacon Device Type Personal Locator Beacons"]
+[1.0096725225448608, -4.335805416107178, "Satellite Mass Up to 1000 kg"]
+[2.3140323162078857, -1.1913259029388428, "Satellite Imagery SAR imagery and eventually also optical imagery"]
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+[2.9194226264953613, -1.814713478088379, "Satellite Market Worldwide customers as well as institutional users in Russia"]
+[1.4335728883743286, 2.756303548812866, "Weather Satellite Launch Date July 8, 2014"]
+[-3.2454590797424316, 5.423490524291992, "Launch Vehicle Delay Date Sept. 27, 2013"]
+[-0.8393220901489258, 11.656803131103516, "Detector Silicon Tracker Constant Temperature"]
+[-0.8092619776725769, 11.5856294631958, "Detector Number of Redundant Cooling Pumps 4"]
+[-0.8107016682624817, 11.599752426147461, "Detector Required Operating Cooling Pumps 1"]
+[-0.7888055443763733, 11.592887878417969, "Detector Number of Years for Spacewalk Planning 4 years"]
+[-0.8376823663711548, 11.636926651000977, "Detector Number of Data Channels Over 300,000"]
+[-1.05475652217865, 11.934703826904297, "Infrared Array Detector Array Size 327 x 240"]
+[-0.9736464023590088, 11.883163452148438, "Infrared Array Detector Operating Mode TDI (Time Delay Integration)"]
+[-0.9556888937950134, 11.93111515045166, "Infrared Array Detector Cumulative Imaging Capability x 40"]
+[-0.9837964773178101, 11.880727767944336, "Infrared Array Detector Instrument Roll Stability 0.01\u00ba/s"]
+[-0.9675335884094238, 11.973891258239746, "Infrared Array Detector Yaw Accuracy \u00b10.1\u00ba"]
+[2.3026773929595947, -2.1058237552642822, "Satellite Type CubeSat nanosatellite"]
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+[-1.1611617803573608, 15.111501693725586, "Imaging multi-spectral radiometers (vis/IR) Instrument Type Imaging multi-spectral radiometers (vis/IR)"]
+[0.7761620879173279, 4.123246192932129, "Atmospheric chemistry Instrument Type Atmospheric chemistry"]
+[5.311917781829834, -4.421850681304932, "Satellite Launch Date 29 Oct 2018"]
+[5.07220983505249, -4.09569787979126, "Satellite End of Life Date Dec 2023"]
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+[-6.713107585906982, 9.985246658325195, "Antenna Frequency Band X-band"]
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+[-4.699981689453125, 7.801896095275879, "Telemetry Standard Features All the DVB-S2 features have been implemented"]
+[-3.566572666168213, 6.809403419494629, "Data Set Across-Track Span Approximately 150 m"]
+[-3.49853253364563, 6.829241752624512, "Data Data File Duration 1 minute"]
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+[1.1418700218200684, -0.7539289593696594, "Satellite Size 10 cm x 10 cm x 34 cm"]
+[1.02138090133667, -4.399740219116211, "Satellite Mass About 3.5 kg"]
+[2.064426898956299, -0.5967832207679749, "Satellite Power Generation 4 W"]
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+[2.5916337966918945, -2.429872989654541, "Air Force Satellite Control Network Function Global data reception/communication"]
+[-1.6907283067703247, 5.344705104827881, "Mission Operations Center Location Te\u00f3filo Tabanera Space Center in the Province of C\u00f3rdoba (Argentina)"]
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+[-4.275697708129883, 15.804930686950684, "Radar Instrument Mission Cost \u20ac190 million"]
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+[-4.324913024902344, 15.80888557434082, "Radar Instrument Prime Contractor Thales Alenia Space"]
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+[0.7334983944892883, -1.7323987483978271, "Satellite Segment Operation Duration More than 3 years"]
+[-1.163432002067566, 4.455929279327393, "Ground Station Data Characterization In-depth validation of Galileo Mission Segment key technology and design aspects"]
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+[-1.1396650075912476, 3.051199436187744, "Celestial Object Mass About 78 million times the Sun\u2019s mass"]
+[-1.150989294052124, 3.0491199493408203, "Celestial Object Mass Loss About three times the mass of Jupiter"]
+[-3.327810287475586, 8.509286880493164, "Memory Device Power Consumption Varies"]
+[-3.289668083190918, 8.460250854492188, "Memory Device Data Rate Performance Better than NAND-Flash"]
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+[0.7489480376243591, 10.170498847961426, "3D Printer and Recycler Function Closed-loop recycler and 3D printer"]
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+[0.7282276153564453, -1.172088861465454, "Satellite Altitude 827 km"]
+[0.726660430431366, -2.2776529788970947, "Satellite Inclination 98.7\u00b0"]
+[3.8884177207946777, -3.174913167953491, "Satellite LTAN 0930 hours"]
+[4.736260890960693, -4.511965274810791, "Satellite Image Capture Date February"]
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+[2.130392074584961, -1.2782073020935059, "Satellite Image Content A portion of the northwest coast of Poland"]
+[-4.243258476257324, 7.197678089141846, "Data Downlink X-band Channels 2 parallel"]
+[-4.223727226257324, 7.1866455078125, "Data Downlink X-band Channels Data Rate 105 Mbit/s"]
+[-4.224456310272217, 7.144991397857666, "Data Downlink S-band Downlink Data Rates 15, 128, 512 kbit/s"]
+[-4.321494102478027, 7.252596855163574, "Data Downlink S-band Uplink Data Rate 4 kbit/s"]
+[-2.6861939430236816, 9.449685096740723, "Power Generation Type Triple junction solar cells"]
+[-8.140450477600098, 8.826387405395508, "Electric Power Subsystem Function Regulates battery charge levels, controls power generation through a peak power tracker on the solar panels, and provides regulated 5 and 12 V DC power outputs to the spacecraft"]
+[-3.698369264602661, 8.29062557220459, "Power Storage Capacity Four 3.2 Ah lithium-ion battery cells"]
+[-2.6732876300811768, 9.432665824890137, "Power Generation Illumination Time 65% of the time"]
+[2.3113720417022705, 22.19491958618164, "Instrument Measurement Altimetric"]
+[2.7689576148986816, 22.036983489990234, "Instrument Application Measure canopy depth"]
+[2.739147424697876, 22.102632522583008, "Instrument Application Estimate land carbon storage"]
+[2.7298786640167236, 22.147409439086914, "Instrument Application Quantify the polar ice sheet mass balance"]
+[2.8050405979156494, 21.953718185424805, "Instrument Application Determine the seasonal cycle of ice sheet changes"]
+[2.734321355819702, 22.113740921020508, "Instrument Application Determine topographic character of ice sheet changes"]
+[2.6660146713256836, 22.107479095458984, "Instrument Application Estimate sea ice thickness"]
+[2.740187168121338, 22.112106323242188, "Instrument Application Measuring vegetation canopy height"]
+[1.4753177165985107, -1.1240458488464355, "Satellite Imaging Resolution 32 m"]
+[1.0481770038604736, -1.370253086090088, "Satellite Swath Width 600 km"]
+[5.259479522705078, -4.51283597946167, "Satellite Launch Date Nov. 28, 2002"]
+[3.2995777130126953, -2.011657953262329, "Satellite Operational Status Nominally as of 2009"]
+[3.110105514526367, -1.7229255437850952, "Satellite Manufacturer EADS Astrium SAS"]
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+[2.8183600902557373, -3.3274753093719482, "Communication Satellite Announcement Date Sept. 22, 2011"]
+[0.14467275142669678, 7.190520286560059, "Experiment Objective To characterize the GPS signal availability at selected altitudes up to GEO"]
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+[-4.3567399978637695, 0.20194123685359955, "GPS Sampling Device Capture Time Up to 400 ms"]
+[0.12982679903507233, 7.184776306152344, "Experiment Ground Segment Observable extraction and orbit determination software"]
+[-0.7976996302604675, 16.334491729736328, "Fourier Transform Infrared Spectrometer Spectral Range 3.3 - 14.0 \u00b5m"]
+[-0.7884951233863831, 16.29147720336914, "Fourier Transform Infrared Spectrometer Spectral Resolution 0.1 cm-1"]
+[-0.7633839249610901, 16.29058837890625, "Fourier Transform Infrared Spectrometer Absolute Accuracy <1 K"]
+[-0.764927864074707, 16.293058395385742, "Fourier Transform Infrared Spectrometer Stability of Measurement <0.1K"]
+[-0.7887879014015198, 16.296159744262695, "Fourier Transform Infrared Spectrometer IFOV 10 mrad"]
+[-0.7874124050140381, 16.325721740722656, "Fourier Transform Infrared Spectrometer Vertical Resolution About 2-6 km"]
+[-0.7944524884223938, 16.332439422607422, "Fourier Transform Infrared Spectrometer Interferogram Scan Time \u2264 10 s"]
+[5.242353916168213, -4.209527015686035, "Satellite Launch Date 1995"]
+[1.5898934602737427, 2.309971809387207, "Geostationary Program First Launch 2002"]
+[1.5516581535339355, 2.3239471912384033, "Geostationary Program Operational Services Start 2004"]
+[1.4995942115783691, 2.624671697616577, "LEO Meteorological Program MetOp Services Start 2005/6"]
+[2.301271677017212, -1.3526291847229004, "Satellite Sensor Synthetic Aperture Radar"]
+[2.8101484775543213, -1.3914433717727661, "Satellite Mission SAR Imagery"]
+[1.7673438787460327, -1.4024871587753296, "Satellite Measurement Goal for Carbon Dioxide 0.5 ppm"]
+[2.0942559242248535, -1.362472653388977, "Satellite Measurement Goal for Methane 5 ppb"]
+[0.8168367147445679, -1.28250253200531, "Satellite Observation Distance 500 km"]
+[2.3625881671905518, -1.4506462812423706, "Satellite Target-Point Observation Capabilities Enhanced"]
+[2.462850332260132, -1.2011767625808716, "Satellite Monitoring Capability Carbon Monoxide concentrations"]
+[-3.558224678039551, 4.386608600616455, "Spacecraft Launch Date 17 November 2020"]
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+[0.519324004650116, 10.921765327453613, "Image Sensor Spatial Resolution 55 m"]
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+[0.5095033645629883, 10.933854103088379, "Image Sensor Area Coverage 30 km by 20 km"]
+[0.5214777588844299, 10.914472579956055, "Image Sensor Spatial Resolution 2 m"]
+[0.5231683850288391, 10.947129249572754, "Image Sensor Area Coverage 5 km by 3 km"]
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+[2.1300888061523438, -2.6604044437408447, "Satellite Number of Satellites Sold 15"]
+[2.109616279602051, -2.6067099571228027, "Satellite Number of Satellite Operators 6"]
+[-1.2200839519500732, 4.593408107757568, "Ground Support Computers Location NASA/MSFC Huntsville AL"]
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+[-1.2047629356384277, 5.269712448120117, "Regional Centers Function Analysis facilities to support physicists from geographically close AMS universities and laboratories, provide access to the AMS-02 data for visualization, detector verification studies and status of data processing, processing sites for the AMS-02 Monte Carlo production and AMS-02 Data reproductions"]
+[2.28596830368042, -1.659303903579712, "Satellite Camera 4 cameras"]
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+[-4.463098049163818, 8.254759788513184, "Terminal Time Synchronization Accuracy Better than 0.5 seconds"]
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+[-3.337458372116089, 4.300114631652832, "Spacecraft Time to Arrive at Halo Orbit Approximately 3 months"]
+[-3.0607807636260986, 4.394085884094238, "Spacecraft Number of Loops about the L1 point 4"]
+[-3.302689552307129, 4.224283695220947, "Spacecraft Time in Halo Orbit About 2 years"]
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+[-5.8700270652771, 16.00747299194336, "Synthetic Aperture Radar Image Content Various eddies and plumes"]
+[-2.619824171066284, 9.612510681152344, "Power Source Quantity 6"]
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+[-3.842911720275879, 7.920501708984375, "Data Storage Error Correction Complete"]
+[-2.440898895263672, 9.203457832336426, "Power Control Module Function Power distribution"]
+[-2.5352203845977783, 9.290207862854004, "Power Control Module Power Delivery Primary power to the Ancillary Electronics Module (AEM), power the camera, power the MCM"]
+[1.646126627922058, 22.184839248657227, "Instrument Size 10 cm x 10 cm x 8.2 cm"]
+[1.5259824991226196, 21.242267608642578, "Instrument Mass 1 kg"]
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+[2.6135141849517822, 22.582853317260742, "Instrument Telemetry 10 byte/min"]
+[1.6255509853363037, 22.202749252319336, "Instrument Size 10 cm x 10 cm x 8.2 cm"]
+[1.5232338905334473, 21.239953994750977, "Instrument Mass 1.3 kg"]
+[1.6331360340118408, 23.20890998840332, "Instrument Power Consumption 1.7 W"]
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+[2.589632511138916, 22.615436553955078, "Instrument Telemetry 10 byte/min"]
+[-0.7101554274559021, 2.9607696533203125, "Supernova Remnant Name Origin Bad H\u00f6nningen am Rhein"]
+[-4.560404300689697, -3.0886874198913574, "Exoplanet Companions Orbital Period 5 to 27 days"]
+[-4.569695949554443, -3.0918898582458496, "Exoplanet Companions Radius 0.81 to 1.66 times that of Jupiter"]
+[-4.565728187561035, -3.0991289615631104, "Exoplanet Companions Mass Between 77 and 98 times more massive than Jupiter"]
+[-4.604864120483398, -3.131227731704712, "Exoplanet Companions Classification Borderline between brown dwarfs and stars"]
+[2.4977712631225586, 22.630878448486328, "Instrument TLE Events Recorded 35,000"]
+[2.255653142929077, 22.712013244628906, "Instrument Elves Percentage 73.93%"]
+[2.177672863006592, 22.558975219726562, "Instrument Red Sprites Percentage 6.54%"]
+[2.2285103797912598, 22.66999626159668, "Instrument Halos Percentage 5.81%"]
+[2.132981061935425, 22.63831329345703, "Instrument Blue Jets Percentage 13.42%"]
+[2.1826248168945312, 22.61873435974121, "Instrument Gigantic Jets Percentage 0.30%"]
+[1.4520806074142456, 2.749145746231079, "Weather Satellite ReBroadcast (GBR) Volume 4"]
+[1.4568957090377808, 2.750549077987671, "Weather Satellite Unique Payload Services (UPS) URL: http://www.goes-r.gov/spacesegment/ups.html"]
+[2.8003997802734375, -1.198961853981018, "Satellite Search and rescue capabilities Aid"]
+[-1.6198619604110718, 1.4806724786758423, "Ancillary Data Relay System Development Partner GOES-R GS"]
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+[-1.9403440952301025, 7.318157196044922, "Computer Function Manages all peripheral instruments including the sensors and the actuators"]
+[-2.7629544734954834, 7.9294657707214355, "Processor Radiation Environment Behavior Good"]
+[-2.7454605102539062, 7.92045259475708, "Processor Function Monitors periodically the status of the OBC"]
+[-2.7544240951538086, 7.91078519821167, "Processor Function Resets the FPGA whenever a critical fault has occurred in the OBC"]
+[-2.7494442462921143, 7.933098316192627, "Processor Reset Function Can be performed automatically or manually"]
+[-3.648444652557373, 12.739441871643066, "Particle Detector Resolution 1.5% at 10 GeV"]
+[-3.632833242416382, 12.757977485656738, "Particle Detector Maximum Detectable Rigidity Above 1 TeV for protons"]
+[-3.6178808212280273, 12.742807388305664, "Particle Detector Charge Separation Range Up to Z=26"]
+[0.002369873458519578, 15.285868644714355, "Scintillator Resolution 120 ps"]
+[-0.0391869992017746, 15.14336109161377, "Scintillator Detector Material Scintillator"]
+[3.70548152923584, 17.679664611816406, "Payload Commissioning Phase End Date End of July"]
+[-3.0199384689331055, 4.171761512756348, "Spacecraft Final Altitude 657 km"]
+[-3.556084394454956, 4.409480094909668, "Spacecraft Commissioning Phase End Date July 24, 2011"]
+[-2.1581451892852783, 2.9092397689819336, "Observatory Commissioning Phase End Date End of July"]
+[-5.324069976806641, 2.7190499305725098, "Telescope Observation Date 17 and 18 October 2019"]
+[-5.343569755554199, 2.745448112487793, "Telescope Sky Sweep Duration 182 days"]
+[-5.372396469116211, 2.7950053215026855, "Telescope Number of X-ray Sources More than one million objects"]
+[-5.3924102783203125, 2.7968173027038574, "Telescope Number of Known X-ray Sources Roughly doubling the number of known X-ray sources discovered over the 60-year history of X-ray astronomy"]
+[-3.5367934703826904, 4.408345699310303, "Spacecraft Launch Date 18 April 2018"]
+[-3.4078986644744873, 4.351768493652344, "Spacecraft Launch Time 22:51 UTC"]
+[-3.173444986343384, 4.2254414558410645, "Spacecraft Launch Site Cape Canaveral Air Force Station in Florida, SLC-40"]
+[-3.2620689868927, 5.420242786407471, "Launch Vehicle Launch Provider SpaceX"]
+[-3.263054609298706, 5.418147087097168, "Launch Vehicle First Stage Landing Site \u201cOf Course I Still Love You\u201d droneship in the Atlantic Ocean"]
+[-3.324122190475464, 4.265927791595459, "Spacecraft Solar Array Deployment Time 60 days"]
+[-5.3759236335754395, 2.810950517654419, "Optical Telescope Field-of-view Wide"]
+[-5.290973663330078, 2.9322359561920166, "Optical Telescope Subassemblies OTA (Optical Telescope Assembly) and the PEA (Payload Electronics Assembly)"]
+[5.226144313812256, -3.814274549484253, "Satellite Launch Year 2018"]
+[4.582263469696045, -2.6155731678009033, "Satellite Orbit Duration A decade"]
+[2.24145245552063, -1.4817285537719727, "Satellite Instrument Laser altimeter"]
+[2.1808815002441406, -1.4245375394821167, "Satellite Instrument Radar altimeter"]
+[-1.8679652214050293, 7.962680339813232, "  "]
+[14.231864929199219, 7.81336784362793, "Nanosatellite Launch Date 12 January 2018"]
+[14.396466255187988, 7.752830505371094, "Nanosatellite Launch Time 03:59 UTC"]
+[14.63713264465332, 7.791900634765625, "Nanosatellite Mass Not provided"]
+[14.488323211669922, 7.733273506164551, "Nanosatellite Orbit Altitude 550 km"]
+[14.465691566467285, 7.672333717346191, "Nanosatellite Orbit Inclination 97.55\u00ba"]
+[-2.239013910293579, 5.930454730987549, "Flight Vehicle Total Mass of Satellites 1323 kg"]
+[0.5963360071182251, 11.988981246948242, "Sensor Purpose Measure Natural Airglow in the Upper Atmosphere"]
+[0.6257436275482178, 12.02245044708252, "Sensor URL http://www.silvereng.com/programs/ssuli.htm"]
+[-4.260465621948242, 15.748361587524414, "Radar Instrument Band L-band"]
+[2.5561025142669678, -1.778350830078125, "Satellite Payload Radar instrument, RLSBO"]
+[2.4808454513549805, -1.6986994743347168, "Satellite Payload Radar instrument, RLSBO (Side Looking Real Aperture Radar)"]
+[4.569880962371826, -2.609668731689453, "Satellite Mission Duration 70 days (data generation) of 105 operational days (1503 orbits)"]
+[4.058047771453857, -2.5846128463745117, "Satellite SAR Data Collection Approximately 42 hours"]
+[-5.914069175720215, 16.030080795288086, "Synthetic Aperture Radar Sensitivity Surface roughness, slope, and land-water boundaries"]
+[-5.874692916870117, 15.991680145263672, "Synthetic Aperture Radar Applications Determine the directional spectra of ocean waves, surface manifestations of internal waves, polar ice-cover motion, geological structural features, soil moisture boundaries, vegetation characteristics, urban land-use patterns, and other geoscientific features of interest"]
+[-5.867037773132324, 16.004459381103516, "Synthetic Aperture Radar Incidence Angle Near-nadir"]
+[-5.846199989318848, 16.037717819213867, "Synthetic Aperture Radar Incidence Angle Issue Produced severe geometric layover distortions on terrain images of high-relief regions"]
+[-0.7963767051696777, 5.77223539352417, "Suspension System Mirror Diameter 10 cm"]
+[-4.434916973114014, 12.041701316833496, "Electromagnets Quantity 8"]
+[0.7701350450515747, 11.98440170288086, "Sensors Quantity 8"]
+[1.436327576637268, 2.7702744007110596, "Weather Satellite Launch Date 2016"]
+[1.4500670433044434, 2.751652717590332, "Weather Satellite Temperature Range -15 \u00baC to 50 \u00baC"]
+[1.44969642162323, 2.7381255626678467, "Weather Satellite Vacuum Chamber Dimensions 8.8 m x 19.8 m"]
+[-0.12347406148910522, 15.578727722167969, "Spectrometer Spectral Range 400-1000 nm"]
+[-0.14947666227817535, 15.546564102172852, "Spectrometer Spectral Bands 61"]
+[-0.12162471562623978, 15.524757385253906, "Spectrometer Radiometric Resolution 10 bits"]
+[-0.09131742268800735, 15.496670722961426, "Spectrometer Sampling Rate 200 frames/s"]
+[0.030044125393033028, 15.423835754394531, "Spectrometer Mass 1.5 kg"]
+[-0.11715228855609894, 15.528185844421387, "Spectrometer Power 3.3 W"]
+[-0.141780823469162, 15.529687881469727, "Spectrometer Size 245 mm x 95 mm x 85 mm"]
+[-0.1602429449558258, 15.577652931213379, "Spectrometer Spectral Resolution 5 or 10 nm"]
+[-0.059421733021736145, 15.55136489868164, "Spectrometer Data Digitization 8 or 10 bit"]
+[-0.13216355443000793, 15.504446029663086, "Spectrometer Detector CCD image sensor"]
+[-0.05839894711971283, 15.592575073242188, "Spectrometer Quantum Efficiency 0.36 @ 620 nm"]
+[-0.08086057752370834, 15.49898910522461, "Spectrometer Frame Rate 200 1/s"]
+[-0.13057753443717957, 15.51347541809082, "Spectrometer Detector Size 640 x 480 pixels"]
+[-0.13036784529685974, 15.537605285644531, "Spectrometer Communication Interface Camera Link\u00ae"]
+[3.897559404373169, 8.976364135742188, "Shuttle Launch Date Nov. 28 - Dec. 8, 1983"]
+[-3.0967280864715576, 2.431321859359741, "Mission Instrument SOLCON-1"]
+[3.893052101135254, 8.973479270935059, "Shuttle Launch Date March 24 - April 2, 1992"]
+[-3.0987112522125244, 2.420968532562256, "Mission Instrument SOLCON-2, ACRIM-II"]
+[3.8412866592407227, 8.926715850830078, "Shuttle Launch Date Jul. 31, 1992 - Jun. 21, 1993"]
+[-3.0992743968963623, 2.433929443359375, "Mission Instrument SOVA-1, SOVA"]
+[3.8939523696899414, 8.972816467285156, "Shuttle Launch Date April 8-17, 1993"]
+[-3.1027090549468994, 2.423738956451416, "Mission Instrument SOLCON-2, ACRIM-II"]
+[3.8919475078582764, 8.975482940673828, "Shuttle Launch Date Nov. 3-14, 1994"]
+[-3.1009185314178467, 2.421835422515869, "Mission Instrument SOLCON-2, ACRIM-II"]
+[3.886159896850586, 8.969117164611816, "Shuttle Launch Date Aug. 7-19, 1997"]
+[3.892963171005249, 8.97152042388916, "Shuttle Launch Date Oct. 29 - Nov. 7, 1998"]
+[3.8946611881256104, 8.97521686553955, "Shuttle Launch Date Jan. 16-Feb. 1, 2003"]
+[3.3193905353546143, 0.4617457091808319, "Satellite Program Operation Duration Over 50 years"]
+[2.894195318222046, -1.9882831573486328, "Satellite Failure Unknown"]
+[2.9442877769470215, -1.8393734693527222, "Satellite Scrapped Due to limited funding"]
+[1.7206920385360718, 6.9617767333984375, "Communication Device Function Receives and relays metrological, hydrological and oceanographic data"]
+[1.7062183618545532, 6.949132919311523, "Communication Device Function Relays distress signals and detects alerts from beacon transmitters"]
+[0.7085826396942139, -4.144677639007568, "Satellite Launch Mass Approximately 2060 kg"]
+[5.178112030029297, -2.2618823051452637, "Satellite Design Life 7.7 years"]
+[2.556187868118286, -1.9601867198944092, "Satellite Bus Subsystems Thermal Control Subsystem (TCS), Bus Management Unit (BMU), Electrical Propulsion Subsystem (EPS), Attitude and Orbit Control Subsystem (AOCS ), Liquid Apogee Motor (LAM) and Radio Frequency (RF) communications"]
+[1.6446013450622559, 7.002703666687012, "Communication Device Number of Sensors 20"]
+[-2.5760421752929688, 9.276514053344727, "DC-DC Converter Efficiency >87%"]
+[-1.4652044773101807, 8.324773788452148, "Diode Driver Peak Current 4 A"]
+[-1.5289344787597656, 8.37374496459961, "Diode Driver Voltage ~28 VDC"]
+[-1.402741551399231, 8.225893020629883, "Diode Driver Frequency 10 kHz"]
+[-1.3336327075958252, 8.164371490478516, "Diode Driver Rise and Fall Times \u00b5s class"]
+[-1.2725467681884766, 8.103482246398926, "Diode Driver Efficiency 85%"]
+[1.5203214883804321, 21.234975814819336, "Instrument Mass 298 kg"]
+[1.6291402578353882, 23.216293334960938, "Instrument Power Consumption 300 W"]
+[2.7122244834899902, 22.23870849609375, "Instrument Data Importance Far more interesting scientifically"]
+[2.737595319747925, 22.10447883605957, "Instrument Data Importance Far more interesting scientifically than the data from SAR"]
+[2.7575926780700684, 22.148183822631836, "Instrument Data Importance Far more interesting scientifically than the data from SAR"]
+[2.7080912590026855, -1.316596508026123, "Satellite Data Release Open release of all data to all interested scientists and engineers"]
+[3.7383570671081543, 17.702075958251953, "Payload Component Motion Causes a small but well-defined disturbance of the spacecraft attitude"]
+[0.9869076013565063, 9.162660598754883, "Attitude and Orbit Control System Real-Time Correction Corrects the scan mirror pointing for the expected spacecraft attitude and orbital effects"]
+[6.320973873138428, 7.423086643218994, "Satellite Component Components Scan mechanism assembly, telescope, aft optics, cooler assembly with cooled detectors, detector heads for un-cooled channels, preamplifiers, and view-port sunshade"]
+[2.7100794315338135, 22.191505432128906, "Instrument Objective Ultra-precise satellite-to-satellite tracking in low-low orbit"]
+[2.273937225341797, 22.191587448120117, "Instrument Measurement Method Dual One Way Ranging (DOWR)"]
+[-5.506021022796631, 9.457944869995117, "Radio Frequency Frequency About 24 GHz"]
+[-5.51560640335083, 9.42655086517334, "Radio Frequency Frequency Near 32 GHz"]
+[2.2016332149505615, 22.937976837158203, "Instrument Frequency Ratio Exact 3-to-4 ratio"]
+[2.075315237045288, 22.506845474243164, "Instrument Range Measurement To the \u00b5m level"]
+[0.4982171654701233, 9.423689842224121, "Attitude Determination Device Mass < 0.5 kg"]
+[0.439502090215683, 9.495758056640625, "Attitude Determination Device Field of View 8\u00ba x 8\u00ba"]
+[0.49203068017959595, 9.428400993347168, "Attitude Determination Device Pointing Accuracy (Yaw and Pitch Axis) 30 arcsec (3\u03c3)"]
+[0.5072106122970581, 9.453020095825195, "Attitude Determination Device Pointing Accuracy (Roll Axis) 0.2\u00ba (3\u03c3)"]
+[-4.836526870727539, 9.705368995666504, "Test Receiver Purpose Verify the acquisition, tracking and noise characteristics of all Galileo signals"]
+[-4.852062225341797, 9.713584899902344, "Test Receiver Signal Tracking Capacity 4 general Galileo signals + 1 wideband AltBOC (Alternate Binary Offset Carrier) signal + 9 GPS satellites (L1+L2)"]
+[0.5943280458450317, 12.205931663513184, "Sensor Nadir Visual Imaging Resolution 0.55 km during daytime and 3.7 km at night"]
+[0.5497695207595825, 12.197447776794434, "Sensor Infrared Subsystem Resolution 3.7 km at the surface day and night"]
+[1.4589349031448364, 5.397940158843994, "Spacecraft Bus Data Transmission Encrypted S-band digital data links"]
+[-0.05664660036563873, 15.179882049560547, "Energy Analyzer Bias Voltage Typically < 10 V"]
+[-0.0370219349861145, 15.352995872497559, "Energy Analyzer Entrance Slit Horizontal from the upper (lower) left"]
+[-0.013136574998497963, 15.23473072052002, "Energy Analyzer Exit Slit Circular cylinder section with vertical axis passing through the entrance slit"]
+[-0.9268285036087036, 6.7607245445251465, "Process Frequency Monthly"]
+[-0.9258051514625549, 6.760707855224609, "Process Main Outcome Acquisition plan"]
+[-0.9253387451171875, 6.766524314880371, "Process Number of Sub-Processes 5"]
+[-0.9143829345703125, 6.754691123962402, "Process Principle Transparency"]
+[-1.9221241474151611, 6.931457042694092, "Software Purpose Perform stray light analysis"]
+[-1.3416200876235962, 6.91175651550293, "Model Purpose Stray light analysis"]
+[-13.861217498779297, -2.2566094398498535, "X-ray Telescope Sensitivity Detecting the highest-energy X-rays"]
+[1.6524652242660522, -1.7798030376434326, "Satellite Ground Range Resolution Stable"]
+[1.6042157411575317, -2.1968612670898438, "Satellite Azimuth Resolution Stable"]
+[1.9660089015960693, -1.5366997718811035, "Satellite Noise Levels Stable and consistent with reported levels"]
+[1.8186229467391968, -1.5311393737792969, "Satellite Noise Levels Within approximately 1 dB of the calibrated noise level of each pulse"]
+[3.505786657333374, 13.468379020690918, "Laser System Energy 250-900 \u00b5J"]
+[3.525247097015381, 13.480184555053711, "Laser System Pulse rate 10 kHz"]
+[3.505040407180786, 13.48615550994873, "Laser System Divergence <130 \u00b5rad"]
+[3.541595697402954, 13.504457473754883, "Laser System Wavelength 532.272 nm"]
+[3.5207719802856445, 13.47907543182373, "Laser System Linewidth <30 pm"]
+[3.522043228149414, 13.476420402526855, "Laser System Efficiency >5%"]
+[3.514296770095825, 13.497984886169434, "Laser System Operational run-time 3.5 years"]
+[-5.868679523468018, 16.00967025756836, "Synthetic Aperture Radar Frequency Band L-band"]
+[2.9384350776672363, -2.021501302719116, "Satellite Development Status Unknown"]
+[5.139587879180908, -4.550584316253662, "Satellite Conference Date Sept. 20-23, 2010"]
+[-1.6104315519332886, 1.4783481359481812, "Data Relay Transponder Uplink Frequency 402.75\u00b10.1 MHz"]
+[-1.6096322536468506, 1.4781866073608398, "Data Relay Transponder Downlink Center Frequency 4506.05 MHz"]
+[-1.5761393308639526, 1.4208420515060425, "Data Relay Transponder Polarization L-V LHCP"]
+[2.2673017978668213, -1.3102174997329712, "Satellite Aided Search & Rescue Uplink Frequency 406.05 MHz"]
+[2.4555675983428955, -1.3242279291152954, "Satellite Aided Search & Rescue Downlink Center Frequency 4507 MHz"]
+[2.4050164222717285, -1.2667332887649536, "Satellite Aided Search & Rescue Polarization L-V LHCP"]
+[-0.4879594147205353, 5.853865146636963, "Unknown Uplink Frequency 4781 MHz"]
+[-0.48331332206726074, 5.864462852478027, "Unknown Downlink Frequency 4798 MHz"]
+[-2.877393960952759, 6.788177013397217, "Profile float Quantity ~300/day"]
+[-2.810072422027588, 6.751112937927246, "Profile float Distribution Ocean-wide"]
+[-2.8616864681243896, 6.806069374084473, "Profile float Min. Depth 5 m"]
+[-2.9787099361419678, 6.795313835144043, "Profile float Latency 1 day"]
+[-0.6098122000694275, 5.4459357261657715, "Mooring Quantity ~70 with salinity"]
+[-0.602340579032898, 5.44563627243042, "Mooring Distribution Tropical Pacific"]
+[-0.6139258742332458, 5.3916449546813965, "Mooring Min. Depth 1 m"]
+[-0.6208175420761108, 5.428844451904297, "Mooring Latency 1 day"]
+[-0.6190463304519653, 5.42423152923584, "Mooring Quantity 15"]
+[-0.6245824098587036, 5.407706260681152, "Mooring Distribution Tropical Atlantic"]
+[-0.620067834854126, 5.40266752243042, "Mooring Min. Depth 1 m"]
+[-0.6235234141349792, 5.4196319580078125, "Mooring Latency 1 day"]
+[-1.6232463121414185, 11.217501640319824, "Surface drifter Latency 2 months"]
+[-2.7808310985565186, 4.95021390914917, "Hull-mounted Min. Depth 5 m"]
+[-2.823948860168457, 4.849135398864746, "Hull-mounted Latency 2 days"]
+[-2.846829414367676, 6.877511501312256, "CTD profile Min. Depth 1 m"]
+[2.5212502479553223, -1.5279253721237183, "Satellite Real-Time Data Broadcast Equipped Department of Defense (DoD) direct readout sites"]
+[2.657289505004883, -2.005424976348877, "Satellite Telemetry Downlink EGS Operations Center"]
+[0.4703301787376404, 12.160865783691406, "Sensor Orbit Sun-synchronized 833 km"]
+[0.46038979291915894, 12.255486488342285, "Sensor Horizontal Resolution Less than 30 km for the 10 GHz channel"]
+[0.8430050015449524, 11.976594924926758, "Sensor Channel Set Unknown"]
+[1.695022463798523, 6.941823959350586, "Communication Device Bandwidth 25 kHz"]
+[1.690665364265442, 6.9341278076171875, "Communication Device Bandwidth 46 kHz"]
+[1.6590543985366821, 6.9665207862854, "Communication Device Bandwidth 100 kHz"]
+[1.7215864658355713, 6.938579559326172, "Communication Device Transmitter Power 8 W"]
+[1.7173051834106445, 6.90753698348999, "Communication Device Mass 24 kg"]
+[1.730419397354126, 6.912911891937256, "Communication Device Size 0.034 m3"]
+[1.7441786527633667, 6.944531440734863, "Communication Device Power 53 W"]
+[-2.774606704711914, 7.9117817878723145, "Processor Max Bandwidth 80 kHz"]
+[-2.763336181640625, 7.904208183288574, "Processor Storage Capacity 324 kbit"]
+[-2.7966136932373047, 7.904496192932129, "Processor Output Data Rate 2.4 kbit/s"]
+[-2.7325594425201416, 7.9005961418151855, "Processor Mass 27.5 kg"]
+[-2.7393693923950195, 7.914917945861816, "Processor Size 0.034 m3"]
+[-2.7150936126708984, 7.89205265045166, "Processor Power 33 W"]
+[-0.3327377736568451, 4.9139299392700195, "Ocean Temperature Cool"]
+[-0.3215031325817108, 4.918166160583496, "Ocean Pressure Low"]
+[-0.26148170232772827, 4.7081475257873535, "Ocean Sky Condition Cloudy"]
+[-0.31046468019485474, 4.889788627624512, "Ocean Ice Spread Slowed"]
+[-3.136883497238159, 5.351970672607422, "Snow Vehicles Tow Capacity Unknown"]
+[-1.111845850944519, 7.263928413391113, "Equipment Dimensions 8 feet wide and 60 feet long"]
+[11.07144546508789, 5.238976955413818, "CubeSat Mass Unknown"]
+[11.092547416687012, 5.2608256340026855, "CubeSat Mass Unknown"]
+[11.077280044555664, 5.246328830718994, "CubeSat Mass Unknown"]
+[11.082050323486328, 5.2541937828063965, "CubeSat Mass Unknown"]
+[11.077898979187012, 5.229224681854248, "CubeSat Mass Unknown"]
+[11.132406234741211, 5.300037860870361, "CubeSat Mass Unknown"]
+[11.072686195373535, 5.239202499389648, "CubeSat Mass Unknown"]
+[11.087027549743652, 5.253851890563965, "CubeSat Mass Unknown"]
+[11.003011703491211, 5.168201446533203, "CubeSat Mass Unknown"]
+[11.043179512023926, 5.2090678215026855, "CubeSat Mass Unknown"]
+[11.069109916687012, 5.232669830322266, "CubeSat Mass Unknown"]
+[11.066614151000977, 5.231129169464111, "CubeSat Mass Unknown"]
+[0.9403744339942932, -4.24735689163208, "Remote Sensing Satellite Mass 250 kg"]
+[1.0589429140090942, -4.332565784454346, "Satellite Mass 80 kg"]
+[0.9764916896820068, -4.40493631362915, "Satellite Mass 3 kg"]
+[-2.4706485271453857, 13.065329551696777, "Multispectral Imager Bands 16"]
+[-2.4625234603881836, 13.078936576843262, "Multispectral Imager VIS Bands Wavelength 0.47 \u00b5m & 0.64 \u00b5m"]
+[-2.46870756149292, 13.066503524780273, "Multispectral Imager IR Bands Wavelength 0.86 \u00b5m to 13.3 \u00b5m"]
+[-2.471450090408325, 13.068641662597656, "Multispectral Imager IGFOV at Nadir for Broadband Visible 0.5 km"]
+[-2.454989194869995, 13.08642292022705, "Multispectral Imager IGFOV at Nadir for SWIR 1.0 km"]
+[-2.472318410873413, 13.073266983032227, "Multispectral Imager IGFOV at Nadir for MWIR and TIR 2.0 km"]
+[-2.46722412109375, 13.0805025100708, "Multispectral Imager CONUS Sector Area 5000 km x 3000 km"]
+[-2.50022292137146, 13.043601989746094, "Multispectral Imager Mesoscale Sector Area 1000 km x 1000 km"]
+[3.6332221031188965, 13.217491149902344, "Laser Power 2 watts"]
+[3.6010079383850098, 13.282814025878906, "Laser Operating Spectrum Near-infrared"]
+[3.6219422817230225, 13.272271156311035, "Laser Size About half the volume of a typical shoe box"]
+[3.5240254402160645, 13.388322830200195, "Laser Receiver Sensitivity Few hundreds of picowatts"]
+[3.5907351970672607, 13.257962226867676, "Laser Beam Spread About 20 km"]
+[-0.8287310004234314, 6.919869899749756, "Count Total 23104"]
+[-0.8378034234046936, 6.885305881500244, "Count Total 2048"]
+[-0.8357847929000854, 6.902710914611816, "Count Total 1883"]
+[-0.8547189831733704, 6.863808631896973, "Count Total 4239"]
+[-0.8307746648788452, 6.892418384552002, "Count Total 95"]
+[-0.8438652157783508, 6.888901233673096, "Count Total 31369"]
+[0.6121770143508911, 12.301101684570312, "Sensor Size 3 cm x 3 cm x 1.2 cm"]
+[0.4317527115345001, 12.15876579284668, "Sensor Field of View \u00b160\u00ba"]
+[0.5272123217582703, 12.284272193908691, "Sensor Angle Accuracy < 0.15\u00ba"]
+[-4.405867576599121, 7.390974998474121, "Data Transmission System Mean Availability >95%"]
+[-1.9175145626068115, 8.121582984924316, "System Functions Completeness checks for constituting blocks and DCP address recognition, Storing of DCP messages and processing information onto a database, Monitoring of reporting DCPs with respect to a predefined schedule (check of transmission chain), A log of received and processed messages, including anomalies, Processing of DCP data and bulletin preparation for distribution, Archiving of DCP data, Retrieval for DCP users, Generation/storage of performance analysis"]
+[0.5530298352241516, 9.428763389587402, "Attitude Determination and Control System Quantity 100-SP(O) wheels"]
+[0.7019699811935425, 11.979451179504395, "Sensors Quantity 4"]
+[-4.520456790924072, 12.088032722473145, "Magnetometer Quantity 2"]
+[-0.9138944149017334, 8.72872543334961, "Gyros Quantity 2"]
+[-4.359687328338623, 0.1967872679233551, "Space GPS Receiver Quantity 1"]
+[-2.362046003341675, 7.30332612991333, "OnBoard Computer Quantity 1"]
+[-5.381045818328857, 8.661688804626465, "RF Communications Quantity 2"]
+[-2.5332181453704834, 9.315204620361328, "Power Distribution Module Quantity 2"]
+[-2.7863075733184814, 9.310776710510254, "Battery Control Module Quantity 3"]
+[-2.629713773727417, 9.612349510192871, "Power Source Quantity 3"]
+[-2.558284282684326, 9.676338195800781, "Power Source Quantity 1"]
+[-1.676446795463562, 9.72410774230957, "Propulsion Quantity 1"]
+[-1.543605923652649, 9.602093696594238, "Propulsion Quantity 2"]
+[-1.610337495803833, 9.682315826416016, "Electric Propulsion Payload Quantity 1"]
+[6.327140808105469, 7.411706447601318, "Satellite Component Data Collection Global (except in polar areas due to ISS orbit)"]
+[6.297607898712158, 7.431002616882324, "Satellite Component Latency Fewer than 5 minutes"]
+[6.20937967300415, 7.488611221313477, "Satellite Component Data-Handling Time Only a few tenths of a second"]
+[6.335452079772949, 7.393207550048828, "Satellite Component Data-Streaming Latency Below 1.5 seconds"]
+[6.635059833526611, 7.074342727661133, "Satellite Component Update Intervals Unknown"]
+[3.6095805168151855, 22.24179458618164, "Instrument Component Function Integrates a large spectralon sunlight diffuser"]
+[-3.267282485961914, 4.261082172393799, "Spacecraft Autonomy Period Up to 15 days"]
+[-0.0015156317967921495, -1.977786660194397, "Satellite Operation Data Transmission 1.6 TB per orbit"]
+[-0.006650874856859446, -1.9857732057571411, "Satellite Operation Swath 290 km"]
+[-0.008876664564013481, -1.987526535987854, "Satellite Operation Spatial Resolution As high as 10 m"]
+[-0.9539822340011597, 6.454168796539307, "Documentation Author Herbert J. Kramer"]
+[-0.9610257148742676, 6.480362415313721, "Documentation Publisher Springer Verlag"]
+[-0.9420655965805054, 6.459859848022461, "Documentation Edition 4th edition"]
+[-0.8695679903030396, 6.143858432769775, "Website Contact Email eoportal@symbios.space"]
+[-0.9101502299308777, 6.170019149780273, "Website Copyright Year 2024"]
+[-4.364565372467041, 0.1971709132194519, "GPS Receiver Channels 16 dual frequency channels (equal to 48 single channels)"]
+[-4.364190101623535, 0.19240780174732208, "GPS Receiver Frequency Band GPS L1: 1575.42 MHz, GPS L2: 1227.6 MHz"]
+[-4.360464572906494, 0.1966586410999298, "GPS Receiver Observables L1CA, L1P & L2P code phase, L1CA & L2P carrier phase, Instantaneous Doppler, Time measurements"]
+[-4.357710361480713, 0.19904766976833344, "GPS Receiver Use Real-time orbit determination, Use of GPS C/A signal observations and navigation messages"]
+[-4.941452980041504, 9.78154468536377, "Receiver Missions OceanSat-2 of ISRO, SAC-D of CONAE and NASA, Megha Tropiques of ISRO and CNES"]
+[4.309306621551514, -2.6750388145446777, "Satellite Image Coverage Time 5 days"]
+[1.4644330739974976, -3.1536624431610107, "Satellites Launch Date 2020/2021"]
+[0.5024343132972717, 4.548227787017822, "Natural Phenomenon Rank 12th-Lowest on Record"]
+[0.4825476408004761, 4.524134635925293, "Natural Phenomenon Date 23 September 2021"]
+[0.5012012124061584, 4.5001068115234375, "Natural Phenomenon Date 19 April 2021"]
+[0.4726984202861786, 4.519441604614258, "Natural Phenomenon Date 6 January 2021"]
+[2.9607224464416504, -1.457105278968811, "Satellite Mission Observation of ultra-fast winds from supermassive black holes"]
+[2.9943974018096924, -1.443968415260315, "Satellite Mission Observation of ultra-fast winds from supermassive black holes"]
+[0.6795532703399658, 4.11677885055542, "Atmospheric Region Dominant Dynamics Interaction with charged particles"]
+[0.6733474731445312, 4.1047515869140625, "Atmospheric Region Density Ratio 1/1000th the neutral species"]
+[-3.59800124168396, 12.77502727508545, "Charged Particles Effect on Neutrals Exert both a frictional drag and a frictional heating on the neutrals"]
+[-4.462541580200195, 8.300345420837402, "MEO Local User Terminal Photo Image credit: ESA"]
+[-4.497569561004639, 8.276123046875, "MEO Local User Terminal Accuracy 2\u20135 km"]
+[-4.467869758605957, 8.282809257507324, "MEO Local User Terminal Number of Antennas 4"]
+[-4.489360809326172, 8.27691650390625, "MEO Local User Terminal Network Configuration Networked to share raw data"]
+[-4.464639663696289, 8.277689933776855, "MEO Local User Terminal Detection Time Unprecedented"]
+[-5.018675327301025, 2.859781503677368, "Space Telescope Launch Date 2026"]
+[-4.993892192840576, 2.8816471099853516, "Space Telescope Number of Telescopes 26"]
+[-4.98322057723999, 2.8847436904907227, "Space Telescope Consortium Lead DLR Institute of Planetary Research"]
+[-4.972593784332275, 2.852355480194092, "Space Telescope Payload Operations Start Date 2025"]
+[-5.006155967712402, 2.889662027359009, "Space Telescope Launch Vehicle Soyuz 2-1b rocket"]
+[1.7923915386199951, 6.842834949493408, "Communication Device Performance 5.6 Gbit/s"]
+[-5.5801472663879395, 7.036707878112793, "Communication Link Data Rate 5.6 Gbit/s"]
+[-3.210967540740967, 16.221935272216797, "Radar Scatterometer Wind Velocity 2 m/s, 3 - 20 m/s, 20 - 30 m/s"]
+[-3.2618637084960938, 16.255542755126953, "Radar Scatterometer Wind Direction 20\u00ba (rms), 3 - 30 m/s"]
+[-3.2344343662261963, 16.227846145629883, "Radar Scatterometer Spatial Resolution 25 km"]
+[-3.2745895385742188, 16.263214111328125, "Radar Scatterometer Location Accuracy 25 km (rms), absolute 10 km (rms)"]
+[-3.249924898147583, 16.23833465576172, "Radar Scatterometer Coverage 90% of ice-free ocean surface every two days"]
+[-3.253422260284424, 16.24554443359375, "Radar Scatterometer Instrument Mass 280 kg"]
+[-3.294304132461548, 16.268991470336914, "Radar Scatterometer Instrument Power 240 W"]
+[8.955636978149414, 8.511723518371582, "Satellite Payload Frequency 406.025 MHz"]
+[8.955946922302246, 8.511412620544434, "Satellite Payload Location Accuracy Within 2 km"]
+[8.95559024810791, 8.511821746826172, "Satellite Payload Global Coverage Yes"]
+[8.956050872802734, 8.513107299804688, "Satellite Payload User Identification Yes"]
+[8.954422950744629, 8.513099670410156, "Satellite Payload Old Frequency 121.5 MHz"]
+[1.6156206130981445, 23.227664947509766, "Instrument Power Consumption 45 W"]
+[1.5221585035324097, 21.23939323425293, "Instrument Mass 48.5 kg"]
+[1.6620383262634277, 22.17145347595215, "Instrument Reflector Dimensions 61 cm x 66 cm"]
+[2.7333223819732666, 22.448884963989258, "Instrument Feed Horn Type Corrugated broadband seven-port horn"]
+[2.881927490234375, 22.426069259643555, "Instrument Subsystems Radiometers, digital data subsystem, mechanical scanning subsystem, and power subsystem"]
+[-2.7795510292053223, 11.507438659667969, "Pushbroom Imager GSD 15 m"]
+[-2.7628965377807617, 11.53573226928711, "Pushbroom Imager Spectral Range 400-1000 nm"]
+[-2.7366576194763184, 11.545055389404297, "Pushbroom Imager Bands 138"]
+[-2.7620651721954346, 11.56063175201416, "Pushbroom Imager SNR > 100"]
+[-2.787881374359131, 11.497011184692383, "Pushbroom Imager Mass ~ 10 kg"]
+[-3.337979793548584, 4.337769508361816, "Spacecraft Launch Date Unknown"]
+[-0.8674007654190063, 6.139895439147949, "Website Contact Email eoportal@symbios.space"]
+[-0.949613630771637, 6.177762985229492, "Website Copyright Year 2024"]
+[7.241028308868408, 12.386829376220703, "Satellite Instrument Purpose Study the upper atmosphere and the impact of space weather on Earth"]
+[7.298232555389404, 12.421353340148926, "Satellite Instrument Integration Location Airbus Defence and Space in Toulouse, France"]
+[7.453286647796631, 12.58989143371582, "Satellite Instrument Arrival Date January 4, 2017"]
+[2.740586519241333, -1.9413224458694458, "Satellite Bathymetry Models Unknown"]
+[2.6651949882507324, -1.9303334951400757, "Satellite Bathymetry Models Unknown"]
+[0.9166530966758728, 0.8993208408355713, "Earth Observation Image URL: https://earthobservatory.nasa.gov/images/148230/sizing-up-remote-lakes"]
+[-1.1040023565292358, 6.522826671600342, "Survey Completion Date 3 March 2021"]
+[-0.44492781162261963, 6.789891242980957, "Test Equipment Purpose Environment test"]
+[-0.41348856687545776, 6.766834259033203, "Test Equipment Purpose Functional test"]
+[-5.251144886016846, 7.750977993011475, "Distributed Network Architecture Type Proof-of-concept test"]
+[16.89586639404297, 6.857589244842529, "Microsatellite Objective Develop and demonstrate an onboard micro-propulsion system"]
+[16.880966186523438, 6.8381733894348145, "Microsatellite Potential Use Future precise attitude control of a nanosatellite"]
+[4.3874969482421875, -2.694039821624756, "Satellite Observation Duration About two hours"]
+[4.364460468292236, -2.7520718574523926, "Satellite Typical Observation Duration Six to eight hours"]
+[5.011166095733643, -4.34603214263916, "Satellite Observation Date Dec. 29, 2020"]
+[-13.970850944519043, -2.282137632369995, "X-ray Optics Based on Single spider scheme"]
+[-14.013659477233887, -2.330432891845703, "X-ray Optics Diameter 50 to 150 mm"]
+[-13.990427017211914, -2.317046642303467, "X-ray Optics Mirror Shell Thickness 250 \u00b5m"]
+[-13.970895767211914, -2.2756810188293457, "X-ray Optics Number of Shells Seven sets of 28 nested shells"]
+[-13.966242790222168, -2.2909228801727295, "X-ray Optics Mirror Coating Ultra-thin layers of reflective iridium coating"]
+[-13.992036819458008, -2.2929372787475586, "X-ray Optics Coating Smoothness 0.5 nanometers"]
+[3.738959789276123, 17.709064483642578, "Payload Resource Impact Low"]
+[3.703338146209717, 17.676109313964844, "Payload Operating Modes Dependent on solar activity and position in the orbit"]
+[3.724397659301758, 17.70682716369629, "Payload Power Consumption > 650 W peak"]
+[3.7331535816192627, 17.711639404296875, "Payload Data Generation Up to 5 GB per orbit"]
+[-5.290975570678711, 7.913830757141113, "Communication System Latitude Limit \u00b120\u00ba about the equatorial plane"]
+[-5.281144618988037, 7.831021308898926, "Communication System Duration Limit Less than 30 minutes"]
+[0.1944536715745926, 7.17252779006958, "Experiment Resource Requirement Downlink of data generated from ACE"]
+[-1.217984676361084, 12.463029861450195, "Electron-Emitting Film Purpose Mitigation of spacecraft charging"]
+[-1.1718716621398926, 12.503217697143555, "Electron-Emitting Film Operation Electrons are emitted from the conductor surface"]
+[-0.9102325439453125, 12.13318157196045, "Surface Charging Monitor Measurement Insulator surface potential"]
+[0.9848217964172363, -4.35270357131958, "Satellite Mass 295 kg"]
+[1.1533949375152588, -0.9346233010292053, "Satellite Radius 212 mm"]
+[2.2622487545013428, -2.530644178390503, "Satellite No of CCRs 303"]
+[0.870988667011261, -2.14298152923584, "Satellite Mass-to-surface ratio relative to LAGEOS 1.5"]
+[1.393945574760437, -1.0044522285461426, "Satellite Computed optical cross-section 3.92 x 10^6 m^2"]
+[1.525194525718689, -1.0468833446502686, "Satellite Measured optical cross-section 2.7 x 10^6 m^2"]
+[2.2948737144470215, -2.6316041946411133, "Satellite Budget Cap $68 M plus launch vehicle costs"]
+[4.822018623352051, -2.5160045623779297, "Satellite Project Go-ahead Implementation Time 28 months"]
+[5.3912248611450195, -4.439484119415283, "Satellite Launch Date June 26, 1978"]
+[5.291777610778809, -4.428408622741699, "Satellite Power Failure Date October 8, 1978"]
+[-0.8268876671791077, 16.4185733795166, "Fourier Transform Spectrometer Spectral Region 665 - 780 cm -1"]
+[-0.8249813914299011, 16.41291618347168, "Fourier Transform Spectrometer Absorption Band CO2"]
+[-0.8439207077026367, 16.416688919067383, "Fourier Transform Spectrometer Application Ozone sounding"]
+[-4.528870105743408, 15.916659355163574, "Onboard Radar Complex Type Radar"]
+[0.23788924515247345, 13.785367012023926, "Calibration Model Purpose Provide a correction to the FLLS data"]
+[0.2942463159561157, 13.817229270935059, "Calibration System Purpose Map the calculated centroid of the imaged beam, in detector coordinates, to the position of the CCRR"]
+[1.666764736175537, -1.233220100402832, "Satellite Radar Measures height"]
+[1.5645650625228882, -1.178070068359375, "Satellite Lidar Measures height"]
+[2.6642816066741943, -1.540805459022522, "Satellite Computer Algorithms Being refined"]
+[1.6796071529388428, -1.6099557876586914, "Satellite Estimates Could be low"]
+[1.4940354824066162, -1.4961150884628296, "Satellite Estimates Could be high"]
+[-0.8509669303894043, 0.1710347980260849, "Satellite System Launch Readiness Capability FY 2015 and FY 2018"]
+[5.264695644378662, -4.134483814239502, "Satellite Launch Date 2016"]
+[5.286626815795898, -4.112064838409424, "Satellite Launch Date 2019"]
+[-0.8394724130630493, 0.16094201803207397, "Satellite System Orbit Afternoon (13:30 hours)"]
+[-0.823724627494812, 0.17743615806102753, "Satellite System Ground System Manager NOAA"]
+[4.076286315917969, 13.926543235778809, "Laser Altimeter System Repetition Rate 10 kHz"]
+[4.095972537994385, 13.937406539916992, "Laser Altimeter System Wavelength 1064 nm"]
+[4.093567371368408, 13.934906005859375, "Laser Altimeter System Pulse Width 6-7 ns"]
+[4.072419166564941, 13.92098331451416, "Laser Altimeter System Energy per Pulse 50 mJ"]
+[4.099850654602051, 13.93331527709961, "Laser Altimeter System Number of Beams 9"]
+[2.671123743057251, -1.2912839651107788, "Satellite Overall Objective Provide high-accuracy global sea level (ocean height) measurements"]
+[2.7185726165771484, -1.6647661924362183, "Satellite Partner Countries USA and France"]
+[2.100900411605835, -2.714632987976074, "Satellite Number of Instruments 7"]
+[0.5884308218955994, -1.4592684507369995, "Satellite Orbit Altitude 600 km"]
+[0.7684407234191895, -2.2369439601898193, "Satellite Orbit Inclination 97.8\u00ba"]
+[3.84275221824646, -3.1139395236968994, "Satellite LTDN 10:30 hours"]
+[4.211665153503418, -2.487938642501831, "Satellite Revisit Time < 8 days"]
+[-3.2450990676879883, 5.436709403991699, "Launch Vehicle Fairing Modified"]
+[1.2623027563095093, -2.8135688304901123, "Small Satellites Deployment Use of 9 ISIPODs of ISIS, 3 XPODs of UTIAS/SFL, 2 PEPPODs of GAUSS, and 1 MRFOD of MSU"]
+[0.627838134765625, 11.881560325622559, "Data-gathering Sensors Purpose Collect critical entry environment and thermal protection performance data"]
+[-3.112236738204956, 4.299314498901367, "Spacecraft MMOD Damage More than the computation models had predicted"]
+[-3.0906295776367188, 4.2223734855651855, "Spacecraft MMOD Unseen threat that all spacecraft need to be protected from"]
+[2.4870755672454834, 22.283567428588867, "Instrument Optics Korsch telescope with a TMA design in SiC"]
+[1.7747689485549927, 22.234525680541992, "Instrument Aperture Diameter 200 mm"]
+[2.0936450958251953, 22.60099220275879, "Instrument Spectral Band (Pan) 0.45-0.9 \u00b5m"]
+[2.0704140663146973, 22.616178512573242, "Instrument Spectral Band (MS B1) 0.45-0.52 \u00b5m"]
+[2.062234401702881, 22.652851104736328, "Instrument Spectral Band (MS B2) 0.53-060 \u00b5m"]
+[2.0824673175811768, 22.618408203125, "Instrument Spectral Band (MS B3) 0.62-0.69 \u00b5m"]
+[2.0650150775909424, 22.654054641723633, "Instrument Spectral Band (MS B4) 0.76-0.89 \u00b5m"]
+[1.9021282196044922, 22.293033599853516, "Instrument GSD 1.5-2.5 m"]
+[1.8563734292984009, 22.23192596435547, "Instrument Pan at nadir 6-10 m"]
+[2.6578807830810547, 22.33667755126953, "Instrument Detectors Silicon area array with 7000 pixels Pan, 1750 pixels in each MS band"]
+[2.661761999130249, 22.490976333618164, "Instrument TDI The Pan band offers TDI services for SNR improvement of the signal"]
+[1.6770572662353516, 21.954687118530273, "Instrument Swath Width 17.5 km at nadir"]
+[2.3902769088745117, 22.523387908935547, "Instrument FOR \u00b130\u00ba"]
+[2.4649343490600586, 22.593482971191406, "Instrument Data Quantization 12 bit (10 bit coding for downlink)"]
+[1.529468059539795, 21.250354766845703, "Instrument Mass 18.5 kg"]
+[1.5454646348953247, 21.254629135131836, "Instrument Camera Mass 13 kg"]
+[0.5484748482704163, 12.0940523147583, "Sensor Measurement Capability Acoustic waves propagating through the satellite structure"]
+[-1.1355334520339966, 9.379861831665039, "Cold-Gas Microthruster Thrust Range Up to 560 \u00b5N"]
+[-1.0898869037628174, 9.427977561950684, "Cold-Gas Microthruster Total Mass 0.835 kg"]
+[-1.0568199157714844, 9.321479797363281, "Cold-Gas Microthruster Throat Dimension 0.02 mm diameter"]
+[-1.8437747955322266, 12.158316612243652, "Infrared Camera Mass ~ 3 kg"]
+[-1.829000473022461, 12.17667007446289, "Infrared Camera Off-nadir Angle 30\u00ba"]
+[-1.8501367568969727, 12.168086051940918, "Infrared Camera Mission Targets Wildfires, volcanoes, heat island phenomena"]
+[-1.8249118328094482, 12.15853500366211, "Infrared Camera Technology Uncooled infrared array detector (microbolometer)"]
+[-5.2583184242248535, 7.949502944946289, "Telecommunications System Use Case Maintain communications during natural disasters"]
+[4.096353530883789, 13.93392562866211, "Laser Altimeter Pulse Rate 10,000 pulses of light a second"]
+[4.103522777557373, 13.935281753540039, "Laser Altimeter Precision Within an inch"]
+[4.098991870880127, 13.931265830993652, "Laser Altimeter Data Collection Tracks of ICESat-2 measurements from 2019"]
+[4.100291728973389, 13.93298053741455, "Laser Altimeter Data Analysis Model to convert volume change to mass change"]
+[-3.126535415649414, 1.7147328853607178, "Satellite Mission Groundwater Monitoring Global"]
+[-3.1149542331695557, 1.7010276317596436, "Satellite Mission Data Resolution High-resolution"]
+[-3.1739401817321777, 1.681811809539795, "Satellite Mission Drought Information Soil moisture, crop health, groundwater, streamflow"]
+[1.5564621686935425, -1.1710528135299683, "Satellite Resolution 2.5 m for the panchromatic band, and 10 m in four multispectral bands"]
+[1.32333242893219, -1.5060043334960938, "Satellite Swath 17.5 swath"]
+[1.3977527618408203, -2.063908100128174, "Satellite Pointing Modes Sun pointing (heliocentric pointing) or toward Earth (geocentric pointing)"]
+[0.8136997818946838, -2.2044014930725098, "Satellite Solar Array Rotation ~ 0.025 \u00ba/s rotation about its \u2013X-axis"]
+[1.514271855354309, -2.2158820629119873, "Satellite Maneuvers Reach \u00b130\u00ba either being in along-track or in cross-track"]
+[-5.397259712219238, 2.769545316696167, "Telescope Data Transfer L0 to L1"]
+[2.7984514236450195, 22.477170944213867, "Instrument Data Collection Within the cusp"]
+[-3.123497247695923, 2.1762545108795166, "Missions Measurement Location Dayside magnetopause"]
+[-1.5097239017486572, 13.405006408691406, "Solar Array Efficiency Higher than existing arrays"]
+[-1.500986933708191, 13.422733306884766, "Solar Array Number of Arrays 6"]
+[-2.738521099090576, 8.708060264587402, "Module Addition Date 2024"]
+[-0.9642114639282227, 8.729720115661621, "Cooler System Design Linear pulse tube cold head that is integral to the compressor assembly and a coaxial remote pulse tube cold head"]
+[-1.6922874450683594, 8.589678764343262, "Thermo-Dynamic Units Quantity 2"]
+[-0.8864350914955139, 8.728293418884277, "Cooler Control Electronics Quantity 2"]
+[3.709367513656616, 17.68402099609375, "Payload Launch Date 25 January 2018"]
+[2.742694616317749, -3.2544782161712646, "Communication Satellite Manufacturer Airbus DS"]
+[-3.267139196395874, 5.4276123046875, "Launch Vehicle Launch Complex ELA-3 in Kourou"]
+[16.915109634399414, 6.80633020401001, "Microsatellite Number of Satellites 60"]
+[16.940885543823242, 6.7985358238220215, "Microsatellite Number of Operational Satellites 17"]
+[6.354569435119629, 7.390312194824219, "Satellite Component Calibration Method Uses the previous net and harpoon experiments"]
+[-1.251878261566162, 7.049026966094971, "Technology Purpose Testing"]
+[-1.2648450136184692, 7.031424522399902, "Technology Purpose Testing"]
+[-3.1366384029388428, 1.690748691558838, "Satellite Mission Observation Timescales Tens of milliseconds to years"]
+[-3.13484787940979, 1.6935324668884277, "Satellite Mission Satellite Position 350 km in front of and behind the Sentinel-1 satellite"]
+[-3.1628687381744385, 1.7506438493728638, "Satellite Mission Flight Formation Approximately 200 - 500 metres apart"]
+[-3.13620924949646, 1.7148348093032837, "Satellite Mission Flight Formation At a distance of 350 km from the Sentinel-1 satellite"]
+[-1.088852882385254, 7.689182758331299, "Device Installation Year 2012"]
+[0.06053667888045311, 7.181048393249512, "Citizen Science Project Components Cities, Stars, Other Objects"]
+[-0.06625057011842728, 7.095746040344238, "Citizen Science Project Task Identify Points in Night Images and Match Them to Positions on Maps"]
+[-0.013956992886960506, 7.146960258483887, "Citizen Science Project Task Identify Cities in Images Encompassing a Circle 310 Miles Around"]
+[-2.6322948932647705, 9.33890438079834, "Power Supply Unknown Unknown"]
+[-0.8095900416374207, 11.54971981048584, "Sub-detector Unknown Unknown"]
+[-8.562135696411133, 13.748254776000977, "Parameter Spatial resolution 25 km"]
+[-8.472046852111816, 13.701116561889648, "Parameter Range of values 3-25"]
+[-8.610549926757812, 13.543109893798828, "Parameter Quantization levels 1"]
+[-8.53093433380127, 13.683091163635254, "Parameter Absolute accuracy \u00b12 m/s"]
+[-8.50887680053711, 13.70270824432373, "Parameter Area covered 25 km"]
+[-8.468589782714844, 13.71191692352295, "Parameter Age 0-100"]
+[-8.501493453979492, 13.678789138793945, "Parameter Edge location \u00b112.5 km"]
+[-8.471120834350586, 13.704838752746582, "Parameter Range of values 0-25"]
+[-8.56567096710205, 13.592082023620605, "Parameter Quantization levels 0.5,10,15,20, \u226525"]
+[-8.47237777709961, 13.70183277130127, "Parameter Range of values 0-1"]
+[-8.565361976623535, 13.600348472595215, "Parameter Quantization levels 0.05"]
+[-8.496916770935059, 13.714259147644043, "Parameter Integrated water vapor 0.1 kg/m 2"]
+[-8.447769165039062, 13.735772132873535, "Parameter Range of values 0-80"]
+[-8.606074333190918, 13.546339988708496, "Parameter Quantization levels 0.10"]
+[-8.56442642211914, 13.608039855957031, "Parameter Integrated water vapor 2.0 kg/m 2"]
+[-8.382802963256836, 13.791744232177734, "Parameter Range of values 0-25"]
+[-8.566130638122559, 13.589646339416504, "Parameter Quantization levels 0.5,10,15,20, \u226525"]
+[-8.525497436523438, 13.759322166442871, "Parameter Range of values 0-60%"]
+[-8.612173080444336, 13.541247367858887, "Parameter Quantization levels 1"]
+[-8.474021911621094, 13.70773983001709, "Parameter Range of values 180-340 K"]
+[-8.61937427520752, 13.534646034240723, "Parameter Quantization levels 1"]
+[-8.504995346069336, 13.721935272216797, "Parameter Range of values 0-50 cm"]
+[-8.613985061645508, 13.539838790893555, "Parameter Quantization levels 1"]
+[-8.479839324951172, 13.708741188049316, "Parameter Range of values 25 km"]
+[-8.607397079467773, 13.546730041503906, "Parameter Quantization levels 12 types"]
+[-8.481054306030273, 13.706025123596191, "Parameter Range of values 0-100%"]
+[-8.6178560256958, 13.537027359008789, "Parameter Quantization levels 1"]
+[-8.560772895812988, 13.71261978149414, "Parameter Absolute accuracy \u00b120%"]
+[4.0757646560668945, 13.928003311157227, "Laser Altimeter System Size About the size of a Smart Car"]
+[4.081814765930176, 13.93236255645752, "Laser Altimeter System Trip Duration Four and a half days"]
+[4.075615882873535, 13.933784484863281, "Laser Altimeter System Trip Distance 2,000 miles"]
+[-0.7514125108718872, 11.596433639526367, "Amplifier and Detector Temperature Control Requirement Maximum change of 0.4\u00ba C (rms) over 7 days"]
+[-1.9262642860412598, 8.08914852142334, "System Fundamental Timing Unit 10 ms"]
+[0.7711729407310486, 11.920886039733887, "Sensors Operation Alternated at a rapid rate"]
+[0.7884294390678406, 11.99310302734375, "Sensors Sampling 7 samples during 120 ms"]
+[-0.16942931711673737, 15.592135429382324, "Spectrometer Spectral Range 350 - 1050 nm"]
+[-0.16208484768867493, 15.575058937072754, "Spectrometer Spectral Resolution 85.4 cm -1 (1.7 nm @ 450 nm)"]
+[-0.1248369887471199, 15.53695297241211, "Spectrometer Number of Usable Spectral Bands 256"]
+[-0.13273948431015015, 15.536177635192871, "Spectrometer FOV (Field of View) 3.0 \u00ba"]
+[0.018054362386465073, 15.612750053405762, "Spectrometer IFOV (Instantaneous Field of View) 0.0058\u00ba or 0.0029\u00ba"]
+[-0.13354596495628357, 15.484126091003418, "Spectrometer Spatial Resolution 28 m x 30 m"]
+[-0.13548776507377625, 15.471908569335938, "Spectrometer Swath Width 7-29 km"]
+[-0.10504575818777084, 15.567132949829102, "Spectrometer Scene Length Range 10 km to 473 km"]
+[-0.13310818374156952, 15.53322982788086, "Spectrometer Instrument Pointing (Control/Knowledge) 0.15\u00ba/0.15\u00ba"]
+[-0.0308370403945446, 15.50728988647461, "Spectrometer Instrument Mass 20.45 kg"]
+[-0.12632766366004944, 15.494406700134277, "Spectrometer Instrument Power 66/60 W (peak/average)"]
+[-0.08981557935476303, 15.53121566772461, "Spectrometer Source Data Rate 20 MByte/s"]
+[-0.16127808392047882, 15.594208717346191, "Spectrometer Spectral Resolution 5 nm"]
+[-0.07937648147344589, 15.558406829833984, "Spectrometer Wavelength Range 1 to 4 \u00b5m"]
+[-2.958051919937134, 4.473826885223389, "Spacecraft Launch Mass 2208 kg"]
+[-3.035991668701172, 4.417026519775391, "Spacecraft Power 2200 W"]
+[-3.017731189727783, 4.25063419342041, "Spacecraft Delta V 100 m/s"]
+[-1.9092758893966675, 8.096736907958984, "System Thrusters 20 x 20 N"]
+[-1.9425818920135498, 8.20936393737793, "System Tank 2 x 96 liter"]
+[-5.195822238922119, 7.8028645515441895, "Communication System X-band Data Rate 26 kbit/s"]
+[-5.153080463409424, 7.831744194030762, "Communication System K-band Data Rate 72 Mbit/s"]
+[1.7006416320800781, 6.946864128112793, "Communication Device Quantity 2 fixed X-band Low Gain, 1 steerable K-band High Gain, 1 steerable X-band Low Gain"]
+[0.9851260185241699, 9.170273780822754, "Attitude and Orbit Control System Stabilization 3 axis stabilized with 4 Reaction Wheels"]
+[-3.777298927307129, 8.047252655029297, "Storage Capacity > 2 TB"]
+[-2.5751569271087646, 9.622557640075684, "Power Source Quantity 3 body mounted and 2 deployable panels"]
+[-6.632610321044922, 9.92096996307373, "Antennas Manufacturer SENER Aeroespacial and CATEC"]
+[-6.667827129364014, 9.945945739746094, "Antennas Technology Metal 3D printing (additive manufacturing)"]
+[-6.6495208740234375, 9.920374870300293, "Antennas Country of Manufacture Spain"]
+[1.2574703693389893, -1.4816744327545166, "Satellite Sky Area Coverage 400 X larger than Kepler"]
+[2.296583652496338, -2.039393424987793, "Satellite Stellar Spectral Types F5 to M5"]
+[-0.7803457975387573, 11.530823707580566, "Observation Target Properties Observed Mass, radius, orbit"]
+[-0.718560516834259, 11.498551368713379, "Observation Target Dynamics Observed Planet-planet interactions, mutual inclinations, moons, tides"]
+[-0.6587043404579163, 11.42365837097168, "Observation Target Atmospheric Composition + Structure Observed Transmission spectrum, emission spectrum, albedo, phase function, clouds, winds"]
+[2.0808606147766113, -2.7738542556762695, "Satellite Number of Satellites 7"]
+[5.228359222412109, -4.166982650756836, "Satellite Operation Start Date November 1977"]
+[5.225352764129639, -4.146283149719238, "Satellite Operation End Date 2017"]
+[-3.199533700942993, 1.643532156944275, "Satellite Mission Purpose Measuring changes in Earth's gravity field, tracking water movement and surface mass changes"]
+[-3.173966407775879, 1.6893914937973022, "Satellite Mission Application Area Monitoring water storage, ice sheets and glaciers, sea level, and solid earth"]
+[-0.09362666308879852, 9.183487892150879, "Navigation System Azimuth Alignment 70 degrees"]
+[-0.10715726763010025, 9.186549186706543, "Navigation System Typical Azimuth Alignment 90 degrees"]
+[-2.3521764278411865, 5.621593475341797, "Flight Path Shift 20-degree to the south"]
+[-3.0775394439697266, 2.451036214828491, "Mission Quality Checks Not detected during the standard quality checks"]
+[-0.4231373369693756, 14.521905899047852, "Imaging Instrument Number of Instruments 1"]
+[-0.4235711097717285, 14.522343635559082, "Imaging Instrument Number of Instruments 1"]
+[0.9025412797927856, 12.198781967163086, "Sensor Number of Instruments 1"]
+[1.3416987657546997, 2.3193070888519287, "Mapper Number of Instruments 1"]
+[2.619926691055298, 22.49827003479004, "Instrument Suite Number of Instruments 1"]
+[2.4130496978759766, 22.78941535949707, "Instrument Number of Instruments 1"]
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+[-5.191110610961914, 7.873262405395508, "Communication Experiment Repeater Mode Data Rate 270 - 1000 Mbit/s"]
+[-5.214264392852783, 7.892385005950928, "Communication Experiment Ground Station Table Mountain facility"]
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+[2.6970443725585938, 14.302324295043945, "Optical Instrument Number of Mirror Systems 7"]
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+[2.5221333503723145, 14.279413223266602, "Optical Instrument Focal Length 2700 mm"]
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+[3.493687391281128, 8.121478080749512, "X-ray Detector Strip Width 550 \u00b5m"]
+[3.484004259109497, 8.11909008026123, "X-ray Detector Inter-strip Distance 75 \u00b5m"]
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+[3.479663848876953, 8.122024536132812, "X-ray Detector Energy Resolution 10% at 14 keV"]
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+[3.4950976371765137, 8.120466232299805, "X-ray Detector Power Consumption 300 W"]
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+[1.0124948024749756, 0.7866665720939636, "Earth Observation Satellite Mission Forest Monitoring"]
+[-0.015412205830216408, 11.338302612304688, "Forest Early Warning System Development Partners JICA (Japan International Cooperation Agency) and JAXA"]
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+[-0.7706233859062195, 8.873668670654297, "Thermal Control System Heat Load Minimization By not allowing any object to come into the FOV of the coolers and incorporating a bi-annual yaw rotation of the spacecraft"]
+[-0.7757978439331055, 8.868298530578613, "Thermal Control System Cooler Face Temperature Achievement 95 K"]
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+[-2.206008195877075, 12.467170715332031, "Ultraviolet Imager Purpose Improve the atmospheric correction accuracy of high turbid water in the near shore"]
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+[-13.922062873840332, -2.235173463821411, "X-ray Space Telescope Mirror Quantity 54 nested gold-coated mirrors each"]
+[-13.951892852783203, -2.302985668182373, "X-ray Space Telescope Camera Cooling Temperature -90\u00b0C"]
+[-5.365682125091553, 2.851195812225342, "Russian Telescope Launch Site Baikonur in Kazakhstan"]
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+[1.5205793380737305, 21.260101318359375, "Instrument Mass 87.5 g"]
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+[2.2190494537353516, 22.679988861083984, "Instrument Performance \u00b10.35\u00ba"]
+[1.487278938293457, 21.198619842529297, "Instrument Mass 40 g"]
+[1.6582170724868774, 23.15216064453125, "Instrument Power 0.2 W"]
+[2.2264864444732666, 22.651948928833008, "Instrument Performance \u00b130 nT"]
+[1.5211584568023682, 21.23855209350586, "Instrument Mass 1.2 kg"]
+[1.6700245141983032, 23.18132781982422, "Instrument Power 6.5 W"]
+[2.6753382682800293, 23.62495231628418, "Instrument Performance 10 arcsec"]
+[1.5201343297958374, 21.23716926574707, "Instrument Mass 225 g"]
+[1.6842504739761353, 23.172779083251953, "Instrument Power 1 W/unit"]
+[2.191180467605591, 22.712356567382812, "Instrument Performance 0-4 Nms"]
+[-5.830483913421631, 15.956852912902832, "Synthetic Aperture Radar Observation Mode High-resolution 10 m mode (dual polarisation)"]
+[-5.947108745574951, 16.118629455566406, "Synthetic Aperture Radar Observation Date July 25, 2017"]
+[-5.8890299797058105, 16.0484619140625, "Synthetic Aperture Radar Observation Image Date 4th August 2017"]
+[-5.869394302368164, 16.021442413330078, "Synthetic Aperture Radar Observation Image Date 1st September 2017"]
+[-5.865626335144043, 16.03201675415039, "Synthetic Aperture Radar Observation Image Date 29th September 2017"]
+[-5.891944885253906, 16.014911651611328, "Synthetic Aperture Radar Flood Proxy Map Area 350 km2"]
+[-5.919433116912842, 16.034318923950195, "Synthetic Aperture Radar Pixel Size About 50 m2"]
+[-4.421386241912842, 15.98547649383545, "Radar Roll Bias Requirement \u00b1 36\u00b0"]
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+[2.5494744777679443, -1.99797523021698, "Satellite Ground Commanding Uploading Steering Coefficients and Bias Commands"]
+[-6.611414909362793, 9.907432556152344, "Antenna System Number of Feeds 19"]
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+[-2.4038736820220947, 9.586926460266113, "Heat Generating Source Maximum Power Output 10.5 W"]
+[-2.357393264770508, 9.553533554077148, "Heat Generating Source Power Output 10.6 W"]
+[-3.1013171672821045, 4.26614236831665, "Spacewalk Tool Attachment Method Off the side of AMS and plug it into the existing system"]
+[-3.154343366622925, 4.1963210105896, "Spacewalk Tool Function Cut into the cooling lines"]
+[-3.116142749786377, 4.2866644859313965, "Spacewalk Tool Function Working on the cooling lines"]
+[-3.1037604808807373, 4.267259120941162, "Spacewalk Tool Function Capture the fasteners the astronauts remove from AMS"]
+[1.1299183368682861, -0.721583902835846, "Satellite Platform Size 10 x 10 x 34 cm"]
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+[0.9891090393066406, -4.385365009307861, "Satellite Mass 3.8 kg"]
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+[2.279937744140625, -2.019063949584961, "Satellite Solar Panels Deployable"]
+[2.481966018676758, -1.2168996334075928, "Satellite Data Collection Autonomously collecting radiometry data"]
+[4.899234294891357, -4.332152366638184, "Satellite Groundwater Storage Measurement Date March 15, 2021"]
+[0.587827742099762, 11.959065437316895, "Sensor Function Find overwatering farms"]
+[-2.5953927040100098, 11.742269515991211, "Imager Image Type Natural color image"]
+[-1.8937970399856567, 8.130197525024414, "System Irrigation Efficiency Threshold 20 percent"]
+[11.847529411315918, 5.331669330596924, "3U CubeSat Objective Increase understanding of the outcomes of relevant collisions among millimeter-sized particles, or \u201cpebbles\u201d, in a protoplanetary disk"]
+[11.702348709106445, 5.387391090393066, "2U CubeSat Mission Education"]
+[11.758591651916504, 5.47207498550415, "3U CubeSat Objective Measure cloud fraction, cloud top height, and cloud top wind"]
+[11.897829055786133, 5.275978088378906, "3U CubeSat Mass 4 kg"]
+[11.845243453979492, 5.329202175140381, "3U CubeSat Data Rate Up to 100 Mbit/s"]
+[11.875059127807617, 5.3180036544799805, "3U CubeSat Objective Investigate the interaction between different materials and the atmospheric flow regime in very low Earth orbits (VLEO)"]
+[-0.0881909430027008, 15.58749008178711, "Spectrometer Spectral Range 0.9-1.7 \u00b5m"]
+[-0.15235455334186554, 15.562748908996582, "Spectrometer Spectral Resolution Approximately 6nm"]
+[-0.09301894158124924, 15.512240409851074, "Spectrometer FOV 0.1\u00ba"]
+[-0.11136992275714874, 15.52868938446045, "Spectrometer Instrument Size 40 mm x 45 mm x 80 mm"]
+[-0.13603663444519043, 15.473222732543945, "Spectrometer Instrument Mass 0.230 kg"]
+[-0.18833287060260773, 15.437479972839355, "Spectrometer Detectors 256 element InGaAs diode arrays"]
+[-0.17921049892902374, 15.57639217376709, "Spectrometer Gratings 12 mm x 12 mm plane gratings, 200 to 600 g/mm"]
+[-0.11582576483488083, 15.571992874145508, "Spectrometer Electronics 8 bit microprocessor with 12 bit ADC, 3.6-4.2 V, input rail 250-1000 mA"]
+[0.00048064315342344344, 15.602765083312988, "Spectrometer Integration Time 100 \u00b5s to 8 s"]
+[0.0023771098349243402, 15.63769817352295, "Spectrometer Volatiles Less than 0.1% volatile internals by mass"]
+[6.349123001098633, 7.394909381866455, "Satellite Component Configuration Harpoon mounted at the top and the deployable boom at the bottom"]
+[6.3166632652282715, 7.383720397949219, "Satellite Component Type Coiled CPFR mono-stable boom"]
+[6.3032450675964355, 7.443100452423096, "Satellite Component Maximum Extension 1.5 m"]
+[6.341139793395996, 7.420254230499268, "Satellite Component Composition Deployer, Projectile and Tether"]
+[0.6817461848258972, -1.1415441036224365, "Satellite Altitude 271.5 km"]
+[2.1881353855133057, 13.378742218017578, "Optical Sensor Purpose Photographing"]
+[-0.4127718210220337, 12.503994941711426, "Atomic Oxygen Monitor Components Atomic Oxygen Fluence Sensor (AOFS) and the Material Degradation Monitor (MDM)"]
+[-4.9448933601379395, 9.800065994262695, "Receiver Malfunction Date Nov. 1, 2004"]
+[-4.9430670738220215, 9.779815673828125, "Receiver Tracking Channels 6"]
+[-4.945742130279541, 9.770734786987305, "Receiver Operating Mode Dual-frequency"]
+[-4.931048393249512, 9.791243553161621, "Receiver Limited Use Duration Approximately the first 16 months in orbit or through January 1994"]
+[-1.4224058389663696, 16.92040252685547, "Altimetry Instrument First Measurement Date 21 August 1992"]
+[5.164274215698242, -4.038936138153076, "Satellite Publication Year 1999"]
+[5.079721450805664, -3.8925857543945312, "Satellite Launch Year 2028"]
+[4.949816703796387, -2.4050822257995605, "Satellite Lifetime 7.5 years"]
+[1.4465057849884033, -2.4047634601593018, "Satellite Orbit 690 km polar orbit"]
+[1.673934817314148, 22.148117065429688, "Instrument Antenna Size 11 m by 3.6 m"]
+[-1.3243310451507568, 6.065593719482422, "Company Contract Value \u20ac482 million"]
+[1.6749639511108398, -1.6804753541946411, "Satellite Sky Coverage 85 percent"]
+[4.323317050933838, -2.722158908843994, "Satellite Sector Observation Time 1 year for southern sky, 1 year for northern sky"]
+[4.737807750701904, -3.9548025131225586, "Satellite Data Release Sectors 1 and 2, observed between July 25 and September 20, 2018"]
+[4.27996301651001, -2.927081823348999, "Satellite Image Capture Time Over the course of 17 hours on July 25"]
+[0.6019237637519836, -1.4324392080307007, "Satellite Comet Distance from Earth About 29 million miles (48 million km)"]
+[-4.319459438323975, 15.798208236694336, "Radar Instrument Orbit 690 km polar orbit"]
+[-6.8256378173828125, 10.074705123901367, "Antenna Size 11 metres by 3.6 metres"]
+[-3.1467578411102295, 1.7339571714401245, "Satellite Mission Lifetime 7.5 years"]
+[7.340306758880615, 12.468138694763184, "Satellite Instrument Data Collection Information collected by the Advanced Baseline Imager (ABI)"]
+[-0.21280784904956818, 15.269856452941895, "Vegetation Measure Ability Can detect subtle seasonal cycles"]
+[0.20087166130542755, 4.564373970031738, "Vegetation Greenness Increase About 10 to 15 percent on average"]
+[-7.3962249755859375, 2.8677592277526855, "Cosmic Ray Detector Repair Completion Date 25 January 2020"]
+[-7.397727966308594, 2.8681702613830566, "Cosmic Ray Detector Publication Date 28 January 2021"]
+[0.721200704574585, -4.153757095336914, "Satellite S/C Mass at Launch 2750 kg"]
+[5.289607524871826, -2.209263801574707, "Satellite Design Life 5 years"]
+[2.359388828277588, -1.3994572162628174, "Satellite Onboard Data Recording Tape recorder (analog)"]
+[2.787835121154785, -2.4117093086242676, "Satellite Imaging Frequency C-band at 5.3 GHz"]
+[1.469578742980957, -1.111454963684082, "Satellite Spatial Resolution of Data 10-100 m"]
+[2.1352219581604004, -1.8660072088241577, "Satellite Polarization HH"]
+[2.516301393508911, -1.6455988883972168, "Satellite Look Direction of SAR Antenna Right"]
+[1.2116289138793945, -0.8373322486877441, "Satellite Ground Antenna Size About 10 m diameter"]
+[1.9888031482696533, -2.108044385910034, "Satellite On-board Location Accuracy Device None"]
+[2.160630941390991, -2.4145824909210205, "Satellite Yaw Steering None"]
+[-14.231040000915527, -2.4661929607391357, "X-ray Telescope Authors M. Pavlinsky, V. Akimov, V. Levin, I. Lapshov, A. Tkachenko, N. Semena, V. Arefiev, A. Glushenko, A. Yaskovich, R. Burenin, S. Sazonov, M. Revnivtsev, M. Buntov, S. Grebenev, A. Lutovinov, M. Kudelin, S. Grigorovich, D. Litvin, V. Lazarchuk, I. Roiz, M. Garin, M. Gubarev, B. Ramsey, K. Kilaru, S. L. O'Dell, R. Elsner"]
+[0.11038251221179962, 7.1595940589904785, "Sub-experiment Module Type Flex-based HDI"]
+[-3.3650758266448975, 4.418181896209717, "Space Technology Research Vehicles Final Report Date August 1995"]
+[16.965917587280273, 6.749690532684326, "Microsatellite Acta Astronautica Publication Date August 1997"]
+[-0.8119701743125916, 7.609028339385986, "Cable Free Length ~ 80 mm"]
+[-0.12939389050006866, 13.63609504699707, "Measurement Nominal Value 65 mm"]
+[-0.9699838757514954, 7.663787364959717, "Device Vibration Robustness Guaranteed"]
+[-1.031746745109558, 7.692893028259277, "Device Flatness Guaranteed"]
+[-0.9709377288818359, 7.808266639709473, "Device CCD Temperature Within Budget"]
+[2.7519948482513428, -1.1901309490203857, "Satellite Aim Provide enhanced meteorological observations and monitoring of land and ocean for weather forecasting and disaster warning"]
+[3.0735161304473877, -1.7001903057098389, "Satellite Owner Indian Space Research Organisation (ISRO)"]
+[1.9205714464187622, -2.1360058784484863, "Satellite Orbit Geostationary"]
+[5.335371971130371, -4.347556114196777, "Satellite Launch Date Early 2018"]
+[1.0965335369110107, -3.944553852081299, "Satellite Ice Loss 600 billion tons"]
+[0.7451831102371216, -1.1343235969543457, "Satellite Sea Level Rise 2.2 millimeters in two months"]
+[1.8292090892791748, -1.5761831998825073, "Satellite Losses Comparison More than double Greenland's 2002-2019 yearly average"]
+[-3.127702236175537, 1.692625641822815, "Satellite Mission Contribution Space Weather Studies"]
+[-3.0960073471069336, 1.645865797996521, "Satellite Mission URL http://www.affects-fp7.eu/helcats-meeting/data/workshop_presentations/"]
+[-3.1237380504608154, 1.676336646080017, "Satellite Mission URL http://m.esa.int/Our_Activities/Space_Engineering_Technology/"]
+[1.911043643951416, 10.72087287902832, "Imaging Device Spectral Range 0.55 \u00b5m - 12.5 \u00b5m"]
+[1.90840744972229, 10.72456169128418, "Imaging Device Spatial Resolution 1 km for VIS and SWIR, 4 km for MWIR, TIR-1 and TIR-2, 8 km for WV"]
+[1.8920518159866333, 10.72531795501709, "Imaging Device IFOV 28 \u00b5rad for VIS and SWIR, 112 \u00b5rad for MWIR, TIR-1, & TIR-2, 224 \u00b5rad for WV"]
+[-2.768723249435425, 14.192456245422363, "Sounder Bands 19 bands, with 18 Infrared(IR) bands, and one visible (VIS) band"]
+[-2.7888901233673096, 14.205658912658691, "Sounder Simultaneous Soundings Four per band"]
+[-2.785754919052124, 14.19188117980957, "Sounder Centre Wavelengths Ranging from 14.71 \u00b5m - 3.74 \u00b5m in the IR bands and 0.695\u00b5m in the VIS band"]
+[-2.771237850189209, 14.183796882629395, "Sounder IFOV 290 \u00b5rad x 280 \u00b5rad"]
+[-2.7779641151428223, 14.194303512573242, "Sounder Spatial Resolution 10 km x 10 km"]
+[2.115110158920288, -0.6240665316581726, "Satellite Power Subsystem More capable"]
+[2.5672364234924316, -1.963145136833191, "Satellite On-board Computer Upgraded"]
+[1.8018065690994263, -1.514651894569397, "Satellite Battery Capacity Better"]
+[1.8651115894317627, -2.111985206604004, "Satellite Attitude Control Subsystem New"]
+[2.521865129470825, -1.5703625679016113, "Satellite Star Tracker Device"]
+[2.0380046367645264, -1.5255836248397827, "Satellite Sensor Payloads Larger"]
+[-1.0763746500015259, 7.698196887969971, "Device Size One inch"]
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+[-1.055949330329895, 7.745434761047363, "Device Polarisation Asymmetry Eliminated"]
+[-1.0934195518493652, 7.657771587371826, "Device Diffraction Pattern Airy pattern"]
+[-1.0313860177993774, 7.768594741821289, "Device Polarisation Effects Reduces the intensity of the central peak of the Airy pattern by approximately a factor of four"]
+[1.5521056652069092, 10.456852912902832, "3D Representation Technology Parameter Extraction x, y and z coordinates"]
+[-1.3692995309829712, 6.123699188232422, "3D Analytics Firm Ownership Acquisition Cost $140 million"]
+[2.945509910583496, -1.446190595626831, "Space and Satellite Imagery Company New Debt Issued $150 million"]
+[-1.9530996084213257, 7.319716930389404, "Computer Interface MIL-STD-1553 bus"]
+[-3.0382678508758545, 4.3516435623168945, "Spacecraft Interface RS-422"]
+[-1.9426640272140503, 7.323853969573975, "Computer Function Provides a large number of general-purpose interface ports, analog sampling, isolated power conversion, and expanded memory management capability"]
+[-1.9347654581069946, 7.298646926879883, "Computer Function Records experimental results, stores them locally, and then communicates those results to the spacecraft for download to the ground station"]
+[-3.08829402923584, 2.433321237564087, "Mission Observation Date February 2021"]
+[1.3930509090423584, 2.3116273880004883, "Lightning Mapper Spatial Filtering Matches the IFOV of each detector element to the typical cloud-top area illuminated by a lightning stroke (i.e., in the order of about 10 km)"]
+[1.3886961936950684, 2.3122925758361816, "Lightning Mapper Spectral Filtering Using a narrowband interference filter centered on a strong optical emission line (e.g., OI at 777.4 nm) in the lightning spectrum"]
+[1.3920133113861084, 2.3104045391082764, "Lightning Mapper Temporal Filtering Takes advantage of the difference in lightning pulse duration which is on the order of 400 \u00b5s versus the background illumination which tends to be constant on the time scale of seconds"]
+[1.3880411386489868, 2.3108084201812744, "Lightning Mapper Integration Time 2 ms"]
+[1.3809518814086914, 2.3260693550109863, "Lightning Mapper Background Illumination to Lightning Signal Ratio Often exceeds 100 to 1"]
+[-0.07967058569192886, 15.564167976379395, "Limb Atmospheric Spectrometer Purpose Ozone Layer Observation"]
+[-0.073201023042202, 15.534563064575195, "Limb Atmospheric Spectrometer Detection Polar Stratospheric Cloud"]
+[2.2803642749786377, 22.23638153076172, "Instrument Parameter Measured Carbon Monoxide in the Troposphere"]
+[2.2407562732696533, 22.10845184326172, "Instrument Parameter Measured Ozone"]
+[-1.1369131803512573, 7.5208420753479, "Entity Requirement Measure atmospheric carbon with great precision and high spatial resolution"]
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+[1.846718192100525, 22.190353393554688, "Instrument Resolution 7.8 km"]
+[2.1862142086029053, 22.64507484436035, "Instrument Time Resolution About 2 ms"]
+[-7.561023235321045, 5.890773773193359, "Camera Operating Wavelength 777.4 nm"]
+[1.8689128160476685, 22.232297897338867, "Instrument Pixel Resolution 400 x 600 pixels"]
+[1.7983869314193726, 22.06952667236328, "Instrument Pixel Footprint Resolution 8-14 km"]
+[2.9744434356689453, 22.599077224731445, "Instrument Manufacturer Harris"]
+[2.8205525875091553, 22.44073486328125, "Instrument Update Authors Ronald Glumb, Peter Mantica, Alan Bell, Christopher Ellsworth, Lawrence Suwinski, and Jeremy Dobler"]
+[-0.09336551278829575, 13.590827941894531, "Measurement Devices Parameter Measured Surface and internal temperatures during reentry, ablation rate of the shield's coating"]
+[-0.45311543345451355, 8.300070762634277, "Ablative Material Percentage Burned Away 20%"]
+[-0.6281960010528564, 9.432497024536133, "Spacecraft Component Arrival Date at NASA/MSFC March 9, 2015"]
+[-0.6312709450721741, 9.417205810546875, "Spacecraft Component Purpose Extract samples of the ablative material, or Avcoat"]
+[-0.6201035976409912, 9.431498527526855, "Spacecraft Component Inspection Date March 11, 2015"]
+[-5.893393516540527, 16.00189971923828, "Synthetic Aperture Radar Average Sigma Naught -7.5 dB"]
+[4.977406978607178, -4.54525899887085, "Satellite Eclipse Phase May 2 \u2013 August 12, 2012"]
+[-1.4659637212753296, 13.37684440612793, "Solar Array Drive Assembly Auto Capture Initiation during the sunlit period"]
+[-5.908585548400879, 16.0173282623291, "Synthetic Aperture Radar Operation during Eclipse Avoided"]
+[-3.132488250732422, 4.295223236083984, "Spacecraft Number of Spacecraft 2"]
+[11.48803424835205, 5.6810688972473145, "CubeSat Size 6U"]
+[11.2701416015625, 5.458126068115234, "CubeSat Distance from Earth 27 million km"]
+[11.293813705444336, 5.50895357131958, "CubeSat Purpose Demonstrate navigation in deep space using innovative plasma thrusters"]
+[14.718255043029785, 7.821672439575195, "Nanosatellite Mass ~ 4 kg"]
+[11.484965324401855, 5.294036388397217, "Tandem Pair of 3U CubeSats Mass Unknown"]
+[11.891519546508789, 5.287461280822754, "3U CubeSat Mass 3 kg"]
+[11.48869514465332, 5.346053600311279, "2U CubeSat Unknown Unknown"]
+[11.643662452697754, 5.458542823791504, "1U CubeSat Unknown Unknown"]
+[11.85099983215332, 5.300208568572998, "1.5U CubeSat Mass 2 kg"]
+[11.682332038879395, 5.370514869689941, "1.5U CubeSat Unknown Unknown"]
+[16.62184715270996, 6.980812072753906, "Minisatellite Mass 138 kg"]
+[-0.4833844006061554, 5.823189735412598, "Unknown Altitude MEO (6-12,000 km)"]
+[6.327430248260498, 7.388184070587158, "Satellite Module SAR Elements Existing developments"]
+[-9.955621719360352, 5.851715564727783, "Search and Rescue System Satellite Tracking Up to 4 satellites"]
+[-9.95039176940918, 5.865967273712158, "Search and Rescue System Signal In Space Acquisition Band 1544.05 \u2013 1544.15 MHz"]
+[-9.953946113586426, 5.856476306915283, "Search and Rescue System DASS POC Band 2226.42 \u2013 2226.52 MHz"]
+[-9.95540714263916, 5.852658748626709, "Search and Rescue System TOA/FOA Measurement High accuracy"]
+[-9.954407691955566, 5.853240966796875, "Search and Rescue System Interface MCC"]
+[0.6459887027740479, 12.04405403137207, "Sensor Orientation Inverted"]
+[0.5649979710578918, 11.947981834411621, "Sensor Function Unable to sense sample return capsule deceleration during atmospheric entry and initiate parachute deployments"]
+[-2.840236186981201, 3.8537824153900146, "Capsule Recovery Date Oct. 4, 2004"]
+[-2.827786684036255, 3.8199520111083984, "Capsule Recovery Location Utah desert"]
+[-2.8411812782287598, 3.8700335025787354, "Capsule Transportation Flown to Ellington Field in Houston, then shipped by van for the short ride to JSC"]
+[-2.304561138153076, 9.281330108642578, "Power Tracking System Design Onboard"]
+[-7.5799641609191895, 5.880800247192383, "Cameras CCD Sensor Pixels 640 x 480"]
+[-7.578135013580322, 5.881944179534912, "Cameras Compression Algorithm JPEG"]
+[-7.582129001617432, 5.8840813636779785, "Cameras Optics and Resolution Different"]
+[-0.04403897374868393, 15.466604232788086, "Ion Mass Spectrometer/Neutral Mass Spectrometer Device Type Mass Spectrometer"]
+[-0.09872666001319885, 15.524493217468262, "Gated Electrostatic Mass Spectrometer Number of Units 2"]
+[-0.07832443714141846, 15.533409118652344, "Gated Electrostatic Mass Spectrometer Manufacturer GSFC"]
+[-2.9275074005126953, 4.562437057495117, "Parachute Location On the centerline of the backshell"]
+[-2.830610752105713, 4.687559604644775, "Parachute Location Packed around the drogue canister"]
+[-1.1459094285964966, 7.951951503753662, "Pyrotechnic Device Function Propels the drogue parachute out"]
+[-1.270015835762024, 8.594462394714355, "Component Release Mechanism Firing three frangible pyrotechnic bolts"]
+[5.07363748550415, -4.3284406661987305, "Satellite Discovery Date January 7, 2020"]
+[-0.36611080169677734, 3.787557363510132, "Planet Size Earth-size"]
+[-0.3722952604293823, 3.7837538719177246, "Planet Habitable Zone Status Confirmed"]
+[2.84906268119812, -1.025130271911621, "Satellite Purpose Find Earth-sized planets orbiting nearby stars"]
+[6.301751613616943, 7.442272663116455, "Satellite Component Pointing Accuracy about 100 \u00b5rad"]
+[1.5689727067947388, -2.076716184616089, "Satellite Orientation Control to a level of a few mrad"]
+[1.746293544769287, -2.129757881164551, "Satellite Attitude Control Scheme Magnetic torque rods and cold gas thrusters"]
+[-0.9331985712051392, 4.975737571716309, "Mobile Station Antenna Diameter 4.6m"]
+[-1.944662094116211, 7.462848663330078, "Room Equipment Storage 3 racks"]
+[-3.515693426132202, 7.183091163635254, "Data System Function Integrates the satellite image data with other data sources and provides the analyzed data"]
+[-2.667898178100586, 11.58841323852539, "Plotter Function Print out the images and analyzed data for the onsite information sharing"]
+[-5.205957889556885, 7.809148788452148, "Room Communication Systems Mobile data communication system and satellite communication system"]
+[2.066889524459839, -2.757652759552002, "Satellite Number of Satellites 6"]
+[3.21811580657959, -1.7423030138015747, "Satellite Manufacturer Maxar-owned manufacturer formerly known as Space Systems Loral"]
+[1.145970106124878, -0.7746904492378235, "Satellite Size Smaller than the earlier generations"]
+[2.1831891536712646, -1.4489954710006714, "Satellite Challenge Miniaturizing electronics while maintaining the performance of the high-resolution optics and keeping cost under control"]
+[1.6203795671463013, -1.1344153881072998, "Satellite Spatial Resolution 1 km"]
+[4.164153099060059, -2.574824571609497, "Satellite Temporal Resolution 1 day"]
+[1.0916622877120972, -1.4069446325302124, "Satellite Swath More than 2900 km"]
+[1.408070683479309, -1.075427532196045, "Satellite Coastal Zones Spatial Resolution 50 m"]
+[1.0457491874694824, -1.374104619026184, "Satellite Coastal Zones Swath More than 950 km"]
+[-0.9994094371795654, 7.761355876922607, "Device Positioning Accuracy < 1m"]
+[-1.0619398355484009, 7.7696452140808105, "Device Signal Overlap ALOS-2 SAR frequency"]
+[-1.0365698337554932, 7.724992752075195, "Device Endurance Against SAR signal"]
+[-4.364687442779541, 0.19272953271865845, "GPS Receiver Channels 9"]
+[-4.941986083984375, 9.5101318359375, "Receiver Module Channels Up to 7"]
+[1.1636875867843628, -1.045140266418457, "Satellite Phase-Center Distance 3.75 m"]
+[2.0837435722351074, -2.7059717178344727, "Satellite Number of Phase Centers 3"]
+[1.033988356590271, -1.4636175632476807, "Satellite Cross-Track Velocity Components 5 m/s"]
+[1.0430328845977783, -1.6592458486557007, "Satellite Accuracy of Cross-Track Velocity Components \u00b10.3 m/s"]
+[0.9845948219299316, -1.8783248662948608, "Satellite Accuracy of Along-Track Velocity Components \u00b14.0 m/s"]
+[-1.8818272352218628, 14.834894180297852, "Radiometer Sensor Type Mechanical scanning (whiskbroom)"]
+[-1.8895107507705688, 14.860615730285645, "Radiometer Measurement Bands 12 bands from 0.402 - 12.5 \u00b5m"]
+[-1.88975191116333, 14.866217613220215, "Radiometer Swath Width 1400 km"]
+[-1.8570388555526733, 14.811419486999512, "Radiometer Spatial Resolution Approx. 700 m"]
+[-1.930782437324524, 14.927963256835938, "Radiometer Operation Requirements Global observation of the Earth during daytime"]
+[3.7324955463409424, 17.65570831298828, "Scientific Payload Deployment Italian Space Agency's LARES-2 scientific payload"]
+[-3.2798566818237305, 5.43063497543335, "Launch Vehicle Performance About 2.2 t in a reference 700 km polar orbit"]
+[-3.2721455097198486, 5.41906213760376, "Launch Vehicle Payload Handling Handles larger payloads"]
+[2.403672218322754, 14.126608848571777, "Viscometer Temperature Very near Xenon's liquid-vapor critical point"]
+[2.459519624710083, 14.186264991760254, "Viscometer Mass < 1 mg"]
+[2.449084758758545, 14.190417289733887, "Viscometer Grid Size 7 mm x 19 mm"]
+[2.5139384269714355, 14.223543167114258, "Viscometer Oscillation Frequency < 13 Hz"]
+[2.4690170288085938, 14.188138961791992, "Viscometer Oscillation Amplitude < 0.01 mm"]
+[-2.1481761932373047, 2.9086530208587646, "Observatory Spotting Date March 12"]
+[-2.1197750568389893, 2.940565347671509, "Observatory Follow-up Studies Date Unknown"]
+[-5.364432334899902, 2.736355781555176, "Telescope Management Caltech and the agency's Jet Propulsion Laboratory"]
+[-0.7224717140197754, 3.119215250015259, "Neutron Star Age About 240 years old"]
+[-0.7366294264793396, 3.111895799636841, "Neutron Star Mass Twice the mass of our Sun"]
+[-0.7279369235038757, 3.123542308807373, "Neutron Star Magnetic Field Strength Up to 1,000 times stronger than a typical neutron star"]
+[-0.7452799081802368, 3.117948055267334, "Neutron Star Belongs to Special class of objects called magnetars"]
+[-2.178983688354492, 2.868025302886963, "Satellite-based observatory Launch Year 2026"]
+[-1.3571501970291138, 6.1141886711120605, "Company In Charge of Avionics and integration for the service module (SVM)"]
+[1.063563585281372, 9.138691902160645, "Attitude and Orbit Control Subsystem Software Expertise Over the last 20 years"]
+[-1.3271567821502686, 6.113119602203369, "Company Expertise Satellite avionics development and testing"]
+[-1.5054677724838257, 13.413834571838379, "Solar Array Deployment Mechanism Friction Very low"]
+[-1.5115890502929688, 13.41439437866211, "Solar Array Deployment Mechanism Torque Margin High"]
+[-1.542548418045044, 13.37964153289795, "Solar Array Deployment Mechanism Deployment Shock Low"]
+[0.9726022481918335, -4.356684684753418, "Satellite Mass ~980 kg"]
+[2.0966622829437256, -0.48214322328567505, "Satellite Power 1.3 kW"]
+[1.1576969623565674, -0.8043621182441711, "Satellite Size 3.5 m height, 2.0 m diameter"]
+[5.124556064605713, -2.2997987270355225, "Satellite Design Life 4 years"]
+[1.5299512147903442, -2.310103416442871, "Satellite Stabilization 3-axis stabilized"]
+[2.672694444656372, -2.3417532444000244, "Satellite Communication Bands S-band, X-band"]
+[6.413568496704102, 7.3335981369018555, "Satellite Component Purpose Understand climate change and support sustainable ecological transition"]
+[-1.3388112783432007, 6.105583667755127, "Company Responsibility Responsible for the spacecraft or payload on 3 of the 6 new generation Copernicus Environment and Earth observation missions: LSTM, CRISTAL and ROSE-L"]
+[2.350517749786377, -1.5452600717544556, "Satellite Instruments Carbon Dioxide Spectrometer and CAPI"]
+[2.388901948928833, -1.5471283197402954, "Satellite Instrument Integration Common structure and electronics device"]
+[2.4274699687957764, -1.607353925704956, "Satellite Instrument Integration Sharing one common electrical box"]
+[2.865734100341797, 21.962636947631836, "Instrument Purpose Monitor Sea Surface Salinity"]
+[3.6814146041870117, 22.980438232421875, "Instrument Publication Date July 2007"]
+[3.0538179874420166, 22.738689422607422, "Instrument Mission Status Unknown"]
+[2.5924057960510254, 13.869527816772461, "Optical Observation System Quantity 2"]
+[2.604968547821045, 13.927261352539062, "Optical Observation System Training Quantity 25 Algerian Aerospace Engineers"]
+[2.5466551780700684, 13.724888801574707, "Optical Observation System Presentation Date Oct. 2-6, 2006"]
+[0.9872545003890991, 0.8399679064750671, "Earth Observation Optical Systems Symposium Date May 31-June 4, 2010"]
+[1.340985655784607, 11.115224838256836, "Observation Device Visibility Certain recurring morning and evening twilight periods"]
+[-0.8968867659568787, 7.375218391418457, "Human Observation Method Measure right ascension and declination at precise times by reference to known stars"]
+[-0.914135217666626, 7.3881683349609375, "Human Observation Method Record the precise time of their observations by the use of stopwatches synchronized with international time signals"]
+[-0.873546838760376, 7.411169052124023, "Human Observation Method Use GPS receivers to measure the latitude, longitude and altitude of their observing sites"]
+[-1.6137726306915283, 7.295571804046631, "Method Orbit Computation Angles-only-method"]
+[1.498579978942871, -2.4238202571868896, "Satellite Orbit Type High elliptic"]
+[1.625304937362671, -1.9416627883911133, "Satellite Apogee Activity Coronagraphy, Formation Flying maneuver tests"]
+[1.3181525468826294, -2.2201156616210938, "Satellite Perigee Phase Free flight and Sun pointing"]
+[1.8582122325897217, -2.251699924468994, "Satellite Phases 2 and 8 Activity Roll flip and a roll flip back"]
+[0.4700077474117279, 4.554826259613037, "Natural Phenomenon Average Age Younger"]
+[0.4567014276981354, 4.520086288452148, "Natural Phenomenon Minimum Extent 4 million square kilometers"]
+[0.4578724503517151, 4.526504039764404, "Natural Phenomenon Next \"Precipitous Drop\" Benchmark 3 million km2"]
+[6.299680233001709, 7.441512584686279, "Satellite Component Log Size Approximately 200-300 bytes"]
+[6.205791473388672, 7.537497520446777, "Satellite Component Number of Brightest Stars Recorded 100"]
+[-3.4465699195861816, 6.846489906311035, "Data Size 600-700 kB"]
+[-2.656134605407715, 7.796566009521484, "Microprocessor Location Payload"]
+[-1.9541901350021362, 7.338311672210693, "Computer Processor Model PowerQUICCII"]
+[-1.941466212272644, 7.33344030380249, "Computer Bus Speed 50 MHz"]
+[-1.912229061126709, 7.282845497131348, "Computer Core Speed 200 MHz"]
+[-1.9545904397964478, 7.328776836395264, "Computer Operating System Integrity"]
+[-1.9669684171676636, 7.312363624572754, "Computer Communication Links 2 ports of 1 Mbit/s CAN bus, 2 ports of 1 Mbit/s MIL-STD-1553B bus, 3 ports of 130 Mbit/s SpaceWire bus, Up to 8 duplex ports of 8 Mbit/s HDLC over opto-isolated or LVDS (Low Voltage Differential Signaling) channels, 3 ports of 25 Mbit/s DATA-CLK-DV raw data over LVDS"]
+[4.699290752410889, -2.5619096755981445, "Satellite Age 120 million years"]
+[-0.7446252107620239, 3.193535566329956, "Star System Infrared Brightness Unusually bright at wavelengths of 12 and 24 micrometers"]
+[-0.7368535399436951, 3.1546449661254883, "Star System Gravitational Bound Companion Located so far from TOI 451 that its light takes 27 days to get there"]
+[3.1830780506134033, -1.595629096031189, "Satellite Mission Lead MIT"]
+[3.0720419883728027, -1.6540330648422241, "Satellite Mission Operator MIT"]
+[-3.1404244899749756, 5.5803399085998535, "Launch Abort System Design Active jettison motor, inert abort motor, inert attitude control system"]
+[-3.1492576599121094, 5.569957733154297, "Launch Abort System Delivery Date 2014"]
+[-3.160560131072998, 5.556497573852539, "Launch Abort System Integration Crew and Service Module assembly"]
+[2.7482829093933105, -1.8405264616012573, "Satellite Global Coverage Yes"]
+[2.1082711219787598, -2.7731106281280518, "Satellite User Count More than 600 scientists in 54 countries"]
+[0.5541237592697144, -1.5141915082931519, "Satellite Orbit Altitude 158 km apart at the equator"]
+[1.0191138982772827, 0.7727499008178711, "Earth Observing Satellite Number of Instruments Ten"]
+[1.0244733095169067, 0.7678178548812866, "Earth Observing Satellite Altimeter Yes"]
+[3.124185800552368, 22.839570999145508, "Instrument Installation Date Unknown"]
+[5.101408958435059, -3.9394617080688477, "Satellite Launch Date 2024"]
+[7.228350639343262, 12.453685760498047, "Space Weather Instrument Purpose Image the solar corona and help detect and characterize CMEs"]
+[7.13627290725708, 12.565990447998047, "Space Weather Instrument Design Review Status Completed"]
+[7.259174823760986, 12.44581127166748, "Space Weather Instrument Fabrication Status Ready to proceed with full-scale fabrication, assembly, integration and test"]
+[-3.08758807182312, 4.282482147216797, "Spacecraft Purpose Detect and reduce plastic pollution in the ocean"]
+[4.330288887023926, -2.647486686706543, "Satellite Altitude Keeping Period 633 days"]
+[-1.6193957328796387, 9.637784957885742, "Ion Engine System Thrust Exceeds atmospheric drag"]
+[-1.587133765220642, 8.760904312133789, "Reaction Control System Value Smaller than the IES"]
+[0.6779831051826477, -1.3099007606506348, "Satellite Altitude Lowest altitude by an Earth observation satellite in orbit"]
+[0.9775405526161194, -4.321812629699707, "Satellite Mass 249.5 kg"]
+[-0.6372467875480652, 9.421170234680176, "Spacecraft Component Structure 12-sided structure measuring 0.95 m point to point"]
+[3.7325873374938965, 17.715042114257812, "Payload Length 0.82 m"]
+[-1.9466482400894165, 8.285572052001953, "Separation System Diameter 0.97 m"]
+[-3.1535885334014893, 1.724294900894165, "Satellite Mission Mission Overview Aquarius/SAC-D Mission Overview"]
+[-3.1012871265411377, 1.6754804849624634, "Satellite Mission URL http://www.tos.org/oceanography/issues/issue_archive/issue_pdfs/21_1/21.1_lagerloef.pdf"]
+[-13.470191955566406, -2.013000249862671, "X-ray Observatory Purpose Study the hot and energetic Universe"]
+[-5.232148170471191, 7.8910017013549805, "Communication Platform Function Enable inter-satellite communication"]
+[7.327258110046387, 12.453208923339844, "Satellite Instrument Mission WSF-E"]
+[1.5889359712600708, 2.320063591003418, "Geostationary Operational Environmental Satellites Number of Backups 2"]
+[1.5757546424865723, 2.3363308906555176, "Geostationary Operational Environmental Satellite Functioning Yes"]
+[-13.749085426330566, -2.0737624168395996, "X-ray Imager FOV 4.6\u00b0 x 4.6\u00b0"]
+[-13.967907905578613, -2.264714241027832, "X-ray Imager Focal Length 27.5 cm"]
+[11.166247367858887, 5.445070743560791, "CubeSat Observatory FOV 4.6\u00b0 x 4.6\u00b0"]
+[-2.6421494483947754, 11.684154510498047, "Imager Function Record and telemeter the position and time of each X-ray photon detection"]
+[4.6746063232421875, -4.508388519287109, "Satellite Image Capture Date 24 July"]
+[0.8251639604568481, -1.2700457572937012, "Satellite Fire Front Length More than four km"]
+[1.0547137260437012, -1.4315205812454224, "Satellite Burn Scars Area Around 1700 hectares"]
+[-1.047271490097046, 6.085952281951904, "International Treaty Signing Year 2015"]
+[-1.0489842891693115, 6.17393159866333, "International Treaty Reporting Frequency Every five years beginning in 2023"]
+[-1.3298003673553467, 6.195898056030273, "Government Rejoining Date Not yet clear"]
+[-5.100961208343506, 15.913878440856934, "L-band SAR Observation Performance Improved"]
+[-5.141623020172119, 15.908577919006348, "L-band SAR Observation Band Wide"]
+[-5.184470176696777, 15.897202491760254, "L-band SAR Observation Data Useful for disaster monitoring"]
+[-2.7040791511535645, 9.442657470703125, "Power Generation Size 10 m2"]
+[-2.7305328845977783, 9.416584968566895, "Power Generation End of Life Power Generation 1790 W"]
+[-3.6706738471984863, 8.327560424804688, "Power Storage Overall Capacity 80 Ah"]
+[-2.9631245136260986, 7.446877479553223, "OnBoard Data Handling CPU TSC695F"]
+[-3.1184017658233643, 7.331941604614258, "OnBoard Data Handling Nominal Bus Voltage 28 V"]
+[6.349762439727783, 7.385648727416992, "Satellite Component Shape Hexagon with a diameter of 50 cm and a height of 53 cm"]
+[6.258735656738281, 7.465123176574707, "Satellite Component Mass About 8 kg"]
+[6.361456871032715, 7.3792033195495605, "Satellite Component Material Graphite fiber"]
+[-1.3787157535552979, 13.329907417297363, "Solar Cell Experiment Type Advanced"]
+[2.6697609424591064, 22.518774032592773, "Instrument Brightness Temperature Calibration Unknown"]
+[4.9739789962768555, -4.098400592803955, "Satellite Phase-A Plan Arrangement Autumn 2022"]
+[3.1023504734039307, -1.8537821769714355, "Satellite Not Selected for Development Due to the strict adherence to the cost constraints established by the PB-EO"]
+[2.9397501945495605, -1.298662543296814, "Satellite Risk-Reduction Studies Will be performed by ESA"]
+[1.2132554054260254, -1.9345225095748901, "Satellite Pointing Accuracy \u2264 6 arcmin"]
+[1.0048984289169312, -2.008594512939453, "Satellite Angular Drift <0.001\u00ba/s"]
+[1.2511529922485352, -1.2465860843658447, "Satellite Solar Arrays Surface Area 9.2m2"]
+[2.077845811843872, -0.5710793733596802, "Satellite Payload Power Consumption 240-1500 W"]
+[0.9934747815132141, -4.393295764923096, "Satellite Total Mass 1150 kg"]
+[0.9645229578018188, -4.318071365356445, "Satellite Payload Mass 350 kg"]
+[5.305615425109863, -2.2015562057495117, "Satellite Design Life 5 years"]
+[4.957087516784668, -2.387200355529785, "Satellite Goal Life 7 years"]
+[0.5273188948631287, -1.4847184419631958, "Satellite Initial Orbit Altitude 387 km"]
+[0.7026916742324829, -2.268646240234375, "Satellite Initial Orbit Inclination 51.6\u00ba"]
+[4.0938920974731445, -2.8408219814300537, "Satellite Orbital Period 90 minutes"]
+[5.144877910614014, -4.478518486022949, "Satellite Reentry Date Feb. 19, 2000"]
+[-0.7862907648086548, 8.807177543640137, "Thermal Protection System Performance Excellent"]
+[-0.6419243812561035, 8.71915340423584, "Heatshield Material Performance Excellent"]
+[-2.1774661540985107, 8.274430274963379, "Avionics, Power and Wiring System Performance Exceptional"]
+[-1.9401696920394897, 6.910501956939697, "Software Performance Excellent"]
+[11.12231159210205, 5.193361759185791, "CubeSat Mass 1.2 kg"]
+[11.334012985229492, 5.572353839874268, "CubeSat Manufacturer University of W\u00fcrzburg"]
+[11.52150821685791, 5.727709770202637, "CubeSat Size 3U"]
+[11.531195640563965, 5.748843669891357, "CubeSat Size 2U"]
+[-2.1052498817443848, 7.761390686035156, "Avionics Unit Manufacturer Hartron-Arkos"]
+[-13.922536849975586, -2.228032350540161, "X-ray Telescope Mission Type All-sky survey"]
+[-13.844925880432129, -2.2067224979400635, "X-ray Telescope URL http://arxiv4.library.cornell.edu/PS_cache/arxiv/pdf/1004/1004.5219v1.pdf"]
+[1.4652633666992188, -2.3912343978881836, "Satellite Orbit Highly elliptical Earth orbit, 600 km x 60,524 km"]
+[4.862820148468018, -2.4166557788848877, "Satellite Mission Lifetime Over 2 years"]
+[2.732923984527588, -1.8998841047286987, "Satellite Radiation Belts Crossing Yes"]
+[0.10531628131866455, -4.040951251983643, "Satellite Platform Radio Frequency Ranging Algorithms Implemented"]
+[-0.09437038004398346, 15.580704689025879, "Spectrometer Wavelength Range 1.61 - 1.68 \u03bcm"]
+[-0.05630745738744736, 15.501622200012207, "Spectrometer Resolution 100 m x 400 m"]
+[-0.018675614148378372, 15.542218208312988, "Spectrometer Swath Width 260 km"]
+[-0.11138205230236053, 15.528297424316406, "Spectrometer Methane Detection Sensitivity 3 parts per billion"]
+[1.4159570932388306, -2.537865400314331, "Satellite Orbit Type Sun-synchronous polar orbit"]
+[0.6878398060798645, -1.136000633239746, "Satellite Altitude 526 km"]
+[4.153242588043213, -2.811541795730591, "Satellite Orbit Period 100 minutes"]
+[3.772073268890381, -2.5484306812286377, "Satellite Global Mapping Frequency Every 3 - 4 days"]
+[0.988224983215332, -4.356472492218018, "Satellite Mass 350 kg"]
+[2.7092854976654053, -2.4293079376220703, "Satellite Launch Vehicle Falcon 9"]
+[-0.8451915383338928, 12.690460205078125, "Radiation Monitoring Instrument Measurement Electron, proton and ion fluxes"]
+[-0.6995440125465393, 11.660463333129883, "Debris/Micrometeorite/\u00b5particle Detector Function Orbital debris/micrometeorite/\u00b5particle detection"]
+[-0.8680089116096497, 12.714873313903809, "Radiation Monitoring Instrument Launch Date Nov. 21, 2000"]
+[-0.8723589777946472, 12.720590591430664, "Radiation Monitoring Instrument Operational Status Still operational as of 2007"]
+[0.6391927599906921, 11.949346542358398, "Sensor Purpose Characterize clouds and provide imagery in theaters of combat"]
+[0.5889090299606323, 12.091352462768555, "Sensor Cross Equator Time Early in the morning local time"]
+[0.576629638671875, 12.102787971496582, "Sensor Capabilities Day-night imagery"]
+[-0.6048847436904907, 11.72732925415039, "Lightning Detector Telescope Aperture Diameter 12 cm"]
+[-0.4653249680995941, 11.842150688171387, "Lightning Detector Interference Filter Bandwidth 1 nm"]
+[-0.499868243932724, 11.807517051696777, "Lightning Detector Broadband Blocking Filter Placed on the front surface of the filter substrate"]
+[-0.6898256540298462, 11.672954559326172, "Lightning Detector Telescope Fast f/1.2"]
+[-0.5751145482063293, 11.777539253234863, "Lightning Detector Data Output Consists primarily of events, not images"]
+[4.213022232055664, -2.808590888977051, "Satellite Emergency Observation Command Ready Time Within 60 minutes"]
+[4.247457981109619, -2.7940289974212646, "Satellite Emergency Product Ready Time Within 60 minutes"]
+[2.915623664855957, 22.056182861328125, "Instrument Science Capabilities Global environmental monitoring, biospheric research, cryospheric research, coastal ocean research, disaster mitigation"]
+[0.7106342911720276, 12.050580024719238, "Sensor Operating Voltage 3 V"]
+[0.5613898634910583, 12.205682754516602, "Sensor Calibration Method Current varying among several fixed values is applied to a coil that generates a constant magnetic field for the three axes"]
+[0.6132891774177551, 11.98906421661377, "Sensor Additional Feature Small temperature sensor (PT-1000)"]
+[3.215761661529541, -0.2721276879310608, "Satellite Sensor Complement OLS, SSH, SSJ/3, SSB, Contamination Monitor"]
+[5.351800918579102, -4.4036126136779785, "Satellite Launch Date 11.9.1976"]
+[4.790369987487793, -3.7706384658813477, "Satellite Mission End 17.9.1979"]
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+[1.5180583000183105, -3.7789788246154785, "Satellite S/C Mass (kg) 450"]
+[3.2179815769195557, -0.26822629570961, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.518974781036377, -3.780416488647461, "Satellite S/C Mass (kg) 450"]
+[3.2171003818511963, -0.268437922000885, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5178430080413818, -3.7816076278686523, "Satellite S/C Mass (kg) 450"]
+[3.218208074569702, -0.26761502027511597, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5239235162734985, -3.775014638900757, "Satellite S/C Mass (kg) 450"]
+[3.2171454429626465, -0.2718701958656311, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.516789197921753, -3.787663221359253, "Satellite S/C Mass (kg) 450"]
+[3.2209062576293945, -0.2624862790107727, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5170626640319824, -3.78456974029541, "Satellite S/C Mass (kg) 450"]
+[3.2233011722564697, -0.2638076841831207, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.534863829612732, -3.775109052658081, "Satellite S/C Mass (kg) 450"]
+[3.2206430435180664, -0.262235552072525, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5178484916687012, -3.789872169494629, "Satellite S/C Mass (kg) 450"]
+[3.220288038253784, -0.2641707956790924, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5192673206329346, -3.784872531890869, "Satellite S/C Mass (kg) 450"]
+[3.2216920852661133, -0.26134949922561646, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5180517435073853, -3.787137031555176, "Satellite S/C Mass (kg) 450"]
+[3.2225112915039062, -0.2589609920978546, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5165307521820068, -3.80564546585083, "Satellite S/C Mass (kg) 450"]
+[3.2208425998687744, -0.26060381531715393, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5151536464691162, -3.7943334579467773, "Satellite S/C Mass (kg) 450"]
+[3.221991777420044, -0.2563764452934265, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5292805433273315, -3.781144857406616, "Satellite S/C Mass (kg) 450"]
+[3.2379696369171143, -0.24195806682109833, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5151829719543457, -3.7945499420166016, "Satellite S/C Mass (kg) 450"]
+[3.223984479904175, -0.2579343318939209, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5106614828109741, -3.8012239933013916, "Satellite S/C Mass (kg) 450"]
+[3.224508762359619, -0.25225380063056946, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5089561939239502, -3.8018198013305664, "Satellite S/C Mass (kg) 450"]
+[3.2237236499786377, -0.2655383348464966, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5116428136825562, -3.797295570373535, "Satellite S/C Mass (kg) 450"]
+[3.221134901046753, -0.26951298117637634, "Satellite Sensor Complement OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
+[1.5043649673461914, -3.8073313236236572, "Satellite S/C Mass (kg) 450"]
+[-6.756114482879639, 10.028434753417969, "Antenna Data Transmission Rate 2-4 Mbit/s"]
+[-4.706320285797119, 9.053383827209473, "Transceiver Downlink Rate Support 2-4 Mbit/s"]
+[1.3827509880065918, 7.045217037200928, "Communication Equipment Location Guildford, UK"]
+[1.3627171516418457, 7.003112316131592, "Communication Equipment Location Bordon, UK"]
+[4.096428394317627, 13.939123153686523, "Laser Altimeter System Operating Temperature -30 C to 50 C"]
+[4.101059913635254, 13.936771392822266, "Laser Altimeter System Laser Power Levels Unknown"]
+[4.109453201293945, 13.949219703674316, "Laser Altimeter System Laser Beam Strength Decreased by 13 orders of magnitude"]
+[4.108718395233154, 13.943696975708008, "Laser Altimeter System Operating Environment Vacuum of space"]
+[3.902085542678833, 8.980956077575684, "Space Shuttle Observation Date 2004"]
+[3.9016270637512207, 8.979472160339355, "Space Shuttle Observation Date January 2005"]
+[3.9052305221557617, 8.981789588928223, "Space Shuttle URL http://wwlln.net/publications/yair.grl.2005.pdf"]
+[0.8971829414367676, 12.029160499572754, "Sensor Quantity 2"]
+[0.858084499835968, 12.043949127197266, "Sensor Quantity Unknown"]
+[0.8105587363243103, 12.046846389770508, "Sensor Quantity Unknown"]
+[0.8547999262809753, 12.06449031829834, "Sensor Quantity 2"]
+[0.840978741645813, 12.057387351989746, "Sensor Quantity 2"]
+[-1.0484755039215088, 7.661717891693115, "Device Quantity Unknown"]
+[-1.0862380266189575, 7.646045207977295, "Device Quantity Unknown"]
+[-1.1292515993118286, 7.666441917419434, "Device Quantity Unknown"]
+[-1.0672041177749634, 7.66462516784668, "Device Quantity Unknown"]
+[-1.0554300546646118, 7.707398891448975, "Device Quantity Unknown"]
+[-1.0020684003829956, 7.622857093811035, "Device Quantity Unknown"]
+[-3.1335766315460205, 1.7183719873428345, "Satellite Mission Formation Flying Yes"]
+[-3.0881049633026123, 1.686452031135559, "Satellite Mission URL of paper http://www.sffmt2013.org/PPAbstract/4111.pdf"]
+[-3.0861034393310547, 1.696329116821289, "Satellite Mission URL of presentation http://www.sffmt2013.org/PPAbstract/4111pr.pdf"]
+[-3.1563150882720947, 1.7287938594818115, "Satellite Mission Acta Astronautica Vol. 82"]
+[-3.1085073947906494, 1.752325177192688, "Satellite Mission Issue 1"]
+[-3.1260578632354736, 1.692627191543579, "Satellite Mission Page Numbers 38-46"]
+[-3.2348437309265137, 1.688211441040039, "Satellite Mission Year 2013"]
+[-5.2028679847717285, 7.837730407714844, "Communication System Antenna Diameter 4.6 m"]
+[-5.372982501983643, 7.9940900802612305, "Communication System Operation Setup Time Short"]
+[-5.176738262176514, 7.880973815917969, "Communication System Operating Temperature Range -30\u00baC to 45\u00baC"]
+[-5.25532341003418, 7.823843955993652, "Communication System Wind Velocity 25 m/s"]
+[-5.229435443878174, 7.881037712097168, "Communication System Storage Temperature -30\u00ba to 60\u00baC"]
+[-0.8276166319847107, 16.41248321533203, "Fourier Transform Spectrometer Data Acquisition Period 5 March to 3 April 2019"]
+[-0.8258087038993835, 16.419675827026367, "Fourier Transform Spectrometer Parameter Retrieved Methane column-averaged dry-air mole fraction (XCH4)"]
+[-0.8280908465385437, 16.417509078979492, "Fourier Transform Spectrometer Concentration Higher CH4 concentration in Southeast and South Asia, Central Africa and in the northern part of South America"]
+[-0.8613592982292175, 0.17433728277683258, "Satellite System Termination Date Feb. 2010"]
+[-0.8308795094490051, 0.155413419008255, "Satellite System Program Components NOAA POES, DoD DMSP, NASA\u2019s long-term continuous climate record collection"]
+[-0.8411667346954346, 0.1541098803281784, "Satellite System Major Challenge Jointly executing the program between three agencies of different size with divergent objectives and different acquisition procedures"]
+[-5.515419960021973, 9.508560180664062, "Frequency Reference Frequency Unknown"]
+[-3.4083478450775146, 8.135007858276367, "Signal Processing Device Frequency Conversion 24 and 32 GHz"]
+[-3.3403241634368896, 8.107952117919922, "Signal Processing Device Function Sampling and digital signal processing"]
+[1.6659414768218994, 6.96835470199585, "Communication Device Transmit and Receive Frequencies Offset 0.5 MHz in the 24 GHz channel, and by 0.67 MHz in the 32 GHz channel"]
+[1.6952764987945557, 6.949822425842285, "Communication Device Phase Change Sample Rate 10 Hz"]
+[3.6794111728668213, 22.95499038696289, "Instrument Observation Date Aug. 1, 2002"]
+[1.49583101272583, 21.20979881286621, "Instrument Mass ~ 130 kg"]
+[3.0219266414642334, 22.380434036254883, "Instrument Components EO (Electro-Optics) module, telescope, scan assembly, detectors, cooler, power-supply modules"]
+[-0.8536949753761292, 12.730504989624023, "Radiation Dosimetry Experiment Objective Characterize the radiation dose received by the spacecraft"]
+[-0.9281687140464783, 12.832178115844727, "Radiation Dosimetry Experiment Instrument History Flown on aircraft [the Concorde (BA) and Boeing-767 (SAS)], on the Shuttle (STS-48, -44, -53, -56, -68, and -63), in sun-synchronous orbit (UoSat-3, since Jan. 23, 1990), and on the USAF APEX satellite"]
+[6.344545364379883, 7.387096405029297, "Satellite Components PID 238 Implementation FPGA and software on the embedded microcontroller"]
+[6.332640171051025, 7.393402576446533, "Satellite Components Interface Architecture Point-to-point"]
+[6.295183181762695, 7.38657808303833, "Satellite Component PID 238 Implementation Same specification as instruments"]
+[6.392256259918213, 7.348475933074951, "Satellite Components Data Link Error Detection Implemented"]
+[-0.9510811567306519, 13.205785751342773, "Radiation Dosimeter Size 46 mm x 27 mm x 18.5 mm"]
+[-0.8826248645782471, 13.294780731201172, "Radiation Dosimeter Mass 30 g"]
+[-0.8862279653549194, 13.163455963134766, "Radiation Dosimeter Shielding Thickness 2 mm"]
+[-1.8173754215240479, 8.590082168579102, "Bus Electronic Unit Type Plug-and-Play"]
+[-1.6121511459350586, 8.409636497497559, "Bus Electronic Unit Function Combines all subsystem and payload electronics into one electronics box"]
+[0.9996514916419983, -4.40386962890625, "Satellite Mass 600 kg"]
+[0.5458081960678101, -1.4934743642807007, "Satellite Orbit Altitude 6-12,000 km"]
+[16.606081008911133, 6.996661186218262, "Minisatellite Mass ~180 kg"]
+[11.221782684326172, 5.3830742835998535, "CubeSat Mass 3U CubeSat, 5 kg"]
+[-5.499741554260254, 2.8902409076690674, "Telescope Module Energy Range 6-30 keV"]
+[-5.425908088684082, 2.8616418838500977, "Telescope Module Angular Resolution 1 arcmin"]
+[-5.474440574645996, 2.874851942062378, "Telescope Module Field of View ~30 arcmin"]
+[-5.519773960113525, 2.9066896438598633, "Telescope Module Energy Resolution 10% at 14 keV"]
+[-5.467409133911133, 2.8700926303863525, "Telescope Module Effective Area 455 cm^2 at 8 keV"]
+[-5.503633975982666, 2.888690233230591, "Telescope Module Effective Area 2500 cm^2 at 1 keV"]
+[-5.490392684936523, 2.917018413543701, "Telescope Module FOV 34 arcmin"]
+[-5.412873268127441, 2.759997606277466, "Telescope Module System Angular Resolution \u22641 arcmin"]
+[-5.463979721069336, 2.8410141468048096, "Telescope Module Energy Resolution 1.4 keV at 14 keV"]
+[-5.507462501525879, 2.837416648864746, "Telescope Module Energy Resolution 130 eV at 6 keV"]
+[6.311373233795166, 7.425697326660156, "Satellite Component Frequency 406 MHz"]
+[1.6808865070343018, -2.2153475284576416, "Satellite Motion Moves relative to the Earth"]
+[3.7244136333465576, 17.70682716369629, "Payload Function Determine the coordinates of the emergency signal"]
+[1.377298355102539, -2.038534641265869, "Satellite Pointing Stability 0.5 arcsec rms"]
+[1.4065732955932617, -1.8855738639831543, "Satellite Pointing Repeatability 1 milliarcsecond rms"]
+[1.0613631010055542, -2.065101146697998, "Satellite Focal Plane Temperature Stability Better than \u00b10.01 K"]
+[-5.23683500289917, 7.840420722961426, "Communication System Speed Up to 1 Gbit/s"]
+[2.684108018875122, -2.7748031616210938, "Satellite Downlink Rate ~800 Mbit/s"]
+[-3.5361623764038086, 6.805036544799805, "Data Prediction Accuracy Better than 90%"]
+[3.727294921875, 17.715686798095703, "Payload Control Hierarchy PLC (Payload Controller) > RF and baseband subsystems > DCG (Digital Chirp Generator), the V and H receivers, the FG (Frequency Generator), Feeder SSPA (Solid\u2010State Power Amplifier), CAL (Calibration Switch Matrix) and four DACSs (Data Acquisition and Compression Subsystems)"]
+[-1.893196702003479, 8.785510063171387, "Controller Interface DC Power and a 1553 interface with the BMU (Bus Management Unit) of the spacecraft"]
+[-1.040737271308899, 8.113394737243652, "Robotic Arm Release Time 6:33 p.m. EST"]
+[-3.155385732650757, 4.7268290519714355, "Cargo Craft Splashdown Time Monday at 12:15 a.m."]
+[-3.1092872619628906, 4.682994842529297, "Cargo Craft Recovery Location Southern California"]
+[-3.0645856857299805, 4.647597312927246, "Cargo Craft Purpose Taking home a variety of critical space research"]
+[4.933339595794678, -3.9446659088134766, "Satellite Mission Failure 16 November 2020"]
+[4.98593282699585, -4.425944805145264, "Satellite Inquiry Commission Appointment 17 November 2020"]
+[1.4967182874679565, -2.4716765880584717, "Satellite Orbit Type Elliptical GTO (Geosynchronous Transfer Orbit)"]
+[0.7240095734596252, -1.625795602798462, "Satellite Perigee 620 km"]
+[0.6978788375854492, -1.5965678691864014, "Satellite Apogee 36,000 km"]
+[0.6680517196655273, -2.320777416229248, "Satellite Inclination 7.5\u00ba"]
+[4.180797100067139, -2.79935622215271, "Satellite Orbital Period About 10.5 hours"]
+[0.5700557231903076, 9.4607572555542, "Attitude Determination and Control System Stabilization Earth-pointing attitude with one panel facing Earth"]
+[-0.03339872881770134, 9.844481468200684, "Inertial Measurement Unit Function Attitude determination"]
+[0.6236545443534851, 11.936748504638672, "Sensor Function Earth horizon sensors and sun sensors"]
+[-0.45722049474716187, 8.65180778503418, "Actuator De-tumble mode function Reduce rates on all three axes to<1\u00ba/s"]
+[-0.08146369457244873, 9.121849060058594, "Navigation Method Function Compares the magnetometer and sun vectors using a model of Earth's magnetic field and an astronomical almanac for sun position comparisons"]
+[2.6210334300994873, 22.938793182373047, "Instrument Time Cadence Software defined and configurable, nominal product telemetered to the ground is 5 s"]
+[1.771457314491272, 22.116235733032227, "Instrument Spatial Resolution 38 km"]
+[-1.6455327272415161, 5.384562969207764, "Operations Center Location Boston University (BU)"]
+[-1.6487363576889038, 5.38925838470459, "Operations Center Location Boston University (BU)"]
+[5.2102532386779785, -4.348588466644287, "Satellite Launch Date 17 August 2021"]
+[5.139575958251953, -4.293478012084961, "Satellite First Light Date 27 August 2021"]
+[-0.6633670926094055, 12.371102333068848, "Monitor Purpose Better space weather forecasts"]
+[-0.5500265955924988, 11.73694896697998, "Silicon Tracker Detector Sensor Layers 8 double-sided silicon sensor layers"]
+[-2.2294044494628906, 6.055941104888916, "Time of Flight System Precision Around 120 ps"]
+[-1.0090965032577515, 12.030241012573242, "Transition Radiation Detector Straw Tubes 5248 straw tubes"]
+[-0.4678277373313904, 11.743659019470215, "Ring Imaging Cherenkov Counter Photomultiplier Tubes 680 R7600-M16 multianode Hamamatsu PMTs"]
+[-2.304368019104004, 15.077857971191406, "Electromagnetic Calorimeter Radiation Depth 17 Xo"]
+[-4.444195747375488, 12.085844039916992, "Cryogenic Superconducting Magnet Magnetic Flux Density 0.86 TeV"]
+[-0.560390293598175, 1.2640942335128784, "Orbit Determination Tool Reference Position Center of the SAR antenna"]
+[-0.5667060613632202, 1.2670812606811523, "Orbit Determination Tool Reference Position Tends towards RADARSAT-2's center of mass, which is approximately 1 m above the center of the SAR antenna"]
+[-0.5324974656105042, 1.23928964138031, "Orbit Determination Tool Estimated Uncertainty Below 1 m"]
+[2.660310983657837, -1.0502010583877563, "Satellite Methane Emissions Detection Almost anywhere on Earth"]
+[0.8333273530006409, -1.408913254737854, "Satellite View Path Width 200 kilometers"]
+[4.124091625213623, -2.4810831546783447, "Satellite Revisit Time Every few days"]
+[5.023560047149658, -4.521249294281006, "Satellite Image Release Date Jan. 03, 2014"]
+[2.5824270248413086, -3.900412082672119, "Satellite URL http://kompsat.satreci.com/ds4_2_1.html?db=gal"]
+[0.5723437666893005, -1.5028380155563354, "Satellite Orbit Altitude 800 km"]
+[3.2441189289093018, -2.13038969039917, "Satellite Deployment Order After PICOSat"]
+[3.2775635719299316, -2.1074581146240234, "Satellite Deployment Order After SAPPHIRE"]
+[0.6567545533180237, -1.4432212114334106, "Satellite Orbit Altitude 500 km"]
+[2.7576091289520264, -1.3126976490020752, "Satellite Primary Objective Involve more school children in radio science"]
+[-1.8644227981567383, 14.831923484802246, "Meter Measured Parameters Ambient electron density and temperature"]
+[-4.507627487182617, 12.115191459655762, "Magnetometer Measured Parameters Geomagnetic fluctuations associated with solar geophysical phenomena"]
+[-2.6439037322998047, 11.686091423034668, "Imager Measured Parameters Vertical profiles from the natural airglow radiation from atoms, molecules and ions in the upper atmosphere and ionosphere"]
+[-2.5774850845336914, 11.739141464233398, "Imager Measured Parameters Composition of the upper atmosphere and ionosphere"]
+[1.741816759109497, -1.657850742340088, "Satellite Spectral Ranges Forward viewing (+20\u00ba) b1: 333-353 nm, b2: 433-453 nm, b3: 664-684 nm, b4: 859-879 nm, b5: 1585-1675 nm"]
+[1.7088278532028198, -1.5856101512908936, "Satellite Spectral Ranges Backward viewing (-20\u00ba) b6: 370-390 nm, b7: 540-560 nm, b8: 664-684 nm, b9: 859-879 nm, b10: 1585-1675 nm"]
+[1.9166834354400635, -1.5496519804000854, "Satellite Spectral Ranges Nadir viewing b1: 370-390 nm, b2: 664-684 nm, b3: 860-880 nm, b4: 1555-1645 nm"]
+[1.6141566038131714, -1.181089162826538, "Satellite Spatial Resolution Band 1-3, 500 m(750 \u00b5rad)"]
+[1.5954208374023438, -1.2057135105133057, "Satellite Spatial Resolution Band 4, 1500 m(2250 \u00b5rad)"]
+[1.4081447124481201, -1.5537811517715454, "Satellite Swath/FOV Band 1-3, 1002 km (72\u00ba)"]
+[1.690700888633728, -1.7255911827087402, "Satellite Swath/FOV Band 4, 786 km (60\u00ba)"]
+[1.5202537775039673, -2.0059187412261963, "Satellite SNR b1: >200 (45/0.158)"]
+[1.5174477100372314, -2.042210817337036, "Satellite SNR b2: >200 (79/0.144)"]
+[1.7677165269851685, -1.9959936141967773, "Satellite SNR b3: >200 (46/0.106)"]
+[5.077704429626465, -4.317008972167969, "Planet Hunter Satellite Discovery Date July 29, 2019"]
+[-0.64482581615448, 3.187291145324707, "Star Type M-type dwarf"]
+[-0.5784150958061218, 3.2335903644561768, "Star Size Compared to Sun About 40% smaller"]
+[-0.6190007328987122, 3.225473165512085, "Star Mass Compared to Sun About 40% smaller"]
+[-0.6030057668685913, 3.2173361778259277, "Star Surface Temperature About one-third cooler than the Sun\u2019s"]
+[-0.5355895161628723, 3.551865577697754, "Planetary System Distance from Earth About 73 light-years"]
+[2.0650196075439453, 22.591934204101562, "Instrument Spectral Range 5 to 15 \u00b5m"]
+[1.9421957731246948, 22.407268524169922, "Instrument Spectral Resolution 0.4 cm-1"]
+[1.7559599876403809, 22.00019073486328, "Instrument Ground Swath 1,000 to 2,500 km"]
+[1.8468444347381592, 22.12141990661621, "Instrument Spatial Resolution About 30 km"]
+[-1.8536792993545532, 14.822948455810547, "Radiometer Radiometric Accuracy 0.5 K"]
+[11.518198013305664, 5.726336479187012, "CubeSat Size 3U"]
+[11.550368309020996, 5.792845726013184, "CubeSat Size 2U"]
+[11.508197784423828, 5.777682304382324, "CubeSat Size 1U"]
+[5.326206207275391, -4.40747594833374, "Satellite Launch Date September 2018"]
+[4.660080909729004, -2.5787105560302734, "Satellite Primary Mission Duration Three years"]
+[-1.7860376834869385, 8.442680358886719, "Electronics Function Create the piezo drive voltages from the raw battery bus, command the stage position, read the stage position, operate the piezo stage in closed loop using strain gauge feedback, and implement a notch filter to avoid exiting resonant frequencies in the stage"]
+[1.7394068241119385, 10.943705558776855, "Imaging Mode Field of View 11.2\u00b0 by 9.6\u00b0"]
+[1.7445539236068726, 10.914532661437988, "Imaging Mode Number of Windows Up to eight"]
+[1.7021560668945312, 10.947689056396484, "Imaging Mode Window Size 64 x 64 pixels"]
+[1.749884843826294, 10.943285942077637, "Imaging Mode Readout Rate 20 Hz"]
+[1.596500039100647, 11.186062812805176, "Observation Mode Integration Time 60 seconds"]
+[2.6644222736358643, 5.392362594604492, "Emergency Beacon Population Unknown"]
+[1.7931709289550781, 6.846888065338135, "Communication Device Data Rate 100 Mbit/s"]
+[1.8099921941757202, 6.823779582977295, "Communication Device Data Rate 10 Mbit/s"]
+[1.7826169729232788, 6.867900848388672, "Communication Device Data Rate 9.6 kbit/s"]
+[-5.575655460357666, 7.052986145019531, "Communication Link Frequency 150 MHz"]
+[-5.581061363220215, 7.036588668823242, "Communication Link Frequency 20 GHz"]
+[-5.575179576873779, 7.060842514038086, "Communication Link Bandwidth 16 MHz"]
+[-5.576074600219727, 7.0518059730529785, "Communication Link Bandwidth 12 MHz"]
+[-5.583454132080078, 7.037803649902344, "Communication Link Gain on transmit 16.15 dB"]
+[-5.582664966583252, 7.035367488861084, "Communication Link Gain on transmit 19.6 dBi"]
+[-5.584278106689453, 7.034358024597168, "Communication Link Gain on receive 2.15 dBi"]
+[-5.584065914154053, 7.034972667694092, "Communication Link Gain on receive 38.74 dB"]
+[-5.5828166007995605, 7.03557014465332, "Communication Link Transmit power 50 W"]
+[-5.598743438720703, 7.030071258544922, "Communication Link Transmit power 0.2 W"]
+[-5.5843281745910645, 7.041707992553711, "Communication Link Propagation distance ~ 1000 km"]
+[-5.5885138511657715, 7.024801731109619, "Communication Link Receiver noise temperature 23 dBK"]
+[-5.5802106857299805, 7.026875972747803, "Communication Link G/T 30 dBK"]
+[-5.5817437171936035, 7.034804821014404, "Communication Link Link margin 4 dB"]
+[-5.582527160644531, 7.033442497253418, "Communication Link C/N 60.515 dB"]
+[-5.587352752685547, 7.028056621551514, "Communication Link C/N 96.862 dB"]
+[2.861459255218506, 22.286630630493164, "Instrument Features VDA reflector coating technology, Noise diodes, Hot load shrouding"]
+[0.25908783078193665, 13.806135177612305, "Calibration Source Type Correlated Noise Source"]
+[-1.3119890689849854, 7.538329601287842, "Various Development Areas RF Digital Polarimetric Receivers, Main Reflector, Reflector Deployment Assembly, Instrument Controller Electronics"]
+[2.4676759243011475, -1.5100141763687134, "Satellite Imaging Radar Instrument (SAR) Flown in 1978"]
+[4.838555335998535, -2.4575283527374268, "Satellite Lifetime 110 days"]
+[2.8383688926696777, -1.311764121055603, "Satellite Objectives Demonstrate techniques to monitor Earth's oceanographic phenomena and features from space on a global scale, Provide timely oceanographic data to scientists studying marine phenomena and users of the oceans as a resource, Determine the key features of an operational full-time ocean-monitoring system"]
+[1.740097165107727, 6.893906116485596, "Communication Device Data Dumping Capacity 6 to 14 Gbit/ pass"]
+[1.7241493463516235, 6.923823833465576, "Communication Device Power Consumption Below 10 W peak, 1 W mean/orbit"]
+[1.6910370588302612, 6.966436386108398, "Communication Device RF Output Power Up to 2 W"]
+[-6.72685432434082, 10.024807929992676, "Antenna Gain 0 dBi at \u00b1 60\u00b0"]
+[1.6718330383300781, 6.966032028198242, "Communication Device Diameter 3.4 m"]
+[1.7323287725448608, 6.91777229309082, "Communication Device Diameter 5 m"]
+[1.5102323293685913, 5.423850059509277, "Satellite Bus Mass 100-500 kg"]
+[1.1928032636642456, -1.253769040107727, "Satellite Ground Sample Distance Comparable to GeoEye-1, WorldView-2 and Pleiades-HR"]
+[6.746087551116943, 6.952695369720459, "Satellite Component Unknown Unknown"]
+[6.270843029022217, 7.456037521362305, "Satellite Component Launch Mass 366 kg"]
+[7.484678268432617, 12.6179780960083, "Satellite Instrument Launch Date October 1, 2022"]
+[6.371133804321289, 7.3643999099731445, "Satellite Component Structural Assembly Two separate structural assemblies: the sensor assembly and the enclosure structure"]
+[6.340373516082764, 7.402970790863037, "Satellite Component Function Transfer heat and decouple any external CTE and/or structural loads into the optical systems"]
+[-5.307582378387451, 7.840229034423828, "Communication Standard Usage Low Rate Information Transmission"]
+[-5.286887168884277, 7.804646968841553, "Communication Standard Usage High Rate Information Transmission"]
+[-1.3385703563690186, 6.135074615478516, "Organization Name World Meteorological Organization"]
+[1.7132738828659058, 6.936168193817139, "Communication Device Acquisition Failure Reason Ephemeris and spacecraft attitude control was out of specification"]
+[1.7112095355987549, 6.935172080993652, "Communication Device Divergence Designed to the ephemeris specification"]
+[-1.2990748882293701, 6.827243804931641, "Specification Cross-Track Error Within \u00b1 100 m"]
+[-1.5276116132736206, 7.005609512329102, "Specification In-Track Error Within \u00b1 500 m"]
+[-1.244081974029541, 6.794261932373047, "Specification Yaw Control Within 1.0\u00ba"]
+[-0.27910834550857544, 10.267789840698242, "Post-Track Analysis Yaw Control Up to 6\u00ba"]
+[-3.037027597427368, 4.275356292724609, "Spacecraft Mission Type Non-EO"]
+[0.4973812401294708, 12.137212753295898, "Sensor Affiliation MPE (Max-Planck-Institute for extraterrestrial Physics), Garching, Germany"]
+[0.6497478485107422, 11.982389450073242, "Sensor Affiliation NASA/MSFC, Huntsville, AL, USA"]
+[0.650850772857666, 12.015213012695312, "Sensor Affiliation IKI (Space Research Institute), Moscow"]
+[-0.06820926815271378, 9.761911392211914, "Inertial Reference Unit Anomaly Found February 7, 2006"]
+[-0.08089923113584518, 9.76718521118164, "Inertial Reference Unit Configuration PS2/CPU2 and gyro A/B/C"]
+[-0.03737623989582062, 9.792963027954102, "Inertial Reference Unit Malfunction September 2006"]
+[-0.5588406920433044, 8.50170612335205, "Reaction Wheel Design Concept Cluster of four wheels in hot redundancy"]
+[-0.6484742164611816, 8.530608177185059, "Reaction Wheel Assembly Components One RW and a single channel WDE"]
+[1.0589935779571533, -0.9164815545082092, "Satellite Height 214 cm"]
+[0.9744271636009216, -4.391720771789551, "Satellite Mass 193 kg"]
+[2.638516902923584, -2.1651878356933594, "Satellite Booster Thor/Burner IIA"]
+[-1.1307631731033325, 4.479923725128174, "Ground Station Operators Location Wallops, VA"]
+[-1.1184766292572021, 4.493208885192871, "Ground Station Location Wallops, VA"]
+[2.4572439193725586, -1.994066596031189, "Satellite Operations Facility Location Suitland, MD"]
+[-0.8331097960472107, 6.113738059997559, "Site Location Fairmont, WV"]
+[-7.577901363372803, 5.874861240386963, "Camera Spatial Resolution 55 m"]
+[-7.557223320007324, 5.894547939300537, "Camera Observed Area 20 x 11 km"]
+[-7.53542423248291, 5.913704872131348, "Camera Resolution 55 m"]
+[-7.51481294631958, 5.938803672790527, "Camera Covers an Area 620 x 180 km"]
+[-7.5919694900512695, 5.867489337921143, "Camera Digital Data Recorder DDR"]
+[2.951916217803955, -1.2281241416931152, "Satellite Mission Purpose Improve observation capabilities and understanding of water cycle"]
+[2.989100694656372, -1.5550880432128906, "Satellite Support Program Strategic Priority Research Program for Space Sciences"]
+[2.481193780899048, -1.3660387992858887, "Satellite Observation Focus Water cycle and global change"]
+[0.09942835569381714, 11.05752182006836, "Observation Tools Fine Spatial and Temporal Resolutions and Accuracies Essential for water cycle and global change research"]
+[-0.1317743957042694, 15.598965644836426, "Spectrometer Spectral Range 758-778 nm"]
+[-0.1003437265753746, 15.49985122680664, "Spectrometer Spectral Resolution 0.044 nm"]
+[-0.17372947931289673, 15.556272506713867, "Spectrometer SNR (Signal-to-Noise Ratio) 360"]
+[-0.11298490315675735, 15.478250503540039, "Spectrometer Spatial Resolution 1 km x2 km, 2 km x 2 km"]
+[1.8091434240341187, 8.653202056884766, "Pointing Subsystem Rotation Range 0 to 360\u00ba"]
+[2.1070971488952637, 22.23710060119629, "Instrument Cross-Track Detection Range -30\u00ba to 10\u00ba"]
+[-4.360802173614502, 0.19920168817043304, "GPS Receiver Dimensions 82 \u00d7 82 mm"]
+[-4.37048864364624, 0.20004501938819885, "GPS Receiver Processor Actel SmartFusion A2F500 system on a chip that includes a hard wired ARM Cortex M3 processor"]
+[-4.361038684844971, 0.19685626029968262, "GPS Receiver Flash Memory 1 MB"]
+[-4.405948638916016, 0.242264062166214, "GPS Receiver External SRAM 1 MB"]
+[-4.397926330566406, 0.16160735487937927, "GPS Receiver RF Front End Zarlink GP2015 L1 RF front end"]
+[-4.390044212341309, 0.16522900760173798, "GPS Receiver Crystal Oscillator 10 MHz voltage controlled temperature compensated crystal oscillator (VC-TCXO)"]
+[-4.370337963104248, 0.1918809562921524, "GPS Receiver Power Supply Latch up detection on the power supply"]
+[-4.364657402038574, 0.19506460428237915, "GPS Receiver PCB Design Consideration of mechanical stresses caused by thermal cycling"]
+[-1.8613771200180054, 8.588006973266602, "Environmental Control and Life Support System (ECLSS) Unit Test Objective Developmental environmental control and life support system (ECLSS) unit returning for testing, teardown, and evaluation (TT&E) to determine the cause of failure and subsequent re-flight"]
+[-1.6039565801620483, 8.305805206298828, "Orbital Replacement Unit Purpose Used for urine distillation, processing, and future use"]
+[-1.9589208364486694, 7.510926723480225, "Hardware Purpose Used in conjunction with the Oxygen Generation System (OGS) for water production needs on-orbit"]
+[-0.3248363435268402, 5.159844398498535, "Habitats Purpose Used during Rodent Research missions"]
+[-1.3954403400421143, 9.226293563842773, "Gas Tanks Purpose Support high-pressure gas operations and activities on-orbit"]
+[1.7114531993865967, 6.95634651184082, "Communication Devices Data Reception Realtime"]
+[2.7303223609924316, -1.6464804410934448, "Satellite Operator NOAA"]
+[-1.6093072891235352, 9.69393253326416, "Propulsion System Propellant Butane cold gas"]
+[-1.5788315534591675, 9.670738220214844, "Propulsion System Integration Method Sliding it through the opening in the bottom of the separation panel"]
+[-1.6472619771957397, 9.701984405517578, "Propulsion System Image Credit SSTL"]
+[2.5451583862304688, 22.835819244384766, "Instrument Data Request Time 72 hours"]
+[1.611680030822754, 22.182722091674805, "Instrument Size 10 cm x 10 cm x 8.2 cm"]
+[1.5245918035507202, 21.244531631469727, "Instrument Mass 1 kg"]
+[1.628989577293396, 23.21990203857422, "Instrument Power Consumption <1.5 W"]
+[2.8224024772644043, 22.466590881347656, "Instrument Interface RS-422 or 1553B"]
+[2.909369945526123, 22.498117446899414, "Instrument Missions TSX-5, STRV-1c, DSP-21"]
+[11.522570610046387, 5.730527400970459, "CubeSat Power Generation 120 W"]
+[11.323389053344727, 5.5642170906066895, "CubeSat Flight Computer Proton 400K made by Space Micro, Inc."]
+[11.392058372497559, 5.688758850097656, "CubeSat GNC System Highly-capable micronized GNC (Guidance, Navigation and Control) system"]
+[11.223319053649902, 5.461275100708008, "CubeSat Attitude Determination and Control Subsystem BCT's (Blue Canyon Technologies) XACT attitude determination and control subsystem"]
+[-5.09696626663208, 9.312230110168457, "X-band Radio Capability High data throughput and Doppler ranging capabilities"]
+[5.348123550415039, -4.506925106048584, "Satellite Launch Date Aug.9, 2010"]
+[2.576853036880493, -3.931157350540161, "Satellite URL http://www.arabianaerospace.aero/article.php?section=technology&article=eiast-celebrates-first-anniversary-of-dubaisat-1-launch"]
+[5.220051288604736, -4.32495641708374, "Satellite Anniversary Date Aug.9"]
+[-1.6015148162841797, 4.102635860443115, "Ground Segment Location Hsinchu, Taiwan"]
+[-1.560878872871399, 4.133693695068359, "Ground Segment Location Hsinchu, Taiwan"]
+[2.433419942855835, -1.6997432708740234, "Satellite Imagery Reception Available to third parties with their own ground stations through cooperative agreements"]
+[11.784257888793945, 5.370830535888672, "1U CubeSat Orbit MEO (~5900 km)"]
+[11.843581199645996, 5.328598499298096, "3U CubeSat Orbit MEO (~5900 km)"]
+[11.794293403625488, 5.377129077911377, "1U CubeSat Orbit LEO (~ 500 km)"]
+[11.869742393493652, 5.351468563079834, "3U CubeSat Orbit LEO (~ 500 km)"]
+[11.854161262512207, 5.32939338684082, "3U CubeSat Orbit LEO (~ 500 km)"]
+[11.87070369720459, 5.316983222961426, "3U CubeSat Orbit LEO (~ 5900 km)"]
+[2.7560975551605225, 13.677722930908203, "Optical Device Dihedral Angle Offset (DAO) 1.25 arcseconds for LAGEOS-1, 1.5 arcseconds for LARES-1"]
+[2.7856242656707764, 13.69191837310791, "Optical Device Tolerance \u00b10.5 arcseconds"]
+[2.8222835063934326, 13.782205581665039, "Optical Device Dihedral Angle Offset (DAO) 1.5 inch"]
+[2.6701278686523438, 13.798601150512695, "Optical Device Mount Floating mount"]
+[2.8034708499908447, 13.719682693481445, "Optical Device Asymmetry Present when linear polarisation is used in an uncoated retroreflector"]
+[4.0971784591674805, 13.93258285522461, "Laser Altimeter System Pass Dates March 22, 2019 and June 21, 2019"]
+[0.9409748315811157, -1.3729329109191895, "Satellite Pass Separation About a half-mile"]
+[0.9498892426490784, 0.8605408668518066, "Earth Observation Instrument Unknown"]
+[-8.505139350891113, 13.66437816619873, "Environmental Parameter Increase 10 per cent"]
+[-0.8393166065216064, 6.778553485870361, "Environmental Process Fine-Tuning Unknown"]
+[-2.566525936126709, 11.883026123046875, "Optical Imager Purpose Take high-resolution images of Algeria for cartography, agricultural management, crop monitoring, and disaster management"]
+[5.258670806884766, -4.640758037567139, "Satellite Launch Date 12 Jul 2010"]
+[5.369085311889648, -4.5444512367248535, "Satellite Launch Date July 2010"]
+[5.319333076477051, -4.418548107147217, "Satellite Launch Date September 2016"]
+[6.299955368041992, 7.43400239944458, "Satellite Component Control Off in the width direction"]
+[6.3349833488464355, 7.40537691116333, "Satellite Component Control Between 2.48\u00ba and 1.67\u00ba"]
+[1.2911068201065063, 10.476901054382324, "Imaging System Ability to Command Gain Adjustments Yes"]
+[1.3934189081192017, 10.5267915725708, "Imaging System On-board Data Smoothing Factor 25"]
+[1.30933678150177, 10.61207103729248, "Imaging System Detector Types Silicon photoconductive diode, HgCdTe photoconductive detector, PMT detector"]
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+[-0.8478726148605347, 11.639030456542969, "Detector Detector Type GaAs opaque photocathode and multiple dynode PMT"]
+[-5.9020609855651855, 16.03713607788086, "Synthetic Aperture Radar Operating Mode Revisit Time 3 or 6 days"]
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+[-5.969577789306641, 16.06814956665039, "Synthetic Aperture Radar Volumetric Soil Moisture Products Spatial Resolution (Regional Scale) 25 m2"]
+[-5.897108554840088, 16.005136489868164, "Synthetic Aperture Radar Volumetric Soil Moisture Products Spatial Resolution (Global Scale) 50 m2"]
+[-5.917853832244873, 15.969290733337402, "Synthetic Aperture Radar Geospatial Maps of Sea Ice Development Resolution 20 m"]
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+[1.6601277589797974, 21.952194213867188, "Instrument Swath Width 1500 km"]
+[-4.566715240478516, -3.088998317718506, "Exoplanet Mass Precision 14 percent"]
+[-4.5666823387146, -3.0894505977630615, "Exoplanet Radius Precision 7 percent"]
+[-0.6815553307533264, 3.2651236057281494, "Red Dwarf Size About half the size of the Sun"]
+[-1.078670859336853, 3.117826223373413, "Stellar Objects Orbited by An average of two to three planets"]
+[-0.6497015953063965, 1.3144303560256958, "Earth Return Orbiter Launch Year 2026"]
+[-2.430978775024414, 8.324871063232422, "Capture, Containment and Return System Function Handle and bio-seal the OS, provide the Earth Entry Vehicle (EEV)"]
+[-0.6505637764930725, 1.3126274347305298, "Earth Return Orbiter Arrival Mars orbit"]
+[-0.6718771457672119, 1.3381052017211914, "Earth Return Orbiter Landing Desert of Utah"]
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+[-6.729135990142822, 9.998106956481934, "Antenna Instrument Mass 350 kg"]
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+[2.8712637424468994, -2.4920568466186523, "Satellite Frequency 3.13 GHz"]
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+[0.7570160627365112, -1.3667683601379395, "Satellite Field of Regard 500 km"]
+[1.1075935363769531, -1.3896980285644531, "Satellite Swath Width 20-150 km"]
+[1.4274013042449951, -1.147082805633545, "Satellite Spatial Resolution 5-30 m"]
+[1.5384953022003174, -1.1288893222808838, "Satellite Spatial Resolution 1-5 m"]
+[0.7870351076126099, -1.2448190450668335, "Satellite Length of a Scene Up to 4000 km"]
+[2.06705641746521, -2.3570337295532227, "Satellite SNR > 2"]
+[2.3231496810913086, -1.5063645839691162, "Satellite Instrument Calibration Performed in HF part of the equipment"]
+[5.135530471801758, -2.282264471054077, "Satellite Design Life 3 years"]
+[4.810173034667969, -2.4806928634643555, "Satellite Propellant Onboard 7 years"]
+[5.015503406524658, -3.996549606323242, "Satellite End of Life Date 6 years (Expected)"]
+[5.306399822235107, -4.475550174713135, "Satellite Launch Date Nov. 21, 2013"]
+[3.0402963161468506, -2.260896921157837, "Satellite Launch Mass Unknown"]
+[16.76127815246582, 6.932687759399414, "Microsatellite Mass ~100 kg"]
+[14.697955131530762, 7.806648254394531, "Nanosatellite Mass 10 kg"]
+[14.694891929626465, 7.80842399597168, "Nanosatellite Mass 7 kg"]
+[14.717386245727539, 7.833141803741455, "Nanosatellites Mass 12 kg"]
+[16.820816040039062, 6.879736423492432, "Microsatellite Mass 28 kg"]
+[16.849224090576172, 6.855568885803223, "Microsatellite Size 50 cm x 50 cm x 50 cm"]
+[11.837258338928223, 5.2885003089904785, "6U CubeSat Ion Propulsion Technology Mission Enabling"]
+[-9.909597396850586, 7.395954608917236, "Mirror Shape Aspheric of-axis concave"]
+[-9.91222095489502, 7.398241996765137, "Mirror Mounting Central fixture at back side"]
+[-9.909420013427734, 7.395868301391602, "Mirror Size (mm) 442 x 190"]
+[-9.909605979919434, 7.39581823348999, "Mirror Mass 2.3 kg"]
+[-9.913150787353516, 7.400260925292969, "Mirror Shape Aspheric on-axis convex"]
+[-9.966072082519531, 7.451581001281738, "Mirror Mounting Central fixture at back side"]
+[-9.91142463684082, 7.397730350494385, "Mirror Size (mm) 147 x 118"]
+[-9.91085147857666, 7.396789073944092, "Mirror Mass 0.3 kg"]
+[-9.911545753479004, 7.401546955108643, "Mirror Shape Aspheric of-axis concave"]
+[-9.915481567382812, 7.401157855987549, "Mirror Mounting Glued bipods on outer edges"]
+[-9.909849166870117, 7.396246910095215, "Mirror Size (mm) 556 x 291"]
+[-9.912883758544922, 7.398703098297119, "Mirror Mass 5.1 kg"]
+[8.490984916687012, 15.221381187438965, "Camera Mount Operation Mode Semi-automatic mapping mode"]
+[8.491911888122559, 15.222193717956543, "Camera Mount Purpose Take pictures of adjacent areas on the surface"]
+[3.746917963027954, -1.6078424453735352, "Satellite Operation Status Nominal"]
+[4.677651405334473, -2.5843663215637207, "Satellite Years on Orbit 6 years"]
+[2.65895938873291, -1.1021678447723389, "Satellite Information Use Ice monitoring, pollution monitoring, disaster management, agricultural monitoring, forest management"]
+[4.8408894538879395, -2.4512226581573486, "Satellite Contract Extension Three years"]
+[4.43967866897583, -3.017233371734619, "Satellite Imagery Provision Until November 2014"]
+[2.5900216102600098, -1.704340934753418, "Satellite Imaging Payload Provider Raytheon"]
+[-0.9449084401130676, -10.015810012817383, "Satellite Constellation Imaging Payload Provider Raytheon"]
+[4.694039344787598, -4.540461540222168, "Satellite Image Capture Dates 15 October 2021, 24 November 2021, 13 January 2022"]
+[-0.4240419566631317, 5.122426509857178, "Reservoir Elevation 1074 m above sea level"]
+[-0.40609753131866455, 5.10172700881958, "Reservoir Lowest Level Date 1980"]
+[-0.43086859583854675, 5.157209396362305, "Reservoir Second-Largest Humanmade Reservoir in the United States "]
+[3.3245651721954346, 0.46782565116882324, "Satellite Program Objective Collect and disseminate worldwide cloud cover data on a daily basis"]
+[3.321944236755371, 0.46909818053245544, "Satellite Program Use Strategic and tactical weather prediction for the US military"]
+[2.223353862762451, -1.5092991590499878, "Satellite Methane Column-Averaged Dry-Air Mole Fraction (XCH4) Parameter Value Unknown"]
+[2.247647523880005, 22.361858367919922, "Instrument Carbon Monoxide Column-Averaged Dry-Air Mole Fraction (XCO) Parameter Value Unknown"]
+[2.0035552978515625, -1.2673507928848267, "Satellite CO Measuring Item"]
+[2.8652420043945312, -1.0587024688720703, "Satellite Purpose Detect gamma-ray bursts"]
+[-5.373128890991211, 2.8697214126586914, "Optical Telescope Data Collection Light curves on everything in its field of view, every half hour"]
+[-5.46506404876709, 2.939689874649048, "Optical Telescope Data Analysis Determine how bright the burst was"]
+[-5.39552116394043, 2.849400281906128, "Optical Telescope Purpose Collects light curves on everything in its field of view"]
+[-13.847960472106934, -2.1938211917877197, "X-ray Telescope Imaging Andromeda galaxy"]
+[-13.918039321899414, -2.27520751953125, "X-ray Telescope Imaging Andromeda"]
+[-13.843976974487305, -2.266754150390625, "X-ray Telescope Imaging Cosmic clumpy doughnut around a black hole"]
+[0.004830010700970888, 15.43507194519043, "Atmospheric Spectrometer Performance Not specified"]
+[-2.757420063018799, 3.940390110015869, "Space Retroreflector Home Page http://www-lidar.nies.go.jp/RIS/index0-e.htm"]
+[3.786522150039673, -1.6451274156570435, "Satellite Operation Status Nominal"]
+[5.300826072692871, -2.2075374126434326, "Satellite Design Life 5 years"]
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+[2.308690071105957, -1.9144524335861206, "Satellite Operation Mode NDO tracking"]
+[1.3951877355575562, -2.4025983810424805, "Satellite Solar Activity Model Marshall solar activity future estimation model"]
+[2.412961006164551, -1.5026036500930786, "Satellite Atmospheric Model NRLMSISE-00"]
+[0.8602614998817444, -1.2045351266860962, "Satellite Altitude -60\u00ba"]
+[0.4714450240135193, -1.481890320777893, "Satellite Orbit Altitude Approximately 500 km"]
+[2.7070798873901367, 22.323326110839844, "Instrument Data Analysis Analyzing the latitude, longitude and elevation represented by each photon"]
+[2.665571689605713, 22.25420570373535, "Instrument Data Analysis Analyzing the preliminary ICESat-2 data"]
+[-3.196582794189453, 5.1125807762146, "Resupply Vehicle Launch Date 3 June 2021"]
+[-3.158994674682617, 5.063542366027832, "Resupply Vehicle End of Life Date 10 July 2021"]
+[-3.1712465286254883, 5.058094024658203, "Resupply Vehicle Mission Status Mission complete"]
+[-3.152947425842285, 5.081958770751953, "Resupply Vehicle Payloads New solar arrays, new science investigations, supplies, and equipment for the international crew"]
+[-4.9156622886657715, 9.803404808044434, "Monitor Receiver Unknown Unknown"]
+[-4.975006103515625, 9.736063957214355, "Receiver Front-End Unknown Unknown"]
+[-4.933713912963867, 9.784138679504395, "Receiver Unknown Unknown"]
+[-0.1000174805521965, 7.289353847503662, "Microprocessor Experiment Objective Evaluate the ESA ERC32 chip set and advanced processing technologies and shielding experiments in the harsh space environment"]
+[-0.18339233100414276, 7.335495948791504, "Microprocessor Experiment Components ESA ERC32 chip set and components"]
+[-0.1754351705312729, 7.323558807373047, "Microprocessor Experiment Number of RADFETS Three"]
+[-2.2002086639404297, 7.5323486328125, "ERC32 Board Location More shielded location"]
+[1.9061648845672607, 8.60607624053955, "Subsystem State-of-Health Normal"]
+[-1.6504323482513428, 9.737448692321777, "Electric Propulsion Subsystem State-of-Health Normal"]
+[1.9240981340408325, 8.590472221374512, "Subsystem State-of-Health Normal"]
+[1.907815933227539, 8.604438781738281, "Subsystem State-of-Health Normal"]
+[2.5717649459838867, 22.6393985748291, "Instrument VNIR Bands 23"]
+[2.0955560207366943, 22.759708404541016, "Instrument VNIR Spectral Range 380 - 830 nm"]
+[2.463559627532959, 22.765209197998047, "Instrument SWIR Bands 6"]
+[2.0480599403381348, 22.6427001953125, "Instrument SWIR Spectral Range 1050 - 2215 nm"]
+[2.506758689880371, 22.7486515045166, "Instrument MWIR and TIR Bands 7"]
+[2.0908830165863037, 22.516080856323242, "Instrument MWIR and TIR Spectral Range 3.715 - 11.95 \u00b5m"]
+[2.1748156547546387, 22.343416213989258, "Instrument IFOV 1.25 mrad"]
+[2.3869361877441406, 22.421628952026367, "Instrument FOV \u00b143\u00b0"]
+[1.8912969827651978, 22.404739379882812, "Instrument Wind Speeds 3 - 20 m/s"]
+[2.1222121715545654, 22.45924186706543, "Instrument Wind Speeds Accuracy 2 m/s"]
+[2.154571533203125, 22.247344970703125, "Instrument Wind Vector Directions Accuracy 20\u00b0"]
+[1.7979475259780884, 22.128225326538086, "Instrument Spatial Resolution 50 km"]
+[1.6981621980667114, 21.96292495727539, "Instrument Swath Width 1600 km"]
+[2.2753496170043945, 22.2807674407959, "Instrument IFOV \u00b152\u00b0"]
+[2.8923590183258057, -1.052901268005371, "Satellite Purpose Mitigate DoD Space-Based Environmental Monitoring gaps"]
+[2.2398478984832764, -1.863188624382019, "Satellite Gaps Ocean surface vector winds (OSVWs), tropical cyclone intensity (TCI) and LEO energetic charged particles"]
+[2.1401476860046387, 22.458145141601562, "Instrument Laser Pulses Per Second 10,000"]
+[3.748201847076416, -2.6003589630126953, "Satellite Data Collection Frequency Every 91 days"]
+[2.6383607387542725, -1.130395531654358, "Satellite Data Usage Near-shore mapping, monitoring coral reefs, coastal mangroves, sediment transport, carbon storage capacity, water clarity, invasive species, and coastal dynamics"]
+[-3.520941734313965, 6.827277660369873, "Data Usage Helping scientists figure out population changes of penguin species"]
+[0.16448743641376495, 7.1807355880737305, "Experiment Execution Dates Critical aspect in the definition of the trajectory profile"]
+[0.1443062573671341, 7.191115379333496, "Experiment Illumination Conditions Define the relative position of the chaser"]
+[0.1179790198802948, 7.205971717834473, "Experiment Drivers for the selection of the RVX execution dates and illumination conditions Part B2 to be performed with illuminated perigee, while Parts A+B1 are to be performed with eclipse in perigee. Part B2 to be performed after Part A. Earth cannot be within the VBS FoV when it is used in non-cooperative mode"]
+[0.14718829095363617, 7.20166015625, "Experiment Sun Azimuth and Elevation Wrt the orbital perigee direction"]
+[-1.0186779499053955, 7.709982872009277, "Device Data Rate Requirement 600 Mbit/s"]
+[-1.6167389154434204, 1.4788053035736084, "Data Relay System Operation LEO-GEO OISL"]
+[-1.6142643690109253, 1.4781244993209839, "Data Relay System Operation RF feeder link between Alphasat and its ground segment"]
+[-5.297659873962402, 7.884940147399902, "Communication System Development Date Sept. 29 to Oct. 3, 2008"]
+[5.069155693054199, -4.555352687835693, "Satellite Conference Date Aug. 10-13, 2009"]
+[1.4199717044830322, -1.1916810274124146, "Micro-satellite Development Date Unspecified"]
+[-2.94889235496521, 4.160167217254639, "Spacecraft Photometry Observation High-Precision"]
+[-3.020397424697876, 4.298750400543213, "Spacecraft Mission Operation URL: http://www.oact.inaf.it/plato/PPLC/ScientificProgramTao_files/2014-12-03Gondoin.pdf"]
+[-3.4089722633361816, 8.135110855102539, "Signal Processing Device Function Amplification and initial down-conversion of the signal"]
+[-1.9976859092712402, 7.507310390472412, "Hardware Update More resilient to single-event upsets"]
+[-5.399710178375244, 8.992779731750488, "Software-defined radio FPGA Xilinx Zynq Z7030"]
+[-5.425961017608643, 9.026732444763184, "Software-defined radio Front End Modules Up to 3"]
+[-5.420875549316406, 9.000085830688477, "Software-defined radio Antenna Location -Z face of the satellite"]
+[0.6884029507637024, 4.0548014640808105, "Ionosphere Layer Variable Yes"]
+[0.6549749374389648, 4.205266952514648, "Atmospheric Phenomenon Mass More than ions"]
+[0.6126343607902527, 4.262866973876953, "Atmospheric Phenomenon Changes Sluggish"]
+[0.6294463872909546, 4.239003658294678, "Atmospheric Phenomenon Changes Rapidly"]
+[0.6356165409088135, 4.20601224899292, "Atmospheric Phenomenon Importance Strongly controls the mass density of the thermosphere"]
+[-3.577164649963379, 4.404921054840088, "Spacecraft Launch Date June 10, 2011"]
+[-2.9195327758789062, 4.1841840744018555, "Spacecraft Orbit Altitude 657 km"]
+[-3.0099844932556152, 4.159272193908691, "Spacecraft Orbit Inclination 98\u00ba"]
+[-3.278902053833008, 4.281539440155029, "Spacecraft Nodal Crossing Time 18:00 hours on the ascending node"]
+[-3.2933402061462402, 4.222707271575928, "Spacecraft Earth Coverage Every 7 days"]
+[-3.121555805206299, 4.203042030334473, "Spacecraft RF Communications S-band and X-band"]
+[2.2033841609954834, 22.25263023376465, "Instrument Field of View 0.8\u00ba (i.e. 3 Rsun)"]
+[2.1104748249053955, 22.65240478515625, "Instrument Wavelengths 0.540 \u00b5m, 0.555 \u00b5m, 0.570 \u00b5m and 0.588 \u00b5m"]
+[1.623179316520691, 22.132427215576172, "Instrument Box Size 30 \u00b5m square"]
+[2.4952352046966553, 22.318145751953125, "Instrument Detector 2 x 2 pixels"]
+[2.330817937850952, 22.26403045654297, "Instrument Field of View 2.7 Rsun"]
+[2.468059778213501, 22.586307525634766, "Instrument Detector Up to 3 Rsun"]
+[-2.0310707092285156, 12.61936092376709, "Solar Ultraviolet Imager Installation Date Recently"]
+[1.42234468460083, 2.316004991531372, "Geostationary Lightning Mapper Design and Build Lockheed Martin"]
+[2.902885675430298, 21.9962158203125, "Instrument Goals Geohazards monitoring, land use monitoring, soil moisture monitoring, Arctic and cryosphere monitoring, maritime surveillance"]
+[1.8243623971939087, 22.19106101989746, "Instrument Spatial Resolution 5 m - 10 m"]
+[2.7228806018829346, 22.79684066772461, "Instrument Revisit Time Three or six days"]
+[-5.548177242279053, 15.940424919128418, "SAR Distinction Capability Between vegetated and non-vegetated areas"]
+[-5.59830379486084, 15.938775062561035, "SAR Analysis Capability Broad forest types"]
+[-2.64463472366333, 11.680459022521973, "Imager Wavelength Bands Visible, shortwave infrared, middle infrared, water vapor and two bands in thermal infrared"]
+[-2.641456127166748, 11.598708152770996, "Imager Image Generation Frequency Every 26 minutes"]
+[-3.7597129344940186, 7.201095104217529, "Data Provider Data Coverage Clear sky region of the data-sparse Indian Ocean"]
+[-3.84267520904541, 7.267528533935547, "Data Provider Spatial Resolution 10 km"]
+[5.012087345123291, -4.36047887802124, "Satellite Operational Date January 15, 2014"]
+[1.9853821992874146, -0.32570821046829224, "Radar Satellite Launch Date May 24, 2014"]
+[2.133617639541626, -0.7369384169578552, "Radar Satellite URL http://global.jaxa.jp/press/2014/05/20140524_daichi2.html"]
+[-1.0205975770950317, 7.729826927185059, "Device Bidirectional Scanning Employed"]
+[-1.3035997152328491, 8.555572509765625, "Component South Movement 1120 \u00b5rad"]
+[-1.2562402486801147, 8.577117919921875, "Component East-West Movement 280 \u00b5rad"]
+[-1.2550138235092163, 8.608732223510742, "Component N-S Stepping Time Integer multiple of the filter wheel rotational period (200 ms)"]
+[-1.2243504524230957, 8.588366508483887, "Component Blackbody Calibration and Space Look Slewing the mirror at a rate of 10\u00ba/s"]
+[-1.2058085203170776, 8.586849212646484, "Component Positional Repeatability Better than 5arcsec"]
+[2.523494005203247, -1.2313541173934937, "Satellite Sea Surface Salinity Monitor Global monitoring"]
+[5.3365478515625, -4.4942779541015625, "Satellite Launch Date June 10, 2011"]
+[2.578815460205078, -3.9179365634918213, "Satellite URL http://aquarius.nasa.gov/pdfs/11-181_Aquarius_Launch_SC.pdf"]
+[-0.7622241377830505, 11.558236122131348, "CMOS Space Qualified Detector Family COBRA, a CMOS Space Qualified Detector Family"]
+[-3.134708881378174, 1.7330065965652466, "Optical High Resolution Mission GMES Operational services Sentinel-2, Optical High Resolution Mission for GMES Operational services"]
+[0.16749568283557892, 7.2412567138671875, "Langmuir Probe Experiment Probe Diameter 20 mm"]
+[0.15195731818675995, 7.186443328857422, "Langmuir Probe Experiment Guard Ring Diameter 100 mm"]
+[0.17706838250160217, 7.178385257720947, "Langmuir Probe Experiment Objective Xenon plasma diagnostic instrument for CAE"]
+[0.5723078846931458, -1.46107816696167, "Satellite Orbital Altitude 167.4 km"]
+[0.568573534488678, -1.4886269569396973, "Satellite Orbital Altitude Range 200 km - 300 km"]
+[4.39221715927124, -2.71110463142395, "Satellite Orbital Duration 7 days"]
+[2.8849830627441406, -1.851150393486023, "Satellite Test Results Successful"]
+[2.491373062133789, -1.2439059019088745, "Satellite Data Acquired Atmospheric density, atomic oxygen density, and the level of deterioration of material samples"]
+[-13.844717025756836, -2.2060887813568115, "X-ray Space Telescope Detection Unexpected periodic pulsed emissions"]
+[-0.7931479811668396, 7.66400146484375, "Object Type Pulsar, a kind of neutron star"]
+[-0.7517995834350586, 3.1280291080474854, "Neutron Star Luminosity Much fainter than ULXs"]
+[1.9024276733398438, 10.718648910522461, "Imaging Device Spectral Bands 0.536-0.843 \u00b5m, 0.783-0.883 \u00b5m"]
+[1.8888306617736816, 10.726183891296387, "Imaging Device Spatial Resolution 8 m"]
+[1.9104520082473755, 10.72366714477539, "Imaging Device Swath Width 96 km"]
+[1.9839200973510742, 10.802699089050293, "Imaging Device Field of Regard in Cross-Track 780 km"]
+[1.9006837606430054, 10.716665267944336, "Imaging Device Data Transmission Rate 15.36 or 61.44 or 122.88 Mbit/s"]
+[-2.4840359687805176, 12.562224388122559, "Spectral Imager Spectral Bands 14"]
+[-2.4887423515319824, 12.56874942779541, "Spectral Imager Bandwidth 0.45 \u00b5m - 13.8 \u00b5m"]
+[-2.4828832149505615, 12.573122024536133, "Spectral Imager Spatial Resolution 0.5 - 4 km"]
+[-2.4778239727020264, 12.583110809326172, "Spectral Imager Spectral Range 0.55 - 14.3 \u00b5m"]
+[-2.472590208053589, 12.570196151733398, "Spectral Imager Spatial Resolution 2 - 16 km"]
+[-2.4830269813537598, 12.574259757995605, "Spectral Imager Spatial Resolution 7.8 km"]
+[-2.47392201423645, 12.56794261932373, "Spectral Imager Temporal Resolution 2 seconds"]
+[1.5153363943099976, 5.4229278564453125, "Satellite Bus Launch Mass Approximately 5300 kg"]
+[1.515623927116394, 5.425076484680176, "Satellite Bus Design Life 7 years"]
+[1.5141773223876953, 5.421563148498535, "Satellite Bus Data Downlink X-band"]
+[5.154019832611084, -4.387377738952637, "Satellite Anomaly Date March 7, 2016"]
+[5.050875663757324, -4.4011616706848145, "Satellite Break-up Date July 24, 2015"]
+[0.16846723854541779, 7.192345142364502, "Experiment Data Storage Capacity Up to 10 GByte"]
+[-1.9281628131866455, 8.060088157653809, "System Mission Life 1 year"]
+[-1.9017362594604492, 8.112434387207031, "System Total Ionizing Dose Tolerance 100 kRad"]
+[-1.8804988861083984, 8.129247665405273, "System Operational Temperature Range -43\u00baC to 41\u00baC"]
+[0.6305328607559204, 12.112874984741211, "Sensor Suite Number of Instruments 4"]
+[0.16584280133247375, 15.316143035888672, "Spectrometer Unknown Unknown"]
+[0.18523149192333221, 15.289922714233398, "Spectrometer Unknown Unknown"]
+[0.16285711526870728, 15.317665100097656, "Spectrometer Unknown Unknown"]
+[0.16319644451141357, 15.31855583190918, "Spectrometer Unknown Unknown"]
+[-0.1036105528473854, 12.63735294342041, "Sun Sensor Axis 2-axis"]
+[0.008556301705539227, 12.561110496520996, "Sun Sensor Size 3 cm x 3 cm"]
+[-0.12439148128032684, 12.663747787475586, "Sun Sensor Mass 24 gram"]
+[-0.21377524733543396, 12.705427169799805, "Sun Sensor Field-of-View Greater than \u00b160\u00ba"]
+[-0.11568883061408997, 12.654269218444824, "Sun Sensor Angle Accuracy Better than 0.15\u00ba"]
+[4.619301795959473, -2.6030056476593018, "Satellite Mission Duration 2 years"]
+[0.6035233736038208, -1.4773954153060913, "Satellite Closest Approach Distance to Lunar Surface 8,253 km"]
+[5.236617565155029, -4.476069927215576, "Satellite Lunar Flyby Date 17 May"]
+[4.38623571395874, -3.340653896331787, "Satellite Lunar Flyby Time 06:34:35 UTC (2:34 AM EST)"]
+[-3.3802366256713867, 4.337089538574219, "Spacecraft Launch Time 1:16 p.m. EST (18:16 GMT) Dec. 5, 2018"]
+[-2.978940486907959, 4.514564037322998, "Spacecraft Cargo Capacity More than 2540 kg"]
+[-2.982069492340088, 4.49808406829834, "Spacecraft Research and Hardware Facilities Weight Approximately 300 kg"]
+[0.027550261467695236, 13.60015869140625, "Pulse Height Analysis Unit Operation Mode List mode"]
+[-3.782900333404541, 7.597298622131348, "Power and Data Interface Function Access TTE data from each DP5G unit and store in a rolling buffer"]
+[-3.9062740802764893, 7.601130962371826, "Power and Data Interface Function Provide high voltage supplies for both the SiPMs and Si-PIN sensors on the GRD and XRD respectively"]
+[-3.813249111175537, 7.606574535369873, "Power and Data Interface Function Provide feedback controls for gain response versus detector temperature"]
+[0.9539155960083008, 0.8577969670295715, "Earth Observation Image Pair Date September 2020 (left) and February 2021 (right)"]
+[0.4831025004386902, 4.519748687744141, "Natural Phenomenon Annual Maximum Date September 28, 2020"]
+[0.45729419589042664, 4.515577793121338, "Natural Phenomenon Annual Maximum Extent 18.95 million km2 (7.32 million square miles)"]
+[0.47509291768074036, 4.501213550567627, "Natural Phenomenon 1981\u20132010 Average Extent 18.6 million km2"]
+[5.226499557495117, -3.8217673301696777, "Satellite Launch Year 2018"]
+[-5.330471038818359, 2.728562355041504, "Telescope Launch Year Recently launched"]
+[-5.298318862915039, 2.7247133255004883, "Telescope Expected Launch Year 2027"]
+[-3.1041691303253174, 2.454025983810425, "Mission Launch Year 2029"]
+[-1.2912676334381104, 6.889107704162598, "Technology Purpose Help zero in on exoplanet clouds and hazes"]
+[2.641979694366455, 22.282814025878906, "Instrument Observing Modes Disk images and limb scans, dayside: T and O/N2, nightside: O+ density, stellar occultations, full disk maps and limb scans with 30 minute cadence"]
+[1.7710891962051392, 22.114459991455078, "Instrument Limiting Resolution ~50 km"]
+[2.2830018997192383, 22.20450782775879, "Instrument Measurement Techniques Temperature obtained on disk from rotational shape of N2 LBH (Lyman-Birge-Hopfield) bands, O/N2 composition measured using ratio of 135.6 doublet to LBH bands, Temperature on limb determined by slope of emission altitude profile, O+ at night observed using 135.6 recombination emission, O2 profile on limb from stellar occultations"]
+[-0.9437501430511475, -10.016850471496582, "Satellite Constellation Revisits per Day Up to 14"]
+[-0.9484047889709473, -10.014472961425781, "Satellite Constellation Ground Sample Distance 0.3\u20131.3 meter"]
+[-0.960498034954071, -9.996217727661133, "Satellite Constellation Sun Angle Above 15\u00ba"]
+[-0.9506180882453918, -10.001448631286621, "Satellite Constellation Latitude 36\u00baN"]
+[-5.207406520843506, 7.508885860443115, "Network Speed 1244 Mbit/s"]
+[-2.786935329437256, 15.242919921875, "Microwave Radiometer Incidence Angle 52\u00ba and 58\u00ba"]
+[-2.794804334640503, 15.251548767089844, "Microwave Radiometer Swath Width 380 km"]
+[-2.813669443130493, 15.248730659484863, "Microwave Radiometer Displacement Across-Track 272 km"]
+[2.4022367000579834, -1.1354455947875977, "Satellite Imagery Acquired over the poorly charted area"]
+[2.0619397163391113, -2.7365095615386963, "Satellite Number of Images Over 400"]
+[-0.6377668380737305, 6.199680328369141, "Event Bathymetric Map Coverage 130,000 km2"]
+[2.5093765258789062, -1.1441594362258911, "Satellite Data Usage Accurately measure the depths (bathymetry) of shallow coastal waters"]
+[-1.903998613357544, 14.871732711791992, "Radiometer Operation Start Date Winter of 2012"]
+[-1.8968391418457031, 14.856846809387207, "Radiometer Data Processing Routines MWIR cross-talk correction and in-flight calibration protocol"]
+[2.0787606239318848, -2.72762131690979, "Satellite Quantity 100"]
+[0.6385136842727661, -1.4791065454483032, "Satellite Orbit Altitude 500 km"]
+[-3.1811602115631104, 1.7376400232315063, "Satellite Mission Launch Opportunity 2022\u20132024"]
+[-3.1541786193847656, 1.7086291313171387, "Satellite Mission Lead Activities Transferred from France to Germany"]
+[-3.1474833488464355, 1.6844338178634644, "Satellite Mission New Lead Heike Rauer (DLR)"]
+[-3.222073554992676, 1.6914317607879639, "Satellite Mission Candidate Since March 2013"]
+[-13.896699905395508, -2.2078986167907715, "X-ray Telescope Energy Release 1056 ergs"]
+[-13.888957977294922, -2.2445969581604004, "X-ray Telescope Number of X-ray Photons Doubled"]
+[-13.85055160522461, -2.2093605995178223, "X-ray Telescope Data Analysis Study the abundance of chemical elements, the degree of their ionization, the density and temperature of the emitting gas in the bubbles, and to identify the locations of shock waves and estimate characteristic timescales"]
+[-13.686868667602539, -2.3336570262908936, "X-ray Telescope Mission Date June 24, 2020"]
+[-13.906533241271973, -2.2506320476531982, "X-ray Telescope Mission Location Russia"]
+[-14.244691848754883, -2.481851816177368, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.254938125610352, -2.489112377166748, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.256192207336426, -2.488849639892578, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.260858535766602, -2.4932374954223633, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.260396003723145, -2.491671562194824, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.269294738769531, -2.5006062984466553, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.249113082885742, -2.484928846359253, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.262053489685059, -2.4940454959869385, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.254020690917969, -2.4886860847473145, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.269627571105957, -2.5000691413879395, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.248880386352539, -2.4844820499420166, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.264703750610352, -2.4961190223693848, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.25101089477539, -2.4867260456085205, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.26894760131836, -2.499523401260376, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.263877868652344, -2.494527578353882, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.259010314941406, -2.4905948638916016, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.264422416687012, -2.4947428703308105, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.264074325561523, -2.4970734119415283, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.258630752563477, -2.4917240142822266, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.271706581115723, -2.502293825149536, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.250884056091309, -2.4863553047180176, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.289239883422852, -2.517885446548462, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.251453399658203, -2.4870262145996094, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.26654052734375, -2.499113082885742, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.283012390136719, -2.510070562362671, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.294791221618652, -2.5179426670074463, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.265886306762695, -2.4982221126556396, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.286319732666016, -2.5147740840911865, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.285201072692871, -2.5103695392608643, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.3138427734375, -2.5386650562286377, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.265111923217773, -2.49739146232605, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.29732894897461, -2.518857002258301, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-14.256877899169922, -2.4926180839538574, "X-ray Telescope Lead Scientist Rashid Sunyaev"]
+[-14.322365760803223, -2.5452523231506348, "X-ray Telescope Principal Investigator Andrea Merloni"]
+[-1.9242202043533325, 8.113438606262207, "System Mass Distribution Continuously Changing"]
+[6.1983561515808105, 7.419685363769531, "Earth System Component Distribution Changes Sub-daily to inter-annual, and decadal"]
+[0.661023736000061, 4.130809783935547, "Climate Proxy Indicator of Climate Variations Driven by natural and/or anthropogenic causes"]
+[1.9551467895507812, -1.8896358013153076, "Satellite Observation Phases Long continuous pointing phases and short duration pointing phases"]
+[4.594760894775391, -2.6015257835388184, "Satellite Long Pointing Phase Duration Up to 3 years"]
+[4.53303861618042, -2.664534091949463, "Satellite Short Observation Phase Duration Between 2 and 5 months"]
+[1.8395452499389648, -1.1680657863616943, "Satellite Measurement Solar-induced Chlorophyll Fluorescence"]
+[-3.2028467655181885, 1.7634950876235962, "Satellite Mission Purpose Performing key ADR demonstrations"]
+[16.897907257080078, 6.825035572052002, "Microsatellite Function Release and capture several space debris targets"]
+[-2.7361092567443848, 4.598586559295654, "Space Debris Targets Type DSAT-1"]
+[1.5005170106887817, 5.429961681365967, "Satellite Bus Dimensions 3.7 m (height) by 1.36 m (diameter)"]
+[-6.736117362976074, 9.996711730957031, "Antenna Number of Radiating Elements 8192"]
+[-6.749380111694336, 10.015932083129883, "Antenna Number of T/R Modules 512"]
+[-6.776458740234375, 10.027167320251465, "Antenna Size 15 m by 1.5 m"]
+[-6.737239837646484, 10.000890731811523, "Antenna Mass Exceeding 700 kg"]
+[2.644686222076416, 14.349905967712402, "Optical Instrument Pulse Energy 2 mJ"]
+[2.6473495960235596, 14.318571090698242, "Optical Instrument Pulse Width < 1.5 ns"]
+[2.6392478942871094, 14.349430084228516, "Optical Instrument PRF 10 kHz"]
+[2.6313459873199463, 14.305110931396484, "Optical Instrument Center Wavelength 1020 - 1080 nm"]
+[2.6438117027282715, 14.287431716918945, "Optical Instrument Wavelength Stability/Linewidth < 60 pm"]
+[2.6514532566070557, 14.333894729614258, "Optical Instrument PER > 100:1"]
+[2.6305737495422363, 14.297541618347168, "Optical Instrument Spatial Mode M 2 < 1.6"]
+[2.673584222793579, 14.295730590820312, "Optical Instrument Pointing Stability (shot-to-shot) < 10% of divergence"]
+[2.620105028152466, 14.295146942138672, "Optical Instrument Pointing Stability (long-term) < 20% of divergence"]
+[2.639547824859619, 14.334684371948242, "Optical Instrument Lifetime > 5 years"]
+[2.620863676071167, 14.346488952636719, "Optical Instrument Operating Temperature 10 \u2013 40\u00baC"]
+[2.649860382080078, 14.376527786254883, "Optical Instrument Non-operating Survival Temperature 0 \u2013 50\u00baC"]
+[2.671281099319458, 14.307518005371094, "Optical Instrument Mass < 10 kg"]
+[2.638075351715088, 14.310880661010742, "Optical Instrument Volume < 40 cm x 25 cm x 15 cm"]
+[2.637022018432617, 14.315817832946777, "Optical Instrument Efficiency (Wall Plug) > 15%"]
+[-4.847939968109131, 2.726414203643799, "Reflector in Space Experiment Date 1999"]
+[2.5189573764801025, -1.9617815017700195, "Satellite Trajectory Determination Accuracy Unknown"]
+[1.106413722038269, -0.8906854391098022, "Satellite Size Up to 50 kg"]
+[2.7019801139831543, -1.7325080633163452, "Satellite Operator Service Roaming services for sensors and devices on trucks, precision agriculture equipment, clean energy infrastructure and other sectors"]
+[-1.6671981811523438, 11.23211669921875, "Lidar Optical Property Retrievals Particulate backscatter product, extinction product, ice water content product"]
+[2.1242897510528564, -0.8662075400352478, "Satellite Sensor Imaging Spectrum Longwave infrared (thermal)"]
+[2.397160053253174, 22.76169776916504, "Instrument Bands 23 bands (380 - 830 nm), 18 channels with 10 nm bandwidth - 6 bands (1050 - 2215 nm) - 7 bands (3.715 - 11.95 \u00b5m)"]
+[2.301382303237915, 22.522865295410156, "Instrument Parameter 1.25 mrad (or 1 km at nadir) for 28 bands 0.3125 mrad (or 250 m at nadir) for 6 bands"]
+[2.1571097373962402, 22.219369888305664, "Instrument Parameter \u00b143\u00ba (swath = 1600 km)"]
+[2.4048991203308105, 22.512256622314453, "Instrument Parameter 12 bit"]
+[2.224897861480713, 22.468528747558594, "Instrument Parameter < 2%"]
+[2.0154871940612793, 22.319562911987305, "Instrument Parameter 4 Mbit/s (for 1 km resolution), 16 Mbit/s (250 m resolution)"]
+[2.257352590560913, 22.25899887084961, "Instrument Parameter +20\u00ba, 0\u00ba, -20\u00ba"]
+[2.694936513900757, 22.2459774017334, "Instrument Device GLI scan mirror"]
+[2.2627649307250977, 22.900781631469727, "Instrument Parameters 450 kg, 400 W"]
+[-2.5981674194335938, 9.61674976348877, "Power Source Power Output 33 W"]
+[-2.170379877090454, 8.926197052001953, "Electrical System Voltage 28V"]
+[-3.7043681144714355, 8.262153625488281, "Power Storage Capacity 46 Whr"]
+[-3.3826193809509277, 7.222798824310303, "Data Handling Technology Radiation tolerant SOS technology"]
+[1.0066286325454712, -4.383782386779785, "Satellite Mass 52 kg"]
+[5.039588928222656, -2.349339008331299, "Satellite Design Life One year"]
+[1.5415241718292236, -2.0521738529205322, "Satellite Magnetic Field Strength 20000 - 70000 nT"]
+[1.5805072784423828, -1.9764715433120728, "Satellite Magnetic Field Strength Difference -2400 nT to +1800 nT"]
+[1.3636454343795776, -1.8923876285552979, "Satellite Changes in Field Strength Mostly negative and ranges up to almost 10% of the total field"]
+[2.9117214679718018, 22.540246963500977, "Instrument Data Downlink During the mission"]
+[2.9153189659118652, 21.98379898071289, "Instrument Purpose Determine the SARR coefficients of ACRIM-III on ACRIMSAT and to verify the VIRGO coefficients on SOHO"]
+[1.72344970703125, 6.911387920379639, "Transceiver/Communication Device Manufacturer ITT-AES (Advanced Engineering & Sciences), Reston, VA, a division of ITT Industries Inc"]
+[1.7393643856048584, 6.987752914428711, "Transceiver/Communication Device Purpose Supporting communications and/or navigation functions of mission applications"]
+[11.25798225402832, 5.464712619781494, "CubeSat Mission Objective Study of thermospheric properties"]
+[11.272907257080078, 5.504449367523193, "CubeSat Sponsor National Science Foundation (NSF)"]
+[11.272395133972168, 5.50826358795166, "CubeSat Collaborators University of Michigan (UMich), NASA/GSFC, NRL (Naval Research Laboratory)"]
+[11.248394012451172, 5.464694976806641, "CubeSat Mission Type Space weather"]
+[11.272356986999512, 5.4903435707092285, "CubeSat Study Area Earth's ionosphere and thermosphere"]
+[-3.584831953048706, 12.724000930786133, "Particle Detector Energy Range Up to 400 GeV/c2"]
+[-3.6414997577667236, 12.762006759643555, "Particle Detector Tracking System Accuracy Microns level"]
+[-3.640218496322632, 12.756378173828125, "Particle Detector Test Beam Incident Angles and Positions Thousands"]
+[-3.6517221927642822, 12.738043785095215, "Particle Detector Particles Collected Hundreds of million"]
+[-3.6373937129974365, 12.748462677001953, "Particle Detector Delivery Date to KSC August 26, 2010"]
+[-2.337423801422119, 7.3546247482299805, "Onboard Computer Processor 80386/80387"]
+[-2.369687795639038, 7.321134567260742, "Onboard Computer Solid State Recorder Speed 300 Mbit/s"]
+[-5.290434837341309, 7.793331623077393, "Communication System Uplink Speed 2 kbit/s"]
+[-5.212603569030762, 7.850074291229248, "Communication System Downlink Speed 2.25 Mbit/s"]
+[0.6329010128974915, 9.323010444641113, "Attitude Control Subsystem Pointing Accuracy < 5 arcsec"]
+[-8.132652282714844, 8.8262357711792, "Electric Power Subsystem Power 220 W"]
+[-1.9094184637069702, 8.665386199951172, "Control Segment Components GMCF, GADS, GTF"]
+[-3.0818848609924316, 2.4406676292419434, "Mission Support Components GUT, GMSF, GSL"]
+[2.2280538082122803, 23.151565551757812, "Instrument Frequency 14.599 GHz"]
+[2.734182596206665, 22.374534606933594, "Instrument Polarizations VV, HH"]
+[2.7081289291381836, 22.41974639892578, "Instrument Scanning Mode Fan-beam (2 sides)"]
+[1.8459616899490356, 22.231918334960938, "Instrument Beam Resolution Fixed"]
+[2.09505558013916, 22.262683868408203, "Instrument Azimuth Angle 45\u00ba, 135\u00ba"]
+[1.7930954694747925, 22.111927032470703, "Instrument Near Edges 200 km from subsatellite track"]
+[1.7441753149032593, 21.96058464050293, "Instrument Swath Width 500 km on either side of the ground track"]
+[1.810206651687622, 22.13913917541504, "Instrument Spatial Resolution 50 km"]
+[-5.2808732986450195, 7.919354438781738, "Communication System Contact Method Ground stations or TDRS"]
+[-5.21994686126709, 7.857640266418457, "Communication System Telemetry Protocol UDP (User Datagram Protocol)"]
+[-5.303236961364746, 7.524781227111816, "Communication Protocol Function Reconfigured the data paths between the control center and the payload automatically"]
+[0.13341236114501953, 7.211549758911133, "Experiment Purpose Study desert dust in the Mediterranean"]
+[0.13571330904960632, 7.163775444030762, "Experiment URL http://irc-iamas.org/files/MEIDEX.doc"]
+[2.1242878437042236, 22.240964889526367, "Instrument Sight Axis Angle 60\u00b0 with nadir"]
+[2.0789220333099365, 22.2351016998291, "Instrument Sight Axis Angle 30\u00b0 with the anti-nadir direction"]
+[-1.236383080482483, 8.599913597106934, "Component Frequency DC - 1 MHz"]
+[-1.2342180013656616, 8.625578880310059, "Component Frequency 100 kHz - 30 MHz"]
+[1.7984793186187744, 22.717836380004883, "Instrument Energy Range ~ 150 keV to 4 MeV"]
+[2.095759630203247, 22.4797420501709, "Instrument Time Resolution Of the order of 1 ms (or less)"]
+[4.686439514160156, -2.5757782459259033, "Satellite Mission Duration 5 years"]
+[2.759375810623169, -1.1956496238708496, "Satellite Science Objectives Quantify variability in incoming solar radiation, determine regions/layers of Earth\u2019s atmosphere that are affected by solar variability, determine whether the Sun\u2019s spectral ultraviolet output is in- or out-of-phase with visible wavelength output, provide TSI and SSI data to support community science in climate, atmosphere, solar physics, and radiative transfer modeling"]
+[3.0172653198242188, -1.500136137008667, "Satellite Project Responsibilities Project management, system engineering, safety and mission assurance, and engineering oversight for the TSIS-1 payload"]
+[2.548253059387207, -1.4011108875274658, "Satellite Data Archive and Distribution ESDIS (Earth Science Data and Information System) Project/GES DISC (Goddard Earth Sciences Data and Information Services Center)"]
+[2.8367679119110107, -1.4970521926879883, "Satellite Design, Development and Testing University of Colorado CU/LASP (Laboratory for Atmospheric and Space Physics), Boulder, CO"]
+[-13.696000099182129, -2.1067988872528076, "X-Ray Flux Monitor Launch Year 2021"]
+[-13.75198745727539, -2.1330623626708984, "X-Ray Flux Monitor Purpose Measure X-ray emissions from the Sun"]
+[-13.744843482971191, -2.0807321071624756, "X-Ray Flux Monitor Impact Provide autonomy over Europe's space weather forecasts and redundancy for space weather forecasters globally"]
+[4.700089931488037, -4.488524913787842, "Satellite Image Acquisition Year 2020"]
+[2.4584028720855713, -1.2547502517700195, "Satellite Data Used for Digital Elevation Model ICESat-2 data"]
+[-0.5003719925880432, 7.099123001098633, "Bathymetry Equipment Depth Range 0 to 10 meters"]
+[-3.4940290451049805, 6.834227561950684, "Data Importance Provide a window into the coastal dynamics and processes"]
+[-0.2167370617389679, 11.147025108337402, "Network Monitoring Tool Function Monitor router interface traffic, data rates, error indicators, and MIP tunnel status"]
+[-0.2752937376499176, 11.246475219726562, "Network Monitoring Tool Function Log all packets in/out of control center"]
+[-3.3494906425476074, 7.420597076416016, "Data Processing System Function Captured LPT housekeeping telemetry, displayed it, and forwarded UDP status packets to multiple systems with LabView graphical status displays"]
+[-3.337858200073242, 7.387042045593262, "Data Processing System Function Downloaded files collected and stored by pass for later analysis"]
+[-3.1662135124206543, 1.7003252506256104, "Satellite Mission Data Release Frequency Weekly"]
+[-3.1546075344085693, 1.6821022033691406, "Satellite Mission Data Distribution Center National Drought Mitigation Center at the University of Nebraska-Lincoln (UNL)"]
+[-8.473251342773438, 13.649309158325195, "Environmental Parameter Importance Essential for managing agricultural crops and predicting their yields"]
+[2.936220645904541, -2.05783748626709, "Satellite Dragsail Unknown"]
+[2.908479928970337, -2.0521156787872314, "Satellite Dragsail Unknown"]
+[2.96288800239563, -2.070995330810547, "Satellite Dragsail Unknown"]
+[0.4995116591453552, 9.224162101745605, "Motion Control Actuation Non-linear rotation of the camera to compensate for the ISS orbital motion"]
+[0.5487666726112366, 11.961407661437988, "Sensor Function Stall warning system"]
+[-0.9730095863342285, 8.676438331604004, "Mechanical Component Function Set and lock the orientation of the NightPod axes"]
+[-1.0085170269012451, 8.494351387023926, "Mechanical Component Connection Connected to the head by two interfaces"]
+[-1.0855361223220825, 8.635854721069336, "Mechanical Component Function Release the system"]
+[2.0765254497528076, -2.65671968460083, "Satellite Engineering Model Quantity 2"]
+[2.52062726020813, -1.742648959159851, "Satellite Material Polycarbonate"]
+[2.7971627712249756, -2.000415563583374, "Satellite Bus Modes of Operation Unknown"]
+[2.7111058235168457, -1.938993215560913, "Satellite Software Protocol Unknown"]
+[1.5059385299682617, -2.355452060699463, "Satellite Orbit Type Highly elliptical"]
+[0.7601004838943481, -1.3992316722869873, "Satellite Perigee Height 600 km"]
+[0.6982811093330383, -1.5752288103103638, "Satellite Apogee Height 60,530 km"]
+[2.3169519901275635, -1.6894035339355469, "Satellite Navigation Optical"]
+[3.0448813438415527, -1.6432198286056519, "Satellite Consortium DEIMOS, Technical University of Denmark (DTU), University Politehnica of Bucharest/Institute of Space Sciences (UPB/ISS)"]
+[-1.5972346067428589, 14.694380760192871, "Photometer Field of View (FOV) Same as that of the camera"]
+[-1.5881153345108032, 14.70852279663086, "Photometer Field of View (FOV) Disk of 700 km radius"]
+[-1.5721015930175781, 14.672554969787598, "Photometer Irradiance Range Requirement Derived from the ISUAL observations"]
+[-1.6379331350326538, 14.728278160095215, "Photometer Sampling Frequency At least 20 kHz"]
+[-1.584228277206421, 14.68211841583252, "Photometer Synchronization Requirement Must be synchronized to be able to compare the recorded waveforms"]
+[1.0148258209228516, 0.781548798084259, "Earth Observation Satellite Development Location Turkey"]
+[5.31491756439209, -4.429888725280762, "Satellite Launch Date Sept. 27, 2003"]
+[5.218866348266602, -4.29459810256958, "Satellite Operation End Date August 2006"]
+[2.571998357772827, -1.8650139570236206, "Satellite Failure Cause Battery system failure"]
+[1.023975133895874, 0.7899063229560852, "Earth Observation Satellite Power Subsystem Unknown"]
+[-1.5524641275405884, 12.827323913574219, "Coronagraph Type Giant, White Light and Emission Line"]
+[-1.5304474830627441, 12.79953670501709, "Coronagraph Mission ESA PROBA-3 Formation FlighT"]
+[2.8992202281951904, 22.16090965270996, "Instruments Purpose Assess if orbital monitoring of plastic might be practical"]
+[-0.2506868839263916, 6.513677597045898, "Test Facility Dimensions 75 m long 9 m wide"]
+[-0.286226361989975, 6.566864967346191, "Test Facility Size Half the size of an Olympic swimming pool"]
+[6.357171535491943, 7.446857452392578, "Satellite Component Material Titanium"]
+[6.194141387939453, 7.5460381507873535, "Satellite Component Number of CCDs 4"]
+[6.336286544799805, 7.405073165893555, "Satellite Component Electrical Isolation Yes"]
+[6.251719951629639, 7.392784595489502, "Satellite Component Thermal Power Dissipation Evacuated to the telescope structure"]
+[-1.3015300035476685, 6.891263961791992, "Technology Unknown Unknown"]
+[-1.2544515132904053, 6.539222240447998, "Acquisition Amount $140 million"]
+[-1.3614859580993652, 6.309560298919678, "Business Strategy Date 10 April 2019"]
+[2.880810499191284, -1.2878167629241943, "Satellite Mission Objectives Global monitoring of oceanographic phenomena and features, provision of oceanographic data, demonstration of key features of an operational ocean dynamics monitoring system"]
+[2.3451387882232666, -1.1383363008499146, "Satellite Sensor Capabilities Wave heights, Wavelength and direction, Surface wind speed and direction, Ocean surface temperature, Atmospheric water content (liquid and vapour), Sea ice morphology and dynamics, Icebergs"]
+[2.464451789855957, -3.4374523162841797, "Communication Satellite Mass 90 kg"]
+[1.906826138496399, 10.71563720703125, "Imaging Device Type Shutter-style"]
+[3.3246853351593018, 0.46587273478507996, "Satellite Program Start Date 1962"]
+[3.3213772773742676, 0.4720229506492615, "Satellite Program Manufacturer RCA (Radio Corporation of America)"]
+[3.322202205657959, 0.4676665961742401, "Satellite Program Various Code Names Program 2, Program 694BH, and Program 417"]
+[1.9278126955032349, 10.732763290405273, "Imaging Device Field of View Not specified"]
+[1.9341834783554077, 10.731060028076172, "Imaging Device Observation Sectors 26 (13 per hemisphere)"]
+[1.9082444906234741, 10.714006423950195, "Imaging Device Photometric Performance Not specified"]
+[-0.9878231883049011, 12.080471992492676, "Transition Radiation Detector Momentum Range 10 to 300 GeV/c"]
+[-1.0710736513137817, 12.094308853149414, "Transition Radiation Detector Particle Types Electrons, positrons, protons, antiprotons"]
+[-0.9893509149551392, 12.097871780395508, "Transition Radiation Detector Principle Detects soft x-rays emitted when charged particles traverse the boundary between two media with different dielectric constants"]
+[-0.9973109364509583, 12.07691478729248, "Transition Radiation Detector Charge Confusion Very small"]
+[2.9043400287628174, -1.9368659257888794, "Satellite Mission Unknown"]
+[2.721527338027954, -1.8742436170578003, "Satellite Sensor Complement Unknown"]
+[0.6729053258895874, 10.99962329864502, "Imaging Sensor Spectral Band (VIS channel) 0.4 - 1.1 \u00b5m"]
+[0.7114810943603516, 10.982442855834961, "Imaging Sensor Nadir Resolution (VIS range) 0.55 km"]
+[0.6793287992477417, 10.990175247192383, "Imaging Sensor Swath Width 2960 km"]
+[0.6829755902290344, 11.001851081848145, "Imaging Sensor Resolution (Infrared channel) ~3.6 km at nadir"]
+[0.6595826745033264, 10.993972778320312, "Imaging Sensor Resolution (Smoothed images) 2.8 km"]
+[0.8085557818412781, -1.6442652940750122, "Satellite Orbit Perigee 600 km"]
+[0.7953726053237915, -1.6984771490097046, "Satellite Orbit Apogee 60,500 km"]
+[0.7275820374488831, -2.260674476623535, "Satellite Orbit Inclination 59\u00ba"]
+[4.182925701141357, -2.845214605331421, "Satellite Orbital Period 19.5 hours"]
+[4.528862476348877, -2.7405953407287598, "Satellite Natural Re-entry Time About 30 months"]
+[16.819713592529297, 6.8758368492126465, "Microsatellite Mass 59 kg"]
+[16.824262619018555, 6.875449180603027, "Microsatellite Mass 22 kg"]
+[1.0123709440231323, -4.41307258605957, "Satellite Mass 157 kg"]
+[16.827138900756836, 6.874233722686768, "Microsatellite Mass 83 kg"]
+[3.737297773361206, 17.698144912719727, "Dummy Payload Mass 80 kg"]
+[14.71379566192627, 7.816483497619629, "Nanosatellite Mass ~7 kg"]
+[14.69820499420166, 7.831791400909424, "Nanosatellite Mass ~3.5 kg"]
+[-5.873379230499268, 15.983953475952148, "Synthetic Aperture Radar Polarization Modes RHCP and LHCP"]
+[-5.905252933502197, 16.02898406982422, "Synthetic Aperture Radar Orbit 536 km"]
+[-5.867067813873291, 16.022985458374023, "Synthetic Aperture Radar Commissioning Start Date 29 April 2012"]
+[-5.874688148498535, 16.022226333618164, "Synthetic Aperture Radar Image Capture Date May 4, 2012"]
+[1.839566707611084, -2.359198808670044, "Satellite Orbit Maintenance Maneuvers 42"]
+[2.047541856765747, -2.529102087020874, "Satellite Collision Avoidance Maneuvers 1"]
+[2.0579910278320312, -2.675122022628784, "Satellite Average Monthly Acquisition Segments Over 4,200"]
+[-0.9883676767349243, 7.8033013343811035, "Device Lateral Movement Twice the movement imaged on the lateral sensor"]
+[-1.0339605808258057, 7.768314361572266, "Device Cropping Effect Decreases power on the two detectors within FLLS"]
+[-1.9131511449813843, 8.073660850524902, "System Method Center-of-mass"]
+[0.6189500689506531, 12.045928001403809, "Sensor Integration Chips located on the sides of a cube"]
+[-0.8339012861251831, 12.667688369750977, "Radiation Monitoring System Measurement Interval Periodically (in minutes)"]
+[-0.8286459445953369, 12.602230072021484, "Radiation Monitoring System Components Two on-board units, commercial RadFETs, thermistor"]
+[0.7246335744857788, -4.155101776123047, "Satellite Launch Mass < 200 kg"]
+[5.3074235916137695, -2.198909282684326, "Satellite Design Life 5 years"]
+[0.6127399802207947, 9.333931922912598, "Attitude Control Subsystem Sensors Fine and Coarse Sun Sensors (FSS & CSS), Magnetometers (MAG), Fiber-optical Gyros (Gyro), and Star Sensors (STS)"]
+[-0.6223585605621338, 8.591097831726074, "Reaction Wheels Quantity 4"]
+[-4.495389938354492, 12.093659400939941, "Magnetorquers Purpose Desaturate the reaction wheel assembly"]
+[-3.57545804977417, 4.396663188934326, "Spacecraft Launch Date December 5, 2014"]
+[-3.028456211090088, 4.245858192443848, "Spacecraft Orbit Type Elliptical orbit"]
+[-3.051588296890259, 4.250239372253418, "Spacecraft Apogee 5800 km"]
+[-3.0126426219940186, 4.184006214141846, "Spacecraft Inclination 28.6\u00ba"]
+[0.009815751574933529, -1.987773060798645, "Satellite Operation True Anomaly 0\u00ba"]
+[0.017809303477406502, -1.9917840957641602, "Satellite Operation Perigee Pass Sun Pointing 161\u00ba"]
+[-0.02662540227174759, -1.9570591449737549, "Satellite Operation CSC Rotation 180\u00ba around xRBF"]
+[0.02626618929207325, -1.9897363185882568, "Satellite Operation Maximum Sun Off-Point 30\u00ba"]
+[-0.010537073016166687, -1.9876904487609863, "Satellite Operation Apogee 180\u00ba"]
+[-0.023014001548290253, -1.9680308103561401, "Satellite Operation CSC Rotation 180\u00ba around xRBF"]
+[0.04202088713645935, -1.9966888427734375, "Satellite Operation Perigee Pass Sun Pointing 360\u00ba"]
+[-13.846863746643066, -2.2423627376556396, "X-ray Telescope Angular Resolution ~ 30 arcseconds"]
+[-13.882092475891113, -2.207195520401001, "X-ray Telescope Sensitivity High"]
+[-13.880326271057129, -2.227679491043091, "X-ray Telescope Number of Compact Sources More than a million"]
+[-13.922764778137207, -2.2420341968536377, "X-ray Telescope Number of Extended Sources Tens of thousands"]
+[2.2896206378936768, 22.210987091064453, "Instrument Measurement Total and spectral solar irradiance"]
+[3.700650930404663, 22.977888107299805, "Instrument Launch Date 2017"]
+[2.5829029083251953, 22.14565658569336, "Instrument Objective Acquire measurements of total and spectral solar irradiance"]
+[-2.4680752754211426, 4.934489727020264, "Debris Removal System Conference Presentation 7th European Conference on Space Debris, ESA/ESOC, Darmstadt/Germany, 18 - 21 April 2017"]
+[-2.4844655990600586, 4.9192938804626465, "Debris Removal System Conference Presentation 7th European Conference on Space Debris, ESA/ESOC, Darmstadt/Germany, 18 - 21 April 2017"]
+[5.3271050453186035, -4.492211818695068, "Satellite Launch Date Jun 12, 2012"]
+[2.8350579738616943, -1.08378005027771, "Satellite Purpose Environmental monitoring, natural resource management, and coastal surveillance"]
+[-0.8670172691345215, 7.985954284667969, "Actuation Device Manufacturer AstroFein (Astro und Feinwerktechnik Adlershof GmbH,)"]
+[-0.8717241883277893, 7.917669296264648, "Actuation Device Manufacturer Clyde Space, UK/Scotland"]
+[-0.8605145812034607, 7.936531066894531, "Actuation Device Quantity 5"]
+[-0.8861312866210938, 7.983510494232178, "Actuation Device Placement 2 on x, 2 on y, and 1 on z-axis"]
+[-1.7395259141921997, 8.849477767944336, "Control System Developer SENER, Spain"]
+[-0.17772293090820312, 15.508004188537598, "Hyperspectral grating Spectrometer Purpose CO2 measurement"]
+[-0.46745800971984863, 15.505051612854004, "Moderate-resolution polarization imaging spectrometer Purpose Cloud and Aerosol measurement"]
+[4.686861038208008, -2.576352119445801, "Satellite Mission Duration 5 years"]
+[3.4830570220947266, 8.114421844482422, "X-ray Detector Mass 4,026 g"]
+[3.4941861629486084, 8.120881080627441, "X-ray Detector Power 2.245 W (BOL)"]
+[3.492201566696167, 8.117802619934082, "X-ray Detector Volume ~34 x 109 x 109 cm3"]
+[3.4946510791778564, 8.12094783782959, "X-ray Detector Effective Area ~95 cm2 (peak)"]
+[3.4948742389678955, 8.120077133178711, "X-ray Detector FOV (Field of View) 30 % sky"]
+[3.4922823905944824, 8.115903854370117, "X-ray Detector Sensitive Range 15 keV \u2013 1 MeV"]
+[3.621180295944214, 13.243925094604492, "Laser Beam Type Diverging"]
+[1.3161441087722778, 10.531242370605469, "Imaging System Depth of Field 25 m to 250 m"]
+[2.6287810802459717, 13.45300579071045, "Optical Component Diameter 50 mm"]
+[-5.331376075744629, 2.77768874168396, "Telescope Components 5 lenses, 2 filters, an alignment cube and a divergent lens"]
+[-0.8413487672805786, 11.608302116394043, "Detector Type Cypress HAS2 CMOS APS detector"]
+[3.6159439086914062, 13.261490821838379, "Laser Type Fiber optic pump laser diode"]
+[3.6168770790100098, 13.257184028625488, "Laser Instantaneous Optical Power 40 W"]
+[1.9049791097640991, 10.73293399810791, "Handheld Ultrasound Device Medical Capabilities Provided to crews on long-term spaceflights where immediate ground support is not an option"]
+[-1.4614641666412354, 13.361754417419434, "Solar Panels Quantity Six"]
+[-1.4423129558563232, 13.326857566833496, "Solar Panels Power Supply Increase in energy available for research and station activities"]
+[-0.6179996132850647, 11.86370849609375, "Plasma Imaging Detector CubeSat Observatory Unknown"]
+[2.602494239807129, 14.280101776123047, "Optical Instrument Aperture Diameter 310 mm"]
+[2.635812282562256, 14.330485343933105, "Optical Instrument Number of Bands 18 Infrared + 1 Visible"]
+[2.628180742263794, 14.31786823272705, "Optical Instrument IFOV 280 \u00b5rad x 280 rad"]
+[2.626098394393921, 14.361250877380371, "Optical Instrument Sampling Interval 280 \u00b5rad"]
+[2.6402053833007812, 14.346891403198242, "Optical Instrument No of Simultaneous Soundings 4 per band"]
+[2.633514642715454, 14.299554824829102, "Optical Instrument Scan Step Angle 10 km E-W, every 0.1 s, and 40 km N-S"]
+[2.6438677310943604, 14.344796180725098, "Optical Instrument Step and Dwell Time 0.1, 0.2 and 0.4 s"]
+[2.694218397140503, 14.391690254211426, "Optical Instrument Turnaround Time 0.1 s per scan"]
+[2.661088466644287, 14.303886413574219, "Optical Instrument Frame Time 160 minutes for 6000 km x 6000 km area sounding"]
+[2.662609100341797, 14.350532531738281, "Optical Instrument Signal Quantization 13 bit/sample"]
+[2.6972129344940186, 14.39028263092041, "Optical Instrument Downlink Data Rate 40 kbit/s"]
+[2.67983078956604, 14.307612419128418, "Optical Instrument Mass 90 kg"]
+[2.6545534133911133, 14.353850364685059, "Optical Instrument Power 100 W"]
+[2.8717195987701416, 22.80839729309082, "Instrument Charge-exchange emission lines and normalized effective area Unknown"]
+[-0.7797294855117798, 5.591691493988037, "Suspension Bridge Length 3.3 km"]
+[-0.7547518014907837, 5.6497955322265625, "Suspension Bridge Main Span Length 1688 m"]
+[-0.7679380774497986, 5.597945213317871, "Suspension Bridge Side Span Length 560 m"]
+[-0.7588584423065186, 5.601466178894043, "Suspension Bridge Material Steel and concrete"]
+[-0.7627425789833069, 5.604750633239746, "Suspension Bridge Consortium Kvaerner-led Joint Venture, the Anglo-Japanese-Turkish Consortium"]
+[-4.521119117736816, 12.115368843078613, "Vector Fluxgate Magnetometer Unknown Unknown"]
+[-0.07586906850337982, 9.826807022094727, "Inertial Measurement Unit Sampling Rate 400 Hz"]
+[-4.496910572052002, 12.110807418823242, "Magnetometer Unknown Unknown"]
+[-0.10624513775110245, 12.652149200439453, "Sun Sensors Quantity 3"]
+[-0.6349560022354126, 8.601316452026367, "Reaction Wheels Torque 25 Nms"]
+[-4.458890438079834, 12.051688194274902, "Magnetic Torque Rods Quantity 3"]
+[-3.2307076454162598, 16.233060836791992, "Radar Scatterometer Frequency 9.6 GHz, 17 GHz"]
+[-3.2524046897888184, 16.24054718017578, "Radar Scatterometer Bandwidth 5 MHz"]
+[-3.269456624984741, 16.23566436767578, "Radar Scatterometer Swath > 1000 km"]
+[-3.2286124229431152, 16.25083351135254, "Radar Scatterometer Peak Power 200 W/150 W"]
+[-3.240525245666504, 16.240907669067383, "Radar Scatterometer Polarisation HH, VV, HV, VH"]
+[-3.2526745796203613, 16.253355026245117, "Radar Scatterometer Antenna Aperture 1.5 m x 1.5 m"]
+[-3.234052896499634, 16.241090774536133, "Radar Scatterometer Incident Angle ~39\u00ba"]
+[-3.226517677307129, 16.229265213012695, "Radar Scatterometer Sigma 0 (\u03c30) Range HH, VV: +15~-25 dB HV,VH: +5~-35 dB"]
+[-3.2218916416168213, 16.232891082763672, "Radar Scatterometer Sigma 0 Precision 0.5 dB"]
+[-3.243999719619751, 16.24971580505371, "Radar Scatterometer Raw Resolution 50 m (azimuth) x 15 km (elevation)"]
+[-3.2312839031219482, 16.24626922607422, "Radar Scatterometer Reconstructed Resolution for SWE (Snow Water Equivalent) 2 - 5 km"]
+[1.891456127166748, -2.1244194507598877, "Satellite Orbit Over sea and land ice"]
+[0.4720973074436188, 4.524838924407959, "Natural Phenomenon Freeboard Total height of the snow cover and sea ice that floats above the ocean"]
+[4.422873497009277, -2.7357568740844727, "Satellite Observation Duration About a month"]
+[3.7180702686309814, -2.5507431030273438, "Satellite Image Collection Frequency Every 30 minutes"]
+[-2.1633942127227783, 2.906320810317993, "Observatory Data Collection Detail Collects less detail on individual outbursts"]
+[-2.141441822052002, 2.9165971279144287, "Observatory Data Collection Duration Provides a longer baseline"]
+[-2.227442741394043, 2.873138427734375, "Space-based Observatory Function Planet-hunting"]
+[-2.213317632675171, 2.8659470081329346, "Space-based Observatory Event Watched a black hole tear apart a star"]
+[-2.2057297229766846, 2.8695602416992188, "Space-based Observatory Event Name ASASSN-19bt"]
+[-2.215848922729492, 2.8655922412872314, "Space-based Observatory Event Start Date September 26, 2019"]
+[-5.71854829788208, 15.96426010131836, "SAR Antenna Polarization Modes SP: Single Polarization, DP: Dual Polarization, FP: Full Polarization (quad), CP: Compact Polarization"]
+[0.8036295175552368, -1.3666819334030151, "Satellite Field of Regard (FOR) Up to about 3 times (from 870 km on Daichi to 2,320 km)"]
+[-6.770768642425537, 10.034608840942383, "Antenna Orientation Nadir (left) and in right-side looking direction"]
+[3.573411226272583, 13.853785514831543, "Laser Ranging Interferometer Effectiveness Demonstration Improving the low-low SST measurement performance"]
+[4.705793380737305, -2.5446372032165527, "Satellite Mission Length 5 years"]
+[1.9084954261779785, -1.3223237991333008, "Satellite Measurement Type Satellite gravimetry"]
+[1.0224376916885376, -4.351751804351807, "Satellite Contribution New fundamental insights into the changing mass distribution"]
+[2.819932222366333, 22.353605270385742, "Instrument Type Hyperspectral imagers"]
+[3.6601738929748535, 22.95901870727539, "Instrument Launch Date Dec. 14, 1998"]
+[3.627596139907837, 22.9249324798584, "Instrument End of Life Date Nov. 12, 2002"]
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+[-0.1088065654039383, 15.487528800964355, "Spectrometer Spatial Coverage 10 - 60 km"]
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+[1.7919660806655884, 10.92102336883545, "Imaging Mode Purpose Provide wide area images along with a few sets of neighboring snap shot images"]
+[1.7419036626815796, 10.919358253479004, "Imaging Mode Purpose Acquire the stereo imagery of the target area"]
+[1.7775275707244873, 10.89587688446045, "Imaging Mode Purpose Acquire zonal imagery - a continuous image with a maximum length of 850 km and a width of 10 km"]
+[3.7168147563934326, 17.693742752075195, "Payload Deployment Date Flight day one"]
+[3.6876986026763916, 17.661516189575195, "Payload Retrieval Date Aug. 16, 1997"]
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+[-4.965631008148193, 2.903796434402466, "Space Telescope Principal Goal Detect small planets with bright host stars in the solar neighborhood"]
+[1.5473544597625732, 2.442575216293335, "Geostationary Weather Monitoring Satellite Operational Life 14 years"]
+[-5.326492786407471, 3.0688161849975586, "Telescope Array URL http://www.nustar.caltech.edu/uploads/updates/NuSTAR_2009oct_update.pdf"]
+[-5.312807559967041, 3.060783863067627, "Telescope Array URL http://www.orbital.com/newsinfo/publications/NuStar_Fact.pdf"]
+[-0.08451292663812637, 13.564541816711426, "Measurement System Conference Date March 6-13, 2010"]
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+[-1.0191807746887207, 7.705419063568115, "Device Tethered Yes"]
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+[3.8969759941101074, 8.976351737976074, "Shuttle Launch Date Nov. 28 - Dec. 8, 1983"]
+[3.894243001937866, 8.975385665893555, "Shuttle Launch Date March 24 - April 2, 1992"]
+[3.8828349113464355, 8.967737197875977, "Shuttle Launch Date Jul. 31, 1992 - Jun. 21, 1993"]
+[3.894582986831665, 8.971405982971191, "Shuttle Launch Date April 8-17, 1993"]
+[3.8884994983673096, 8.970288276672363, "Shuttle Launch Date Nov. 3-14, 1994"]
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+[3.893177032470703, 8.971436500549316, "Shuttle Launch Date Jan. 16-Feb. 1, 2003"]
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+[-4.45548677444458, 7.428280830383301, "Data Dissemination System Transmission Rate 2400 bit/s"]
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+[-4.4153923988342285, 7.398054122924805, "Data Dissemination System Bandwidth \u00b110 kHz"]
+[-5.798526763916016, 8.500483512878418, "Downlink Channel Center Frequency 1695.6938 MHz"]
+[-5.772809982299805, 8.556458473205566, "Downlink Channel Center Frequency 1695.7250 MHz"]
+[-5.7933197021484375, 8.511932373046875, "Downlink Channel Center Frequency 1695.7562 MHz"]
+[-5.856391429901123, 8.548430442810059, "Downlink Channel Center Frequency 1695.7874 MHz"]
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+[2.579346179962158, -2.1636462211608887, "Satellite Navigation Message Consistent with the transmission protocol"]
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+[-3.1055288314819336, 4.258316516876221, "Spacecraft Docking Port Space-facing port on the station\u2019s Harmony module"]
+[-3.082792282104492, 2.447774887084961, "Mission Launch Date 03 June 2021"]
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+[3.5031070709228516, 13.818902015686035, "Laser Interferometer Space Antenna Mission Duration 8 March to 5 May 2017"]
+[-3.0878384113311768, 2.4169085025787354, "Mission Technology Demonstration Detect gravitational waves from space"]
+[-1.2107657194137573, 8.624186515808105, "Component Distortion Measurement Affects the fabric of spacetime on the minuscule scale of a few millionths of a millionth of a meter over a distance of a million kilometers"]
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+[-1.3113811016082764, 4.269015312194824, "Ground-based Relay Uplink Frequency X-band"]
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+[-5.8639020919799805, 15.995712280273438, "Synthetic Aperture Radar (SAR) Mission Copernicus expansion"]
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+[-0.5773633718490601, 8.168686866760254, "Structure Number of Accelerometers 22"]
+[-0.5562154650688171, 8.180469512939453, "Structure Number of Load Cells 6"]
+[-0.6476544141769409, 8.12514877319336, "Structure Number of Micro-g Accelerometers 24"]
+[-0.6187214851379395, 8.26292896270752, "Structure Frequency Range of Shaker Tests 9-300 Hz"]
+[-0.6004149913787842, 8.174736022949219, "Structure Load Range of Shaker Tests 0.048 to 0.00055 kg"]
+[6.3991193771362305, 7.337963104248047, "Satellite Component Gyro-holding Mode Keeps the antenna pointed into the same location in the sky during periods when the beacon is suddenly lost"]
+[6.345693111419678, 7.444108009338379, "Satellite Component Tracking Test Speed Approximately 10 km/h"]
+[6.3458757400512695, 7.393115997314453, "Satellite Component Static Cold Start Acquisition Time < 720 s"]
+[6.325940132141113, 7.411068916320801, "Satellite Component Static Warm Start Acquisition Time < 300 s"]
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+[6.328647136688232, 7.417396545410156, "Satellite Component Moving Warm Start Acquisition Time < 300 s"]
+[8.491220474243164, 15.22157096862793, "Camera Mount Motion Compensation Yes"]
+[8.499746322631836, 15.233908653259277, "Camera Mount Installation Date February 24, 2012"]
+[8.49156665802002, 15.222110748291016, "Camera Mount Operation All Crew Members flying to the ISS"]
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+[2.9000775814056396, -1.365049958229065, "Satellite Mission Carbon Dioxide (CO2) detection and monitoring"]
+[5.157145023345947, -4.332402229309082, "Research Satellite Launch Date August 2017"]
+[4.702762126922607, -2.5823183059692383, "Research Satellite Minimum Mission Life 5 years"]
+[-0.8471928238868713, 0.16911134123802185, "Satellite System Development Lead JPL"]
+[-0.8590425252914429, 0.1812489926815033, "Satellite System Partner Astrium GmbH"]
+[-1.0964521169662476, 6.698624610900879, "Project Phase 1 Date October and November 2019"]
+[-1.0837359428405762, 6.6611456871032715, "Project Phase 2 Date July and August 2021"]
+[-0.9845939874649048, 7.431146621704102, "Individual Emissions Cut Target At least 50% by 2030"]
+[-1.546038031578064, 9.322839736938477, "Gas Warming Power More than 80 times the warming power of carbon dioxide over 20 years"]
+[1.9555152654647827, 10.660191535949707, "Imaging Device Data Collection Time About 45 minutes before the tornado touched down"]
+[0.5458618402481079, 4.338741779327393, "Weather Phenomenon Maximum Altitude Tropopause"]
+[0.5621615052223206, 4.344330310821533, "Weather Phenomenon Formation Process Intense updrafts puncture the tropopause and airflow draws cirrus cloud tops into the stratosphere"]
+[6.279179096221924, 7.459676742553711, "Satellite Component Mission Lifetime 15 years"]
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+[1.384310007095337, -1.577120065689087, "Satellite Formation Control Accuracy Less than 1 mm"]
+[-3.0770723819732666, 4.3433380126953125, "Coronagraph SpaceCraft Wet Mass ~300 kg"]
+[-3.0437700748443604, 4.148799896240234, "Occulter SpaceCraft Wet Mass ~250 kg"]
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+[-2.4594521522521973, 13.128314018249512, "Multispectral Camera Repeat Cycle 31 days"]
+[-2.463968276977539, 13.124580383300781, "Multispectral Camera Mass 115 kg"]
+[-2.4643642902374268, 13.10346794128418, "Multispectral Camera Power Consumption 66 W"]
+[-2.50201416015625, 13.082725524902344, "Multispectral Camera Data Rate 68 Mbit/s"]
+[2.081760883331299, -1.4571031332015991, "Satellite Optical Payloads Operating in the visible spectrum with resolutions in the range of 2 to 60 meters"]
+[2.1870250701904297, -1.953199028968811, "Satellite Configuration Similar to those of CBERS-3 & 4 satellites, with improvements to accommodate the new Chinese Imager camera"]
+[2.5224719047546387, -1.8187644481658936, "Satellite Modules Service Module and a Payload module"]
+[3.0368292331695557, 22.802797317504883, "Instrument Unknown Unknown"]
+[-0.7214220762252808, 8.914246559143066, "Thermal Control Subsystem Roll Axis Rotation \u00b1 36\u00b0"]
+[-0.751835823059082, 8.91130542755127, "Thermal Control Subsystem Heat Dissipating Packages Number of packages"]
+[-0.7502012252807617, 8.867427825927734, "Thermal Control Subsystem Thermal Control Elements OSR (Optical Solar Reflector), MLI (Multilayer Insulation), paints, thermal control tapes, quartz wool blanket, sink plates and heat pipes"]
+[2.477102279663086, -1.7241464853286743, "Satellite SAR Antenna Deployment Mechanism Employed"]
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+[-1.947386622428894, 14.884539604187012, "Earth radiation budget radiometers Instrument Type Earth radiation budget radiometers"]
+[-2.5462396144866943, 12.230162620544434, "High resolution optical imagers Instrument Type High resolution optical imagers"]
+[1.6701122522354126, 6.963707447052002, "Communication Device Purpose Conduct active experiments to quantify spaceborne VLF wave-injection efficiency and determine the details of the wave-particle interactions"]
+[-6.688901901245117, 9.96407699584961, "Antennas Alignment Normal to the local magnetic field line when spacecraft is within \u00b120\u00ba of equatorial"]
+[-6.689487934112549, 9.966960906982422, "Antennas Pointing Requirements 2\u00ba control and a 1\u00ba knowledge requirements"]
+[1.9621446132659912, -2.1846117973327637, "Satellite Orbit Type Geostationary"]
+[2.135559558868408, -2.7111916542053223, "Satellite Number of Ka-band user beams 53"]
+[2.075847864151001, -2.7460696697235107, "Satellite Number of gateway beams 4"]
+[2.098457098007202, -0.5179855823516846, "Satellite Payload Electrical Power Approximately 8.0 kW"]
+[5.234238147735596, -3.795942783355713, "Satellite Launch Year 2018"]
+[-3.8483028411865234, 6.819819450378418, "Data Collection Platforms Report Schedule Several times per hour to once every 24 hours"]
+[-3.8292272090911865, 6.857065200805664, "Data Collection Platforms Number of Timeslots per Hour 40"]
+[-3.8686161041259766, 6.852410316467285, "Data Collection Platforms Maximum Report Duration About one minute"]
+[-3.823577642440796, 6.85530948638916, "Data Collection Platforms Guard Time At least 30 seconds"]
+[-3.870102643966675, 6.825345516204834, "Data Collection Platforms Transmission Duration About 10 seconds"]
+[-0.9505599737167358, -10.011241912841797, "Satellite Constellation Number of active satellites 17/24"]
+[-0.9395095109939575, -9.982333183288574, "Satellite Constellation Number of orbital planes 6"]
+[-0.9585217237472534, -9.98710823059082, "Satellite Constellation Orbital inclination 55\u00ba"]
+[-0.9450720548629761, -10.009930610656738, "Satellite Constellation Orbital altitude 20,180 km"]
+[-0.971661388874054, -9.978739738464355, "Satellite Constellation Orbital period 11 h 58 m"]
+[2.052973508834839, -2.6028213500976562, "Satellite Number of active satellites 2/24"]
+[2.071718692779541, -2.749415636062622, "Satellite Number of orbital planes 3"]
+[0.7250763773918152, -2.2460484504699707, "Satellite Orbital inclination 64\u00ba"]
+[0.5498098731040955, -1.475378155708313, "Satellite Orbital altitude 19,140 km"]
+[0.8036704659461975, -1.6373757123947144, "Satellite Orbital period 11 h 15 m"]
+[2.0785255432128906, -2.657559633255005, "Satellite Number of active satellites 6/24"]
+[2.0932979583740234, -2.7419185638427734, "Satellite Number of orbital planes 3"]
+[0.792924165725708, -2.225414991378784, "Satellite Orbital inclination 56\u00ba"]
+[0.5075099468231201, -1.4891235828399658, "Satellite Orbital altitude 23,222 km"]
+[1.2128812074661255, -1.8412268161773682, "Satellite Orbital period 14 h 22 m"]
+[5.259922504425049, -4.431943893432617, "Satellite First launch date October 2012"]
+[5.114804744720459, -4.025372505187988, "Satellite First launch date Planned 2020"]
+[2.130476236343384, -2.6993489265441895, "Satellite Number of DASS POC payloads with S-band 16"]
+[2.135064125061035, -2.7229795455932617, "Satellite Number of additional DASS POC payloads with S-band anticipated to be deployed by 2019 12"]
+[2.089895009994507, -2.761540412902832, "Satellite Number of L-band MEOSAR payloads 2"]
+[2.1170172691345215, -2.7154123783111572, "Satellite Number of L-band payloads scheduled for operational deployment by 2019 Approximately 35"]
+[2.866126775741577, 21.992023468017578, "Instrument Purpose Provides high-resolution imagery and atmospheric measurements for short-term forecasts and severe weather warnings"]
+[2.843554735183716, 21.986961364746094, "Instrument Environmental Hazards Detection Wildfires, dust storms, volcanic eruptions, turbulence, and fog"]
+[2.4562268257141113, 22.25457000732422, "Instrument Post-Launch Testing Status Undergoing testing, validation and calibration"]
+[-4.566715240478516, -3.084803819656372, "Exoplanet Size Compared to Earth 2.4 times larger"]
+[-4.603221893310547, -3.133741855621338, "Exoplanet Orbit Period 5.7 days"]
+[-4.565839767456055, -3.0863442420959473, "Exoplanet Mass Compared to Earth 7 times Earth\u2019s mass"]
+[-4.563156604766846, -3.0848679542541504, "Exoplanet Size Compared to Earth 2.1 times larger"]
+[-4.579547882080078, -3.106823444366455, "Exoplanet Orbit Period 11.4 days"]
+[-4.562122344970703, -3.083559274673462, "Exoplanet Mass Compared to Earth 5 times Earth\u2019s mass"]
+[-4.562976360321045, -3.096985101699829, "Exoplanet Equilibrium Temperature 150\u00ba Fahrenheit (66\u00ba C)"]
+[-6.7426018714904785, 10.013296127319336, "Antenna Frequency 5.350 GHz"]
+[-6.763646602630615, 10.027203559875488, "Antenna Size 6 m (along-track) x 2 m (cross-track)"]
+[-6.692887783050537, 9.970439910888672, "Antenna Side Lobe Level -13 dB (azimuth), -13 dB (elevation)"]
+[-2.697441816329956, 8.770105361938477, "Module Quantity 288"]
+[-2.7062861919403076, 8.756799697875977, "Module Peak Power 10 W"]
+[-1.9143245220184326, 8.097052574157715, "System Pulse Width 20/10 \u00b5s"]
+[-1.9341001510620117, 8.112432479858398, "System Average DC Input Power 1.8-3.9 kW"]
+[-1.9546465873718262, 8.072759628295898, "System Operating Mode HRS FRS-1 FRS-2 MRS/CRS"]
+[-1.897745132446289, 8.070000648498535, "System Chirp Bandwidth 225 MHz 75 MHz 37.5 MHz 18.75 MHz"]
+[-1.8713699579238892, 8.053686141967773, "System Sampling Rate 250 MHz 83.3 MHz 41.67 MHz 20.83 MHz"]
+[-1.9424382448196411, 8.088146209716797, "System PRF 3500 Hz \u00b1 200 Hz 3000 Hz \u00b1 200 Hz 3000 Hz \u00b1 200 Hz 3000 Hz \u00b1 200 Hz"]
+[-1.9117671251296997, 8.116654396057129, "System Data Quantization 2/3 BAQ 2/3/4/5/6 bit BAQ"]
+[-1.9286246299743652, 8.092535018920898, "System Data Rate 739 Mbit/s (single pol.) 1478 Mbit/s (dual pol.) 556 Mbit/s (single pol.) 1112 Mbit/s (dual pol.) 564 Mbit/s 142 Mbit/s (single pol.) 284 Mbit/s (dual pol.)"]
+[-1.8978276252746582, 14.87230396270752, "Radiometer Spectral Bands 6"]
+[-1.9115437269210815, 14.867766380310059, "Radiometer Visible Band Resolution 1 km"]
+[-1.8590149879455566, 14.820770263671875, "Radiometer SWIR Band Resolution 1 km"]
+[-1.955825686454773, 14.846139907836914, "Radiometer MWIR Band Resolution 4 km"]
+[-1.8952710628509521, 14.860098838806152, "Radiometer TIR Channel Resolution 4 km"]
+[-1.883852481842041, 14.880073547363281, "Radiometer TIR Channel Windows 10.2-11.2 and 11.5-12.5 \u00b5m"]
+[-1.9037846326828003, 14.849327087402344, "Radiometer Visible Channel Resolution 1 km"]
+[-1.906645655632019, 14.861858367919922, "Radiometer Thermal IR Channels Resolution 4 km"]
+[7.197453022003174, 12.324535369873047, "Remote Sensing Instruments Operation Principle Sending radio or laser light pulses toward Earth\u2019s surface and recording the reflections as they bounce back"]
+[7.083768844604492, 12.200222969055176, "Remote Sensing Instruments Measurement Method By measuring the time between the outgoing and returning signal, and knowing the precise altitude of the satellite above ground"]
+[7.199354648590088, 12.331233024597168, "Remote Sensing Instruments Application Measure changes to ice elevation"]
+[2.591240406036377, 14.261802673339844, "Optical Instrument Aperture Diameter 310 mm"]
+[2.653278112411499, 14.338279724121094, "Optical Instrument Number of Bands 6"]
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+[2.680192470550537, 14.361187934875488, "Optical Instrument Band 5 Wavelength Range 10.3 - 11.3 \u00b5m"]
+[2.6340622901916504, 14.319580078125, "Optical Instrument Band 6 Wavelength Range 11.5 - 12.5 \u00b5m"]
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+[2.627488374710083, 14.306052207946777, "Optical Instrument Band Separation Beam splitter, interference filters"]
+[2.6361117362976074, 14.353671073913574, "Optical Instrument IFOV for VIS and SWIR 28 \u00b5rad (1 km)"]
+[2.597166061401367, 14.292006492614746, "Optical Instrument IFOV for MWIR, TIR-1, & TIR-2 112 \u00b5rad (4 km)"]
+[2.6530964374542236, 14.27563762664795, "Optical Instrument IFOV for WV 224 \u00b5rad (8 km)"]
+[2.6235921382904053, 14.347238540649414, "Optical Instrument Sampling Interval for VIS, SWIR,MIR & TIR-1 / -2 1.75 samples / IFOV"]
+[2.642493486404419, 14.33585262298584, "Optical Instrument Sampling Interval for WV 3.5 samples / IFOV"]
+[2.5887999534606934, 14.277801513671875, "Optical Instrument Scan Step Angle 8 \u00b5rad step size"]
+[2.6187193393707275, 14.357351303100586, "Optical Instrument Line Step 224 \u00b5rad in N-S direction"]
+[2.673699140548706, 14.356367111206055, "Optical Instrument Scan Rate 200\u00ba/s"]
+[2.639281988143921, 14.336418151855469, "Optical Instrument Turnaround Time +0.2 s"]
+[2.6403746604919434, 14.308294296264648, "Optical Instrument Full Aperture Blackbody and Space Views Scan modes Full, normal and programmable sector for quick repetivity"]
+[2.684786796569824, 14.320391654968262, "Optical Instrument Frame Time 25 minutes for normal mode"]
+[2.7153401374816895, 14.232827186584473, "Optical Instrument Signal Quantization 10 bit/sample"]
+[2.6527905464172363, 14.35000991821289, "Optical Instrument Source Data Rate 4.0 Mbit/s"]
+[-5.2480387687683105, 2.7343368530273438, "Telescope Observation Date Between October and December 2018"]
+[-5.346696853637695, 2.741577386856079, "Telescope Observation Date 2019 and 2020"]
+[4.944647312164307, -4.244146347045898, "Satellite Archival Data Collection Date Between 2009 and 2011"]
+[-5.873589515686035, 15.995735168457031, "Synthetic Aperture Radar Wave Length about 24 cm"]
+[-5.882477760314941, 16.028799057006836, "Synthetic Aperture Radar Observation Frequency Once a year"]
+[-5.886851787567139, 16.017593383789062, "Synthetic Aperture Radar Emergency Observation Period January 6-16, 2016"]
+[7.289261341094971, 12.420099258422852, "Satellite Instrument Ground Swath 15 km"]
+[7.3376665115356445, 12.458647727966309, "Satellite Instrument Spotlight Mode Resolution 1-2 m"]
+[7.302192687988281, 12.418185234069824, "Satellite Instrument Stripmap Mode Resolution 1-3 m"]
+[7.335239887237549, 12.44395637512207, "Satellite Instrument ScanSAR Mode Resolution 5-30 m"]
+[-1.9367905855178833, 8.110017776489258, "System Redundancy Fully redundant"]
+[-1.9341765642166138, 8.120704650878906, "System Reconfigurability Can be reconfigured on orbit"]
+[-5.222285747528076, 7.865321159362793, "Communication System Encryption NSA Type-1/2 encryption"]
+[-0.8037362694740295, 8.854528427124023, "Thermal Control System Heater Control Precision"]
+[-3.0331130027770996, 4.2421040534973145, "Spacecraft Propulsion For orbit establishment, maintenance, collision avoidance, and end-of-life (EOL) disposal"]
+[6.3430705070495605, 7.399633884429932, "Satellite Component FUS Baseplate Tilt 15\u00ba"]
+[6.3437066078186035, 7.402291774749756, "Satellite Component CPA Azimuth Rotation Axis Distance More than 3\u00ba"]
+[6.356318473815918, 7.384554862976074, "Satellite Component HTS Condenser Plate Interface Connected to dedicated radiators through heat pipe networks"]
+[0.35702913999557495, 4.686762809753418, "Natural Event Magnitude 7.8"]
+[0.36779704689979553, 4.641221523284912, "Natural Event Date 23 Mar 2017"]
+[0.42433783411979675, 4.609613418579102, "Natural Event URL http://science.sciencemag.org/content/early/2017/03/22/science.aam7194"]
+[-13.80322265625, -2.2775063514709473, "X-Ray Telescope Mission Duration 10 Years"]
+[-13.691627502441406, -2.3381409645080566, "X-Ray Telescope Discovery Date 1 March 2022"]
+[-2.5735132694244385, 9.681127548217773, "Energy Source Efficiency 24%"]
+[-2.5709152221679688, 9.697643280029297, "Energy Source Cell Types GaInP/GaAs/Ge"]
+[-2.5554141998291016, 9.716176986694336, "Energy Source Absorption Wavelength 300 nm to 650 nm"]
+[-2.5637049674987793, 9.701102256774902, "Energy Source Efficiency Comparison 24% efficient under air mass zero (AM0) compares favorably to silicon solar cells that are 16% efficient or GaAs cells at 20% efficiency"]
+[2.6656601428985596, -1.6801570653915405, "Satellite Ice Loss Detection Yes"]
+[-3.6420557498931885, 12.757485389709473, "Particle Detector Particle Bending Opposite directions"]
+[-3.6442928314208984, 12.757878303527832, "Particle Detector Matter/Antimatter Separation Left-positive, right-negative"]
+[1.5119460821151733, -1.4735126495361328, "Satellite Spectral Calibration Accuracy Superior to 1/10 FWHM"]
+[1.5278048515319824, -1.7830910682678223, "Satellite Radiometric Calibration Accuracy (Relative) 3%"]
+[1.667602300643921, -1.7794452905654907, "Satellite Radiometric Calibration Accuracy (Absolute) 5%"]
+[0.24269968271255493, 13.802897453308105, "OnBoard Calibrator Calibration Method LED + solar calibration"]
+[-0.9405642747879028, 7.757770538330078, "Device Calibration Method LED +lunar + solar calibration"]
+[2.0253350734710693, -1.6784768104553223, "Satellite Observation Mode Nadir observation mode"]
+[2.0011537075042725, -1.6700273752212524, "Satellite Observation Mode Sun-glint observation mode"]
+[-3.2975432872772217, 8.77231216430664, "Memory Module User Storage Capacity 2.4 Tbit (EoL)"]
+[-3.3032712936401367, 8.76838207244873, "Memory Module Mass \u2264 29 kg"]
+[-3.281569242477417, 8.764384269714355, "Memory Module Max Volume 710 mm x 260 mm x 310 mm"]
+[-3.2584762573242188, 8.803021430969238, "Memory Module Power (record & replay) \u2264 130 W"]
+[-3.279310703277588, 8.771841049194336, "Memory Module Power (data retention) < 29 W (0 W)"]
+[-3.3206241130828857, 8.746352195739746, "Memory Module Instrument Input Data Rate 490 Mbit/s + 80 kbit/s (housekeeping)"]
+[-3.3179943561553955, 8.795105934143066, "Memory Module Output Data Rate (downlink) 2 x 280 Mbit/s"]
+[-3.2834761142730713, 8.767487525939941, "Memory Module Life Time in Orbit Up to 12.5 years"]
+[-3.3009145259857178, 8.764151573181152, "Memory Module Reliability \u2265 0.98"]
+[-3.342665672302246, 8.758545875549316, "Memory Module Bit Error Rate (GCR) \u2264 9 x 10 -13  / day"]
+[0.548952579498291, 4.671848773956299, "Phenomenon Count 25,998"]
+[0.550323486328125, 4.6525373458862305, "Phenomenon Count 2,300"]
+[0.555194616317749, 4.662066459655762, "Phenomenon Count 2,043"]
+[0.566067636013031, 4.668463706970215, "Phenomenon Count 4,720"]
+[0.5530005097389221, 4.659958362579346, "Phenomenon Count 104"]
+[-3.797741174697876, 6.917917728424072, "Data Collection Observation Period 17 years"]
+[-0.547033429145813, 4.9190239906311035, "Region Above-Normal Precipitation 3 to 5 inches"]
+[-0.40489840507507324, 5.063060283660889, "Water Level Running Above the 95th Percentile Yes"]
+[1.438312292098999, 2.75221586227417, "Weather Forecast Issued Date December 7"]
+[1.4336596727371216, 2.7559211254119873, "Weather Forecast Forecast Period Next week"]
+[-1.8834964036941528, 14.88931941986084, "Interferometric Radiometer System Complexity Lower than two-dimensional interferometric radiometers"]
+[-1.8639514446258545, 14.916959762573242, "Interferometric Radiometer Calibration Accuracy Higher than two-dimensional interferometric radiometers"]
+[-1.8495275974273682, 14.868648529052734, "Interferometric Radiometer Spatial Resolution Better than real aperture system"]
+[-1.8098498582839966, 14.9690523147583, "Interferometric Radiometer Observation Swath Wider than real aperture system"]
+[-1.8981895446777344, 14.918171882629395, "Interferometric Radiometer Frequency Bands S- and C-band"]
+[-1.8740469217300415, 14.876893997192383, "Interferometric Radiometer Application Soil moisture observation, salinity and sea surface temperature"]
+[-1.869839072227478, 14.871715545654297, "Interferometric Radiometer Simulation Platform Matlab"]
+[-1.8965848684310913, 14.869572639465332, "Radiometer Bands Three bands in the visible (VIS) and thermal infrared (TIR) ranges"]
+[-1.8874883651733398, 14.862539291381836, "Radiometer Spatial Resolution 560 metres in fine mode and 2.7 km in smooth mode"]
+[-1.9028520584106445, 14.911382675170898, "Radiometer Frequency Range 19-184 GHz"]
+[-1.9359281063079834, 14.840532302856445, "Radiometer Spatial Resolution Varies with the frequency with the highest spatial resolution of 25 km x 17 km and the lowest at 70 km x 42 km"]
+[0.7789488434791565, -1.151758074760437, "Satellite Altitude Ranging between 833 km and 850 km"]
+[0.6703484058380127, -2.2470571994781494, "Satellite Orbital Inclination 98.7\u00b0"]
+[4.139317989349365, -2.824598550796509, "Satellite Orbital Period 101 minutes"]
+[0.4715852737426758, 4.542698383331299, "Natural Phenomenon Annual Maximum Extent Date August 31"]
+[0.47506183385849, 4.528552532196045, "Natural Phenomenon Daily Record Lows Reached by November"]
+[0.4582761824131012, 4.528425693511963, "Natural Phenomenon Air Temperatures 2 to 4 degrees Celsius above average"]
+[0.4903812110424042, 4.526953220367432, "Natural Phenomenon Annual Minimum Extent Date February"]
+[0.46773165464401245, 4.525439262390137, "Natural Phenomenon Total Extent Increase About 1 percent per decade since 1979"]
+[-2.651113510131836, 11.662826538085938, "Imager No of Spectral Bands 16"]
+[-2.632335901260376, 11.678771018981934, "Imager Data Rate 2.6 Mbit/s - 75 Mbit/s"]
+[-2.636056423187256, 11.66860580444336, "Imager Spatial Resolution (VIS) 0.64 \u00b5m"]
+[-2.6570277214050293, 11.647482872009277, "Imager Time for Full Disk Scan 26 minutes, 15 or 5 minutes"]
+[-2.627317428588867, 11.713058471679688, "Imager Absolute INR 54 \u00b5rad (EW), 21 \u00b5rad (NS)"]
+[-2.6187453269958496, 11.70128059387207, "Imager Registration Between Images 36 \u00b5rad (0.5, 1.0 km), 16 \u00b5rad (0.5, 1.0 km), 21 \u00b5rad (2.0 km)"]
+[-2.626309871673584, 11.672394752502441, "Imager Cross-channel Image Co-registration 50 \u00b5rad (VIS to IR), 28 \u00b5rad (IR to IR), 6.3 \u00b5rad (0.5, 1.0 to2 km), 5.2 \u00b5rad (0.5, 1.0 to1 km)"]
+[-2.6686642169952393, 11.674355506896973, "Imager VIS (Reflective Bands) Calibration Yes"]
+[0.5718498826026917, 4.673121929168701, "Phenomenon Detection Confirmed"]
+[2.5007989406585693, -1.9198541641235352, "Satellite Follow-on Satellite ALOS-2"]
+[5.089993953704834, -4.6371941566467285, "Satellite Workshop Date Jan. 26-30, 2009"]
+[2.489438533782959, -1.863721251487732, "Satellite Workshop Location ESA/ESRIN, Frascati, Italy"]
+[2.578096389770508, -3.9222750663757324, "Satellite URL http://earth.esa.int/workshops/polinsar2009/participants/535/pres_8_Shimada_535.pdf"]
+[-0.8030680418014526, 12.62627124786377, "Total Ionizing Dose Sensitive Devices Gate-Oxide Thickness 400 nm"]
+[-0.8382202386856079, 12.712268829345703, "Total Ionizing Dose Sensitive Devices Gate-Oxide Thickness 1 \u00b5m"]
+[-0.82288658618927, 12.693018913269043, "Total Ionizing Dose Sensitive Devices Idle State Irradiation mode"]
+[-0.8335100412368774, 12.6671781539917, "Total Ionizing Dose Sensitive Devices Terminal States Grounded"]
+[-0.8672513365745544, 11.627389907836914, "Area-source Detector Field of View Hundreds of kilometres wide"]
+[-0.8459099531173706, 11.568181037902832, "Area-source Detector Detection Threshold At least 10 times more sensitive than the current GHGSat satellite"]
+[-0.9198936820030212, 11.529228210449219, "Area-source Detector Size Comparison 10 times bigger than GHGSat"]
+[-0.7599372267723083, 11.535759925842285, "Area-source Detector Purpose Fill critical data and observes gaps between point source and global mapping satellites"]
+[-3.797603130340576, 6.94838285446167, "Reference Database Construction Method Fully automatic matching with acquired image data and image correction"]
+[-1.4183838367462158, 4.342456340789795, "Ground System Overview An overview of the ASNARO ground system"]
+[1.1340733766555786, -0.7227357625961304, "Satellite Size Small school bus"]
+[0.9099786877632141, -4.417708873748779, "Satellite Weight Over 6,000 pounds (~3000 kg)"]
+[3.628020763397217, 18.07600212097168, "Instrument Payload Provider L3Harris Technologies"]
+[3.6569628715515137, 17.912954330444336, "Instrument Payload Type Imager"]
+[3.672145366668701, 17.89718246459961, "Instrument Payload Ground System Provider L3Harris Technologies"]
+[3.705451488494873, 22.927406311035156, "Instrument Conference Presentation Date Sept. 29-Oct. 3, 2014"]
+[2.777435064315796, 22.47884178161621, "Instrument Suite URL http://www.goes-r.gov/spacesegment/seiss.html"]
+[3.154909372329712, 22.492666244506836, "Instrument URL http://www.goes-r.gov/spacesegment/mag.html"]
+[-1.5983165502548218, 4.098910331726074, "Ground Segment Conference Date March 5-12, 2011"]
+[2.7386386394500732, -1.8575984239578247, "Satellite Sensor Complement Unknown"]
+[2.8132078647613525, -1.9353454113006592, "Satellite Ground Segment Unknown"]
+[-1.6207551956176758, 9.691889762878418, "Propulsion System Isp >2,000 s"]
+[-2.1737289428710938, 6.085484027862549, "Flight System Volume 1.6U"]
+[-2.1921961307525635, 6.004968166351318, "Flight System Wet Mass 3 kg"]
+[11.239837646484375, 5.465412616729736, "CubeSat Development Status Passed essential environmental testing"]
+[11.234936714172363, 5.470305919647217, "CubeSat Mission Investigate the amount and distribution of water ice on the Moon"]
+[5.15999174118042, -4.229028701782227, "Satellite Launch Date August 27, 2021"]
+[2.663912296295166, -2.3979721069335938, "Satellite Communication Frequency S-band"]
+[2.0863330364227295, -2.391793966293335, "Satellite Solar Panels Four"]
+[11.236217498779297, 5.546456813812256, "CubeSat First Results Date Next month"]
+[3.173602819442749, -1.5382870435714722, "Satellite Mission Type Non-EO"]
+[5.4396586418151855, -4.590847492218018, "Satellite Launch Date August 8, 2001"]
+[5.132665634155273, -4.213047981262207, "Satellite End of Life Date September 8, 2004"]
+[1.495477557182312, -2.390800952911377, "Satellite Orbit Halo orbit around the Lagrangian point L1"]
+[2.6521077156066895, -1.2240879535675049, "Satellite Objective Monitor the solar wind and to collect particles of the solar wind by ion implantation into the collector materials for a duration of two years, and to return these samples for isotopic and chemical analysis in terrestrial laboratories"]
+[2.784011125564575, 22.073667526245117, "Instrument Objectives In-space engineering testbed for future spaceborne laser altimeters, acquire samples of land topography and vegetation data, measure cloud and aerosol layers in the atmosphere"]
+[1.7688403129577637, 22.163551330566406, "Instrument Laser Footprint Diameter 100 m"]
+[1.7752481698989868, 22.18804168701172, "Instrument Laser Footprint Spacing 700 m"]
+[1.0150378942489624, 0.7771970629692078, "Earth Observation Satellite Purpose Monitor soil moisture and groundwater wetness"]
+[-3.4549524784088135, 6.846323490142822, "Data Product Update Frequency Weekly"]
+[-3.446240186691284, 6.8421854972839355, "Data Product Distribution Online by the National Drought Mitigation Center at the University of Nebraska-Lincoln (UNL)"]
+[-8.473613739013672, 13.648126602172852, "Environmental Parameter Importance Essential for managing agricultural crops and predicting their yields"]
+[-8.50001049041748, 13.652242660522461, "Environmental Parameter Importance Source of water for crop irrigation, sustains streams during dry periods, and is a useful indicator of extended drought"]
+[16.805030822753906, 6.887363433837891, "Microsatellite Mass 2.7 kg"]
+[16.88164710998535, 6.837189197540283, "Microsatellite Observation Objectives Provide hyperspectral imagery for agricultural applications, Acquire visualization of Earth warming by measuring NDVI (Normalized Differential Vegetation Index), Provide high quality video data of Earth's surface using a HDTV (High Definition Television) camera"]
+[16.8912410736084, 6.822530269622803, "Microsatellite Attitude Accuracy \u00b12\u00ba"]
+[16.837284088134766, 6.879446983337402, "Microsatellite ACS Components COTS (Commercial Off The Shelf) parts"]
+[0.2847837209701538, 10.63292407989502, "Vision-Based System Objective Measure the relative state of the target spacecraft"]
+[0.40671151876449585, 10.801860809326172, "Vision-Based System Components Optical sensors and highly advanced image processing techniques"]
+[-1.8925410509109497, 14.8423490524292, "Radiometer Objective Collection of data on shortwave and longwave radiation"]
+[-1.902284860610962, 14.873029708862305, "Radiometer Number of Channels 4"]
+[-1.931844711303711, 14.892888069152832, "Radiometer Main Channels Channels 2 and 3"]
+[-1.9145976305007935, 14.827089309692383, "Radiometer Auxiliary Channels Channels 1 and 4"]
+[-1.896868348121643, 14.86456298828125, "Radiometer Telescopes Four parallel telescopes, one telescope per channel"]
+[-8.097539901733398, 8.818281173706055, "Power Subsystem Components EPS card, battery, solar array"]
+[1.252149224281311, 10.90302848815918, "EPS Card Functions Conditioning the solar array input, regulating the battery charge/discharge cycle, and providing power to the other subsystems"]
+[-8.096309661865234, 8.817283630371094, "Power Subsystem Output Channels Raw battery voltage, regulated 3.3 V, 5 V, and 12 V channels"]
+[-8.104872703552246, 8.81669807434082, "Power Subsystem Fault Protection Overcurrent protection, load switching, autonomous transitions between internal modes based on battery voltage"]
+[5.130730628967285, -4.0442070960998535, "Satellite Launch Date Late 2022"]
+[2.0741865634918213, -1.226562261581421, "Satellite Measurement Types Global mapping, point-source detection, area-source detection"]
+[1.2434042692184448, -1.629516839981079, "Satellite Field of View Wider than a point-source system"]
+[2.0593934059143066, -1.405828595161438, "Satellite Detection Threshold Much lower than a point-source system"]
+[2.4375970363616943, 22.798315048217773, "Instrument Number of Channels 12"]
+[2.204685926437378, 23.039173126220703, "Instrument Frequency Bands Near 90 GHz, 118 GHz, 183 GHz, 206 GHz"]
+[2.890144109725952, 22.054779052734375, "Instrument Purpose Observes the radiance of the atmosphere at microwave wavelengths"]
+[-5.337494850158691, 8.053415298461914, "Communication System X-band Downlink Frequency 8192 MHz"]
+[-5.187236309051514, 7.806169033050537, "Communication System X-band Data Rate 7.68 Mbit/s"]
+[-5.309590816497803, 8.032683372497559, "Communication System UHF Downlink Frequency 466.5 MHz"]
+[2.673611879348755, -2.7294530868530273, "Satellite Data Rate 15.36 or 61.44 Mbit/s"]
+[2.5402159690856934, -2.0812675952911377, "Satellite Modulation Type BPSK (NRZ-M)"]
+[-5.285665988922119, 8.016736030578613, "Communications System Operating Frequency 435-438 MHz"]
+[-5.237837314605713, 7.861375331878662, "Communications System Data Rate 9.6 kbit/s"]
+[-4.751129627227783, 9.272746086120605, "Transmitter Frequency Band 8.025 and 8.4 GHz"]
+[-4.7251105308532715, 9.239557266235352, "Transmitter Polarization RHCP"]
+[-4.753593444824219, 9.264223098754883, "Transmitter Axial Ratio <3dB"]
+[-4.7335028648376465, 9.210037231445312, "Transmitter Gain >0 dBi"]
+[-4.7316155433654785, 9.264690399169922, "Transmitter Return Loss <12 dB"]
+[1.736875295639038, -1.222933053970337, "Satellite Image Resolution Not provided"]
+[0.30771300196647644, 4.553360462188721, "Agricultural Feature Diameter Around 750 m"]
+[-0.8495742678642273, 5.164218425750732, "Italian City Known For World-famous marble"]
+[-0.5921108722686768, 4.9388837814331055, "Region Vegetation Lush green"]
+[2.8896636962890625, -1.2407302856445312, "Satellite Mission Objectives Habitat mapping of coral reefs, Coral reef change detection, Bathymetry over coral reefs"]
+[-3.7524728775024414, 6.9811625480651855, "Data Collection Duration 6 days"]
+[-0.42124471068382263, 6.358984470367432, "Survey Site Water Temperature Exceeding 30\u00b0C"]
+[-0.5581415295600891, 6.322288513183594, "Survey Site Coral Bleaching Observed"]
+[-3.45823335647583, 7.5895915031433105, "Compression Algorithm Error Reduction More than the BAQ technique"]
+[-3.573517322540283, 7.661709785461426, "Compression Algorithm Error Reduction Better than BAQ"]
+[-1.0503126382827759, 7.694316387176514, "Device Compression Modes DS-BAQ, the original BAQ, and direct output without data compression"]
+[2.663193941116333, 22.391035079956055, "Instrument Observation Types Microwave, Electrooptical, Infrared"]
+[5.242343425750732, -3.906724214553833, "Satellite Launch Year 1995"]
+[2.2686846256256104, -1.8094156980514526, "Satellite Imaging Modes Multiple"]
+[2.2088782787323, -1.247922420501709, "Satellite Daily Imagery Usage 3000-4000 scenes"]
+[-3.280334949493408, 4.257025241851807, "Spacecraft Mission Lifetime 7.25 years"]
+[-1.3909788131713867, 9.367637634277344, "Fuel Sizing Duration 12 years"]
+[-3.1959874629974365, 4.154080390930176, "Spacecraft Autonomy 2 weeks"]
+[-3.115974187850952, 4.30047082901001, "Spacecraft Decoupling Maximum"]
+[2.6653525829315186, 5.387482166290283, "Emergency Beacon Accuracy Better than 4 km"]
+[2.706354856491089, 5.3497796058654785, "Emergency Beacon Ambiguity Resolution 90% on first pass"]
+[2.665588140487671, 5.387505054473877, "Emergency Beacon Location Probability Better than 90% on one pass"]
+[-4.405086994171143, 15.74510383605957, "Radar Imager Operation Modes HRS (High Resolution Spotlight), FRS-1 (Fine Resolution Stripmap-1), FRS-2 (Fine Resolution Stripmap-2), MRS (Medium Resolution ScanSAR), CRS (Coarse Resolution ScanSAR)"]
+[-4.252492427825928, 15.565317153930664, "Radar Imager Imaging Modes Co-polarisation and cross-polarisation"]
+[5.199186325073242, -4.18852424621582, "Satellite Launch Date February 2022"]
+[11.289690017700195, 5.5189666748046875, "CubeSat Sensor Pointing Accuracy 1\u00ba"]
+[11.227668762207031, 5.441672325134277, "CubeSat Imager Pointing Accuracy 0.31\u00ba"]
+[2.730435609817505, 21.627931594848633, "Scientific Instrument Purpose Taking pictures of the inner solar corona"]
+[2.9667272567749023, -1.471968173980713, "Satellite Mission Objectives Demonstrate formation flying technologies, obtain scientific results from a coronagraph science payload, including also dedicated rendezvous demonstration"]
+[2.307157516479492, -1.8178616762161255, "Satellite Technology Experiments 6DOF formation control with thrusters, realistic collision avoidance demonstration and technology payloads"]
+[-5.323675632476807, 2.8290536403656006, "Telescope Technology Hard X-ray optics"]
+[-1.0749666690826416, 6.715944766998291, "Mast Heritage SRTM"]
+[-0.830750584602356, 11.593361854553223, "Detector Technology Material Cadmium Zinc Telluride"]
+[-3.2658698558807373, 5.432767868041992, "Launch Vehicle Service Provider ULA"]
+[-3.173255681991577, 4.98248291015625, "Cargo Vehicle Launch Date 2016"]
+[11.793535232543945, 5.363275051116943, "3U CubeSats Quantity 12"]
+[11.811075210571289, 5.3578314781188965, "3U CubeSat Technology Mission University of Michigan"]
+[11.839556694030762, 5.308333396911621, "3U CubeSat Mission Solar physics"]
+[11.542313575744629, 5.627310752868652, "1.5 CubeSats Quantity 2"]
+[11.710576057434082, 5.42827033996582, "1U CubeSat Location Arlington, VA"]
+[16.893680572509766, 6.839841365814209, "Microsatellite Provider NanoRacks"]
+[11.15321159362793, 5.341983795166016, "NanoRacks MicroSat Deployer Purpose Deploy microsatellites from the ISS orbit"]
+[-1.5073856115341187, 16.896390914916992, "Altimeter Radio frequency (GHz) 13.5"]
+[-1.4811410903930664, 16.876474380493164, "Altimeter Swath width (km) 2.8"]
+[-1.5003005266189575, 16.898303985595703, "Altimeter Spatial Resolution (km) 7"]
+[-2.9803855419158936, 16.161588668823242, "Scatterometer System Radio frequency (GHz) 14.6"]
+[-2.9740355014801025, 16.151010513305664, "Scatterometer System Swath width (km) 750+"]
+[-2.984611749649048, 16.167171478271484, "Scatterometer System Spatial Resolution (km) 50"]
+[-2.7293028831481934, 15.305452346801758, "Scanning Multichannel Microwave Radiometer Radio frequency (GHz) 6.6"]
+[-2.7334799766540527, 15.289734840393066, "Scanning Multichannel Microwave Radiometer Swath width (km) 10.7"]
+[-2.697460412979126, 15.344667434692383, "Scanning Multichannel Microwave Radiometer Spatial Resolution (km) 18.0"]
+[-5.889026641845703, 16.009906768798828, "Synthetic Aperture Radar Radio frequency (GHz) 1.3"]
+[-5.904535293579102, 16.020814895629883, "Synthetic Aperture Radar Swath width (km) 100"]
+[-5.887125492095947, 16.002283096313477, "Synthetic Aperture Radar Spatial Resolution (km) 0.025"]
+[-1.503259301185608, 14.866568565368652, "Visible and Infrared Radiometer Radio frequency (GHz) 0.49-0.94"]
+[-1.4802595376968384, 14.862813949584961, "Visible and Infrared Radiometer Swath width (km) 10.5-12.5"]
+[-1.5356395244598389, 14.852409362792969, "Visible and Infrared Radiometer Spatial Resolution (km) 2280"]
+[-0.8430497646331787, 12.737082481384277, "Irradiance Monitor Continuation Provided by TSIS"]
+[-0.8341963291168213, 12.735283851623535, "Irradiance Monitor Continuation Provided by TSIS"]
+[5.104272842407227, -3.996873378753662, "Satellite Launch Date 2023"]
+[2.1448850631713867, -2.7007243633270264, "Satellite Contract Value $32.9 million"]
+[-5.355790138244629, 2.755851984024048, "Telescope Length 33-foot-long (10-meter-long)"]
+[-5.387942790985107, 2.7661476135253906, "Telescope Function Collects X-rays"]
+[-5.440217971801758, 2.7673630714416504, "Telescope Issue Stray light"]
+[-3.7531585693359375, 6.906525135040283, "Data Catalog Number of Objects About 80"]
+[1.6635584831237793, -2.382671594619751, "Satellite Formation Triangular Yes"]
+[3.0178840160369873, -1.4230667352676392, "Satellite Mission Objectives Study the formation and evolution of compact binary stars in the Milky Way galaxy; Trace the origin, growth and merger history of massive black holes across cosmic ages; Probe the dynamics of dense nuclear clusters using extreme mass-ratio inspirals (EMRIs); Understand the astrophysics of stellar-origin black holes; Explore the fundamental nature of gravity and black holes; Probe the rate of expansion of the Universe; Understand stochastic gravitational wave backgrounds and their implications for the early Universe and TeV-scale particle physics; Search for gravitational wave bursts and unforeseen sources"]
+[-1.46280038356781, 13.380293846130371, "Solar Array Panel Output Voltage Varies"]
+[-3.098559856414795, 9.65742015838623, "Battery Capacity 50 Ah"]
+[-2.1839120388031006, 8.9734468460083, "Power Control Unit Data Bus Interface SpaceWire type"]
+[-2.16867995262146, 8.985695838928223, "Power Control Unit Functionality High"]
+[-2.2092344760894775, 9.025019645690918, "Power Control Unit Size Compact"]
+[-2.1597118377685547, 8.952064514160156, "Power Control Unit Mass Low"]
+[3.4734606742858887, 13.42394733428955, "Laser Communication System Components Laser transmitter, optical unit, pointing control mechanism, laser receiver"]
+[3.467555284500122, 13.457509994506836, "Laser Communication System Modulation Technique IM/DD (Intensity Modulation / Direct Detection)"]
+[3.4660532474517822, 13.47337818145752, "Laser Communication System Scan Range \u00b13\u00ba"]
+[3.4681408405303955, 13.432352066040039, "Laser Communication System Feedback Signal Content Angel error and the received intensity"]
+[3.4575071334838867, 13.41098690032959, "Laser Communication System Data Downlink Start Condition When the received intensity is over a threshold value"]
+[3.038862705230713, 22.809494018554688, "Instrument Unknown Unknown"]
+[-4.869332790374756, 9.675973892211914, "Receiver Component Number of Elements 4"]
+[-4.844264507293701, 9.73793888092041, "Receiver Component Inter-element Spacing 90 mm"]
+[-3.4196999073028564, 8.33647346496582, "Signal Converter Function Converts received signals to intermediate frequency, performs signal amplification and filtering"]
+[-3.3678479194641113, 8.044917106628418, "Signal Processing Unit Function Samples the analog IF signals and performs the IF signal processing"]
+[0.201820507645607, 7.147840976715088, "Experiment Objective Measurement of atomic oxygen (AO) by silver loss determination in different material specimens"]
+[0.13501565158367157, 7.227408409118652, "Experiment Components Twelve silver resistance sensors"]
+[0.05397677794098854, 7.286679744720459, "Experiment Coating Materials Polyethylene, PTFE, carbon, and silica"]
+[0.16069889068603516, 7.177299499511719, "Experiment Objective Demonstration of control techniques using conventional constant current battery charging, followed by current tapering"]
+[-3.026284694671631, 4.208652019500732, "Spacecraft Lunar Orbit Insertion Location Sinus Iridum (Bay of Rainbows, 43\u00b0N 31\u00b0W)"]
+[-3.048558473587036, 4.310919761657715, "Spacecraft Data Transmission Speed 12 Mbit/s"]
+[-2.9771156311035156, 4.185949325561523, "Spacecraft Landing Camera Type Brand-new"]
+[-3.034109592437744, 4.253590106964111, "Spacecraft Camera Type Micro CMOS-camera"]
+[-0.4905093312263489, 5.852385520935059, "Unknown Unknown Unknown"]
+[3.7361702919006348, 17.704578399658203, "Payload Parameter Value"]
+[3.7008986473083496, 17.668399810791016, "Payload Parameter Value"]
+[3.7390506267547607, 17.699445724487305, "Payload Parameter Value"]
+[3.7614948749542236, 17.695049285888672, "Payload Quantity 3"]
+[3.7273411750793457, 17.706037521362305, "Payload Accuracy 0.2\u00ba"]
+[4.957491397857666, -2.404162645339966, "Satellite Lifetime 3 years"]
+[4.761757850646973, -2.432253837585449, "Satellite Extended Mission 5-7 years"]
+[4.684451580047607, -2.619621992111206, "Satellite Possibly > 10 years Possibly > 10 years"]
+[2.0233278274536133, -2.110595226287842, "Satellite Orbit SSO"]
+[0.7423428297042847, -1.1695963144302368, "Satellite Altitude 677 km x 586 km"]
+[0.7112773060798645, -2.3082375526428223, "Satellite Inclination 98.09\u00ba"]
+[3.8723716735839844, -3.1961467266082764, "Satellite LTAN 11 hours"]
+[4.026721954345703, -2.873838186264038, "Satellite Period 97.34 minutes"]
+[1.1266030073165894, -0.7754623889923096, "Satellite Size 44 cm between sides and 47 cm body height"]
+[0.9458179473876953, -4.41008996963501, "Satellite Mass 23.9 kg"]
+[6.230817794799805, 7.507453918457031, "Satellite Component Quantity 13"]
+[6.292674541473389, 7.447757720947266, "Satellite Component Power 23 W"]
+[-3.0961427688598633, 9.667601585388184, "Battery Capacity 2x 5.8 Ah"]
+[-3.0264334678649902, 9.602058410644531, "Battery Voltage 24 V"]
+[-1.0798646211624146, 7.717024803161621, "Device Model Motorola 68332 microprocessor"]
+[-1.0363833904266357, 7.748486042022705, "Device Memory 512 kB EEPROM & 2 MB RAM"]
+[6.327390193939209, 7.4093170166015625, "Satellite Component Control Zero momentum 3-axis stabilized control with nadir pointing (5\u00ba)"]
+[6.349085330963135, 7.394075393676758, "Satellite Component Communication RF communications TM: 4.5 W RF, 40 kbit/s TM at 387.1 MHz; TC at 400 MHz. S-band TM-TC at 2.043 & 2.223 GHz 40-175 kbit/s"]
+[7.291685104370117, 12.430423736572266, "Satellite Instrument Purpose Locate and measure methane from human sources worldwide"]
+[7.292357444763184, 12.422707557678223, "Satellite Instrument Resolution High"]
+[7.281357765197754, 12.41978931427002, "Satellite Instrument Warming Power of Methane More than 80 times the warming power of carbon dioxide during its first 20 years"]
+[1.4429740905761719, 2.7644596099853516, "Weather Satellite Launch Date July 25, 2013"]
+[1.4507285356521606, 2.755699634552002, "Weather Satellite Launch Vehicle Ariane-5 ECA"]
+[1.4540297985076904, 2.7455666065216064, "Weather Satellite Launch Mass ~ 6650 kg"]
+[1.445734977722168, 2.7559409141540527, "Weather Satellite Flight Duration 32 minutes and 48 seconds"]
+[1.465859293937683, 2.7149734497070312, "Weather Satellite Orbit Elliptical GTO (Geosynchronous Transfer Orbit)"]
+[1.4431662559509277, 2.7686927318573, "Weather Satellite Control Facility ISRO's MCF (Master Control Facility) at Hassan in Karnataka"]
+[-3.8224399089813232, 7.965917587280273, "Data Storage Device Status Limited onboard resources"]
+[-0.0763801708817482, 9.778585433959961, "Inertial Reference Unit Components 4 gyros, 2 processing units, 2 power supplies"]
+[-0.0466264970600605, 9.753429412841797, "Inertial Reference Unit Redundancy 3 among 4 cold redundancies for the inertial attitude estimation purpose"]
+[-0.09364452213048935, 9.765482902526855, "Inertial Reference Unit Power Supply Redundancy Full redundancy"]
+[-0.052067361772060394, 9.734613418579102, "Inertial Reference Unit Gyro Configuration Four gyros in a tetrahedron configuration"]
+[-2.817427158355713, 15.248270034790039, "Microwave Radiometer Power On Time 81 days"]
+[-2.817784547805786, 15.255595207214355, "Microwave Radiometer First Tb Image Production Time ~ 6 hours after the data reception on August 31, 2011"]
+[-2.8134584426879883, 15.2528715133667, "Microwave Radiometer Algorithm Version v2.0"]
+[-2.821246862411499, 15.250085830688477, "Microwave Radiometer Number of MWR Orbits Gathered 65"]
+[-2.7539405822753906, 15.310783386230469, "Microwave Radiometer Ta Bias Model Linear function of MWR Ta"]
+[-0.44320762157440186, 8.673794746398926, "Actuators Type Three-axis stabilized (nadir pointing)"]
+[0.7895456552505493, 11.911728858947754, "Sensors Attitude Determination Via"]
+[-6.667842388153076, 9.945355415344238, "Antennas Quantity Steerable high-gain antenna dish and two omni antennas"]
+[-2.9413630962371826, 4.4863152503967285, "Spacecraft Mass 2388 kg (launch mass) and 2169 kg of dry mass"]
+[-2.611227035522461, 9.6300687789917, "Power Source Capacity 3.4 kW (BOL)"]
+[-3.694133996963501, 8.321212768554688, "Energy Storage Capacity 50 Ah"]
+[-1.6082782745361328, 9.679853439331055, "Propulsion System Type Hydrazine"]
+[-1.7638263702392578, 5.76948356628418, "Operations Location POCC (Project Operations Control Center) at JPL, Pasadena, CA"]
+[-3.121469020843506, 2.1560921669006348, "Mission Duration Nominal 3 years plus 2 years for an extended mission"]
+[8.955316543579102, 8.511617660522461, "Satellite Payload Purpose Support search and rescue operations"]
+[8.955312728881836, 8.511523246765137, "Satellite Payload Purpose Support search and rescue operations"]
+[8.955232620239258, 8.51176643371582, "Satellite Payload Development Russia (former Soviet Union) in the mid-1970s"]
+[8.957223892211914, 8.514053344726562, "Satellite Payload Development France, Canada, and the USA"]
+[2.64729380607605, 14.348785400390625, "Optical Instrument Micro-Roughness 0.5 nm RMS"]
+[2.6636505126953125, 14.361804962158203, "Optical Instrument Micro-Roughness 1 nm RMS"]
+[2.636338949203491, 14.33114242553711, "Optical Instrument Observation Range From 1.04 Rsun"]
+[-5.878604412078857, 16.014490127563477, "Synthetic Aperture Radar Observation Date Feb. 21, 2015"]
+[-5.895761489868164, 16.039846420288086, "Synthetic Aperture Radar Observation Date May 2, 2015"]
+[-5.899526596069336, 16.008649826049805, "Synthetic Aperture Radar LOS Distance Change At least 1.5 metres"]
+[-5.892899036407471, 16.007526397705078, "Synthetic Aperture Radar Local Displacement Up to 30 cm in the satellite-ground direction"]
+[16.914833068847656, 6.814455509185791, "Microsatellites Constellation Size 30 satellites"]
+[16.95028305053711, 6.770063877105713, "Microsatellites Revisit Time Every 30 minutes"]
+[16.856128692626953, 6.865506172180176, "Microsatellites Imagery Delivery Real-time"]
+[1.6805427074432373, -1.106338381767273, "Satellite Imagery Resolution High-resolution"]
+[1.679517149925232, -2.3082261085510254, "Satellite Orbit Control Maneuvers 10 regular station keeping OCM performed for ground track corrections and 2 OCMs were performed as emergency collision avoidance maneuvers"]
+[0.5809329152107239, -1.4879196882247925, "Satellite Orbit Altitude 629 km"]
+[0.6810702085494995, -2.294121742248535, "Satellite Orbit Inclination 97.9\u00b0"]
+[4.105650901794434, -2.8488657474517822, "Satellite Orbit Period 97.3 minutes"]
+[4.150610446929932, -2.4697554111480713, "Satellite Repeat Cycle 31 days"]
+[1.0368452072143555, -4.378915309906006, "Satellite Mass 1,730 kg"]
+[-3.268702268600464, 5.428289413452148, "Launch Vehicle Launch Site Taiyuan Satellite Launch Complex in Shanxi, China"]
+[-1.2869056463241577, 6.116399765014648, "Partnership Countries Brazil and China"]
+[-1.3342591524124146, 6.144140720367432, "Partnership Organizations INPE (National Institute for Space Research) and CAST (China Academy of Space Technology)"]
+[1.9023709297180176, 10.723211288452148, "Imaging Device Required Spacecraft Stability High"]
+[1.9002008438110352, 10.718484878540039, "Imaging Device Cost (sensor + spacecraft) High"]
+[1.8896883726119995, 10.722688674926758, "Imaging Device Area Collection Rate Very high"]
+[1.9163432121276855, 10.727161407470703, "Imaging Device Required Spacecraft Stability Low"]
+[1.901327133178711, 10.714384078979492, "Imaging Device Cost (sensor + spacecraft) Very low"]
+[1.8893543481826782, 10.71261978149414, "Imaging Device Area Collection Rate Very low"]
+[0.5273621082305908, 9.420540809631348, "Attitude Determination and Control System Stabilization 3-axis"]
+[0.4986865222454071, 9.426161766052246, "Attitude Determination and Control System Pointing Capability \u00b130\u00ba"]
+[0.5488676428794861, 9.4291410446167, "Attitude Determination and Control System Pointing Accuracy 0.02\u00ba (3\u03c3)"]
+[-8.139586448669434, 8.825729370117188, "Electric Power Subsystem Power 65 W (max)"]
+[-8.142337799072266, 8.823806762695312, "Electric Power Subsystem Power Storage Li-ion battery of 9 Ah capacity"]
+[-2.714000701904297, 7.883642673492432, "Processor Speed 200 MHz"]
+[-2.7787609100341797, 7.894302845001221, "Processor Bit 32-bit"]
+[-3.320751667022705, 8.542805671691895, "Memory Program Memory 4 MByte TMR protected SRAM"]
+[-3.356369972229004, 8.527266502380371, "Memory FLASH for boatload 2 MByte"]
+[-3.3652384281158447, 8.547261238098145, "Memory SDRAM with ECC functionality 2 Gbyte"]
+[-4.749607563018799, 9.250877380371094, "Transmitter Output Power 7 W (min)"]
+[-4.755109786987305, 9.263859748840332, "Transmitter Output Frequency 8.23 GHz"]
+[-4.749317646026611, 9.238821029663086, "Transmitter Data Rate 25, 50 or 100 Mbit/s (selectable)"]
+[-4.755084037780762, 9.254584312438965, "Transmitter Modulation QPSK/OQPSK (selectable)"]
+[-4.782833099365234, 9.29908561706543, "Transmitter Mass 3 kg"]
+[-4.756560802459717, 9.267024993896484, "Transmitter Size 9 cm x 31 cm x 8 cm"]
+[1.0327706336975098, -4.398720741271973, "Satellite Mass 95 kg"]
+[5.133207321166992, -2.2827353477478027, "Satellite Design Life 3 years"]
+[1.1729300022125244, -0.775862455368042, "Satellite Size 700 mm x 700 mm x 554 mm"]
+[1.7852554321289062, 8.451214790344238, "Data Handling Subsystem Operation Modes Real-time, real-time stretch mode, record, and playback"]
+[1.7682042121887207, 8.441288948059082, "Data Handling Subsystem Data Rate Threshold 640 Mbit/s"]
+[1.761855125427246, 8.434774398803711, "Data Handling Subsystem Memory Type Memories for burst data formatting"]
+[1.782465934753418, 8.461228370666504, "Data Handling Subsystem Components FPGAs (Field-Programmable Gate Arrays)"]
+[11.398117065429688, 5.579078674316406, "CubeSat Release Speed 5cm/s"]
+[11.487713813781738, 5.703990459442139, "CubeSat Size Representative of the size of a large space debris"]
+[-1.0532838106155396, 7.710177898406982, "Device Unavailability Period Up to 20 minutes"]
+[-0.9394204616546631, 7.759284496307373, "Device Estimated Drift Standard deviation"]
+[-1.0666625499725342, 7.758983135223389, "Device Unavailability Period Up to 20 minutes"]
+[-1.0413157939910889, 7.723656177520752, "Device Tracking Loss Transition to survival mode"]
+[0.2383391559123993, 11.56009292602539, "Sensor System Purpose Advanced Earth Imaging"]
+[-1.9046272039413452, 6.8951849937438965, "Software Function Navigation, guidance, and control"]
+[-1.8886240720748901, 6.921545028686523, "Software Manufacturer Unknown"]
+[-1.9273828268051147, 6.902937889099121, "Software Manufacturer NGC (NGC Aerospace Ltd.)"]
+[-4.569777488708496, -3.0860002040863037, "Exoplanet Age About a few million years"]
+[-4.580259799957275, -3.1078672409057617, "Exoplanet Orbit Period About seven days"]
+[-4.590515613555908, -3.1174094676971436, "Exoplanet Diameter About 10 times the diameter of Earth"]
+[-4.56101131439209, -3.084132194519043, "Exoplanet Distance from Earth About 490 light-years"]
+[3.395280599594116, 13.660903930664062, "Photon-counting Device Approach Micro-pulse multi-beam"]
+[-5.518558979034424, 7.123319149017334, "Communications Link Data Transfer Ground stations"]
+[-5.515512466430664, 7.117406368255615, "Communications Link Data Transfer NASA Ground Network"]
+[-3.0965278148651123, 4.285621166229248, "Spacecraft Manufacturer Orbital ATK"]
+[3.0379693508148193, -1.8229583501815796, "Satellite Mission Objectives Unknown"]
+[2.5786335468292236, -3.9103498458862305, "Satellite URL http://www.nasa.gov/feature/goddard/lasers-path-through-icesat-2"]
+[-1.4390078783035278, 1.219099521636963, "Data Relay Satellite Mission Type Non-EO"]
+[-1.387798547744751, 1.1562663316726685, "Data Relay Satellite Launch Date Jan 28, 2013"]
+[-1.4469894170761108, 1.221289873123169, "Data Relay Satellite Program ARTES-7 (Advanced Research in Telecommunications Systems)"]
+[-1.430185079574585, 1.2016034126281738, "Data Relay Satellite Constellation Two geostationary data relay satellites"]
+[-1.4398857355117798, 1.1967499256134033, "Data Relay Satellite Ground Segment EDRS Services"]
+[1.761663556098938, 22.205787658691406, "Instrument Telescope Diameter 12.7 cm"]
+[1.689247488975525, 21.9631290435791, "Instrument Swath Width 2280 km"]
+[2.1629698276519775, 22.231651306152344, "Instrument Scan Angle \u00b151.2\u00ba"]
+[2.6808414459228516, 22.094751358032227, "Instrument Objective Provide images of visual reflection and thermal infrared emission from oceanic, coastal, and atmospheric features"]
+[-5.012451648712158, 2.880857467651367, "Space Telescope Data Type X-ray emission"]
+[-13.507979393005371, -2.0286812782287598, "X-ray Observatory Data Type X-ray emission"]
+[2.6751768589019775, 14.095191955566406, "Optical Data Source Data Type Optical data"]
+[-4.980525493621826, 2.887193202972412, "Space Telescope Mission European Space Agency's"]
+[-5.2367448806762695, 7.815513610839844, "Communication System Data Transmission Scheme SSMA (Spread Spectrum Multiple Access)"]
+[-5.287038326263428, 8.027616500854492, "Communication System Uplink Frequency 388 MHz"]
+[-5.282548904418945, 7.976981163024902, "Communication System Downlink Frequency 400.6 MHz"]
+[-5.23602294921875, 7.795986175537109, "Communication System Chip-Based Timing Resolution 0.2 \u00b5s"]
+[-5.204787254333496, 7.895949363708496, "Communication System Coarse Localization Accuracy <3 km"]
+[-5.180752277374268, 7.851181507110596, "Communication System Fine Localization Accuracy <1 km"]
+[-5.487401008605957, 7.9627485275268555, "Communication Mode Purpose Communication between the user terminal and the payload (or vice versa)"]
+[-5.470386028289795, 7.900691509246826, "Communication Mode Purpose High-rate communication link between the payload and the HUB station"]
+[6.344921588897705, 7.389469623565674, "Satellite Component Purpose Combines and encodes data streams, performs data rate adaptation"]
+[-2.322439432144165, 8.240309715270996, "Interface Adaption Unit Input Data Stream 8-bit wide"]
+[-2.3398756980895996, 8.218738555908203, "Interface Adaption Unit Output Data Stream 16-bit wide"]
+[-2.2866790294647217, 8.229958534240723, "Interface Adaption Unit Data Rate 600 Mbit/s"]
+[-1.2423170804977417, 3.145915985107422, "Cosmic Object X-ray Light Source Bright"]
+[-1.2441914081573486, 3.1496753692626953, "Cosmic Object Precession Wobbles on its axis"]
+[-1.2758461236953735, 3.1830968856811523, "Cosmic Object Cone Tilt Periodically tilts slightly toward Earth"]
+[-1.238109827041626, 3.1576125621795654, "Cosmic Object X-ray Light Enough to officially call SS 433 a ULX"]
+[-1.1763696670532227, 3.137364625930786, "Cosmic Object Mass Millions to billions of times the mass of the Sun"]
+[-13.880173683166504, -2.2249929904937744, "X-ray Telescope Wavelengths Almost the whole range of X-ray wavelengths"]
+[-1.419075846672058, 4.341184139251709, "Ground System Functions Data processing, archiving, cataloging and user service functions"]
+[-1.410998821258545, 4.344017505645752, "Ground System Communication Data relay communication and very fast X-band direct downlink"]
+[-3.538874626159668, 6.986453533172607, "Observation Data Data Rate 278 Mbit/s for Ka-band and at 800/400/200 Mbit/s via X-band"]
+[-13.922128677368164, -2.1937503814697266, "X-ray Telescope Sensitivity High-energy X-rays"]
+[-13.86759090423584, -2.177609920501709, "X-ray Telescope Pulse Rate 1.37 seconds"]
+[-13.920520782470703, -2.1847894191741943, "X-ray Telescope Energy Output 10 million suns"]
+[-0.8260573148727417, 3.718806743621826, "ULX Mass About the mass of our sun"]
+[-0.8150401711463928, 7.6184163093566895, "ULX Size The size of Pasadena"]
+[1.0483298301696777, 9.143519401550293, "Attitude and Orbit Control Subsystem Functionality Variable"]
+[0.9923959374427795, 9.164687156677246, "Attitude and Orbit Control Electronics Manufacturing Difficult to produce by repetitive manufacturing"]
+[1.0957149267196655, 9.121192932128906, "Attitude and Orbit Control Subsystem Technology SpaceWire"]
+[1.0594511032104492, 9.138961791992188, "Attitude and Orbit Control Subsystem Platform Standard platform AOCS"]
+[1.0695440769195557, 9.133631706237793, "Attitude and Orbit Control Subsystem Features Standardization of hardware and software at the module level"]
+[2.703200340270996, 22.348098754882812, "Instrument Suite Components Four electrostatic analyzers (two for ions and two for neutrals) and two mass spectrometers (one for ions and one for neutrals)"]
+[2.3982725143432617, 22.356887817382812, "Instrument Suite Measurement In-situ density, temperature and composition of the thermosphere"]
+[2.5731945037841797, 22.28925323486328, "Instrument Suite Measurement Neutral winds and ion flows"]
+[7.266660690307617, 12.39470100402832, "Satellite Instrument Detects Size and energy of lightning flashes"]
+[0.029048658907413483, 4.501197338104248, "Hurricane Rapid Intensification Definition An increase in 30 kts (35 mph) in sustained winds over 24 hours"]
+[0.07953927665948868, 4.551477909088135, "Hurricane Flash Rate During Weakening More than three times that during rapid intensification"]
+[1.7343374490737915, -2.0418190956115723, "Satellite Shape Spin-stabilized octagon"]
+[1.134100079536438, -0.7152484059333801, "Satellite Dimensions 76 cm in diameter and 74 cm high"]
+[1.0174144506454468, -4.40932035446167, "Satellite Mass About 80 kg"]
+[2.3092355728149414, -1.5377572774887085, "Satellite Cameras Two vidicon cameras"]
+[1.4800773859024048, -1.1014797687530518, "Satellite Camera Resolution 1.5 km at image center to about 5.5 km at the edge of a picture"]
+[2.4271180629730225, -1.0907111167907715, "Satellite Sensor Low-resolution VIS (0.4 - 4 \u00b5m) and infrared (8.0 - 12 \u00b5m) sensor"]
+[-2.2997496128082275, 7.414754867553711, "Motherboard Purpose House the OEM615 adjacent to a dedicated A3200 ADCS computer"]
+[-0.6550849676132202, 8.5363130569458, "Reaction Wheel Configuration Tetrahedron"]
+[0.5295788645744324, 12.108527183532715, "Sensor Measurement 2-axis sun vector"]
+[-6.696230888366699, 9.950921058654785, "UHF Antenna Configuration Canted turnstile"]
+[-6.731050491333008, 9.984838485717773, "UHF Antenna Antenna Elements 4"]
+[-6.715583324432373, 9.973743438720703, "UHF Antenna Gain Pattern Omnidirectional"]
+[-5.364943981170654, 8.092657089233398, "Communication System Frequency 145.825 MHz"]
+[-5.207795143127441, 7.772663116455078, "Communication System Data Rate 9.6 kbit/s"]
+[-5.272665500640869, 7.88326358795166, "Communication System Modulation FSK"]
+[-5.251735210418701, 7.897058010101318, "Communication System Encoding NRZ"]
+[-2.625720500946045, 9.345696449279785, "Power Supply Type Integrated Microelectronic Power Supply"]
+[-2.6434061527252197, 9.358879089355469, "Power Supply Function Power generation and power storage for microelectronic applications"]
+[-2.590634346008301, 9.34586238861084, "Power Supply Components Thin-film photovoltaic array, thin-film lithium-ion battery"]
+[-0.9550327658653259, 6.444192409515381, "Documentation Author Herbert J. Kramer"]
+[-0.9529872536659241, 6.475485324859619, "Documentation Publisher Springer Verlag"]
+[-0.92824786901474, 6.465822696685791, "Documentation Edition 4th edition"]
+[-0.8499707579612732, 6.130918502807617, "Website Contact Email eoportal@symbios.space"]
+[-1.0129544734954834, 6.273280620574951, "Copyright Year 2024"]
+[2.0296900272369385, -1.7628129720687866, "Satellite Polarimetric Sensor Hybrid"]
+[1.6888989210128784, -2.069261312484741, "Satellite Polarization Circular"]
+[0.7189247012138367, -2.2560081481933594, "Satellite Incidence Angle Range 12\u00b0 to 55\u00b0"]
+[1.1770919561386108, -1.9953808784484863, "Satellite Linear Polarimetric Mode Restricted coverage of 20\u00b0 to 30\u00b0 incidence angle"]
+[1.0190874338150024, -4.19468879699707, "EO Satellites Mass 100 kg"]
+[16.61257553100586, 6.989306926727295, "Minisatellite Payload Capacity 50-100 kg"]
+[16.60975456237793, 6.989224433898926, "Minisatellite Compatible with ESPA-class secondary launch adaptors"]
+[11.24912166595459, 5.480465412139893, "CubeSat Payload Proprietary spectrometer and components"]
+[11.298014640808105, 5.484522342681885, "CubeSat Payload Two-way VHF Data Exchange System (VDES)"]
+[-1.9235496520996094, 6.901627063751221, "Software Unknown Unknown"]
+[2.979631185531616, -2.083595037460327, "Satellite Unknown Unknown"]
+[-5.309454441070557, 3.0832560062408447, "Telescope Array Mission Date March 23, 2017"]
+[-0.7475758194923401, 7.63289213180542, "Object Type Possible pulsar"]
+[-0.7573005557060242, 7.650082588195801, "Object Spectrum Very similar to known pulsars in the Milky Way"]
+[-0.8099827766418457, 7.690413475036621, "Object Color in Image Blue"]
+[-0.8039414882659912, 7.839540958404541, "Object Brightness Brighter in high-energy X-rays than anything else in the galaxy"]
+[5.307497978210449, -4.480907917022705, "Satellite Launch Date May 29, 2012"]
+[2.8633673191070557, -1.4325594902038574, "Satellite Mission Type Earth observation and disaster monitoring"]
+[3.6407899856567383, 22.236309051513672, "Instrument Component Developer M. Gubarev, B. Ramsey, S. L. O\u2019Dell, R. Elsner, K. Kilaru, J. McCracken, M. Pavlinsky, A. Tkachenko, I. Lapshov"]
+[3.054401159286499, 22.60251808166504, "Instrument Mission Spectrum-Roentgen-Gamma"]
+[-3.113828182220459, 4.706211090087891, "Cargo Craft Departure Time 11:10 a.m. EST"]
+[-3.1239213943481445, 4.791593551635742, "Cargo Craft Cargo Removal More than 2,500 kg"]
+[-3.089301824569702, 4.734923839569092, "Cargo Craft CubeSat Deployment Three CubeSats via the NanoRacks External Cygnus Deployer at two different altitudes and two CubeSats from the Slingshot CubeSat Deployer System"]
+[-3.144577741622925, 4.747912883758545, "Cargo Craft Reentry Time Feb. 25 at 4:05 a.m. EST"]
+[2.3177316188812256, 22.714553833007812, "Instrument Radio Wave Length L-band"]
+[2.2030410766601562, 22.99997329711914, "Instrument Bandwidth 1.2 GHz"]
+[0.2691408097743988, 4.588499069213867, "Volcanic Feature Length 210 m"]
+[0.19518768787384033, 4.634146213531494, "Volcanic Feature Width 70 m"]
+[2.5715432167053223, 12.222729682922363, "Radar Beam Mode Width 450 km"]
+[2.5713531970977783, 12.232429504394531, "Radar Beam Mode Sub-beams 7 (in the HH polarization channel only)"]
+[2.596107244491577, 12.220403671264648, "Radar Beam Mode Incidence Angles 34\u00ba to 57\u00ba"]
+[2.5784287452697754, 12.235763549804688, "Radar Beam Mode Width 530 km"]
+[2.5818381309509277, 12.26012897491455, "Radar Beam Mode Sub-beams 8 (in the HH and HV polarization channels)"]
+[2.603152275085449, 12.21795654296875, "Radar Beam Mode Incidence Angles 20\u00ba to 50\u00ba"]
+[-14.114206314086914, -2.3989264965057373, "X-ray Telescope Number of Clusters of Galaxies Approximately 100,000"]
+[-13.903860092163086, -2.24001407623291, "X-ray Telescope Number of Accreting Supermassive Black Holes Around 3 million"]
+[-13.88932991027832, -2.245396375656128, "X-ray Telescope Number of Active Stars Half a million"]
+[2.417419910430908, -2.0752906799316406, "Satellite Autonomous Precision Orbit Control Unknown"]
+[2.45748233795166, -2.0618703365325928, "Satellite Orbit Control and Determination Unknown"]
+[-1.515561580657959, 14.865335464477539, "Visible and Infrared Radiometer Goal Provide low-resolution visible and infrared images of oceans, coasts, and clouds"]
+[-1.4694254398345947, 14.86474609375, "Visible and Infrared Radiometer Failure Early failure of the instrument limited its usefulness"]
+[-1.5025320053100586, 14.879378318786621, "Visible and Infrared Radiometer Image Duration 62 days"]
+[-1.506649374961853, 14.856071472167969, "Visible and Infrared Radiometer Sea-Surface Temperature Accuracy \u00b1 1.5\u00baC"]
+[-1.506891131401062, 14.87274169921875, "Visible and Infrared Radiometer Sea-Surface Temperature Accuracy \u00b1 1.7 \u00baC"]
+[2.5123298168182373, -1.1812397241592407, "Satellite Data Usage Groundwater data for the initial conditions"]
+[1.3980779647827148, 2.749094247817993, "Weather Forecast Model Input Data GRACE-FO data"]
+[-3.453826665878296, 6.840775966644287, "Data Product Availability Freely available"]
+[-5.369730472564697, 2.7391839027404785, "Telescope Aperture Diameter 80 cm"]
+[-5.260461807250977, 2.641683340072632, "Telescope Focal Length 8.6 m"]
+[-5.401435375213623, 2.7574846744537354, "Telescope F Number f/12"]
+[-0.9117151498794556, 11.43427848815918, "CCD Detector Line Array 24,000 pixels"]
+[-0.958063006401062, 11.345733642578125, "CCD Detector Pixel Pitch 8.75 \u00b5m"]
+[-0.9429661631584167, 11.403923988342285, "CCD Detector Source Data Rate 16 x 15 Mpixel/s (or 3.84 Gbit/s)"]
+[-0.906803548336029, 11.441417694091797, "CCD Detector Line Array 6,000 pixels"]
+[-0.9555680155754089, 11.369300842285156, "CCD Detector Pixel Pitch 2 x 17.5 \u00b5m"]
+[-0.9429720640182495, 11.374974250793457, "CCD Detector Source Data Rate 4 x 240 Mbit/s"]
+[6.313206195831299, 7.432411193847656, "Satellite Component Data Compression CCSDS 120.1-G-1E"]
+[6.326961040496826, 7.420856475830078, "Satellite Component Data Memory 512 Gbit"]
+[6.28156042098999, 7.45766019821167, "Satellite Component Data Rate 1 GB/s"]
+[-2.672987937927246, 11.54422664642334, "Image Capture Date 30 January 2022"]
+[-0.406658798456192, 5.1067938804626465, "Lake and Reservoir Location Southern Egypt and northern Sudan"]
+[1.1652311086654663, -0.8081088066101074, "Satellite Size 6U"]
+[1.3108437061309814, 7.078462600708008, "Communication Equipment Size 21 m"]
+[2.906881332397461, 21.915945053100586, "Instrument Purpose Prospect for water in ice, liquid, and vapor forms"]
+[1.3837796449661255, -2.4012482166290283, "Satellite Orbit Highly inclined elliptical lunar orbit"]
+[1.5252773761749268, -2.3261640071868896, "Satellite Trajectory Low-thrust trajectory to lunar orbit with very little propellant"]
+[1.5369760990142822, -1.8267462253570557, "Satellite Position Improvement 20%"]
+[1.6020158529281616, -1.9382214546203613, "Satellite Polar Motion Improvement (x-component) 24%"]
+[1.2412296533584595, -2.0636367797851562, "Satellite Polar Motion Improvement (y-component) 18.7%"]
+[1.6231021881103516, -1.856475591659546, "Satellite LOD Improvement 19.8%"]
+[0.6295194625854492, 12.104445457458496, "Sensor Package Channels 24"]
+[0.5627316236495972, 12.21279525756836, "Sensor Package Center Frequencies 19.35 GHz to 183.31 GHz"]
+[0.538825273513794, 12.18951416015625, "Sensor Package Orbital Altitude ~833 km"]
+[0.6417462229728699, 12.064187049865723, "Sensor Package Inclination 98.8\u00ba"]
+[0.6443921327590942, 12.115839004516602, "Sensor Package Ascending Nodal Crossing Time 20:03 hours local time"]
+[6.332447052001953, 7.410983085632324, "Satellite Component Material W/Si, Pt/SiC, Pt/C"]
+[6.233565330505371, 7.507663249969482, "Satellite Component Coating Depth-graded multilayers"]
+[6.191861152648926, 7.548354625701904, "Satellite Component Number of Groups 10"]
+[2.839146137237549, -1.7934471368789673, "Satellite Daily Revisit Capability Yes"]
+[1.1109027862548828, -1.8612092733383179, "Satellite Agility \u00b145\u00ba"]
+[1.660849690437317, -1.245012879371643, "Satellite Resolution High"]
+[4.22132682800293, -2.813950777053833, "Satellite Response Time Quick"]
+[2.1184215545654297, 22.71265983581543, "Instrument Spectral Bands PH1: 160 to 260 nm, PH2: 337 \u00b1 5 nm, PH3: 762 \u00b1 5 nm, PH4: 600 to 900 nm"]
+[-2.974963903427124, 20.16490364074707, "Spectral Band Wavelength Range 160 to 260 nm"]
+[-2.9779257774353027, 20.17196273803711, "Spectral Band Wavelength 337 \u00b1 5 nm"]
+[-2.9367117881774902, 20.20337677001953, "Spectral Band Wavelength 762 \u00b1 5 nm"]
+[-2.971203327178955, 20.1691837310791, "Spectral Band Wavelength Range 600 to 900 nm"]
+[-5.39733362197876, 2.812220335006714, "Telescope Aperture 2.5 cm"]
+[-5.341862678527832, 2.7495810985565186, "Telescope Effective Focal Length 187 cm"]
+[0.79881352186203, 12.098624229431152, "Sensor Unit Number of Photo Diodes Four pairs"]
+[0.5949491262435913, 12.087059020996094, "Sensor Unit Diodes Intensity Difference Range \u00b1120 arcseconds"]
+[-0.05179986730217934, 9.334211349487305, "Pointing System Pointing Adjustment Time About 30 s"]
+[-0.028532911092042923, 9.306634902954102, "Pointing System Maximum Pointing Adjustment Time < 2 minutes"]
+[11.278078079223633, 5.502811908721924, "CubeSat Bands 89 GHz (window), 118 (temp), 183 GHz (humidity), 207 GHz (cloud ice)"]
+[11.296969413757324, 5.569736957550049, "CubeSat Attitude Control Dual-spinner local-vertical local-horizontal"]
+[11.256220817565918, 5.482301235198975, "CubeSat Risk Reduction NASA TROPICS , NOAA EON-MW CubeSat missions"]
+[-5.788391590118408, 15.91187858581543, "Synthetic Aperture Radar Image Resolution Not specified"]
+[-5.884298801422119, 15.993488311767578, "Synthetic Aperture Radar Area of Observation Nantucket Shoals"]
+[2.656350612640381, 14.325614929199219, "Optical Instrument Quantity 1"]
+[2.628767251968384, 13.484545707702637, "Optical Component Quantity 3"]
+[2.637739419937134, 13.435772895812988, "Optical Component Function Defines the channels in each band"]
+[2.858588218688965, -1.146937370300293, "Satellite Mission Objectives Observe environmental changes to Earth\u2019s atmosphere, with particular areas of focus being deforestation, reduction of the ozone layer and a wider study of global warming"]
+[5.016623497009277, -4.12258768081665, "Satellite Mission Failure June 1997"]
+[3.02758526802063, -1.5527831315994263, "Satellite Managing Agency NASDA, the National Space Development Agency of Japan"]
+[-1.7118903398513794, 5.339189052581787, "Mission Control Center Functions Collect, store and sort the data from LUTs and other MCCs; provide data exchange within the Cospas-Sarsat System; and distribute alert and location data to associated RCC (Rescue Co-ordination Centers) or to SPOCs (SAR Points Of Contacts)"]
+[-1.724549412727356, 5.355478763580322, "Mission Control Center Tasks Receive data from national LUTs and foreign MCCs, Attempt to match signals coming from the same beacon source, Merge beacon signals from the same source to improve location accuracy, Geographically sort data to determine appropriate recipient of alert message, Transmit alert messages to search and rescue authorities"]
+[-1.711553692817688, 5.362739086151123, "Mission Control Center Location Moscow, Russia"]
+[-1.6989232301712036, 5.345043182373047, "Mission Control Center Location NOAA in Suitland, MD"]
+[-1.6894282102584839, 5.335958003997803, "Mission Control Center Location CNES in Toulouse, France"]
+[-1.701346516609192, 5.346602439880371, "Mission Control Center Location Trenton, Ontario"]
+[0.9191451072692871, 10.454448699951172, "Digital Mapping System Image Acquisition Date November 3, 2017"]
+[0.2974793612957001, 4.479796886444092, "Natural Feature Length About 13 miles"]
+[0.33757326006889343, 4.589885711669922, "Natural Feature Width 7 miles"]
+[4.353159427642822, -2.7665960788726807, "Satellite Imaging Duration Nearly a month"]
+[2.146155834197998, -1.5979530811309814, "Satellite Imaging Mode Continuous"]
+[1.8001865148544312, -1.6374551057815552, "Satellite Observation Uniformity Very uniform"]
+[2.228952407836914, -2.3599438667297363, "Satellite Atmospheric Interference None"]
+[-3.068319797515869, 2.051194190979004, "Space Mission Design Low-Cost, R&D Space Mission with Responsive Enabling Technologies"]
+[1.0013697147369385, -4.339475154876709, "Satellite Mass 350 kg"]
+[0.7094669938087463, -1.3763477802276611, "Satellite Field of View 260 km"]
+[1.4477176666259766, -1.1435190439224243, "Satellite Spatial Resolution 100 x 400 meters"]
+[2.367367744445801, -1.3873387575149536, "Satellite Ability to Accurately Measure Methane Levels 2 parts per billion"]
+[3.1417343616485596, -1.551832675933838, "Satellite Mission Lead MIT"]
+[3.0453784465789795, -1.6489471197128296, "Satellite Mission Operator MIT"]
+[2.963221549987793, -1.766247034072876, "Satellite Managed By NASA's Goddard Space Flight Center"]
+[2.904877185821533, -1.5080792903900146, "Satellite Additional Partners Northrop Grumman, NASA\u2019s Ames Research Center, Harvard-Smithsonian Center for Astrophysics, MIT\u2019s Lincoln Laboratory, Space Telescope Science Institute"]
+[5.108271598815918, -4.298119068145752, "Satellite First Year of Science Operations Completion Date July 18"]
+[2.0238125324249268, -2.6751742362976074, "Satellite Number of Images in Southern Panorama 208"]
+[4.999749660491943, -4.484692573547363, "Satellite Mission Analysis Date Nov. 19, 2012"]
+[5.08278226852417, -4.5605034828186035, "Satellite Workshop Date March 13-15, 2013"]
+[2.568504571914673, -3.928772211074829, "Satellite URL http://www.esa.int/Our_Activities/Technology/Proba_Missions/About_Proba-3"]
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+[2.8363938331604004, -1.9374325275421143, "Satellite Soil Moisture Data Unknown"]
+[2.117021322250366, -1.2747907638549805, "Satellite Microwave Spectrum Measures the wetness of the land"]
+[-3.151782274246216, 1.869820237159729, "Shuttle Research Mission Reentry Date Feb.1, 2003"]
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+[3.855659008026123, 8.943100929260254, "Shuttle Orbiter Accident Investigation Largest investigation ever by NASA"]
+[3.841367244720459, 8.929459571838379, "Shuttle Orbiter Accident Investigation Help from many other institutions"]
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+[3.520975112915039, 13.400751113891602, "Laser Threat Warning Sensor Operation Static Earth viewing"]
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+[-1.4242454767227173, 13.360352516174316, "Solar Cells Application Powering Boeing's CST-100 Starliner spacecraft"]
+[0.6479828953742981, 12.008349418640137, "Sensor Data Availability Available for the general user community"]
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+[-2.560159921646118, 11.627372741699219, "Imagery Product Resolution 2.7 km"]
+[11.36355972290039, 5.580690383911133, "CubeSat Dimensions 100 x 100 x 227 mm"]
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+[-1.3698662519454956, 8.846487045288086, "Valve Role Allow trapped air escape during the launch phase"]
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+[-0.8324460983276367, 11.632893562316895, "Detector Cosmic Ray Events 40 billion"]
+[-0.8146551251411438, 11.557107925415039, "Detector Deployment Date 19 May 2011"]
+[-0.7823469638824463, 11.565683364868164, "Detector Presentation Date 2\u20139 July, 2013"]
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+[-3.0391805171966553, 4.329570293426514, "Spacecraft Battery Depth of Discharge Less than 10% of the battery capacity"]
+[-5.247215747833252, 7.4570841789245605, "Network Quantity 12,000+"]
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+[4.918099880218506, -4.375967025756836, "Satellite Formation Conference Date May 29-31, 2013"]
+[1.8055591583251953, -2.37636399269104, "Satellite Formation URL http://www.sffmt2013.org/PPAbstract/4067p.pdf"]
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+[0.09812281280755997, 15.286239624023438, "Electron Spectrometer Function Investigate the link between deep dielectric charging and the spacecraft anomalies"]
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+[-0.3338179886341095, 8.132006645202637, "Material Coefficient of Thermal Expansion Low"]
+[-0.34174641966819763, 8.171534538269043, "Material Mirror Surface Roughness A few angstrom (1\u00c5= 10-10 m)"]
+[-0.7928406596183777, 11.544967651367188, "Detector Design Modular"]
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+[-0.8219761848449707, 11.604243278503418, "Detector Scintillation Panels Thickness 8 mm"]
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+[-0.7846079468727112, 11.549538612365723, "Detector Total Mass 54 kg"]
+[0.5139763355255127, 10.920839309692383, "Image Sensor Development Date June 8-11, 2015"]
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+[-0.4093084931373596, 16.218660354614258, "Spectrograph Observation Start Date August 2019"]
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+[-4.941847801208496, 9.778902053833008, "Receiver Antenna Array Two by two"]
+[-4.935897350311279, 9.773285865783691, "Receiver Signal Power Boost Approximately 6 dB"]
+[-4.941226959228516, 9.781246185302734, "Receiver Direction of Arrival Estimation Accuracy Within a few degrees"]
+[-6.72348165512085, 10.078685760498047, "Antenna Array Components E1/E5 active antenna array with calibration network"]
+[-4.474672317504883, 15.917152404785156, "Radar Resolution 3 m"]
+[-4.470544815063477, 15.891892433166504, "Radar Polarimetry Modes Amplitude and phase information"]
+[-4.508666038513184, 15.942980766296387, "Radar Downlink Power Increased"]
+[-4.496875286102295, 15.912652015686035, "Radar GPS Position Knowledge Real-time within 60 m"]
+[-4.500821113586426, 15.912822723388672, "Radar Recording Technology Solid-state"]
+[1.4299458265304565, 2.8720874786376953, "Weather Facsimile Transmission Format Start signal (300 Hz), 3 seconds; Phasing signal, 5 seconds; Image (800 lines), 200 seconds; Stop signal (450 Hz), 5 seconds"]
+[1.4324710369110107, 2.805997848510742, "Weather Facsimile Transmission Schedule 4-minute slots with a break of 27 seconds between two transmissions"]
+[-3.8895349502563477, 6.842583656311035, "Data Collection Platform Report Dissemination Occurs in the 27-second intervals between WEFAX transmissions"]
+[-5.5521626472473145, 3.0167784690856934, "Telescope Component Misalignment Error Reduction From about 1 mm to about 1 \u00b5m"]
+[2.6648693084716797, 14.337174415588379, "Optical Instrument Collimation Procedure Can be performed at any time during the mission"]
+[2.6538515090942383, 14.363391876220703, "Optical Instrument Temperature Range Much wider"]
+[11.288165092468262, 5.512007236480713, "CubeSat Development Started As of 2007"]
+[5.220658779144287, -3.8775923252105713, "Satellite Launch Year 1999"]
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+[3.0815985202789307, -2.33241868019104, "Satellite Launch Year Unknown"]
+[-0.9576464891433716, -9.991247177124023, "Satellite Constellation Launch Year 2021"]
+[-0.9291276931762695, -10.02942180633545, "Satellite Constellation Imaging Capacity Maximize"]
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+[-2.1038217544555664, 6.220704078674316, "Aircraft Equipment Current Fleet Installation 70%"]
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+[-0.15464934706687927, 15.58538818359375, "Echelle Grating Spectrometer Design and Performance Unknown"]
+[-0.03424978256225586, 15.521038055419922, "Echelle Grating Spectrometer User's Handbook Version 1.1"]
+[-0.1216026172041893, 15.54499340057373, "Echelle Grating Spectrometer URL http://db.cger.nies.go.jp/ilas2/en/document/usershb/UHB_ALL_E.pdf"]
+[11.313492774963379, 5.5367350578308105, "CubeSat Mission Type Non-EO"]
+[11.225451469421387, 5.470559120178223, "CubeSat Mission Status Planned"]
+[11.188307762145996, 5.554330825805664, "CubeSat Launch Date Planned for 2024"]
+[11.302452087402344, 5.479151248931885, "CubeSat Development Status In development"]
+[11.28381633758545, 5.519993782043457, "CubeSat Spacecraft Type 12U CubeSat"]
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+[-0.06900171935558319, 9.77915096282959, "Inertial Reference Unit Angular Velocity Range 10\u00ba/s to 0.5\u00ba/s"]
+[-0.07404768466949463, 9.79711627960205, "Inertial Reference Unit Angular Random Walk 0.008\u00ba/sqrt hr"]
+[-4.361947059631348, 0.1924673616886139, "GPS Receiver Position Error 20 m in 3-D (1\u03c3)"]
+[-4.365027904510498, 0.18872563540935516, "GPS Receiver Linear Velocity Error 1 m/s (1\u03c3)"]
+[-4.356904983520508, 0.1519736349582672, "GPS Receiver Time Error < 0.2 \u00b5s (1\u03c3)"]
+[-0.7188962697982788, 7.662600994110107, "Concept Definition The perception of the elements in the environment within a volume of time and space, the comprehension of their meaning and the projection of their status in the near future"]
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+[0.2862081229686737, 10.631735801696777, "Situation Awareness Level Definition Comprehension of the current situation"]
+[0.27280551195144653, 10.635113716125488, "Situation Awareness Level Definition Projection of the future status"]
+[2.5142152309417725, -2.417786121368408, "Satellite Laser Pulses 10,000 per second"]
+[0.9332780241966248, -1.152575969696045, "Satellite Surface Height Measurements Interval Every 28 inches (70 cm)"]
+[0.4957974851131439, -1.4609042406082153, "Satellite Orbit Altitude 35,876 km"]
+[0.9642683267593384, -2.1588428020477295, "Satellite Orbit Location 9\u00baE"]
+[5.481298446655273, -4.4309868812561035, "Satellite Launch Date 6 August 2019"]
+[4.418118000030518, -3.3874106407165527, "Satellite Launch Time 19:30 UTC"]
+[2.637856960296631, -2.3278732299804688, "Satellite Launch Vehicle Ariane-5 ESA"]
+[2.761953830718994, 22.730886459350586, "Instrument Operating Mode Scan mode"]
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+[2.448086977005005, 22.750595092773438, "Instrument Wavelength Channels Six"]
+[4.081712245941162, 13.919837951660156, "Laser Altimeter System Measurement Method Sending pulses of light to Earth\u2019s surface and measuring the time for individual photons to return to the sensor"]
+[5.399044036865234, -4.395655155181885, "Satellite Launch Date September 2018"]
+[1.6427935361862183, -1.1112630367279053, "Satellite Measurement Capability Height of Earth\u2019s surfaces in remarkable detail"]
+[2.401153802871704, -1.251380205154419, "Satellite Data Collection Detailed elevation measurements over tropical and temperate latitudes"]
+[2.903707504272461, -1.3324916362762451, "Satellite Mission Goals Maintain continuous, reliable operational environmental, and storm warning systems to protect life and property; Monitor the Earth's surface and space environmental and climate conditions; Introduce improved atmospheric and oceanic observations and data dissemination capabilities; Develop and provide new and improved applications and products for a wide range of federal agencies, state and local governments, and private users"]
+[2.632256507873535, -1.333851933479309, "Satellite Additional Capabilities GBR (GOES-R Re-Broadcast), S&R (Search & Rescue), DCS (Data Collection System), EMWIN (Emergency Managers Weather Information Network), and LRIT (Low Rate Information Transmission) communications"]
+[-0.5339141488075256, 8.252458572387695, "Composite Structure Material Titanium-glass-epoxy-graphite"]
+[-0.5430036783218384, 8.308363914489746, "Support Structure Material Titanium"]
+[-5.80496883392334, 15.88000202178955, "Aperture Covers Material 5 \u00b5m polyimide"]
+[6.147129535675049, 7.570730686187744, "Satellite Components Quantity 3"]
+[-2.2203714847564697, 6.3364152908325195, "Flight Modules Function First two modules are the flight units, and the third module is to provide for more extensive X-ray characterization"]
+[-2.563066005706787, 8.164863586425781, "Fault Detection, Isolation, and Recovery System Purpose Ensure continuous monitoring of the RVX GNC and the satellites\u2019 relative state, and prompt response to failures"]
+[-2.5682218074798584, 8.21218204498291, "Fault Detection, Isolation, and Recovery System Design Requirement Ensure that the overall RVX SW is single-failure tolerant"]
+[-2.573519468307495, 8.214200973510742, "Fault Detection, Isolation, and Recovery System Failure Response Trigger a CAM (Collision Avoidance Maneuver) in case of imminent risk of collision"]
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+[1.6677541732788086, -1.4371650218963623, "Satellite Detection Range Under 15 keV"]
+[2.3769307136535645, -1.7622522115707397, "Satellite Component Thermal component"]
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+[6.3671135902404785, 7.376259803771973, "Satellite Component Test Date September 2021"]
+[6.324463844299316, 7.415763854980469, "Satellite Component Hosts The cameras"]
+[6.340366363525391, 7.401460647583008, "Satellite Component Production, Assembly, and Testing Successfully Exercised"]
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+[2.1138548851013184, -1.6689095497131348, "Satellite Operating Mode MRS (Medium Resolution ScanSAR)"]
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+[1.282325029373169, -1.8976448774337769, "Satellite Radiometric Balance Within \u00b1 0.5 dB"]
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+[-3.6166701316833496, 12.746859550476074, "Particle Detector Energy Range 20-200 GeV"]
+[-3.7207131385803223, 12.846661567687988, "Particle Detector Positron Flux Higher than the rate for electrons"]
+[-3.643120527267456, 12.760127067565918, "Particle Detector Electron and Positron Fluxes Fundamental Difference"]
+[2.807587146759033, -2.464005470275879, "Satellite Frequency Range 0.1 mHz to 1 Hz"]
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+[2.793564796447754, -2.185214042663574, "Satellite Wavelength Much longer"]
+[1.8431092500686646, -2.0636649131774902, "Satellite Orbits Much wider"]
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+[0.05769045278429985, 7.264431953430176, "Experiment Vacuum Cases Structures Mechanically identical"]
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+[-2.2629544734954834, 7.414373874664307, "On-Board Computer Function Task management, data conversion, time management"]
+[-2.245891809463501, 7.430294513702393, "On-Board Computer Function RF communication subsystems"]
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+[-2.255490779876709, 7.3845438957214355, "On-Board Computer Communication Interface SPI (Serial Peripheral Interface)"]
+[2.4730238914489746, -2.2818970680236816, "Satellite Radio Transmission Mode CW (beacon) transmission and FM transmission"]
+[2.4344372749328613, -2.0511035919189453, "Satellite CW Transmission Mode Provides the sensor data of the satellite health monitoring, such as power, temperature, and attitude to the ground station via the Morse code"]
+[-5.898646831512451, 16.005586624145508, "Synthetic Aperture Radar Band L-band"]
+[-5.864046573638916, 15.989550590515137, "Synthetic Aperture Radar System Components Exciter (EX), Transmitter (TX), Receiver (RX), Digital Processor (DP), and System controller (SC)"]
+[11.834979057312012, 5.287266731262207, "6U CubeSat Mission Reconnaissance of an asteroid, take pictures and observe its position in space"]
+[11.809768676757812, 5.303490161895752, "6U CubeSat Mission Detect, measure and compare the impact of deep space radiation on living organisms over long durations in deep space"]
+[11.796076774597168, 5.315525531768799, "6U CubeSat Mission Look for ice deposits and identify locations where resources may be extracted from the lunar surface"]
+[11.808076858520508, 5.309517860412598, "6U CubeSat Mission Measure particles and magnetic fields in space, testing the practicality for a network of stations to monitor space weather"]
+[11.821181297302246, 5.274120330810547, "6U CubeSat Mission Map hydrogen within craters and other permanently shadowed regions throughout the moon\u2019s south pole"]
+[-3.3774936199188232, 7.205799579620361, "Data Handling System CPU 8086 rad-hard"]
+[-3.373147487640381, 7.1954827308654785, "Data Handling System Power 6 W"]
+[-3.3949997425079346, 7.202945709228516, "Data Handling System SCI ports Six RS-422, MIL-STD-1553 S/C bus"]
+[-3.3842179775238037, 7.151771545410156, "Data Handling System RAM 512 k"]
+[-3.3459737300872803, 7.209445953369141, "Data Handling System PROM 32 k PROM"]
+[-3.324655055999756, 7.149026870727539, "Data Handling System Total mass of assembly 2 kg"]
+[-3.375080108642578, 7.20260763168335, "Data Handling System Power to sub-experiments 28 V isolated +5 V, \u00b112 V"]
+[-3.3568665981292725, 7.191421031951904, "Data Handling System Radiation hardness about 100 krad"]
+[-3.3528189659118652, 7.1717071533203125, "Data Handling System CPU 8051 rad-hard"]
+[-3.3377034664154053, 7.216352939605713, "Data Handling System Power 3 W"]
+[-3.388000011444092, 7.1799211502075195, "Data Handling System SCI ports Eleven RS-422"]
+[-3.3663339614868164, 7.193332672119141, "Data Handling System RAM 1024 k"]
+[-3.354020833969116, 7.177004337310791, "Data Handling System PROM 32 k PROM"]
+[-3.345848560333252, 7.232417106628418, "Data Handling System Total mass of assembly 1.2 kg"]
+[-3.325246572494507, 7.230929851531982, "Data Handling System Power to sub-experiments +5 V, \u00b112 V"]
+[-3.3538103103637695, 7.210398197174072, "Data Handling System Radiation hardness about 100 krad"]
+[1.5385099649429321, -2.396967887878418, "Satellite Orbit Type Elliptical GTO"]
+[0.7053372263908386, -1.187968134880066, "Satellite Perigee Altitude 280 km"]
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+[3.9703328609466553, -2.8601748943328857, "Satellite Period 10 hours and 27 minutes"]
+[1.3416839838027954, -1.380014181137085, "Satellite Radiation Exposure Very high"]
+[2.6062536239624023, -2.226619243621826, "Satellite Receiver Usability One receiver on each spacecraft remained usable"]
+[-5.303936958312988, 7.495704174041748, "Protocol Responsible for Core subsystem communication"]
+[0.5426799058914185, 11.970977783203125, "Sensor Bus Purpose Allow interstage boards to act as intermediaries between sensors and the ADCS computer"]
+[-5.28031063079834, 7.478039264678955, "Communication Protocol Usage For some specialized payloads"]
+[3.697747230529785, 22.96196937561035, "Instrument Inter-Calibration Date 25 July 2018"]
+[3.032078504562378, 22.512920379638672, "Instrument URL https://www.wmo-sat.info/oscar/instruments/view/88"]
+[0.4378391206264496, 12.053037643432617, "Space Debris Sensor Surface Area 1 m2"]
+[0.42659205198287964, 11.990677833557129, "Space Debris Sensor Minimum Detectable Size 50 \u00b5m"]
+[0.3577077090740204, 11.994280815124512, "Space Debris Sensor Operation Duration At least two years"]
+[-0.9870330095291138, 13.121795654296875, "Solar Irradiance Sensor Mounting Location ELC-3 platform, which is attached to the station\u2019s P3 port truss segment"]
+[-0.9897237420082092, 13.13167667388916, "Solar Irradiance Sensor Measurement Sun's energy input to Earth"]
+[-3.572509765625, 4.367931842803955, "Spacecraft Departure Date January 2018"]
+[-3.0176141262054443, 4.4030232429504395, "Spacecraft Return Cargo More than 1630 kg of research, hardware and crew supplies"]
+[0.7326198220252991, -1.1786476373672485, "Satellite Altitude 270 km"]
+[0.7496829032897949, -2.299689292907715, "Satellite \u03b2 Angle -60\u00ba"]
+[1.9030323028564453, -0.8081145882606506, "Satellite Solar Power Generation Proportional to sin|\u03b2|"]
+[0.851485550403595, -2.3091890811920166, "Satellite Change of \u03b2 Angle Consists mostly of the long-term change of right ascension of the ascending node by geopotential (d\u03a9/dt)"]
+[-1.122467279434204, 4.485192775726318, "Ground Station Location Maspalomas station, at the southern end of the largest island of the Canary Islands"]
+[-1.1211366653442383, 4.466827869415283, "Ground Station Location Svalbard site on Spitsbergen in the Norwegian Arctic"]
+[-9.951689720153809, 5.8525285720825195, "Search and Rescue System Founders Canada, France, Russia and the US"]
+[-2.0375282764434814, 15.013825416564941, "Geophysical Variable Accuracy Range 2 m/s or 10%"]
+[-2.0914242267608643, 15.076798439025879, "Geophysical Variable Accuracy Range 2 K"]
+[-2.102349042892456, 15.071503639221191, "Geophysical Variable Accuracy Range 20%"]
+[-2.073237895965576, 15.068103790283203, "Geophysical Variable Accuracy Range 0-5 mm/hr"]
+[-2.097883462905884, 15.075788497924805, "Geophysical Variable Accuracy Range 0.4 g/kg 2-20 g/kg"]
+[-2.143143892288208, 15.111372947692871, "Geophysical Variable Accuracy Range 35 Wm- 2 0-200 Wm -2"]
+[-5.924099445343018, 15.993182182312012, "Synthetic Aperture Radar Swath Width 100 km"]
+[-5.880847454071045, 15.982738494873047, "Synthetic Aperture Radar Resolution 25 km"]
+[-5.893367767333984, 16.023080825805664, "Synthetic Aperture Radar Mapped Area 100 million km2"]
+[14.231919288635254, 7.820988655090332, "Nanosatellite Launch Date Nov. 21, 2013"]
+[14.711518287658691, 7.808837890625, "Nanosatellite Mass 10 kg"]
+[14.696757316589355, 7.809515953063965, "Nanosatellite Mass 7 kg"]
+[14.710962295532227, 7.83492374420166, "Nanosatellites Mass 12 kg"]
+[16.822669982910156, 6.876156806945801, "Microsatellite Mass 28 kg"]
+[-4.962833404541016, 2.9002065658569336, "Space Telescope Observational Target Rocky Exoplanets"]
+[-0.4115600287914276, 16.22572898864746, "Spectrographs Location Calar Alto Observatory (Almeria, Spain)"]
+[2.735499858856201, 22.244861602783203, "Instrument Location W. M. Keck Observatory (Mauna Kea, Hawaii)"]
+[2.124971389770508, -1.5091270208358765, "Satellite Observation Method Measured the \u201cwobble\u201d of the star, caused by the gravitational tugs from orbiting planets (radial velocity)"]
+[-3.1392133235931396, 1.70088529586792, "Satellite Mission Purpose Planet-hunting"]
+[-3.146265983581543, 1.675870418548584, "Satellite Mission URL https://www.cosmos.esa.int/web/plato/"]
+[-3.267918109893799, 1.6892260313034058, "Satellite Mission Announcement Date 11 April, 2018"]
+[-4.263469696044922, 7.367154598236084, "Data Transmission Data Rate 1.33 MBit/s"]
+[-4.281405448913574, 7.36555814743042, "Data Transmission Data Rate 2.66 Mbit/s"]
+[-4.234761714935303, 7.396156311035156, "Data Transmission Data Stream 3.072 Mbit/s"]
+[-0.42425537109375, 14.510502815246582, "Imaging Instrument Full Disk Circle Size 17.4\u00ba diameter"]
+[-0.4223770499229431, 14.520853042602539, "Imaging Instrument CONUS Rectangle Size 4.81\u00ba 8.02\u00ba"]
+[-0.4175851345062256, 14.503432273864746, "Imaging Instrument Mesoscale Square Size 1.60\u00ba 1.60\u00ba"]
+[-0.4233663082122803, 14.535630226135254, "Imaging Instrument Full Disk Circle Height 3000 km"]
+[-0.4268839657306671, 14.582352638244629, "Imaging Instrument Full Disk Circle Width 5000 km"]
+[-0.41980645060539246, 14.526208877563477, "Imaging Instrument CONUS Rectangle Height 3000 km"]
+[-0.41536182165145874, 14.52645206451416, "Imaging Instrument CONUS Rectangle Width 5000 km"]
+[-0.39542919397354126, 14.512542724609375, "Imaging Instrument Mesoscale Square Height 1000 km"]
+[-0.3974008560180664, 14.506575584411621, "Imaging Instrument Mesoscale Square Width 1000 km"]
+[-2.466890335083008, 13.309226036071777, "Hyperspectral Camera Spectral Range 400-800 nm"]
+[-2.466763973236084, 13.326699256896973, "Hyperspectral Camera Detector Size 640 x 480 pixels"]
+[-2.428990364074707, 13.257122039794922, "Hyperspectral Camera Data Quantization 8 bits"]
+[-2.45281720161438, 13.298479080200195, "Hyperspectral Camera Sampling Rate 30 frames/s"]
+[3.666628360748291, 17.640913009643555, "Payload Cryomag with planes of detectors Above, inside and below the magnet"]
+[-0.6300561428070068, 11.723684310913086, "Silicon Tracker Detector Function Measures the particle's momentum in the strong magnetic (B) field of the AMS"]
+[-0.6467303037643433, 11.70526123046875, "Silicon Tracker Detector Detects The trajectory of the incoming particles and identifies the magnitude and polarity of the particles\u2019 electrical charge"]
+[-6.707072734832764, 9.973156929016113, "Antenna Polarization Circular"]
+[-6.715845584869385, 9.981529235839844, "Antenna Type Dipole"]
+[-0.02610461786389351, 15.400459289550781, "Aerosol Monitoring Instrument Number of CCD cameras 2"]
+[-0.08608264476060867, 15.433964729309082, "Aerosol Monitoring Instrument Spectral Range 430-900 nm"]
+[0.5609927177429199, 12.0353364944458, "In Situ Impact Sensor Sensor Type Piezoelectric devices"]
+[0.13651064038276672, 7.18765115737915, "Experiment Purpose Evaluate a new way of providing tactile and visual feedback to astronauts when operating robots"]
+[0.1768583059310913, 7.227798938751221, "Experiment Equipment Virtual reality headset and a haptic joystick"]
+[-3.0901453495025635, 4.798879146575928, "Resupply Ship Cargo Capacity Over 7,300 pounds"]
+[-0.6857977509498596, 6.783120155334473, "Research Purpose Improve treatments for kidney stones and osteoporosis"]
+[-0.6293330192565918, 8.462539672851562, "Freezers Content Biological samples"]
+[1.5208290815353394, -1.1702231168746948, "Satellite Spotlight Mode Resolution Better than one meter in azimuth"]
+[4.908621311187744, -4.31455135345459, "Satellite Polarimetric SAR Test Data Availability May 2008"]
+[2.2451345920562744, -1.9075422286987305, "Satellite Left or Right Looking Modes Available"]
+[1.8857840299606323, -1.3117986917495728, "Satellite Pre-defined Modes Performance Met requirements in all aspects of image quality"]
+[4.847967147827148, -4.473036766052246, "Satellite Initial Image Acquisition Dec. 18, 2007"]
+[-2.6176257133483887, 8.319900512695312, "Net Capture Mechanism Deployment Time Approximately 100 s"]
+[-2.5717716217041016, 8.34585952758789, "Net Capture Mechanism Manufacturer Airbus DS, Bremen"]
+[-2.6082019805908203, 8.372584342956543, "Net Capture Mechanism Closure Method Motor driven winches"]
+[-0.13450656831264496, 11.188167572021484, "Monitoring System Data Source Climate, soil, and water conditions"]
+[-1.340361475944519, 6.176876068115234, "Organization Provider of Experimental Measurements and Models Unknown"]
+[-3.579010009765625, 6.90601921081543, "Data Source Contributor to Map Unknown"]
+[0.46846282482147217, 11.269146919250488, "Vision Based Sensor Components WAC, NAC, ISM, MOH, AMU, STR CHU, MIRU, DPU"]
+[-7.555245876312256, 5.896255016326904, "Wide Angle Camera Observation Range 12 - 100 m"]
+[-7.561848163604736, 5.881943702697754, "Narrow Angle Camera Observation Range 50 - 550 m"]
+[-4.654754161834717, 7.983317852020264, "Integration Synchronization Module Function Registers the pulse from the Mire Beacons on CSC to synchronize the integration of the WAC and NAC with the pulsed Beacon"]
+[2.697510004043579, 13.615718841552734, "Mire Optical Head Function Emits a pulsed infrared signal. Combined, the MOHs enable 6 DOF resolution of the relative state when operating in cooperative mode"]
+[-1.5934323072433472, 8.332368850708008, "Acquisition Mire Unit Function Emits a high-power beacon that enables target acquisition at far range with Earth in the background of CSC"]
+[-0.7405338287353516, 3.254406213760376, "Star Tracker Camera Head Unit Function Observes the stellar sky to resolve the inertial pointing of the spacecraft"]
+[-0.05885275453329086, 9.81092643737793, "Micro Inertial Reference Unit Function Is co-integrated with the STR CHU delivering angular rates at high bandwidth"]
+[-3.2050039768218994, 7.705323219299316, "Digital Processing Unit Function Controls the optical sensor and processes the images. Determines the inertial pointing of the STR CHUs and the relative state of CSC using the VBS cameras"]
+[-3.001426935195923, 20.191234588623047, "Spectral Band Center Wavelength 3.8 \u00b5m"]
+[-2.9447598457336426, 20.14766502380371, "Spectral Band Spectral Range 3.4-4.2 \u00b5m"]
+[-2.9545114040374756, 20.165748596191406, "Spectral Band Temperature 300 K (min)"]
+[-2.8939974308013916, 20.162277221679688, "Spectral Band Temperature 700 K (max)"]
+[-2.726445436477661, 20.34333610534668, "Spectral Band NETD < 0.5 K @ 400 K scene"]
+[-2.9502668380737305, 20.182971954345703, "Spectral Band Ground Pixel Size 351 m"]
+[-2.56795334815979, 19.988136291503906, "Spectral Band Swath Width 182 km"]
+[-2.592334508895874, 20.002798080444336, "Spectral Band In Field Separation 18 km"]
+[-2.9778144359588623, 20.14901351928711, "Spectral Band Boresight Pointing \u00b130\u00ba from nadir"]
+[-2.6017041206359863, 20.002901077270508, "Spectral Band FOR in Cross-Track 1060 km"]
+[-4.943988800048828, 9.776342391967773, "Receiver Designed for Cubesat Operations"]
+[1.4168426990509033, -3.1668508052825928, "Satellites General Relativity Test Conducted"]
+[-1.2038682699203491, 3.8875162601470947, "Earth Gravity Model Used in Test Yes"]
+[-3.1175217628479004, 1.7494803667068481, "Satellite Mission Ice Mass Loss 280 Gt per year"]
+[-3.1520965099334717, 1.7237567901611328, "Satellite Mission Global Sea Level Rise 11.2 mm (0.4 inches)"]
+[-3.1582608222961426, 1.7026702165603638, "Satellite Mission Greenland Ice Loss 600 gigatons in two months"]
+[-3.151799440383911, 1.7058758735656738, "Satellite Mission Global Sea Level Rise Contribution from Greenland and Antarctic ice sheets 1.2 mm per year"]
+[-3.172799587249756, 1.7323771715164185, "Satellite Mission Mountain Glaciers Ice Loss 200 gigatons per year"]
+[-2.6575827598571777, 11.679656028747559, "Imager Time of Image Acquisition 1:20 p.m. Eastern Standard Time (17:20 Universal Time)"]
+[2.0951650142669678, -2.7255260944366455, "Satellite Instrument Count 6"]
+[-2.6526119709014893, 11.62401294708252, "Imager Restoration Time Earlier this morning"]
+[3.304354190826416, -1.8673386573791504, "Satellite Expected Full Recovery On track for a full recovery with no lasting effects to the satellite"]
+[1.7645708322525024, -2.124516487121582, "Satellite Orbit Near-Earth space"]
+[-0.8915584087371826, 12.413854598999023, "Radiation Belts Shape Doughnut-shaped"]
+[-2.4747202396392822, 4.089356899261475, "Space Region Location Gap between two of Earth\u2019s vast radiation belts"]
+[-1.3799563646316528, 6.239921569824219, "Team Members Michael Xapsos, Yihua Zheng"]
+[-1.8638371229171753, 14.921854972839355, "Scanning Radiometer Unknown Unknown"]
+[1.20785653591156, 10.912461280822754, "Scanner Unknown Unknown"]
+[-3.2706243991851807, 5.422392845153809, "Launch Vehicle Payload NASA\u2019s space telescope, James Webb"]
+[1.4146897792816162, -3.1108264923095703, "Satellites Manufacturer Thales Alenia Space"]
+[1.4005911350250244, -3.1269805431365967, "Satellites Purpose Connectivity and security"]
+[-4.98022985458374, 2.891054630279541, "Space Telescope Launch Partner European Space Agency"]
+[-1.7710059881210327, 14.988578796386719, "Imaging Radiometer Detector Array Uncooled"]
+[-1.7739980220794678, 15.049837112426758, "Imaging Radiometer Focal Plane Array 327 x 240 pixel"]
+[-1.7095187902450562, 15.066817283630371, "Imaging Radiometer Technology Microbolometer Focal Plane Arrays"]
+[-1.7412554025650024, 14.981348037719727, "Imaging Radiometer Operation Infrared imaging without external cooling"]
+[-1.7701654434204102, 14.98166561126709, "Imaging Radiometer Objective Measurement of the infrared brightness temperature of cloud tops as well as the Earth's surface"]
+[-8.108341217041016, 8.81638240814209, "Power Subsystem Total Array Area 7.1 m2"]
+[-8.114441871643066, 8.819321632385254, "Power Subsystem Total Power (BOL) 2300 W"]
+[-8.106773376464844, 8.814764976501465, "Power Subsystem Total Power (EOL) 1730 W"]
+[-8.112747192382812, 8.816655158996582, "Power Subsystem Mass < 40 kg"]
+[-1.6431188583374023, 9.605018615722656, "Drive Mechanism Motor Step Angle 1.5\u00ba"]
+[-1.481909990310669, 9.257649421691895, "Drive Mechanism Mass < 3.2 kg"]
+[-2.2992055416107178, 9.121785163879395, "Power Control and Distribution Unit Main Power Bus Voltage 28 V \u00b14 V"]
+[-2.347639560699463, 9.158135414123535, "Power Control and Distribution Unit Mass < 21.6 kg"]
+[-3.0948171615600586, 9.64968490600586, "Batteries Total Capacity 102 Ah @ EOL"]
+[-3.0631725788116455, 9.622478485107422, "Batteries Mass 51 kg"]
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+[-0.9462991952896118, 6.459384441375732, "Documentation Author Herbert J. Kramer"]
+[-0.9628791213035583, 6.478893280029297, "Documentation Publisher Springer Verlag"]
+[-0.9468936324119568, 6.464653968811035, "Documentation Edition 4th edition"]
+[-0.8496874570846558, 6.132714748382568, "Website Contact Email eoportal@symbios.space"]
+[-0.9746217131614685, 6.233976364135742, "Copyright Year 2024"]
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+[-5.417635440826416, 2.7840969562530518, "Telescope Ability Measure the energy of smaller microflares"]
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+[-7.333293437957764, 6.1391472816467285, "Camera System Image Credit NASA/Digital Mapping System"]
+[-0.8342882394790649, 12.656461715698242, "Space Radiation Monitor Measurement Objective Measure the total ionizing dose from the population of charged particles at the orbital altitude"]
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+[4.2894392013549805, -2.753040075302124, "Satellite Data Downlink Time Within eight hours"]
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+[-1.2232837677001953, 13.288249015808105, "Solar Instrument Stray Light Rejection Experimental Developments"]
+[-0.7165004014968872, 11.482926368713379, "Filter Function Energetic electron detector in sprites and aurora"]
+[-0.7724857926368713, 11.568315505981445, "Filter Function Detect N2 1st positive emission from sprites"]
+[-0.7935746312141418, 11.533914566040039, "Filter Function Detect lightning and act as a possible TLE event trigger"]
+[1.879563570022583, 10.721132278442383, "Imaging Device Image Capture Five images in quick sequence"]
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+[-0.6079872250556946, 8.67228889465332, "Heat Shield Material Composition Heat-retardant substance similar to what the Apollo missions used, with the exception of toxic materials like asbestos"]
+[-0.6304656267166138, 8.736861228942871, "Heat Shield Material Function Burns away (i.e., it ablates) in order to prevent heat being transferred into the crew module"]
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+[-7.5685505867004395, 5.884037017822266, "Camera Affiliation Suisse d'Electronique et de Microtechnique SA - Recherche et Development (CSEM), Switzerland"]
+[11.24984359741211, 5.413101673126221, "CubeSat Component Affiliation Stellenbosch University \u2013 Electronic System Laboratory (ESL), South Africa"]
+[-2.2603490352630615, 2.8349342346191406, "Gravitational Wave Observatory Spacecraft Separation 2.5 million km"]
+[2.642174005508423, 14.312451362609863, "Optical Instrument Coherent Laser Light Wavelength 1.06 \u00b5m"]
+[-0.8022230863571167, 3.1645913124084473, "White-dwarf Binary Orbital Period 7 minutes"]
+[-0.9430602192878723, 3.17092227935791, "White-dwarf Binary Eclipsing Behavior The white dwarfs eclipse each other as viewed from Earth"]
+[1.8750420808792114, -0.28835612535476685, "Radar Imaging Satellite Data Transmission Rate 640 Mbit/s"]
+[1.8741140365600586, -0.2297276109457016, "Radar Imaging Satellite Mass 1858 kg"]
+[1.8751709461212158, -0.23679372668266296, "Radar Imaging Satellite Number of Processors 300"]
+[1.8633934259414673, -0.2872762978076935, "Radar Imaging Satellite Number of Beams 126"]
+[1.8613170385360718, -0.21574394404888153, "Radar Imaging Satellite Flexibility Reconfigurable to meet different imaging requirements"]
+[-3.7854037284851074, 6.952697277069092, "Data Collection System Data Flows Unknown"]
+[7.298633098602295, 12.433867454528809, "Satellite Instrument Technical Requirements Document S-415-200, March 2000"]
+[6.39333438873291, 7.3382649421691895, "Satellite Component Stressful Periods Low beta angle (long eclipse)"]
+[6.361915111541748, 7.380202293395996, "Satellite Component Stressful Periods High beta angle"]
+[6.283245086669922, 7.462732791900635, "Satellite Component Effect of Low Beta Angle Reduced"]
+[6.38289737701416, 7.355602264404297, "Satellite Component Effect of High Beta Angle Higher"]
+[1.681889295578003, 6.954757213592529, "Communication Device Downlink Frequency S-band"]
+[-6.719899654388428, 9.985638618469238, "Antenna Frequency Range 2226.42 \u2013 2226.52 MHz"]
+[-1.9461054801940918, 8.086773872375488, "System Operational Link Frequency L-band"]
+[-1.9263856410980225, 8.060751914978027, "System Primary Partner Agencies NASA, NOAA, USAF, and USCG"]
+[-1.911763310432434, 8.121803283691406, "System Managing Agencies NOAA, the USAF, and the USCG"]
+[1.4377864599227905, -1.6107410192489624, "Satellite Energy Range 0.03 - 100 keV"]
+[-5.352455139160156, 2.766617774963379, "Telescope Manufacturer Space Research Center of the University of Leicester, UK"]
+[1.4414660930633545, -1.8760918378829956, "Satellite Radiometric Accuracy Stable and within expectations"]
+[1.2616164684295654, -1.7789820432662964, "Satellite Mean Radiometric Error Approximately -0.1 dB on ascending passes and +0.15 dB on descending passes"]
+[1.908990740776062, -2.0389740467071533, "Satellite Population Standard Deviation 0.3 dB"]
+[-4.675053596496582, 7.8634185791015625, "Telemetry, Tracking and Command System Frequency Band S-band"]
+[-1.575703740119934, 4.122011184692383, "Ground Segment Facility Location NRSC (National Remote Sensing Center), Shadnagar, Hyderabad Complex"]
+[-5.63386869430542, 15.900633811950684, "Hardware Quick Look SAR Processor Manufacturer MRSA/SAC team"]
+[-5.694931983947754, 15.937451362609863, "Near Real Time SAR Processor Manufacturer MRSA/SAC team"]
+[-0.8319529891014099, 7.669424533843994, "Cloud Discrimination Device Band 1.60 \u00b5m"]
+[7.305910110473633, 12.434303283691406, "Satellite Instrument Bands 1, 2, 3"]
+[0.5342183113098145, 12.249160766601562, "Sensor Measurement Wavelengths 308.6, 312.5, 317.5, 322.3, 331.2 and 360 nm"]
+[0.5008630156517029, 12.17951488494873, "Sensor Swath Width 2795 km"]
+[0.5891078114509583, 12.159520149230957, "Sensor IFOV 50 km at nadir"]
+[0.5196768641471863, 12.104763984680176, "Sensor Cross-track Scan 111\u00ba (37 3\u00ba steps)"]
+[0.6964753270149231, 12.086445808410645, "Sensor Mass 34 kg"]
+[0.7259595394134521, 12.079914093017578, "Sensor Power 24 W"]
+[0.5136929750442505, 12.184880256652832, "Sensor Data Rate 700 bit/s"]
+[-0.809565007686615, 11.572187423706055, "Detector Photon Detection Thousands of photons per laser fire"]
+[-5.357245445251465, 2.8031551837921143, "Telescope and Detector Photon Detection Few to ~10 photons per footprint per laser fire"]
+[-0.8069072365760803, 11.61056137084961, "Detector Time Tagging Precision 0.15 ns"]
+[-3.4802327156066895, 7.097812652587891, "Data Output Range Precision < 20 cm"]
+[-3.4984142780303955, 7.061777114868164, "Data Output Elevation Data Resolution Higher spatial and vertical resolution"]
+[5.302194118499756, -4.492116451263428, "Satellite Launch Date 27 May 1999"]
+[5.082512378692627, -4.181077003479004, "Satellite End of Life Date 21 January 2003"]
+[2.114072799682617, -1.2845929861068726, "Satellite Measurement Domain Atmosphere"]
+[2.017822027206421, -1.2306653261184692, "Satellite Measurement Category Atmospheric Temperature Fields, Atmospheric Humidity Fields, Atmospheric Winds"]
+[2.3063087463378906, -1.439067006111145, "Satellite Instrument Type Other, Atmospheric chemistry, Data collection, Atmospheric temperature and humidity sounders"]
+[-5.874189853668213, 16.000995635986328, "Synthetic Aperture Radar Observation Capabilities Longer wavelength and enhanced penetration"]
+[2.3946170806884766, -1.1287635564804077, "Satellite Measurement Capabilities Land, disasters, geohazards, and the cryosphere"]
+[2.2373971939086914, 23.1783504486084, "Instrument Frequency 13.4 GHz"]
+[1.6521486043930054, 23.197683334350586, "Instrument Power 110 W"]
+[2.265070676803589, 23.234325408935547, "Instrument Pulse Repetition Frequency 189 Hz"]
+[1.7439302206039429, 22.214658737182617, "Instrument Diameter 1 m"]
+[2.064758062362671, 22.425132751464844, "Instrument Accuracy 2 m/s"]
+[2.1403768062591553, 22.32592010498047, "Instrument Accuracy 20\u00ba"]
+[1.8331626653671265, 22.15822410583496, "Instrument Resolution 25 km"]
+[-4.481545925140381, 15.920440673828125, "Radar Mass 205 kg"]
+[-4.500020980834961, 15.938104629516602, "Radar Power 250 W"]
+[-4.48870849609375, 15.918757438659668, "Radar Data Rate 40 kbit/s"]
+[5.332519054412842, -4.450620651245117, "Satellite Launch Date Aug. 23, 1962"]
+[2.8317525386810303, -1.106076955795288, "Satellite Purpose Provide information on cloud cover over the Soviet Union"]
+[2.8783867359161377, -1.4930473566055298, "Satellite Use Support military operations"]
+[2.740389823913574, -1.3752387762069702, "Satellite Use Weather forecasting"]
+[2.8886876106262207, -1.570046067237854, "Satellite Use Help plan future launches"]
+[3.023653030395508, -1.4691940546035767, "Satellite Mission Type Small Explorer"]
+[-1.1703734397888184, 3.0638582706451416, "Celestial Object Diameter Hundreds of thousands of times smaller than the Sun"]
+[-1.167494535446167, 3.071315288543701, "Celestial Object Mass One to two times the mass of the Sun"]
+[-1.180363655090332, 3.0730490684509277, "Celestial Object Brightness Even brighter than average"]
+[-1.1685206890106201, 3.063937187194824, "Celestial Object Class Ultraluminous neutron stars"]
+[11.276329040527344, 5.48772668838501, "CubeSat Designing University Korea Aerospace University (KAU)"]
+[6.32894229888916, 7.41757345199585, "Satellite Component Components Multi-anode photon multiplier tube(MaPMT), a camera, and a real-time image processing engine"]
+[2.1058900356292725, -2.643693685531616, "Satellite Quantity 64"]
+[2.3676490783691406, -2.1366913318634033, "Satellite Type 15 microsatellites and 49 CubeSats"]
+[2.4037561416625977, -1.6723212003707886, "Satellite Countries United States, Australia, Italy, Netherlands, Finland, South Korea, Spain, Switzerland, UK, Germany, Jordan, Kazakhstan, Thailand, Poland, Canada, Brazil, and India"]
+[-3.107388496398926, 4.694263935089111, "Cargo Freighter Length 17.6 m"]
+[1.32867431640625, -3.091895341873169, "Satellites Size 3.5 cm2 per side"]
+[-2.1267178058624268, 4.312417984008789, "Space Station Operational Period Until 2030"]
+[-0.7169626355171204, 5.106059551239014, "Country Station Operations Period Until 2028"]
+[-2.771108627319336, 7.915558338165283, "Processor Number of Processors 4"]
+[-2.774500608444214, 7.91036319732666, "Processor Processing Power 120 Megaflop"]
+[-2.6977953910827637, 7.901228427886963, "Processor Mass 1.4 kg"]
+[-2.729926586151123, 7.900821208953857, "Processor Power 17 W"]
+[2.6847026348114014, -2.242169141769409, "Satellite Band Ka-band"]
+[-1.9418883323669434, 6.913414478302002, "Software Function Enable the dynamic control and optimization of power, throughput, beams and frequency allocation"]
+[2.8841440677642822, -1.6545429229736328, "Inflight Connectivity Service Region Americas and the Atlantic Ocean region"]
+[4.650188446044922, -2.6217970848083496, "Satellite Mission Duration Ten years"]
+[4.540431499481201, -2.5140602588653564, "Satellite Mission Duration Not specified"]
+[-3.623192310333252, 7.240175247192383, "Data Flow Data Rate 600 Mbit/s or 1.8 Gbit/s"]
+[-3.64981746673584, 7.198025226593018, "Data Flow Data Rate 500 bit/s or 4 kbit/s"]
+[-3.6609785556793213, 7.1797637939453125, "Data Flow Data Rate 300 Mbit/s"]
+[-3.6123058795928955, 7.290556907653809, "Data Flow Data Rate 1 Mbit/s"]
+[-3.1978402137756348, 7.588033676147461, "Data Processing Unit Data Stream Width 16-bit"]
+[-3.210016965866089, 7.559618949890137, "Data Processing Unit Data Stream Rate 1800 Mbit/s"]
+[-3.2076222896575928, 7.6279988288879395, "Data Processing Unit Information Rate 300 Mbit/s"]
+[-3.1921186447143555, 7.611301422119141, "Data Processing Unit Useful Data Rate 600 Mbit/s"]
+[-1.92059326171875, 14.89785099029541, "Radiometer Unknown Unknown"]
+[-1.8940094709396362, 14.818520545959473, "Radiometer URL http://www.eorc.jaxa.jp/ADEOS/Project/Avnir.html"]
+[0.516883373260498, 10.928573608398438, "Image Sensor Saturation Limit IC = 7:5"]
+[0.518430769443512, 10.920854568481445, "Image Sensor Read Noise 10 e-"]
+[2.8384156227111816, 22.797096252441406, "Instrument Optimal Size Unknown"]
+[1.5996170043945312, -1.4452930688858032, "Satellite Bright Limit IC~4 or perhaps even brighter"]
+[-6.7314982414245605, 10.004655838012695, "Radiating Surface Height 10 to 20 km altitude"]
+[-1.3713114261627197, 7.015540599822998, "3D Model Diameter 3 km"]
+[-1.315253734588623, 7.004347801208496, "3D Model Base Diameter 3 km"]
+[-1.387890100479126, 6.991924285888672, "3D Model Top Diameter 15 km"]
+[-6.697263717651367, 9.963744163513184, "Radiating Surface Altitude ~90 km altitude"]
+[-8.503222465515137, 13.677818298339844, "Parameter Value 1.1 x 1012 photons/s/m3/sr at 762 nm"]
+[-8.48626708984375, 13.700437545776367, "Parameter Value ~9 x 10-7 W/m2 on the entrance pupil"]
+[3.13288950920105, -1.7338252067565918, "Satellite Manufacturer Astrium"]
+[3.1827170848846436, -1.7947453260421753, "Satellite Manufacturer ALAS"]
+[1.4258983135223389, -3.0682661533355713, "Satellites Launch Vehicle PSLV (Polar Satellite Launch Vehicle)"]
+[1.413144588470459, -3.1135332584381104, "Satellites Launch Site Satish Dhawan Space Centre (SDSC) in India"]
+[-1.7004486322402954, 5.330887317657471, "Mission Operations Center Interface Coordinates the overall mission"]
+[-1.6946083307266235, 5.334247589111328, "Mission Operations Center Ground Stations Harwell, Weilheim, and Redu"]
+[14.229402542114258, 7.814843654632568, "Nanosatellite Launch Date May 17, 2012"]
+[14.46088981628418, 7.721195697784424, "Nanosatellite Launch Vehicle H-IIA of Japan"]
+[14.50492000579834, 7.7222771644592285, "Nanosatellite Launch Site TNSC (Tanegashima Space Center), Japan"]
+[14.662640571594238, 7.811679840087891, "Nanosatellite Mass 7.1 kg"]
+[0.9899618625640869, -4.405855655670166, "Satellite Mass ~1990 kg"]
+[0.9900797009468079, -4.397286891937256, "Satellite Mass 970 kg"]
+[1.0106960535049438, -4.3664164543151855, "Satellite Mass ~48 kg"]
+[-7.485802173614502, 5.964463710784912, "Camera Electronics Unit Communication Interface MIL-STD-1553B"]
+[-5.2846221923828125, 2.894807815551758, "Korsch-Type Telescope Optical Elements 5 mirrors, the FPA (Focal Plane Assembly) with 1 panchromatic and 4 multispectral bands, and two Star Trackers"]
+[-5.281083106994629, 2.8951470851898193, "High Stability Telescope Structure Manufacturer EADS Astrium"]
+[-6.660701751708984, 9.985013961791992, "Antenna Tracking Method Closed-loop tracking"]
+[1.9170104265213013, 8.61892032623291, "Subsystem Tracking Systems Mono-pulse and gyro-tracking systems"]
+[1.8928840160369873, 8.603848457336426, "Subsystem Properties Quick and precise error determination"]
+[1.8225774765014648, 22.15165901184082, "Instrument Area 900 cm2"]
+[1.8510221242904663, 22.757808685302734, "Instrument Energy Range 20 keV - 10 MeV"]
+[2.3091371059417725, 22.74755096435547, "Instrument Time Tagging Accuracy About one microsecond"]
+[1.8559632301330566, 22.21055793762207, "Instrument Sensor Area 300 cm2"]
+[2.115751266479492, 22.23720932006836, "Instrument Sensor Angle About 40\u00b0"]
+[2.1545708179473877, 22.638521194458008, "Instrument Count Rate 104 \u2013 105 cm-2 s-1"]
+[2.4469308853149414, 22.632234573364258, "Instrument Dead Time < 300 ns"]
+[2.45037841796875, 22.51711082458496, "Instrument Datation Triggers 300 ns relative time accuracy"]
+[2.1727700233459473, 22.570772171020508, "Instrument TGF Events 1 \u00b5s relative time accuracy"]
+[-3.265652894973755, 5.427210330963135, "Launch Vehicle Inclination 98.6\u00ba"]
+[0.6851863265037537, -2.3285858631134033, "Satellite Inclination 98.3\u00ba"]
+[0.7310401797294617, -1.165388584136963, "Satellite Altitude 393 km"]
+[1.5142139196395874, 5.423159122467041, "Satellite Bus Payload Mass 35 kg"]
+[1.5050225257873535, 5.420050621032715, "Satellite Bus Payload Volume 46 cm x 46 cm x 25 cm"]
+[1.5124536752700806, 5.421821117401123, "Satellite Bus Payload Power 32 W"]
+[1.5111767053604126, 5.426572322845459, "Satellite Bus ACS Pointing Accuracy \u00b12 arcsec"]
+[1.5138649940490723, 5.420196056365967, "Satellite Bus ACS Jitter \u00b10.125 arcsec/s"]
+[1.5156751871109009, 5.419299602508545, "Satellite Bus Downlink Frequency X-band"]
+[1.5184955596923828, 5.42147970199585, "Satellite Bus Downlink Data Rate 150 Mbit/s"]
+[6.34160852432251, 7.3971052169799805, "Satellite Component Preload Force at South Pole About 140000 N"]
+[6.318526744842529, 7.415398597717285, "Satellite Component Pressure Exerted by the Pushing Spring About 2500 N"]
+[6.336097240447998, 7.402895927429199, "Satellite Component Spring Force Slightly below the weight of the satellite"]
+[0.0976317748427391, 7.176337718963623, "Experiment Package Mission Objectives 1) Determine VLF injection efficiency from a space-based antenna. 2) Map VLF fields from geophysical and man-made sources 3) Measure precipitating particles scattered by VLF from geophysical, ground-based transmitter, and DSX VLF transmitter sources"]
+[-4.933408737182617, 9.761663436889648, "Broadband Receiver Unknown Unknown"]
+[-4.755733489990234, 9.281838417053223, "Transmitter and Tuning Units Unknown Unknown"]
+[-4.71116828918457, 9.259871482849121, "Transmitter Control Unit Unknown Unknown"]
+[-4.936694145202637, 9.772942543029785, "Narrowband Receiver Unknown Unknown"]
+[-0.46456730365753174, 5.86182975769043, "Tri-Axial Search Coil Unknown Unknown"]
+[-4.483313083648682, 12.083239555358887, "Vector Magnetometer Unknown Unknown"]
+[-0.7557660341262817, 7.408418655395508, "Experiment Computer System Unknown Unknown"]
+[-2.657428741455078, 11.677330017089844, "Loss Cone Imager Unknown Unknown"]
+[-6.628961086273193, 10.091584205627441, "Antenna Unknown Unknown"]
+[-6.629210472106934, 9.935128211975098, "Antenna Unknown Unknown"]
+[4.697611331939697, -2.5965826511383057, "Satellite Operation Duration 2 years"]
+[1.657425880432129, -1.7732274532318115, "Satellite Sky Coverage 85 percent"]
+[4.446595668792725, -2.7051243782043457, "Satellite Sector Monitoring Duration 27 days"]
+[4.462210178375244, -2.700587511062622, "Satellite Southern Sky Study Duration First year of operations"]
+[4.5572896003723145, -2.6941471099853516, "Satellite Northern Sky Study Duration Second year of operations"]
+[-1.894888162612915, 14.853639602661133, "Radiometer Spatial Resolution 1 km"]
+[-1.910197377204895, 14.872601509094238, "Radiometer Number of Channels 6"]
+[-2.6361031532287598, 11.714780807495117, "Imager Spatial Resolution 50 m and 100 m"]
+[-1.8549898862838745, 14.890209197998047, "Radiometer Spectral Range 10.6-183 GHz"]
+[-0.8312771916389465, 16.42250633239746, "Fourier Transform Spectrometer Spectral Range 5-15 \u00b5m"]
+[-4.494915962219238, 15.905957221984863, "Radar Spatial Resolution 500 m and 1000 m"]
+[2.7059292793273926, -1.8073488473892212, "Satellite Primary Payload Yes"]
+[1.9989081621170044, -1.736088514328003, "Satellite Orbit Tracking Method Laser"]
+[2.9651741981506348, -1.4368526935577393, "Satellite Mission Objective Look for subtle distortions in spacetime caused by Earth's own mass"]
+[-1.400193452835083, 12.513815879821777, "Arcing Mitigation Method Coverage Entire TJ array"]
+[-1.4020705223083496, 12.640196800231934, "Arcing Mitigation Method Thermal Cycle Test -100 to +70\u00baC, 15 cycles, N2 atmosphere"]
+[2.379091501235962, -1.9955445528030396, "Satellite Modular Architecture Optimal solution"]
+[2.624577760696411, -1.844967007637024, "Satellite MAIT Phase Parallel and independent for Payload and Service modules"]
+[1.9346487522125244, -1.899036169052124, "Satellite Thermal Isolation Maximum"]
+[2.5052378177642822, -1.894153356552124, "Satellite Components Optical Bench Assembly (OBA), Payload Thermal shield, Payload Electronics panel, Central Module - Structure and Propulsion, Avionics and Electronics panels, Sunshield (SS) and Solar Array"]
+[0.2667218744754791, 4.621582984924316, "Natural Disaster Wind Speed 150 miles (240 kilometers) per hour"]
+[0.18977594375610352, 4.635599613189697, "Natural Disaster Storm Surge 9 to 15 feet (3 to 5 meters)"]
+[0.2670324444770813, 4.600621223449707, "Natural Disaster Rainfall 5 to 10 inches"]
+[0.28451570868492126, 4.5915846824646, "Natural Disaster Landfall Central America, same part of Nicaragua"]
+[0.28938743472099304, 4.590019226074219, "Natural Disaster Intensification Stalled and rapidly intensified"]
+[-3.481173515319824, 6.821208953857422, "Data Purpose Deformation forecast/monitoring"]
+[-3.4827067852020264, 6.805761337280273, "Data Purpose Evaluation of irrigated rice"]
+[-3.5075340270996094, 6.822968006134033, "Data Purpose Detecting oil and mineral resources in the ground and seabed"]
+[-3.478235960006714, 6.8012003898620605, "Data Purpose Identify carbon sinks"]
+[-0.06612066179513931, 13.6965913772583, "Measurement Instrument Date of Measurement February 21"]
+[0.45590847730636597, 4.522635459899902, "Natural Phenomenon Measurement 2.69 million km2 (1.04 million square miles)"]
+[-0.8852357864379883, 7.226663112640381, "Animal Behavior Struggling to complete essential tasks because of declining concentrations of Arctic sea ice"]
+[0.742143988609314, 11.963716506958008, "Sensor Status Operational"]
+[3.738234043121338, 17.715553283691406, "Payload TLEs Recorded 31,369"]
+[3.822350263595581, 17.606271743774414, "Payload Elves 73.65%"]
+[3.75520920753479, 17.698524475097656, "Payload Red Sprites 6.53%"]
+[3.7382702827453613, 17.719982147216797, "Payload Halos 6.00%"]
+[3.736346483230591, 17.69195556640625, "Payload Blue Jets 13.51%"]
+[3.736067056655884, 17.712989807128906, "Payload Gigantic Jets 0.30%"]
+[1.6637804508209229, 6.971677780151367, "Communication Device Frequency X-band"]
+[-0.24319347739219666, 9.254251480102539, "Navigation Signal Detector Signal Type ADS-B (Automatic Dependent Surveillance\u2013Broadcast)"]
+[1.7336273193359375, 6.9118733406066895, "Communication Device Passes per Day 5.0"]
+[1.6960909366607666, 6.95169734954834, "Communication Device Average Pass Length 7.4 minutes"]
+[-2.6967921257019043, 4.581060409545898, "Spacecraft Platform Launch Mass 1387 kg"]
+[-2.71946382522583, 4.578217029571533, "Spacecraft Platform Power 1.2 kW"]
+[-2.7389161586761475, 4.5377421379089355, "Spacecraft Platform Stabilization 3-axis, zero momentum bias, nadir pointing"]
+[-2.6828439235687256, 4.584439277648926, "Spacecraft Platform Pointing Control 13.3 arcsec (3\u03c3)"]
+[-2.6971240043640137, 4.579884052276611, "Spacecraft Platform Data Storage Capacity 704 Gbit at EOL"]
+[-2.747769355773926, 4.530604362487793, "Spacecraft Platform Data Downlink X-band, data rate of 220 Mbit/s"]
+[-2.731863260269165, 4.563076496124268, "Spacecraft Platform Propulsion Blowdown hydrazine, four 22 N thrusters and eight 4.5 N thrusters, 158 kg tank capacity"]
+[-2.7627532482147217, 4.550682067871094, "Spacecraft Platform Mission Design Life 3 years with a 5 year goal; 7 years of propellant available"]
+[2.781888246536255, 22.374008178710938, "Instrument Location of Construction NASA's Goddard Space Flight Center in Greenbelt, Maryland"]
+[2.4988694190979004, 22.753135681152344, "Instrument Data Downlink X-band, data rate of 220 Mbit/s"]
+[-0.11243554949760437, 13.587023735046387, "Measurement Device Grid Dimensions 7 mm x 19 mm"]
+[-0.09899022430181503, 13.60722541809082, "Measurement Device Grid Weight Less than 1 mg"]
+[-0.09523506462574005, 13.591961860656738, "Measurement Device Electrode Position 4 mm to each side of the screen"]
+[0.13200829923152924, 7.249098300933838, "Sample Cell Xenon Critical Temperature Tc=16.6\u00baC"]
+[0.12860187888145447, 7.248654842376709, "Sample Cell Xenon Critical Density 1.1 times that of water"]
+[0.17019079625606537, 7.278592586517334, "Sample Cell Xenon Pressure 58 atmospheres"]
+[-2.695993423461914, 9.442936897277832, "Power Generation Installation Requirement Two spacewalks"]
+[-2.7048580646514893, 9.436431884765625, "Power Generation Quantity 6"]
+[-2.728635311126709, 9.414178848266602, "Power Generation Installation Location On top of the existing solar panels"]
+[14.56692123413086, 7.63336706161499, "Nanosatellite Mission Goal Contributing to the local educational program for elementary and junior high school students"]
+[14.485350608825684, 7.725582122802734, "Nanosatellite Risk Electrostatic discharge"]
+[14.482719421386719, 7.691366195678711, "Nanosatellite Communication Ground communications and the distribution of Earth surface imagery"]
+[5.353245735168457, -4.501681804656982, "Satellite Launch Date November 20, 2013"]
+[-3.2487850189208984, 5.421229839324951, "Launch Vehicle Manufacturer Orbital Sciences Corporation"]
+[3.710155963897705, 17.73016357421875, "Payload Function Uses launch vehicle orbital targeting and range safety planning processes to protect public safety from an errant launch vehicle during flight"]
+[11.368882179260254, 5.482836723327637, "Deep Space CubeSat Presentation Date March 21-25, 2016"]
+[7.284644603729248, 12.420608520507812, "Satellite Instrument Purpose Characterisation of clouds and aerosols and their microphysical and radiative properties"]
+[7.32488489151001, 12.451667785644531, "Satellite Instrument Operator Unknown"]
+[-4.2035722732543945, 7.364831924438477, "Data Handling and Communications Source Data Rate Up to 960 Mbit/s"]
+[-3.62125301361084, 7.84192419052124, "Data Recording Device Capacity 192 Gbit"]
+[-5.180521011352539, 7.782041072845459, "Communication System Data Rate 61 Mbit/s to regional data centers, and up to 350 Mbit/s to the central data center"]
+[5.272916793823242, -4.47452974319458, "Satellite Launch Date June 27, 2013"]
+[4.355513095855713, -3.3305561542510986, "Satellite Launch Time 16:53 UTC"]
+[4.677079200744629, -2.581542491912842, "Satellite Primary Mission Duration Two years"]
+[2.044025421142578, -2.802919626235962, "Satellite Number of Oscillating Red Giant Stars 158,000"]
+[2.0530593395233154, -2.716762065887451, "Satellite Number of Pulsating Giants Identified 158,505"]
+[-0.6392223834991455, 3.1960158348083496, "Stars Number of Exoplanets Four"]
+[-2.9662134647369385, 20.174863815307617, "Spectral Band Channel Band (\u00b5m) 0.45-0.49"]
+[-2.848367929458618, 20.12143325805664, "Spectral Band Spatial resolution (km) 1"]
+[-2.981642484664917, 20.195024490356445, "Spectral Band Sensitivity S/N \u2265 90"]
+[-2.9403250217437744, 20.165576934814453, "Spectral Band Channel Band (\u00b5m) 3.5-4.0 (high)"]
+[-2.9659032821655273, 20.167640686035156, "Spectral Band Sensitivity NEDT \u2264 0.7 K"]
+[-2.9494707584381104, 20.184410095214844, "Spectral Band Channel Band (\u00b5m) 8.0-9.0"]
+[-3.052042007446289, 20.173566818237305, "Spectral Band Sensitivity NEDT \u2264 0.2 K"]
+[1.8915163278579712, -1.1851128339767456, "Satellite Measurement CO2 and methane"]
+[1.2172876596450806, -0.9109547138214111, "Satellite Measurement Area 10 km diameter"]
+[0.8693976998329163, -1.4160404205322266, "Satellite Separation About 150 km"]
+[1.80982506275177, 22.14093017578125, "Instrument Observation Resolution 49 km2"]
+[1.7939659357070923, -1.4901167154312134, "Satellite Data Sharing Resolution 50 m2"]
+[1.6735174655914307, -1.376784324645996, "Satellite Data Sharing Resolution 1 km"]
+[-1.1235271692276, 4.47873592376709, "Ground Station Distress Localization Accuracy Unprecedented"]
+[-1.1476649045944214, 4.45997953414917, "Ground Station Response Time Unprecedented"]
+[-2.009079694747925, 8.090677261352539, "Service Function Relays Return Link Messages from the RLSP to new generation beacons through the Galileo navigation signal"]
+[-5.27982759475708, 7.482802867889404, "Protocol Protocol ID 238"]
+[-5.280955791473389, 7.525019645690918, "Protocol Requirements Utilize the SpaceWire capabilities to provide a packet delivery protocol that is able to detect and recover lost packets"]
+[-5.252567768096924, 7.528696537017822, "Protocol Requirements Be flexible so that it can be adapted as needed to different host data throughput requirements and resources"]
+[-3.2025740146636963, 1.7432070970535278, "Satellite Mission Date November 20-21, 2014"]
+[-3.1544313430786133, 1.6877849102020264, "Satellite Mission Location Qu\u00e9bec, Canada"]
+[-3.223362684249878, 1.721617579460144, "Satellite Mission Date July 13-18, 2014"]
+[2.6301474571228027, -1.9967695474624634, "Satellite Pointing Performance Unknown"]
+[5.1212053298950195, -4.5143232345581055, "Satellite Conference Presentation Date 1-5 October 2018"]
+[2.5791358947753906, -3.9303886890411377, "Satellite URL https://iafastro.directory/iac/proceedings/IAC-18/IAC-18/A7/3/manuscripts/IAC-18,A7,3,5,x42024.pdf"]
+[-13.891324996948242, -2.2202372550964355, "X-ray Telescope Science Goals Locate massive black holes, Study the population of compact objects in the Galaxy, Understand explosion dynamics and nucleosynthesis in core collapse and Type Ia SNe, Constrain particle acceleration in relativistic jets in supermassive black holes"]
+[-13.893424987792969, -2.2201602458953857, "X-ray Telescope Effective Area Function of off-axis angle, as a fraction of on-axis area, for several energies"]
+[-1.6070148944854736, 9.677885055541992, "Propulsion System Propellant Sulfur hexafluoride (SF6)"]
+[-1.6434791088104248, 9.720900535583496, "Propulsion System Total Mass < 0.5 kg"]
+[-1.604892611503601, 9.67821216583252, "Propulsion System Thrust Level 50-100 mN"]
+[-1.604455590248108, 9.675954818725586, "Propulsion System Specific Impulse 500-1000 m/s"]
+[-1.6132943630218506, 9.669310569763184, "Propulsion System Total Delta V > 35 m/s"]
+[-2.649467706680298, 11.689377784729004, "Imagers Device Type CMOS/APS"]
+[5.107037544250488, -4.562859058380127, "Satellite Acceptance Date August 19, 2014"]
+[5.327005386352539, -4.469399929046631, "Satellite Launch Date April 3, 2014"]
+[5.160252094268799, -4.39847469329834, "Satellite Operational Date March 2010"]
+[-0.9542977809906006, -9.998710632324219, "Satellite Constellation Number of Primary Operational Satellites 2 (F-16, and F-17)"]
+[-0.9559177756309509, -10.000418663024902, "Satellite Constellation Number of Partially Operational Satellites 3 (F-13, F-15)"]
+[-3.351655960083008, 8.531511306762695, "Memory Technology Technology Type SLC NAND-Flash"]
+[-3.359997510910034, 8.545805931091309, "Memory Technology Technology Type SDR-SDRAM"]
+[2.627101182937622, -2.2353806495666504, "Satellite Launch Vehicle Sentinel 2 satellite"]
+[-3.3516507148742676, 8.49418830871582, "Memory Technology Launch Date Unknown"]
+[-13.828722953796387, -2.203176498413086, "X-ray Telescope Observation Capability Peered inside dense doughnuts surrounding supermassive black holes"]
+[-1.2309579849243164, 3.1374239921569824, "Cosmic Structure Shape Clumpy"]
+[-1.27721107006073, 3.140962839126587, "Cosmic Structure Orientation Effect Blocks black hole if viewed edge-on, allows detection if viewed face-on"]
+[11.221651077270508, 5.47725772857666, "CubeSat OBC Manufacturer GomSpace"]
+[-5.882007598876953, 9.425775527954102, "UHF radio Manufacturer GomSpace"]
+[11.341715812683105, 5.566768169403076, "CubeSat Bus Type Power System"]
+[11.170413970947266, 5.391718864440918, "CubeSat Bus Type Battery Pack"]
+[1.2029882669448853, -0.8353298306465149, "Satellite Size 3U"]
+[-1.4290971755981445, 13.369722366333008, "Solar Cells Type Body-mounted"]
+[7.333443641662598, 12.465845108032227, "Satellite Instrument Manufacturer ITT Industries"]
+[7.297645568847656, 12.424601554870605, "Satellite Instrument Development Location Fort Wayne, IN"]
+[7.446902751922607, 12.577539443969727, "Satellite Instrument Development Date Sept. 2004"]
+[7.293551445007324, 12.432439804077148, "Satellite Instrument Manufacturer ITT Exelis"]
+[-0.08684829622507095, 15.520228385925293, "Spectrometer Energy Range 0.3-30 keV"]
+[-0.05485791340470314, 15.52257251739502, "Spectrometer Field of View 90\u00ba"]
+[-0.1280619502067566, 15.549707412719727, "Spectrometer Manufacturer Amptek Inc."]
+[-0.04853346571326256, 15.523483276367188, "Spectrometer First Flight DMSP F16, launch Oct. 18, 2003"]
+[-0.11037988215684891, 15.480921745300293, "Spectrometer Instrument Type Electrostatic analyzer detector"]
+[-1.3935154676437378, 1.1592966318130493, "Data Relay Satellite System Orbit Geostationary"]
+[1.8969523906707764, -2.065265655517578, "Satellite Orbit Low"]
+[-1.4075881242752075, 1.1689077615737915, "Data Relay Satellite System Orbit Geostationary"]
+[-1.3793607950210571, 1.1151665449142456, "Data Relay Satellite System Orbit Altitude 35,800 km"]
+[-1.7497507333755493, 8.82997989654541, "Control System Function Control the position or speed loops"]
+[-7.433060169219971, 6.020556449890137, "Camera Electronics Box Function Operate the CCD, digitize the image data and transfer it to the CCM"]
+[-2.7745745182037354, 7.468691825866699, "Field-Programmable Gate Array Function Receive commands from the CCM, generate all the clocks necessary for driving the CCD and drive the DACs responsible for providing the bias voltages"]
+[0.6580153703689575, -2.219221830368042, "Satellite Temperature Range -67\u00ba Fahrenheit to 188\u00ba Fahrenheit"]
+[2.7491185665130615, 23.48883819580078, "Instrument Issue Cooling system malfunction"]
+[2.7815048694610596, 22.563405990600586, "Instrument Problem Foreign object debris blocking the flow of the coolant"]
+[2.829050064086914, 22.229297637939453, "Instrument Design Change Eliminates the filters that are susceptible to debris"]
+[-2.5875284671783447, 9.676054954528809, "Energy Source Mounting Modified mirror mount"]
+[-3.70127534866333, 8.363092422485352, "Energy Storage Nominal Voltage 4.2 V"]
+[-3.6950690746307373, 8.327933311462402, "Energy Storage Capacity per Cell 1.5 Ah"]
+[-0.3403110206127167, 8.162952423095703, "Material Application Fabricating solar concentrator lenses"]
+[1.6737186908721924, 21.967967987060547, "Instrument Swath Width 3000 km"]
+[1.8359277248382568, 22.039318084716797, "Instrument Orbit Altitude 833 km"]
+[1.9147374629974365, 22.182985305786133, "Instrument Linear Resolution 0.56 km"]
+[2.294393301010132, 14.022992134094238, "VIS Wavelength 0.4 - 1.1 \u00b5m"]
+[2.2089736461639404, 13.8721342086792, "VIS Dynamic Range Approximately 107"]
+[-2.676316976547241, 11.729604721069336, "TIR Wavelength 10.0 - 13.4 \u00b5m"]
+[-2.668609857559204, 11.674391746520996, "TIR Resolution 0.56 km"]
+[-2.7470476627349854, 11.787957191467285, "TIR Ground Resolution 5.4 km"]
+[2.0394654273986816, 22.517494201660156, "Instrument Sensitivity 0.47 - 0.95 \u00b5m"]
+[2.792100429534912, 22.362682342529297, "Instrument Provides Visible Imagery (0.5 - 0.85 \u00b5m) at night"]
+[0.4505021572113037, 12.132466316223145, "Sensor X-Ray Sensor (XRS) Measures soft X-rays"]
+[0.4855327606201172, 12.223356246948242, "Sensor Extreme Ultraviolet Sensors (EUVS) Measure extreme ultraviolet light"]
+[2.2140145301818848, -1.2062294483184814, "Satellite Advanced Baseline Imager (ABI) Captured stunning views of Earth"]
+[0.6563687324523926, -2.2630536556243896, "Satellite Inside Temperature Range 0 to 18\u00baC"]
+[0.6877750754356384, -2.2255196571350098, "Satellite Battery Temperature Range 10 to 12\u00baC"]
+[2.073725938796997, -0.6136584877967834, "Satellite Power Generation Test 300 V"]
+[-1.1094822883605957, 3.0461275577545166, "Celestial Body Quantity 5000+"]
+[-1.1495463848114014, 3.058410167694092, "Celestial Body Types Small, rocky worlds like Earth, gas giants many times larger than Jupiter, hot Jupiters, super-Earths, mini-Neptunes, planets orbiting two stars at once, planets orbiting the collapsed remnants of dead stars"]
+[-0.8106133937835693, 12.751275062561035, "Radiation Measurement Device Measurement Methods Proton fluence through displacement damage effects, ionizing current"]
+[-0.8369162082672119, 12.582535743713379, "Radiation Sensor Shielding Material Aluminum foils of different thicknesses"]
+[-0.7933578491210938, 12.528432846069336, "Radiation Sensor Minimum Proton Energy Detection Different for each floor"]
+[-0.8734130859375, 12.320369720458984, "Radiation Detector Proton Energy Detection Range Above 75 MeV"]
+[-0.864310085773468, 12.375385284423828, "Radiation Detector Flux Variations Can also be obtained"]
+[-13.722704887390137, -2.307480812072754, "X-ray Telescope Survey Completion Date 11 June 2020"]
+[-13.670848846435547, -2.315624475479126, "X-ray Telescope Launch Date 13 July 2019"]
+[-13.955205917358398, -2.290189743041992, "X-ray Telescope Orbit Second Lagrange point of the Earth-Sun-system"]
+[-13.972219467163086, -2.2290563583374023, "X-ray Telescope Mode Continuous scanning"]
+[2.868210792541504, 22.464393615722656, "Instruments Operation MWIR and Lasercom"]
+[1.7138166427612305, 6.926295280456543, "Communication Device Data Downlink Via Lasercom"]
+[-3.503814935684204, 6.828890323638916, "Data Collection Selected wavelength bands at low and high altitudes"]
+[-0.8674366474151611, 11.631270408630371, "Detector First Event 20 GeV electron"]
+[-0.8519578576087952, 11.610452651977539, "Detector Second Event 42 GeV Carbon nucleus"]
+[-0.8245954513549805, 11.619253158569336, "Detector Cosmic-Ray Hits ~10,000 hits per minute"]
+[0.9873319268226624, -4.388988018035889, "Satellite Total Mass Approximately 80 kg"]
+[1.1706228256225586, -0.776744544506073, "Satellite Dimensions 0.524 m x 0.524 m x 0.62 m"]
+[1.2156273126602173, -0.9952781200408936, "Satellite Solar Panel Length 1.2 m"]
+[1.6466385126113892, 7.010092258453369, "Communication Device Quantity 2"]
+[1.7370202541351318, 6.913896560668945, "Communication Device Attachment Location +Z face of the spacecraft and one on the -Z face"]
+[-0.9432656168937683, 6.420025825500488, "Author Documentation Observation of the Earth and Its Environment: Survey of Missions and Sensors"]
+[-0.8647616505622864, 6.1004743576049805, "Website Contact Email eoportal@symbios.space"]
+[-0.9798879027366638, 6.237401962280273, "Copyright Year 2024"]
+[-7.564865589141846, 5.889858245849609, "Digital Camera Model Nikon D3S"]
+[-2.137835741043091, 4.3138556480407715, "Space Station Location Iberian Peninsula"]
+[2.4571821689605713, 22.609514236450195, "Instrument Communication Capability Communicate with the spacecraft, even when it is out of visibility from ground antenna"]
+[-1.0698124170303345, 7.750633239746094, "Device Function Provide secondary voltage to the various instruments"]
+[-1.0073055028915405, 7.755217552185059, "Device Function Format and date data, both scientific and housekeeping in X-band"]
+[-1.0299237966537476, 7.750579357147217, "Device Function Format and date housekeeping data in S-band"]
+[-1.0174857378005981, 7.715586185455322, "Device Function Manage the transfer of data to the mass storage"]
+[-1.0835857391357422, 7.755023956298828, "Device Function Serve as a host structure for instrumentation analyzers"]
+[-1.0743465423583984, 7.752284526824951, "Device Function Make in-flight modifications to analyzer software"]
+[-1.066078543663025, 7.748380661010742, "Device Function Make in-flight modifications to the MEXIC software"]
+[-0.11480005085468292, 9.202041625976562, "Guidance, Navigation and Control Design Coping with nominal and failure scenarios"]
+[-1.9356976747512817, 8.11217975616455, "System Objective Provide the appropriate references to ensure that the S/C follow the nominal trajectory profile for the RVX"]
+[-1.9127551317214966, 8.117620468139648, "System Inputs Navigation and Mode Manager"]
+[-1.9274673461914062, 8.084431648254395, "System Outputs Control"]
+[-0.05537959560751915, 15.510570526123047, "Spectrometer Mass 2.5 kg"]
+[-0.15320169925689697, 15.516532897949219, "Spectrometer Power Consumption 10-15 W"]
+[-0.14420339465141296, 15.569791793823242, "Spectrometer Spectral Resolution 10 nm"]
+[-0.10855845361948013, 15.53402042388916, "Spectrometer Signal-to-Noise Ratio >400"]
+[-0.06799352169036865, 15.53307056427002, "Spectrometer Wavelength Range 1 to 4 \u00b5m"]
+[-0.19102297723293304, 15.553694725036621, "Spectrometer Iris Adjustable 4-sided"]
+[-0.1450812965631485, 15.477436065673828, "Spectrometer Spot Size Maintains the same spot size regardless of variations in altitude (by up to a factor of 5) or to vary spot size at a given altitude"]
+[-0.1115652546286583, 15.518136024475098, "Spectrometer Mode Imager"]
+[3.2256834506988525, 2.375777006149292, "Satellite Subsystem Factors Considered Electrical requirements, interfaces, physical size, location feasibility, look angle, FOV requirements, thermal requirements, mechanical loads, transmissibility factors, physical parameters, balancing, ease of assembly/dis-assembly, accessibility"]
+[3.225145101547241, 2.3786916732788086, "Satellite Subsystem Location Equipment decks/panels"]
+[16.996341705322266, 6.719257354736328, "Microsatellite Launch Date 31 December 2023"]
+[17.025527954101562, 6.696341037750244, "Microsatellite End of Life Date 31 December 2028"]
+[16.882253646850586, 6.836317539215088, "Microsatellite Measurement Domain Land"]
+[16.86314582824707, 6.853976726531982, "Microsatellite Measurement Category Multi-purpose imagery (land), Vegetation"]
+[16.91253089904785, 6.802731037139893, "Microsatellite Mission Type EO"]
+[16.90690803527832, 6.817146301269531, "Microsatellite Technology Demonstration Mission Hyperspectral imaging, experimental high-rate optical (laser) data transmissions"]
+[-5.6888628005981445, 9.328343391418457, "Radio Operating Band UHF band at 400.5 MHz"]
+[-5.768101692199707, 9.336461067199707, "Radio Protocol AX.25"]
+[-6.769935607910156, 10.022918701171875, "Antenna Dimensions 10 x 30 cm"]
+[5.274958610534668, -4.335618495941162, "Satellite Launch Date 27 September 2021"]
+[4.384579658508301, -3.342507839202881, "Satellite Launch Time 18:12 UTC"]
+[-8.102416038513184, 8.827449798583984, "Power Subsystem Device Function Track the solar panels to obtain the maximum power operative condition"]
+[-8.093609809875488, 8.825520515441895, "Power Subsystem Device Type Step-up DC/DC converter"]
+[-2.5463974475860596, 9.346663475036621, "Power Generation System Number of Cells 14"]
+[-2.597930669784546, 9.382974624633789, "Power Generation System Nominal Open Circuit Voltage 7.6 V"]
+[-0.11078985035419464, 13.587417602539062, "Measurement Device Manufacturer Honeywell"]
+[-0.09859452396631241, 13.583231925964355, "Measurement Device Model HM2003"]
+[-0.08775525540113449, 13.577333450317383, "Measurement Device Function Measure the Earth's magnetic field (strength and direction)"]
+[0.9874902963638306, 0.7985474467277527, "Earth Observation Satellite Orbital Altitude 167.4 km"]
+[3.6949338912963867, 22.960662841796875, "Instrument Integration Date May 23, 2017"]
+[3.6965301036834717, 22.967247009277344, "Instrument Installation Date May 17, 2017"]
+[-0.7801671624183655, 8.233261108398438, "Box Structure Arrival Date May 2014"]
+[5.039096355438232, -4.465648174285889, "Satellite Mission Critical Design Review Date February 18, 2014"]
+[5.057799816131592, -4.401089668273926, "Satellite Instrument CDR Date January 17, 2014"]
+[5.004316806793213, -4.472644805908203, "Satellite Ground Systems CDR Date Sept. 6, 2013"]
+[5.0981011390686035, -4.406525135040283, "Satellite Phase C Status Date December 17, 2012"]
+[5.050272464752197, -4.457400798797607, "Satellite Instrument PDR Date Nov. 18, 2011"]
+[5.168251991271973, -4.506375789642334, "Satellite SRR Date May 25, 2011"]
+[5.2503662109375, -4.460525989532471, "Satellite ISRE Date December 1, 2010"]
+[5.1338958740234375, -4.476341247558594, "Satellite KDP-A Review Date December 11, 2009"]
+[2.251732349395752, -2.2963812351226807, "Satellite Propulsion None"]
+[2.272069215774536, -2.2068140506744385, "Satellite GPS Unit None"]
+[2.2269277572631836, -2.113593816757202, "Satellite Star Trackers None"]
+[2.4898793697357178, -2.134878635406494, "Satellite IMU Present"]
+[2.1030871868133545, -2.556051015853882, "Satellite Sun Sensors 3"]
+[2.394402265548706, -1.6669167280197144, "Satellite Magnetometer Present"]
+[1.4844239950180054, -2.29333233833313, "Satellite ADCS 3-axis stabilized"]
+[-0.9317404627799988, -10.01911735534668, "Satellite Constellation Mission Status Operational (nominal)"]
+[-0.9452267289161682, -10.004990577697754, "Satellite Constellation Mission Type EO"]
+[-0.9364030361175537, -9.985742568969727, "Satellite Constellation Agency NASA, NOAA"]
+[-0.9432777762413025, -9.991070747375488, "Satellite Constellation Purpose Space-based monitoring of air quality, greenhouse gases, the ozone layer and natural climate drivers like solar energy"]
+[-1.3661023378372192, 6.911253452301025, "Model Data Source Satellite, aircraft, and ground-based observing systems"]
+[-0.9315612316131592, 8.663677215576172, "Fire Burned Area More than 137,000 acres"]
+[-1.0315250158309937, 8.60793685913086, "Fire Burned Area More than 130,000 acres"]
+[-2.8897926807403564, 20.150510787963867, "Spectral Band Resolution 0.29 m"]
+[-2.823256731033325, 20.09741973876953, "Spectral Bands Resolution 1.16 m"]
+[-0.9467616081237793, -10.008940696716309, "Satellite Constellation Swath Width 9km"]
+[-0.8987168669700623, -10.053895950317383, "Satellite Constellation Altitude 450 km"]
+[-0.946823239326477, -10.016923904418945, "Satellite Constellation Daily Imaging Capacity 5 million km2"]
+[4.226474761962891, -2.8328301906585693, "Satellite Antenna Pointing Interruption No more than 16 hours"]
+[4.158726215362549, -2.7632346153259277, "Satellite Ka-band Science Data Downlink Period 4 hr"]
+[1.1941940784454346, -1.0282807350158691, "Satellite Angular Momentum Build-up ~1.5 N m"]
+[2.2618813514709473, -2.3438563346862793, "Satellite Thrusters Hydrazine"]
+[3.046863317489624, -2.0633578300476074, "Satellite Development Status Arrived in Florida"]
+[-2.400509834289551, 9.209022521972656, "Power System Purpose Improve the performance of the onboard power generation system"]
+[-2.3432984352111816, 9.187575340270996, "Power System PCB Layers 6"]
+[-2.330261468887329, 9.134799003601074, "Power System PCB Volume 50 mm x 82,4 mm"]
+[-2.3637259006500244, 9.204187393188477, "Power System PCB Mass ~ 50 g"]
+[-2.347148895263672, 9.150824546813965, "Power System Electronics COTS (Commercial-of-the-Shelf) components"]
+[2.236466884613037, -1.5564565658569336, "Satellite Radar Altimeter Device"]
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+[-2.2762537002563477, 7.429067611694336, "On-Board Computer I/O Capabilities Provided"]
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+[-5.3996992111206055, 2.8209738731384277, "Telescope Maximum Field Distortion 3.84%"]
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+[0.934669554233551, -1.1242958307266235, "Satellite Bathymetry Measurement Depth 10 meters or more"]
+[5.092662811279297, -4.334606170654297, "Satellite Data Release Date May 2019"]
+[2.1883621215820312, -2.3972177505493164, "Satellite Users More than 350"]
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+[7.3044281005859375, 12.375998497009277, "Satellite Instrument Impact of 1 mrad Error Radiometric error of \u00b10.5 dB or less"]
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+[5.201909065246582, -4.363655090332031, "Satellite Launch Date December 2021"]
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+[-0.5848607420921326, 1.2539786100387573, "Orbit Determination Software Fast-delivery position knowledge \u00b1 60 m (3\u03c3 in each axis)"]
+[-0.5702775120735168, 1.2457174062728882, "Orbit Determination Software Post-processed position knowledge \u00b1 15 m (3\u03c3 in each axis)"]
+[-3.6853187084198, 8.044992446899414, "Solid-State Recorder Capacity 150 Gbit BOL"]
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+[-0.9123462438583374, -10.037595748901367, "Satellite Constellation Builder SSL"]
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+[-0.9126594662666321, 8.694276809692383, "Cooling System Operation Time 3 days out of 13 days"]
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+[-1.3066918849945068, 9.432059288024902, "N/A N/A N/A"]
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+[-2.41497802734375, 9.217495918273926, "Power Collection System Type Large"]
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+[-0.13821129500865936, 9.158349990844727, "Navigation Primary System GPS"]
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+[11.463239669799805, 5.6713738441467285, "CubeSat Size 3 standardised 10-cm boxes"]
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+[11.302604675292969, 5.492323398590088, "CubeSat Manufacturer University of Maribor in Slovenia with SkyLabs"]
+[11.272424697875977, 5.507229804992676, "CubeSat Components Solar panels from DHV, antennas and CubeSat deployer from ISISpace, satellite structure from RIEDL AeroSpace, main NANOsky platform from SkyLabs"]
+[-1.0145236253738403, 13.192486763000488, "Solar Spectral Irradiation Measurement Instrument Number of Configurations 13"]
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+[-1.0210247039794922, 13.189179420471191, "Solar Spectral Irradiation Measurement Instrument Uncertainty 0.42% for the range of 200-460 nm, 0.24% for the range of 460-2400nm"]
+[-0.9916151762008667, 13.119780540466309, "Total and Spectral solar Irradiance Sensor Mission Duration Five years"]
+[-1.003247857093811, 13.128778457641602, "Total and Spectral solar Irradiance Sensor Replacement Year 2023"]
+[-0.5231641530990601, 1.2091107368469238, "Satellite Orbit Perigee 108,000 km"]
+[-0.5292002558708191, 1.2316946983337402, "Satellite Orbit Apogee 373,000 km"]
+[-0.5250189900398254, 1.2329797744750977, "Satellite Orbit Inclination 28.5\u00ba"]
+[-0.5372850298881531, 1.2391592264175415, "Satellite Orbit Period 13.7 days"]
+[-0.5353574752807617, 1.241042137145996, "Satellite Orbit Total Ionizing Dose <1 krad"]
+[-1.0060981512069702, 7.770313739776611, "Device Operating Temperature Near -75\u00baC"]
+[-0.5527682900428772, 1.2575502395629883, "Satellite Orbit Temperature Variations <0.1\u00baC /hr for 90% of the orbit, and <2\u00baC/hr throughout the entire orbit"]
+[4.583101749420166, -2.6037068367004395, "Satellite Imaging Duration 1 year"]
+[2.092017650604248, -2.7286980152130127, "Satellite Number of Exoplanets Discovered 29"]
+[2.075334310531616, -2.7645697593688965, "Satellite Number of Candidate Planets More than 1,000"]
+[2.0483806133270264, -2.1406216621398926, "Satellite Sky Division 13 sectors"]
+[3.7900962829589844, -2.562580108642578, "Satellite Imaging Frequency Every 30 minutes"]
+[2.0969460010528564, -2.7619667053222656, "Satellite Number of Science Images Captured 15,347"]
+[2.503107786178589, -1.2174631357192993, "Satellite Data Returned More than 20 terabytes of southern sky data"]
+[-5.064141273498535, 2.8295857906341553, "Space Telescope Parameter Value"]
+[-0.797100841999054, 3.182457685470581, "Stellar System Distance from Earth 7,500 light-years"]
+[-0.7634719610214233, 3.1905603408813477, "Stellar System Mass of Stars 90 and 30 times the mass of our Sun"]
+[-0.7807128429412842, 3.1493587493896484, "Stellar System Closest Approach Distance 140 million miles (225 million kilometers)"]
+[-0.8137706518173218, 3.1638705730438232, "Stellar System Orbital Period 5.5 years"]
+[-2.9387495517730713, 4.3829851150512695, "Space Technology Purpose Detect marine plastic litter using satellites"]
+[-2.8880746364593506, 4.395674228668213, "Space Technology Application Water management, orbital tracking of water quality and pollution, spacecraft-grade recycling systems, identify marine plastic litter using satellites"]
+[-8.101885795593262, 8.822056770324707, "Power Subsystem Solar Cell Type Monocrystalline silicon"]
+[-8.109732627868652, 8.819482803344727, "Power Subsystem Nominal Efficiency 15%"]
+[-8.099020957946777, 8.828959465026855, "Power Subsystem Solar Cell Type Triple junction GaAs cells"]
+[-8.088974952697754, 8.794133186340332, "Power Subsystem Nominal Efficiency 21%"]
+[-8.103780746459961, 8.821093559265137, "Power Subsystem Array Configuration Two parallel arrays"]
+[6.2756428718566895, 7.450774669647217, "Satellite Component Quantity 192 quartz corner-cubes"]
+[6.354351997375488, 7.386819362640381, "Satellite Component Positional Accuracy Within 3 cm"]
+[-0.8643661737442017, 0.13239482045173645, "Satellite System Full Form Doppler Orbitography and Radiopositioning Integrated by Satellite"]
+[16.781963348388672, 6.8703413009643555, "Geomagnetic Research Microsatellite Mission Name \u00d8rsted"]
+[16.74867820739746, 6.896162986755371, "Geomagnetic Research Microsatellite Mission Developer NBI (Niels Bohr Institute) of the University of Copenhagen, the Technical University of Denmark (DTU), the Solar-Terrestrial Physics Division of DMI (Danish Meteorological Institute), the Danish Space Research Institute (DSRI) of Copenhagen, Terma A/S, and Computer Resources International (now part of Terma A/S)"]
+[16.73983383178711, 6.86060094833374, "Geomagnetic Research Microsatellite International Contributors NASA, CNES, DLR and ESA"]
+[16.77290916442871, 6.89597225189209, "Geomagnetic Research Microsatellite Name Origin Hans Christian \u00d8rsted"]
+[16.773000717163086, 6.896463394165039, "Geomagnetic Research Microsatellite Name Change DNSC (Danish National Space Center), DTU Space"]
+[16.76005744934082, 6.9103193283081055, "Geomagnetic Research Microsatellite Illustration Figure 1"]
+[2.921272039413452, 21.989177703857422, "Instrument Purpose Improve storm forecasts and warnings"]
+[-5.190764904022217, 7.768974304199219, "Communication System Uplink Data Rate 4 kbit/s"]
+[-5.200665473937988, 7.8255181312561035, "Communication System Downlink Data Rate 4 kbit/s"]
+[-5.180086612701416, 7.916883945465088, "Communication System Transmitter Power 30 dBm (1 W)"]
+[2.6655972003936768, 5.388125419616699, "Beacon Morse Code Rate 15 words/minute"]
+[1.899285912513733, 10.720852851867676, "Imaging Device Size Microwave oven"]
+[1.9111459255218506, 10.719014167785645, "Imaging Device Purpose Provide unprecedented imaging of the Earth\u2019s upper atmosphere"]
+[2.6655383110046387, 5.387664794921875, "Beacon Location Information Encoding GPS, Glonass or the future Galileo system"]
+[-9.970292091369629, 5.871492862701416, "Search and Rescue System Introduction Year 1992"]
+[-9.952666282653809, 5.857656002044678, "Search and Rescue System Adoption Year 2004"]
+[2.725454568862915, -2.607557773590088, "Satellite Data Collection Rate 1 Hz"]
+[-3.031811475753784, 7.239563941955566, "Processing Center Location ESA/ESTEC in Noordwijk, The Netherlands"]
+[2.265697479248047, -2.0007174015045166, "Ground Satellite Centre Location Guildford (UK)"]
+[3.444959878921509, 13.443769454956055, "Laser Communication Terminal Advantages Higher data rate, larger link distance, lower size, weight and power"]
+[3.435594320297241, 13.434615135192871, "Laser Communication Terminal Optical Technology Homodyne BPSK (Binary Phase Shift Keying)"]
+[4.371119976043701, -2.746628999710083, "Satellite Monitoring Duration About a month"]
+[1.6750397682189941, -1.7699339389801025, "Satellite Sky Coverage About 75%"]
+[1.449710488319397, -1.1323790550231934, "Satellite Image Size 24-by-24 degrees"]
+[3.736893892288208, -2.5620956420898438, "Satellite Image Capture Frequency Every 30 minutes"]
+[3.7555294036865234, -2.5998568534851074, "Satellite Image Capture Frequency Every 10 minutes"]
+[2.066213369369507, -2.74269437789917, "Satellite Number of Stars Nearly 24 million"]
+[-3.5162065029144287, 4.390316963195801, "Spacecraft Launch Date Fall 2027"]
+[5.083054542541504, -4.225508689880371, "Lander Launch Date Summer 2028"]
+[-3.8456714153289795, 3.7481689453125, "Rover Landing Date Feb. 18, 2021"]
+[-4.475010395050049, 15.913182258605957, "Radar Operating Temperature -30\u00baC"]
+[-4.5047149658203125, 15.927360534667969, "Radar Altitude about 3 km"]
+[0.43062248826026917, 12.191246032714844, "Sensor Footprint at Nadir 48 km to 120 km"]
+[0.6216915249824524, 12.187576293945312, "Sensor Noise Levels (NEDT) 0.6 K to 0.8 K"]
+[0.5072649121284485, 12.196150779724121, "Sensor Peaking Measurement Heights 0 to 10 km"]
+[0.6380757093429565, 12.045859336853027, "Sensor Step Stare System 28 steps per scan"]
+[0.5462189316749573, 12.109694480895996, "Sensor Scan Period 8 seconds per scan"]
+[0.5441962480545044, 12.129863739013672, "Sensor Data Usage Determine water vapor mass in seven layers, and specific and relative humidity at six levels"]
+[-2.9541049003601074, 4.58746337890625, "Parachute Altitude of Deployment Around 7 \u00bd km"]
+[-2.8437399864196777, 4.720517635345459, "Parachute Diameter 35 m"]
+[-3.0433237552642822, 4.237105846405029, "Spacecraft Splashdown Location Pacific Ocean"]
+[-3.3408455848693848, 4.204679012298584, "Spacecraft Recovery Time One hour after splashdown"]
+[-3.0194602012634277, 4.223373889923096, "Spacecraft Recovery Process Powered down, put in a safe mode"]
+[-3.10622239112854, 4.30808162689209, "Spacecraft Recovery Team U.S. Navy divers in several rigid hull and Zodiac boats"]
+[4.661484241485596, -2.5675933361053467, "Satellite Mission Duration Minimum of two years"]
+[2.061767339706421, -2.685678720474243, "Satellite Telescope Quantity 26"]
+[2.6252593994140625, 14.288561820983887, "Optical Instrument Aperture 12 cm"]
+[2.6736464500427246, 14.291491508483887, "Optical Instrument Focal Plane Four large-format CCD sensors"]
+[11.25786018371582, 5.502035617828369, "Cubesats Manufacturer Boeing"]
+[11.232596397399902, 5.520177364349365, "CubeSat Purpose Enhancing Space Situational Awareness"]
+[-1.2617764472961426, 6.509138107299805, "Workshop Date April 20-22, 2011"]
+[2.8870198726654053, 21.957462310791016, "Instrument Purpose Enhance the flow of solar wind onto a small target to make possible oxygen and nitrogen measurements"]
+[3.0428075790405273, 22.403200149536133, "Instrument Manufacturer Los Alamos National Laboratory"]
+[2.6065714359283447, 21.916067123413086, "Instrument Function Make possible oxygen and nitrogen measurements"]
+[2.65733003616333, 22.194190979003906, "Instrument Impact Revealed differences between the sun and planets in oxygen and nitrogen"]
+[-0.24506399035453796, 6.96928071975708, "Investigation URL http://sprg.ssl.berkeley.edu/sprite/ago96/isual/ROCSAT.html"]
+[2.2957944869995117, -1.7619192600250244, "Satellite Journal Article J. L. Chern, R. R. Hsu, H. T. Su, S. B. Mende, H. Fukunishi, Y. Takahashi, L .C. Lee, \"Global Survey of Transient Luminous Events by ROCSat-2 Satellite,\" Journal of Atmospheric and Solar-Terrestrial Physics, Vol. 65, 2003, pp. 647\u2013 659"]
+[2.579826593399048, -3.9237170219421387, "Satellite URL https://web.archive.org/web/20170812134946/http://sprite.phys.ncku.edu.tw/En/Eindex.html"]
+[1.146317481994629, -0.7183815836906433, "Satellite Size 10 cm x 10 cm x 34.5 cm"]
+[0.9621686339378357, -4.439952850341797, "Satellite Mass ~ 3.8 kg"]
+[0.8475129008293152, 12.07539176940918, "Sensor Quantity 2"]
+[0.9030752182006836, 12.131941795349121, "Sensor Quantity 1"]
+[-3.137110948562622, 1.7096011638641357, "Satellite Mission Theme Gravitational Universe"]
+[0.14386685192584991, 7.190608024597168, "Experiment Discovery Date 2015"]
+[0.1600102335214615, 7.159181594848633, "Experiment Signal Trigger Merging of two black holes"]
+[0.1385049819946289, 7.188130855560303, "Experiment Distance to Signal Source 1.3 billion light-years"]
+[0.0947544127702713, 7.147748947143555, "Experiment Number of Subsequent Detections Two"]
+[-3.7940587997436523, 6.967241287231445, "Data Collection System Downlink Frequency 460-470 MHz"]
+[-3.8369791507720947, 6.985069751739502, "Data Collection System Downlink Data Rate 200 bit/s"]
+[-3.885432004928589, 6.861832618713379, "Data Collection Platform Received Frequency 401.65 MHz"]
+[-3.891068935394287, 6.8380303382873535, "Data Collection Platform Data Rate 400 bit/s"]
+[-3.8101048469543457, 6.942137718200684, "Data Collection System Mass 76 kg"]
+[-3.818681001663208, 6.934544563293457, "Data Collection System Power Consumption 60 W"]
+[1.4298121929168701, -2.512864589691162, "Satellite Orbit Type Sun-synchronous"]
+[0.7407659888267517, -1.1562080383300781, "Satellite Altitude 693 km"]
+[0.6932818293571472, -2.3135387897491455, "Satellite Inclination 98.19\u00b0"]
+[4.044269561767578, -2.861687183380127, "Satellite Period 98.74 minutes"]
+[4.119019508361816, -2.470475673675537, "Satellite Repeat Cycle 12 days"]
+[-1.894461989402771, 14.858866691589355, "Radiometer Operating Bands K-band and Ka-band"]
+[-1.8699113130569458, 14.8514986038208, "Radiometer 3db Beamwidth 1.64\u00ba"]
+[-1.9088190793991089, 14.834017753601074, "Radiometer IFOV Resolution 50 km"]
+[-5.336195945739746, 7.958280086517334, "Communication System Modulation Type 16QAM, QPSK"]
+[-5.190941333770752, 7.79191780090332, "Communication System Data Rate 800, 400, or 200 Mbit/s"]
+[-5.318594455718994, 8.034419059753418, "Communication System Frequency Bandwidth < 275 MHz"]
+[-5.224447250366211, 7.833827018737793, "Communication System Temperature -20 to + 50\u00baC"]
+[-5.341424465179443, 7.791982650756836, "Communication System Voltage 30 to 53 VDC"]
+[-5.323510646820068, 7.949792385101318, "Communication System Power +5 dBm \u00b1 1 dB"]
+[-5.243520736694336, 7.879526138305664, "Communication System Power Consumption \u2264 25.5 W"]
+[-5.215963363647461, 7.893524646759033, "Communication System Mass \u2264 3.36 kg"]
+[-5.242998123168945, 7.882329940795898, "Communication System Size 277 mm x 106 mm x 186 mm"]
+[-1.9024028778076172, 14.855854034423828, "Radiometer Image Credit DMSP Program Office USAF, NOAA"]
+[-3.0561001300811768, 14.86362361907959, "Special Sensor Microwave Temperature Sounder Device Type Radiometer"]
+[2.7746741771698, 22.442771911621094, "Instrument Type Gravity instruments"]
+[2.7832682132720947, 22.37688636779785, "Instrument Type Laser Ranging Interferometer"]
+[2.7658321857452393, 22.439504623413086, "Instrument Type Accelerometer"]
+[2.8756041526794434, 22.444738388061523, "Instrument Type Star Camera Assembly"]
+[2.842170238494873, 22.438278198242188, "Instrument Type GNSS"]
+[2.6346828937530518, 22.449974060058594, "Instrument Type Radio Occultation receiver"]
+[1.8625723123550415, -2.16748046875, "Satellite Orbit Drift Eastward"]
+[5.25216817855835, -4.440694808959961, "Satellite Orbit Lowering Manoeuvre Date December 2, 2009"]
+[2.145416498184204, -1.7020853757858276, "Satellite Star Tracker (STR) Main instrument used to verify the satellite orientation"]
+[1.9168410301208496, -2.109079599380493, "Satellite Gyro Mode Used only for a few minutes on each rotation"]
+[2.5710861682891846, -1.7265526056289673, "Satellite Payload Rotating wheel inside the payload could change the satellite orientation"]
+[-2.3205995559692383, 13.364803314208984, "Hyperspectral Sensor Design and Ground Testing Unknown"]
+[3.6625702381134033, 22.96973419189453, "Instrument Evaluation Date Sept. 1990"]
+[2.6028831005096436, 22.523283004760742, "Instrument User's Interpretation Guide Revision C"]
+[3.6763596534729004, 22.963069915771484, "Instrument Proceedings Date Aug. 1993"]
+[-0.38335639238357544, 6.767883777618408, "Testing Equipment Status Will be removed"]
+[-0.806349515914917, 8.862469673156738, "Thermal Control Devices Location Near the top and the bottom of the outer aluminum enclosure"]
+[3.006918430328369, 22.61895751953125, "Instrument Design Status Flight model production has started"]
+[1.64956533908844, 6.980334758758545, "Communication Device Frequency Band S-band"]
+[1.6512011289596558, 6.983273983001709, "Communication Device Frequency Band X-band"]
+[1.7673512697219849, 6.871413230895996, "Communication Device Data Download Capacity Up to 17 GB/day"]
+[1.773028016090393, 6.857815742492676, "Communication Device Data Rate High Data Rate-Telemetry"]
+[4.733616352081299, -2.6186747550964355, "Satellite Mission Duration Over the past two decades"]
+[2.8546478748321533, 22.485698699951172, "Instruments Data Collection 1991-1997 and 2009-2015"]
+[2.7873220443725586, 22.249401092529297, "Instrument Data Collection In situ measurements"]
+[0.46046221256256104, 4.53220272064209, "Natural Formation Decline Rate 13 percent each decade since 1979"]
+[0.6823211908340454, -1.1353627443313599, "Geographic Area Warming Rate Twice as fast as the rest of the world"]
+[-14.056890487670898, -2.3262476921081543, "X-ray Camera Field-of-view Wide"]
+[-13.87995719909668, -2.1866261959075928, "X-ray Camera X-ray Type Soft"]
+[-13.897455215454102, -2.1950294971466064, "X-ray Camera Development Time Sixteen years"]
+[-13.975221633911133, -2.1581499576568604, "X-ray Camera Development Location Goddard and Wallops Flight Facility on Wallops Island, Virginia"]
+[2.2962942123413086, -1.318299651145935, "Satellite Radar Measurements Ice"]
+[2.10589861869812, -1.2913460731506348, "Satellite Laser Measurements Ice"]
+[16.792613983154297, 6.904219150543213, "Microsatellite Mass 56 kg"]
+[-3.2774665355682373, 5.449736595153809, "Launch Vehicle Launch Date 3 December 2018"]
+[-3.261861562728882, 5.432528495788574, "Launch Vehicle Launch Time 18:34 GMT"]
+[-3.094498634338379, 2.4233899116516113, "Mission Payloads 64"]
+[-3.0897412300109863, 2.4376158714294434, "Mission Deployment Time Approximately 13 to 43 minutes after liftoff"]
+[-3.0941667556762695, 2.4033026695251465, "Mission Expected Deployment Duration Six hours"]
+[6.4266839027404785, 7.303335189819336, "Satellite Component Doppler Shift Happening due to the spinning disk"]
+[-1.1144033670425415, 3.026888132095337, "Celestial Body Speed Approaches the speed of light"]
+[-1.162455677986145, 3.0497193336486816, "Celestial Body Gravity Enormous"]
+[-1.614763617515564, 1.4786620140075684, "Data Relay System Data Transmission High speed OISL (Optical Intersatellite Links) between LEO and GEO relay satellite and multi channel RF downlinks in Ka-band for the GEO to ground links"]
+[-1.6220639944076538, 1.4827245473861694, "Data Relay System Manufacturer Tesat Spacecom"]
+[0.07782693952322006, 7.098107814788818, "Space Experiment Frame-Dragging Accuracy Approximately 2 x 10-3"]
+[1.438106894493103, -1.8834716081619263, "Satellite Frame-Dragging Accuracy 2%"]
+[1.48973548412323, -1.8386677503585815, "Satellite Frame-Dragging Accuracy 2%"]
+[1.4336212873458862, -1.8641241788864136, "Satellite Frame-Dragging Accuracy 2%"]
+[-1.8098808526992798, 8.521931648254395, "Switches Activation After spacecraft deployment"]
+[-1.939119815826416, 7.306375026702881, "Computer Operation Start Since 2017"]
+[-1.9161473512649536, 8.026388168334961, "System Operation Start Since 2014"]
+[-2.2844033241271973, 9.061878204345703, "Electrical Power System Qualification Status Qualified for flight"]
+[1.4680901765823364, -3.170320987701416, "Satellites Launch Date July 14, 2017"]
+[5.311734199523926, -4.34068489074707, "Satellite Launch Date November 28, 2017"]
+[-2.152860403060913, 5.908056259155273, "Test Flight Launch Date August 2, 2017"]
+[5.373785018920898, -4.432848930358887, "Satellite Launch Date December 3, 2018"]
+[5.2566633224487305, -4.355518817901611, "Satellite Launch Date November 20, 2020"]
+[4.091856956481934, 13.935004234313965, "Laser Altimeter System Elevation Measurement Date October 31, 2018"]
+[4.070384502410889, 13.93046760559082, "Laser Altimeter System Image Credit NASA Earth Observatory, image by Joshua Stevens, using ICESat-2 data from the National Snow & Ice Center, topographic data from SRTM, and Landsat data from the U.S. Geological Survey"]
+[2.045959711074829, -2.7746756076812744, "Satellite Number of Spacecraft 2"]
+[2.091769218444824, -2.806426525115967, "Satellite Total Number in Space 55"]
+[2.2038092613220215, -2.6134033203125, "Satellite Remaining Launches 2 of 10 satellites each"]
+[5.2548933029174805, -4.487660884857178, "Satellite Shipping Schedule This week"]
+[2.229006767272949, -2.094305992126465, "Satellite Location VAFB Harris Corporation facility"]
+[2.926433801651001, 22.005281448364258, "Instrument Purpose Provide maps of salt concentration on the ocean surface"]
+[2.633366107940674, 22.9278507232666, "Instrument Data Collection Duration At least three years"]
+[2.3661627769470215, 22.180999755859375, "Instrument Measurement Sea Surface Salinity (SSS)"]
+[2.2010586261749268, 22.247087478637695, "Instrument Measurement Sea Surface Temperature (SST)"]
+[2.241421937942505, 22.187057495117188, "Instrument Measurement Atmospheric Parameters"]
+[2.2373197078704834, 22.191591262817383, "Instrument Measurement Temperature and humidity profile of the troposphere and the stratosphere"]
+[2.2513489723205566, 22.16325569152832, "Instrument Measurement Rain rates, surface wind speeds, water vapor and cloud liquid water, over the oceans"]
+[2.2484145164489746, 22.11346435546875, "Instrument Measurement Sea ice concentration"]
+[-3.626640558242798, 12.774221420288086, "Particle Detector Tube Diameter 6 mm"]
+[-3.634817361831665, 12.751182556152344, "Particle Detector Gas Mixture 80% Xe / 20% CO2"]
+[-3.599569082260132, 12.726203918457031, "Particle Detector Gas Pressure 1.0 bar absolute"]
+[-0.5876790881156921, 8.35920238494873, "Mechanical Support Precision 0.1 mm"]
+[-0.5297502875328064, 8.285815238952637, "Support Structure Width 1.5 m at the bottom to 2.2 m at the top"]
+[2.684173345565796, 13.800665855407715, "Optical System Wavelength Range 1249 \u2013 1305 nm"]
+[2.730625867843628, 13.801392555236816, "Optical System Spectral Sampling 0.1 nm"]
+[2.688746213912964, 13.828688621520996, "Optical System Spectral Resolution 0.3 nm"]
+[0.8890662789344788, -2.08127498626709, "Satellite Field of View 21\u00ba"]
+[1.1875191926956177, -1.5073341131210327, "Satellite Observing Swath About 200 km"]
+[1.4987047910690308, -1.0984718799591064, "Satellite Spatial Resolution ~100 x 400 m"]
+[1.5735160112380981, -1.1049734354019165, "Satellite Focal Plane 2048-pixel wide"]
+[1.090213656425476, -1.3557335138320923, "Satellite Swath Width 1990 pixels"]
+[2.1388909816741943, -1.7346659898757935, "Satellite Cryogenic System Focal Plane Cooling"]
+[1.6348925828933716, -1.8928760290145874, "Satellite Room-temperature System Thermal Stability of the Optics"]
+[-2.1930360794067383, 2.920037269592285, "Space Observatory Light Detection X-rays"]
+[-2.2002005577087402, 2.872406482696533, "Space Observatory X-ray Study Low-energy X-rays from Jupiter's auroras"]
+[-2.1714026927948, 2.8737993240356445, "Space Observatory X-ray Study Low-energy X-rays from Jupiter's auroras"]
+[-3.380392551422119, 4.288158893585205, "Spacecraft Arrival Date at Jupiter 2016"]
+[-2.182626962661743, 2.8810718059539795, "Space Observatory Purpose Confirm hypothesis of higher-energy X-rays from Jupiter"]
+[-2.1926333904266357, 8.877423286437988, "Electrical System Potential Negative"]
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+[-2.277631998062134, 7.426429271697998, "On-Board Computer Malfunction None"]
+[-4.868256092071533, 9.20170783996582, "Transmitter-Receiver Modules Power Amplification Higher"]
+[-4.88721227645874, 9.126786231994629, "Transmitter-Receiver Modules Operational Frequency Range Wider"]
+[3.4837429523468018, 10.568924903869629, "High-Power Amplifier Output Power 34 W"]
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+[-0.8293471336364746, 0.14422480762004852, "Satellite System Design Life At least 14 years"]
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+[-0.8302052617073059, 0.14742791652679443, "Satellite System Longitude 75\u00ba West and 137\u00ba West"]
+[-0.8425868153572083, 0.14505398273468018, "Satellite System Inclination 0\u00ba"]
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+[0.7670632600784302, -1.2191994190216064, "Satellite Coastline Length Around 800 km"]
+[2.892728805541992, -1.2240961790084839, "Satellite Mission Purpose Provide detailed information about Earth\u2019s vegetation, play a key role in mapping differences in land cover, understand the landscape, map how it is used and monitor changes over time"]
+[-0.23179425299167633, 10.127249717712402, "Global Positioning System Precise Tracking Unknown"]
+[6.292868614196777, 7.455961227416992, "Satellite Component Structure Similar to that of the Imager"]
+[6.32734489440918, 7.416873455047607, "Satellite Component Components Scan mechanism assembly, telescope, aft optics, filter-wheel assembly with its cooler, cooler assembly with the cooled detectors, detectors for the uncooled channels, preamplifiers, viewport sunshade"]
+[-3.3169052600860596, 7.47286319732666, "Data Processing Probability Calculation Based on event intensity, the electronics noise, and the photon noise of the background"]
+[-3.3354907035827637, 7.453206539154053, "Data Processing Probability Threshold Adjustable"]
+[-2.192958116531372, 5.956885814666748, "Formation Flying System Design and Prototyping Unknown"]
+[-2.2247262001037598, 5.8951239585876465, "Formation Flying System Conference Date May 29-31, 2013"]
+[-2.1942214965820312, 5.941326141357422, "Formation Flying System URL of Paper http://www.sffmt2013.org/PPAbstract/4069p.pdf"]
+[-2.1670656204223633, 5.928192615509033, "Formation Flying System URL of Presentation http://www.sffmt2013.org/PPAbstract/4056pr.pdf"]
+[2.6847572326660156, -2.08445405960083, "Satellite Operations Team Size 7 to 10 JPL staff members"]
+[2.5605592727661133, -1.9224470853805542, "Satellite Ground Station Operators Half-dozen talented students"]
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+[2.855577230453491, -1.7015936374664307, "Satellite Operations Center JPL Earth Orbiting Mission Operations Center"]
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+[5.35595178604126, -4.462278842926025, "Satellite Launch Date March 7, 2017"]
+[2.569321632385254, -3.9375975131988525, "Satellite URL http://m.esa.int/Our_Activities/Observing_the_Earth/Copernicus/Sentinel-2/Second_colour_vision_satellite_for_Copernicus_launched"]
+[-0.6293851733207703, 9.42661190032959, "Spacecraft Component Manufacturer Airbus Defence and Space"]
+[-0.5939422845840454, 9.435744285583496, "Spacecraft Component Development and Construction November 2014"]
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+[2.301162004470825, -1.7616490125656128, "Satellite Structure Essentially a cube"]
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+[-4.803522109985352, 7.61775016784668, "Internet-based Service Information Provided Flight tracks, origins and destinations, flight numbers, aircraft types, positions, altitudes, headings, speeds"]
+[-4.501817226409912, 7.531565189361572, "Internet-based Service Data Source Crowdsourced information gathering by volunteers with ADS-B receivers"]
+[5.406142234802246, -4.3347368240356445, "Satellite Launch Date Q3 of 2014"]
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+[-8.530951499938965, 13.614524841308594, "Environmental Parameter Uncertainty 0.5 mm per year"]
+[2.341688632965088, -1.294460654258728, "Satellite Observation Tool Global view of water mass changes"]
+[-1.4349474906921387, 13.351144790649414, "Solar Panels Power 37 W EOL"]
+[-2.203439712524414, 8.979442596435547, "Power Control Units Quantity 2"]
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+[-1.8493901491165161, 7.32031774520874, "Computers Quantity 2"]
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+[-1.966409683227539, 7.318274021148682, "Computers CPU 80C186, 16 MHz"]
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+[14.564935684204102, 7.764837265014648, "Nanosatellite Power Generation 300 V"]
+[14.46107292175293, 7.70704460144043, "Nanosatellite Orbit LEO"]
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+[6.01596212387085, 7.779524803161621, "SARSAT Repeater Provider CRC/Canada"]
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+[-5.278706073760986, 7.907018661499023, "Communication System Provider USA"]
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+[7.44675350189209, 12.579495429992676, "Satellite Instrument Design Milestone Date 21 February 2020"]
+[5.112476348876953, -4.293449401855469, "Satellite Critical Design Review Completion Date 21 September 2020"]
+[3.0616044998168945, -1.6574747562408447, "Satellite Mission Operations Control Center Creator Rocket Lab"]
+[-0.6385817527770996, 9.442580223083496, "Spacecraft Component Processing Speed 480 million instructions/second"]
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+[-0.5218981504440308, 15.543015480041504, "Imaging Spectrometer Provider French National Centre for Space Studies (CNES)"]
+[-0.1662399172782898, 15.552741050720215, "Spectrometer Centre Frequency Range 6.925 - 89.0 GHz"]
+[-0.16132760047912598, 15.570222854614258, "Spectrometer Bandwidth Range 100 - 3000 MHz"]
+[-0.124839648604393, 15.48229694366455, "Spectrometer Spatial Resolutions 3 x 6 km - 40 x 60 km"]
+[-0.15452814102172852, 15.545548439025879, "Spectrometer Incidence Angle 55\u00b0"]
+[-0.09716975688934326, 15.496586799621582, "Spectrometer Swath Width 1600 km"]
+[-1.6947792768478394, 5.335711479187012, "Mission Operations Center Function Transfer science data"]
+[-1.5513250827789307, 5.548238754272461, "Science Operations Center Function Process and validate the data, and distribute products to the science team"]
+[2.336535930633545, -2.424025774002075, "Satellite Proprietary Period None"]
+[2.514127731323242, -1.741248607635498, "Satellite Public Science Archive Location HEASARC"]
+[4.869714260101318, -4.456619739532471, "Satellite Image Acquisition Date Feb. 11, 2016"]
+[4.870034217834473, -4.470643043518066, "Satellite Image Acquisition Date Jan. 31, 2016"]
+[0.35299015045166016, 4.549756050109863, "Ecosystem Response to Global Climate Changes Increased sea surface temperature (SST), ultraviolet radiation (UV) and acidification of seawater"]
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+[2.746098756790161, -1.9535220861434937, "Satellite Environmental Monitoring Unknown"]
+[1.422213077545166, -3.1059398651123047, "Satellites Environmental Monitoring Unknown"]
+[-3.3344969749450684, 8.532695770263672, "Memory Endurance About 10^5 cycles"]
+[-3.3184814453125, 8.528684616088867, "Memory Radiation Sensitivity High"]
+[-3.3383965492248535, 8.529549598693848, "Memory Radiation Sensitivity General"]
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+[2.627563238143921, 14.32752799987793, "Optical Instrument Spectral Range 0.5 - 0.9 \u00b5m"]
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+[2.589543104171753, 14.323481559753418, "Optical Instrument Ground Pixel Size 2.5 km x 2.5 km"]
+[2.5941500663757324, 14.278181076049805, "Optical Instrument Scan Lines per Image 5000 (each line of 5000 pixels)"]
+[2.60225772857666, 14.404229164123535, "Optical Instrument Line Duration 30 ms"]
+[2.612537145614624, 14.266511917114258, "Optical Instrument Number of Pixels/Image 25 Mpixel"]
+[2.679276704788208, 14.351493835449219, "Optical Instrument Image Duration/Recurrence 25 min (scanning), 30 min (duty cycle = 100%), with 5 minutes spare time for a retrace of the scan mirror"]
+[2.6688437461853027, 14.367849349975586, "Optical Instrument Detector Type Si HgCdTe HgCdTe"]
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+[2.5569400787353516, 14.399497985839844, "Optical Instrument Radiometer Performance SNR > 200 for 25% albedo NEDT < 1.0 K at 260 K NEDT < 1.0 K at 260 K"]
+[2.658576488494873, 14.370841026306152, "Optical Instrument Data Transmission Rate 333 kbit/s (normal), 2.7 Mbit/s (burst mode)"]
+[2.6789939403533936, 14.272235870361328, "Optical Instrument Mass 63 kg"]
+[0.6749024391174316, -1.1163825988769531, "Satellite Altitude Adjustment Just more than half a mile (900 meters)"]
+[1.5062172412872314, -2.4458603858947754, "Satellite Orbit Overlap Every 19th orbit of CryoSat-2 and 20th orbit of ICESat-2"]
+[-0.2511810064315796, 8.297972679138184, "Sea Ice Component Insulating Effect Insulates sea ice from frigid polar air, slowing ice growth"]
+[-5.217408180236816, 7.777792453765869, "Communication System Data Transfer Rate 12 Mbit/s"]
+[-1.110772967338562, 4.491013050079346, "Ground Station Data Transmission X-band deep space transponder"]
+[-5.187727451324463, 3.0459675788879395, "Lunar Probe Camera Resolution Higher resolution camera compared to Chang'e-1"]
+[7.276309490203857, 12.387666702270508, "Satellite Instrument Data Downlink Frequency 2.265 GHz"]
+[-1.3268840312957764, 4.394096851348877, "Ground Equipment Number of Stations 5"]
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+[-3.456723213195801, 6.855100154876709, "Data Product Processing Technique Analogue techniques, incorporating optical lenses and photographic film"]
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+[3.0459861755371094, 22.80928611755371, "Instrument Unknown Unknown"]
+[2.6366732120513916, 14.29446792602539, "Optical Instrument Effective Focal Length 1150 mm"]
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+[1.9428634643554688, 10.735427856445312, "Imaging Device Size 2048 x 2048 pixels"]
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+[1.9312045574188232, 10.71914005279541, "Imaging Device Operating Temperature < 60\u00baC"]
+[2.6090753078460693, 14.322741508483887, "Optical Instrument Bandpass 540\u2013590 nm"]
+[2.629222869873047, 14.331132888793945, "Optical Instrument Wavelengths Fe XIV 530.3 nm; He I 587.6 nm"]
+[2.571194887161255, 14.365589141845703, "Optical Instrument Calibration Lamp Wavelength 546.1 nm"]
+[-6.593746662139893, 9.897072792053223, "Antenna System G/T 32 dB/\u00b0K @ 5\u00b0 EL"]
+[-4.686489105224609, 7.567618370056152, "Data Reception System Signal Reception Frequency 8212.5 MHz"]
+[-4.703678607940674, 7.56124210357666, "Data Reception System Signal Reception Frequency Bandwidth 320 MHz"]
+[-4.669177055358887, 7.550428867340088, "Data Reception System RF Carrier Data Rate 160 Mbit/s"]
+[-4.704279899597168, 7.591846466064453, "Data Reception System Demodulator Data Rate 320 Mbit/s"]
+[-13.51889419555664, -2.069504737854004, "X-ray Observatory Launch Date June 13, 2012"]
+[-13.460210800170898, -1.9969056844711304, "X-ray Observatory Principal Investigator Fiona Harrison"]
+[-13.497509956359863, -2.015005111694336, "X-ray Observatory Mission Operations Center University of California, Berkeley"]
+[-13.48611831665039, -2.005873918533325, "X-ray Observatory Ground Station Provider ASI"]
+[-13.492534637451172, -2.0253970623016357, "X-ray Observatory Mirror Data Archive Provider ASI"]
+[-13.47861385345459, -2.010251760482788, "X-ray Observatory Design Quirk Allows study of previously unwanted light"]
+[1.3113820552825928, -1.2375506162643433, "Satellite Ground Resolution Up to 10 m"]
+[2.1226837635040283, 22.54871368408203, "Instrument Time Resolution Better than several hundred \u00b5s"]
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+[0.6121607422828674, 12.222423553466797, "Sensor Bands Pan: (0.42 - 0.73 \u00b5m), MS: (0.42 - 0.55, 0.55 - 0.63, 0.58 - 0.73 \u00b5m)"]
+[0.4978595972061157, 12.199252128601074, "Sensor Ground Sample Distance Pan: 7.5 m, MS: 15 m"]
+[0.5406565070152283, 12.144911766052246, "Sensor Swath Width 30 km"]
+[0.5875040888786316, 12.183836936950684, "Sensor Field of Regard ~ 800 km"]
+[0.5322614312171936, 12.202077865600586, "Sensor Modulation Transfer Function Pan: 8%, MS: 15%"]
+[0.5132055878639221, 12.249786376953125, "Sensor Signal-to-Noise Ratio \u2265 64"]
+[0.5748192667961121, 12.226042747497559, "Sensor Mass Storage Capacity 7 Gbit"]
+[0.5979631543159485, 12.139689445495605, "Sensor Mass, Power Consumption 6.5 kg, 22 W"]
+[0.48334670066833496, 12.193556785583496, "Sensor Size Telescope: 170 mm x 420 mm, Electronics: 265 mm x 200 mm x 85 mm"]
+[0.4742407202720642, 12.251276969909668, "Sensor Data Rate 25 Mbit/s"]
+[-3.6100401878356934, 12.776604652404785, "Sub-Atomic Particle Detector Purpose Looks for dark matter, antimatter and measures cosmic rays"]
+[-3.5239672660827637, 12.842328071594238, "Sub-Atomic Particle Detector Installation Date 2011"]
+[-3.603383779525757, 12.764284133911133, "Sub-Atomic Particle Detector Lifespan Surpassed three years"]
+[0.9562946557998657, -4.37837553024292, "Satellite Weight 600 kg"]
+[2.749809741973877, -2.2545833587646484, "Satellite Launch Site Vandenberg Air Force Base"]
+[5.276556015014648, -4.399662971496582, "Satellite Launch Date December"]
+[-1.2990999221801758, 6.193526744842529, "Human Resources Quantity 15"]
+[1.7446069717407227, -1.9342445135116577, "Satellite Test Location IABG in Ottobrunn near Munich"]
+[5.225665092468262, -3.7697720527648926, "Satellite Launch Campaign 2018"]
+[-0.3149488568305969, 6.563075065612793, "Test Facility Dimensions 75 m long, 9 m wide"]
+[-0.29464855790138245, 6.523902893066406, "Test Facility Purpose Simulate the deep ocean environment"]
+[2.5315356254577637, -2.040585994720459, "Satellite Ground Segment Upgraded from the RADARSAT-1 infrastructure"]
+[-1.6763852834701538, 5.322258949279785, "Mission Operations Center Installation Date May 2006"]
+[3.0039939880371094, -1.4076061248779297, "Satellite Mission Stakeholder Canadian Government"]
+[5.3203840255737305, -4.405059814453125, "Satellite Launch Date 24 July"]
+[2.1020398139953613, -2.504728078842163, "Satellite Optical Links 20,000"]
+[2.710090398788452, -2.206533670425415, "Satellite Communication Secure laser communication to receive data from the low-Earth orbiting satellites and beams the information back to Earth via radio frequency"]
+[2.208289384841919, 23.135587692260742, "Instrument Frequency Noise Power Spectral Density 30 Hz/\u221aHz"]
+[2.2246639728546143, 23.131738662719727, "Instrument Frequency Range 10 mHz to 100 mHz"]
+[1.71721613407135, 21.982572555541992, "Instrument Length Scales 700 km to 70 km"]
+[-1.259307622909546, 8.586729049682617, "Component Frequency Stability Limit One order of magnitude lower than the adopted goal"]
+[-0.8303660750389099, 0.16693401336669922, "Satellite System Survival Goal Launch vibration and on-orbit thermal extremes"]
+[-1.6182810068130493, 1.4816899299621582, "Data Relay Service User Data Volume Improved"]
+[-1.6200283765792847, 1.481036901473999, "Data Relay Service Timeliness Improved"]
+[-1.6276586055755615, 1.4943960905075073, "Data Relay Service Access Time Restricted by the visibility time"]
+[-1.6132028102874756, 1.4691518545150757, "Data Relay Service Visibility Time Around 50% of the LEO satellite\u2019s orbital period"]
+[-1.6170538663864136, 1.4744646549224854, "Data Relay Service Coverage Wide European"]
+[2.8308732509613037, -1.0479990243911743, "Satellite Purpose Measure methane emissions worldwide"]
+[-1.7783417701721191, 8.731006622314453, "Control Centre Funding Source Strategic Science Investment Fund"]
+[-1.2728221416473389, 6.661663055419922, "Research Program Funding Source Catalyst: Strategic"]
+[-1.3563443422317505, 6.184248924255371, "Team Leader Affiliation NIWA"]
+[4.082310676574707, 13.927976608276367, "Laser Altimeter System Laser Pulse Photon Count More than 200 trillion"]
+[4.08524227142334, 13.923531532287598, "Laser Altimeter System Number of Photons Returning to Telescope Only a dozen or so"]
+[-5.3856730461120605, 2.9337852001190186, "Receiver Telescope Assembly Alignment Requirement Perfect"]
+[4.0990071296691895, 13.93660831451416, "Laser Altimeter System Launch Date June 2018"]
+[4.110683917999268, 13.949398040771484, "Laser Altimeter System Integration and Testing Team Size 250 engineers, fabricators and scientists"]
+[7.310380458831787, 12.446915626525879, "Satellite Instrument Observation Total solar eclipse in South America"]
+[7.278244972229004, 12.406115531921387, "Satellite Instrument Observation Planet-scale waves in the lower atmosphere"]
+[7.279816150665283, 12.423050880432129, "Satellite Instrument Measurement Changes in the chemical composition of the thermosphere during the total solar eclipse of July 2, 2019"]
+[-0.798237144947052, 11.560089111328125, "Detector Performance Unknown"]
+[-0.7203949689865112, 11.49632740020752, "Detector Function Unknown"]
+[-2.409420967102051, 9.222888946533203, "Power Distribution Unit Bus Voltage 28 V"]
+[-2.5599260330200195, 9.626263618469238, "Power Source Number of Deployable Wings 2"]
+[-5.1990838050842285, 7.892390251159668, "Communication Subsystem Ground Station Links Up and down links"]
+[-6.768035411834717, 10.026155471801758, "High Gain Antenna Assembly Data Transmission Rate Up to 72 Mbit/s"]
+[16.865509033203125, 6.855013370513916, "Microsatellite Operating Status Nominal"]
+[16.864660263061523, 6.842294216156006, "Microsatellite Years on Orbit 6"]
+[16.903621673583984, 6.837879180908203, "Microsatellite Orbit Lower orbit (3.9 km below the orbit of the A-train)"]
+[16.977584838867188, 6.73737096786499, "Microsatellite Join Date Early February 2005"]
+[-5.259838581085205, 7.960784912109375, "Communication System Downlink Frequency Ka-band"]
+[-5.221219539642334, 7.760754585266113, "Communication System Downlink Data Rate 278 Mbit/s"]
+[-5.071416854858398, 7.710592269897461, "Communication System Ground Stations Downlink Data Rate X-band at 800, 400, or 200 Mbit/s"]
+[-5.298625469207764, 7.930184841156006, "Communication System TT&C Frequency S-band"]
+[2.685483932495117, -2.338440418243408, "Satellite Launch Vehicle Mitsubishi vehicle - an H-IIA F24 bus"]
+[2.650130033493042, -1.2522857189178467, "Satellite Objective Provide data continuity to be used for cartography, regional observation, disaster monitoring, and environmental monitoring"]
+[-3.1399335861206055, 1.695763111114502, "Satellite Mission Measurement Frequency Weekly"]
+[2.8852627277374268, -1.71247398853302, "Satellite Series Observation Type Similar to Copernicus Anthropogenic Carbon Dioxide Monitoring, CO2M mission"]
+[2.7824559211730957, -1.8147428035736084, "Satellite Series Observation Type Similar to Copernicus Anthropogenic Carbon Dioxide Monitoring, CO2M mission"]
+[-4.478692531585693, 15.919585227966309, "Radar Center Frequency 9.623 GHz"]
+[-4.488869667053223, 15.919937133789062, "Radar Incidence Angle Range 25-48\u00ba"]
+[-4.487553119659424, 15.9232816696167, "Radar Swath Width 450-600 km"]
+[-4.438989162445068, 15.869637489318848, "Radar Spatial Resolution in Medium Resolution Mode 400-500 m"]
+[-4.484833240509033, 15.91146469116211, "Radar Spatial Resolution in Low Resolution Mode 700-1000 m"]
+[-4.508378028869629, 15.933711051940918, "Radar Data Rate 10 kbit/s"]
+[-4.472594261169434, 15.912071228027344, "Radar Antenna Array Uncontrolled"]
+[-4.509557723999023, 15.921198844909668, "Radar Transmitter Klystron"]
+[-4.495355606079102, 15.931450843811035, "Radar Power Consumption Not more than 1 kW"]
+[-4.483891487121582, 15.929525375366211, "Radar Mass Not more than 150 kg"]
+[-4.462263584136963, 15.943084716796875, "Radar Antenna Mass Not more 40 kg"]
+[-4.503453254699707, 15.936444282531738, "Radar Radio-link Data Transfer Rate Not more than 10 kbit/s"]
+[2.649231433868408, -2.0610618591308594, "Satellite Planned First Indigenous Satellite Build Is Planned By Turkey\u2014T\u00dcRKSAT 6A"]
+[5.073054790496826, -4.155740737915039, "Satellite Second Anniversary Gokturk-2 Celebrates Second Anniversary"]
+[2.704305410385132, -1.6306219100952148, "Satellite Data Distribution Network NRT (Near-Real-Time)"]
+[2.2195348739624023, -2.5150742530822754, "Satellite Users 16"]
+[4.62995719909668, -2.6251420974731445, "Satellite Study Duration Two years"]
+[2.5438647270202637, -1.1661546230316162, "Satellite Data Usage Improve the forecast of winds, waves, and the location of storms"]
+[2.4761619567871094, -1.2198251485824585, "Satellite Data Usage Better routing of ships with substantial savings in operating costs"]
+[3.088379383087158, -1.8432567119598389, "Satellite Mission Status Complete"]
+[4.984382152557373, -2.3746745586395264, "Satellite Operational Life Three years"]
+[2.044184923171997, -2.743229866027832, "Satellite Slew Count 620"]
+[2.0411112308502197, -2.756373405456543, "Satellite Slew Count 570"]
+[5.445079803466797, -4.474661827087402, "Satellite Launch Date March 6"]
+[2.5145339965820312, -3.876185417175293, "Satellite URL http://m.esa.int/spaceinimages/Images/2017/01/Revealing_Sentinel-2B"]
+[-3.2990198135375977, 15.336480140686035, "Microwave Instrument Function Provides precise Satellite to Satellite Tracking (SST) in low-low orbit"]
+[2.6257708072662354, 21.933252334594727, "Instrument Function Measures the same range fluctuations as KBR but with reduced noise and provides accurate measurements of the relative pointing of the two satellites"]
+[2.5767886638641357, 21.941360473632812, "Instrument Function Provides better thermal stability and characterisation"]
+[2.6180050373077393, 21.879669189453125, "Instrument Function Provides Precise Orbit Determination (POD), Global Navigation Satellite System (GNSS) Radio Occultation, neutral atmosphere, ionosphere and scintillation and GNSS reflections"]
+[0.7730671763420105, -1.16925048828125, "Satellite Altitude About 490 km"]
+[1.0620462894439697, -1.2195204496383667, "Satellite Spacing 220 km"]
+[0.7180625796318054, -2.3035356998443604, "Satellite Inclination Approximately 89\u00b0"]
+[0.8698534369468689, -2.1578433513641357, "Satellite Eccentricity Less than 0.0025"]
+[4.122697353363037, -2.4522252082824707, "Satellite Repeat Cycle 30 days"]
+[1.007925271987915, -4.383564472198486, "Satellite Mass Around 580 kg"]
+[-5.215228080749512, 7.814568996429443, "Communication System Data Transmission Streams 25 kbit/s, 800 kbit/s, 20 MHz"]
+[-3.848174810409546, 7.960936546325684, "Data Storage Capacity ~ 350 Mbit"]
+[1.694865345954895, 6.960363388061523, "Communication Devices Function Provide the communications link for engineering and payload data"]
+[1.727651596069336, 6.925196170806885, "Communication Device Power 5 W"]
+[2.638763904571533, 23.61582374572754, "Instrument Spin Rate 100 rpm"]
+[2.985112190246582, 22.50066566467285, "Instrument Manufacturer Matra Marconi Space"]
+[2.856511354446411, 21.92450714111328, "Instrument Usage Day/Night Cloud Coverage, Cloud Motion Winds, Cloud Top Heights, Upper Tropospheric Humidity, Precipitation and Sea Surface Temperature"]
+[2.5632498264312744, -2.779930830001831, "Satellite Operational Service Years 8"]
+[1.7342661619186401, -1.8547989130020142, "Satellite Acquisition Success Rate Above 98%"]
+[1.8250305652618408, -1.96162748336792, "Satellite Percentage of Availability 99.95%"]
+[1.7576903104782104, 10.916754722595215, "Imaging Mode Ship Detection Capability Ships 25 meters in length or greater"]
+[1.743431806564331, 10.904035568237305, "Imaging Mode Scene Size 450 km x 500 km"]
+[1.8998697996139526, 8.617846488952637, "Subsystem Uplink Frequency 145.84 MHz"]
+[1.917036771774292, 8.600966453552246, "Subsystem Downlink Frequency 437.465 MHz"]
+[1.9342759847640991, 8.644516944885254, "Subsystem Modulation FSK"]
+[1.9345604181289673, 8.626832008361816, "Subsystem OS VxWorks"]
+[-3.0037994384765625, 4.17071008682251, "Spacecraft Orbit Altitude 650 km"]
+[-3.0004115104675293, 4.159343719482422, "Spacecraft Orbit Inclination 98\u00ba"]
+[-13.913142204284668, -2.210991144180298, "X-ray Telescope Image Resolution High"]
+[-14.298479080200195, -2.5309560298919678, "X-ray Telescope Principal Investigator Peter Predehl"]
+[-13.998234748840332, -2.3308937549591064, "X-ray Telescope Image Credit Jeremy Sanders, Hermann Brunner, Andrea Merloni and the eSASS team (MPE); Eugene Churazov, Marat Gilfanov (on behalf of IKI)"]
+[0.12264434248209, 7.174986839294434, "Flight Experiment Dynamic Response Amplitude Micrometers or less"]
+[0.01077603455632925, 7.065318584442139, "Science Campaign Duration Three weeks"]
+[-1.4224936962127686, 13.349678039550781, "Solar Cells Average Efficiency 21%"]
+[-1.432003378868103, 13.361720085144043, "Solar Cells Quantity 13 strings of 40 GaAs cells"]
+[-1.4233286380767822, 13.363726615905762, "Solar Cells Quantity Six strings of 18 GaInP cells"]
+[-1.4368120431900024, 13.382404327392578, "Solar Cells Dimensions 2cm x 4 cm"]
+[-1.4258168935775757, 13.385160446166992, "Solar Cells Dimensions 2 cm x 2 cm"]
+[-3.3630146980285645, 8.55672836303711, "Mass Memory System Technology NAND-Flash Storage"]
+[2.645759344100952, 22.253061294555664, "Instrument Detects Energetic electrons"]
+[2.7205257415771484, 22.256778717041016, "Instrument Detects Energetic electrons"]
+[2.674793004989624, -2.7265737056732178, "Satellite Transmission Speed 155 Mbit/s"]
+[1.1599085330963135, -0.9046521186828613, "Satellite Antenna Diameter 1.2 m"]
+[1.2127405405044556, -0.9368475079536438, "Satellite Antenna Diameter 45 cm"]
+[2.677598237991333, -2.7583560943603516, "Satellite Transmission Speed 155 Mbit/s"]
+[5.383953094482422, -4.49589204788208, "Satellite Orbit Control Maneuvers Start Date March 2, 2008"]
+[5.288102626800537, -4.421402454376221, "Satellite Geostationary Orbit Start Date Late June 2008"]
+[-1.0591305494308472, 10.968022346496582, "CCDs Model CCD270"]
+[-1.098719835281372, 10.937676429748535, "CCDs Readout Modes Full frame (FF) or frame transfer (FT)"]
+[-1.0901238918304443, 10.920433044433594, "CCDs Temperature Lower than \u201365\u00b0C"]
+[-1.057752013206482, 10.999937057495117, "CCDs Quantum Efficiency Highest over a broad wavelength range"]
+[5.043972015380859, -4.4557108879089355, "Satellite Mission Status Presentation Date Sept. 9-11, 2015"]
+[5.011916637420654, -4.555830478668213, "Satellite Symposium Presentation Date June 22-26, 2015"]
+[2.586750030517578, -3.916464328765869, "Satellite URL http://www.sasmac.cn/AP-GEOSS8/PDFversion/DAY2/WG6/2.1-TanSat-GEOSS.YiLiu1.pdf"]
+[2.5811216831207275, -3.9236209392547607, "Satellite URL http://earth.esa.int/dragon-2015-programme/liu-monitoring_carbon_dioxide_from_space-220_ppt_present.pdf"]
+[-0.4393943250179291, 11.60372543334961, "Imaging Detector Data Collection Capacity 25 million square kilometres per day"]
+[-0.5086469650268555, 11.608320236206055, "Imaging Detector Ground Resolution 2.5 m"]
+[-0.5763038396835327, 11.630085945129395, "Imaging Detector Swath 25 km"]
+[-0.44748419523239136, 11.606620788574219, "Imaging Detector Revisit Time One to four days"]
+[2.2704410552978516, -1.6694775819778442, "Satellite Data Collection Capacity Up to 150 million square kilometres per day"]
+[4.152379512786865, -2.8348195552825928, "Satellite Orbit Period 94 - 97 minutes"]
+[0.6944578886032104, -2.3090624809265137, "Satellite Orbit Inclination Approximately 97\u00b0"]
+[0.5636284947395325, -1.4751367568969727, "Satellite Orbit Altitude Ranging from 481 - 585 km"]
+[6.2727274894714355, 7.37806510925293, "Satellite Component Temperature Fluctuation Less than 0.02 Fahrenheit"]
+[1.15345299243927, -0.7590984106063843, "Satellite Size 10 x 20 x 30 cm"]
+[5.178941249847412, -4.4161529541015625, "Satellite Deployment Date November 21, 2017"]
+[2.786241054534912, -1.1206640005111694, "Satellite Purpose Test the use of CubeSats for astronomy research"]
+[1.0158075094223022, -4.364321708679199, "Satellite Mass 350 kg"]
+[0.9928189516067505, -4.381208419799805, "Satellite Mass 35 kg"]
+[1.0859726667404175, -1.3833684921264648, "Satellite Swath Width 260 km"]
+[1.1192941665649414, -1.3641611337661743, "Satellite Swath Width 12 km"]
+[1.9424104690551758, -2.0569875240325928, "Satellite Detection Threshold 2 ppb"]
+[1.980877161026001, -1.9094270467758179, "Satellite Detection Threshold ~100 ppb"]
+[1.4791719913482666, -0.9275470972061157, "Satellite Pixel Size 400 x 100 m"]
+[1.433614730834961, -1.083463191986084, "Satellite Pixel Size 30 x 30 m"]
+[2.144519090652466, -2.665497303009033, "Satellite Planned Number of Satellites 1"]
+[2.1551382541656494, -2.5858616828918457, "Satellite Planned Number of Satellites >10"]
+[-5.696341037750244, 8.813272476196289, "RF Channels Polarimetric Capability V, H, 3rd and 4th Stokes"]
+[-4.949268341064453, 9.765600204467773, "Receiver Phase-matched v-pol and h-pol channels Based on the heritage GMI design"]
+[-4.9726643562316895, 9.804770469665527, "Receiver Output Down converted to an intermediate frequency Enabling sampling by a high-speed analog-to-digital converter and processing by the digital backend"]
+[-2.7888753414154053, 7.879188537597656, "Processor Computes the complex correlation between the v-pol and h-pol channels Yielding the 3rd and 4th Stokes parameters essential to OSVW retrievals"]
+[-4.947129726409912, 9.78415584564209, "Receiver Provides Low noise figures and very good stability for excellent radiometric performance"]
+[-1.9183460474014282, 15.033823013305664, "Multiple direction/polarisation radiometers Instrument Type Multiple direction/polarisation radiometers"]
+[16.97279930114746, 6.743837356567383, "Microsatellite Launch Date 18 Dec 2004"]
+[16.952423095703125, 6.764523983001709, "Microsatellite End of Life Date 11 Oct 2013"]
+[1.899818778038025, 8.602343559265137, "Subsystem Processor 32-bit"]
+[1.8993571996688843, 8.605223655700684, "Subsystem Solid-State Memory 300 MByte"]
+[1.893057107925415, 8.601083755493164, "Subsystem Data Bus MIL-STD-1553"]
+[1.9081523418426514, 8.58635425567627, "Subsystem Data Interface RS-422"]
+[1.880354881286621, 8.619966506958008, "Subsystem Data Rate Up to 900 kbit/s"]
+[-2.61930513381958, 9.663692474365234, "Power Source Power Output 220 W"]
+[-2.5876331329345703, 9.687148094177246, "Power Source Total Area 2 m2"]
+[-3.7112507820129395, 8.309289932250977, "Energy Storage Capacity 9 Ah"]
+[-3.25089168548584, 4.264514446258545, "Spacecraft Design Life 1 year"]
+[-2.9587690830230713, 4.474488735198975, "Spacecraft Mass 250 kg"]
+[2.6370270252227783, 14.344950675964355, "Optical Instrument Power Dissipation Varies"]
+[2.633589744567871, 14.352103233337402, "Optical Instrument Interface Temperature Requirement Lower than 15\u00baC"]
+[2.6471590995788574, 14.361039161682129, "Optical Instrument Interface Requirements Electrical, mechanical, data bus"]
+[-0.6918520927429199, 6.695850849151611, "Study Location Beijing and Hefei, China"]
+[-3.546840190887451, 7.142039775848389, "Data Retrieval Method Ground-based high spectral resolution solar absorption"]
+[-3.336113929748535, 7.357699871063232, "Data Assimilation System Location China"]
+[-0.6279392838478088, 6.722262859344482, "Study Location China"]
+[3.670168876647949, 17.640039443969727, "Projectile Testing Location Airbus DS test range"]
+[-0.4555913209915161, 6.743414402008057, "Test Rig Design Variables Projectile configuration, panel type, panel offset, chaser momentum"]
+[-3.099335193634033, 2.422692060470581, "Mission Functionality Demonstration Vision Based Navigation"]
+[1.0138154029846191, 0.7471222877502441, "Earth Observation Satellite Satellite Mass 1350 kg"]
+[0.9883788824081421, 0.7709393501281738, "Earth Observation Satellite Orbit Altitude 514 km"]
+[1.0199655294418335, 0.7672073245048523, "Earth Observation Satellite Formation Control Accuracy 10 m (1\u03c3)"]
+[-3.0950310230255127, 1.9825996160507202, "Space Mission Mango Satellite Mass 95 kg"]
+[-3.0986573696136475, 1.9437658786773682, "Space Mission Tango Satellite Mass 50 kg"]
+[-3.0945091247558594, 2.013155937194824, "Space Mission Orbit Altitude ~725 km"]
+[-3.0471224784851074, 2.027548313140869, "Space Mission Formation Control Accuracy Decimeter level"]
+[-3.084172010421753, 2.0434491634368896, "Space Mission Formation Control Accuracy Millimeter level"]
+[-3.0709586143493652, 2.0966880321502686, "Space Mission Formation Station Keeping 25 m to 250 m"]
+[-0.7426443696022034, 12.363625526428223, "Space Testing and Monitoring Device Performance Testing and monitoring of Single Event Upsets (SEUs), Multiple Bit Upsets (MBUs), Single Event Functional Interrupts (SEFIs) and Latch-Ups"]
+[0.11878452450037003, 7.180718421936035, "Experiment Purpose Probe phenomenon by performing satnav fixes in the midst of the ionosphere"]
+[-0.5382089018821716, 1.2340964078903198, "Satellite Orbit Path Through part of the Van Allen belts"]
+[6.353126049041748, 7.377803325653076, "Satellite Components Purpose Performing a radiation census of this segment of space"]
+[2.127603054046631, -2.5740668773651123, "Satellite Observation Sectors 26"]
+[4.434197902679443, -2.6877832412719727, "Satellite Sector Observation Duration At least 27 days"]
+[4.142492294311523, -2.7783827781677246, "Satellite Brightest Stars Observation Cadence 1-minute"]
+[3.9280972480773926, -2.684269905090332, "Satellite Full Frame Images Cadence 30-minute"]
+[4.271623611450195, -3.368007183074951, "Satellite Northern Hemisphere Mapping First year"]
+[3.725794553756714, -2.8330254554748535, "Satellite Southern Hemisphere Mapping Second year"]
+[-1.0695220232009888, 7.828978061676025, "Device Net Bit Rate 1800 Mbit/s"]
+[-4.3278045654296875, 7.396913051605225, "Data Transmission SNR Variations Limited to about 1 dB"]
+[-4.249012470245361, 7.3657708168029785, "Data Transmission FER 10-7"]
+[-2.3478143215179443, 9.188379287719727, "Electronic Power Conditioner Type Miniaturized pulsed EPC"]
+[-1.8816944360733032, 8.499038696289062, "Application Specific Integrated Circuit Function Controls both H and V TR modules and the PCPU"]
+[-1.8702596426010132, 8.871888160705566, "Tile Control Unit Function Controls all 24 TR modules on a tile"]
+[-1.876427412033081, 8.823933601379395, "Tile Control Unit Function Provides synchronization of the TR modules with a master reference"]
+[-1.958297848701477, 8.819246292114258, "Tile Control Unit Function Provides requisite amplitude and phase correction required on each TR module"]
+[-3.37229323387146, 7.451902866363525, "Data Processing Background Removal Flexible"]
+[-2.332005500793457, 9.123239517211914, "Power System Solar Array Size 1cm2"]
+[-2.363239288330078, 9.193562507629395, "Power System Solar Array Output Nearly 7 V"]
+[-2.3807437419891357, 9.19805908203125, "Power System Solar Array Current Up to 3 mA"]
+[-2.411522150039673, 9.214903831481934, "Power System Battery Type Manganese/lithium-ion rechargeable"]
+[-2.4319138526916504, 9.192696571350098, "Power System Battery Capacity 45 mAh"]
+[-2.336409330368042, 9.210585594177246, "Power System Battery Load Rating Continuous 100 \u03bcA"]
+[-2.3252522945404053, 9.156620025634766, "Power System Battery Backup Duration 90 days"]
+[1.785123586654663, -1.2844302654266357, "Satellite Imaging Geometry Varies"]
+[1.8988832235336304, -1.331769347190857, "Satellite Radar Parameters Resolution and sensitivity"]
+[-3.4349560737609863, 7.4127912521362305, "Automatic Identification System Information Provided Ship identity, location, size, speed, heading, cargo, destination"]
+[-0.2714637517929077, 10.225310325622559, "Long Range Identification and Tracking System Information Provided Ship identity, location"]
+[5.42270565032959, -4.384757995605469, "Satellite Launch Date December 2007"]
+[4.729427337646484, -2.537733793258667, "Satellite Years on Orbit 10 years"]
+[-7.603085517883301, 5.854758262634277, "Camera Type Medium Aperture"]
+[-7.567261695861816, 5.895448207855225, "Camera Image Transmission Date Aug. 9, 2009"]
+[-7.612774848937988, 5.857882022857666, "Camera Image Content Snapshot of the Palm Jebel Ali"]
+[-0.4052724242210388, 16.213289260864258, "Spectrograph IFOV cross-track 0.3\u00ba"]
+[-0.40636831521987915, 16.22018051147461, "Spectrograph IFOV along-track 0.18\u00ba - 11.84\u00ba"]
+[-0.4038379490375519, 16.2180118560791, "Spectrograph Pixel IFOV 10 km x 10 km"]
+[-0.40671390295028687, 16.212678909301758, "Spectrograph Pixel step period 0.112 s, 0.112 s"]
+[-0.4085773825645447, 16.21563148498535, "Spectrograph Spectral resolution (nm) 1.2, 1.9, 4.2"]
+[-0.40777817368507385, 16.215620040893555, "Spectrograph Sensitivity (counts/s/Rayleigh) 0.016, 0.120, 0.160, 0.160, 0.020"]
+[-0.4134630858898163, 16.239206314086914, "Spectrograph Data frame Date rate 3816 bit/s"]
+[-0.40878307819366455, 16.225574493408203, "Spectrograph Data frame period 22 s"]
+[-0.40723511576652527, 16.217374801635742, "Spectrograph Spatial pixels per frame 24, 8"]
+[-0.40313926339149475, 16.20855140686035, "Spectrograph Output word size 6 bits, 6 bits"]
+[7.266592025756836, 12.394283294677734, "Satellite Instrument Objective Collect comprehensive multispectral images of solar plasmas at temperatures from 104 - 107 K with 1 arcsecond spatial resolutions and excellent temporal resolution and continuity"]
+[7.263158798217773, 12.420108795166016, "Satellite Instrument Science Goal Explore the relation between diffusion of the surface magnetic fields and changes in heating and structure throughout the transition region and corona"]
+[1.3635553121566772, 7.0642595291137695, "Communication Equipment Size 9.1 m"]
+[-5.161788463592529, 7.7710394859313965, "Communication System Function Receive GRB and legacy GVAR downlinks"]
+[-5.1600542068481445, 7.801969051361084, "Communication System Data Path Primary path for L1b data from WCDAS to NSOF"]
+[-0.8669809103012085, 12.897336959838867, "Total Irradiance Monitor Number of Configurations 7"]
+[-0.9049043655395508, 13.01230525970459, "Spectral Irradiance Monitor Number of Configurations 13"]
+[2.9155795574188232, 23.06117057800293, "Instrument Operational Period 5 years"]
+[-1.0600727796554565, 13.195975303649902, "Total Solar Irradiance Measurement Range Outer boundaries of atmosphere"]
+[-1.0727629661560059, 13.165498733520508, "Spectral Solar Irradiance Measurement Range 200 \u2013 2400 nm"]
+[-0.19581486284732819, 9.23333740234375, "Thermal Pointing System Tracking The sun each orbit with a two-axis gimbal"]
+[2.7778143882751465, 22.59787368774414, "Instrument Retrieved Thermospheric Temperatures Unknown"]
+[1.0018001794815063, -4.388890266418457, "Satellite Mass \u22642480 kg"]
+[1.1333011388778687, -0.7209597229957581, "Satellite Size 2000 mm x 1720 mm x 2200 mm"]
+[-1.9194713830947876, 8.091005325317383, "System Accuracy \u2264\u00b11\u00ba (3\u03c3)"]
+[-1.9064950942993164, 8.109885215759277, "System Stability \u22640.005\u00ba/s"]
+[-1.8943395614624023, 8.066389083862305, "System Power 1466 W"]
+[-1.9712564945220947, 8.086092948913574, "System Modulation Mode BPSK"]
+[-1.9353994131088257, 8.106091499328613, "System Rate 6 Mbit/s"]
+[-1.9339408874511719, 8.105489730834961, "System Rate 3 Mbit/s"]
+[-1.9070653915405273, 8.084258079528809, "System Rate 1.5 Mbit/s"]
+[-1.9437164068222046, 8.134526252746582, "System Rate 750 kbit/s"]
+[-1.898242712020874, 8.140264511108398, "System Rate 12 Mbit/s"]
+[2.901568651199341, 22.080739974975586, "Instruments Purpose Measure air quality and detect global methane emissions"]
+[2.2290689945220947, -2.575366497039795, "Satellite Cost $26 million"]
+[2.8677480220794678, -1.0223891735076904, "Satellite Purpose Detect global methane emissions"]
+[2.307631015777588, -1.973544955253601, "Satellite Mission Control Centre Location New Zealand"]
+[3.080657482147217, -1.4837208986282349, "Satellite Mission Leader United States-based NGO Environmental Defense Fund (EDF) and its subsidiary MethaneSAT LLC"]
+[-13.807291030883789, -2.2814390659332275, "X-ray Telescope Sky Scanning Interval 6 months"]
+[-13.855997085571289, -2.1439456939697266, "X-ray Telescope Energy Band 0.6-1.0 keV"]
+[-13.871406555175781, -2.2314395904541016, "X-ray Telescope Bubble Size Several kiloparsecs (or up 50,000 light-years) across"]
+[-13.868287086486816, -2.218646764755249, "X-ray Telescope Halo Temperature Millions of degrees"]
+[-1.3364442586898804, 6.119555473327637, "Company Launch Date Jan. 10"]
+[-0.9457332491874695, 9.837462425231934, "Rocket Launch Date Jan. 6, 2014"]
+[-8.139751434326172, 8.82514476776123, "Electrical Power Subsystem Power Generation 7.2 W"]
+[-8.145602226257324, 8.827266693115234, "Electrical Power Subsystem Regulated Voltages +3.3 V, +4 V, +5 V, +5.5 V, \u00b1 12 V"]
+[-5.170042037963867, 7.938992023468018, "On-Board Communications Subsystem Bus Type Wireless CAN (Controller Area Network)"]
+[-5.141233921051025, 7.899415493011475, "On-Board Communications Subsystem Subsystem Type Internal wireless optical communications subsystem"]
+[8.491589546203613, 15.222229957580566, "Camera Mount Tracking Accuracy 7 arcsec"]
+[8.491929054260254, 15.222519874572754, "Camera Mount Maximum Integration Time 10 seconds"]
+[8.491671562194824, 15.222190856933594, "Camera Mount Best Ground Resolution 10 m/pixel"]
+[8.491766929626465, 15.222055435180664, "Camera Mount Tracking Range \u00b1 18\u00ba"]
+[8.491789817810059, 15.221881866455078, "Camera Mount Safety Compliance Human spaceflight safety for pressurized payloads"]
+[8.491600036621094, 15.221989631652832, "Camera Mount Operation Designed to be operated with one hand"]
+[-3.5154871940612793, 14.267651557922363, "Radio Plasma Imager Operating Voltage 3 kV"]
+[2.0356810092926025, -0.6558912992477417, "Satellite Transmitter Voltage < 10 kV"]
+[1.9880982637405396, -0.7123034596443176, "Satellite Transmitter Voltage 5 kV"]
+[0.42684391140937805, 12.144248008728027, "Compact Environmental Anomaly Sensor Measurement Capabilities Radiation dose, dose rate, surface dielectric charging, deep dielectric charging, and single event effects"]
+[0.466241717338562, 12.138482093811035, "Compact Environmental Anomaly Sensor Angular FOV Relatively large"]
+[0.4929896891117096, 12.040648460388184, "Compact Environmental Anomaly Sensor Mounting Location Exterior panel of the payload module"]
+[0.438818097114563, 12.069706916809082, "Compact Environmental Anomaly Sensor Change for DSX CEASE will capture and downlink the full dose spectra from each dosimeter"]
+[1.506892204284668, 21.220266342163086, "Instrument Total Mass 103 kg"]
+[1.6285405158996582, 23.217487335205078, "Instrument Power Consumption 100 W"]
+[-1.9013444185256958, 14.886521339416504, "Radiometer Device Type Visible and Infrared"]
+[4.915712356567383, -3.5923709869384766, "Satellite Operation Period From launch to the end of initial operation (March 2018)"]
+[5.137017250061035, -4.268669128417969, "Satellite RCS Stoppage Period 9 February to 7 March, 2018"]
+[4.196688175201416, -2.859647512435913, "Satellite Perigee Point Wait Time 15min"]
+[1.4856045246124268, -2.077587842941284, "Satellite Attitude Change Point D point"]
+[1.6552066802978516, -2.2849929332733154, "Satellite Control Phase Elliptical to circular"]
+[5.283007621765137, -4.421103000640869, "Satellite Launch Date May 2018"]
+[2.9133615493774414, -1.1992641687393188, "Satellite Mission Purpose Measuring changes in high-resolution monthly global models of Earth\u2019s gravitational field"]
+[-1.9324569702148438, 8.084702491760254, "System Purpose Commanding and monitoring the EDRS-A payload"]
+[-1.9277849197387695, 8.104942321777344, "System Number of Links per Day Up to 400"]
+[-1.9214547872543335, 8.094648361206055, "System Late Request Window Up to 45 minutes before execution"]
+[2.245750904083252, 23.18973731994629, "Instrument Frequency 1.41 GHz"]
+[2.199997663497925, 23.111251831054688, "Instrument Frequency 1.26 GHz"]
+[0.6242361068725586, 12.055033683776855, "Sensor Performance Continues to perform well"]
+[0.6384845972061157, 12.002123832702637, "Sensor Interruptions During much of the second half of 2012 there were interruptions in the precise geodetic pointing, and some safe hold events"]
+[2.7225074768066406, -3.250965118408203, "Satellite Communication System Data Transmission Speed 1.8 Gbit/s"]
+[2.6638786792755127, -3.20317006111145, "Satellite Communication System Data Relay Capacity 40 terabytes per day"]
+[5.349018096923828, -4.290390968322754, "SpaceDataHighway Relay Satellite Launch Year 2016"]
+[5.400760173797607, -4.193439483642578, "SpaceDataHighway Relay Satellite Launch Year 2019"]
+[1.880746603012085, -0.21529559791088104, "Radar Imaging Satellite Launch Date June 27, 2013"]
+[5.226180076599121, -4.4201812744140625, "Satellite Launch Date January 1, 2020"]
+[-0.7792181968688965, 11.632586479187012, "Detector Head Assembly Number of Channels 19"]
+[-0.7038690447807312, 11.722479820251465, "Detector Head Assembly Detector Element Size 10 km x 10 km"]
+[-0.8908196687698364, 11.591117858886719, "Detector Head Assembly IGFOV 280 \u00b5rad"]
+[-0.7323998212814331, 11.585578918457031, "Detector Head Assembly Footprint 10 km x 40 km"]
+[-0.8122960925102234, 11.594196319580078, "Detector Number of Detectors 4"]
+[-0.7679312825202942, 11.512127876281738, "Detector Redundancy Yes"]
+[1.157029151916504, -0.8766642808914185, "Satellite Structure Diameter 94 cm"]
+[0.9583864808082581, -4.358388900756836, "Satellite Structure Mass 91 kg"]
+[2.058985471725464, -2.7977139949798584, "Satellite Mirrors Quantity 1500"]
+[2.065363645553589, -2.7652063369750977, "Satellite Laser Retro-reflectors Quantity 31"]
+[2.1041643619537354, -0.6715501546859741, "Satellite Power Supply Integrated power supply (combined solar cells and thin film batteries)"]
+[-2.4782679080963135, 13.067099571228027, "Multispectral Imager Generation 3rd"]
+[-2.4688329696655273, 13.056449890136719, "Multispectral Imager Imaging Cycles Faster"]
+[-2.4630813598632812, 13.055660247802734, "Multispectral Imager Spatial Resolution Higher than the current imager generation of GOES-N to -P"]
+[0.7187009453773499, -4.127335548400879, "Satellite Launch Mass ~ 1990 kg"]
+[1.0137436389923096, -4.35174036026001, "Satellite Mass ~ 48 kg"]
+[0.9291190505027771, -4.391028881072998, "Satellite Mass ~ 7 kg"]
+[7.272021770477295, 12.401235580444336, "Satellite Instrument URL http://nsidc.org/data/docs/daac/ssmi_instrument.gd.html"]
+[2.9151792526245117, 21.914133071899414, "Instrument Purpose Examine the response of the upper atmosphere to forcing from the Sun, the magnetosphere and the lower atmosphere"]
+[1.972412347793579, -2.407011032104492, "Satellite Propulsion System Electric plasma propulsion system"]
+[2.5960731506347656, -1.9953323602676392, "Satellite Digital Transparent Processor (DTP) Increases payload flexibility and will provide customized bandwidth solutions to SES\u2019s customers"]
+[3.679168939590454, 22.943391799926758, "Instrument Integration Date May 23, 2017"]
+[-13.890856742858887, -2.2337846755981445, "X-ray Telescope Sky Image Depth 4 times deeper than the previous all-sky survey by the ROSAT telescope 30 years ago"]
+[-13.869144439697266, -2.225501775741577, "X-ray Telescope Number of Sources Around 10 times more sources than the previous all-sky survey"]
+[-13.843777656555176, -2.2567203044891357, "X-ray Telescope Source Types Active galactic nuclei, accreting supermassive black holes, clusters of galaxies, stars with strong, magnetically active hot coronae, X-ray binary stars containing neutron stars, black holes or white dwarves, and spectacular supernova remnants"]
+[-2.4836041927337646, 13.071903228759766, "Multispectral Imager Unknown Unknown"]
+[2.5899136066436768, 14.264822959899902, "Optical Instrument Diameter 60 cm"]
+[-1.0223114490509033, 7.684665679931641, "Redundant Devices Quantity 2"]
+[3.7166080474853516, 17.716875076293945, "Payload Interface Unit Function Provides the connection to the JEM-EF"]
+[2.8361048698425293, 22.0263671875, "Instrument Purpose Study the impact of clouds and aerosols on global energy balance and climate feedback mechanisms"]
+[2.782623052597046, 23.322450637817383, "Instrument Manufacturer L3Harris Technologies"]
+[2.8140342235565186, 22.371912002563477, "Instrument Type Imager"]
+[2.9868721961975098, 22.557462692260742, "Instrument Ground System Provider L3Harris Technologies"]
+[2.7071492671966553, -2.1213252544403076, "Satellite Operational Name GOES-18"]
+[2.735093355178833, -1.9469451904296875, "Satellite Operational Service GOES West"]
+[1.9048075675964355, 8.60045337677002, "Subsystem Mission Life 6 months"]
+[1.9096012115478516, 8.604780197143555, "Subsystem Reliability Exceeding 90%"]
+[1.5464951992034912, -2.413134813308716, "Satellite Orbit Elliptical orbit of 410 km x 1710 km"]
+[0.6913021206855774, -2.3265841007232666, "Satellite Inclination 68\u00ba"]
+[4.013829708099365, -2.8912181854248047, "Satellite Period 106 minutes"]
+[-0.8307752013206482, 11.583070755004883, "Detector Module Quantity 328"]
+[-0.8497519493103027, 11.610957145690918, "Detector Total Quantity 5248"]
+[-0.8007824420928955, 11.613506317138672, "Detector Length Range 0.8 m to 2.0 m"]
+[-0.8483497500419617, 11.621916770935059, "Detector Wall Material 72 \u00b5m kapton foil"]
+[-0.8464401960372925, 11.624676704406738, "Detector Sense Wires Material 30 \u00b5m gold plated tungsten"]
+[-3.5208559036254883, 7.385183811187744, "Data Acquisition System Part Quantity 2"]
+[-3.6079399585723877, 7.38888692855835, "Data Acquisition System Function Digitization of the signals from the straw tubes"]
+[1.2321748733520508, -1.5854487419128418, "Satellite Field of View 2232\u00ba x 2232\u00ba"]
+[2.1042540073394775, -2.715341567993164, "Satellite Number of Cameras 24, 18, 12 or 6"]
+[4.475852012634277, -2.6047205924987793, "Satellite Rotation Interval 3 months"]
+[-1.2173666954040527, 15.090558052062988, "Imaging multi-spectral radiometer Instrument Type Imaging multi-spectral radiometers (vis/IR)"]
+[-1.2197130918502808, 15.088306427001953, "Imaging multi-spectral radiometer Instrument Type Imaging multi-spectral radiometers (vis/IR)"]
+[1.0128397941589355, 0.7818782329559326, "Earth Observation Satellite Launch Date 17 August 2011"]
+[1.0215229988098145, 0.7764560580253601, "Earth Observation Satellite End of Life Date 28 August 2022"]
+[1.0221718549728394, 9.160663604736328, "Attitude Orbit Control Subsystem Pointing Accuracy 0.05\u00ba"]
+[1.0714051723480225, 9.125105857849121, "Attitude Orbit Control Subsystem Drift Rate 5.0 x 10 \u20135 \u00ba/s"]
+[1.0415505170822144, 9.14803409576416, "Attitude Orbit Control Subsystem Attitude Knowledge 0.02\u00ba"]
+[-1.501477599143982, 13.424788475036621, "Solar array Generating Capacity 2.2 kW"]
+[-3.062593698501587, 9.637853622436523, "NiH2 battery set Capacity 70 Ah"]
+[-3.7030727863311768, 6.885739326477051, "TT&C data Frequency S-band"]
+[3.7298545837402344, 17.702545166015625, "Payload data Frequency X-band"]
+[3.721449375152588, 17.705947875976562, "Payload data Transmission Rate 640 Mbit/s"]
+[-3.6675968170166016, 8.053170204162598, "Solid State Recorder Capacity 300 Gbit"]
+[0.9816736578941345, -4.366754055023193, "Satellite Mass ~ 200 kg"]
+[5.322608470916748, -2.1900787353515625, "Satellite Design Life 5 years"]
+[6.3440022468566895, 7.340996742248535, "Satellite Component Size 1.2 m in diameter, 1.35 m high"]
+[0.6471149325370789, 9.314437866210938, "Attitude Control Subsystem Pointing Knowledge Accuracy < 10 arcsec"]
+[0.6493422389030457, 9.312512397766113, "Attitude Control Subsystem Control Stability < 0.016 \u00ba/s"]
+[-8.130101203918457, 8.829240798950195, "Electric Power Subsystem Power > 330 W"]
+[-8.147637367248535, 8.830121040344238, "Electric Power Subsystem Battery Capacity 14.4 Ah"]
+[-5.470267295837402, 8.13758659362793, "Communication System Transmission Frequency S-band"]
+[-5.2336554527282715, 7.797070026397705, "Communication System Downlink Data Rate 9.6 or 38.4 kbit/s"]
+[-5.20032262802124, 7.757227897644043, "Communication System Uplink Data Rate 9.6 kbit/s"]
+[-5.173357963562012, 7.768329620361328, "Communication System Downlink Data Rate 30 Mbit/s"]
+[-0.8477600812911987, 0.1687900722026825, "Satellite System Function Calculate the orbit of the satellite with high accuracy"]
+[-0.8299287557601929, 0.15019287168979645, "Satellite System Function Perform the planning of the satellite orbit control"]
+[-0.839566171169281, 0.16536787152290344, "Satellite System Function Planning of the maintenance of the solar array paddle and the battery"]
+[-0.8207985162734985, 0.15615244209766388, "Satellite System Function Operation planning of each ground station"]
+[-3.3411922454833984, 7.483366966247559, "Data Processing Real Time Unknown"]
+[5.033788681030273, -4.583733081817627, "Satellite User Interaction Meeting Date Feb. 16-17, 2012"]
+[-4.390960693359375, 9.053837776184082, "Modulator Data Rate 800 Mbit/s"]
+[-4.39723539352417, 9.127155303955078, "Modulator Modulation Scheme QPSK"]
+[-4.4354448318481445, 9.166413307189941, "Modulator Frequency Bandwidth Allocation 375 MHz"]
+[2.8249120712280273, 22.872716903686523, "Instrument Operation Mode Nominal science mode"]
+[3.644056797027588, 22.956249237060547, "Instrument Commissioning Completion Date Aug. 24, 2011"]
+[1.8701273202896118, 22.100692749023438, "Instrument Final Orbit Altitude 657 km above Earth"]
+[2.1209657192230225, 22.699419021606445, "Instrument Spectral Bands Pan: 450-900 nm, MS: 450-520 (blue), 520-600 nm (green), 630-690 nm (red), 760-900 nm (NIR), SWIR: 1000-2400 nm (experimental)"]
+[1.7862905263900757, 22.18367576599121, "Instrument Spatial Resolution Pan = 2.5 m, MS = 10 m, SWIR = 20 m"]
+[1.6642521619796753, 21.92804527282715, "Instrument Swath Width 20 km x 640 km (one pass)"]
+[2.509023666381836, 22.49944496154785, "Instrument Data Quantization 8 bit (dynamic), 11 bit (total)"]
+[1.7750155925750732, 22.197498321533203, "Instrument Telescope Aperture Diameter 492 mm"]
+[1.8348859548568726, 22.21512222290039, "Instrument Telescope Aperture Length 985 mm"]
+[2.092346668243408, 22.354389190673828, "Instrument Instrument Mass < 41 kg (optics < 35 kg, electronics < 6 kg)"]
+[1.6845297813415527, 23.164228439331055, "Instrument Instrument Power < 69 W (peak power with all heaters on)"]
+[3.6650402545928955, -2.567030668258667, "Satellite Orbit Maneuver Frequency Once every 3 weeks"]
+[3.6607162952423096, -2.578885078430176, "Satellite Slew Maneuvers Frequency 150 times a month"]
+[2.0438711643218994, -2.578139305114746, "Satellite Collision Avoidance Maneuvers 2"]
+[2.1283419132232666, -2.6736865043640137, "Satellite Alternate Downlink Locations Up to four"]
+[-1.1065343618392944, 4.486663341522217, "Ground Station Downlink Capability S-band"]
+[-1.1512773036956787, 4.451852798461914, "Ground Station Downlink Capability X-band"]
+[-1.701433539390564, 5.323540210723877, "Mission Operations Center Functions Mission operations planning and design, Science and instrument operations support, Command planning, verification and uploads, Ground station interaction, Observatory health monitoring and housekeeping trending, Observatory navigation and orbit maintenance maneuver implementation"]
+[-1.6997623443603516, 5.330214023590088, "Mission Operations Center Responsible Organization CONAE"]
+[-1.675957202911377, 5.341305255889893, "Mission Operations Center Architecture An evolution of the proven design currently supporting SAC-C"]
+[2.200979709625244, -2.325653553009033, "Satellite Camera 4"]
+[-2.9780185222625732, 4.325580596923828, "Small Spacecraft Camera Unknown"]
+[-2.965508460998535, 4.321626663208008, "Small Spacecraft Earth-sun L-5 Lagrange point Distance One astronomical unit, or about 150 million kilometers"]
+[-6.639804840087891, 9.919238090515137, "Multi-beam Antennas Coverage Japan and south-east Asia"]
+[-6.979394912719727, 11.148046493530273, "Active Phased Array Antenna Coverage Global"]
+[2.414673089981079, -1.925612449645996, "Satellite Communication Modes Regenerative mode, bent pipe mode relay"]
+[-5.147890090942383, 8.229737281799316, "ATM Baseband Switching Paths Three paths"]
+[-3.0495545864105225, 20.136232376098633, "Band Pass Filters Paths Six paths"]
+[-1.9768857955932617, 8.582562446594238, "TX/RX IF switch matrixes Function Distribute the TDMA signals of each time slot to the beams"]
+[-4.509990692138672, 12.104872703552246, "Magnetometer Frequency Range 0 \u2013 8 Hz"]
+[-4.504989147186279, 12.10842514038086, "Magnetometer Accuracy \u00b1 0.1 nT"]
+[-4.547812461853027, 12.071791648864746, "Magnetometer Measurement Range 100-10000 nT"]
+[-4.509444713592529, 12.106860160827637, "Magnetometer Accuracy \u00b10.1 nT"]
+[-4.453834533691406, 12.14954948425293, "Magnetometer Mounting Location On the tip of the -Z boom"]
+[-1.8946647644042969, 14.891338348388672, "Optical Radiometer Mass 50 kg"]
+[-1.8676586151123047, 14.866148948669434, "Optical Radiometer Power 70 W"]
+[-1.8041054010391235, 14.888019561767578, "Optical Radiometer Data Rate 670 kbit/s"]
+[-1.729920506477356, 14.78824520111084, "Optical Radiometer Band 1 Bandwidth 0.402-0.422 \u00b5m"]
+[-1.7556036710739136, 14.835238456726074, "Optical Radiometer Band 1 SNR 9.103"]
+[-1.8023085594177246, 14.842127799987793, "Optical Radiometer Band 1 Max Radiance 13.94"]
+[6.299596309661865, 7.4400858879089355, "Satellite Component Design Requirements OSVW, TCI, Imagery SDR"]
+[-1.6902775764465332, 6.955105781555176, "Simulation Tool Predicted Performance OSVW across the wind speed range of 5 to 25 m/s"]
+[-1.6676584482192993, 6.94895076751709, "Simulation Tool Noise Equivalent Delta Temperature (NEDT) Unknown"]
+[-1.6601924896240234, 6.9694013595581055, "Simulation Tool Calibration Uncertainty Unknown"]
+[-1.3937336206436157, 6.931295871734619, "Model Margin on Wind Direction Minimum of 20%"]
+[-1.3765718936920166, 6.932924747467041, "Model Margin on Wind Speed Minimum of 70%"]
+[-0.46975642442703247, 5.8407301902771, "Unknown Resolution < 0.5 \u00b5rad"]
+[-0.4612375497817993, 5.825916767120361, "Unknown Position Jitter < 1 \u00b5rad rms"]
+[-0.4821764826774597, 5.853890895843506, "Unknown Velocity > 25\u00ba/s"]
+[-0.4887132942676544, 5.821556091308594, "Unknown Electric Power < 3 W"]
+[-0.4419192373752594, 5.807762145996094, "Unknown Mass < 300 g"]
+[-0.46837860345840454, 5.834582328796387, "Unknown Temperature Range -30\u00baC \u2264 T \u2264+70\u00baC"]
+[-0.4630497395992279, 5.837220668792725, "Unknown Vibration Design 150 g static, random 24.7 g rms"]
+[-0.4801276922225952, 5.868864059448242, "Unknown Radiation Environment GEO and LEO orbit"]
+[-0.45291316509246826, 5.833643913269043, "Unknown Lifetime 15 years"]
+[6.344217300415039, 7.394354343414307, "Satellite Component Purpose Observation"]
+[-5.3096089363098145, 2.83351731300354, "Telescope Mission Actionable refinement of ephemeris pathfinder"]
+[0.8035942316055298, 11.996230125427246, "Sensor Athermalized Yes"]
+[-2.616227388381958, 11.78632926940918, "Imager Temperature Measurement Laser beam wavelengths"]
+[-2.6674323081970215, 11.701298713684082, "Imager Temperature Measurement \u00b120oC"]
+[-2.6357266902923584, 11.682533264160156, "Imager Light Source Unit Pigtailed tunable laser"]
+[-2.6310224533081055, 11.692286491394043, "Imager Sensing Unit Two FBGs mounted onto a steel support"]
+[-2.6487793922424316, 11.681206703186035, "Imager Receiver Unit Pigtailed PIN InGaAs photodiode (model EPM605 from JDSU)"]
+[-2.6792919635772705, 11.6116943359375, "Imager Processing Unit PCB (Printed Circuit Board)"]
+[6.253167629241943, 7.4849443435668945, "Satellite Component Quantity 4 in cold redundancy"]
+[6.181558609008789, 7.545080661773682, "Satellite Component Quantity 4 in hot redundancy"]
+[1.8929314613342285, 10.69817066192627, "Imaging Device Anomaly Dark line appears in the images"]
+[2.544275999069214, -1.8845980167388916, "Satellite Functionality About 70% after 11 years"]
+[1.634572982788086, -1.8978394269943237, "Satellite Agility Reduced to ~50%"]
+[1.6247292757034302, -2.168506383895874, "Satellite Attitude Control Stabilized to the Sun pointing within 60\u00ba"]
+[-0.6095525622367859, 3.2203481197357178, "Delta Scuti Star Pulsation Patterns 55"]
+[-0.7447336316108704, 3.153118371963501, "Delta Scuti Star Observation Duration 27 days"]
+[-0.7720231413841248, 3.195233106613159, "Delta Scuti Star Pulsation Speed Sped up by 54,000 times"]
+[3.5842223167419434, -2.3197720050811768, "Satellite New Observing Strategy Full images every 10 minutes"]
+[0.5569873452186584, -1.4475347995758057, "Satellite Orbit Altitude 684 km"]
+[0.7611409425735474, -2.2296786308288574, "Satellite Orbit Inclination 98.1\u00ba"]
+[4.141663074493408, -2.8127434253692627, "Satellite Orbit Period 98.3 minutes"]
+[3.8715319633483887, -3.1663362979888916, "Satellite LTAN 10.30 hours"]
+[5.27374792098999, -4.412686824798584, "Satellite Launch Date December 2012"]
+[-5.444797515869141, 2.7926390171051025, "Telescope UV Detection Capabilities Yes"]
+[3.4785542488098145, 13.41429328918457, "Laser Transmitter Development Status In Progress"]
+[3.6304147243499756, 13.243996620178223, "Laser Type Low-mass, compact micro non-planar ring oscillator (m- NPRO) laser"]
+[3.4771430492401123, 10.55488395690918, "Amplifier Design Robust mechanical design based on fiber components"]
+[-1.2212384939193726, 8.590914726257324, "Component Purpose Core of the laser interferometry measurement system"]
+[3.5009236335754395, 13.484817504882812, "Laser System Unknown Unknown"]
+[-0.5231691598892212, 5.881988525390625, "Expertise Key to Gravitational Waves Study Unknown"]
+[-2.264310121536255, 7.319268703460693, "On-board Package Total Mass 17 kg"]
+[-2.239210605621338, 7.322766304016113, "On-board Package Power 20 W"]
+[-2.2650911808013916, 7.312374591827393, "On-board Package Size 385 x 280 x 210 mm"]
+[-2.257972478866577, 7.300912380218506, "On-board Package IFOV 125\u00ba centered on nadir"]
+[-2.219216823577881, 7.320284843444824, "On-board Package Data Rate 200 bit/s"]
+[-2.2622225284576416, 7.341585636138916, "On-board Package Duty Cycle 100%"]
+[-2.2470386028289795, 7.358184337615967, "On-board Package Thermal Operating Range -10-50\u00baC"]
+[4.711183547973633, -4.522771835327148, "Satellite Image Capture Date 13 August 2021"]
+[0.11484982818365097, 4.682478427886963, "Volcano Eruption Start Time Around 16:15 local time"]
+[0.05342712253332138, 4.660379409790039, "Volcano Gas and Ash Column Height Around 200 m"]
+[-1.9567301273345947, 8.029674530029297, "Irrigation System Description Equipment rotates around a central pivot and crops are watered with sprinklers"]
+[-2.2591707706451416, 2.879073143005371, "Space Observatory Launch Mass ~2650 kg"]
+[-2.183744430541992, 2.885854482650757, "Space Observatory Total Payload Mass 1160 kg"]
+[-13.88647174835205, -2.2544643878936768, "X-ray Telescope URL http://www.nustar.caltech.edu/news/nustar170131"]
+[-6.739924430847168, 10.004563331604004, "Navigation Antenna Frequency Bands E5 and E1-band"]
+[-6.705385208129883, 9.978682518005371, "Navigation Antenna Signal Path Separate for E5 and E1-band"]
+[-6.732654571533203, 9.994072914123535, "Navigation Antenna E5 to E1 Port Isolation Better than 20 dB"]
+[-6.732060432434082, 9.98868179321289, "Navigation Antenna E5 to E1 Port Isolation Higher than 40 dB"]
+[1.6731053590774536, 6.923475742340088, "Communication Device Flight Heritage Over 15 years"]
+[1.6846076250076294, 6.952774524688721, "Communication Device Ground Network Compatibility Tesat LCT DTE and the BridgeSat optical communications ground network"]
+[-5.260139465332031, 7.839396953582764, "Communication Node Positioning Over the Asia-Pacific (APAC) region by 2020"]
+[6.74517297744751, 6.952756881713867, "Satellite Component Unknown Unknown"]
+[6.734760761260986, 6.963975429534912, "Satellite Component Unknown Unknown"]
+[-1.1980135440826416, 3.0948572158813477, "Celestial Object Surface Temperature Millions of degrees"]
+[-1.1767873764038086, 3.081075668334961, "Celestial Object Mass About the same mass as our Sun"]
+[-1.1446021795272827, 3.0766162872314453, "Celestial Object Size About the size of a large city"]
+[-1.166451096534729, 3.0680770874023438, "Celestial Object Spinning Speed Thousands of miles per hour"]
+[-2.2675414085388184, 13.366233825683594, "Small Hyperspectral Sensor Development Date Unknown"]
+[-2.3290107250213623, 13.376472473144531, "Small Hyperspectral Sensor Symposium Date May 4-7, 2009"]
+[-2.3674817085266113, 13.322040557861328, "Small Hyperspectral Sensor Symposium Location Berlin, Germany"]
+[-2.975710868835449, 4.17279052734375, "Spacecraft Altitude Approximately 5800 km"]
+[-0.9699052572250366, 9.822081565856934, "Rocket Integration Partner Orion spaceflight vehicle"]
+[-3.1883301734924316, 4.934842586517334, "Space Launch System Purpose Carry astronauts to destinations beyond LEO"]
+[2.1752591133117676, -2.0808403491973877, "Satellite Signal Photons per Laser Shot 8.5 for strong beam, 2.1 for weak beam"]
+[-0.9793588519096375, 7.753746032714844, "Device Data Densities 46% of the expected ICESat-2 data densities"]
+[-3.644944429397583, 12.744715690612793, "Particle Detector Detected Events 17 billion cosmic ray events"]
+[-3.5937561988830566, 12.773819923400879, "Particle Detector Energy Range 100\u2019s of MeV to several TeV"]
+[-3.6424453258514404, 12.751355171203613, "Particle Detector Detection Rate About 50 million of cosmic rays/day"]
+[-3.6383211612701416, 12.759334564208984, "Particle Detector Control Center POCC (Payload Operation Control Center) from NASA/JSC, Houston"]
+[3.903719186782837, 8.977104187011719, "Space Shuttle Landing Time June 1, 2011, at 6:35 GMT"]
+[-3.1421308517456055, 1.705790638923645, "Satellite Mission Goal Enable more accurate specification and prediction of the state of the thermosphere"]
+[-3.169092893600464, 1.697076678276062, "Satellite Mission Source of Uncertainty Lack of understanding of the upper atmospheric response to energy input near the poles"]
+[-2.6838011741638184, 9.448341369628906, "Power Generation Cell Type Third generation Azur GaAs triple junction cells"]
+[-2.7268521785736084, 9.475140571594238, "Power Generation Cell Efficiency 28%"]
+[-2.827540874481201, 9.539874076843262, "Battery Charge Regulator Number of Regulators 12"]
+[-2.928375005722046, 9.550420761108398, "Battery Charge Regulator Solar Cell Sections Twelve solar cell sections in total on three solar panels"]
+[-3.708636999130249, 8.304306030273438, "Energy Storage Nominal Capacity 34.8 Ah"]
+[-0.24047866463661194, 10.251091003417969, "Tracking System Orbit Accuracy 3-10 cm radial distance"]
+[-0.25202569365501404, 10.26501178741455, "Tracking System Range Rate Accuracy 0.3 mm/s"]
+[-0.2610926926136017, 10.253837585449219, "Tracking System Components Receiver, ultra-stable oscillator, antenna"]
+[-0.13673189282417297, 9.077445983886719, "Navigation Equipment Frequency Bands L1 and L2"]
+[-0.15445315837860107, 9.075441360473633, "Navigation Equipment Measurement Accuracy < 10 m (95%, 3Drss)"]
+[-0.1333315670490265, 9.094282150268555, "Navigation Equipment Signal L1"]
+[-0.1424577832221985, 9.120072364807129, "Navigation Equipment Algorithm Estimate of ionospheric delay and its change"]
+[-1.9978952407836914, 7.539880752563477, "Hardware Provides Structural, electrical, and C&DH interfaces"]
+[-0.5372811555862427, 8.296181678771973, "Support Structure Components Upper USS-02 Assembly, Vacuum Case Assembly, Lower USS-02 Assembly, Keel Assembly, passive Payload Attach System (PAS) Assembly/Umbilical Mechanism Assembly (UMA)"]
+[-0.5493556261062622, 8.281882286071777, "Support Structure Attachment Space Shuttle Orbiter"]
+[-3.1860504150390625, 7.599843502044678, "Data Processing Unit Interface VCU (Video Compression Unit)"]
+[-3.1629810333251953, 7.614182472229004, "Data Processing Unit Interface PDICs (Payload Data Interface Controllers)"]
+[-3.1751468181610107, 7.578317642211914, "Data Processing Unit Memory Module FMM (Flash Memory Module)"]
+[-3.184478998184204, 7.603658199310303, "Data Processing Unit Memory Module SMM (SDR-SDRAM memory module)"]
+[-3.178104877471924, 7.57796573638916, "Data Processing Unit Memory Module TFGs (Transfer Frame Generators)"]
+[-3.171980381011963, 7.590534210205078, "Data Processing Unit Controller Memory System Supervisor"]
+[6.311927795410156, 7.4327712059021, "Satellite Component Phase Data Number 4,096"]
+[-0.0007631767075508833, -1.98484206199646, "Satellite Operation Beam Direction Pointing Period 2 ms"]
+[6.349806308746338, 7.432016849517822, "Satellite Component Phase Data Memorized"]
+[2.2616536617279053, -2.512647867202759, "Satellite Spectral Bands 13"]
+[1.555994987487793, -1.245224118232727, "Satellite Spectral Bands Resolution 10 to 60 m"]
+[1.4798989295959473, -1.1009206771850586, "Satellite Bands Resolution 10 m"]
+[1.4889434576034546, -1.133522868156433, "Satellite Bands Resolution 20 m"]
+[1.4873037338256836, -1.1714297533035278, "Satellite Bands Resolution 60 m"]
+[2.1951630115509033, -2.540538787841797, "Satellite Bands in the \u2018red edge\u2019 3"]
+[2.8482494354248047, 22.45428466796875, "Instrument Type High resolution optical imagers"]
+[5.263649940490723, -4.423137664794922, "Satellite Launch Date 23 June 2015"]
+[5.041311264038086, -4.089412212371826, "Satellite End of Life Date 2038"]
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+[-0.7020886540412903, 8.33117389678955, "Mechanism Function Directs the laser at the ground below and has fine control over where the laser is pointing"]
+[-0.671730101108551, 8.39957332611084, "Mechanism Connection Connected with components on the instrument's telescope receiver"]
+[-0.5541475415229797, 8.425965309143066, "Mechanism Goal Automatically point the lasers at the exact spot on the ground where the telescope is observing"]
+[-2.0617289543151855, 6.9477434158325195, "Enterprise Management Function Supervising the overall systems and networks of the core GS"]
+[-2.1411445140838623, 6.848433494567871, "Enterprise Management Function Monitor, report, and enable an operator response to anomalous conditions"]
+[-0.8212725520133972, 6.1612772941589355, "Website URL https://earthobservatory.nasa.gov/images"]
+[-1.3436583280563354, 6.201183319091797, "Organization URL https://www.nasa.gov/feature/jpl/nasa-maps-surface-changes-from-california-quakes"]
+[2.959184169769287, -1.9958146810531616, "Satellite Mission Status Unknown"]
+[0.26610222458839417, 15.052018165588379, "Analyzers FOV 30\u00ba x 2\u00ba"]
+[0.21945470571517944, 15.083136558532715, "Analyzers Angular Pixels 15"]
+[0.2556712329387665, 15.043346405029297, "Analyzers Energy Distribution Steps 20"]
+[0.19407965242862701, 15.103241920471191, "Analyzers Cross-Track Speed ~2 km/s"]
+[0.26365014910697937, 15.006424903869629, "Analyzers Slit Half Height 1\u00ba"]
+[0.22694188356399536, 15.035792350769043, "Analyzers FOV 15\u00ba"]
+[6.367717266082764, 7.367428779602051, "Satellite Component Purpose Alignment of two formation-flying satellites"]
+[-3.220762252807617, 1.7243638038635254, "Satellite Mission Conference Presentation Date March 13-15, 2013"]
+[-1.1737990379333496, 6.020222187042236, "Conference Date May 29-31, 2013"]
+[11.271327018737793, 5.537145614624023, "CubeSat Launch Date 6 December 2015"]
+[11.241305351257324, 5.477346420288086, "CubeSat Mission Status Mission complete"]
+[2.836432933807373, -1.8034683465957642, "Satellite Mission Requirements and Specifications Unknown"]
+[2.578889846801758, -3.9297919273376465, "Satellite URL http://global.jaxa.jp/projects/sat/gosat2/"]
+[5.241837501525879, -4.544625282287598, "Satellite Release Date Dec. 12, 2013"]
+[0.5426360368728638, 11.915630340576172, "Sensor Function Measure Earth's magnetic field"]
+[0.5702693462371826, 12.104889869689941, "Sensor Data Contribution Update the IGRF model"]
+[0.5883941650390625, 12.064974784851074, "Sensor Contribution Improved understanding of ionospheric and magnetospheric current systems"]
+[1.9018877744674683, 10.719801902770996, "Imaging Device Information Delivery Target distance"]
+[6.297287464141846, 7.443984508514404, "Satellite Component Measurement Target distance"]
+[-0.6011888980865479, 7.383554935455322, "Demonstration Device Target Structural panels on old, large satellites"]
+[2.926129102706909, -2.085900068283081, "Satellite Product Description Unknown"]
+[2.718151092529297, -1.8751739263534546, "Satellite Examples of InSAR and other land applications Unknown"]
+[2.949402332305908, -1.7904212474822998, "Satellite Mission Management Unknown"]
+[-6.68817663192749, 9.986909866333008, "Antenna Polarization RHCP (Right Hand Circular Polarized)"]
+[-6.678986549377441, 9.95781421661377, "Antenna Frequency Bands L1, L2, L5, E5, E6 and E1"]
+[-3.9393303394317627, 8.54015827178955, "Signal Simulator Components RF constellation signal simulator"]
+[-1.093276023864746, 7.677691459655762, "Device Design Confirmed"]
+[-1.3915297985076904, 6.7888031005859375, "Development Model Unknown Unknown"]
+[-0.4870463013648987, 5.850234508514404, "Unknown Unknown Unknown"]
+[0.7807276844978333, 12.080078125, "Sensor Quantity 6"]
+[-2.7735259532928467, 7.914551258087158, "Processor Module CPU TSC695F"]
+[-1.9073784351348877, 6.908996105194092, "Software Function Performs precision attitude determination"]
+[0.11613820493221283, 7.165635108947754, "Experiment URL http://setas-www.larc.nasa.gov/mpid/mpid.html"]
+[1.310869812965393, -1.1126809120178223, "Small Satellite Manufacturer General Dynamics"]
+[5.834173679351807, 14.375242233276367, "Transponder URL http://www.nrl.navy.mil/pao/pressRelease.php?Y=2000&R=54-00r"]
+[-0.8610809445381165, 6.159395217895508, "Website URL http://reentrynews.aero.org/26414.html"]
+[-0.4369496703147888, 15.77068042755127, "FUV Imaging Spectrograph Channels 2"]
+[-0.414810448884964, 15.792119026184082, "FUV Imaging Spectrograph Cadence 30 minutes"]
+[-0.4217097759246826, 15.631757736206055, "FUV Imaging Spectrograph Wavelength Range 132 to 162 nm"]
+[0.24153533577919006, 11.545464515686035, "Sensor System Sensor Units 2"]
+[0.29245802760124207, 11.64644718170166, "Sensor System Measurement Type Impact momentum detection, penetration measurement, impact plasma detection"]
+[0.2925816774368286, 11.712323188781738, "Sensor System Measurement Continuous, in situ measurement of individual impact events"]
+[0.2755621075630188, 11.602398872375488, "Sensor System Data Tagging Time tag and spin phase tag"]
+[0.26393797993659973, 11.55085277557373, "Sensor System Spin Phase Derivation Using an analogue sun sensor (solar cell) mounted on the +Y face sensor"]
+[3.116760730743408, -2.3491744995117188, "Satellite Launch Date Unknown"]
+[2.546873092651367, -1.1494719982147217, "Satellite Data Usage Improve global hydrological science"]
+[2.2793843746185303, -1.6821774244308472, "Satellite Challenge Insufficient resolutions of the instruments"]
+[0.9388846158981323, -4.402092933654785, "Satellite Mass 10.165 kg"]
+[1.163230538368225, -0.7319122552871704, "Satellite Stowed Dimensions 239 mm x 116 mm x 366 mm"]
+[2.0754244327545166, -0.5688977837562561, "Satellite Power Generation 48 W"]
+[2.0061490535736084, -0.8266200423240662, "Satellite Energy Storage 52.7 Whr"]
+[2.699164390563965, -2.343132734298706, "Satellite Telecom Frequency S-band"]
+[2.668449878692627, -2.721457004547119, "Satellite Uplink Data Rate 32 kbit/s"]
+[2.663909912109375, -2.7428247928619385, "Satellite Downlink Data Rate 1 Mbit/s"]
+[2.5349109172821045, -2.0349292755126953, "Satellite Processor Xilinx Virtex 4FX / PowerPC405"]
+[2.55629563331604, -2.437654495239258, "Satellite Onboard Storage 14.5 GB"]
+[-4.503263473510742, 12.114215850830078, "Magnetometer Angular Resolution 1 arcsec"]
+[-4.5108795166015625, 12.10739803314209, "Magnetometer Absolute Measurement Error < 1 nT"]
+[-4.505917549133301, 12.105733871459961, "Magnetometer Dynamic Range \u00b165,536 nT"]
+[-4.50869607925415, 12.10984992980957, "Magnetometer Resolution < 0.25 nT"]
+[-4.493410110473633, 12.114981651306152, "Magnetometer Sampling Rate 100 vector samples/s in burst mode over polar latitudes"]
+[-4.500699520111084, 12.110325813293457, "Magnetometer Sensor Mass 300 g"]
+[-4.501396656036377, 12.114212989807129, "Magnetometer Instrument Mass 2.1 kg"]
+[-4.50325870513916, 12.111065864562988, "Magnetometer Power Consumption 1.1 W"]
+[2.5123157501220703, -1.6636979579925537, "Satellite Payloads ISUAL (Imager of Sprites and Upper Atmospheric Lightning), RSI (Remote Sensing Instrument)"]
+[3.7008068561553955, 17.65118408203125, "Scientific Payload Operation Alternately in eclipsed and sunlight times"]
+[0.9865294098854065, 0.7907285094261169, "Earth Observation Payload Operation Alternately in eclipsed and sunlight times"]
+[5.311798572540283, -2.1968088150024414, "Satellite Design Life 5 years"]
+[4.488084316253662, -2.458995819091797, "Satellite On-Orbit Operations Over 11 years"]
+[1.936325192451477, -1.2598415613174438, "Satellite Imagery Coverage ~8 times the land area of the Earth"]
+[2.72344970703125, -1.2180424928665161, "Satellite Daily Revisit Capability Significant and very useful for post disaster assessment and environmental monitoring"]
+[-3.826730251312256, 3.7057697772979736, "Sample Fetch Rover Function Collect Martian samples"]
+[-0.6560287475585938, 1.3212569952011108, "Earth Return Orbiter Mission Duration 5 years"]
+[-0.6574825644493103, 1.3140532970428467, "Earth Return Orbiter Manufacturer Airbus"]
+[-0.6780206561088562, 1.3293402194976807, "Earth Return Orbiter Mission Bring samples back to Earth from Mars"]
+[-4.931121826171875, 9.76550579071045, "Receiver Frequency L1/L2 code"]
+[-1.2095545530319214, 6.967831134796143, "Assembly Quantity 3"]
+[-1.5738208293914795, 8.19990348815918, "Unit Quantity 2"]
+[0.7139301896095276, 11.971059799194336, "Sensors Purpose Earth magnetic field information"]
+[0.7248919606208801, 11.956048965454102, "Sensors Purpose Coarse Earth and Sun direction determination"]
+[-0.625015377998352, 8.5798921585083, "Reaction Wheels Quantity 4"]
+[-1.345687747001648, 9.364288330078125, "Torquers Quantity 3"]
+[-1.5984737873077393, 9.679152488708496, "Propulsion System Thrust 1 N"]
+[0.7128217220306396, -4.133615970611572, "Satellite Launch Mass 620 kg"]
+[1.1135495901107788, -0.6729255318641663, "Satellite Dimensions 150 cm x 180 cm x 185 cm"]
+[5.075468063354492, -2.3222804069519043, "Satellite Design Lifetime Three years"]
+[2.0765573978424072, -2.3673934936523438, "Satellite Propulsion System Four 1N hydrazine thrusters with 10 kg of propellant on board"]
+[2.586768627166748, -2.1993408203125, "Satellite TT&C Subsystem S-band link"]
+[2.6622161865234375, -2.708577871322632, "Satellite Uplink Data Rate 2 kbit/s"]
+[2.6873652935028076, -2.7204723358154297, "Satellite Downlink Data Rate 8.192 kbit/s"]
+[-1.624646782875061, 9.703022956848145, "Electric Propulsion System \u0394V 1.2 km/s-1"]
+[-1.6605744361877441, 9.741395950317383, "Electric Propulsion System Trajectory Low energy manifold"]
+[2.931831121444702, -1.571176290512085, "Satellite Mission Type Science"]
+[7.289340496063232, 12.409961700439453, "Satellite Instrument Wavelength 308.68 nm"]
+[7.269465923309326, 12.396586418151855, "Satellite Instrument Albedo cal constant 0.093 steradian -1"]
+[7.285885334014893, 12.408740043640137, "Satellite Instrument Adjustment factor 1.000"]
+[2.7118782997131348, 22.194862365722656, "Instrument Photo Image credit: NASA"]
+[-0.25739479064941406, 10.218302726745605, "Tracking System Operation Mode Cooperative tracking, non-cooperative tracking"]
+[-0.2661459743976593, 10.266209602355957, "Tracking System Disturbance Source Short-lived glints from the target"]
+[-0.2377767115831375, 10.297065734863281, "Tracking System Glint Handling Special filter attempts to recover optical information from the non-affected parts of the image"]
+[-0.2560557425022125, 10.227523803710938, "Tracking System Image Processing If the glint is massive, the image will be suppressed from further processing"]
+[-0.23422260582447052, 10.254587173461914, "Tracking System Match Process Equipped with a suite of filters, testing the match between the measured and the reference target model"]
+[1.0190613269805908, -4.428633689880371, "Satellite Mass 812 kg"]
+[-3.262857437133789, 5.42280912399292, "Launch Vehicle Type Liquid-propellant intercontinental ballistic missile"]
+[-0.937781572341919, 9.67934799194336, "Upper Stage Propellant Solid-propellant"]
+[0.5587410926818848, -1.4589923620224, "Satellite Orbit Altitude 833 km"]
+[0.07614319026470184, 7.244123935699463, "Experiment Device Flight Hard Drive Data Recovery Successful"]
+[0.08475745469331741, 7.188783168792725, "Experiment Unknown Unknown"]
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+[-3.0195653438568115, 4.173708915710449, "Spacecraft Maneuver Sinusoidal about 1\u00b0"]
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+[2.3540823459625244, 22.147247314453125, "Instrument Calibration Spectrometric calibration, Radiometric calibration"]
+[-8.593859672546387, 13.613348960876465, "Parameter Date March 21, 2021"]
+[-8.532087326049805, 13.732430458068848, "Parameter Extent 14.77 million km2 (5.70 million square miles)"]
+[-8.625943183898926, 13.810056686401367, "Parameter Rank Seventh-lowest in the 43-year satellite record"]
+[1.6316128969192505, -1.0762317180633545, "Satellite Measurement Arctic Snow Depth and Sea Ice Thickness"]
+[1.939294695854187, -2.19474196434021, "Satellite Volume Volume125"]
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+[4.930600643157959, -4.349775314331055, "Satellite Publication Date 10 March 2020"]
+[2.6408209800720215, -3.8107872009277344, "Satellite DOI 10.1029/2019JC016008"]
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+[-0.5021987557411194, 5.879039764404297, "Unknown Value 0.2 K"]
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+[-0.49307963252067566, 5.858441352844238, "Unknown Value 0.2 K"]
+[-0.4561140537261963, 5.857660293579102, "Unknown Temperature Range 200-320K"]
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+[-5.386570453643799, 9.01179027557373, "Software Defined Radio Information Received Aircraft identification, position, altitude, and intent"]
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+[-0.11206050217151642, 15.539782524108887, "Spectrometer Max Radiance 1000"]
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+[11.271931648254395, 5.5033159255981445, "CubeSat Detection Type Marginal"]
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+[-3.1460065841674805, 1.7014316320419312, "Satellite Mission Monitoring Changes in ice mass"]
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+[-3.1498348712921143, 1.779618501663208, "Satellite Mission Management JPL"]
+[1.5189374685287476, -1.152109980583191, "Satellite Imagery Resolution 2m in Pan, 4 m MS"]
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+[2.0830447673797607, -2.7459912300109863, "Satellite Number of Targets 307 in northern polar areas, 37 in Antarctic areas"]
+[3.431429862976074, 13.445435523986816, "Laser Communication Terminal IOV Activities LCT self-test, IOV with an OGS Optical Ground Station, IOV with LEO user satellite"]
+[3.488036870956421, 13.42774772644043, "Laser Communication Terminal Ground Station ESA\u2019s OGS on Tenerife Island (Spain), DLR\u2019s mobile OGS"]
+[3.4520771503448486, 13.409427642822266, "Laser Communication Terminal User Satellite LEO Sentinel-1A/-2A satellites"]
+[-6.726839542388916, 10.002490043640137, "Antenna Material Aluminum alloy"]
+[-6.7550578117370605, 10.022083282470703, "Antenna Manufacturer SENER Aeroespacial"]
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+[3.6479225158691406, 22.941072463989258, "Instrument Review Date Jan. 8, 2013"]
+[-0.814924418926239, 12.637720108032227, "Radiation Experiment Purpose Investigating how best to safeguard the health of America's future astronauts"]
+[-0.8426041603088379, 12.538357734680176, "Radiation Experiment Design Competition Duration One year"]
+[-0.8499419689178467, 12.57441520690918, "Radiation Experiment Winning Team Governor's School for Science and Technology in Hampton, Va"]
+[-0.8589428663253784, 12.55416202545166, "Radiation Experiment Goal Build and test designs for shields to minimize radiation exposure and damaging human health effects inside NASA's new Orion spacecraft"]
+[0.6692099571228027, 11.009875297546387, "Imaging Sensor Band Count 6"]
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+[-2.651155471801758, 11.672103881835938, "Imager Channel SWIR"]
+[-2.7676823139190674, 14.181910514831543, "Sounder Data Collection Vertical temperature and moisture profile"]
+[-0.8228787779808044, 11.598523139953613, "Filters Spectral Cross-Talk Minimization Masks"]
+[-1.971761703491211, 6.381778240203857, "Focal Plane Assembly Manufacturer e2v (UK)"]
+[-2.0722756385803223, 6.332164764404297, "Focal Plane Assembly Dynamic Range Optimization Mastered"]
+[-2.0717382431030273, 6.336442470550537, "Focal Plane Assembly Power Consumption < 1 watt"]
+[-0.8214640021324158, 11.6256103515625, "Detector Number of Pixels 7000 pixels for the panchromatic band"]
+[-0.7495127320289612, 11.682987213134766, "Detector Number of Pixels Four lines of 1750 pixels for the MS (multispectral) bands"]
+[-0.8198699951171875, 11.605230331420898, "Detector Characteristics High MTF and high quantum efficiency"]
+[0.7432926297187805, -1.2292449474334717, "Earth Terminal Antenna Diameter 45 cm"]
+[0.8174290657043457, -1.123565912246704, "Earth Terminal Antenna Diameter 120 cm"]
+[-6.6254353523254395, 9.937751770019531, "Antenna System Data Rate 1.2 Gbit/s"]
+[-6.615200042724609, 9.914470672607422, "Antenna System Number of Beams 19"]
+[-6.641448020935059, 9.940224647521973, "Antenna System Number of Beams aiming toward Japan 12"]
+[-6.6482720375061035, 9.94383430480957, "Antenna System Number of Beams aiming toward Asia/Pacific 7"]
+[4.864495754241943, -4.479097366333008, "Satellite Image Acquisition Date Feb. 10, 2016"]
+[0.4519769847393036, 4.513796329498291, "Environmental Phenomenon Indicator of Anthropogenic Stressors and Climate Change Impacts Provides indications of anthropogenic stressors and climate change impacts"]
+[0.43311595916748047, 4.525863170623779, "Environmental Phenomenon Indicator of Future Reef State May be a key determinant of future reef state"]
+[3.4737708568573, 10.552565574645996, "Amplifier Chirped Pulse Duration 20 \u00b5s"]
+[-4.271152496337891, 8.84652328491211, "Signal Generator Bandwidths 225, 75, 37.5 and 18.75 MHz"]
+[-4.26423454284668, 8.855117797851562, "Signal Generator Chirped Carrier Frequency 5.35 GHz"]
+[-2.0516958236694336, 12.617765426635742, "Solar Ultraviolet Imager Observation Spectrum Extreme ultraviolet"]
+[5.286724090576172, -4.333591938018799, "Satellite Launch Date March 1, 2022"]
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+[-2.0145370960235596, 12.646212577819824, "Solar Ultraviolet Imager CME Capture Date July 10, 2022"]
+[-3.869688034057617, 7.955301761627197, "Data Storage Storage Capacity 2400 Gbit"]
+[-3.8503365516662598, 7.892696857452393, "Data Storage Input Data Rate 2 x 540 Mbit/s"]
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+[-3.8567960262298584, 7.919433116912842, "Data Storage Size L: 302 x W: 345 x H: 240 mm"]
+[-3.8749501705169678, 7.960023403167725, "Data Storage Power Consumption < 35 W"]
+[-3.863203763961792, 7.925229549407959, "Data Storage Data Formatting Rate 2 x 280 Mbit/s"]
+[-3.859712839126587, 7.935202121734619, "Data Storage Lifetime 7.5 years"]
+[-6.787505626678467, 10.056180953979492, "Antenna Gain 23 dBiC"]
+[-1.8406246900558472, 8.783991813659668, "Controller Tracking Software Gpredict"]
+[-6.6854753494262695, 9.959774017333984, "Antenna Polarisation RHCP or LHCP"]
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+[3.7143099308013916, 22.9777774810791, "Instrument Launch Date 28 Jan 2018"]
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+[-5.091434955596924, 8.049263954162598, "Communication Module Operating Frequency S-band"]
+[1.5813243389129639, -2.36446475982666, "Satellite Orbit Type Circular MEO"]
+[0.7415876388549805, -1.1680296659469604, "Satellite Altitude 5893 km"]
+[0.8183286190032959, -2.3064401149749756, "Satellite Eccentricity 0-0.0025"]
+[0.6759932041168213, -2.343329906463623, "Satellite Inclination 70.16\u00ba"]
+[-4.391976833343506, 9.145244598388672, "Modulator Development Test Date June 5-12, 2011"]
+[2.3569607734680176, 22.200576782226562, "Attitude Reference Instrument Precision Few arcseconds"]
+[-8.017809867858887, 11.658686637878418, "CCD Star Imager Resolution 6 arcsec or less"]
+[-4.499429225921631, 12.111952781677246, "Magnetometer Pointing Vector Determined by CCD star imager"]
+[5.021080493927002, -4.396541595458984, "Satellite Mission Date June 28-July 2, 2010"]
+[0.9340618252754211, 0.8750007152557373, "European Earth Observation Programme New Name Announcement Date Dec. 12, 2012"]
+[4.96635627746582, -4.515475749969482, "Satellite Bulletin Publication Date May 11, 2015"]
+[-2.848961353302002, 9.520608901977539, "Battery Charge Regulators Malfunction Detected"]
+[-7.556916236877441, 5.895381927490234, "Camera Detector Design CMOS"]
+[-7.541262626647949, 5.899284839630127, "Camera Objective Study the degradation of lenses in the space environment"]
+[-0.7798803448677063, 8.841473579406738, "Thermal Control Type Passive"]
+[-1.561890721321106, 9.611076354980469, "Propulsion Type Monopropellant hydrazine"]
+[-1.5486706495285034, 9.614049911499023, "Propulsion Number of Thrusters 8"]
+[0.47111016511917114, 9.37793254852295, "Attitude Control Method Three-axis stabilized"]
+[0.5280584692955017, 9.352663040161133, "Attitude Control Capability 0.04\u00ba (3\u03c3)"]
+[0.49883919954299927, 9.365046501159668, "Attitude Control Knowledge 0.002\u00ba (3\u03c3)"]
+[-3.7997257709503174, 7.93248176574707, "Onboard Data Storage Type Mass memory"]
+[-3.8311517238616943, 7.929477691650391, "Onboard Data Storage Capacity 768 Mbit"]
+[-2.5036213397979736, 9.433374404907227, "Power Array Type Fixed, 3 panels, 1 body"]
+[-1.496902346611023, 13.423582077026367, "Solar Array Size 5.2 m 2"]
+[-1.4074690341949463, 13.356884002685547, "Solar Cell Type Multi-junction GaAs"]
+[-1.4370224475860596, 13.360843658447266, "Solar Cell Efficiency 27%"]
+[-2.691617488861084, 9.427176475524902, "Power Generation Beginning of Life 1.6 kW"]
+[-2.6559107303619385, 9.392961502075195, "Power Generation End of Life 1.48 kW"]
+[-3.08389949798584, 9.644336700439453, "Battery Type NiCd"]
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+[-3.828977584838867, 6.851547718048096, "Data Collection Platform Transmission Duration About 1 minute"]
+[-3.8266892433166504, 6.852753639221191, "Data Collection Platform Message Format Elements Unmodulated carrier for 5 seconds, 250-bit preamble, 15-bit synchronization word, DCP address, Data field, 31-bit End of Transmission (EOT) sequence"]
+[-3.837170124053955, 6.872072696685791, "Data Collection Platform RF Uplink Frequency Between 402.001 and 402.199 MHz"]
+[-3.82641863822937, 6.853970527648926, "Data Collection Platform Number of International Channels Up to 33"]
+[-3.8930232524871826, 6.859738349914551, "Data Collection Platform Number of Regional Channels Up to 33"]
+[-3.8473105430603027, 6.900916576385498, "Data Collection Platform Modulation Index 60o"]
+[1.1509891748428345, -1.9741714000701904, "Satellite Primary Coverage Location 0o location over the equator"]
+[1.0686278343200684, -1.9924217462539673, "Satellite Backup Location 63o E over the Indian Ocean"]
+[1.0163646936416626, -2.069577693939209, "Satellite Repositioned Location 50o (75o W in Feb. 1993)"]
+[-3.0444071292877197, 4.251375675201416, "Spacecraft Spin Configuration Dual-spin at 100 rpm"]
+[-3.025798797607422, 4.318511486053467, "Spacecraft Diameter 2.10 m"]
+[-2.945152521133423, 4.3693528175354, "Spacecraft Length 3.195 m"]
+[-3.0221846103668213, 4.319466590881348, "Spacecraft Solar Panels Six"]
+[-3.0163705348968506, 4.321925163269043, "Spacecraft Solar Panels More than 8000 cells"]
+[-3.0263426303863525, 4.3854522705078125, "Spacecraft Power Generation 200 W average"]
+[2.5025999546051025, -1.2422817945480347, "Satellite Data Collection Oceanic circulation, tides, El Ni\u00f1o, La Ni\u00f1a, Pacific Decadal Oscillation, ocean floor topography"]
+[5.166804790496826, -4.3015947341918945, "Satellite Mission Completion Date August 1995"]
+[-1.9733513593673706, 6.938488483428955, "Software System Configuration Easily configurable and customized"]
+[-1.6058499813079834, 4.088100433349609, "Ground Segment Location Brazil and China"]
+[0.5860030651092529, 4.683071613311768, "Phenomenon Properties Provide information on the properties of magnetopause reconnection"]
+[0.5681660771369934, 4.675408363342285, "Phenomenon Evidence A single steady ion dispersion in the cusp may be evidence for a single steady reconnecting separator at the dayside magnetopause"]
+[0.5548220276832581, 4.651628494262695, "Phenomenon Evidence Multiple ion dispersions observed within a single spacecraft pass through the cusp have been provided as evidence for pulsed magnetopause reconnection"]
+[0.5686756372451782, 4.645848751068115, "Phenomenon Evidence Multiple overlapping dispersions have also been presented as evidence for multiple discontinuous reconnection sites along the magnetopause"]
+[-0.7999817132949829, 0.12588928639888763, "Satellite System Chirp Signal Management Up/down chirp signals alternatively"]
+[-5.357969284057617, 15.898262977600098, "SAR Instrument Maximum Data Rate 800 Mbit/s"]
+[-5.2369065284729, 15.88105297088623, "SAR Instrument Maximum Data Rate 240 Mbit/s"]
+[-7.418949127197266, 2.850259304046631, "Cosmic Ray Detector Service Life Long after its original three-year mission"]
+[3.6148366928100586, 22.256267547607422, "Instrument Component Service Life Wore out in 2017"]
+[-1.0127131938934326, 6.923548698425293, "Activity Duration Six hours and two minutes"]
+[-1.1363722085952759, 6.944179534912109, "Activity Number Four"]
+[3.1518218517303467, -2.379960060119629, "Satellite Launch Date Unknown"]
+[5.201570510864258, -4.518049240112305, "Satellite Project Start Date April 7, 2015"]
+[5.191140651702881, -4.547143459320068, "Satellite Project Update Date April 17, 2015"]
+[-3.273859977722168, 4.347443580627441, "SAR Spacecraft Mission Type EO"]
+[-3.243497371673584, 4.315484046936035, "SAR Spacecraft Agency NPOMash"]
+[-3.490229368209839, 4.349000930786133, "SAR Spacecraft Launch Date 27 June 2013"]
+[-3.3396196365356445, 4.346309185028076, "SAR Spacecraft End of Life Date 27 June 2019"]
+[-3.275236129760742, 4.315839767456055, "SAR Spacecraft Measurement Domain Land"]
+[-3.404278039932251, 4.377471446990967, "SAR Spacecraft Measurement Category Multi-purpose imagery (land), Soil moisture"]
+[2.8809187412261963, -1.1941875219345093, "Satellite Purpose Operate spacecraft in the harsh radiation environment of the Van Allen radiation belts"]
+[2.8087551593780518, -1.1069093942642212, "Satellite Purpose Develop technologies to protect low Earth orbiting (LEO) satellites from the effects of HANE (High Altitude Nuclear Explosions)"]
+[2.6479101181030273, -1.2067065238952637, "Satellite Purpose Gather data on the radiation environment in medium Earth orbit"]
+[2.858506441116333, -1.029966115951538, "Satellite Purpose Test methods to control the orientation of very large structures in space"]
+[-5.396674633026123, 8.928235054016113, "SDR (Software Defined Radio) Function Communications and networking platform"]
+[1.8971916437149048, 8.606913566589355, "Subsystem Function Provide time correlation and synchronization between the two satellites, enable the exchange of formation control data among the platforms and determine their relative distance during the complete orbit including the precise formation flying maneuvers"]
+[1.905627727508545, 8.599488258361816, "Subsystem Environmental Requirement Survive the harsh radiation environment"]
+[-2.6316232681274414, 4.673191070556641, "Floating Platform Size 90 m x 50 m"]
+[-0.9650753140449524, 9.503324508666992, "Rocket Component Span 18 m"]
+[-0.14384271204471588, 13.688461303710938, "Performance Metric  10 m"]
+[-3.1155056953430176, 2.466423749923706, "Mission Goal Safely deliver NASA's contracted cargo to the ISS"]
+[1.2730885744094849, -2.33933687210083, "Satellite Orbit Parameters Perigee of 6000 km, apogee of 12000 km, inclination of 43\u00ba"]
+[1.3912885189056396, -1.5470221042633057, "Satellite Total Ionizing Dose (TID) 10 krad/year behind 8 mm of aluminum shielding"]
+[4.695523738861084, -2.5595879554748535, "Satellite Mission Duration 23 months"]
+[5.337601184844971, -4.3839240074157715, "Satellite Launch Date June 25, 2019"]
+[2.3380959033966064, 22.669631958007812, "Instrument Bands 8.2 - 9.0 \u00b5m; 10.3 - 11.3 \u00b5m; 11.5 - 12.5 \u00b5m; and 7.0 - 13 \u00b5m"]
+[1.9295947551727295, 22.376270294189453, "Instrument Temperature Sensitivity 0.01 K to 0.06 K"]
+[1.8961061239242554, 22.23297119140625, "Instrument Resolution 1 mrad"]
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+[1.5267168283462524, 21.263111114501953, "Instrument Mass 13 kg"]
+[1.6649272441864014, 23.181026458740234, "Instrument Power 20 W operating, 120 W during cold calibration"]
+[1.6410104036331177, 22.17700958251953, "Instrument Size 45 cm x 35 cm x 30 cm"]
+[2.317448377609253, 22.91095733642578, "Instrument Data Rate 368 kbit/s"]
+[-5.160473346710205, 8.9116849899292, "RF Module Transmit Power Amplification Channels 2"]
+[-5.138494491577148, 8.945038795471191, "RF Module Receive Channels 2"]
+[-5.141773223876953, 8.948145866394043, "RF Module Polarized Signals V and H"]
+[-5.134085178375244, 8.95744800567627, "RF Module Transmit Operation Can alternate between H and V on alternate pulses"]
+[0.8851227760314941, -1.1186774969100952, "Satellite Snow Depth Measurement Up to 27 cm"]
+[0.8089869618415833, -1.100212812423706, "Satellite Sea Ice Thickness Measurement Up to 5 meters"]
+[4.618856430053711, -2.5574800968170166, "Satellite Greenland and Antarctic Ice Sheets Elevation Change Measurement Over 16 years"]
+[0.7767184972763062, -1.219904899597168, "Satellite Altitude 268 and 220 km for more than 31days, 250, 240, 230, 220 and 180 km for more than 7 days"]
+[-1.6930586099624634, 9.353915214538574, "Engine System Altitude Usage Above 220 km"]
+[-1.6548389196395874, 9.303409576416016, "Engine System Electrical Consumption About half of total consumption of SLATS"]
+[0.6553337574005127, -1.3014118671417236, "Satellite Altitude Control Accuracy \u00b11km (1\u03c3) at each altitude"]
+[-1.6183829307556152, 9.460983276367188, "Engine System Thrust Time About 80 sec in the one cycle"]
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+[-1.6276146173477173, 9.706306457519531, "Propulsion System Potential Mission Services Value $60.2 million"]
+[-1.620693325996399, 9.696636199951172, "Propulsion System Maximum Potential Value $84.5 million"]
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+[1.1435165405273438, -0.7221079468727112, "Satellite Dimensions 6 x 4 x 4 m"]
+[0.9527965188026428, -4.346449851989746, "Satellite Mass 3700 kg"]
+[0.9776134490966797, -4.3091535568237305, "Satellite Payload Mass 1300 kg"]
+[0.9762924909591675, -2.088489294052124, "Satellite Pointing Accuracy < 0.3\u00b0"]
+[2.6222376823425293, -1.544647216796875, "Satellite Data Collection System Argos-Next"]
+[-3.8077189922332764, 6.919267654418945, "Data Collection System Supplier NASDA/CNES"]
+[1.363881230354309, -1.849157452583313, "Satellite Pointing Subsystem GPS Receiver Channels 10-channel and 8-channel"]
+[1.463503122329712, -1.8697699308395386, "Satellite Pointing Subsystem GPS Receiver Frequency L1 (1575.42 MHz)"]
+[1.4211686849594116, -1.9358937740325928, "Satellite Pointing Subsystem Antenna Type Micro-strip patch antenna"]
+[-1.9188960790634155, 14.887689590454102, "Radiometer System Objective Measure SSS (Sea Surface Salinity)"]
+[-1.9200518131256104, 14.876880645751953, "Radiometer System Design Polarimetric with four separate channels and four noise diode calibration sources"]
+[-1.9124579429626465, 14.872428894042969, "Radiometer System Calibration Method Three-position Dicke switching method"]
+[-3.793748617172241, 8.443342208862305, "Signal Divider Isolation 60 dB"]
+[4.098391532897949, 13.934749603271484, "Laser Altimeter Data Acquisition Elevation data"]
+[2.1646339893341064, -1.1951746940612793, "Satellite Image Source Images from Landsat 8"]
+[-0.08989399671554565, 4.995944499969482, "Iceberg Size Largest iceberg floating anywhere in the world"]
+[1.74662446975708, 8.429375648498535, "Communication and Data-Handling Subsystem Function Receives and decodes command signals, communicates with instruments, edits temperature, voltage, and status, transmits telemetry signals"]
+[-5.325410842895508, 7.936031341552734, "Inter-Orbit Communication Subsystem Band S-band and Ka-band"]
+[-3.6787383556365967, 7.739013671875, "Optical Data Recorder Data Recording Capacity High-speed, large-volume data recorder"]
+[-8.147536277770996, 8.822083473205566, "Electrical Power Subsystem Power Generation Capacity At least 5 kW (EOL)"]
+[1.8953924179077148, 8.606229782104492, "Paddle Subsystem Solar-Battery Cells 55,680"]
+[1.0465360879898071, 9.14318561553955, "Attitude and Orbit Control Subsystem Attitude Control Three-axis attitude control"]
+[0.6901422739028931, 9.180342674255371, "Reaction Control Subsystem Thrusters 1 N thruster and 20 N thruster"]
+[-5.1377949714660645, 7.917940616607666, "Direct Transmission Subsystem for local users Band UHF band (467.7 MHz)"]
+[2.145026683807373, -1.390552282333374, "Satellite Radar Measures height by sending out signals and timing how long they take to reflect off Earth\u2019s surface and return to their respective satellites"]
+[2.0101120471954346, -1.32662034034729, "Satellite Laser Instrument (Lidar) Measures height by sending out signals and timing how long they take to reflect off Earth\u2019s surface and return to their respective satellites"]
+[2.8538670539855957, 22.394895553588867, "Instruments Type Lightning Detection"]
+[5.203176975250244, -4.393037796020508, "Satellite Launch Date 17 Nov 2020"]
+[5.072282791137695, -4.125994682312012, "Satellite End of Life Date 17 Nov 2020"]
+[2.069366931915283, -1.2613756656646729, "Satellite Measurement Domain Atmosphere"]
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+[-1.1537567377090454, 4.454155921936035, "Ground Station Quantity 2"]
+[-1.1548117399215698, 4.450173854827881, "Ground Station Quantity 2"]
+[3.7884836196899414, 17.761499404907227, "Payload Control Center Quantity 1"]
+[2.130750894546509, -2.212820053100586, "Satellite Control Center Quantity 1"]
+[-1.9022364616394043, 8.109159469604492, "System Operational Capability Full"]
+[-1.9168592691421509, 8.0886869430542, "System Commercial Operations Start Date August 1st, 2008"]
+[-1.9029228687286377, 8.12297248840332, "System Signal Upgrade Completion Date Early 2010"]
+[-1.35076904296875, 9.717589378356934, "Projectile Launcher Required Velocity 20m/s"]
+[-2.5664098262786865, 9.688095092773438, "Energy Source Activation Method Gas release into the chamber volume"]
+[-2.4932007789611816, 8.104199409484863, "Fault Tolerance Device Purpose Provide fault tolerance against premature deployment"]
+[-0.9950163960456848, 7.774097442626953, "Penetrating Device Misalignment Tolerance Up to 45\u00ba"]
+[-2.5198416709899902, 8.353474617004395, "Harpoon Capture System Accuracy Influence Free release of the tether"]
+[-0.4225618541240692, 15.865734100341797, "Ultraviolet Imaging Spectrograph Manufacturer University of Colorado Boulder\u2019s Laboratory for Atmospheric and Space Physics (LASP)"]
+[-0.40310975909233093, 15.835817337036133, "Ultraviolet Imaging Spectrograph Host Satellite SES-14"]
+[-0.46206235885620117, 15.878545761108398, "Ultraviolet Imaging Spectrograph Mission Global-scale Observations of the Limb and Disk"]
+[3.739420175552368, -1.6119153499603271, "Satellite Operation Status Nominal"]
+[-0.5306400060653687, 5.839227199554443, "Dam Embankment Height 184 m"]
+[-0.5447465181350708, 5.87963342666626, "Dam Embankment Length 1,820 m"]
+[-0.4239429831504822, 5.124439239501953, "Reservoir Size 817 km2"]
+[-0.4036615192890167, 5.110583782196045, "Reservoir Volume 48.7 km3"]
+[-1.4102517366409302, 8.005048751831055, "Lab-on-a-Chip Spore Quantity 8"]
+[-1.3779716491699219, 8.128657341003418, "Lab-on-a-Chip Function Measures the fern spores"]
+[2.828815460205078, -1.4726531505584717, "Small Science Satellite Function Study the gravity response of ion channels"]
+[2.818887233734131, -1.5032234191894531, "Small Science Satellite Technology Variable-rate centrifuge"]
+[3.210843086242676, -2.4587855339050293, "Satellite Launch Date Unknown"]
+[5.086592674255371, -4.365914344787598, "Satellite Commissioning Update Date January 4, 2012"]
+[5.1838531494140625, -4.52724027633667, "Satellite First Map Release Date Sept. 22, 2011"]
+[-0.5292975306510925, 1.2277792692184448, "Satellite Orbit Altitude 628 km"]
+[-0.5343957543373108, 1.2264028787612915, "Satellite Orbit Inclination 97.9\u00ba"]
+[-0.5311693549156189, 1.2415493726730347, "Satellite Orbit Period 97.4 minutes"]
+[-0.5121429562568665, 1.2145472764968872, "Satellite Orbit Revisit Time 14 days"]
+[-0.5382431745529175, 1.23631751537323, "Satellite Orbit Number of Orbits/Day 15 3/14"]
+[-0.5352750420570374, 1.2332948446273804, "Satellite Orbit LSDN 12:00 hours \u00b1 15 min"]
+[-5.429113388061523, 2.8883988857269287, "Telescope Data Collection Sensitive to different wavelengths of light"]
+[2.3909029960632324, -1.3104283809661865, "Satellite Data Collection Sensitive to different wavelengths of light"]
+[-0.5439518094062805, 6.217940807342529, "Event Frequency Most predictable and frequent recurring"]
+[-0.576090931892395, 6.23073673248291, "Event Cause Supermassive black hole at the galaxy\u2019s center creates the bursts as it partially consumes an orbiting giant star"]
+[1.350055456161499, 10.527325630187988, "Imaging System Bands 5"]
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+[1.3821953535079956, 10.536833763122559, "Imaging System Band 2 Wavelength 450 nm - 520 nm"]
+[1.3718361854553223, 10.553064346313477, "Imaging System Band 3 Wavelength 520 nm - 600 nm"]
+[1.3784407377243042, 10.563152313232422, "Imaging System Band 4 Wavelength 630 nm - 690 nm"]
+[1.3846038579940796, 10.54439640045166, "Imaging System Band 5 Wavelength 760 nm - 900 nm"]
+[-4.483460903167725, 15.916753768920898, "Radar Antenna Type Phased array antenna"]
+[-1.8789725303649902, 14.88801097869873, "Radiometer Observation Wavelengths Five different wavelengths"]
+[-1.5045523643493652, 16.90178680419922, "Altimeter Antenna Type Parabolic 1 m antenna"]
+[-2.978595495223999, 16.1709041595459, "Scatterometer Operation Simultaneous operation with all sensors"]
+[-3.0401949882507324, 4.240123271942139, "Spacecraft Control Center SSTL in Guildford (UK)"]
+[-3.084310531616211, 4.257166862487793, "Spacecraft TT&C stations Oxford (UK), Santiago (Chile), Kuala Lumpur (Malaysia), Fucino (Italy), Kiruna (Sweden)"]
+[-1.6342946290969849, 4.069981098175049, "Ground Mission Segment Operator GAIN in Noordwijk (The Netherlands)"]
+[-5.183588027954102, 7.515738010406494, "Global Network Operator Not specified"]
+[6.286901473999023, 7.456152439117432, "Satellite Component Manufacturing Date Oct. 4-8, 2010"]
+[-0.4266361594200134, 6.772564888000488, "Test Equipment Design Date May 2008"]
+[-1.0662859678268433, 6.471745014190674, "Thesis Publication Date Dec. 2011"]
+[-1.0962568521499634, 6.611998558044434, "Thesis Publication Date December 2011"]
+[-0.8250234127044678, 6.351477146148682, "Article Publication Date April/May 2012"]
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+[2.6401779651641846, 12.224190711975098, "Beam Mode Azimuth Resolution 2.8 m"]
+[2.597352981567383, 12.223061561584473, "Beam Mode Incidence Angle 30-50\u00ba"]
+[2.625490188598633, 12.18461799621582, "Beam Mode Nominal Swath Width 90 km"]
+[2.626605272293091, 12.184203147888184, "Beam Mode Swath Width for Regular Corresponding Mode 50 km"]
+[2.632237195968628, 12.207953453063965, "Beam Mode Range Resolution 3.1-10.4 m"]
+[2.6360604763031006, 12.217428207397461, "Beam Mode Azimuth Resolution 4.6-7.6 m"]
+[2.638197898864746, 12.20284366607666, "Beam Mode Incidence Angle 29 - 50\u00ba"]
+[2.6284427642822266, 12.191489219665527, "Beam Mode Nominal Swath Width 120-170 km"]
+[2.6209170818328857, 12.178245544433594, "Beam Mode Swath Width for Regular Corresponding Mode 50 km"]
+[2.6296517848968506, 12.198155403137207, "Beam Mode Range Resolution 5.2-15.2 m"]
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+[2.6311230659484863, 12.188186645507812, "Beam Mode Nominal Swath Width 50 km"]
+[2.6017956733703613, 12.191983222961426, "Beam Mode Swath Width for Regular Corresponding Mode 25 km"]
+[2.634892702102661, 12.202080726623535, "Beam Mode Range Resolution 5.2-17.3 m"]
+[2.6232755184173584, 12.2069091796875, "Beam Mode Azimuth Resolution 7.6 m"]
+[2.6296095848083496, 12.197784423828125, "Beam Mode Incidence Angle 18 - 42\u00ba"]
+[2.6334524154663086, 12.190260887145996, "Beam Mode Nominal Swath Width 50 km"]
+[2.622965097427368, 12.182027816772461, "Beam Mode Swath Width for Regular Corresponding Mode 25 km"]
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+[1.0464987754821777, -1.3477141857147217, "Satellite Total Coverage Area 4,650,000 km2"]
+[5.117542266845703, -2.284400463104248, "Satellite Design Life 3 years"]
+[1.7706245183944702, -1.9046382904052734, "Satellite Coverage of Turkey 98%"]
+[1.9848920106887817, -2.0811095237731934, "Satellite Lesson Learned In-orbit calibration is absolutely necessary"]
+[-9.955554962158203, 5.849656105041504, "Search and Rescue System Operation Hours 24 hours a day, 365 days a year"]
+[-9.952731132507324, 5.857177734375, "Search and Rescue System Cost Free"]
+[-9.955720901489258, 5.852109432220459, "Search and Rescue System Purpose Detect and locate transmissions from emergency beacons carried by ships, aircraft, or people"]
+[2.288137435913086, 22.366905212402344, "IR Instrument Application Fire and sea surface temperature measurement"]
+[7.322514533996582, 12.382163047790527, "Satellite Instrument Scan Mode 4 (Continuous Full Disk) 5 minutes"]
+[7.290172576904297, 12.419445991516113, "Satellite Instrument Scan Mode 3 (Flex Mode) 15 minutes"]
+[7.351595401763916, 12.474841117858887, "Satellite Instrument Scan Mode 6 (Super Flex Mode) 10 minutes"]
+[7.3339691162109375, 12.471604347229004, "Satellite Instrument Mesoscale #1 0.5 minutes"]
+[7.308728218078613, 12.428584098815918, "Satellite Instrument Mesoscale #1 1 minute"]
+[7.281863212585449, 12.427090644836426, "Satellite Instrument Mesoscale #2 1 minute"]
+[-5.394909381866455, 2.8004648685455322, "Telescope Field of View 2.08\u00ba x 1.67\u00ba"]
+[-5.342361927032471, 2.811830520629883, "Telescope Beam f/2.5"]
+[-5.293663501739502, 2.808356523513794, "Telescope Imager Size 8.6 mm x 6.9 mm"]
+[3.551046371459961, 13.514016151428223, "Laser System Quantity 2"]
+[-0.8244357705116272, 11.617888450622559, "Detector Type PSD (Position Sensitive Detectors)"]
+[-7.565019130706787, 5.878665924072266, "Camera Location On the optics (outboard) bench"]
+[2.288646936416626, -1.8058687448501587, "Satellite Antenna Performance Verification"]
+[2.9620988368988037, -1.9705826044082642, "Satellite Status On the home stretch"]
+[2.1043732166290283, -2.775522470474243, "Satellite Number of Conflicts 395 in August 2014"]
+[4.9814982414245605, -3.9739322662353516, "Satellite Number of Conflicts 202 in February"]
+[-0.8740668892860413, 6.751569747924805, "Process Purpose Maximize use of the RADARSAT-2 satellite"]
+[-0.8821612000465393, 6.807399749755859, "Process Impact Eliminated the need for the use of higher priority programming levels"]
+[1.5834639072418213, -2.353131055831909, "Satellite Orbit Geostationary orbit of 35,786 km"]
+[0.9593087434768677, -2.144056797027588, "Satellite Location 82\u00b0E over the equator"]
+[2.7441115379333496, 13.778040885925293, "Optical System Depth of Focus 10 \u00b5m"]
+[-2.6260266304016113, 11.660279273986816, "CMOS Imager Format 1280 x 1024"]
+[-2.578662633895874, 11.709331512451172, "CMOS Imager Pixel Size 6.7 \u00b5m"]
+[-2.621256113052368, 11.651898384094238, "CMOS Imager Manufacturer Cypress"]
+[-2.631545305252075, 11.654800415039062, "CMOS Imager Microprocessor PXA 270"]
+[-5.1177191734313965, 7.116368293762207, "Link Management System Late Request Window 45 minutes"]
+[-5.049405574798584, 7.0823469161987305, "Link Management System Scheduling Trigger Reception of a payload link configuration request or when the Automator delivers the current state of the TTC buffer to the LMS"]
+[-5.217414855957031, 7.859096050262451, "On-board Time-Tagged Telecommand Buffer Operation Constantly kept as full as possible"]
+[-5.013180255889893, 7.089695453643799, "Link Management System Planning Cycle Constantly tries to schedule any request in its request database"]
+[-5.268532752990723, 3.1632883548736572, "Telescope Array Optics Overview and Current Status Unknown"]
+[-5.322721481323242, 3.1399073600769043, "Telescope Array Update May 2010"]
+[-3.337721586227417, 7.461690902709961, "Data Processing Method Unknown Unknown"]
+[-3.423590660095215, 6.885503768920898, "Data Analysis Unknown Unknown"]
+[-3.144850969314575, 1.7638317346572876, "Satellite Mission Preliminary Design Unknown"]
+[1.1248544454574585, 13.203983306884766, "Modulation Scheme Data Rate 800 Mbit/s"]
+[-4.804194927215576, 9.267111778259277, "RF Carrier Type Single"]
+[1.1283844709396362, 13.194231033325195, "Modulation Technique Compliance Existing ground stations and improve robustness"]
+[6.326520919799805, 7.415066242218018, "Satellite Component Devices WizardLink family of multi-Gigabit Serializer/Deserializers (Ser/Des), SRAM-based FPGA (Virtex-4QV), High-speed Digital-to-Analog Converter (DAC5675A-SP), antifuse-FPGA, TCXO (Temperature Compensated Crystal Oscillator)"]
+[-3.217665910720825, 1.7170120477676392, "Satellite Mission Launch Date 2 April 2018"]
+[-3.1970255374908447, 1.7502399682998657, "Satellite Mission Mission Type Non-EO"]
+[-3.12115216255188, 1.7703561782836914, "Satellite Mission Mission Status Ongoing"]
+[-3.137317657470703, 1.7218272686004639, "Satellite Mission Platform EU (European Union) Framework 7 (FP7) research project"]
+[-5.3841166496276855, 2.7940237522125244, "Telescope Size Small"]
+[-1.0842763185501099, 3.333843946456909, "Black Hole Mass 10 million times the mass of our sun"]
+[-1.1670784950256348, 3.2826766967773438, "Black Hole Diameter 30 times the diameter of the sun"]
+[-1.1475510597229004, 3.3293089866638184, "Black Hole Distance from Earth About 324 million light-years"]
+[-2.3033607006073, 9.208792686462402, "Power Conditioner Type Miniaturized pulsed"]
+[-2.6999549865722656, 8.766636848449707, "Module Quantity Three"]
+[-6.771662712097168, 10.053407669067383, "Antenna Design Location ISRO"]
+[-1.745266079902649, 8.575844764709473, "Integrated Circuit Design Location In-house"]
+[-6.710450649261475, 9.99106502532959, "Antenna Facility Design Location In-house"]
+[-7.513582229614258, 5.928804397583008, "Tripod Head Usage Accurately track a SLR camera"]
+[-7.519732475280762, 5.921919822692871, "Tripod Head Compatibility Large SLR cameras"]
+[-7.533746242523193, 5.90672492980957, "Tripod Head Focal Length Limit 180 mm"]
+[-7.456984043121338, 5.987472057342529, "Tripod Head Application Optical observation"]
+[-1.6884963512420654, 11.22359561920166, "Lidar Purpose Aerosol and cloud profiling"]
+[-1.6719201803207397, 11.230266571044922, "Lidar Platform International Space Station"]
+[-1.6741329431533813, 11.235020637512207, "Lidar Measurement Capability Fly on the International Space Station"]
+[0.5368419289588928, 10.91972827911377, "Image Sensor Frame Store Transfer Time 200 \u00b5s"]
+[0.5066397190093994, 10.90832233428955, "Image Sensor Exposure Time 50 ms"]
+[0.48874643445014954, 10.936308860778809, "Image Sensor Readout Time Less than 10 ms"]
+[0.08688708394765854, 11.956805229187012, "CMOS Amplifier and MultiplEXer Standby Mode Minimize the average heat dissipation to the focal plane CCD"]
+[-0.7942676544189453, 11.5697660446167, "Detector Module Size 2 cm x 2 cm"]
+[-1.897998571395874, 8.353950500488281, "Safety System Weight 410 kg"]
+[-1.9424798488616943, 8.38773250579834, "Safety System Activation Time Milliseconds"]
+[-1.931075930595398, 8.307924270629883, "Safety System Jettison Time 6 minutes and 20 seconds"]
+[2.683838129043579, -1.621445655822754, "Satellite Payload Scientific Persuasions"]
+[3.1176862716674805, -2.371556520462036, "Satellite Maiden Flight Date Unknown"]
+[0.11223695427179337, -4.023784637451172, "Satellite Platform Deployment Date Aug. 7"]
+[0.1338759958744049, -4.0433244705200195, "Satellite Platform Retrieval Date Aug. 16"]
+[-2.1949448585510254, 5.994580268859863, "Manipulator Flight Development Purpose Evaluate the operation of the SFA (Small Fine Arm)"]
+[-0.9765329360961914, 8.159904479980469, "Small Fine Arm Intended Use Future RMS (Remote Manipulator System) of JEM (Japanese Experiment Module) on ISS"]
+[-1.192968487739563, 15.090009689331055, "Imaging multi-spectral radiometers Instrument type Imaging multi-spectral radiometers (vis/IR)"]
+[-2.9807779788970947, 16.152565002441406, "Scatterometers Instrument type Scatterometers"]
+[-0.5170504450798035, 1.239447832107544, "Precision orbit Instrument type Precision orbit"]
+[-1.727091908454895, 16.987802505493164, "Radar altimeters Instrument type Radar altimeters"]
+[-1.2213045358657837, 15.083802223205566, "Imaging multi-spectral radiometers Instrument type Imaging multi-spectral radiometers (passive microwave)"]
+[-1.7274925708770752, 16.989131927490234, "Radar altimeters Instrument type Radar altimeters"]
+[-1.223320722579956, 15.083253860473633, "Imaging multi-spectral radiometers Instrument type Imaging multi-spectral radiometers (passive microwave)"]
+[-1.4087320566177368, 4.362265110015869, "Ground System Components 2,100 servers, 149 racks of network equipment, 317 workstations, and storage services totaling three petabytes (3 PB)"]
+[-1.4183498620986938, 4.338743686676025, "Ground System Blade Servers 454"]
+[-1.4191908836364746, 4.342858791351318, "Ground System Blade Servers Cores 3,632"]
+[-1.430091381072998, 4.339820384979248, "Ground System Processing Power Approximately 40 trillion floating point operations per second"]
+[0.9207518100738525, -4.4006757736206055, "Satellite Dry Mass < 2800 kg"]
+[2.0780327320098877, -0.5179756283760071, "Satellite Power Capability > 4 kW (EOL)"]
+[1.7753777503967285, 8.444604873657227, "Command and Data Handling Subsystem Function Serves as the hub for all data received by and sent from the spacecraft"]
+[-5.114876747131348, 9.011274337768555, "Hand-held radio terminal Compatibility with the downlink"]
+[-5.063815593719482, 9.007780075073242, "Hand-held radio terminals Built-in Components AX.25 Terminal Node Controllers (TNCs) and RS-232 ports"]
+[-5.110204219818115, 9.050628662109375, "Hand-held radio terminals Data Header STRSHN3 N7YTK"]
+[1.9170074462890625, 10.722477912902832, "Imaging Device Model Engineering model"]
+[-3.6305224895477295, 12.757309913635254, "Particle Detector Operating Stability Stable since May 2011"]
+[-3.6438748836517334, 12.752985000610352, "Particle Detector Events Collected 60 billion"]
+[-3.6449310779571533, 12.757810592651367, "Particle Detector Leptons Identified 10.6 million"]
+[-3.6459856033325195, 12.752401351928711, "Particle Detector Positron Flux Measurement Up to 500 GeV"]
+[-3.648618698120117, 12.711292266845703, "Particle Detector Electron Flux Measurement Up to 750 GeV"]
+[-3.6459240913391113, 12.748373031616211, "Particle Detector Electron+Positron Flux Measurement Up to 1 TeV"]
+[-3.6227493286132812, 12.759359359741211, "Particle Detector Positron Fraction Measurement Up to 500 GeV"]
+[-3.58778715133667, 12.795183181762695, "Particle Detector Positron Fraction Turnover Beyond 200 GeV"]
+[-3.629953145980835, 12.760241508483887, "Particle Detector Electron Spectrum Turnover Beyond 30 GeV"]
+[0.6743823289871216, -1.49696946144104, "Satellite Orbit Altitude 385 km"]
+[0.7328563928604126, -2.227259635925293, "Satellite Orbit Inclination 51.6\u00ba"]
+[-0.6893787980079651, 8.457284927368164, "Advanced Composite Structure Status Reentered the Earth's atmosphere on Nov. 16, 1999"]
+[2.073512077331543, -2.753682851791382, "Satellite Number of Experiments 5"]
+[2.1067044734954834, -2.7453362941741943, "Satellite Number of Bus Components 2"]
+[1.4348466396331787, -2.4281117916107178, "Satellite Orbit Sun-synchronous Orbit"]
+[0.9702830910682678, -4.402823448181152, "Satellite Mass \u2264 25 kg"]
+[2.07035231590271, -0.5053852200508118, "Satellite Power > 20 W"]
+[1.0092740058898926, -2.1327877044677734, "Satellite Attitude Control Accuracy (Pitch) < \u00b11\u00ba"]
+[0.9209789633750916, -2.205042839050293, "Satellite Attitude Control Accuracy (Roll, yaw) < \u00b13\u00ba"]
+[2.5862834453582764, -2.398045778274536, "Satellite RF Communications UHF, downlink data rate = 9.6 kbit/s VHF uplink data rate = 2.4 kbit/s FSK modulation"]
+[4.959874153137207, -2.364197254180908, "Satellite Mission Design Life 2 years"]
+[4.620410919189453, -2.4695229530334473, "Satellite Operation Mission 1 year"]
+[2.5612852573394775, -1.7753932476043701, "Satellite Payload Double payload with 5G connection and end-to-end encryption device"]
+[0.7310589551925659, -1.1783543825149536, "Satellite Altitude About 600 km"]
+[1.1523877382278442, -0.7428832054138184, "Satellite Size The size of a microwave"]
+[2.663666248321533, -2.35603404045105, "Satellite Communication Technology 5G connection and Quantum Key Distribution"]
+[3.0464859008789062, 22.799400329589844, "Instrument Unknown Unknown"]
+[3.042659044265747, 22.803403854370117, "Instrument Unknown Unknown"]
+[-1.0705195665359497, 7.722285270690918, "Device Energy Range < 1 MeV to >10 MeV"]
+[-1.0806710720062256, 7.7140326499938965, "Device Storage Capacity 200 000 photons"]
+[1.8311256170272827, 22.79473876953125, "Instrument Energy Range 20 keV-12 MeV"]
+[2.163294553756714, 22.65974235534668, "Instrument Accuracy at 20 keV 30%"]
+[2.200535535812378, 22.595314025878906, "Instrument Accuracy at 511 keV 9%"]
+[2.4057745933532715, -1.748256802558899, "Satellite Operational Modes Initial, Nominal, Scientific, Observation, Safe"]
+[1.9777143001556396, -0.6997970342636108, "Satellite Power Budget Low"]
+[1.639237403869629, -1.5069109201431274, "Satellite Operational Mode Power Consumption Unknown"]
+[-5.253261089324951, 7.876275062561035, "Communication System Unknown Unknown"]
+[-3.2207586765289307, 1.7268154621124268, "Satellite Mission Launch Date Nov. 21, 2013"]
+[3.047008514404297, -1.5039674043655396, "Satellite Mission Name Alabama Burst Energetics eXplorer (ABEX)"]
+[-1.3303730487823486, 6.165603160858154, "University Project Role Management, System Engineering, Science & Payload"]
+[-1.3326376676559448, 6.165408134460449, "University Project Role Power Systems, Command & Data Handling"]
+[-1.3581182956695557, 6.116364479064941, "University Project Role Orbital Analysis, Flight Software, Structures and Mechanisms, Thermal & Radiation Design & Analysis"]
+[-1.3145891427993774, 6.160065174102783, "University Project Role Guidance & Navigation Systems, Communications"]
+[-1.3330004215240479, 6.141743183135986, "University Project Role Structural Design"]
+[2.8162975311279297, -1.1371883153915405, "Satellite Purpose Study exoplanets"]
+[3.162097930908203, -1.6742759943008423, "Satellite Project Scientist Stephen Rinehart"]
+[2.9844954013824463, -1.600839376449585, "Satellite Management NASA/GSFC (Goddard Space Flight Center)"]
+[-2.306800365447998, 7.420498371124268, "On-Board Computer Processor 386 based computer"]
+[-2.2506446838378906, 7.441805839538574, "On-Board Computer Data Bus Dual redundant CAN (Controller Area Network) bus"]
+[-2.274956464767456, 7.415354251861572, "On-Board Computer Data Links ESA standard SpaceWire connections"]
+[-2.263664484024048, 7.420682907104492, "On-Board Computer Data Rates 130 Mbit/s"]
+[-2.3370141983032227, 7.471197128295898, "On-Board Computer Memory Radiation-hardened SDRAMs (Synchronous Dynamic Random Access Memory)"]
+[2.8294894695281982, -1.2642980813980103, "Satellite Mission Goal Provide high-quality topographic measurements for estimating ice sheet volume change"]
+[2.8899409770965576, -1.2105695009231567, "Satellite Mission Goal Provide high-accuracy altimetry for making long-sought repeat estimates of sea ice freeboard and hence sea ice thickness change"]
+[2.8759193420410156, -1.232879400253296, "Satellite Mission Goal Estimate the flux of low-salinity ice out of the Arctic basin into the marginal seas"]
+[0.10086488723754883, -4.036962509155273, "Satellite Platform Interface Type Directly interface with the launch box via braces"]
+[-0.5673781037330627, -0.140040785074234, "Small Satellite Deployment System Location JEM airlock"]
+[2.1837940216064453, 13.381043434143066, "Optical Sensor Manufacturer Not specified"]
+[-2.690431594848633, 11.727975845336914, "Active Imager Manufacturer CSEM (Swiss Centre for Electronics and Microsystems)"]
+[-2.6427524089813232, 11.699180603027344, "Active Imager Technology Flash imaging LiDAR"]
+[-2.6582729816436768, 11.703961372375488, "Active Imager Application Debris tracking and capture control"]
+[-1.5503612756729126, 8.441131591796875, "System Component Accuracy 100 parts per billion"]
+[-1.5691202878952026, 8.42631721496582, "System Component Effect on Displacement Measurement Scales with distance"]
+[-1.5866007804870605, 8.397754669189453, "System Component Effect on Displacement Measurement Can be accounted for"]
+[6.277713298797607, 7.464231014251709, "Satellite Component Power Capacity 140 W"]
+[6.298046588897705, 7.434635162353516, "Satellite Component Delta-V Capacity More than 154 m/s"]
+[6.29153299331665, 7.417142868041992, "Satellite Component Instrument Support Capacity Up to 206 kg"]
+[2.4450578689575195, 22.285518646240234, "Instrument Focal Plane Cooling Passively cooled"]
+[6.1483683586120605, 7.591144561767578, "Satellite Component Quantity Four"]
+[-6.6934919357299805, 9.977442741394043, "Antenna Pointing Body-pointing"]
+[7.359140396118164, 12.500753402709961, "Satellite Instrument Emergency Observation Time 5:59 (GMT) on July 2, 2015"]
+[-3.2415149211883545, 1.696489930152893, "Satellite Mission Agreement Conclusion Date April 30, 2015"]
+[-3.1904244422912598, 1.6732838153839111, "Satellite Mission Purpose of Agreement Survey secular changes in landscape and ash fall, isolated islands for their upkeep"]
+[-2.5831425189971924, 8.740415573120117, "Electronic Module Housing Number of Modules 5"]
+[-1.4852765798568726, 12.727584838867188, "Coronagraph Control Module Main Processor System LEON-3 based"]
+[-1.4593833684921265, 12.729105949401855, "Coronagraph Control Module Processing Power 20-30 MIPS"]
+[-1.5021417140960693, 12.703567504882812, "Coronagraph Control Module FPGA Microsemi RTAX"]
+[-1.45054030418396, 12.709368705749512, "Coronagraph Control Module In-flight Reconfigurable FPGA Xilinx Virtex"]
+[-0.07909051328897476, 4.7608232498168945, "Oceanographic Feature Location About 100 km southeast of Delaware Bay"]
+[-0.019136279821395874, 4.731818199157715, "Oceanographic Feature Boundary Characteristics Concentric curvilinear lines"]
+[0.018791334703564644, 4.702820301055908, "Oceanographic Feature Wave-Like Patterns Location J2 to J5"]
+[-0.12348150461912155, 4.766763687133789, "Oceanographic Feature Location Off Point Arena, California"]
+[-6.768302917480469, 10.029296875, "Antenna Size 16.4 m"]
+[-6.731664657592773, 10.018869400024414, "Antenna Operating Conditions Category 2 hurricane"]
+[-6.6744914054870605, 9.942854881286621, "Antenna Operating Conditions Ice and snow"]
+[4.7220988273620605, -4.275723934173584, "Satellite Imagery Distribution Agreement Date November 2012"]
+[5.332993030548096, -4.458107948303223, "Satellite Operation Start Date September"]
+[2.223350763320923, -1.4555854797363281, "Satellite Image Scene Jeodong Port on Ulleungdo Island, Korea"]
+[4.237960338592529, -2.893115282058716, "Satellite Separation Time 23 minutes after launch"]
+[-2.580289602279663, 9.344827651977539, "Power Supply Module Power Source +28 V"]
+[-4.389595985412598, 7.997819900512695, "Communication and Storage Module Image Data Storage Capacity 7 Gbit"]
+[-4.855319499969482, 7.907712459564209, "Communication and Storage Module Primary and Redundant CAN Buses Communication"]
+[-4.649791717529297, 7.9201979637146, "Communication and Storage Module LVDS Image Data Ports Quantity: 4"]
+[-4.595801830291748, 7.968359470367432, "Communication and Storage Module LVDS Image Data Ports Operating Frequency: 25 MHz"]
+[8.956730842590332, 8.512409210205078, "Satellite Payload Emergency Message Collection Yes"]
+[8.957015037536621, 8.512608528137207, "Satellite Payload Emergency Message Collection Yes"]
+[8.956903457641602, 8.512521743774414, "Satellite Payload Emergency Message Collection Yes"]
+[-0.4532259404659271, 0.21355563402175903, "Satellite Navigation System Frequency Bands E5a, E5b, E6, L1"]
+[2.571451425552368, -2.352247714996338, "Satellite Signal Pilot Component Included"]
+[2.617126941680908, -2.3782310485839844, "Satellite Signal Modulation Schemes Result in significant reduction of both tracking and multipath noise"]
+[2.6357526779174805, -2.3674659729003906, "Satellite Signal Coding Scheme FEC-encoding, interleaving and improved CRC"]
+[1.2641721963882446, 5.580231666564941, "Bus Management Unit Processor MAR 31750"]
+[1.29485023021698, 5.544444561004639, "Bus Management Unit Software Language ADA"]
+[-2.6041224002838135, 9.62258243560791, "Power Source Power Output 1164 W"]
+[-3.6967689990997314, 8.334040641784668, "Energy Storage Capacity 18 Ah"]
+[-1.4843275547027588, 13.392581939697266, "Solar Array Drive Assembly Function Reduce the spacecraft disturbances"]
+[-0.21979650855064392, 0.21161781251430511, "S-band spacecraft navigation and communication device Function Receives GPS signals (L1 C/A) as input for navigation support and provides low-rate data communications links to ground stations and the TDRS system"]
+[-0.23153960704803467, 0.20574244856834412, "S-band spacecraft navigation and communication device Mounting Mounted on a two HH Single Bay Pallets (SBP) on top of the HH MPESS"]
+[16.849111557006836, 6.869356155395508, "Microsatellite Ground Segment Unknown"]
+[16.805498123168945, 6.897947788238525, "Microsatellite Data Products Unknown"]
+[-0.10327619314193726, 15.54175853729248, "Spectrometer Purpose Lunar Volatile Dynamics"]
+[-0.10351970791816711, 15.544246673583984, "Spectrometer Mission Lunar Ice Cube"]
+[-1.9078311920166016, 6.910637378692627, "Software Innovation Date Unknown"]
+[-1.7114545106887817, 8.849186897277832, "Control System Conference Date June 5-10, 2011"]
+[0.934105396270752, -4.354244709014893, "Satellite Dry Mass 2350 kg"]
+[0.9461331367492676, -4.3515191078186035, "Satellite Wet Mass 2712.5 kg"]
+[6.233941078186035, 7.484384059906006, "Satellite Component Maximum Capacity 300 kg"]
+[-0.8347079753875732, 0.15487512946128845, "Satellite System Pointing 2 arcmin"]
+[-0.8322817087173462, 0.15214644372463226, "Satellite System Stabilization \u00b12.5 arcsec"]
+[-0.8324183821678162, 0.15570378303527832, "Satellite System Average Stabilization Velocity 0.36 arcsec/s"]
+[-0.8376425504684448, 0.1573053002357483, "Satellite System Re-orientation Velocity (max) 0.25\u00ba/s"]
+[-0.8521403074264526, 0.16662245988845825, "Satellite System Supply Voltage 27 \u00b1 1.35 V"]
+[-0.8789941072463989, 0.19495761394500732, "Satellite System Science Equipment Power 1500 W"]
+[4.829314231872559, -2.47074294090271, "Satellite Goal 7.5 years"]
+[-5.176840782165527, 7.805352687835693, "Communication System Data Transmission Rate 2 Mbit/s"]
+[7.440913200378418, 12.575577735900879, "Satellite Instrument Operations End Date June 17, 2015"]
+[7.451623916625977, 12.587845802307129, "Satellite Instrument Meeting Date Nov. 11-14, 2014"]
+[-2.7411134243011475, 4.543366432189941, "Spacecraft Platform Payload Power Up to 2 kW"]
+[-2.666240692138672, 4.584060192108154, "Spacecraft Platform Payload Capacity Up to 500 kg"]
+[-2.704873561859131, 4.585531711578369, "Spacecraft Platform Performance Options Redundancy, propulsion capability, high data rate communications, high-agility/high-accuracy pointing"]
+[4.746586799621582, -2.524817705154419, "Satellite Operation Duration More than four years"]
+[2.9646403789520264, -2.04107403755188, "Satellite Planned Mission Advantages Unknown"]
+[5.145742893218994, -4.499149799346924, "Satellite Retirement Date May 12, 2011"]
+[4.355096817016602, -2.755368709564209, "Satellite Communication Attempt Duration About three weeks"]
+[0.5020428895950317, -1.4826513528823853, "Satellite Orbit Altitude 35,786 km"]
+[0.8772238492965698, -2.1547629833221436, "Satellite Nominal Position 0\u00b0 longitude"]
+[-3.1086020469665527, 4.22368049621582, "Spacecraft Testing Thermal vacuum, instrument testing and calibration"]
+[-0.07773157209157944, 15.57978343963623, "Spectrometer Functionality Verification Completed"]
+[-3.114431858062744, 4.238607406616211, "Spacecraft Funding NASA\u2019s Next Space Technologies for Exploration Partnerships program"]
+[-3.094322443008423, 4.249610424041748, "Spacecraft Mission Lead Morehead State University in Morehead, Kentucky"]
+[5.331259727478027, -4.433820724487305, "Satellite Launch Date April 28, 2008"]
+[2.696744680404663, -2.3334686756134033, "Satellite Launch Vehicle PSLV"]
+[2.7781896591186523, -2.3310317993164062, "Satellite Launch Site SDSC (Satish Dhawan Space Centre), Sriharikota, India"]
+[16.780500411987305, 6.914993762969971, "Microsatellite Mass 83 kg"]
+[-1.0591083765029907, 7.720984935760498, "Device Power Generation Over 1 W"]
+[-1.015406608581543, 7.772115230560303, "Device Thermal Conductance ~1 W/K"]
+[-0.984158456325531, 7.804900169372559, "Device Temperature Control \u00b10.5 K"]
+[-0.9930142760276794, 7.780434608459473, "Device Temperature Control \u00b10.01 K"]
+[-7.5505900382995605, 5.884153366088867, "Camera Optics Focal Length 2.5 mm"]
+[-7.538912773132324, 5.907088279724121, "Camera Field of View 84.6\u00ba"]
+[-7.534158229827881, 5.913249969482422, "Camera Resolution 0.8 km/pixel"]
+[-7.51783561706543, 5.895735740661621, "Camera Optics Focal Length 6 mm"]
+[-7.5637288093566895, 5.897324085235596, "Camera Field of View 36.8\u00ba"]
+[-7.5617194175720215, 5.883306980133057, "Camera Resolution 0.3 km/pixel"]
+[0.5244316458702087, 12.246292114257812, "Sensor Optics Focal Length 2.5 mm"]
+[-10.259265899658203, 9.984440803527832, "Accelerometer Proof Mass Mass 72 gram"]
+[-10.260682106018066, 9.980118751525879, "Accelerometer Resolution Better than 10-10 ms-2 Hz-1/2"]
+[-10.264594078063965, 9.979291915893555, "Accelerometer Output Analog voltages"]
+[-10.265206336975098, 9.978836059570312, "Accelerometer Subsystems SU (Sensor Unit) and the ICU (Interface Control Unit)"]
+[-3.589580535888672, 4.38824462890625, "Spacecraft Observation Date August 19, 2015"]
+[0.2284453958272934, 13.802552223205566, "Calibration Instrument Beams 116"]
+[0.23759210109710693, 13.792925834655762, "Calibration Instrument Calibration Time 3 and a half months"]
+[0.21697674691677094, 13.796613693237305, "Calibration Instrument Calibrated Beams 58"]
+[0.26497119665145874, 13.767570495605469, "Calibration Instrument Performance Extremely good with high-quality SAR imagery"]
+[-1.4955875873565674, 13.406916618347168, "Solar Panel Array Concentration Ratio 3:1"]
+[-1.473008632659912, 13.3998441696167, "Solar Panel Array Pointing Tolerance 20\u00ba"]
+[-1.4908349514007568, 13.408795356750488, "Solar Panel Array Power Output 37 W (BOL, 27.5 W EOL)"]
+[-1.482138991355896, 13.402066230773926, "Solar Panel Array Mass 0.74 kg"]
+[1.3741463422775269, 5.542423248291016, "Bus Structure Material New materials"]
+[1.4315036535263062, 5.467111110687256, "Bus Structure Features Integrated thermal management system, robust structural integrity, high-attitude control accuracy, and precision three-axis stabilization"]
+[-3.534301280975342, 7.381885528564453, "Data Acquisition Equipment Monitored Parameters Radiation absorption, memory malfunction, static charge voltage, contamination, heavy ions"]
+[-3.5438051223754883, 7.462841033935547, "Data Acquisition Equipment Function Measure the space environment surrounding the S/C"]
+[-1.8491840362548828, 6.907147407531738, "Financial Tool Update Frequency Throughout development"]
+[-1.0242310762405396, 6.532472610473633, "Regulatory Act Impact Imposed new regulatory requirements"]
+[2.962547540664673, 22.443737030029297, "Instrument Mission Cluster"]
+[-2.964416742324829, 4.191566467285156, "Spacecraft Radial Distance 5.9 RE"]
+[-3.0061984062194824, 4.215194225311279, "Spacecraft Travel Direction From low to high latitude"]
+[2.340823173522949, 22.33719253540039, "Instrument Measurement Type Ion Dispersion"]
+[2.279406785964966, 22.155315399169922, "Instrument Measurement Type Ion Density"]
+[-2.149980068206787, 6.47242546081543, "Flight Software Framework F Prime"]
+[-2.1731481552124023, 6.565916538238525, "Flight Software Architecture Components and ports"]
+[-2.1745760440826416, 6.5926408767700195, "Flight Software Auto-generated Components Partial C++ implementation, C++ code for instantiating the components and connecting the ports, interface dictionaries for use by the ground data system"]
+[5.139579772949219, -4.398237705230713, "Satellite Service Date 26 February 2019"]
+[2.88858699798584, -1.1075522899627686, "Imagery Service Agreement Date 17 December 2018"]
+[0.6707424521446228, 12.047962188720703, "Sensing Unit Optics Fiber Channel Transfer the light from the laser"]
+[-1.7660510540008545, 8.502696990966797, "Electronics Electrical Currents 5 different"]
+[-1.0247478485107422, 7.766251087188721, "Device Clock Basis Several MHz"]
+[-1.0614184141159058, 7.779229640960693, "Device Type Giant Magneto-Resistance"]
+[-3.1674695014953613, 1.6749355792999268, "Satellite Mission Objectives Ocean topographic mapping, measurements of sea surfaces, development of climate models"]
+[-3.107642412185669, 2.288175106048584, "Mission Requirement Number of Independent Systems 3"]
+[14.371498107910156, 7.7511491775512695, "Nanosatellite Platform-Based Lab-on-a-Chip Investigating Parameter Gravitational Threshold for Calcium Ion Channel Activation"]
+[14.537879943847656, 7.607484817504883, "Nanosatellite Platform-Based Lab-on-a-Chip URL http://www.nasa.gov/centers/ames/engineering/projects/sporesat.html#.U0J-C6KegkA"]
+[-2.6768836975097656, 11.646410942077637, "Imager Application Cartography and disaster monitoring"]
+[2.7529172897338867, 13.71054744720459, "Electro-Optical Subsystem Modules OM (Optical Module) and CEU (Camera Electronics Unit)"]
+[-7.456692695617676, 5.999364376068115, "Camera Electronics Unit Modules CEUP (CEU Power supply), CC (Camera Controller), and FPA"]
+[1.9529533386230469, 10.672893524169922, "Imaging Device Power Source Ancillary Electronics Units (AEUs)"]
+[-1.9417694807052612, 8.810178756713867, "Control Units Redundancy Cold redundancy"]
+[-2.459862470626831, 7.931109428405762, "Core Function Receives command packets from the DPU and timing and synchronization data from the AEU"]
+[-2.5400946140289307, 7.9342942237854, "Core Function Generates all the clocks necessary for driving the 4 CCDs and drives the DACs responsible for providing the bias voltages"]
+[-2.2240853309631348, 8.181975364685059, "Interface Communication Protocol SpaceWire"]
+[-2.232590675354004, 8.146943092346191, "Interface Protocol RMAP"]
+[-2.2873587608337402, 8.153228759765625, "Interface Protocol Simulated RMAP with e.g. control registers, HK data, memory mapped for simple access"]
+[2.0455517768859863, 22.356075286865234, "Instrument Required Accuracy 4.0 cm"]
+[2.14140248298645, 22.3858642578125, "Instrument Achieved Accuracy 3.2 cm"]
+[-0.13498874008655548, 13.594661712646484, "Measurement Required Accuracy 12.8 cm"]
+[-0.135328471660614, 13.62509536743164, "Measurement Achieved Accuracy 2.8 cm"]
+[-0.12388163059949875, 13.600852012634277, "Measurement Required Accuracy 13.4 cm"]
+[-0.11898165941238403, 13.6212158203125, "Measurement Achieved Accuracy 4.3 cm"]
+[2.2398009300231934, 22.179988861083984, "Instrument Measurement Type Vertical measurements"]
+[3.202230215072632, -1.5292439460754395, "Satellite Mission Type Non-EO"]
+[3.0684306621551514, -1.5511436462402344, "Satellite Agency SSRL (Space Systems Research Laboratory)"]
+[2.9808363914489746, -1.5016810894012451, "Satellite Development Program SSRL (Space System Research Laboratory) at Hankuk Aviation University"]
+[11.225351333618164, 5.504782676696777, "CubeSat Launch Failure Date July 26, 2006"]
+[8.95470142364502, 8.513958930969238, "Satellite Payload Mass 600 kg"]
+[8.953232765197754, 8.509952545166016, "Satellite Payload Power Consumption 800 W"]
+[8.955572128295898, 8.512144088745117, "Satellite Payload Data Production 103 Gb/day"]
+[-5.348121166229248, 2.85200572013855, "Telescope Optical Configuration 6 lenses, plus one window"]
+[-5.460880756378174, 2.7115330696105957, "Telescope Entrance Pupil Diameter 120 mm"]
+[-5.344089984893799, 2.751797676086426, "Telescope Field of View Up to 18.9\u00b0"]
+[1.0092840194702148, -4.401092529296875, "Satellite Mass 125 kg"]
+[0.9425886869430542, -4.435329437255859, "Satellite Mass 195 kg"]
+[-3.4076380729675293, 7.215939521789551, "Data Handling System Data Storage Volume 130 GB"]
+[6.331000804901123, 7.411633491516113, "Satellite Component Components System Controller (SC), Data Processor (DP)"]
+[4.09206485748291, 13.931561470031738, "Laser Altimeter Measurement Elevation"]
+[4.103572368621826, 13.93710708618164, "Laser Altimeter Measurement Atmospheric Backscatter"]
+[2.6885643005371094, -1.1912904977798462, "Satellite Objective 1 Quantify the polar ice sheet mass balance"]
+[2.655224561691284, -1.2118136882781982, "Satellite Objective 2 Determine the seasonal cycle and topographic character of ice sheet changes"]
+[2.607494592666626, -1.2139164209365845, "Satellite Objective 3 Estimate sea ice thickness"]
+[-3.1234822273254395, 4.21397590637207, "Spacecraft Launch Location Cape Canaveral, Florida"]
+[-3.071582078933716, 4.248164653778076, "Spacecraft Landing Location Pacific Ocean off the west coast of the United States"]
+[-0.12619760632514954, 6.899414539337158, "Test Number of Orbits 2"]
+[-0.1341516673564911, 6.866902828216553, "Test Altitude Higher than any achieved by a spacecraft intended for human use since 1972"]
+[-0.11223488301038742, 6.8475494384765625, "Test Landing Speed Higher than a low altitude orbital mission"]
+[11.394996643066406, 5.595710277557373, "CubeSat Ejection Velocity ~ 0.05 m/s"]
+[-1.1113197803497314, 7.874451637268066, "Deorbiting Technology Provides a larger target area Unknown"]
+[-2.5061118602752686, 8.328847885131836, "Capture Device Ejection Velocity Unknown"]
+[-1.0426483154296875, 7.664912700653076, "Device Reel in the neck of the net Unknown"]
+[-2.6003811359405518, 9.617289543151855, "Power Source Purpose Ensure a sufficient power supply for NASA\u2019s exploration technology demonstrations for Artemis and beyond as well as utilization and commercialization"]
+[-0.06933815032243729, 13.606104850769043, "Measurement Instrument Function Measure the distance change between the two satellites"]
+[-0.055466488003730774, 13.673803329467773, "Measurement Instrument Power Down Date July 19"]
+[-0.0748705342411995, 13.630622863769531, "Measurement Instrument Backup Redundant systems"]
+[-0.05969608575105667, 13.674447059631348, "Measurement Instrument Power Up Date October 19"]
+[-3.8921167850494385, 7.976881980895996, "Data Storage Capacity 16 Gbit"]
+[-5.272294044494629, 8.032276153564453, "Communication System Frequency 2.2 GHz"]
+[-5.238393306732178, 7.742365837097168, "Communication System Downlink Data Rate 400 kbit/s"]
+[-5.22515869140625, 7.772912502288818, "Communication System Uplink Data Rate 20 kbit/s"]
+[-5.271336078643799, 8.025989532470703, "Communication System Frequency 8 GHz"]
+[-5.140924453735352, 7.738293170928955, "Communication System Data Rate 16.8 Mbit/s"]
+[-5.322466850280762, 7.834897518157959, "Communication System Modulation Scheme QPSK"]
+[-5.280487537384033, 7.472947597503662, "Protocol Standard CCSDS"]
+[6.304987907409668, 7.430130958557129, "Satellite Component Deployment Time Within the first hour of the launch"]
+[6.3505988121032715, 7.381361484527588, "Satellite Component Deployment Time Long after launch"]
+[6.339420318603516, 7.395106792449951, "Satellite Component Endurance Up to several months in orbit"]
+[-3.311659574508667, 7.3996477127075195, "Data Processing System Designers P. D. Beaulne, C. H. Gierull, C. E. Livinstone, I. C. Sikaneta, S. Chiu, S. Gong, M. Quinton"]
+[1.3193151950836182, -2.0738637447357178, "Satellite Function Test Plan Presenters P. D. Beaulne, C. E. Livingstone"]
+[0.1367776244878769, 7.185498237609863, "Experiment Presenters Shen Chiu, Chuck Livingstone, Ishuwa Sikaneta, Christoph Gierull, Pete Beaulne"]
+[-1.8164665699005127, 8.33824348449707, "Proof Mass System Material Gold coated ultra low expansion silica"]
+[-1.8323029279708862, 8.330129623413086, "Proof Mass System Motion Detection Capacitive sensors"]
+[-1.845083236694336, 8.352219581604004, "Proof Mass System Actuation Quasi DC actuation voltages"]
+[-1.8887550830841064, 8.353005409240723, "Proof Mass System Vacuum Level Maintenance Getter material"]
+[-1.8926560878753662, 8.397012710571289, "Proof Mass System Ion Pump Used to maintain the vacuum and monitor the level of residual pressure"]
+[-1.8692259788513184, 8.429044723510742, "Front End Electronics Unit Contents Position sensing, analog control loops, Analog to Digital Sigma Delta converters"]
+[-1.8841381072998047, 8.48940372467041, "Front End Electronics Unit Contents Precise and stable references voltages Vp for actuation linearization, Vd for position sensing and Vref for Analog to Digital accurate conversion"]
+[-1.9104223251342773, 8.335412979125977, "Front End Electronics Unit Contents FPGA"]
+[2.865631103515625, -0.9606546759605408, "Satellite Purpose SAR surveys of land and ice"]
+[2.821133852005005, -1.753816843032837, "Satellite Program Very similar to SeaSat"]
+[-1.1372673511505127, 6.6604533195495605, "Project Purpose Satellite altimetry"]
+[2.5446085929870605, -1.570765733718872, "Satellite Program SAR (Synthetic Aperture Radar)"]
+[2.788292407989502, -1.583524227142334, "Satellite Program Navy satellite program to complete SeaSat altimetry mission"]
+[2.868725299835205, -1.135623574256897, "Satellite Purpose Advanced altimeter satellite for ocean circulation"]
+[-1.0499534606933594, 7.729933738708496, "Device Type DoD multifrequency microwave radiometer"]
+[5.257823467254639, -4.3916120529174805, "Geosynchronous Satellite Launch Date November 23, 1977"]
+[1.986549973487854, -2.2410688400268555, "Geosynchronous Satellite Provision of Satellite Data Continuous basis"]
+[3.268306016921997, -2.7607951164245605, "Geosynchronous Satellite Exploitation Period November 1983 until November 1995"]
+[7.275294303894043, 12.40672492980957, "Satellite Instrument Imagery First Imagery"]
+[2.314030170440674, -1.0716665983200073, "Satellite Imagery First Imagery"]
+[0.08830069750547409, 4.6267571449279785, "Volcano Eruption Date 19 January 2022"]
+[0.5975092649459839, 4.299576282501221, "Weather Phenomenon Image Date 26 October 2021"]
+[1.4293456077575684, 2.770941972732544, "Weather Satellite Operation Duration Nearly five years"]
+[1.4535272121429443, 2.7446670532226562, "Weather Satellite Operation Duration Until mid-August 1991"]
+[1.4664984941482544, 2.731654167175293, "Weather Satellite Type Civil and military low-altitude weather satellite"]
+[-0.021699925884604454, 15.196041107177734, "Scintillation Material Material Cesium Iodide"]
+[0.8016706109046936, 12.37148666381836, "Light Sensors Position Mounted to the large face of the detector"]
+[-1.8885000944137573, 8.472665786743164, "Front-End Electronics Function Convert the current sources of the SiPMs into voltage"]
+[3.7447564601898193, 17.694915771484375, "Payload Interface Unit Function Performs the final signal processing for energy determination and time stamping"]
+[3.7269818782806396, 17.698627471923828, "Payload Interface Unit Function Provides the power supply for the FEE and SiPMs"]
+[2.4728713035583496, -1.2322661876678467, "Satellite Data Small-Scale Structure of the Geodynamo"]
+[2.5158162117004395, -1.248917818069458, "Satellite Data Small-Scale Structure of the Geodynamo"]
+[-3.5102386474609375, 6.807965278625488, "Data Model Input Field-Aligned Currents"]
+[0.9325377941131592, -4.431122779846191, "Satellite Mass 6 ton"]
+[1.0939946174621582, -0.9627834558486938, "Satellite Height 6 m"]
+[1.2052260637283325, -1.2258093357086182, "Satellite Solar Arrays Area 144 m2"]
+[1.1366679668426514, -1.2494596242904663, "Satellite Solar Arrays Span Over 40 m"]
+[2.1170239448547363, -2.4008872509002686, "Satellite Propulsion System Hybrid"]
+[2.051046371459961, -2.414583206176758, "Satellite Propulsion System Electric propulsion for the cruise and spiral down phases and chemical propulsion for Mars orbit insertion"]
+[1.3627885580062866, -1.0405067205429077, "Satellite Resolution 50 cm"]
+[2.1792192459106445, -1.3371667861938477, "Satellite Imaging Capabilities Short-wave infrared (SWIR) for low light and nighttime imaging"]
+[4.1193623542785645, -2.4806771278381348, "Satellite Revisit Time One-hour average dawn-to-dusk imaging revisits"]
+[4.270549297332764, -2.8397581577301025, "Satellite Delivery Time 90-minute average delivery times"]
+[-10.26443099975586, 9.977768898010254, "Accelerometer Development Status Unknown"]
+[-10.2653169631958, 9.977865219116211, "Accelerometers Development Status Unknown"]
+[1.759926438331604, -2.070716619491577, "Satellite Aero Attitude Control Modes Aero-braking mode, Aero-through mode"]
+[2.006971836090088, -1.848712682723999, "Satellite Attitude Mode NM-PX or the NM-MX"]
+[1.7931329011917114, -2.042341709136963, "Satellite Attitude Mode NM-Z"]
+[4.191162586212158, -2.8708531856536865, "Satellite Duration of Attitude Modes About 40% of the orbital period"]
+[1.4701423645019531, -2.4064793586730957, "Satellite Orbit Type Elliptical polar orbit"]
+[0.7597858309745789, -1.5690598487854004, "Satellite Perigee 655 km"]
+[0.6773064136505127, -1.518473744392395, "Satellite Apogee 857 km"]
+[0.6696674227714539, -2.343083143234253, "Satellite Inclination 96.5\u00ba"]
+[4.05411958694458, -2.8082120418548584, "Satellite Period 100 min"]
+[4.2224273681640625, -3.0110344886779785, "Satellite Initial Local Equator Crossing Time 14:39 hours"]
+[4.005984306335449, -2.7862296104431152, "Satellite Orbit Drift Approximately 0.91 minutes in local time each day"]
+[0.6985548734664917, -1.5898981094360352, "Satellite Updated Perigee 640 km"]
+[0.656035840511322, -1.5970410108566284, "Satellite Updated Apogee 845 km"]
+[4.093690872192383, -2.8203229904174805, "Satellite Updated Period 99.7 minutes"]
+[-1.8400746583938599, 14.822123527526855, "Radiometer Objectives Measurement of sea surface temperature (SST), soil water content (moisture), sea wind speed, water equivalent of snow cover, precipitation intensity, sea ice distribution, precipitable water"]
+[-2.9816105365753174, 16.16810417175293, "Scatterometer Manufacturer NASA/JPL"]
+[-0.1339963972568512, 15.551801681518555, "Spectrometer Manufacturer Japanese Environment Ministry"]
+[2.815065622329712, 22.456729888916016, "Instrument Type Polarization and Directionality of the Earth's Reflectance"]
+[-3.804037570953369, 6.93001127243042, "Data Collection Instrument Developers NASDA and CNES"]
+[4.876116752624512, -2.441772699356079, "Satellite Mission Lifetime 5 years"]
+[3.1116557121276855, -1.8123763799667358, "Satellite Extended Mission Phase Ongoing"]
+[2.421799898147583, -1.4332894086837769, "Satellite Agility Able to take imagery over the disaster area during its first pass"]
+[0.2122371941804886, 13.812560081481934, "Calibration Device Dimensions 48 m x 48 m"]
+[0.24473392963409424, 13.816621780395508, "Calibration Device Dimensions 30 m x 30 m"]
+[-5.0636138916015625, 8.110174179077148, "Communication Component Mass ~70 kg"]
+[-5.079825401306152, 8.126545906066895, "Communication Component Mass ~70 kg"]
+[-5.044954776763916, 8.129889488220215, "Communication Component Mass ~70 kg"]
+[-5.0505051612854, 8.131869316101074, "Communication Component Mass ~70 kg"]
+[1.6539194583892822, -1.5344048738479614, "Satellite Shape Octagonal prism"]
+[1.132511854171753, -0.7196744084358215, "Satellite Dimensions 40 cm in diameter and a height of 25 cm"]
+[1.1347496509552002, -0.7153231501579285, "Satellite Tray Dimensions Octagonal plates of 150 mm side with an overall height of 250 mm"]
+[1.1398630142211914, -0.6997793912887573, "Satellite Column Dimensions Aluminium threaded rods, 6 mm in diameter"]
+[1.7029078006744385, -2.1854498386383057, "Satellite Attitude Control Passive magnetic attitude control"]
+[1.8670734167099, -2.1607227325439453, "Satellite Energy Dissipation System Three magnetic hysteresis rods"]
+[1.7180407047271729, -1.885179877281189, "Satellite Attitude Sensor COTS three-axes magnetoresistive magnetometer (TAM)"]
+[1.611127257347107, -1.9591535329818726, "Satellite Attitude Determination Magnetometer readings and the telemetry data of three solar panels"]
+[-7.484032154083252, 5.962954044342041, "Camera Head Unit CCD Device Resolution 752 x 588 pixel"]
+[-7.491342544555664, 5.960996150970459, "Camera Head Unit Mass 1.647 kg"]
+[-7.474265098571777, 5.979982376098633, "Camera Head Unit Power Consumption 4.5 W"]
+[16.767906188964844, 6.92924690246582, "SAR Microsatellite Mass <100 kg"]
+[11.829651832580566, 5.297486782073975, "6U CubeSat Mass ~10 kg"]
+[11.804621696472168, 5.311431884765625, "6U CubeSat Purpose Test attitude control, power, and communication systems as well as a photo-display-and-retransmission system"]
+[11.587380409240723, 5.486880302429199, "1U CubeSat Purpose Radio amateur and technology research"]
+[11.562917709350586, 5.5230560302734375, "3U CubeSats Manufacturer Spire Global Inc."]
+[11.815336227416992, 5.308379173278809, "6U CubeSat Purpose Provide multispectral imagery of 22 m resolution on a swath of 220 km"]
+[11.891545295715332, 5.292258262634277, "3U CubeSat Mass 3.8 kg"]
+[11.052934646606445, 5.255264759063721, "Picosatellites Form Factor 0.25 CubeSat"]
+[11.816198348999023, 5.331977367401123, "3U CubeSat Purpose Technology demonstration and astronomy mission"]
+[1.0003916025161743, -4.395060062408447, "Satellite Total Mass 52 kg"]
+[0.9907311201095581, -4.403368949890137, "Satellite Total Mass 54 kg"]
+[1.1438292264938354, -0.6913941502571106, "Satellite Dimensions 440 mm x 440 mm x 420 mm"]
+[2.4157943725585938, -1.7056888341903687, "Satellite Structure Carbon/PEEK thermoplastic skinned Al honeycomb"]
+[2.0240695476531982, -1.95771324634552, "Satellite Thermal Control Passive"]
+[2.059756278991699, -0.7101667523384094, "Satellite Power Generation Four body-mounted GaAs solar panels"]
+[2.1002092361450195, -0.585206925868988, "Satellite Power Generation 46 Whr NiCd battery"]
+[2.17800235748291, -0.7147578597068787, "Satellite Power (at start of mission) 31 W (at 28 V)"]
+[2.1063156127929688, -0.6693264245986938, "Satellite Power (at start of mission) 33 W (at 28 V)"]
+[2.066190481185913, -0.5459399223327637, "Satellite Power Available to Payload 19 W (average), 120 W (peak)"]
+[1.5601210594177246, -2.276035785675049, "Satellite Stabilization Spin at 5 rpm"]
+[1.8470045328140259, -1.7908776998519897, "Satellite Attitude Sensing Subsystem V-slit sun/Earth sensors and analog sun sensors"]
+[1.7939411401748657, -2.1429994106292725, "Satellite Attitude Control Subsystem (ACS) Magnetorquer coils & cold gas thruster"]
+[-2.3799633979797363, 7.30997896194458, "Onboard computer Type Dual-redundant GEC/Plessey Mil Std SOS 1750a microprocessor"]
+[-3.378307342529297, 8.542550086975098, "Onboard computer memory Capacity Dual-redundant 128 kBytes SOS RAM, 64 kBytes ROM"]
+[2.757148027420044, -3.2605297565460205, "Satellite Communication Standard ESA packet TM/TC CCSDS standard"]
+[2.744781732559204, -3.2787926197052, "Satellite Communication Antenna 12 m antenna at DERA Lasham ground station (26 m DSN antennas)"]
+[3.672417163848877, 22.94083595275879, "Instrument Status Update Date March 12, 2015"]
+[3.608914852142334, 22.937618255615234, "Instrument Status Update Date Feb. 16, 2015"]
+[3.620833396911621, 22.902240753173828, "Instrument Status Update Date Feb. 26, 2015"]
+[-1.0747977495193481, 7.774809837341309, "Deorbit Device Inflatable Mast Extension 1m"]
+[-1.0878446102142334, 7.717530250549316, "Deorbit Device CFRP Booms Deployment Radially outwards"]
+[-1.1478499174118042, 7.856512069702148, "Deorbit Device Similarity to CubeSat InflateSAIL Very similar"]
+[1.8085532188415527, 22.18326759338379, "Instrument Spatial Resolution (VIS) 210 m"]
+[1.818593978881836, 22.02968978881836, "Instrument Spatial Resolution (TIR) 700 km"]
+[-1.2325949668884277, 13.313400268554688, "Solar Constant Instrument Solar Constant Channel Spectral Band 0.2 - 10.5 \u00b5m"]
+[-1.1965663433074951, 13.281844139099121, "Solar Constant Instrument Solar Constant Channel FOV 5\u00ba"]
+[-1.204817771911621, 13.282422065734863, "Solar Constant Instrument Solar Constant Channel Accuracy of One Measurement 0.05%"]
+[-1.0998303890228271, 13.231510162353516, "Solar Constant Instrument Reflected Radiation Channel Spectral Band 0.3 - 3.0 \u00b5m"]
+[-1.2266101837158203, 13.30845832824707, "Solar Constant Instrument Reflected Radiation Channel FOV 60\u00ba"]
+[-1.2297149896621704, 13.324422836303711, "Solar Constant Instrument Reflected Radiation Channel Accuracy 1%"]
+[1.6666957139968872, 6.965218544006348, "Communication Device Frequency 8.23 GHz"]
+[1.8025951385498047, 6.841856002807617, "Communication Device Data Rate Up to 100 Mbit/s"]
+[1.688267469406128, 6.953873634338379, "Communication Device Modulation QPSK/OQPSK (Quadrature Phase Shift Keying / Offset Quadrature Phase Shift Keying)"]
+[-2.935673475265503, 4.510096549987793, "Spacecraft Total Mass ~95 kg"]
+[-3.3807361125946045, 4.236650466918945, "Spacecraft Design Life 3 years"]
+[-3.8085384368896484, 7.5828752517700195, "Real-time Processing, Compression and Encryption Board Data Rate 100 Mbit/s"]
+[-2.9633359909057617, 9.58452320098877, "Intelligent Li-ion Battery Charge Regulator Battery Type Li-ion"]
+[4.733747482299805, -2.578526258468628, "Satellite Operation Duration 10 years"]
+[3.1715567111968994, -1.7848654985427856, "Satellite Owner Maxar Technologies Ltd."]
+[2.6239535808563232, -1.4059561491012573, "Satellite Technology State-of-the-art"]
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+[5.307013511657715, -4.418788909912109, "Satellite Launch Date May"]
+[-5.232820987701416, 7.871231555938721, "Communication System Successful Laser Connections 10,000"]
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+[-5.192034721374512, 7.718733787536621, "Communication System Data Download More than 500 terabytes"]
+[-1.5621304512023926, 12.799321174621582, "Lyot Coronagraph Optical Design Classically occulted Lyot coronagraph"]
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+[3.574467658996582, 13.329878807067871, "Flight Laser Energy Levels Increased and started to oscillate"]
+[3.6251330375671387, 13.310953140258789, "Flight Laser Energy Readings Stabilizing at lower than nominal values (~70 to 80% of nominal)"]
+[3.564976215362549, 13.30695629119873, "Flight Laser Optical Slab Fracture The crystal optical slab within the pre-amplifier assembly fractured towards the center at a point where thermal stress is low"]
+[-2.9999680519104004, 16.17058563232422, "Scatterometer Frequency 1.26 GHz"]
+[-2.991389513015747, 16.171112060546875, "Scatterometer Bandwidth 4 MHz"]
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+[-2.981905937194824, 16.166833877563477, "Scatterometer Transmit Power Level 200 W"]
+[-2.990452527999878, 16.175817489624023, "Scatterometer Noise Equivalent \u03c3o 0 dB to -40 dB"]
+[3.684410333633423, 22.961488723754883, "Instrument Launch Year 2013"]
+[2.425511360168457, -1.0613187551498413, "Satellite Imagery Usage Disaster monitoring, land-use (change) detection, environmental monitoring"]
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+[7.292539119720459, 12.413642883300781, "Satellite Instrument Imaging Wavelength 135.6 nm"]
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+[7.314781665802002, 12.375248908996582, "Satellite Instrument LBH Emission Production Mechanism Photoelectron impact on N2"]
+[7.291357040405273, 12.420478820800781, "Satellite Instrument 135.6 nm Emission Production Mechanism Photoelectron impact on O"]
+[-0.9615042209625244, 6.478930950164795, "Documentation Publisher Herbert J. Kramer"]
+[-0.9543663859367371, 6.446659564971924, "Documentation Edition 4th"]
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+[-0.962914228439331, 6.398837089538574, "Scientific Journal Publication Name Astrophysical Journal"]
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+[2.963857412338257, -2.7689709663391113, "Telecommunications Satellite Technology Fully-digital and highly-innovative"]
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+[-0.8585835695266724, 6.144245624542236, "Downlink Specifications Unknown"]
+[-1.961670160293579, 8.052496910095215, "System Overview Unknown"]
+[-4.952452182769775, 9.764395713806152, "Receiver Endurance Against L-band SAR signal"]
+[1.4640474319458008, -2.3071954250335693, "Satellite Orbit Control Requirement Within 500 m orbital tube"]
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+[-0.9321570992469788, -10.023075103759766, "Satellite Constellation Number of Galileo FOC satellites 2"]
+[-0.6992865204811096, 5.097762107849121, "Country Plan Incorporate Canada-supplied L-band SAR repeaters on 24 GPS satellites"]
+[2.0606629848480225, -0.7587620615959167, "Remote Sensing Satellite Image Distribution Approximately 90,000 images"]
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+[-0.33701181411743164, 3.8176536560058594, "Planet Size 1.8 times bigger than Jupiter"]
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+[-0.3563673496246338, 3.7865090370178223, "Planet Dayside Temperature 7,800\u00ba Fahrenheit (4,300\u00ba C)"]
+[4.840167045593262, -4.468660354614258, "Satellite Image Acquisition Date April 5th, 2016"]
+[-1.9168866872787476, 8.128643035888672, "System Unknown Unknown"]
+[3.730058431625366, 17.708309173583984, "Payload High Performance Computing and Application Flexibility Unknown"]
+[2.9218924045562744, -2.116471767425537, "Sub-satellite Nodal Position Unknown"]
+[2.9680614471435547, -2.2069215774536133, "Sub-satellite Nodal Position Unknown"]
+[3.675546884536743, -2.4845454692840576, "Sub-satellite Mission Life About a week"]
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+[3.0467453002929688, -2.199838876724243, "Sub-satellite Operating Concepts Unknown"]
+[4.688979625701904, -2.634544610977173, "Satellite Operation Duration 9 years"]
+[2.6994996070861816, -2.0404303073883057, "Satellite Anomalies 43 AROs (Automatic Reconfiguration Orders) and lots of error events"]
+[2.502655506134033, -2.0390372276306152, "Satellite Permanent Failures IRU malfunction and gyro-A noise"]
+[4.768616199493408, -3.3209500312805176, "Satellite Operation Expectation Next decade"]
+[-3.581831455230713, 4.4001078605651855, "Spacecraft Splashdown Date Dec. 5, 2014"]
+[-3.062018871307373, 4.253178119659424, "Spacecraft Recovery Location Pacific Ocean"]
+[-2.9555938243865967, 4.199891567230225, "Spacecraft Peak Temperature 2,200\u00b0C"]
+[-2.871659517288208, 4.3807220458984375, "Spacecraft Speed Before Jettisoning 480 km/hr"]
+[5.114227294921875, -4.271262168884277, "Satellite Vibration Testing Date April 2021"]
+[3.0820212364196777, -1.6677353382110596, "Satellite Principal Investigator Brian Walsh"]
+[5.139754295349121, -4.393463611602783, "Satellite Departure Date July 2021"]
+[-0.4375154376029968, 15.909302711486816, "Ultraviolet Imaging Spectrograph Observation Target Earth"]
+[-0.454839825630188, 15.913923263549805, "Ultraviolet Imaging Spectrograph Observation Type Earth's Upper Atmosphere"]
+[-0.41597965359687805, 15.875712394714355, "Ultraviolet Imaging Spectrograph Observation Start Date October 2018"]
+[-0.46028414368629456, 15.875494956970215, "Ultraviolet Imaging Spectrograph Observation Target Changes Western Hemisphere"]
+[-0.9926857948303223, -9.953632354736328, "Satellite Constellation Transfer Date May 1998"]
+[-0.9535995125770569, -9.983678817749023, "Satellite Constellation Transfer Date May 1998"]
+[-0.9547399878501892, -9.987911224365234, "Satellite Constellation Launch Date 2009"]
+[2.540508985519409, -1.6328667402267456, "Satellite Payload Three telescopes and four spectrometers"]
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+[2.6704890727996826, 21.5620059967041, "Science Instrument Mass 314 kg"]
+[2.7249350547790527, 21.60992431640625, "Science Instrument Purpose Surveys severe thunderstorms in Earth\u2019s atmosphere and upper-atmospheric lightning"]
+[-1.3555725812911987, 13.307577133178711, "Solar Cell Technology Experiment Objective To measure the IV curves of up to 47 new solar cell and coverglass technologies"]
+[-1.38185453414917, 13.34281063079834, "Solar Cell Technology Experiment Number of Solar Cells Up to 47"]
+[-1.3757861852645874, 13.370299339294434, "Solar Cell Technology Experiment Parts Flight demonstration of advanced cells on the power generating panels of STRV-1c/d and in-flight measurement of the current-voltage characteristics of 38 individual solar cells"]
+[0.13203704357147217, 7.241100788116455, "Sample Cell Dimensions 62 mm long by 38 mm wide"]
+[0.15252161026000977, 7.218992710113525, "Sample Cell Enclosure Three-layer thermostat"]
+[0.124119333922863, 7.199596881866455, "Experiment Canister Mounting Two adjacent canisters"]
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+[-1.15147066116333, 8.699670791625977, "Canister Components Data acquisition and control electronics, power conditioning systems"]
+[4.847144603729248, -4.493841648101807, "Satellite Data Acquisition Date Dec. 31, 2014"]
+[4.315786838531494, -2.843567371368408, "Satellite Image Delivery Time Typically within 1 hour"]
+[4.980104923248291, -4.401900291442871, "Satellite Calibration Experiment Date Nov. 2014"]
+[1.9137157201766968, -1.4294030666351318, "Satellite Calibration Experiment Targets Triangular tetrahedral corner reflectors"]
+[1.452510952949524, -1.1239069700241089, "Satellite Height Measurement Precise"]
+[-2.8695781230926514, 1.6344455480575562, "Earth-observing mission Data Collection Decades-long record"]
+[0.71988445520401, -2.274134635925293, "Satellite Surface Solar Zenith Angle Constraint < 70\u00b0"]
+[0.7215098142623901, -2.243598222732544, "Satellite Latitude Range for Surface Target Detection -43\u00b0 to 46\u00b0"]
+[0.7721154689788818, -2.2170586585998535, "Satellite Longitude Range for Surface Target Detection -86\u00b0 to 79\u00b0"]
+[0.7847148776054382, -2.2186594009399414, "Satellite View Angle Range -60\u00b0 to 60\u00b0"]
+[0.6462106108665466, -2.2274956703186035, "Satellite Ground Track Distribution -30\u00b0 ~ 10\u00b0"]
+[4.341920375823975, -2.7623045444488525, "Satellite Observation Duration 8-10 minutes"]
+[0.6831696033477783, -2.3267159461975098, "Satellite Maximum Slew Rate 0.6\u00b0/s"]
+[1.9203852415084839, 10.706710815429688, "Imaging Device Lens System Wide field-of-view (FOV) lens of 30\u00ba"]
+[1.9332270622253418, 10.696610450744629, "Imaging Device Detector Size 1280 x 1024 pixels"]
+[1.917066216468811, 10.7304048538208, "Imaging Device Star Tracking Capability Yes"]
+[1.9110468626022339, 10.709248542785645, "Imaging Device Technology Chosen over CCD technology because of their power efficiency and performance"]
+[1.9491395950317383, 10.689920425415039, "Imaging Device Main Use Take snapshots of targets of interest (Earth, moon, etc.)"]
+[1.5304006338119507, 21.243223190307617, "Instrument Mass \u2264140 kg"]
+[1.6413437128067017, 23.20208168029785, "Instrument Power Consumption \u2264200 W"]
+[-7.486160755157471, 5.972188472747803, "Camera Function Obtain three-dimensional stereo image of the lunar surface"]
+[-1.5043952465057373, 16.898420333862305, "Altimeter Function Probe the features of the lunar soil and the space environment near the moon"]
+[-0.07871325314044952, 15.530895233154297, "Spectrometer Function Obtain the abundances and distributions of various elements/materials on the lunar surface"]
+[-0.039663370698690414, 15.480059623718262, "Spectrometer Function Explore the lunar soil properties"]
+[-0.07623202353715897, 15.529167175292969, "Spectrometer Function Explore the lunar soil properties"]
+[-1.8780391216278076, 14.953365325927734, "Radiometer Function Explore the lunar soil properties"]
+[-3.665822744369507, 12.719512939453125, "Particle Detector Function Probe the near-moon space environment"]
+[-0.8735737204551697, 11.836641311645508, "Ion Detector Function Probe the near-moon space environment"]
+[-0.8634492754936218, 0.17423968017101288, "Satellite System Presentation Date 1-5 October 2018"]
+[-0.8685087561607361, 0.19572383165359497, "Satellite System URL https://iafastro.directory/iac/proceedings/IAC-18/IAC-18/A7/3/manuscripts/IAC-18,A7,3,2,x47061.pdf"]
+[-0.8632470369338989, 0.1781187802553177, "Satellite System Presentation Date 17 July 2017"]
+[-0.8450294137001038, 0.16630184650421143, "Satellite System URL http://www.esa.int/Our_Activities/Space_Engineering_Technology/"]
+[-2.982933521270752, 16.15826416015625, "Satellite Scatterometer Geophysical Evaluation Remotely Sensed Wind Vectors Over the Ocean"]
+[2.537824869155884, -1.496518850326538, "Satellite Legacy Satellite Scatterometer Wind Vector Measurements"]
+[2.322981119155884, -1.3948339223861694, "Satellite SAR SeaSat Sees the Winds with SAR"]
+[-13.66539478302002, -2.3212857246398926, "X-ray Telescope First Look Date 22 October 2019"]
+[-13.720739364624023, -2.2702505588531494, "X-ray Telescope All-Sky Survey Date 19 June 2020"]
+[11.24948501586914, 5.520979881286621, "CubeSat Mission Date Aug. 4-9, 2018"]
+[11.381847381591797, 5.595953941345215, "CubeSat URL https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4067&context=smallsat"]
+[11.197303771972656, 5.519874095916748, "CubeSat Deployment Date 7 Dec. 2017"]
+[11.36107349395752, 5.585982799530029, "CubeSat URL https://www.jpl.nasa.gov/news/news.php?release=2017-314"]
+[0.6105265617370605, -1.3632978200912476, "Satellite Orbital Altitude 891 km"]
+[1.0217342376708984, -2.031644821166992, "Satellite Side-Looking Capability \u00b145\u00ba"]
+[4.671738624572754, -2.5893282890319824, "Satellite Mission Duration 10 years"]
+[2.1532907485961914, -2.293548583984375, "Satellite Failed Components One gyro (out of four) and one reaction wheel (out of four)"]
+[1.6597977876663208, -1.610360860824585, "Satellite Monitoring Coverage More than 80 percent of global oil and gas production"]
+[2.632976531982422, -1.160035252571106, "Satellite Capability Measure emissions from industrial agriculture and other human-made methane sources"]
+[-0.4159407317638397, 14.511783599853516, "Imaging Instrument Application Taking images of cities at night, mapping fishing activities, light pollution and fires"]
+[-0.4200168251991272, 14.515955924987793, "Imaging Instrument Design Combination of custom built parts and ISS compatible COTS items"]
+[-0.4141973555088043, 14.520902633666992, "Imaging Instrument Components \"head\", \"legs\", lens support"]
+[-0.41919800639152527, 14.519044876098633, "Imaging Instrument Camera Nikon D3s"]
+[-0.41764673590660095, 14.520121574401855, "Imaging Instrument Lens Nikkor 400mm"]
+[-0.738227903842926, 1.3633174896240234, "Lunar Orbiter Propellant Left 520 kg"]
+[-0.7895204424858093, 1.3993858098983765, "Lunar Orbiter Mission Duration 6 months"]
+[-0.7296030521392822, 1.3602988719940186, "Lunar Orbiter Attitude Transition Twice"]
+[-0.7401481866836548, 1.3638246059417725, "Lunar Orbiter Orbit Maintenance Three times"]
+[0.6992881894111633, -4.12069845199585, "Satellite Launch Mass 720 kg"]
+[1.0843443870544434, -2.090336799621582, "Satellite Attitude Pointing Accuracy 0.1\u00ba"]
+[0.9760925769805908, -2.1437172889709473, "Satellite Attitude Rate Control Accuracy 0.001\u00ba/s"]
+[2.078993558883667, -0.5164805054664612, "Satellite Power 1400 W"]
+[1.1071503162384033, -2.0850894451141357, "Satellite Cross-Track Pointing Capability \u00b130\u00ba from nadir"]
+[5.311243057250977, -2.199152946472168, "Satellite Design Life 5 years"]
+[5.145084381103516, -4.410125255584717, "Satellite Retirement Date Late July 2006"]
+[4.871417045593262, -4.12677001953125, "Satellite Measurement Period June 2000 through July 2006"]
+[3.173887014389038, 22.973432540893555, "Instrument Status Still active"]
+[5.303048610687256, -4.452461242675781, "Satellite Announcement Date July 11, 2000"]
+[7.35516357421875, 12.510740280151367, "Miniaturized Helio Instrument Delivery Date Fall"]
+[-5.198570251464844, 7.811821937561035, "Telecommunication Standard Receiver Type Commercial mass-market"]
+[-4.776065349578857, 9.264196395874023, "Transmitter Telemetry Standard DVB-S2 CCSDS"]
+[-4.609755516052246, 7.814938068389893, "Telemetry Mode Data Increase 60%"]
+[-4.620981216430664, 7.793154716491699, "Telemetry Mode Link Budget Improvement About 2 dB in QPSK for the same transmitted power"]
+[-4.567149639129639, 7.8135085105896, "Telemetry Mode Spectral Efficiency Better"]
+[2.96091365814209, -1.3834739923477173, "Satellite Mission Gather observations of greenhouse gases"]
+[2.9463469982147217, -1.294451117515564, "Satellite Mission Provide observation data to environmental administrations and drive international anti-global warming efforts"]
+[-2.642592668533325, 11.69035530090332, "Imager Product Cloud Masks, Cloud Type, Cloud Top Temperature, Cloud Top Pressure, Cloud Optical Depth, Cloud Liquid Water, Cloud Particle Size Distribution, Aerosol Detection, Aerosol Optical Depth, Downward Longwave Radiation, Upward Longwave Radiation, Reflected Shortwave Radiation"]
+[-2.643275499343872, 11.684844017028809, "Imager Product Derived Motion Winds, Lightning Detection, Rainfall Rate /QPE, Convective Initiation, Tropopause Folding Turbulence Prediction, Sea Surface Temperature (skin), Fire/Hot Spot Characterization, Land Surface (Skin) Temperature, Land Surface Emissivity, Snow Cover"]
+[-2.7772159576416016, 14.199599266052246, "Sounder Product Atmospheric Temperature, Humidity and Ozone Profiles (Clear), Atmospheric Temperature and Humidity Profiles"]
+[-3.661807060241699, 12.741535186767578, "Particle Detector Product Distribution of High Energy Particle Products, Intensity of Magnetic Field, Effects of Spatial Environment"]
+[-1.2741875648498535, 4.365771770477295, "Large Earth Station Max Data Rate (Mbit/s) Uplink: 1244 Downlink: 1244"]
+[-4.050677299499512, 7.282106399536133, "Super-high Data Rate VSAT Max Data Rate (Mbit/s) Uplink: 622 Downlink: 622"]
+[-4.059471607208252, 7.272339820861816, "High-data-rate VSAT Max Data Rate (Mbit/s) Uplink: 155 Downlink: 155"]
+[-5.783217906951904, 15.513276100158691, "Ultra Small Aperture Terminal Max Data Rate (Mbit/s) Uplink: 1.5-6 Downlink: 1.5-6"]
+[-1.2315757274627686, 4.387409687042236, "Large Earth Station Antenna Diameter 5 m"]
+[-4.052232265472412, 7.2552080154418945, "Super-high Data Rate VSAT Antenna Diameter 2.4 m"]
+[-4.0721282958984375, 7.2885003089904785, "High-data-rate VSAT Antenna Diameter 1.2 m"]
+[-5.783105373382568, 15.522150039672852, "Ultra Small Aperture Terminal Antenna Diameter 45 cm"]
+[-1.1682167053222656, 4.507761001586914, "Large Earth Station Tx Power 200 W"]
+[-4.059305191040039, 7.283675670623779, "Super-high Data Rate VSAT Tx Power 200 W"]
+[-4.049787521362305, 7.267688274383545, "High-data-rate VSAT Tx Power 100 W"]
+[-5.785392761230469, 15.510039329528809, "Ultra Small Aperture Terminal Tx Power 5-10 W"]
+[-1.2487131357192993, 4.403109550476074, "Large Earth Station EIRP > 78 dBW"]
+[-4.056046009063721, 7.310068607330322, "Super-high Data Rate VSAT EIRP > 76 dBW"]
+[-4.042889595031738, 7.2470927238464355, "High-data-rate VSAT EIRP > 66.9 dBW"]
+[-5.780457973480225, 15.522077560424805, "Ultra Small Aperture Terminal EIRP > 41.5 dbW"]
+[-1.236555576324463, 4.3936686515808105, "Large Earth Station G/T > 28.5 dB/K"]
+[-4.024917125701904, 7.262142181396484, "Super-high Data Rate VSAT G/T > 24.5 dB/K"]
+[-4.018801689147949, 7.263399600982666, "High-data-rate VSAT G/T > 19.0 dB/K"]
+[-5.784054279327393, 15.522652626037598, "Ultra Small Aperture Terminal G/T > 11.5 dB/K"]
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+[3.906587600708008, -2.9709112644195557, "Satellite LTDN 10:00 hours"]
+[1.5936981439590454, -2.4683876037597656, "Satellite Orbits/Day 14 orbits/day"]
+[0.7352807521820068, -1.234445333480835, "Satellite Initial Altitude 728 km"]
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+[2.054727792739868, -2.7032291889190674, "Satellite Total Photos 2.55 million"]
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+[-3.079707622528076, 9.650394439697266, "Battery Rated Voltage 1.2 V"]
+[-3.0827784538269043, 9.658318519592285, "Battery Stored Power 4200 mAh"]
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+[-1.6176261901855469, 7.373322486877441, "Experiment Computer System Design Highly generalized"]
+[-1.348067045211792, 6.186557292938232, "Organization Role Principal investigator for the attitude control experiment"]
+[-5.392889976501465, 2.8002047538757324, "Telescope Principal Investigator Fiona Harrison"]
+[-1.165077805519104, 3.062019109725952, "Celestial Object Age 5 years on Orbit"]
+[-0.9874810576438904, 3.123058319091797, "Active Galactic Nucleus Enshrouded Yes"]
+[-0.832145631313324, 3.1505517959594727, "Active Galactic Nucleus Cocooned Yes"]
+[11.293957710266113, 5.531638145446777, "CubeSat Mission Type Exoplanet Survey"]
+[11.379966735839844, 5.579407215118408, "CubeSat Number of Spacecraft Dozens"]
+[11.2157564163208, 5.4929423332214355, "CubeSat Target Star Monitoring One star at a time"]
+[-3.3200249671936035, 8.49997329711914, "Memory Device Die Capacity 8 Gbit"]
+[-3.305074691772461, 8.506932258605957, "Memory Device Die Capacity 512 Mbit"]
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+[-3.2182934284210205, 8.502204895019531, "Memory Device Operating Voltage 3.0 V \u2013 3.6 V"]
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+[-3.315950870513916, 8.507538795471191, "Memory Device Data Bus Width 8 bit"]
+[-3.2867321968078613, 8.503422737121582, "Memory Device Temperature Range - 40\u00baC to + 85\u00baC"]
+[-3.336747407913208, 8.514078140258789, "Memory Device Temperature Range 0\u00baC to +70\u00baC"]
+[-3.3125698566436768, 8.491739273071289, "Memory Device Maximum Read Performance < 250 Mbit/s @ 40 MHz on page level (4 k x 8)"]
+[-3.347989082336426, 8.53446102142334, "Memory Device Maximum Read Performance < 800 Mbit/s @ 100 MHz burst operation"]
+[-3.311815023422241, 8.488271713256836, "Memory Device Erase Time 2 ms on block level (256 k x 8)"]
+[-3.329401731491089, 8.510200500488281, "Memory Device Endurance > 10 5 \u221e"]
+[-3.3315439224243164, 8.496153831481934, "Memory Device Data Retention 10 years"]
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+[1.810503363609314, 22.24711799621582, "Instrument Beam Diameter 14-meter"]
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+[4.096924304962158, -2.81197452545166, "Satellite Orbit Period N/A"]
+[1.1737852096557617, -0.8299057483673096, "Satellite Size 1.9 times Earth\u2019s size"]
+[0.9897448420524597, -4.269547462463379, "Satellite Mass Ranges from two to 12 times Earth\u2019s"]
+[4.068648338317871, -2.8194963932037354, "Satellite Orbit Period N/A"]
+[1.1158818006515503, -0.8027442693710327, "Satellite Size Three times larger than Earth"]
+[0.986793041229248, -4.362171649932861, "Satellite Mass Holds between three and 16 times Earth\u2019s mass"]
+[4.104641437530518, -2.793593406677246, "Satellite Orbit Period N/A"]
+[1.1471312046051025, -0.8385154008865356, "Satellite Size Four times the size of our planet"]
+[1.0501810312271118, -4.471127033233643, "Satellite Mass Weighs between four and 19 Earth masses"]
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+[2.825382709503174, -1.0228550434112549, "Satellite Purpose Monitor water resources, agriculture, urban growth, land use, deforestation and burning of the Amazon rainforest"]
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+[1.8056071996688843, 22.2766170501709, "Instrument Resolution 16 m"]
+[1.6663929224014282, 21.9543514251709, "Instrument Swath Width 95 km"]
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+[3.1701712608337402, -1.7503093481063843, "Satellite Manufacturer LeoStella"]
+[2.2913997173309326, -2.599219560623169, "Satellite Cash Infusion $450 million"]
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+[1.510667324066162, 5.4129533767700195, "Satellite Bus Onboard Communication Bus 1553B+SpaceWire"]
+[1.5139514207839966, 5.421401500701904, "Satellite Bus Raw Data Transmission X-band"]
+[1.4865375757217407, 5.442770957946777, "Satellite Bus Output Power \u2265 3.2 kW"]
+[1.512947678565979, 5.423895835876465, "Satellite Bus Design Life 7 years"]
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+[0.5843373537063599, 11.946746826171875, "Sensor Mounting Location +x panel of the spacecraft"]
+[11.19217586517334, 5.523702621459961, "CubeSat Launch Date 21 November 2013"]
+[11.3009033203125, 5.504202842712402, "CubeSat Mission Objective Qualify several in-house built hardware and software components"]
+[11.153215408325195, 5.379756450653076, "CubeSat Components Fault tolerant power system, attitude determination & control algorithms, fine sun sensor, solar panel"]
+[6.349636554718018, 7.449589252471924, "Satellite Component Function Collect, store, and forward AIS messages globally"]
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+[6.323734283447266, 7.40135383605957, "Satellite Component Receiving Sensitivity -112 dBm"]
+[6.274240493774414, 7.4702582359313965, "Satellite Component Swath Width \u2265950 km"]
+[2.7700705528259277, 13.686132431030273, "Optical Device Material Zerodur"]
+[2.7625694274902344, 13.664305686950684, "Optical Device Material Zerodur"]
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+[2.77677845954895, 13.718697547912598, "Optical Device Function Mixes light output from the cavity with the input light from the laser"]
+[2.043851375579834, -2.7770395278930664, "Satellite Number of Satellites Up to four"]
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+[4.923164367675781, -3.523960828781128, "Service Agreement Start Date 2015"]
+[4.842460632324219, -3.3524107933044434, "Service Agreement End Date About 2030"]
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+[0.510543167591095, 9.244845390319824, "Motion Compensation Mechanism Launch Date December 21 2011"]
+[0.4550672173500061, 9.208728790283203, "Motion Compensation Mechanism Utilization ISS-based long-exposure imaging"]
+[0.4755680561065674, 9.22795295715332, "Motion Compensation Mechanism Design Crew-attended and operated device"]
+[0.5144292116165161, 9.211465835571289, "Motion Compensation Mechanism Mission Objective Assist the crew in taking high-resolution (long exposure) picture tracking of Earth targets at night from the Cupola"]
+[1.9206546545028687, 10.727269172668457, "Imaging Device Acquisition Date October 7, 2020"]
+[1.909855842590332, 10.7183837890625, "Imaging Device Acquisition Date October 15, 2017"]
+[0.819074273109436, 4.0764851570129395, "Measure of Sea Surface Temperatures Status Dropped below normal in May"]
+[0.5412735939025879, 4.375359535217285, "Climate Phenomenon Forecast To persist through at least the end of 2020"]
+[5.197938919067383, -4.271104335784912, "Satellite Launch Date June 27, 2023"]
+[5.333909034729004, -4.498844146728516, "Satellite Launch Date July 5, 2019"]
+[5.3674163818359375, -4.360108375549316, "Satellite Launch Date November 28, 2017"]
+[-2.9357776641845703, 4.471823215484619, "Spacecraft Mass 700 kg"]
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+[-3.5766372680664062, 4.402906894683838, "Spacecraft Launch Date Aug. 26, 2005"]
+[-3.545280933380127, 4.380732536315918, "Spacecraft Removal from Service Date August 2008"]
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+[2.862287998199463, -2.039780855178833, "Satellite Communication Status Lost"]
+[4.959176063537598, -4.448472499847412, "Satellite Last Communication Date Dec. 5, 2019"]
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+[-7.4952263832092285, 5.929548740386963, "Camera Focal Length 50 mm"]
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+[11.53042984008789, 5.737879276275635, "CubeSat Size 3U"]
+[11.51813793182373, 5.7248406410217285, "CubeSat Size 3U"]
+[11.530400276184082, 5.772364616394043, "CubeSat Size 1U"]
+[11.527202606201172, 5.743980884552002, "CubeSat Size 2U"]
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+[1.0214228630065918, 9.15880012512207, "Attitude and Orbit Correction Subsystem Attitude Knowledge 0.02\u00b0"]
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+[-4.603194713592529, 7.846055030822754, "Tracking, Telemetry and Control Data Rate 4 Kbit/s"]
+[-5.198974609375, 8.003890037536621, "Communication System Transmission Band X-band"]
+[-5.123846054077148, 7.746340274810791, "Communication System Data Rate Up to 640 Mbit/s"]
+[-2.4809181690216064, 4.9124755859375, "Space Debris Removal Device Diameter 5 m"]
+[-2.5290441513061523, 4.865962982177734, "Space Debris Removal Device Material Kevlar"]
+[-2.4932401180267334, 4.911436557769775, "Space Debris Removal Device Total Mass Approximately 0.6 kg"]
+[-2.4866299629211426, 4.9038310050964355, "Space Debris Removal Device Mesh Size 80 mm"]
+[0.768100917339325, 4.108180522918701, "Atmospheric Constituent Absorption at 1.24 \u00b5m 10 -21 mol cm -2"]
+[0.7639289498329163, 4.104958534240723, "Atmospheric Constituent Absorption at 1.42 \u00b5m 10 -22 mol cm -2"]
+[0.7897141575813293, 4.087521076202393, "Atmospheric Constituent Absorption at 0.90 \u00b5m 10 -21 mol cm -2"]
+[0.7693816423416138, 4.106553077697754, "Atmospheric Constituent Absorption at 1.2 \u00b5m 10 -21 mol cm -2"]
+[0.7741049528121948, 4.10259485244751, "Atmospheric Constituent Absorption at 1.4 \u00b5m 10 -19 mol cm -2"]
+[0.7654025554656982, 4.105201244354248, "Atmospheric Constituent Absorption at 1.63 \u00b5m 10 -22 mol cm -2"]
+[0.7562956213951111, 4.118801593780518, "Atmospheric Constituent Absorption at 1.67 \u00b5m 10 -20 mol cm -2"]
+[0.7660874724388123, 4.111454963684082, "Atmospheric Constituent Absorption at 1.265 \u00b5m 10 -19 mol cm -2"]
+[0.5457777380943298, 12.171804428100586, "Sensor Pointing Accuracy Within 0.01 degree"]
+[0.47221916913986206, 9.362910270690918, "Attitude Control System Quantity Three"]
+[0.4907636046409607, 9.365409851074219, "Attitude Control System Quantity Three"]
+[0.49440115690231323, 9.382291793823242, "Attitude Control System Function Update attitude position"]
+[0.4530881941318512, 9.399428367614746, "Attitude Control System Function Furnished pitch and roll information"]
+[0.4381342828273773, 9.393360137939453, "Attitude Control System Function Provided yaw information"]
+[-1.949215054512024, 7.364006042480469, "Computer Redundancy Two redundant central computers"]
+[5.272754669189453, -4.320367813110352, "Satellite Launch Date December 2016"]
+[2.8221685886383057, -0.9711671471595764, "Satellite Purpose Monitors global atmospheric CO2 concentrations and is capable of measuring SIF"]
+[-3.250377893447876, 7.466731548309326, "Algorithm SIF Emission Data Micro-Windows 757 nm and 771 nm"]
+[-3.2515130043029785, 7.518625736236572, "Algorithm O2 A-band Within the O2 A-band"]
+[1.7481460571289062, -1.2613286972045898, "Satellite Measurement Resolution Doubled compared with the Fengyun-4A satellite"]
+[1.7639803886413574, -1.3855525255203247, "Satellite Measurement Sensitivity Doubled compared with the Fengyun-4A satellite"]
+[3.690790891647339, 22.95212173461914, "Instrument Image Acquisition Date 1 February 2019"]
+[5.169371128082275, -4.424412727355957, "Satellite Operational Date May.8, 2018"]
+[5.319111347198486, -4.470403671264648, "Satellite Post Launch Test Finish Date Dec.31,2017"]
+[3.7370223999023438, 22.982940673828125, "Instrument Image Acquisition Date 1 February 2019"]
+[3.7238290309906006, 22.973520278930664, "Instrument Image Acquisition Date 1 February 2019"]
+[-3.104264259338379, 4.348028659820557, "Spacecraft Fuel Limited amount"]
+[-3.066584587097168, 4.302860260009766, "Spacecraft Cost-Benefit Analysis Factors Fuel use, satellite destruction cost, collision probability"]
+[-1.3797028064727783, 6.93423318862915, "Models Accuracy Not yet exist"]
+[-3.304391622543335, 4.1638689041137695, "Spacecraft Useful Lifespan Shortened by moving more often than needed"]
+[4.038057804107666, -2.86604905128479, "Satellite Data Latency <5 minutes"]
+[1.2809116840362549, -1.5016051530838013, "Satellite Positioning Accuracy 7 km"]
+[2.6336820125579834, -2.706883668899536, "Satellite Data Transmission Rate 19.2 kbit/s"]
+[2.802753210067749, -2.470264434814453, "Satellite Helical Antenna Frequency 1090 MHz"]
+[2.18993878364563, -2.1208558082580566, "Satellite Helical Antenna Gain 10 dB"]
+[2.813774824142456, -2.5275518894195557, "Satellite UHF Transceiver Frequency Range 435-438 MHz"]
+[2.7868847846984863, -2.545344114303589, "Satellite Patch Antenna Frequency 1592 MHz"]
+[1.0618654489517212, -2.077712297439575, "Satellite Pointing Accuracy 3\u00b0"]
+[0.5791014432907104, -1.4642966985702515, "Satellite Orbit Altitude Approximately 400 km"]
+[0.6675413250923157, -2.1841166019439697, "Satellite Orbit Inclination 51.6\u00b0"]
+[2.124204635620117, -2.7385809421539307, "Satellite Passes per Day 5"]
+[4.165734767913818, -2.7934134006500244, "Satellite Average Pass Length 7.4 minutes"]
+[0.9873215556144714, -4.382263660430908, "Satellite Mass 60 kg"]
+[0.9933943748474121, -4.390148639678955, "Satellite Mass 60 kg"]
+[0.9971959590911865, -4.378471851348877, "Satellite Mass 56 kg"]
+[1.0046800374984741, -4.404374122619629, "Satellite Mass 44 kg"]
+[16.8105411529541, 6.884719371795654, "Microsatellite Mass 55 kg"]
+[16.76471519470215, 6.927484512329102, "Microsatellite Mass 55 kg"]
+[16.79497528076172, 6.901036739349365, "Microsatellite Mass 56 kg"]
+[16.80026626586914, 6.895844459533691, "Microsatellite Mass 56 kg"]
+[17.231613159179688, 6.717694282531738, "Microsatellite Launch Status Failure"]
+[16.961042404174805, 6.756438255310059, "Microsatellite Launch Date 15 May 2021"]
+[16.95703887939453, 6.776612281799316, "Microsatellite Launch Time 11:11 UTC"]
+[16.87439727783203, 6.868593215942383, "Microsatellite Launch Vehicle Rocket Lab\u2019s Electron"]
+[17.48604393005371, 6.636662006378174, "Microsatellite Launch Site New Zealand"]
+[16.872331619262695, 6.856459617614746, "Microsatellite Launch Service Provider Rocket Lab"]
+[16.905214309692383, 6.826513767242432, "Microsatellite Launch Service Provider Spaceflight Inc."]
+[17.763460159301758, 6.54110050201416, "Microsatellite Launch Failure Cause Anomaly in the second stage of the launch vehicle"]
+[16.973739624023438, 6.79009485244751, "Microsatellite Launch Failure Investigation Status Under investigation"]
+[17.76289939880371, 6.54142951965332, "Microsatellite Launch Failure Issue Time Shortly after stage two ignition"]
+[17.762794494628906, 6.541409492492676, "Microsatellite Launch Failure Tweet The issue occurred shortly after stage two ignition"]
+[17.76296615600586, 6.541329860687256, "Microsatellite Launch Failure Tweet The issue occurred shortly after stage two ignition"]
+[17.763086318969727, 6.5412702560424805, "Microsatellite Launch Failure Tweet The issue occurred shortly after stage two ignition"]
+[17.764455795288086, 6.540798187255859, "Microsatellite Launch Failure Tweet The issue occurred shortly after stage two ignition"]
+[17.764265060424805, 6.540796756744385, "Microsatellite Launch Failure Tweet The issue occurred shortly after stage two ignition"]
+[17.765827178955078, 6.540210247039795, "Microsatellite Launch Failure Tweet The issue occurred shortly after stage two ignition"]
+[17.765033721923828, 6.540450096130371, "Microsatellite Launch Failure Tweet The issue occurred shortly after stage two ignition"]
+[17.764720916748047, 6.540924072265625, "Microsatellite Launch Failure Tweet The issue occurred shortly after stage two ignition"]
+[17.764419555664062, 6.541059494018555, "Microsatellite Launch Failure Tweet The issue occurred shortly after stage two ignition"]
+[17.76390266418457, 6.5415778160095215, "Microsatellite Launch Failure Tweet The issue occurred shortly after stage two ignition"]
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+[3.526762008666992, 13.43774127960205, "Laser Relay Service Technology Developed by European industry"]
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+[3.3275065422058105, 0.4638611972332001, "Satellite Program Rumors about Funding I\u2019ve heard rumours that you don\u2019t have enough money for Worldview Legion"]
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+[2.939948320388794, 22.29112434387207, "Instrument Technology State-of-the-art"]
+[-3.371598958969116, 8.5203218460083, "Mass Memory and Formatting Unit Technology NAND-Flash memory devices"]
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+[-1.145104169845581, 7.293308734893799, "Equipment Launch Date March 1983"]
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+[-3.493144989013672, 6.778329372406006, "Data Latency 2 days"]
+[-3.526376962661743, 6.777664661407471, "Data Latency 2 days"]
+[-3.464711904525757, 6.80101203918457, "Data Latency 21 days"]
+[-3.544996976852417, 6.783273220062256, "Data Latency 21 days"]
+[-3.478783130645752, 6.7838239669799805, "Data Latency 45 days"]
+[-3.5107955932617188, 6.789109230041504, "Data Latency 45 days"]
+[-3.4995107650756836, 6.777041435241699, "Data Latency 45 days"]
+[-3.499753713607788, 6.702998638153076, "Data Latency 45 days"]
+[-3.519533157348633, 6.74339485168457, "Data Latency 45 days"]
+[1.5757519006729126, -1.14542818069458, "Satellite Image Resolution Unspecified"]
+[4.965412139892578, -4.3526411056518555, "Satellite Observation Date Fall of 2012"]
+[3.2934658527374268, -1.4799209833145142, "Satellite Mission Type Non-EO"]
+[5.372367858886719, -4.41514778137207, "Satellite Launch Date 23-12-2017"]
+[2.6903727054595947, -1.8056919574737549, "Satellite Sensor Complement Unknown"]
+[2.715977430343628, -1.2763160467147827, "Satellite Specific Goals Verification of super low altitude satellite system, Measurement of atmospheric density in super low altitude, On-orbit monitoring of atomic oxygen"]
+[0.45772889256477356, 4.525366306304932, "Natural Phenomenon Extent 4.72 million km2"]
+[0.44220736622810364, 4.53299617767334, "Natural Phenomenon Extent 1.82 million square miles"]
+[0.46606770157814026, 4.527075290679932, "Natural Phenomenon Extent Trend Downward"]
+[0.45837295055389404, 4.5320892333984375, "Natural Phenomenon Multi-Year Ice Amount Second-lowest on record"]
+[0.4550621807575226, 4.502344608306885, "Natural Phenomenon Polar Ice Decline Since the start of the satellite record in the 1970s"]
+[-6.715677261352539, 9.978803634643555, "Antenna Health Check Experiment Conducted"]
+[3.4752566814422607, 10.552560806274414, "Amplifier Band Ka-band"]
+[2.568070411682129, -1.8494658470153809, "Satellite SAR C-band"]
+[-13.90291976928711, -2.237025737762451, "X-ray Telescope Purpose Capture X-ray light from regions near a supermassive black hole"]
+[-1.136879563331604, 3.324815511703491, "Black Hole Component Nature Superheated disk of material feeding the black hole"]
+[-1.119301438331604, 3.263423204421997, "Black Hole Component Nature Cloud of particles traveling near the speed of light"]
+[0.5529805421829224, 4.652164936065674, "Phenomenon Nature Reflected off the accretion disk"]
+[-1.0472877025604248, 7.7466816902160645, "Device Activation Frequency Every 2 minutes"]
+[-1.0126068592071533, 7.734386920928955, "Device Activation Times Between 1:00 and 4:18 (UTC), and between 13:00 and 16:18 (UTC)"]
+[-1.0625308752059937, 7.731792449951172, "Device Number of Activations per Day 438"]
+[-1.0330960750579834, 7.768542289733887, "Device Activation Times Between 21:00 and 4:18 (UTC), and between 9:00 and 16:18 (UTC)"]
+[2.767876625061035, 21.69404411315918, "Scientific Instrument Installation Date May 19, 2011"]
+[-2.4285221099853516, 7.933229923248291, "Verification and Validation System Purpose Eliminating false or erroneous signals"]
+[-1.912516474723816, 8.097870826721191, "System Purpose Removing non-stellar objects"]
+[-1.9269723892211914, 8.130149841308594, "System Purpose Propagating star centroids with a reasonable shape"]
+[-1.908860445022583, 8.137757301330566, "System Purpose Matched centroid and star list error distribution validation"]
+[-2.1814804077148438, 8.037124633789062, "Verification and Validation System Recovery Automatic and optimized for robustness and speed"]
+[-2.0808796882629395, 7.72307014465332, "Avionics System Computer GN&C flight software"]
+[-3.0760977268218994, 4.225157737731934, "Spacecraft Trajectory Lingering for many hours in the Van Allen radiation belts"]
+[-2.580406665802002, 8.788117408752441, "A/D Converter Sampling Frequency 80 MHz"]
+[-2.486874580383301, 8.743056297302246, "A/D Converter Bit Depth 14 bits"]
+[-2.447352647781372, 8.71356201171875, "A/D Converter Sampling Interval 12 \u00b5s"]
+[-3.4270923137664795, 8.07068920135498, "Signal Processing Order 9th order"]
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+[3.7385168075561523, 17.713773727416992, "Payload Communication Contact Time Almost 60 hours"]
+[3.7534265518188477, 17.682106018066406, "Payload Operating System Red Hat Linux 6.1"]
+[3.720485210418701, 17.69855308532715, "Payload Data Collection Interval 10 seconds"]
+[3.7295446395874023, 17.706199645996094, "Payload Data Collection Timestamp SYSLOG facility or application logs"]
+[2.860964298248291, 22.3633975982666, "Instrument Principal Investigator Professor Samuel Ting (MIT/CERN)"]
+[2.9446427822113037, 22.504884719848633, "Instrument Deputy Principal Investigator Stefan Schael"]
+[2.7777810096740723, 22.25554656982422, "Instrument Debris Shield Exposure Eight years"]
+[2.7811691761016846, 22.288227081298828, "Instrument Debris Shield Disposal Eventually burn up harmlessly in Earth\u2019s orbit"]
+[-3.159907579421997, 1.7062090635299683, "Satellite Mission Purpose Creating an artificial solar eclipse every day"]
+[2.6671197414398193, 22.438188552856445, "Instrument Imaging Capability Yes"]
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+[2.7187559604644775, 22.07524299621582, "Instrument Observation Location Low Earth orbit"]
+[-1.7741039991378784, 8.87429428100586, "Control System Redundancy One OBC is redundant, two TMC are redundant"]
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+[-2.326648235321045, 7.377739429473877, "On-Board Computer Software FCS (Flight Control Software)"]
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+[-2.008326768875122, 8.645526885986328, "Electronic System Cardframe Structure Grown and split into two separate units"]
+[-2.106745958328247, 8.653716087341309, "Electronic System CAN Bus Distributed data interface"]
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+[2.6365039348602295, 22.255352020263672, "Instrument Location European Southern Observatory's 3.6m Telescope"]
+[-4.565741062164307, -3.0831682682037354, "Exoplanet Radius 72 percent that of Earth's"]
+[-4.560552597045898, -3.0852973461151123, "Exoplanet Mass 55 percent that of Earth's"]
+[2.67643141746521, 21.984130859375, "Instrument Function Capture the reflections of signals sent by Sentinel-1 to Earth"]
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+[1.510250449180603, 21.222082138061523, "Instrument Mass 43 kg"]
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+[-3.4806768894195557, 7.6945271492004395, "Image Data Compression Algorithm Implementation Reconfigurable core in a high density, space qualified reconfigurable FPGA"]
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+[-0.961532473564148, 6.476844787597656, "Documentation Publisher Springer Verlag"]
+[-0.9568815231323242, 6.3853440284729, "Publication Year 2002"]
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+[4.299007415771484, -2.882518768310547, "Satellite Ground Station Acquisition Time About 75 minutes after launch"]
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+[-0.8386875987052917, 0.15161626040935516, "Satellite System Envelope Dimensions 180 x 88 x 102 mm"]
+[-0.8416306376457214, 0.16520383954048157, "Satellite System Wet Mass 3 kg"]
+[-1.2032004594802856, 8.59335708618164, "Component Capacity 1.5 kg"]
+[-1.2379244565963745, 8.594100952148438, "Component Actuation \u00b110\u00ba"]
+[-1.2280079126358032, 8.588998794555664, "Component Accuracy 0.1\u00ba"]
+[1.4632638692855835, -1.065795660018921, "Satellite Image Resolution 50-cm"]
+[1.5610265731811523, -1.1825222969055176, "Satellite Image Resolution 1-meter"]
+[3.87973690032959, -2.5091073513031006, "Satellite Daily Revisit Rate 15 times a day"]
+[3.4132304191589355, -2.6019506454467773, "Satellite Network Revisit Rate Six consistent visits per day"]
+[-1.3951237201690674, 6.93475866317749, "Model Aim Qualification with respect to environmental requirements relevant to the spacecraft structure and the thermal control system"]
+[-1.3776696920394897, 6.9184794425964355, "Model Objective Validate the electrical architecture and the on board software"]
+[-1.399027943611145, 6.914048671722412, "Model Purpose The final Spacecraft to be launched"]
+[-1.3521091938018799, 6.9082350730896, "Model Development Phase Phase 1"]
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+[-5.375270366668701, 2.7990100383758545, "Telescope Energy Range 10-200 MeV/n"]
+[-5.385872840881348, 2.819965124130249, "Telescope Detector Type Silicon"]
+[-5.37681245803833, 2.773444175720215, "Telescope Number of X-Y Planes 16"]
+[-5.4048686027526855, 2.7779078483581543, "Telescope Detector Dimensions 60 mm x 60 mm"]
+[-5.468034744262695, 2.714808225631714, "Telescope Detector Thickness 150\u00b115 \u00b5m for the first plane, and 380\u00b115 \u00b5m for the remaining 15 planes"]
+[-5.412116050720215, 2.7678747177124023, "Telescope Geometric Factor 8.6 cm 2 sr for low energy particles to 1 cm 2 sr for particles crossing the detector"]
+[-5.395151615142822, 2.7609786987304688, "Telescope Mass 40 kg"]
+[-5.392693519592285, 2.774221658706665, "Telescope Power 40 W"]
+[-5.258473873138428, 7.856889247894287, "Inter-Orbital Communication Subsystem Data Transmission Observation data"]
+[-3.005300521850586, 4.302823543548584, "Spacecraft Body Dimensions Approx. 4 m x 4 m x 5 m"]
+[-2.9910523891448975, 4.23408317565918, "Spacecraft Solar Paddle Dimensions Approx. 3 m x 26 m"]
+[-2.979983329772949, 4.469128608703613, "Spacecraft Launch Mass 3560 kg"]
+[-2.9563307762145996, 4.439435005187988, "Spacecraft Payload Mass 1300 kg"]
+[-3.0284576416015625, 4.366134166717529, "Spacecraft Power 4.5 kW"]
+[-3.2921903133392334, 4.211928844451904, "Spacecraft Design Life 3 years"]
+[-2.9999680519104004, 4.214318752288818, "Spacecraft Stabilization 3-axis stabilized with zero momentum attitude control"]
+[-3.5713186264038086, 4.394067764282227, "Spacecraft Launch Date August 17, 1996"]
+[-3.042659282684326, 4.283872127532959, "Spacecraft Launch Vehicle H-II"]
+[-5.358836650848389, 2.7540652751922607, "Focusing Telescopes Development Date 2005"]
+[-5.307549476623535, 2.716799736022949, "Telescope PDR Date June 9-10, 2009"]
+[-0.7929760217666626, 11.553987503051758, "Detection Chain Image Credit EADS Astrium SAS"]
+[-0.7993903160095215, 11.578927040100098, "Detector Image Credit EADS Astrium"]
+[-5.411709785461426, 2.7633895874023438, "Telescope Parameter Measurement Black hole's spin"]
+[-5.359359264373779, 2.7346386909484863, "Telescope Parameter Measurement Temperature variations in black hole winds"]
+[-5.465108394622803, 2.8116917610168457, "Telescope Parameter Measurement Distance particles in jets travel before they \"turn on\""]
+[-0.02886980213224888, 14.828042984008789, "Pulse Height Analyzer Purpose Improved dosimetry and measurement of linear energy transfer (LET) value"]
+[0.11139560490846634, 7.173980712890625, "NASA Sub-experiment Purpose Examine controversial elements of analog electronics in which the Elder's phenomena has been observed"]
+[0.030917255207896233, 7.112669467926025, "NASA Sub-experiment Purpose Examine synergistic radiation effects on a variety of newer state-of-the-art digital microcircuit and multi-chip module (MCM) technologies"]
+[0.07001020014286041, 7.134040832519531, "NASA Sub-experiment Purpose Examine new photonics technologies, in particular optocoupler components"]
+[-0.8374858498573303, 12.669318199157715, "Dose Radiation Shielding Experiment Purpose Provide a distribution of dosimeters in key spacecraft locations during the STRV-1d mission"]
+[-0.37113937735557556, 12.204916000366211, "Infrared Sensor Number of Detector Elements 4"]
+[-1.0336300134658813, 11.899928092956543, "Infrared Detectors Type HgCdTe detectors"]
+[-0.9357151389122009, 11.811671257019043, "Infrared Detectors Type InSb detectors"]
+[-0.7545733451843262, 8.569085121154785, "Cooler Operating Temperature 95 K"]
+[-0.7159067988395691, 8.590707778930664, "Cooler Temperature Stability Better than \u00b10.25 K"]
+[-1.6001408100128174, 1.4534887075424194, "Data Relay Transponder Data Relay Type Globally metrological, hydrological and oceanographic data"]
+[-1.6175986528396606, 1.4960508346557617, "Data Relay Transponder Downlink Frequency Extended C -band"]
+[6.335995197296143, 7.399738311767578, "Satellite Component Responsible for Generating estimates of the relative states \u2013 namely relative position, (linear) velocity, attitude, and angular velocity \u2013 of the S/C, in addition to (probabilistic or deterministic) bounds on the error of each estimate"]
+[6.352612495422363, 7.391583442687988, "Satellite Component Based on Extended Kalman Filtering (EKF) theory"]
+[0.7718964219093323, 11.926543235778809, "Sensors Integration The strategies for integrating the measurements from the available sensors (MIRU and VBS) must be carefully considered"]
+[-6.615063667297363, 10.018732070922852, "Antenna Interface Unit Function Command & control and power distribution"]
+[-2.6968626976013184, 8.166227340698242, "Column Drive Unit Quantity 16"]
+[-3.2172868251800537, 7.943205833435059, "Column Drive Unit Location One on each column"]
+[1.1440130472183228, -0.726340651512146, "Satellite Dimensions 3.5 x 3.5 cm"]
+[1.0322248935699463, -4.420960426330566, "Satellite Mass Just a few grams"]
+[4.362844467163086, -2.6985137462615967, "Satellite Expected Orbit Duration Merely a few days"]
+[-1.3431971073150635, 6.106529712677002, "Company Number of Satellites Deployed 231"]
+[-1.3496674299240112, 6.103588581085205, "Company Number of Satellites Deployed from Cygnus 35"]
+[1.5883419513702393, -2.2143609523773193, "Satellite Attitude Stabilization Passive Magnetic"]
+[-1.454639196395874, 7.98491907119751, "Deorbiting System Autonomy Autonomous"]
+[-5.305179595947266, 3.0596251487731934, "Telescope Array Mission Date May 13, 2013"]
+[-5.319385051727295, 3.130058765411377, "Telescope Array DOI 10.1088/0004-637X/770/2/103"]
+[1.9048510789871216, 22.76757049560547, "Instrument Photon Energy Range 20 keV-10 MeV"]
+[2.100452184677124, 22.495399475097656, "Instrument Measurement of Rise Time 10-100 \u00b5s"]
+[2.4116644859313965, 22.799562454223633, "Instrument Event Duration 10-100 ms"]
+[2.0571646690368652, 22.524843215942383, "Instrument Relative Time Resolution 1 \u00b5s"]
+[1.9125715494155884, 22.69264030456543, "Instrument Range of Relativistic Electrons 1 MeV - 10 MeV"]
+[2.3753278255462646, 22.322216033935547, "Instrument NaI Scintillators 900 cm2 detector area"]
+[3.7292027473449707, 17.695449829101562, "Payload Parameter Soil moisture - L band BT sensitive to soil moisture"]
+[3.71120285987854, 17.684415817260742, "Payload Parameter Sea Surface Salinity - L-band BT sensitive to SSS"]
+[3.7382357120513916, 17.703142166137695, "Payload Parameter Sea surface evaporation - Corrections for sea surface roughness"]
+[3.7312653064727783, 17.703187942504883, "Payload Parameter Freeze/thaw - Soil surface parameters"]
+[3.7345876693725586, 17.70754051208496, "Payload Parameter Snow water equivalence - Soil surface parameters"]
+[3.7530195713043213, 17.71392250061035, "Payload Parameter Vapour and precipitation - Help for determination of land surface emissivity"]
+[-2.133841037750244, 7.156391620635986, "On Board Software Main Task Keep an autonomous and safe operation environment, ensure housekeeping data generation and collection, manage communications windows, manage on board time, manage and execute TC"]
+[2.8639683723449707, -2.015536308288574, "Satellite Health Status Optimal"]
+[2.5187315940856934, -1.9191598892211914, "Satellite Antennas Deployment Confirmed"]
+[2.1974120140075684, -1.9968169927597046, "Satellite Solar Panels and Battery Deployment Confirmed"]
+[-2.1787140369415283, 7.1550211906433105, "On Board Software Patching Capability Included in this version"]
+[-10.263137817382812, 9.978455543518066, "Accelerometers Full-Scale Unit 5 gram"]
+[-10.259763717651367, 9.981040000915527, "Accelerometers Full-Scale Unit 2 gram"]
+[-3.6429145336151123, 8.047636985778809, "Solid State Recorder Board Purpose Evaluate the performance of HCSM (High Capacity Spaceborne Memory) SRAM module in the space environment"]
+[-0.7242651581764221, 12.423240661621094, "Environment Monitor Board Purpose Measure the temperature inside the Maple-1 enclosure"]
+[0.14154598116874695, 7.188558101654053, "Experiment Purpose Comparison of military grade commercial and radiation hardened bulk silicon anti-fuse-based field-programmable gate arrays"]
+[-2.3768465518951416, 7.276894569396973, "Onboard Computer Architecture Space Cube Architecture"]
+[-5.311500072479248, 7.467470645904541, "Communication Protocol URL http://spacewire.computing.dundee.ac.uk"]
+[-5.879385471343994, 15.997103691101074, "Synthetic Aperture Radar Data Product Levels Raw Signal Products (level-0), Geo-Tagged Products (level-1), Terrain-corrected Geocoded Products (level-2)"]
+[-2.908390522003174, 7.8148112297058105, "Data Processor Number of SMP Nodes 6"]
+[-3.0008254051208496, 7.763965129852295, "Data Processor Number of Cores per Node 8"]
+[-3.034886598587036, 7.763518810272217, "Data Processor Data Product Levels Raw Signal Products (level-0), Geo-Tagged Products (level-1), Terrain-corrected Geocoded Products (level-2)"]
+[2.5176808834075928, -1.8498438596725464, "Satellite Structure Bus module, payload module, ESS"]
+[-0.5147664546966553, 8.259139060974121, "Extendible Support Structure Function Deploy the antenna and provide rigid support"]
+[-6.687140464782715, 9.967048645019531, "Antenna Support ESS"]
+[-1.3278703689575195, 6.127444267272949, "Company Acquisition Bought by MDA"]
+[1.746195912361145, 6.93918514251709, "Communication Device Form Factor CubeSat with a height of about 4 cm"]
+[1.7200944423675537, 6.925838470458984, "Communication Device Diplexer Height About 2.5 cm"]
+[-6.650834560394287, 9.904052734375, "Antennas Frequency 2 GHz"]
+[-6.68844747543335, 9.961548805236816, "Antennas Quantity 2"]
+[-1.9732773303985596, 14.899543762207031, "L-band Radiometer Mission Date July 31-Aug. 4, 2006"]
+[-1.854111671447754, 14.83458423614502, "Radiometer Conference Date Sept. 20\u202224, 2004"]
+[7.140614986419678, 12.20698356628418, "Remote Sensing Model Conference Date Sept. 20\u202224, 2004"]
+[-2.4437170028686523, 13.189457893371582, "Hyperspectral Imager Spectral Bands Hundreds"]
+[-2.4315805435180664, 13.170842170715332, "Hyperspectral Imager Spectral Range Visible to far-infrared"]
+[-2.4507179260253906, 13.195550918579102, "Hyperspectral Imager Spatial Resolution Variable"]
+[-2.4549059867858887, 13.177359580993652, "Hyperspectral Imager Temporal Resolution None"]
+[2.6660916805267334, 5.386972904205322, "Emergency Beacon Quantity in Use About 350,000"]
+[2.5952892303466797, -2.4583098888397217, "Satellite Signal Cease Processing Date 1 February 2009"]
+[-3.8242478370666504, 8.425259590148926, "Signal Type False Alarm Rate 97 percent"]
+[2.665933132171631, 13.49668025970459, "Micropore Optical Element W/L Ratio 1/50"]
+[-8.26610279083252, 13.778671264648438, "Point Spread Function FWHM Less than 0.22\u00b0"]
+[-8.188272476196289, 13.809062004089355, "Point Spread Function Imaging Spatial Resolution Less than 0.22\u00b0"]
+[0.6956110000610352, -2.2371678352355957, "Satellite Star Temperature 2,700 to 5,000 degrees Kelvin"]
+[0.6683653593063354, -1.4554169178009033, "Satellite Closest Star Distance Approximately 6 light-years from Earth"]
+[2.069373369216919, -2.7533936500549316, "Satellite Number of Stars in Catalog 227"]
+[2.047752857208252, -2.704807758331299, "Satellite Number of Stars in Continuous Viewing Zone of James Webb Space Telescope 137"]
+[5.118292331695557, -4.086926460266113, "Satellite Launch Date April 2024"]
+[1.5755479335784912, -2.280501127243042, "Satellite Orbit Geostationary orbit 22,236 miles above Earth"]
+[2.297929525375366, -1.937894582748413, "Satellite Testing Location Lockheed Martin Corporation\u2019s Littleton, Colorado, facility"]
+[4.222711563110352, -2.7434659004211426, "Satellite Orbit Period 91 days"]
+[1.8686875104904175, 22.1446533203125, "Instrument Beam Pair Separation 3 km"]
+[1.8974202871322632, -1.730317234992981, "Satellite Spatial Coverage Improved"]
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+[-3.0522220134735107, 4.3197245597839355, "Spacecraft Mission Phase Science Commissioning"]
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+[-0.9665926694869995, 9.701872825622559, "Rocket Stage Speed Around 2 m/s"]
+[-3.044741630554199, 4.442283630371094, "Drone Ship Dimensions 90 m x 30 m"]
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+[-3.081519603729248, 4.494905948638916, "Drone Ship Landing Accuracy Within 10 m"]
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+[1.1174689531326294, -2.0051355361938477, "Satellite Pointing Stability \u2264 0.001\u00ba/s"]
+[5.359697341918945, -4.421582221984863, "Satellite Launch Date August 2017"]
+[5.250831604003906, -4.358718395233154, "Satellite Preliminary Design Review Date January"]
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+[-2.526057004928589, 9.75143051147461, "Light Source Advantages High energy efficiency, long life, small size, design flexibility"]
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+[-0.36672672629356384, 3.7849113941192627, "Planet Size Almost exactly Earth-size"]
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+[-0.3705664277076721, 3.793661594390869, "Planet Size 2.6 times larger than Earth"]
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+[-0.36550453305244446, 3.7872376441955566, "Planet Size 20% larger than Earth"]
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+[-0.3677385747432709, 3.802823305130005, "Planet Energy from Star 86% of the energy that the Sun provides to Earth"]
+[-5.348187446594238, 2.821110963821411, "Telescope Data Improvement Sharpened their measurements of its orbital period by 56% and its size by 38%"]
+[-5.396620273590088, 2.7718887329101562, "Telescope Data Improvement Improve scientists\u2019 confidence in the orbital period and size of TOI 700 c by 30% and 36%"]
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+[2.3365538120269775, 22.906429290771484, "Instrument Data Rate 9.8 kbit/s"]
+[-6.698071002960205, 9.96655559539795, "Antenna Dual-frequency Ku, C"]
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+[-6.765657424926758, 10.034252166748047, "Antenna Bandwidth 320 MHz (Ku), 320 or 100 MHz (C)"]
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+[-6.726240634918213, 9.99487018585205, "Antenna Power 237 W"]
+[-6.720700740814209, 9.963272094726562, "Antenna Redundancy Yes"]
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+[0.10910426825284958, 7.167569637298584, "Experiment URL http://spaceresearch.nasa.gov/sts-107/107_cvx.pdf"]
+[-1.335872769355774, 6.102554798126221, "Company Instrument Provider Unknown"]
+[-1.3381712436676025, 6.102311611175537, "Company Platform Bus Supplier Unknown"]
+[-1.2935643196105957, 6.128509044647217, "Company Spectrometer-based Methane Sensing System Developer Unknown"]
+[-1.3233685493469238, 6.146683216094971, "Company X-SAT Saturn-Class Platform Adapter Unknown"]
+[11.174596786499023, 5.37758731842041, "CubeSat Deployer Total Deployed 176"]
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+[11.478483200073242, 5.69731330871582, "CubeSat Size 4U"]
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+[0.14436587691307068, 7.196377277374268, "Experiment Quantity 3"]
+[2.831397533416748, -1.138547420501709, "Satellite Purpose Survey the slot region and study radiation damage to instruments"]
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+[-3.088484048843384, 2.003605604171753, "Space Mission Telescope and Camera System 34 separate small telescopes and cameras"]
+[-3.0552444458007812, 2.0222275257110596, "Space Mission Number of Stars Up to a million"]
+[-3.087477684020996, 2.046265125274658, "Space Mission Sky Coverage Half of the sky"]
+[-3.084468126296997, 2.0007739067077637, "Space Mission Exoplanet Detection Terrestrial exoplanets in the habitable zone of solar-type host stars"]
+[-1.576838493347168, 9.635462760925293, "Propulsion System Manufacturer ENPULSION"]
+[5.053726673126221, -4.426258087158203, "Satellite Mission Date August 7-12, 2021"]
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+[11.519621849060059, 5.727693557739258, "CubeSat Size 3U"]
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+[2.6624228954315186, 13.47020149230957, "Optical Component Control Scan mechanism assembly"]
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+[-2.7151308059692383, 8.752538681030273, "Module Radiometric Performance Maintained by limiting the temperature change between views of cold space"]
+[3.180753707885742, -1.6832184791564941, "Satellite Prime Contractor MEI (Matsushita Electric Industrial Co. Ltd.)"]
+[-1.5590531826019287, 12.826760292053223, "Solar Coronagraph Formation Flying Complete Metrology"]
+[1.14632248878479, -2.078996419906616, "Satellite Attitude Uncertainty Bounds 1\u03c3 (68%)"]
+[4.79290771484375, -2.4805727005004883, "Satellite Orbit Lifetime Well over 1 year"]
+[2.83249831199646, -2.0369350910186768, "Satellite Bstar Drag Term Historical"]
+[1.3399543762207031, -2.022845983505249, "Satellite Attitude Ram pointing"]
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+[-5.206993103027344, 7.815733909606934, "Communication System Ka-band Data Rate 120 Mbit/s max"]
+[5.301699161529541, -4.4470953941345215, "Satellite Routine Operational Phase Start Date November 26, 1996"]
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+[4.455615520477295, -2.6592609882354736, "Satellite Initial Mission Checkout Duration 90 days"]
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+[-4.337709903717041, 7.366524696350098, "Data Transmission Device Link Protocol X.25 (CCITT)"]
+[-4.28633975982666, 7.384740829467773, "Data Transmission Device Application Broadcast of operational meteorological charts"]
+[-0.37031644582748413, 12.454304695129395, "Atomic Oxygen Monitor System Quantity of TQCMs 8"]
+[0.27449992299079895, 8.1768217086792, "Thermoelectric Quartz Crystal Microbalances Location Inside/outside of the SLATS structure"]
+[-0.19898663461208344, 15.570667266845703, "Material Degradation Monitor Components Material samples and the optical camera"]
+[2.232245922088623, 13.409978866577148, "Optical Sensor Purpose Earth observation"]
+[2.2094433307647705, 13.394804954528809, "Optical Sensor Spatial Resolution Proportional to the altitude"]
+[-0.13016074895858765, 15.519299507141113, "Micro-spectrometer Spectral Range 900-1700 nm"]
+[-0.10658752918243408, 15.49057674407959, "Micro-spectrometer Spectral Resolution About 6 nm"]
+[-0.1035943329334259, 15.50403118133545, "Micro-spectrometer IFOV 1 mrad"]
+[-0.15470948815345764, 15.491844177246094, "Micro-spectrometer Detector InGaAs with diffractive optics"]
+[-0.13837994635105133, 15.46358871459961, "Micro-spectrometer Cooler Programmable Peltier-effect cooler"]
+[-0.08697817474603653, 15.438191413879395, "Micro-spectrometer Integration Times Microseconds to seconds"]
+[1.6979198455810547, 6.937008857727051, "Communication Device Wavelength 1.064 \u00b5m"]
+[1.7380025386810303, 6.912074089050293, "Communication Device Number of ISLs More than 100"]
+[1.6650255918502808, 6.965487480163574, "Communication Device Launch Date Q2 2013"]
+[1.8682141304016113, 22.731508255004883, "Instrument Energy Range 1/4 keV"]
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+[2.5890142917633057, 14.250359535217285, "Optical Instrument Effective Focal Length 466.7 mm"]
+[2.6473371982574463, 14.36258316040039, "Optical Instrument MTF Value > 0.3"]
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+[-1.9391534328460693, 14.867940902709961, "Metering Structure First Natural Frequency > 300 Hz"]
+[-0.8789007663726807, 11.665534973144531, "Detector Array Imaging Channels One panchromatic and three multi-spectral channels"]
+[-0.8788702487945557, 11.696961402893066, "Detector Array Proximity Electronics Provide clock pulses and biases for the operation of the detector array"]
+[6.273146152496338, 7.457001209259033, "Satellite Component Mass 96 kg"]
+[6.293578624725342, 7.4503092765808105, "Satellite Component Power 135 W"]
+[6.2866926193237305, 7.454851150512695, "Satellite Component Data Rate 14.2 kbit/s"]
+[1.7245103120803833, 6.926875591278076, "Communication Device Diameter 61 cm"]
+[1.7007331848144531, 6.885844707489014, "Communication Device Beam Width 0.4\u00ba-1.9\u00ba"]
+[6.3879008293151855, 7.369647979736328, "Satellite Component Inclination 23\u00ba"]
+[6.347060203552246, 7.404663562774658, "Satellite Component Direction 45\u00ba to nadir"]
+[5.176008224487305, -4.243370056152344, "Satellite Design Date December 2017"]
+[5.0503010749816895, -4.473078727722168, "Satellite Symposium Date 13-16 January 2020"]
+[-2.65362286567688, 11.681329727172852, "Imager Proceedings Date 2014"]
+[6.229344367980957, 7.513889312744141, "Satellite Component Structure Material Aluminum core and aluminum face skin"]
+[6.314329147338867, 7.424187183380127, "Satellite Component Structure Material CFRP face skin"]
+[-6.705942630767822, 9.985676765441895, "Antenna Number of Panels 3"]
+[-6.726607322692871, 9.99685287475586, "Antenna Panel Quantity for a Panel 4"]
+[2.4580554962158203, -1.7764183282852173, "Satellite Main Structure Cuboid module"]
+[0.16945035755634308, 15.31431770324707, "Spectrometer Unknown Unknown"]
+[0.18047897517681122, 15.308465003967285, "Spectrometer Unknown Unknown"]
+[0.2298033982515335, 15.281484603881836, "Spectrometer Unknown Unknown"]
+[2.540440082550049, 22.81331443786621, "Instrument Observation Duration Minimum 1,000 hours"]
+[-2.9310145378112793, 4.19533634185791, "Spacecraft Inter Satellite Distance About 150 m"]
+[-3.1352310180664062, 2.1133487224578857, "Mission Phase Duration About 4.5 months"]
+[0.07560944557189941, 7.178241729736328, "Experiment Description 6 Degree of Freedom control with thrusters"]
+[0.16162145137786865, 7.1966986656188965, "Experiment Description Rendezvous experiment and Realistic Collision Avoidance"]
+[0.1376017928123474, 7.183594703674316, "Experiment Description FDIR (Failure Detection, Isolation and Recovery) test maneuvers"]
+[1.5226463079452515, 2.5083117485046387, "Geostationary Meteorological Satellite Performance Improvement Data amount, network transmission bandwidth, product type and quantity, archiving data and applications"]
+[1.524155855178833, 2.5006320476531982, "Geostationary Meteorological Satellite Imaging Capability Enhanced"]
+[1.519303321838379, 2.527977228164673, "Geostationary Meteorological Satellite Atmospheric Sounding Capability Enabled"]
+[1.5219379663467407, 2.517033815383911, "Geostationary Meteorological Satellite Solar Observations Enabled for EUV (Extreme Ultraviolet) and X-ray monitoring"]
+[1.5303277969360352, 2.5004117488861084, "Geostationary Meteorological Satellite Mission Imagery, sounding, lightning mapping, and space environment monitoring"]
+[-1.0368971824645996, 7.713778018951416, "Release Device Quantity 4"]
+[-1.0292348861694336, 7.7215166091918945, "Release Device Technology Shape-memory alloy (Nitinol)"]
+[-1.0292561054229736, 7.729485988616943, "Release Device Objective Demonstration of a new class of low-shock release devices"]
+[1.7439178228378296, -2.0703177452087402, "Satellite Position Geostationary orbit with visibility over central Europe"]
+[3.7334342002868652, 17.701305389404297, "Hosted Payload Position Geostationary orbit with visibility over central Europe"]
+[-1.9352223873138428, 8.094747543334961, "System Start of Services 2014"]
+[-1.9253724813461304, 8.1136474609375, "System Operation Commitment Next 15 years"]
+[-0.9496854543685913, -9.995590209960938, "Satellite Constellation Purpose Relay user data between LEO satellites, as well as UAVs (Unmanned Aerial Vehicles) in the future, and ground stations"]
+[-0.9553736448287964, -9.99683952331543, "Satellite Constellation Operating Position 9\u00ba longitude over Europe"]
+[-0.9414790868759155, -9.997878074645996, "Satellite Constellation Operator Eutelsat"]
+[-0.9559443593025208, -9.997682571411133, "Satellite Constellation Communication Improvement Significantly improve the stringent timeliness requirements of demanding Earth observation missions"]
+[-1.5967919826507568, 9.685567855834961, "Propulsion System Propellant Xenon gas"]
+[-1.6291303634643555, 9.714251518249512, "Propulsion System Propellant Pressure Approximately 7MPa"]
+[-1.640315294265747, 9.692127227783203, "Propulsion System Mass Flow Rate 10.5 cm3/s"]
+[-1.6079083681106567, 9.668866157531738, "Propulsion System Mass Flow Rate for Neutralizer 2 cm3/s"]
+[1.4466495513916016, 2.763395071029663, "Weather Satellite Sensor Complement Newly defined"]
+[1.4406718015670776, 2.7636334896087646, "Weather Satellite Development Status Under development"]
+[1.446926236152649, 2.752148151397705, "Weather Satellite Management Collaborative effort between NOAA and NASA"]
+[1.4477853775024414, 2.7591795921325684, "Weather Satellite Program Location Goddard Space Flight Center (GSFC), Greenbelt, MD"]
+[0.893997848033905, 12.097687721252441, "Sensor Number of Segments 4"]
+[0.5397451519966125, 12.226799964904785, "Sensor Conversion Factor ~16 r (3\u03bb)-1"]
+[0.4822585880756378, 12.206981658935547, "Sensor Numerical Simulation Factor about 20000 rad/rad"]
+[-0.720720648765564, 2.9731130599975586, "Supernova Remnant Radioactive 44Ti Detected"]
+[-2.1836092472076416, 6.386001110076904, "Free-flyer platform Use Simulation exercises for ISS assembly flight"]
+[-1.431838870048523, 14.949572563171387, "Infrared Spectral Imaging Radiometer Unknown Unknown"]
+[4.10003137588501, 13.933126449584961, "Shuttle Laser Altimeter Unknown Unknown"]
+[-1.1831302642822266, 13.246467590332031, "Solar Constant Experiment Unknown Unknown"]
+[-0.2501193881034851, 6.514010429382324, "Critical Viscosity of Xenon Unknown Unknown"]
+[-0.4922065734863281, 8.094947814941406, "Cryogenic on-orbit long life active refrigerator Flight Experiment Unknown Unknown"]
+[-0.44305798411369324, 5.787925720214844, "Two Phase Flow Unknown Unknown"]
+[-0.030872946605086327, 7.0344624519348145, "Space Experiment Module Unknown Unknown"]
+[1.531001329421997, -1.86185884475708, "Satellite Temperature Stability mK (milliKelvin)-level"]
+[-0.4525376260280609, 11.608448028564453, "Imaging Detector Thermal Control Passive cooling using a space-facing radiative surface"]
+[-0.48892226815223694, 11.6326265335083, "Imaging Detector Temperature Corrections Small adjustments over the course of an observation"]
+[-0.4278227388858795, 11.61658763885498, "Imaging Detector Stability To the required precision"]
+[0.7039989233016968, 12.010332107543945, "Sensor Objective To characterize and to flight test a novel zinc-oxide sensitive renewable atomic oxygen flux sensor based on semiconducting thin films"]
+[0.7189658880233765, 12.004812240600586, "Sensor Heritage Heritage of STRV-1a"]
+[4.280228614807129, -2.7670462131500244, "Satellite Deployment Time 10 minutes"]
+[-2.738027572631836, 8.725574493408203, "Module Mass 11,800 kg"]
+[-7.569222927093506, 5.883668899536133, "Camera Unknown Unknown"]
+[2.9912617206573486, -2.1024889945983887, "Satellite Unknown Unknown"]
+[-3.8143808841705322, 6.935945510864258, "Data Collection System Data Collection From DCPs (Data Collection Platforms)"]
+[-3.8444151878356934, 6.85398006439209, "Data Collection Platforms Types Regional, or international"]
+[2.075360059738159, -2.6742947101593018, "Satellite Baseline Products 28"]
+[2.9518094062805176, -1.9709051847457886, "Satellite Algorithm Design Status Completed"]
+[-0.8259633779525757, 11.542426109313965, "Detector Component Unknown"]
+[-0.07702603191137314, 15.45020866394043, "Scintillator Counters Component Unknown"]
+[-0.8634217977523804, 6.979450225830078, "Counter Component Unknown"]
+[-1.5865532159805298, 14.819445610046387, "Calorimeter Component Unknown"]
+[-1.940049409866333, 9.168200492858887, "Gas Supply System Component Unknown"]
+[-0.9098572134971619, 8.728515625, "Crates/Radiators Component Unknown"]
+[-1.71098792552948, 8.475018501281738, "Electronics Boxes Component Unknown"]
+[-1.62809419631958, 8.518373489379883, "Electronics Boxes Component Unknown"]
+[-2.108867645263672, 7.716965675354004, "Avionics Box Component Unknown"]
+[-1.3350741863250732, 8.692983627319336, "Rectifiers Component Unknown"]
+[-1.3395527601242065, 8.598974227905273, "Electrical cables and components Component Unknown"]
+[-1.100266456604004, 8.4327392578125, "Fixture Component Unknown"]
+[-1.2747257947921753, 6.926759243011475, "Assembly Component Unknown"]
+[-1.1289727687835693, 8.479262351989746, "Fixture Component Unknown"]
+[-1.2768224477767944, 6.9142374992370605, "Assembly Component Unknown"]
+[-7.3335347175598145, 6.133512020111084, "Camera System Component Unknown"]
+[-1.0897871255874634, 8.41578483581543, "Fixture Component Unknown"]
+[-1.0917326211929321, 7.890462398529053, "Mount Component Unknown"]
+[-1.7150055170059204, 6.29595422744751, "Handrails Component Unknown"]
+[1.9315392971038818, 10.718528747558594, "Imaging Device Focal Plane 3 CCD lines"]
+[-7.554287433624268, 5.895115852355957, "Camera Observation Directions \u00b117\u00ba, 0\u00ba (nadir)"]
+[-7.550911903381348, 5.899097442626953, "Camera Observation Directions \u00b18.7\u00ba, 0\u00ba"]
+[2.5681138038635254, 21.917970657348633, "Instrument Function Mounting fixture of three separate cameras"]
+[-3.1475400924682617, 1.7061320543289185, "Satellite Mission Purpose Measure gravity and show how mass is distributed around the planet"]
+[-3.124415397644043, 1.7169972658157349, "Satellite Mission Data Collection Monthly variations of the Earth gravity field"]
+[-3.195349931716919, 1.7352904081344604, "Satellite Mission Operation Start Date March 2002"]
+[-3.129056453704834, 1.688567876815796, "Satellite Mission Data Continuity Still providing valuable information to the science community in 2015"]
+[16.81724739074707, 6.878518581390381, "Microsatellite Mass 25 kg"]
+[16.855083465576172, 6.857224464416504, "Microsatellite Size 32 cm x 32 cm x 40 cm"]
+[16.901424407958984, 6.819577217102051, "Microsatellite Stabilization Method 3-axis stabilized using bias momentum method in the pitch axis"]
+[0.6669549942016602, 9.323965072631836, "Attitude Determination and Control Subsystem Components CSS (Coarse Sun Sensor), FSS (Fine Sun Sensor), MAG (Magnetometer), and 2 ST (Star Tracker)"]
+[0.6679861545562744, 9.318934440612793, "Attitude Determination and Control Subsystem Actuation 3 MTQs (Magnetic Torquer) and a MW (Momentum Wheel)"]
+[1.775407075881958, 8.43994426727295, "Command & Data Handling Subsystem Function Process instrument information and send commands to actuators"]
+[-5.291514873504639, 8.01916790008545, "Communication System Frequency Range 300 MHz to 3 GHz"]
+[-5.27947998046875, 7.980175971984863, "Communication System Bandwidth 40 MHz"]
+[-5.162026405334473, 7.764432907104492, "Communication System Data Rate Up to 80 Mbit/s"]
+[-5.271814346313477, 7.896213054656982, "Communication System Positioning Precision 5 m"]
+[-5.360474109649658, 8.075271606445312, "Communication System GPS Update Rate 5 Hz"]
+[-5.304366588592529, 7.835910320281982, "Communication System PCB Size 95.9 x 90.2 x 11 (mm)"]
+[-5.230825901031494, 7.919829368591309, "Communication System Total PCB Mass < 100 g"]
+[-5.163796424865723, 7.811296463012695, "Communication System Data Interface I2C, UART"]
+[-5.14454984664917, 7.8022990226745605, "Communication System Storage Capacity From 2 x 2 GB"]
+[-5.208602428436279, 7.834496974945068, "Communication System Supply Voltage 3.3 V or 5 V"]
+[3.5971291065216064, 13.617774963378906, "Laser Measurement System Short-range < 7 m"]
+[3.5923233032226562, 13.585680961608887, "Laser Measurement System Mid-range 7 \u2013 70 m"]
+[3.54457688331604, 13.567907333374023, "Laser Measurement System Long-range 70 \u2013 250 m"]
+[-0.29476961493492126, 6.73234748840332, "Test Component Lateral Range \u00b125 mm in Z and Y axes"]
+[-0.3361119031906128, 6.817755222320557, "Test Component Maximum Longitudinal Displacement 6 m (TBC)"]
+[-0.27299124002456665, 6.74160099029541, "Test Component Displacement Intervals 0.2 m (TBC)"]
+[-3.7576513290405273, 8.157971382141113, "Cryogenic Storage System Liquid Methane Capacity 42 liters"]
+[11.090744972229004, 5.23291540145874, "CubeSat Mass 4 kg"]
+[11.498977661132812, 5.707803249359131, "CubeSat Size 6U"]
+[11.27181339263916, 5.420274257659912, "CubeSat Affiliation JHU/APL (Johns Hopkins University /Applied Physics Laboratory)"]
+[11.517471313476562, 5.698452949523926, "CubeSat Size 1U"]
+[4.167097568511963, -2.814593553543091, "Satellite Orbit Period 51.4 days"]
+[0.7222285866737366, -2.2168734073638916, "Satellite View Angle About three degrees above the stars\u2019 orbital plane"]
+[-0.6134651899337769, 3.241088390350342, "Star Size 4.3 times bigger than the Sun"]
+[-0.5982213020324707, 3.225973606109619, "Star Surface Temperature Around 17,500\u00ba Fahrenheit (9,700\u00baC)"]
+[-0.614526629447937, 3.2106542587280273, "Star Distance from Earth About 270 light-years"]
+[4.389572620391846, -2.733868360519409, "Satellite Monitoring Duration 27 days"]
+[-0.6050061583518982, 4.901389122009277, "Geographic Area Endured Unusually Active and Destructive Fire Seasons Yes"]
+[-1.315024733543396, 6.183776378631592, "Occupation Anticipate Poor Yields Yes"]
+[-0.33515045046806335, 4.977181911468506, "Water Bodies Reaching Unusually Low Levels Yes"]
+[5.369651794433594, -4.439709186553955, "Satellite Launch Date Sept. 19, 1977"]
+[4.160287380218506, -2.8459577560424805, "Satellite Orbit Insertion Time Launch plus 57 minutes"]
+[4.081923007965088, -2.5023062229156494, "Satellite Ground Track Repeat 3 days"]
+[1.2243305444717407, -1.426782250404358, "Satellite SAR Operation Swath 97 km wide and 4023 km long"]
+[2.505342960357666, -1.4045019149780273, "Satellite SAR Instrument Data Collection About 60 hours of data"]
+[-5.542243003845215, 15.889915466308594, "SAR Receiving Station Real-time SAR Data Downlinks 272 minutes"]
+[-7.561520576477051, 5.892283916473389, "Digital Staring Camera Field of View (FOV) \u00b1 43\u00b0 along track; \u00b1 51\u00b0 cross track"]
+[-7.557725429534912, 5.886904239654541, "Digital Staring Camera Spectral Channels 9"]
+[-7.577599048614502, 5.87318229675293, "Digital Staring Camera Spectral Region 443 to 910 nm"]
+[-7.562860012054443, 5.8822431564331055, "Digital Staring Camera Ground Spatial Resolution 6 km x 7 km at nadir"]
+[-7.57179594039917, 5.87792444229126, "Digital Staring Camera Swath Width 2400 km"]
+[-7.552059173583984, 5.898532390594482, "Digital Staring Camera Repeat Cycle 16 days"]
+[0.5799506306648254, -1.4727293252944946, "Satellite Orbit Altitude 705 km"]
+[0.7384704351425171, -2.2268142700195312, "Satellite Orbit Inclination 98.21\u00b0"]
+[2.652881145477295, 13.444478034973145, "Optical Component Yaw Coupling Factor 2.2 mm/rad"]
+[2.6425864696502686, 13.45662784576416, "Optical Component Yaw Coupling Factor 10 \u00b5m/rad"]
+[2.635910749435425, 13.465117454528809, "Optical Component Thickness 7 mm"]
+[-0.8301252722740173, 12.625166893005371, "Space Radiation Monitor Parameter Value"]
+[-7.568777561187744, 5.883274555206299, "Camera Resolution Up to several meters per a pixel"]
+[2.821129083633423, -1.049249529838562, "Satellite Purpose Monitoring of wildlife behavior"]
+[2.778787612915039, -1.192891240119934, "Satellite Purpose Demonstrate the detector technology and electronics for the future \u201cCubeSats Applied for MEasuring and LOcalizing Transients\u201d (CAMELOT) mission"]
+[2.854438066482544, -1.0919333696365356, "Satellite Purpose Internet of Things"]
+[2.7936699390411377, -1.2019968032836914, "Satellite Purpose Sending telemetry data and photos from the space to the ground station"]
+[2.899834394454956, -1.0588585138320923, "Satellite Purpose Provides global connectivity for Internet-of-Things devices"]
+[-2.816460132598877, 15.257672309875488, "Microwave Radiometer Reflector Diameter 6.6 cm"]
+[-2.824069023132324, 15.239416122436523, "Microwave Radiometer Bandwidth 91 to 183.3 GHz"]
+[-2.8193817138671875, 15.246642112731934, "Microwave Radiometer Number of Earth Viewing Positions 28"]
+[-2.7897417545318604, 15.235084533691406, "Microwave Radiometer Hot-Load Target Temperature About 300 K"]
+[-2.806746482849121, 15.237957000732422, "Microwave Radiometer Cosmic Background Radiation Temperature About 3 K"]
+[-13.878745079040527, -2.1619253158569336, "X-ray Telescope System Energy Coverage Up to 30 keV"]
+[-13.901215553283691, -2.177252769470215, "X-ray Telescope System Sensitivity Limited above 12 keV"]
+[-4.581321716308594, -3.07033634185791, "Exoplanet Size 25% larger than Earth"]
+[-4.577889919281006, -3.104421854019165, "Exoplanet Orbital Period 3.4 days"]
+[-4.562203407287598, -3.0866005420684814, "Exoplanet Distance from Star About 13 times closer than Mercury orbits the Sun"]
+[-4.573235511779785, -3.075308084487915, "Exoplanet Mass Around 1.9 times greater than Earth\u2019s"]
+[-4.5636444091796875, -3.094484329223633, "Exoplanet Equilibrium Temperature Around 490 \u00ba Fahrenheit (254\u00baC)"]
+[2.7376363277435303, 22.355506896972656, "Instrument Pointing Control Internal"]
+[0.5505623817443848, 12.046597480773926, "Sensor Function Differential Wavefront Sensing"]
+[-0.4480774402618408, 8.659378051757812, "Actuator Function Optimizes the interferometer contrast in the receive path as well as the transmit beam pointing"]
+[-1.2028427124023438, 8.59819221496582, "Component Alignment Requirement 100 \u00b5m"]
+[7.229647159576416, 12.541166305541992, "Space Instrument Testing Date 2012"]
+[5.192172527313232, -3.994049310684204, "Satellite Development Start Year 2015"]
+[2.898627996444702, -1.0790700912475586, "Satellite Purpose Lower cost, allowing the democratization of space"]
+[-2.5371100902557373, 4.843413352966309, "Space Debris Removal Operation Successful"]
+[-1.9714173078536987, 7.458544731140137, "Hardware and Software Performance Proven"]
+[0.07306618243455887, 7.134045124053955, "Experiment Anomalies Manifested"]
+[3.0293233394622803, -1.820963978767395, "Satellite Manufacturer Surrey Space Centre at the University of Surrey"]
+[2.88496732711792, -1.8189456462860107, "Satellite Operator Surrey Satellite Technology Ltd"]
+[-0.09658748656511307, 15.484247207641602, "Telescope and Spectrometer System Purpose Measure infrared radiation emitted by the Earth's middle atmosphere"]
+[-0.4119710922241211, 16.22239875793457, "Spectrograph Purpose Measure ultraviolet radiation emitted and scattered by the Earth's atmosphere"]
+[0.9293209910392761, 0.9339998960494995, "Earth Sensor Purpose Gather operational data of the Earth horizon positions"]
+[3.288045883178711, 13.929912567138672, "Interferometer Purpose Measure the vibration of the SPAS structure"]
+[2.6335439682006836, 22.38048553466797, "Instrument Image Collection Full Disk, CONUS, Mesoscale"]
+[1.9921865463256836, 22.292224884033203, "Instrument Image Size Provided in Table 8"]
+[2.6133992671966553, 23.013839721679688, "Instrument Image Location Provided in Table 9"]
+[1.7870830297470093, 22.103748321533203, "Instrument Image Size in Kilometers Based on the conversion factor of 28 \u00b5rad/km"]
+[-1.5889338254928589, 4.111022472381592, "Ground Segment Component Objectives Track COSPAS-SARSAT satellites, recover beacon signals from satellites, perform Doppler processing calculations to locate signal sources, and to relay Doppler solutions to an associated MCC"]
+[-1.5266940593719482, 4.170722007751465, "Ground Segment Component Tasks Receive data from nationally associated LUTs and international MCCs, match signals originating from the same signal source, merge beacon signals from identical sources, geographically sort data and transmit data and alerts to relevant RCCs"]
+[-1.5611696243286133, 4.127386569976807, "Ground Segment Component Composition Formed from a variety of different state rescue services, depending on the responding nation"]
+[8.955771446228027, 8.512212753295898, "Satellite Payload Band C- and Ku-band"]
+[8.955960273742676, 8.511812210083008, "Satellite Payload Number of Beams 20"]
+[0.9457242488861084, -4.362715244293213, "Satellite Take-off Weight 4,200 kg"]
+[2.084256172180176, -0.5063378214836121, "Satellite Electric Power 16 kW"]
+[5.290884017944336, -4.233067035675049, "Satellite Launch Date Late 2017"]
+[4.441801071166992, -2.7142956256866455, "Satellite Time to Reach Geostationary Orbit Four months"]
+[-2.642204523086548, 11.908984184265137, "Panchromatic Imager Power Consumption Unknown"]
+[-2.4756598472595215, 13.062612533569336, "Multispectral Imager Power Consumption Unknown"]
+[-2.649786949157715, 11.874052047729492, "Panchromatic Imager Operation Mode Along-track imaging (default mode)"]
+[-2.4857592582702637, 13.046345710754395, "Multispectral Imager Operation Mode Along-track imaging (default mode)"]
+[-3.553151845932007, 14.255399703979492, "Radiometric Imager Bands 2 visual spectrum bands, and 14 infrared bands"]
+[-3.5639586448669434, 14.24400520324707, "Radiometric Imager Resolution 500m at nadir"]
+[-3.554765224456787, 14.242528915405273, "Radiometric Imager Resolution 1 km"]
+[-3.573230743408203, 14.240172386169434, "Radiometric Imager Resolution 2 km"]
+[-3.554563283920288, 14.263239860534668, "Radiometric Imager Temporal Resolution Every fifteen or five minutes"]
+[-3.54390549659729, 14.270162582397461, "Radiometric Imager Data Rate 75 Mbit/s"]
+[-3.5688576698303223, 14.263378143310547, "Radiometric Imager Field of View 17.76\u00b0"]
+[1.599169135093689, -2.253521203994751, "Satellite Orbit Geostationary orbit at a longitude of 75\u00b0 West"]
+[2.2468271255493164, -1.8694740533828735, "Satellite Ground Segment Sites West Virginia, Maryland and Virginia"]
+[-3.6738369464874268, 8.037519454956055, "Solid State Recorder Capacity 300 Gbit"]
+[-3.6821351051330566, 8.044058799743652, "Solid State Recorder Memory Boards Capacity 50 Gbit"]
+[-3.6734375953674316, 8.04220962524414, "Solid State Recorder Number of Control Units 2"]
+[-3.669203996658325, 8.044154167175293, "Solid State Recorder Number of Files per Input Port Up to 32"]
+[-5.275207042694092, 7.987279415130615, "Communication System Frequency Band X-band"]
+[5.318350791931152, -4.463784217834473, "Satellite Launch Date 2nd of April 2018"]
+[0.5936631560325623, -1.4574605226516724, "Satellite Orbit Altitude 405 km"]
+[2.329934597015381, -1.6110879182815552, "Satellite Technology Demonstrations Use of a net, a harpoon, VBN (Vision-Based Navigation) and a dragsail"]
+[1.9089175462722778, 10.722569465637207, "Imaging Device Resolution 7.5 m in the panchromatic band and 15 m in the multispectral bands"]
+[-4.755967140197754, 9.258319854736328, "Transmitter Downlink Transmission Rate Efficient"]
+[2.55770206451416, -1.9474965333938599, "Satellite Based on BILSAT bus and module heritage"]
+[2.6555612087249756, -1.1164660453796387, "Satellite Science Goal Investigate the distribution of water as a function of time of day, latitude, and regolith composition"]
+[1.6996046304702759, -1.0968724489212036, "Satellite Measurement Completely encompass the broad 3 \u00b5m band resulting from absorption by water in the solid and vapor states"]
+[11.849021911621094, 5.322534561157227, "3U CubeSat Launch Date March 2021"]
+[-0.9530316591262817, -10.002628326416016, "Satellite Constellation Number of Satellites At least 250"]
+[-0.956497073173523, -10.00556755065918, "Satellite Constellation Number of Satellites in 2024 64"]
+[-0.9739211201667786, -10.021306037902832, "Satellite Constellation Number of Satellites in 2025 250"]
+[-0.9528248310089111, -10.005311012268066, "Satellite Constellation Operator Open Cosmos Ltd. (UK)"]
+[3.220520257949829, -1.5355945825576782, "Satellite Mission Lead MIT in Cambridge, Massachusetts"]
+[3.0287420749664307, -1.5903552770614624, "Satellite Management NASA's Goddard Space Flight Center"]
+[5.101325988769531, -4.3604326248168945, "Satellite Discovery Date July 25, 2019"]
+[2.0989701747894287, -2.7608330249786377, "Satellite Number of Planets Discovered 21"]
+[2.009716749191284, -2.708674430847168, "Satellite Candidate Exoplanets Over 850"]
+[-1.018619179725647, 7.706068992614746, "Device Purpose Measure radiation"]
+[3.7314999103546143, 17.69690704345703, "Payload Purpose Test susceptibility of commercial computer memories to space radiation"]
+[1.2524431943893433, -0.9442159533500671, "Satellite Shielding Thickness 7 mm"]
+[2.8886826038360596, -1.8898873329162598, "Satellite Operating Condition Without disruption"]
+[5.045742034912109, -2.262037992477417, "Satellite Design Life 3 years for prime plus 2 for extended mission"]
+[0.7236277461051941, -4.1552324295043945, "Satellite Mass at Launch 2388 kg"]
+[0.941369354724884, -4.376046657562256, "Satellite Dry Mass 2169 kg"]
+[1.1749200820922852, -0.772831916809082, "Satellite Size 5.5 m x 6.6 m x 2.8 m"]
+[-2.605482339859009, 9.629985809326172, "Power Source Size 8.9 m x 3.3 m"]
+[2.08958101272583, -0.5297406315803528, "Satellite Power 3.4 kW (BOL), 2.1 kW (after 5 years)"]
+[2.497671127319336, -1.9989298582077026, "Satellite Bus Type MMS (Multimission Modular Satellite), Fairchild RF communication"]
+[1.7605665922164917, 6.86892032623291, "Communication Device Data Rates 0.125 to 1024 kByte/s"]
+[-2.03328800201416, 8.789237976074219, "Wiring Function Connecting satellite components and payload and for transmitting power, commands, and signals"]
+[-1.0921449661254883, 7.240673542022705, "Equipment Function Main loading equipment for the satellite integration and testing procedures"]
+[-0.577357828617096, 8.189971923828125, "Structure Function Carries the different satellite components and payloads"]
+[0.8409885764122009, 12.108538627624512, "Sensor Quantity 6 units"]
+[0.7368782162666321, 12.055208206176758, "Sensor Quantity Single unit"]
+[0.7471125721931458, 12.04537582397461, "Sensor Quantity Single unit"]
+[0.6158888339996338, 12.094934463500977, "Sensor Quantity Several sensors"]
+[0.7465018033981323, 12.043997764587402, "Sensor Quantity Single unit"]
+[-0.4573031961917877, 8.676055908203125, "Actuator Quantity Three wheels"]
+[-0.4713127613067627, 8.67202377319336, "Actuator Quantity Three rods"]
+[-0.43914595246315, 8.682127952575684, "Actuator Quantity Orbital maneuvering and 2-axis TVC"]
+[3.7302114963531494, -1.608925700187683, "Satellite Operation Status Nominal"]
+[-4.441829204559326, 15.904370307922363, "Radar Calibration Frequency Every 3 months"]
+[-4.522613048553467, 15.936649322509766, "Radar Observation Mode Major observation modes"]
+[-4.474703788757324, 15.898558616638184, "Radar Emergency Observation Mount Agung in Bali Island, Indonesia"]
+[-0.5839792490005493, 8.129206657409668, "Container Structure Purpose Integrate/package P-PODs as secondary payloads"]
+[11.218832969665527, 5.448433876037598, "CubeSat Mission Orbit Elliptical orbit of 770 km x 480 km"]
+[11.251554489135742, 5.480011463165283, "CubeSat Mission Inclination 66\u00ba"]
+[0.82862389087677, 12.056775093078613, "Sensor Quantity 3"]
+[0.8753453493118286, 12.030902862548828, "Sensor Quantity 3"]
+[-0.45120474696159363, 8.673404693603516, "Actuator Quantity 4"]
+[0.8665294647216797, 12.093446731567383, "Sensor Quantity 1"]
+[0.8656452298164368, 12.10938835144043, "Sensor Quantity 1"]
+[0.7487069964408875, 12.091946601867676, "Sensor Quantity 6"]
+[-1.4585498571395874, 9.509577751159668, "Thruster Quantity 2"]
+[1.6785129308700562, 6.9643378257751465, "Communication Device Quantity 1"]
+[-1.070307970046997, 7.698683261871338, "Device Quantity 2"]
+[-1.1560059785842896, 3.3000776767730713, "Black Hole Mass 6 million times the Sun\u2019s mass"]
+[-1.170198917388916, 3.115112543106079, "Celestial Event Frequency Once every 10,000 to 100,000 years in a galaxy the size of our own Milky Way"]
+[-1.23585844039917, 3.029665946960449, "Celestial Event Frequency Happen every 100 years or so"]
+[4.5831499099731445, -2.636124849319458, "Satellite Mission Duration Initial two-year mission"]
+[2.9727728366851807, -1.612215280532837, "Satellite Managed By MIT in Cambridge, Massachusetts, and managed by NASA's Goddard Space Flight Center"]
+[-3.0932657718658447, 2.4219095706939697, "Mission Managed By NASA's Goddard Space Flight Center in collaboration with Penn State in University Park, the Los Alamos National Laboratory in New Mexico and Northrop Grumman Innovation Systems in Dulles, Virginia"]
+[2.609858989715576, -2.214566707611084, "Satellite Launch Location United Arab Emirates (UAE)"]
+[3.1229236125946045, -1.5032066106796265, "Satellite Collaborating Organizations Yahsat, Khalifa University of Science and Technology, and Northrop Grumman"]
+[-3.116610288619995, 1.775413990020752, "Space Shuttle Observation Mission Conference Presentation ICAE (International Conference on Atmospheric Electricity) 2003, Versailles, France, June 9-13, 2003"]
+[-3.198577404022217, 1.8180773258209229, "Space Shuttle Observation Mission Conference Presentation AGU Fall Meeting 2003, San Francisco, CA, Dec. 8-12, 2003"]
+[2.6777279376983643, -2.610199213027954, "Satellite Data Sampling Rates 1 to 100 samples/s"]
+[3.799715518951416, -2.589399814605713, "Satellite On-board Data Storage and Downlinking Interval Every 12 hours or less"]
+[2.7549638748168945, -2.495109796524048, "Satellite Uplink and Downlink Frequency S-band (2.114 GHz and 2.296 GHz)"]
+[2.626574993133545, -2.693798542022705, "Satellite Maximum Downlink Rate 256 kbit/s"]
+[2.6486449241638184, -2.6854257583618164, "Satellite Uplink Date Rate 4 kbit/s"]
+[0.7401691675186157, -1.203816294670105, "Satellite Altitude 270 km"]
+[5.278810024261475, -4.446614742279053, "Satellite Launch Date December 23, 2017"]
+[5.32643985748291, -4.428696155548096, "Satellite Initial Operations Completion Date March 2018"]
+[5.147158622741699, -4.449058532714844, "Satellite Phase Transition Date June 1, 2018"]
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+[-1.01446533203125, 7.686295986175537, "Device Cost Savings Reducing the launch mass and volume required for printer feedstock"]
+[-3.1294326782226562, 14.70561408996582, "Microwave Imager Sounder Channel Nr. 1-5"]
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+[-3.1190481185913086, 14.706750869750977, "Microwave Imager Sounder Peaking altitude (km) 0-10"]
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+[-3.122922897338867, 14.722600936889648, "Microwave Imager Sounder Beam width 3.3\u00ba-6\u00ba"]
+[2.360825300216675, 13.683731079101562, "Optics Optics Type Athermal"]
+[2.365116596221924, 13.665037155151367, "Optics Temperature Range -15\u00ba to 50\u00baC"]
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+[-4.38994836807251, 7.395563125610352, "Data Transmission System Frequency Range 8025-8400 MHz"]
+[-4.3760223388671875, 7.378113269805908, "Data Transmission System Nominal Carrier Frequency 8192 (T1); 8320 (T2) MHz"]
+[-4.366077423095703, 7.364605903625488, "Data Transmission System Data Transmission Rate 15.36, 30.72, 61.44, or 122.88 Mbit/s"]
+[-4.359588623046875, 7.379438877105713, "Data Transmission System Transmitter Output Power 10 W"]
+[-4.375336647033691, 7.353741645812988, "Data Transmission System Data Modulation Type RFM, DRFM (Digital Radio Frequency Memory)"]
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+[-4.376502513885498, 7.364277362823486, "Data Transmission System Data Transmission Rate 80 kbit/s"]
+[-4.351284027099609, 7.336248397827148, "Data Collection and Transmission System Number of DCPs in Visibility Zone 150, < 500"]
+[-4.372132301330566, 7.344956874847412, "Data Collection and Transmission System Message Volume 250 bit"]
+[-4.369154930114746, 7.354869365692139, "Data Collection and Transmission System Data Transmission Rate 1200 or 400 bit/s"]
+[-4.34514045715332, 7.358555316925049, "Data Collection and Transmission System Location Accuracy of DCP 3.6 km (for one session)"]
+[-4.299725532531738, 7.306210994720459, "Data Collection and Transmission System Total Volume of Stored Data for One Orbital Revolution 300 kByte"]
+[-4.398011207580566, 7.356495380401611, "Data Collection and Transmission System Data Reception Frequency from DCPs 401.2-402.0 MHz"]
+[-4.369338035583496, 7.364023685455322, "Data Collection and Transmission System Data Transmission from S/C to Ground 1690-1710 MHz"]
+[-0.8384516835212708, 0.1566726267337799, "Satellite System Processing Time for One Snapshot Scene Unknown"]
+[-0.8593170046806335, 0.17500653862953186, "Satellite System Cumulative Processing Time from Raw Data Unknown"]
+[-0.8430871963500977, 0.16110943257808685, "Satellite System Level 1 B Pan-Sharpen Processing Time Unknown"]
+[0.6252943277359009, 12.10869312286377, "Sensor Operation Time Day and night"]
+[1.4326913356781006, 2.302429676055908, "Geostationary Lightning Mapper Function Improve storm hazard identification and increase warning lead-time"]
+[-1.8610854148864746, 12.826057434082031, "Solar Ultraviolet Imaging Operation Solar-pointing"]
+[0.41744568943977356, 12.203516006469727, "Sensor Measurement Localized measurements of particles and fields in geosynchronous orbit"]
+[-2.8454477787017822, 15.216972351074219, "Microwave Radiometer Channels 10 GHz to 89 GHz"]
+[-2.8413867950439453, 15.241388320922852, "Microwave Radiometer Number of Channels 17"]
+[-2.8180220127105713, 15.247562408447266, "Microwave Radiometer Operation Duration Over 5 years"]
+[-2.9314754009246826, 9.600593566894531, "Battery-Powered Device Power Source Battery"]
+[-3.8097221851348877, 7.941216468811035, "Data Storage Device Data Storage Tapes"]
+[0.10279231518507004, -4.030653953552246, "Satellite Platform Attitude Determination Star field camera and a gyro package in combination with a GPS (global positioning system) position determination"]
+[0.1072772890329361, -4.038287162780762, "Satellite Platform Attitude Control Cold-gas system"]
+[2.207185745239258, -1.995223045349121, "Satellite Attitude Control Software Available"]
+[1.0518791675567627, -2.074829339981079, "Satellite Pointing Accuracy 0.1\u00b0"]
+[2.5799458026885986, -2.2683191299438477, "Satellite RF Communications S-band"]
+[2.727137565612793, -2.4201877117156982, "Satellite Downlink Frequency X-band"]
+[1.8449761867523193, -1.867188811302185, "Satellite Attitude Sensing Star sensor, sun sensors, magnetometer, gyroscopes"]
+[-4.630389213562012, 9.035757064819336, "RF Signal Generator Center Frequencies 1257.5, 1236.5 or 1278.5 MHz"]
+[-4.58325719833374, 9.015442848205566, "RF Signal Generator Bandwidth 84 MHz, 42 MHz, 28 MHz or 14 MHz"]
+[-3.5254228115081787, 7.900786399841309, "Signal Compressor Compression Mode 4 bit, 2 bit, and no compression with or without the improved compression mode"]
+[-1.4595532417297363, 9.539421081542969, "Thruster Type Microthruster"]
+[-1.461513876914978, 9.531228065490723, "Thruster Purpose Orbit raising"]
+[5.065601825714111, -4.304530143737793, "Satellite Completion of CDR September 21, 2020"]
+[3.02996563911438, -1.7288858890533447, "Satellite Design Stage Production"]
+[1.6115666627883911, 23.224790573120117, "Instrument Power Consumption < 1 W"]
+[1.52463960647583, 21.24018669128418, "Instrument Mass 0.250 kg"]
+[1.6537452936172485, 22.16045379638672, "Instrument Dimensions 50 mm x 60 mm x 80 mm"]
+[2.4377999305725098, 22.39870262145996, "Instrument Optics Infrared optical triplet lens"]
+[2.4529619216918945, 22.346176147460938, "Instrument Detector Array Linear InGaAs photodiode array with 256 high-quantum efficiency pixels"]
+[2.5759522914886475, 22.414995193481445, "Instrument Order Filter Prevents visible radiation (below 900 nm) from entering the spectrometer chamber"]
+[-0.4385358393192291, 5.03146505355835, "Desert Lake Area 9,300 km2 (3,600 square miles)"]
+[-0.4000757038593292, 5.036442279815674, "Desert Lake Flooding Frequency Few times per century"]
+[-0.4256433844566345, 5.071831226348877, "Desert Lake Water Holding Time Varies"]
+[1.1323120594024658, 13.20358657836914, "Frequency and Modulation Type Binary Offset Carrier 1.1"]
+[-0.4136386513710022, 0.20263125002384186, "Satellite Navigation Systems Geodesy Nearly identical at ~ 2 cm"]
+[-0.4452546536922455, 0.21705465018749237, "Satellite Navigation Systems Timing Different but each system will transmit timing offsets"]
+[-0.4438149333000183, 0.196967214345932, "Satellite Navigation Systems Radio Frequency Compatible"]
+[-4.340095043182373, 0.1849546730518341, "GPS-Galileo Signal Use Civilian"]
+[7.225269794464111, 12.360079765319824, "Satellite Instrument Purpose Locate and measure methane emissions"]
+[0.869171679019928, -4.4430413246154785, "Satellite Weight 350 kg"]
+[2.8874664306640625, -1.254378080368042, "Satellite Mission Focus Collecting data about methane emissions from the oil and gas industry"]
+[2.764791250228882, -1.0858182907104492, "Satellite Emission Reduction Goal Cut methane emissions by 45% by the year 2025 from the oil and gas industry"]
+[-1.2708251476287842, 4.425400257110596, "Ground Station Equipment Parameter Value"]
+[-1.2931723594665527, 4.4036712646484375, "Ground Station Equipment Function Process TTC signals"]
+[-1.2762566804885864, 4.4113054275512695, "Ground Station Equipment Function Station Computer"]
+[-1.306973934173584, 4.387316703796387, "Ground Station Equipment Function Monitor and control ground station operations"]
+[-1.1518970727920532, 4.457136631011963, "Ground Station Function Frequency Band S-band"]
+[-1.2016016244888306, 4.4151787757873535, "Ground Station Function Mode Auto track and ranging functions"]
+[-1.2628716230392456, 4.426383972167969, "Ground Station Equipment Function Provide real-time voice/data/fax connectivity"]
+[1.1776349544525146, -0.7526699304580688, "Satellite Structure Size 60 cm x 60 cm x 80 cm"]
+[1.1106624603271484, -1.9829767942428589, "Satellite Pointing Accuracy 0.1\u00ba"]
+[1.2174943685531616, -2.0495965480804443, "Satellite Knowledge 0.02\u00ba"]
+[2.001960277557373, -0.6568365097045898, "Satellite Solar Power 180 W"]
+[1.202265977859497, -1.066726803779602, "Satellite Solar Array Length 1.7 m"]
+[1.7146390676498413, -1.901862382888794, "Satellite Solar Array Efficiency 26%"]
+[1.7742384672164917, -1.4763007164001465, "Satellite Li-ion Battery Capacity 15 Ah"]
+[2.0871596336364746, -2.421140193939209, "Satellite Hydrazine Thrusters Four 1 N thrusters"]
+[0.9829724431037903, -4.396421909332275, "Satellite Hydrazine Quantity 4.5 kg"]
+[1.9284389019012451, -2.921241044998169, "Satellite Hydrazine Thrusters Isp 210 s"]
+[0.7228497266769409, -4.1493048667907715, "Satellite Mass at Launch 120 kg"]
+[4.898723602294922, -2.3703765869140625, "Satellite Mission Design Life One year"]
+[4.762563705444336, -2.4824626445770264, "Satellite Goal Mission Life Two years"]
+[0.0885000079870224, 7.120237350463867, "Rendezvous Experiment GNC Functions Guidance, Navigation, and Control"]
+[0.10160184651613235, 7.143441200256348, "Rendezvous Experiment TRL Technology Readiness Level"]
+[1.6098589897155762, 2.2393593788146973, "Geostationary Satellite Band Ka-band"]
+[1.6028046607971191, 2.2698049545288086, "Geostationary Satellite Band S-band"]
+[-3.418009042739868, 8.172554016113281, "Signal Processing Equipment Signal Processing Bandwidth 200 MHz"]
+[-3.267773389816284, 8.191532135009766, "Signal Processing Equipment Port Configuration 3 x 3"]
+[-3.276477336883545, 8.154818534851074, "Signal Processing Equipment Components A/D converters, de-multiplexers, switches, multiplexers, D/A converters, and control unit"]
+[5.3331170082092285, -4.487173557281494, "Satellite Launch Date April 19, 2014"]
+[5.353768348693848, -4.404181003570557, "Satellite Launch Date November 2006"]
+[5.099796295166016, -4.461498737335205, "Satellite In-Space Disintegration Date February"]
+[2.012869358062744, -2.7106099128723145, "Satellite Number of Fragments Larger than 1 mm More than 50,000"]
+[4.193397045135498, -2.7664105892181396, "Satellite Potential Debris Release Prevention Within hours"]
+[2.343467950820923, -1.1992111206054688, "Satellite Sensor Complement Sea surface winds, sea surface temperatures, wave heights, internal waves, atmospheric water, sea ice features, ice sheet topography and ocean topography"]
+[0.14541983604431152, 7.194997310638428, "Experiment Dust Composition Forsterite (Mg2SiO4)"]
+[0.08143510669469833, 7.193635940551758, "Experiment Particle Size About the diameter of a human hair"]
+[0.13079394400119781, 7.1696953773498535, "Experiment Operation Start As soon as the universal serial bus (USB) connects to the NanoRacks platform"]
+[0.13007071614265442, 7.162770748138428, "Experiment Operation Duration In the first hour"]
+[-3.1510021686553955, 1.6994562149047852, "Satellite Mission Measurement Capabilities Vegetation, ice, and ocean parameters"]
+[-3.142582893371582, 1.6882108449935913, "Satellite Mission Purpose Better understand climate change and simulate its impact on humankind"]
+[0.15885856747627258, 15.744656562805176, "Alpha Magnetic Spectrometer Mass ~7,000 kg"]
+[0.1362844705581665, 15.723916053771973, "Alpha Magnetic Spectrometer Power Requirement 2.4 kW @ 28 V"]
+[0.1263786256313324, 15.739838600158691, "Alpha Magnetic Spectrometer Data Pipeline 10 Gbit/s"]
+[0.14189107716083527, 15.737225532531738, "Alpha Magnetic Spectrometer Data Connection 2 MB/s"]
+[0.18450219929218292, 15.74402141571045, "Alpha Magnetic Spectrometer Data Storage Approximately 200 TB"]
+[0.20390698313713074, 15.771016120910645, "Alpha Magnetic Spectrometer Computing Power Four 750 MHz PowerPC computers running Linux"]
+[-1.6673529148101807, 11.236814498901367, "Methane Remote Sensing Lidar Mission Launch Date Early 2023"]
+[1.1479886770248413, 0.6985232830047607, "Greenhouse Gas Satellite - Demonstrator Launch Date Early 2023"]
+[-0.97609943151474, -9.967023849487305, "Satellite Constellation Launch Date Early 2023"]
+[-0.09223559498786926, 15.535595893859863, "Spectrometer Spectral Range 5.0-15 \u00b5m (2000-667 cm -1)"]
+[-0.16466419398784637, 15.577276229858398, "Spectrometer Spectral Resolution FWHM (Full Width Half Maximum) 0.5 cm -1"]
+[-0.1166040301322937, 15.549921035766602, "Spectrometer Digitization Interval 0.25 s m -1"]
+[-0.1399656981229782, 15.537744522094727, "Spectrometer Detection Limit at 6 \u00b5m 3 x 10 -4  W m -2  sr -1  s m"]
+[-0.07030759006738663, 15.506997108459473, "Spectrometer Detection Limit at 13 \u00b5m 1 x 10 -4"]
+[-0.06137097626924515, 15.455367088317871, "Spectrometer Measurement Error 0.5 K"]
+[0.013421932235360146, 15.564310073852539, "Spectrometer IFOV 40 mrad x 40 mrad"]
+[-0.12013068795204163, 15.523046493530273, "Spectrometer Swath Width 2500 km"]
+[-0.09831330925226212, 15.519100189208984, "Spectrometer Pitch 100-110 km"]
+[-0.05881161242723465, 15.54992389678955, "Spectrometer Source Data Rate ~600 kbit/s"]
+[-0.03315999358892441, 15.506453514099121, "Spectrometer Mass ~50 kg"]
+[-0.11059552431106567, 15.535945892333984, "Spectrometer Power 50 W"]
+[0.636742889881134, 9.317431449890137, "Attitude Control Subsystem Attitude Knowledge \u00b10.02\u00ba"]
+[0.638759195804596, 9.30970573425293, "Attitude Control Subsystem Attitude Control \u00b10.05\u00ba"]
+[6.370746612548828, 7.363897323608398, "Satellite Component Position Knowledge \u00b160 m"]
+[6.382445335388184, 7.46049690246582, "Satellite Component Downlink < 300 m"]
+[6.3216657638549805, 7.386931419372559, "Satellite Component Processed Imagery < 100 m"]
+[2.8682143688201904, -1.0388230085372925, "Satellite Purpose Widely observe Algeria"]
+[1.6236932277679443, -1.2665406465530396, "Satellite Image Resolution High"]
+[2.776794910430908, -1.242165446281433, "Satellite Applications Cartography, agricultural management, crop monitoring, disaster management"]
+[-3.6316802501678467, 12.760509490966797, "Particle Detector Path Length 200 \u03bcm"]
+[-3.6572954654693604, 12.780838966369629, "Particle Detector Area 10 mm x 10 mm"]
+[-3.661994695663452, 12.77631664276123, "Particle Detector Separation 1.75 mm"]
+[-3.6535398960113525, 12.783339500427246, "Particle Detector Number of Channels 15"]
+[-0.7982004880905151, 14.206799507141113, "Dosimeter Number of Locations 3"]
+[-0.938232958316803, 14.121976852416992, "Dosimeter Function Trap positive charges and shift the threshold voltage"]
+[-5.406649589538574, 2.775287389755249, "Telescope Type Medium Wave Infra Red"]
+[-2.639619827270508, 11.687360763549805, "Imager Type Medium Wave Infrared"]
+[0.2463177591562271, 13.771382331848145, "Calibration System Black Body Temperatures 290 K, 340 K"]
+[3.3842694759368896, 13.497790336608887, "Laser Retro-reflectors Time Standard Synchronization Accuracy 10-9 s"]
+[3.314088821411133, 13.533839225769043, "Laser Retro-reflectors Orbital Distance Measurement Accuracy 10 cm"]
+[-4.748418807983398, 9.267387390136719, "Transmitter Output Power 2 W"]
+[-4.942913055419922, 9.778783798217773, "Receiver Function Uplink redundancy"]
+[3.467425584793091, 10.567540168762207, "Low-noise amplifier Characteristics Low noise and high gain"]
+[-6.714428901672363, 9.987610816955566, "Antennas Placement On the top and bottom of the spacecraft"]
+[5.308323383331299, -2.1993746757507324, "Satellite Design Life 5 years"]
+[5.026317596435547, -2.3591179847717285, "Satellite Working Life 10 years"]
+[3.732278347015381, 17.71996307373047, "Payload Observation Results Enormous"]
+[3.7459938526153564, 17.73423957824707, "Payload Observation Results Significant"]
+[-7.566948890686035, 5.891829967498779, "Camera Objective Monitoring (imaging) of reflected radiation of the Earth's surface and atmosphere (clouds)"]
+[-7.560050964355469, 5.888820171356201, "Camera Spatial Resolution 1.6 km x 1.8 km"]
+[11.335247993469238, 5.588583469390869, "Array of corner cubes Design Fizeau style reflectors similar in design to those used on Meteor-2-21"]
+[3.040148973464966, 22.802770614624023, "Instrument Unknown Unknown"]
+[2.8645660877227783, -1.0974494218826294, "Satellite Purpose Carry several experiments into orbit"]
+[4.961436748504639, -2.43501877784729, "Satellite Development Time Years"]
+[3.000563144683838, -1.3944761753082275, "Satellite Advancement Provides university students and faculty with a unique platform on which they can conduct science and engineering experiments"]
+[-3.842932939529419, 7.99664306640625, "Non-volatile Storage Function Allows configurations, calibrations, and more to be modified easily without a lengthy software upload"]
+[-1.6695706844329834, 8.376627922058105, "System Component Function Mitigate the risk of single-event upsets by resetting parameters, subsystems, or the entire system in the case of anomalous behaviour"]
+[-1.9315264225006104, 6.88112735748291, "Software Functionality Function Can save a mission if the software is not perfect at orbital insertion"]
+[0.2417096495628357, 13.793456077575684, "Sensor Calibration Function Can reduce tedious ADCS ground testing"]
+[-2.588400363922119, 9.649619102478027, "Power Source Size 9.29 m2"]
+[-2.6301229000091553, 9.568964004516602, "Power Source Power Output 2.2 kW"]
+[1.1585434675216675, -0.8932206630706787, "Satellite Length 7.3 m"]
+[0.9614115953445435, -4.35725736618042, "Satellite Mass 1220 kg"]
+[2.332653522491455, -0.7366873621940613, "Satellite Retirement Reason Power failure"]
+[2.9917681217193604, -1.874527931213379, "Satellite Disposal Scrapped"]
+[11.249306678771973, 5.5045857429504395, "CubeSat Manufacturer PIST (Pakistan Institute of Space Technology)"]
+[11.268866539001465, 5.49785041809082, "CubeSat Manufacturer University of Vigo, Spain"]
+[11.732072830200195, 5.404299259185791, "1U CubeSat Manufacturer Pontificia Universidad Cat\u00f3lica del Per\u00fa-Satellite"]
+[11.72397518157959, 5.359248161315918, "3U CubeSat Manufacturer Planet Labs Inc. (formerly Cosmogia Inc.)"]
+[-1.071936011314392, 7.874922275543213, "1.5U PocketQube Manufacturer MSU (Morehead State University)"]
+[-1.0606633424758911, 7.788567066192627, "2.5U PocketQube Manufacturer MSU (Morehead State University)"]
+[-0.9568336606025696, 7.836287021636963, "FemoSat (1U PocketQube) Manufacturer StaDoKo UG, Aachen, Germany"]
+[-1.0543497800827026, 7.781351566314697, "2.5U PocketQube Manufacturer University of Maryland"]
+[14.530428886413574, 7.672667503356934, "Nanosatellite Manufacturer TU Delft (Delft University of Technology)"]
+[14.5151948928833, 7.689639091491699, "Nanosatellite Manufacturer ISIS-BV, The Netherlands"]
+[14.529324531555176, 7.68220329284668, "Nanosatellite Manufacturer KHU (Kyung Hee University), Seoul, Korea"]
+[14.543782234191895, 7.683351993560791, "Nanosatellite Manufacturer KHU (Kyung Hee University), Seoul, Korea"]
+[11.629141807556152, 5.429318904876709, "2U CubeSat Manufacturer GomSpace ApS of Aalborg, Denmark"]
+[11.174424171447754, 5.411281108856201, "CubeSat Manufacturer EXA (Ecuadorian Civilian Space Agency)"]
+[-5.278961658477783, 7.91252326965332, "Communication System Beam Type Narrow"]
+[-5.198347091674805, 7.812966346740723, "Communication System Data Rate High"]
+[-5.228592395782471, 7.89417028427124, "Communication System Simultaneous Operation Imaging and Downlinking"]
+[-5.271017074584961, 7.910945415496826, "Communication System Pointing Type Body-pointed"]
+[2.6287028789520264, 14.321121215820312, "Optical Instrument Observation Angles Various"]
+[2.655700206756592, 14.360227584838867, "Optical Instrument Spectral Bands Not specified"]
+[2.663874626159668, 14.313044548034668, "Optical Instrument Telecentric Optics Array Angle 90\u00ba"]
+[2.6116394996643066, 14.318946838378906, "Optical Instrument Waveband 1020 nm"]
+[3.5875189304351807, 22.256519317626953, "Instrument Component Function Enables the successive study of different wavebands of visible light"]
+[0.5181679725646973, 12.271458625793457, "Sensor Spectrum Expansion By adding a band in the near-infrared, POLDER-P expands the spectrum being analyzed"]
+[0.829630970954895, 11.956657409667969, "Sensor Complement Unknown"]
+[0.8472333550453186, 11.975899696350098, "Sensor Complement Unknown"]
+[0.8385516405105591, 11.980941772460938, "Sensor Complement Unknown"]
+[0.8238182663917542, 11.979312896728516, "Sensor Complement Unknown"]
+[0.814275860786438, 11.953316688537598, "Sensor Complement Unknown"]
+[0.8822042942047119, 11.972467422485352, "Sensor Complement Unknown"]
+[0.8605526089668274, 11.956923484802246, "Sensor Complement Unknown"]
+[0.8550477027893066, 11.976778984069824, "Sensor Complement Unknown"]
+[-0.5288543105125427, 1.2235945463180542, "Satellite Orbit Altitude 490 \u00b110 km"]
+[-0.5340980291366577, 1.2437105178833008, "Satellite Orbit Inclination 89.0\u00b10.06\u00ba"]
+[-0.533636212348938, 1.2358478307724, "Satellite Orbit Eccentricity < 0.0025"]
+[0.9452991485595703, -1.4081591367721558, "Satellite Separation ~220 km"]
+[7.2209649085998535, 12.374189376831055, "Intersatellite Ranging Instrument Pointing Information TLE-based"]
+[7.234560966491699, 12.400729179382324, "Intersatellite Ranging Instrument Pointing Accuracy Not accurate enough"]
+[0.983278214931488, -4.35054874420166, "Satellite Mass 350 kg"]
+[1.5256297588348389, 21.242816925048828, "Instrument Satellite Mass 900 kg"]
+[1.1193116903305054, -1.3834037780761719, "Satellite Swath Width 260 km"]
+[1.6995395421981812, 21.980037689208984, "Instrument Swath Width 2600 km"]
+[2.0273540019989014, -2.04752254486084, "Satellite Detection Threshold 2 ppb"]
+[2.4804697036743164, 22.63431739807129, "Instrument Detection Threshold 12 ppb"]
+[1.422630786895752, -0.9612492322921753, "Satellite Pixel Size 400 x 100 m"]
+[1.745459794998169, 22.21043586730957, "Instrument Pixel Size 7000 x 7000 m"]
+[2.1485438346862793, -2.653975248336792, "Satellite Planned Number of Satellites 1"]
+[2.4753897190093994, 22.80390739440918, "Instrument Planned Number of Satellites 1"]
+[6.744216442108154, 6.954603672027588, "Satellite Component Unknown Unknown"]
+[2.9232490062713623, -2.122835874557495, "Satellite Unknown Unknown"]
+[4.437890529632568, -2.694465398788452, "Satellite Monitoring Duration Nearly a month"]
+[2.1602113246917725, -1.4491382837295532, "Satellite Method of Exoplanet Detection Measuring small dips in stellar brightness caused when a planet crosses in front of, or transits, its star"]
+[0.11027801036834717, 7.156234264373779, "Experiment Maneuver Description Does not advance towards or away from the target over multiple orbits"]
+[0.10732334852218628, 7.167224884033203, "Experiment Subgroup Description Sun-aligned stationkeeping is performed while the perigee is in eclipse and the VBS is used in cooperative mode"]
+[0.05981537699699402, 7.099432468414307, "Experiment Subgroup Description An identical maneuver is performed but at a later stage when the perigee is illuminated and the VBS can operate in non-cooperative mode"]
+[-0.6881678104400635, 8.582003593444824, "Cooler Unknown Unknown"]
+[-4.292476654052734, 0.20147795975208282, "GNSS Receiver Lock Maintenance Period 20 to 30 minutes"]
+[-4.308568000793457, 0.2154776006937027, "GNSS Receiver Euclidean Difference 4 to 10 km"]
+[-4.277180194854736, 0.22354543209075928, "GNSS Receiver Average Euclidean Difference 7 km"]
+[-4.945251941680908, 9.756649017333984, "Receiver Data Collection Frequency 1090 MHz"]
+[-4.945036888122559, 9.780518531799316, "Receiver Plane Positions Collected Thousands per day"]
+[14.285675048828125, 7.787613391876221, "Nanosatellite Delivery Schedule About 1 year after project kickoff"]
+[14.233068466186523, 7.813963890075684, "Nanosatellite Launch Date August 19, 2015"]
+[14.482574462890625, 7.721207618713379, "Nanosatellite Orbit Altitude ~400 km"]
+[14.52037525177002, 7.740606307983398, "Nanosatellite Orbit Inclination 51.6\u00b0"]
+[-4.764339923858643, 9.26887321472168, "Transmitter Frequency Bands 121.5 MHz, 406.025 MHz"]
+[-4.739101409912109, 9.248236656188965, "Transmitter Operational Characteristics High peak power output and a low duty cycle, Improved radio frequency stability, A unique identification code in each beacon, Digital transmissions that could be stored in a satellite's memory"]
+[-3.2386043071746826, 5.463341236114502, "Launch Vehicle Flight Number VA255"]
+[5.255824089050293, -4.279060363769531, "Satellite Launch Date 24 October 2021"]
+[5.055257797241211, -4.197839736938477, "Satellite Commercial Service Entry Date 22 July 2022"]
+[1.587256908416748, -1.2837233543395996, "Satellite Panchromatic Imagery Resolution 0.7m"]
+[1.5767791271209717, -1.24151611328125, "Satellite Multispectral Imagery Resolution 2.8m"]
+[4.116297245025635, -3.072779893875122, "Satellite Local Access Time 13:30 hours"]
+[2.1184234619140625, -1.4035145044326782, "Satellite Imaging Capability Afternoon"]
+[-1.8006384372711182, 8.744176864624023, "Controller Design Robust structured 6DoF controller using H-infinity and mu-tools"]
+[-2.7409698963165283, 8.717812538146973, "FFSW module Function Controls the absolute attitude of the spacecraft and estimates its absolute position"]
+[-0.14577780663967133, 9.180428504943848, "Navigation function Function Computes the absolute position, velocity and attitude of the spacecraft from sensors data and performs Angular Momentum Management (AMM) monitoring"]
+[-0.1565028876066208, 9.225179672241211, "Guidance function Function Computes the attitude profiles to be followed by the spacecraft"]
+[-1.7299349308013916, 8.875968933105469, "Control function Function Processes navigation estimates and guidance attitude profiles to generate the commanded torques needed to follow the reference profiles"]
+[-2.712263584136963, 8.687867164611816, "FFS module Function Distributes the actuations computed by the SC-GNC/FF-GNC (force and torque) to each single thruster and reaction wheels mounted in the spacecraft depending on their configuration"]
+[-0.8735591173171997, 12.36746597290039, "Radiation Detector Foil Material Aluminum"]
+[-0.8596665859222412, 12.387923240661621, "Radiation Detector Ion Blockage Energy Below 1 MeV"]
+[-0.8777481913566589, 12.39892292022705, "Radiation Detector Electron Pass Energy Greater than 50 keV"]
+[-0.862369179725647, 12.372393608093262, "Radiation Detector Foil Material Nickel"]
+[-0.8983561992645264, 12.229048728942871, "Radiation Detector Ion and Electron Pass Energy Greater than 50 keV"]
+[0.6102098822593689, -1.435896873474121, "Satellite Orbit Altitude 705 km"]
+[1.4647059440612793, -2.569593667984009, "Satellite Orbit Type Sun-Synchronous Orbit (SSO)"]
+[4.65669059753418, -2.604105234146118, "Satellite Station Keeping Duration > 10 years"]
+[2.9303901195526123, -1.5104180574417114, "Satellite Mission Observe clouds and aerosols in the A-train"]
+[5.834364414215088, 14.375603675842285, "Transponder Pass Band Channels 66"]
+[5.834362030029297, 14.375475883483887, "Transponder Channel Bandwidth 3 kHz"]
+[5.833033084869385, 14.37454891204834, "Transponder Uplink Frequency 402 MHz"]
+[5.834386825561523, 14.37547779083252, "Transponder Downlink Frequency 1675 MHz"]
+[-0.48189130425453186, 7.0428667068481445, "Technique Purpose Assess the collision risk to space missions from small-sized debris"]
+[5.363135814666748, -4.416774272918701, "Satellite Launch Date March 24, 1995"]
+[5.122776031494141, -4.475573539733887, "Satellite Explosion Date Feb. 3, 2015"]
+[2.0711510181427, -2.7875633239746094, "Satellite Number of Debris Pieces Produced 43"]
+[2.954556703567505, -2.0176637172698975, "Satellite Status Oldest continuously operational satellite in the DMSP weather constellation"]
+[2.0561952590942383, -1.9927383661270142, "Satellite Power Subsystem Issue Sudden spike in temperature, followed by an unrecoverable loss of attitude control"]
+[2.1012747287750244, -1.9046884775161743, "Satellite Debris Field Location Near the satellite"]
+[2.1386234760284424, -2.698190212249756, "Satellite Number of DMSP Satellites in Service 6"]
+[5.358669757843018, -4.462950706481934, "Satellite Launch Date April 2014"]
+[-5.376095294952393, 3.0257132053375244, "Telescope Array Unknown Unknown"]
+[-1.1918853521347046, 15.09308910369873, "Imaging multi-spectral radiometers Instrument type Imaging multi-spectral radiometers (vis/IR)"]
+[-5.376010417938232, 7.789251327514648, "Communications Instrument type Communications"]
+[0.1458577811717987, 7.191577911376953, "Experiment Purpose Search for antimatter, dark matter, other exotic matter, cosmic ray studies"]
+[0.08106902241706848, 7.127532958984375, "Experiment Team Composition 600 physicists and 56 institutes and organizations from 16 countries"]
+[0.1348702311515808, 7.175744533538818, "Experiment Collaboration North America (USA, Mexico), Asia (China, Korea, Taiwan), Europe, including nine ESA Member States (Denmark, Finland, France, Germany, Italy, The Netherlands, Portugal, Spain, Switzerland) and Russia"]
+[-3.0840187072753906, 1.7162754535675049, "Satellite Mission Observation Area Global-Scale"]
+[-3.1355478763580322, 1.6962326765060425, "Satellite Mission Observation Thermosphere-Ionosphere System"]
+[-0.8982325792312622, 3.204115390777588, "Black Hole or Neutron Star Mass About 10 times the mass of our Sun"]
+[-0.7843684554100037, 3.1946873664855957, "Black Hole or Neutron Star Material Consumption Rate About 30 times the mass of Earth per year"]
+[-0.4626513719558716, 5.831110954284668, "Unknown Population Far larger than currently observed"]
+[-0.4671894609928131, 5.827195167541504, "Unknown Number Found in Other Galaxies About 500"]
+[-7.5413384437561035, 5.913506507873535, "Camera Temperature Range -80\u00b0C"]
+[-7.482099533081055, 5.843343257904053, "Camera Focusing Length Adjustment 1 \u00b5m"]
+[0.5100778341293335, 10.974935531616211, "Image Sensors Quantity 112"]
+[0.4872203469276428, 10.931022644042969, "Image Sensors Contract Value \u20ac42 M"]
+[2.659857988357544, 5.390981674194336, "Beacon Frequency 162 MHz and 324 MHz"]
+[-1.8804830312728882, 7.257667064666748, "Platform Primary Structure Material Aluminum alloy"]
+[-1.8515030145645142, 7.359942436218262, "Platform Diameter 25.4 cm"]
+[-1.2830979824066162, 6.848989009857178, "Assemblies Quantity Two"]
+[-1.2893024682998657, 6.793170928955078, "Assemblies Location Near the forward end on the tubular supports"]
+[-0.17490915954113007, 6.388235092163086, "Test Site Image Acquisition Date 26 Dec. 2013"]
+[-0.08728108555078506, 6.413314342498779, "Test Site Mean \u0394E (m) 1.8"]
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+[-0.09682104736566544, 6.417463302612305, "Test Site \u0394r (m) 3.3"]
+[-0.17210978269577026, 6.384807109832764, "Test Site Image Acquisition Date 14 Mar. 2013"]
+[-0.1107286736369133, 6.434854507446289, "Test Site Mean \u0394E (m) 3.9"]
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+[-0.17391753196716309, 6.391940116882324, "Test Site Image Acquisition Date 20 Jan. 2014"]
+[-0.09035677462816238, 6.439988136291504, "Test Site Mean \u0394E (m) 2.4"]
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+[-0.16971957683563232, 6.383152961730957, "Test Site Image Acquisition Date 20 Jan. 2013"]
+[-0.09625566750764847, 6.427403450012207, "Test Site Mean \u0394E (m) 3.2"]
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+[-0.16383597254753113, 6.387063503265381, "Test Site Image Acquisition Date 14 Jul. 2014"]
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+[-0.19729074835777283, 6.365408420562744, "Test Site Image Acquisition Date 04 Feb. 2014"]
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+[-0.16798721253871918, 6.3783369064331055, "Test Site Image Acquisition Date 13 Jul. 2014"]
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+[-0.17202144861221313, 6.39704704284668, "Test Site Image Acquisition Date 24 Feb. 2013"]
+[-0.09554628282785416, 6.436849594116211, "Test Site Mean \u0394E (m) -8.4"]
+[-0.06852222979068756, 6.423988342285156, "Test Site Mean \u0394N (m) 4.4"]
+[-0.08990906178951263, 6.404166221618652, "Test Site \u0394r (m) 9.4"]
+[-0.16425633430480957, 6.400674343109131, "Test Site Image Acquisition Date 26 Jun. 2014"]
+[-0.09094401448965073, 6.4137115478515625, "Test Site Mean \u0394E (m) 6.2"]
+[-0.07969663292169571, 6.417086124420166, "Test Site Mean \u0394N (m) 4.6"]
+[-0.08913595974445343, 6.402439117431641, "Test Site \u0394r (m) 7.7"]
+[-0.18211199343204498, 6.392735958099365, "Test Site Image Acquisition Date 17 Aug. 2014"]
+[-0.0653853714466095, 6.42574405670166, "Test Site Mean \u0394E (m) -0.2"]
+[-3.633833169937134, 12.757607460021973, "Particle Detector Silicon Tracker Measures charged particle bending"]
+[-3.6432738304138184, 12.765563011169434, "Particle Detector Scintillation Counter Hodoscopes Determines particle time of flight (TOF) and velocity"]
+[-4.498390197753906, 12.071215629577637, "Magnet Goal Extend the energy range of particle and nuclei measurements to the multi-TeV region"]
+[-4.47925329208374, 12.056045532226562, "Magnet Components 2 main dipole coils and 12 racetrack coils, a superfluid helium vessel and a cryogenic system, all enclosed in an aluminum vacuum tank"]
+[-1.485929250717163, 16.883771896362305, "Altimeter Height Measurement Accuracy \u00b1 10 cm"]
+[-1.497601866722107, 16.89942169189453, "Altimeter Wave Height Measurement Accuracy \u00b1 10% or 0.5 m, whichever is greater"]
+[-1.5057330131530762, 16.90318489074707, "Altimeter Backscatter Coefficient Measurement Accuracy \u00b1 1.0 dB"]
+[2.075035572052002, -1.7161129713058472, "Satellite Observation Mode DRC and full-pol. observation simultaneously"]
+[1.1135454177856445, -1.5072438716888428, "Satellite Swath 40-50 km"]
+[1.4461019039154053, -1.1321097612380981, "Satellite Resolution Down to 6 m"]
+[0.7212092280387878, -2.2735369205474854, "Satellite Off-nadir Angle 18-35\u00ba"]
+[-0.7556962966918945, 8.610050201416016, "Cooler Nominal Temperature 95 K"]
+[-0.797508955001831, 11.586368560791016, "Detectors Number of Elements 16"]
+[-0.8325788378715515, 11.63420295715332, "Detectors IGFOV 28 microradians (\u00b5rad)"]
+[-5.9327545166015625, 8.41954231262207, "Channel ROIC Technology Thick-film technology"]
+[-5.906527519226074, 8.457764625549316, "Channel ROIC Components Capacitive trans-impedance amplifiers, 8:1 multiplexer, output buffer"]
+[-7.556114673614502, 5.89519739151001, "Camera Resolution 7 m"]
+[-7.534238338470459, 5.914231777191162, "Camera Resolution 1.05 m"]
+[-7.597052097320557, 5.866076946258545, "Camera Quantity 4"]
+[-7.557727813720703, 5.898371696472168, "Camera Design Smart and low mass, low power, and highly-integrated"]
+[-7.542196273803711, 5.905333042144775, "Camera Technologies Auto-exposure, high-speed compression of color imagery and static gray image, and sub-sampling methods"]
+[4.795722484588623, -4.377469539642334, "Satellite Groundwater Storage Measurement Date January 11, 2021"]
+[1.8031729459762573, -1.2384655475616455, "Satellite Groundwater Storage Measurement Wetness Percentile"]
+[2.0022635459899902, -1.2635908126831055, "Satellite Groundwater Storage Measurement Blue areas have more water than usual, and orange and red areas have less"]
+[-2.218158721923828, 7.1824116706848145, "Onboard Management Unit Developer Acer Inc."]
+[-1.9346638917922974, 6.9087138175964355, "Software Module Developer Tatung System Technologies Corp."]
+[0.6019248366355896, 12.041071891784668, "Sensor Developer Shihlin Electric & Engineering Corporation"]
+[-6.580334186553955, 9.888733863830566, "Antennas Manufacturer Victory Industrial Corp."]
+[-3.684985637664795, 6.956367015838623, "Data Repository Purpose Providing open access to night time images for use by the media, public, and scientists"]
+[-3.4685633182525635, 6.832927227020264, "Data Use Estimating the types of light sources, comparing the lighting and the economic health of a city, evaluating lighting for road and public safety, correlating light pollution with effects on human health and biodiversity"]
+[-1.5933423042297363, 9.686895370483398, "Propulsion System Propellant Iodine"]
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+[-2.9834752082824707, 4.16204309463501, "Spacecraft Orbital Path Uses the gravity of the sun, Earth and moon"]
+[-3.023845911026001, 4.217483997344971, "Spacecraft Trajectory Low energy trajectory using gravitational manifolds"]
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+[-5.0337443351745605, 2.9005749225616455, "Space Telescope Observation Result Inner regions of a star are extremely turbulent at the time of detonation"]
+[-2.2116520404815674, 5.945888042449951, "Aircraft Altitude Lower"]
+[-2.2013094425201416, 5.94185209274292, "Aircraft Measurement Duration Few seconds"]
+[-2.224119186401367, 5.9595208168029785, "Aircraft Purpose Measure wind speed and direction"]
+[-2.227473735809326, 5.923434734344482, "Aircraft Purpose Adjust route to fly over sea ice"]
+[-2.203765392303467, 5.945621967315674, "Aircraft Purpose Drop lower again to measure wind speed"]
+[3.0504486560821533, 22.811250686645508, "Instrument Unknown Unknown"]
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+[-5.2898454666137695, 9.023470878601074, "SGLS Transponder Radio Downlink Speed Up to 2 Mbit/s"]
+[-5.2876715660095215, 9.020708084106445, "SGLS Transponder Radio Orbit 6,000 km x 12,000 km"]
+[-5.292596817016602, 9.027295112609863, "SGLS Transponder Radio Uplink Margin 23.2 dB worst case"]
+[-5.319753170013428, 9.041287422180176, "SGLS Transponder Radio Downlink Margin 5.0 dB for safe mode at 500 bit/s and 5.1 dB in nominal operations at 1 Mbit/s"]
+[-5.294872760772705, 9.028097152709961, "SGLS Transponder Radio Ranging Margin 8.1 dB"]
+[-5.289455890655518, 9.016575813293457, "SGLS Transponder Radio Command Uplink Speed 2 kbit/s"]
+[-5.266961574554443, 9.033804893493652, "SGLS Transponder Radio Antenna Coverage Approximately 4\u03c0 steradian"]
+[-5.280383110046387, 9.049445152282715, "SGLS Transponder Radio Antenna FOV 64\u00ba"]
+[1.7305883169174194, -0.47107598185539246, "Satellite Imager Detector Output Sampling Rate 5460 samples/s for MIR, WV, TIR-1 and TIR- 2 channels and 21840 samples/s for the VIS and SWIR channels"]
+[1.7420722246170044, -0.5215474963188171, "Satellite Imager Scan Rate 20\u00b0/s"]
+[1.7151515483856201, -0.5070759057998657, "Satellite Imager Over-sampling Ratio 1.75 for all channels except WV, 3.5 for WV channel"]
+[1.6951813697814941, -0.41467323899269104, "Satellite Imager VIS and SWIR Sample Size 16 \u00b5rad E/W"]
+[1.6987614631652832, -0.4693043828010559, "Satellite Imager IR Sample Size 64 \u00b5rad E/W"]
+[1.3308501243591309, -1.2043548822402954, "Satellite Height Measurements Thousands"]
+[2.3874382972717285, -1.4564954042434692, "Satellite Measure Area Frequency More frequent than ICESat-2"]
+[2.335598945617676, -1.4387011528015137, "Satellite Measure Area Frequency More frequent than ICESat-2"]
+[2.7160420417785645, -1.6870990991592407, "Satellite Take Measurements Through Clouds Yes"]
+[2.6836037635803223, -1.673100233078003, "Satellite Take Measurements Through Clouds Yes"]
+[2.270616292953491, -1.5924679040908813, "Satellite L-band Synthetic Aperture Radar Parameter Value Unknown"]
+[2.8515496253967285, -1.646925449371338, "Satellite Software Provider SPACEBEL"]
+[2.6112639904022217, -1.7393033504486084, "Satellite Payload VBN payload"]
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+[-1.4247028827667236, 1.1989295482635498, "Data Relay Satellite Launch Date 29 May 2020"]
+[-1.4478107690811157, 1.2221405506134033, "Data Relay Satellite URL http://www.esa.int/Applications/Telecommunications_Integrated_Applications"]
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+[-0.46852830052375793, 5.841487407684326, "Unknown Number of Feeds Too many"]
+[-6.823726654052734, 10.174544334411621, "Antenna Array Size Doubling Doubled"]
+[11.193523406982422, 5.302743434906006, "CubeSat Mass 4.1 kg"]
+[11.178866386413574, 5.262681007385254, "CubeSat Mass 1.3 kg"]
+[11.167969703674316, 5.23494291305542, "CubeSat Mass 1.1 kg"]
+[11.184507369995117, 5.282416343688965, "CubeSat Mass 3.7 kg"]
+[11.152234077453613, 5.260140895843506, "CubeSat Mass 4.0 kg"]
+[11.149053573608398, 5.263947486877441, "CubeSat Mass 3.5 kg"]
+[11.16638469696045, 5.252420425415039, "CubeSat Mass 2.6 kg"]
+[11.182293891906738, 5.240011692047119, "CubeSat Mass 1.1 kg"]
+[11.163780212402344, 5.2679829597473145, "CubeSat Mass 2.8 kg"]
+[2.0369277000427246, 22.654325485229492, "Instrument Wavelength 443 nm"]
+[2.1869990825653076, 22.773216247558594, "Instrument Bandwidth 20 nm"]
+[2.6543021202087402, 22.498138427734375, "Instrument Polarization yes"]
+[2.008280038833618, 22.424640655517578, "Instrument Dynamic Range (Normalized Radiance) 0.05-0.22"]
+[2.388610601425171, 22.121461868286133, "Instrument Main Measurement Objective Ocean colour"]
+[2.0449182987213135, -2.7390270233154297, "Satellite Number of Stars Monitored More than 200,000"]
+[2.050485372543335, -2.7570855617523193, "Satellite Number of Transiting Exoplanet Candidates More than 1,500"]
+[2.0411646366119385, -2.762526750564575, "Satellite Number of Earth-sized and \u2018Super Earth\u2019 planets ~500"]
+[3.1827261447906494, -1.5614913702011108, "Satellite Lead Institution MIT (Massachusetts Institute of Technology)"]
+[2.3617281913757324, -1.5229870080947876, "Satellite Responsible for the Cameras MIT/LL (Lincoln Laboratory)"]
+[3.042907476425171, -1.589406132698059, "Satellite Project Management Provider NASA/GSFC (Goddard Space Flight Center)"]
+[1.8366416692733765, -2.2358927726745605, "Satellite Spacecraft Builder and Operator Orbital ATK (OA)"]
+[2.9485151767730713, -1.6989142894744873, "Satellite Mission Operations Center OA Mission Operations Center"]
+[1.0084850788116455, -4.443154811859131, "Satellite Mass 694 kg"]
+[14.644603729248047, 7.786025047302246, "Nanosatellite Mass 6.5 kg"]
+[11.132071495056152, 5.230648994445801, "CubeSat Mass 1 kg"]
+[-0.15405626595020294, 15.420559883117676, "High Energy Proton Spectrometer Proton Energy Range 15-440 MeV"]
+[-0.16769269108772278, 15.400036811828613, "High Energy Proton Spectrometer Electron Energy Range 1.5-20 MeV"]
+[-0.22701960802078247, 15.373696327209473, "Low Energy Imaging Proton Spectrometer Proton Energy Range 30 keV - 2 MeV"]
+[-0.20346009731292725, 15.3646240234375, "Low Energy Imaging Proton Spectrometer Electron Energy Range 30 keV - 2 MeV"]
+[-0.18346522748470306, 14.939229011535645, "Low Energy Electrostatic Analyzer Particle Energy Range 100 eV - 50 keV"]
+[-0.16462509334087372, 15.451227188110352, "High Energy Imaging Proton Spectrometer Proton Energy Range 30-300 MeV"]
+[-0.15595126152038574, 15.425650596618652, "High Energy Imaging Proton Spectrometer Electron Energy Range 1-10 MeV"]
+[-3.6938071250915527, 7.1967363357543945, "Data Distribution Centers Data Distribution Frequency Daily"]
+[-4.49216890335083, 8.281205177307129, "Local User Terminals Operation With the LEOSAR payloads on the various spacecraft in orbit"]
+[-4.458637714385986, 8.300725936889648, "Local User Terminals Operation With the GEOSAR payloads flown on various GEO missions"]
+[-4.552603721618652, 8.278717041015625, "Local User Terminals Status In the definition/prototype phase as of 2008"]
+[-4.487367630004883, 8.305400848388672, "Local User Terminals Basic Tasks Track Cospas and Sarsat satellites, Recover beacon signals from satellites, Perform Doppler processing to determine geographic location, Send resulting Doppler solutions to the associated MCC"]
+[-4.517528057098389, 12.112239837646484, "Magnetometer Absolute Measurement Error < 0.5 nT"]
+[-4.505757808685303, 12.108162879943848, "Magnetometer Measurement Range 16,000 - 64,000 nT"]
+[-4.502875804901123, 12.106568336486816, "Magnetometer Sampling Rate 1 Hz"]
+[-4.512840270996094, 12.109704971313477, "Magnetometer Sensor Mass 1 kg"]
+[-4.497549533843994, 12.122467041015625, "Magnetometer Instrument Mounting Boom-mounted at a distance of 8 m"]
+[-4.5205464363098145, 12.107556343078613, "Magnetometer Instrument Mass 2.5 kg"]
+[-4.515830039978027, 12.059757232666016, "Magnetometer Power 3 W"]
+[2.0144293308258057, -1.413256049156189, "Satellite Distance Metrology Laser-based"]
+[-0.9250481724739075, -10.032727241516113, "Satellite Constellations Orbit Inclinations Different"]
+[-0.9402474761009216, -10.012406349182129, "Satellite Constellations Absorbed Effects Daily and Subdaily Phenomena"]
+[-0.9269956946372986, -10.005508422851562, "Satellite Constellations De-aliasing Not Needed"]
+[-0.9619242548942566, -10.032686233520508, "Satellite Constellations Striping Almost Entirely Removed"]
+[1.4273860454559326, -1.2079733610153198, "Satellite Radio Wave Wavelength 15 - 30 cm"]
+[2.2403695583343506, -1.4364250898361206, "Satellite Ability Penetrate rain and clouds, penetrate forest canopies"]
+[2.0338189601898193, -1.740003228187561, "Satellite Operational Modes Rate Damping Mode, Sun Acquisition Mode, Earth Acquisition Mode, Fine Normal Mode"]
+[-13.863212585449219, -2.2392578125, "X-ray Telescope Sensitivity 25 times more sensitive than its predecessor ROSAT"]
+[-13.85926342010498, -2.2137739658355713, "X-ray Telescope Number of All-Sky Surveys 8"]
+[-0.7210050225257874, 2.977642059326172, "Supernova Remnant Radio Emission Confirmation Confirmed in 10-year-old surveys"]
+[-0.7160540223121643, 2.9659173488616943, "Supernova Remnant X-ray Data Discovery Expected to discover new supernova remnants in its X-ray data over the next few years"]
+[2.40600323677063, -1.5003377199172974, "Satellite Sensor Payloads Dual optical-infrared sensor payloads"]
+[2.235673189163208, -1.2775439023971558, "Satellite Sensor Payloads Capability See at nighttime, in low light conditions and in bad weather"]
+[-1.9141777753829956, 6.88682746887207, "Software Included Features Global activity monitoring, Comprehensive commercial satellite imagery, Automated tipping and cueing, Secure online environment for analyst collaboration"]
+[2.2331953048706055, -2.470745325088501, "Satellite Provider Number of 1-meter satellites in orbit Four"]
+[2.2768967151641846, -2.4630587100982666, "Satellite Provider Number of satellites in its constellation by early 2021 16"]
+[3.174816846847534, -1.791038990020752, "Satellite Manufacturer SSTL (Surrey Space Technology Ltd.)"]
+[2.6326353549957275, -1.9615676403045654, "Satellite Former Name GSTB-V2/A"]
+[-0.8518056273460388, 0.1713016927242279, "Satellite System RNSS Signal Allocations Deadline Mid-2006"]
+[-0.8346591591835022, 0.151253804564476, "Satellite System Number of Satellites Two"]
+[-6.731081485748291, 9.996397018432617, "VLF Antenna Length 80 m"]
+[-6.7184319496154785, 9.996393203735352, "VLF Antenna Length 16 m"]
+[2.5216586589813232, 21.895687103271484, "Instrument Function Measures the local magnetic field"]
+[2.5327463150024414, 22.01983642578125, "Instrument Function Measures the local electric field"]
+[-6.72437047958374, 9.994091033935547, "VLF Antenna Design Consideration Longer and wider is better"]
+[-1.3215186595916748, 6.1296067237854, "Educational Institution Location Arabic Language Institute"]
+[-1.3970768451690674, 6.204092502593994, "Educational Institution Type Largest all-female university in the world"]
+[-1.8141354322433472, 7.472412109375, "Infrastructure Lighting Bright, regular"]
+[-0.7939085960388184, 5.182300567626953, "Residential Area Lightning Blue-gray"]
+[0.03814537078142166, 7.115703105926514, "Research Experiment Sponsor DLR, the German Space Agency, and DreamUp"]
+[0.09770814329385757, 7.149857044219971, "Research Experiment University Goethe University in Frankfurt"]
+[-3.6102187633514404, 12.714521408081055, "Particles Size Submillimeter to millimeter"]
+[2.06955623626709, -2.746419906616211, "Satellite Quantity 2"]
+[2.5783021450042725, -2.0399510860443115, "Satellite Names MySat-1 and the second CHEFSat satellite"]
+[-3.1047298908233643, 9.666247367858887, "Battery Capacity 7700 mAh"]
+[-3.0733323097229004, 9.63870906829834, "Battery DOD (Depth of Discharge) 17.9%"]
+[-1.912204623222351, 8.722508430480957, "Circuit Type Constant current/constant voltage charging"]
+[-2.56778621673584, 9.11303424835205, "Converter Output +5 V, +3.3 V"]
+[-1.37030827999115, 8.55483627319336, "Electrical Component Fuse To protect the circuit from the overcurrent"]
+[2.6835336685180664, 14.497150421142578, "Multispectral Instrument Spatial Resolution 10 meter"]
+[2.636486053466797, 14.51452350616455, "Multispectral Instrument NIR/SWIR Bands Additional NIR/SWIR bands"]
+[2.6633493900299072, 14.515958786010742, "Multispectral Instrument Re-visit Time Short"]
+[-0.8981310129165649, 6.787349224090576, "Process Objective Develop and validate new algorithms relevant for coral reef monitoring based on Sentinel-2 observations"]
+[-2.567434310913086, 9.350985527038574, "Power Generation System Voltage 300 V"]
+[-2.57893967628479, 9.330982208251953, "Power Generation System Monitoring Frequency Every minute"]
+[-2.5832459926605225, 9.362900733947754, "Power Generation System Arc Detection Monitoring Frequency Every second"]
+[-0.15627580881118774, 6.841858863830566, "Test Time 60 minutes"]
+[-1.5100581645965576, 13.437562942504883, "Solar Array Test Time 60 minutes"]
+[-2.1422348022460938, 4.306595802307129, "Space Station Operation Authorization Through 2024"]
+[-2.1343607902526855, 4.311191082000732, "Space Station Funding $17 million in fiscal year 2021"]
+[-2.14339017868042, 4.3045268058776855, "Space Station Prime Contractor Boeing"]
+[-2.1295573711395264, 4.310847282409668, "Space Station Solar Arrays Six additional"]
+[-0.8293282389640808, 12.64277458190918, "Radiation Monitor Objective To monitor aspects of space radiation which cause single event effects in microelectronic components"]
+[-0.8491881489753723, 12.677553176879883, "Radiation Monitor Instrument Type Compact, low power monitor housed on a single board"]
+[-0.8590072989463806, 12.687453269958496, "Radiation Monitor Telescopes Two telescopes"]
+[-0.8652742505073547, 12.40076732635498, "Radiation Detector Diodes Area 3cm2"]
+[-0.8678150773048401, 12.285418510437012, "Radiation Detector Coincidence Two pin diodes in coincidence"]
+[-0.8604274392127991, 12.390143394470215, "Radiation Detector Data Storage Programmable time bins"]
+[1.4369927644729614, 2.7551538944244385, "Weather Satellite Launch Date Nov. 4"]
+[1.4477596282958984, 2.7485463619232178, "Weather Satellite Launch Site Kennedy Space Center, Florida"]
+[1.4486753940582275, 2.7553865909576416, "Weather Satellite Ground System Global network of receiving stations linked to NOAA"]
+[1.4380009174346924, 2.7552292346954346, "Weather Satellite Number of Planned Mission Rehearsals 6"]
+[1.4384431838989258, 2.7646777629852295, "Weather Satellite Launch Date October 2016"]
+[-1.4716532230377197, 8.094067573547363, "Electronic Equipment Location Fit in the other half of the chassis"]
+[-5.323735237121582, 2.8477277755737305, "Telescope Location Takes up approximately half of the chassis volume"]
+[-0.792788565158844, 12.609445571899414, "Radiation Sensor Location Fit in the other half of the chassis"]
+[-5.3987345695495605, 2.7386906147003174, "Telescope Dimensions 10 cm x 20 cm x 30 cm"]
+[1.134382963180542, -0.670673131942749, "Satellite Dimensions Roughly 10 x 20 x 30 cm"]
+[5.336699485778809, -4.336524486541748, "Satellite Launch Date 1978"]
+[4.520519256591797, -2.6198248863220215, "Satellite Mission Duration 105 days"]
+[2.4987480640411377, -1.4703699350357056, "Satellite Image Catalogue Availability Freely available"]
+[-0.9363949298858643, -10.004552841186523, "Satellite Constellation Number of Satellites 2"]
+[-0.9547082185745239, -9.992603302001953, "Satellite Constellation Planned Number of Satellites 8 by year\u2019s end"]
+[-0.9496888518333435, -10.001402854919434, "Satellite Constellation Long-Term Goal Deploy 30 satellites by 2023, and possibly 60 in the years after"]
+[-0.9381232261657715, -10.015049934387207, "Satellite Constellation Imaging Type High-revisit"]
+[-0.9495953321456909, -10.004222869873047, "Satellite Constellation Service Type Global monitoring and alerting services"]
+[2.8721656799316406, -1.6980972290039062, "Satellite Operator Measure Emissions from Individual Facilities Unknown"]
+[5.309042930603027, -4.343617916107178, "Satellite Operator Launch Date No earlier than Oct. 1, 2022"]
+[-1.3395721912384033, 6.097198963165283, "Company Senior Executive Vice President Massimo Comparini"]
+[-2.1457574367523193, 2.904489755630493, "Observatory Official Launch Date Toward the end of the third quarter \u2014 or early in the fourth quarter \u2014 of this year"]
+[-3.569612503051758, 12.770742416381836, "Charged Particle Detector Electron Energy Range 50 keV - 1 MeV"]
+[-3.5223093032836914, 12.745628356933594, "Charged Particle Detector Proton Energy Range 250 keV - 30 MeV"]
+[-3.5836236476898193, 12.773418426513672, "Charged Particle Detector Alpha-particle Energy Range 1-100 MeV"]
+[-3.5829885005950928, 12.760554313659668, "Charged Particle Detector Field of View 15-45\u00ba"]
+[-3.5834507942199707, 12.77619743347168, "Charged Particle Detector Mass 2.3 kg"]
+[-3.593334913253784, 12.768060684204102, "Charged Particle Detector Power Consumption 1 W"]
+[-3.555771827697754, 12.761154174804688, "Charged Particle Detector Size 260 mm x 199 mm x 113 mm"]
+[-1.3040523529052734, 9.447750091552734, "N/A N/A N/A"]
+[0.5104120373725891, 10.932526588439941, "Image Sensor Image Resolution 20 megapixels"]
+[0.522495687007904, 11.000329971313477, "Image Sensor Measurement Interval Every 25 seconds"]
+[0.5186782479286194, 10.977483749389648, "Image Sensor Measurement Interval Every 2.5 seconds"]
+[-5.4716796875, 2.735085964202881, "Telescope Image Resolution About 80 Mpixels"]
+[1.575089693069458, -1.1409192085266113, "Satellite Total Image Resolution 2.12 gigapixels"]
+[0.5128224492073059, 10.921988487243652, "Image Sensor Optically Sensitive Surface 0.74 m2"]
+[0.5098971724510193, 10.926671981811523, "Image Sensor Operating Temperature Lower than -65\u00b0C"]
+[-6.648306369781494, 9.955915451049805, "Antenna System Thermal Model Identification Unknown"]
+[-6.694185733795166, 9.988618850708008, "Antenna Unknown Unknown"]
+[-0.08748374134302139, 13.569461822509766, "Measurement System Components Lateral system and longitudinal system"]
+[-0.11665940284729004, 13.507935523986816, "Measurement System Sensor CMOS sensor"]
+[-0.0815695971250534, 13.523606300354004, "Measurement System Sensor Photodiode"]
+[-1.0469061136245728, 7.9493536949157715, "Device Function Converts the lateral and longitudinal signals into a 3D displacement"]
+[0.16498731076717377, 7.157803535461426, "Experiment Dust 56%"]
+[0.13669143617153168, 7.163940906524658, "Experiment Cals 100%"]
+[0.1397329568862915, 7.176236152648926, "Experiment Sprites 100%"]
+[0.14281189441680908, 7.19119119644165, "Experiment Ozone Limb Sounding 100%"]
+[0.1377113163471222, 7.178389072418213, "Experiment Ozone Limb Sounding 88%"]
+[0.13931898772716522, 7.161710739135742, "Experiment Critical Viscosity of Xenon 100%"]
+[0.15566398203372955, 7.153850078582764, "Experiment Solar Constant 100%"]
+[0.14037807285785675, 7.184142589569092, "Experiment Communications and Navigation 100%"]
+[0.13983319699764252, 7.174289703369141, "Experiment Space Experiment Module 100%"]
+[3.0573160648345947, -1.4339210987091064, "Satellite Applications Team Organize and develop a mission applications program"]
+[2.4921422004699707, -1.8767082691192627, "Satellite Ground Segment Overview"]
+[-0.13089428842067719, 9.16043758392334, "Navigation Device Data Types Time, position, velocity, HDOP, GDOP"]
+[0.8331953287124634, 12.060546875, "Sensor Quantity 3"]
+[0.5689062476158142, 12.13573169708252, "Sensor Technology Magneto resistive device of Honeywell HMC 2003"]
+[0.5511800646781921, 12.035528182983398, "Sensor Technology Fluxgate sensor by Applied Physics Systems"]
+[1.6542260646820068, 6.974186897277832, "Communication Device Frequency Band S-band"]
+[0.5572816729545593, 12.069019317626953, "Sensor Purpose Fine Lateral and Longitudinal Sensor"]
+[-3.095010757446289, 2.4319353103637695, "Mission Formation-flying Date 6 May, 2013"]
+[0.05393505096435547, 13.417891502380371, "Metrology System Presentation Date July 24, 2014"]
+[-0.24049809575080872, 15.816405296325684, "Spectrogram Device Time Period 7 seconds"]
+[-0.24460721015930176, 15.724559783935547, "Spectrogram Device Radio Frequency Range Not provided"]
+[1.519405722618103, -2.4031572341918945, "Satellite Orbit Medium Earth Orbit (MEO)"]
+[1.1010912656784058, -1.1253522634506226, "Satellite Span Nearly the length of a football field"]
+[0.4469154179096222, 12.19420337677002, "Sensor Swath Width 10 km"]
+[0.5371106266975403, 12.212350845336914, "Sensor Ground Sample Distance (GSD) 2 m"]
+[0.4961085915565491, 12.226194381713867, "Sensor Ground Sample Distance (GSD) 0.5 m"]
+[0.593636691570282, -1.4711108207702637, "Satellite Orbit Altitude 504 km"]
+[0.6830902695655823, -2.280186891555786, "Satellite Orbit Inclination 97.4\u00b0"]
+[-1.6732375621795654, 11.235273361206055, "Lidar Instrument Type Lidars"]
+[-1.6913573741912842, 11.233162879943848, "Lidar Measurement Domain Atmosphere"]
+[-1.6861624717712402, 11.228357315063477, "Lidar Measurement Category Cloud type, amount and cloud top temperature, Atmospheric Temperature Fields, Cloud particle properties and profile, Aerosols"]
+[-1.666908860206604, 11.23117446899414, "Lidar Launch Date 10 Jan 2015"]
+[-1.6739389896392822, 11.226541519165039, "Lidar End of Life Date 30 Sep 2018"]
+[0.5741368532180786, 12.100274085998535, "Sensor Scanning Period Up to 140 ms"]
+[0.518744707107544, 12.280549049377441, "Sensor Spectral Bands 3.8, 10.85, and 11.85 \u00b5m"]
+[0.5316663980484009, 12.286238670349121, "Sensor Spectral Bands 3.8, 10.85, and 11.85 \u00b5m"]
+[0.5120624899864197, 12.091462135314941, "Sensor Application Forest fires detection and monitoring"]
+[0.5243771076202393, -1.8911055326461792, "Satellite Parameter Value 268 km"]
+[0.5568300485610962, -2.004021167755127, "Satellite Parameter Value -62 \u00ba"]
+[0.5451464653015137, -1.9267112016677856, "Satellite Parameter Value 0.3"]
+[0.5373395085334778, -1.966995120048523, "Satellite Parameter Average Value 9.75 m"]
+[0.5333072543144226, -1.8956329822540283, "Satellite Parameter Standard Deviation 66.0 m"]
+[2.4892332553863525, -1.2043161392211914, "Satellite Data Collection Elevation measurements of Earth\u2019s surface"]
+[2.380709409713745, -1.6266480684280396, "Satellite Function Measure the shape and depths of lake beds and shallow seafloors"]
+[2.358952522277832, -1.1487356424331665, "Satellite Data Correlation Satellite-derived bathymetry results were correlated with field measurements of the lake taken via boat, helicopter, and land surveyors between June 1974 and September 1976"]
+[1.241434097290039, -1.1669875383377075, "Small Satellite Mission of the Year Award 14 August 2018"]
+[1.2642550468444824, -1.1286191940307617, "Small Satellite Image of Los Angeles 1 16 May 2019"]
+[-3.149794816970825, 2.2485713958740234, "Resupply Mission Launch Unknown"]
+[-1.746429204940796, 16.997222900390625, "Radar Altimeter Frequency 13.6 GHz (Ku-band) and 5.3 GHz (C-band)"]
+[-1.7403252124786377, 16.98052215576172, "Radar Altimeter Bandwidth 320 MHz"]
+[-1.713680386543274, 16.992326736450195, "Radar Altimeter Antenna Control Pointing Accuracy 0.14\u00ba (1 \u03c3)"]
+[-1.6966521739959717, 16.972227096557617, "Radar Altimeter Mass 230 kg"]
+[-1.7248915433883667, 16.988800048828125, "Radar Altimeter Power 237 W"]
+[-1.7232344150543213, 16.98550033569336, "Radar Altimeter Altitude Measurement Accuracy 2.4 cm"]
+[-1.8649768829345703, 8.791168212890625, "Electronic Separation Switch Module Voltage 28\u00b15 V"]
+[-2.514326333999634, 9.20655345916748, "Power Conditioning Module Voltage Conversion Raw 28\u00b15 V battery voltage level to regulated \u00b15 V level"]
+[-2.5524473190307617, 9.291302680969238, "Power Conditioning Module Power Consumption 164.2 W"]
+[-2.4790077209472656, 9.188891410827637, "Power Conditioning Module Redundancy Cold redundant"]
+[-3.0647976398468018, 4.263708591461182, "Spacecraft Data Downlinking Busy downlinking all of the stored data"]
+[-2.258617639541626, 2.9075257778167725, "Infrared Observatory Operating Period 2003 until its decommissioning on Jan. 30, 2020"]
+[-4.546881198883057, -3.1078226566314697, "Exoplanet Size About 8% larger than Neptune"]
+[-4.557520389556885, -3.09134840965271, "Exoplanet Mass Smaller than 58 Earths"]
+[1.460168719291687, -2.45732045173645, "Satellite Orbit Type Highly elliptical, equatorial periapsis"]
+[1.6182608604431152, -1.5806734561920166, "Satellite Coverage Up to 10% of the lunar surface across all latitudes"]
+[-1.7077605724334717, 5.354097843170166, "Mission Control Center Unknown Unknown"]
+[-9.8930082321167, 5.848508834838867, "Rescue Coordination Center Unknown Unknown"]
+[-9.982575416564941, 5.8256611824035645, "Search and Rescue Point of Contact Unknown Unknown"]
+[-4.481427192687988, 8.27452278137207, "Local User Terminals Unknown Unknown"]
+[-9.95689868927002, 5.853309631347656, "Geostationary Search and Rescue System Unknown Unknown"]
+[-0.7717483639717102, 11.638972282409668, "Optical Event Detector Observation Coverage Most of the western hemisphere, including the Atlantic and Eastern Pacific tropical basins"]
+[-0.7569932341575623, 11.655428886413574, "Optical Event Detector Measurement Changes in cloud top radiance produced by lightning"]
+[-0.7617194652557373, 11.635972023010254, "Optical Event Detector Ability Detect not only flash location but average flash area and total optical energy"]
+[5.140745162963867, -4.136552810668945, "Satellite Launch Date December 2026"]
+[1.4766850471496582, -2.457155227661133, "Satellite Orbit Type Halo orbit around L2"]
+[0.6047847867012024, -1.4380502700805664, "Satellite Orbit Distance 1.5 million km beyond Earth"]
+[-7.3403425216674805, 6.131697177886963, "Camera System Components Cameras made of telescopes, their focal planes, all related electronics and the on-board DPS (Data Processing System)"]
+[-3.220602035522461, 1.7089471817016602, "Satellite Mission Data Release Date 12 June 2019"]
+[-3.145343065261841, 1.7006340026855469, "Satellite Mission Operational Science Phase Duration 5 years"]
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+[-3.0933377742767334, 1.6587910652160645, "Satellite Mission Science Data Collection Nearly continuous"]
+[-3.251957893371582, 1.7654187679290771, "Satellite Mission MWI Switchover Date November 01, 2018"]
+[0.6961971521377563, -1.6016972064971924, "Satellite Perigee 600 km"]
+[0.6981898546218872, -1.5702619552612305, "Satellite Apogee 60,530 km"]
+[0.6650089025497437, -1.4057846069335938, "Satellite Semi-major axis 36943 km"]
+[0.9729189872741699, -2.228053569793701, "Satellite Eccentricity 0.8111"]
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+[0.8115944862365723, -2.1532421112060547, "Satellite RAAN 84\u00ba"]
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+[4.156237602233887, -2.8245127201080322, "Satellite Orbital period 19 hr 38 minutes"]
+[0.6864832043647766, -1.4185162782669067, "Satellite Distance between spacecraft About 150 m"]
+[1.1804224252700806, -1.5307973623275757, "Satellite Accuracy of positioning Around a few mm"]
+[2.8466179370880127, -1.2063812017440796, "Satellite Purpose Technology verification"]
+[2.8510096073150635, -1.1273610591888428, "Satellite Purpose Technology verification"]
+[2.271740198135376, -1.483146071434021, "Satellite Detection Method Inter-spacecraft laser interferometry"]
+[-5.187158107757568, 7.780805587768555, "Communication Bus Data Rates 10-100 Mbit/s"]
+[-1.8843648433685303, 8.43136978149414, "Application Specific Integrated Circuit Manufacturer BAE (British AeroSpace)"]
+[0.6799018979072571, -4.121784687042236, "Satellite Launch Mass 2778 kg"]
+[0.9972577691078186, -4.328452110290527, "Satellite Payload Mass 1200 kg"]
+[-6.719032287597656, 9.991684913635254, "Antenna Type Large deployable"]
+[-2.586947441101074, 9.665393829345703, "Power Source Type Deployable sun-tracking"]
+[6.271003723144531, 7.471786975860596, "Satellite Component Shape Rectangular"]
+[7.2710862159729, 12.463574409484863, "Satellite Instrument Application Aerosol detection and visibility estimation"]
+[7.2189040184021, 12.374011039733887, "Satellite Instrument Application Determining vegetation amount, aerosols and ocean/land studies"]
+[7.241133689880371, 12.460039138793945, "Satellite Instrument Application Daytime sensitivity to very thin cirrus"]
+[7.174908638000488, 12.540574073791504, "Satellite Instrument Application Detection of volcanic cloud with sulfuric acid aerosols, thin cirrus, determination of cloud microphysical properties"]
+[7.276031494140625, 12.433849334716797, "Satellite Instrument Application Determination of microphysical properties of clouds, accurate determination of cloud particle size"]
+[-1.7440887689590454, 8.809404373168945, "Controller Robustness Requirements All significant sensor and actuator errors, CSC uncertainties, OSC uncertain/time varying orbital parameters"]
+[-1.7616480588912964, 8.888103485107422, "Linear Time-Invariant Multiple-Input Multiple-Output Controller Design Method Optimization problem aimed to ensure the CL robustness to complex-valued model uncertainty, as well as uncertain parameters"]
+[-1.859322190284729, 8.030770301818848, "System Model Framework LFT (Linear Fractional Transformation)"]
+[-0.19804847240447998, 14.118997573852539, "Electric Field Measurement Instrument Frequency Range Few kHz up to 37 MHz"]
+[0.00888163223862648, 13.999771118164062, "Electric Field Measurement Instrument Scientific Goals Identification of possible wave signatures associated with transient luminous phenomena during storms, Characterization of lightning flashes from their HF electromagnetic signatures, Identification of possible HF electromagnetic or/and electrostatic signatures of precipitated and accelerated particles, Determination of characteristic frequencies of the medium using natural waves properties, Global mapping of the natural and artificial waves in the HF frequency range"]
+[5.367916584014893, -4.531182765960693, "Satellite Launch Date April 3, 2012"]
+[3.3261332511901855, 0.4587502181529999, "Satellite Program URL http://www.nsmc.cma.gov.cn/newsite/NSMC_EN/Channels/100099.html"]
+[5.195047378540039, -4.031193256378174, "Satellite Mission Start Year 1987"]
+[2.966655969619751, -1.545607089996338, "Satellite Predecessor Missions GEOS-3, SEASAT, GEOSAT"]
+[-3.0982563495635986, 4.2983269691467285, "Spacecraft Mission Type Non-EO"]
+[-3.115245819091797, 4.2880048751831055, "Spacecraft Agency UK (Dstl)"]
+[-3.5663809776306152, 4.383336544036865, "Spacecraft Launch Date 17 June 1994"]
+[-3.4958603382110596, 4.329371452331543, "Spacecraft End of Life Date 2001"]
+[-3.0587007999420166, 4.2138285636901855, "Spacecraft Prime Objective Provide opportunities for the evaluation of several new technologies in-orbit"]
+[1.3385071754455566, 10.547508239746094, "Imaging System Swath Width 15 km"]
+[1.3689794540405273, 10.546998977661133, "Imaging System Focal Length 8.6 m"]
+[1.3657156229019165, 10.546348571777344, "Imaging System Ground Sample Distance 0.7 m for the panchromatic band at nadir, and 2.8 m for multispectral bands at nadir"]
+[1.3701976537704468, 10.548781394958496, "Imaging System Signal-to-Noise Ratio > 100"]
+[1.3582196235656738, 10.534581184387207, "Imaging System Spatial Resolution 0.7 m"]
+[0.5426812171936035, -1.479130744934082, "Satellite Orbit Altitude 685 km"]
+[0.6894299387931824, -2.3054027557373047, "Satellite Orbit Inclination 98.1\u00b0"]
+[3.839827537536621, -3.1577088832855225, "Satellite LST 1050 hours"]
+[4.13871955871582, -2.8295319080352783, "Satellite Orbit Period 98.5 minutes"]
+[4.145719051361084, -2.451340675354004, "Satellite Repeat Cycle 28 days"]
+[-0.8916949033737183, 12.990460395812988, "Spectral Irradiance Monitor Device Type Constant-deviation monochromator"]
+[-0.9193190932273865, 13.037891387939453, "Spectral Irradiance Monitor Focal Plane Detectors Three separate photodiode detectors for rapid scan solar measurements and an Electrical Substitution Radiometer (ESR) for long-term SSI calibration maintenance"]
+[2.74454665184021, 13.675848007202148, "Optical Encoder Mechanism Control Prism incidence angle to ~0.5 arc-second rotational resolution"]
+[4.6789140701293945, -2.579568862915039, "Satellite Mission Duration Five years"]
+[5.15069055557251, -4.115954875946045, "Satellite Launch-readiness Date February 2023"]
+[3.1902408599853516, 13.995094299316406, "Laser Ranging Instrument Operation Successful"]
+[5.279320240020752, -4.427916526794434, "Satellite Launch Date May 22"]
+[4.374973773956299, -2.6569671630859375, "Satellite In-Orbit Checkout Period 85 days"]
+[-0.6298869848251343, 15.35727310180664, "VIS/IR Radiometer/Imaging Spectrometer Number of Channels 36"]
+[-0.6172106862068176, 15.379569053649902, "VIS/IR Radiometer/Imaging Spectrometer Scan Mirror Rotation Frequency 16.7 Hz"]
+[-0.7201954126358032, 15.335142135620117, "VIS/IR Radiometer/Imaging Spectrometer Scan Mirror Tilt \u00b120\u00ba from nadir"]
+[-0.5607033371925354, 15.393146514892578, "VIS/IR Radiometer/Imaging Spectrometer Number of VNIR Focal Planes 2"]
+[-0.6956746578216553, 15.339261054992676, "VIS/IR Radiometer/Imaging Spectrometer Number of SWIR Focal Planes 2"]
+[-0.6788436770439148, 15.347990989685059, "VIS/IR Radiometer/Imaging Spectrometer Number of MWIR/TIR Focal Planes 1"]
+[-0.6835779547691345, 15.366774559020996, "VIS/IR Radiometer/Imaging Spectrometer VNIR Detector Material Si"]
+[-0.6704636812210083, 15.37983226776123, "VIS/IR Radiometer/Imaging Spectrometer SWIR Detector Material InGaAs"]
+[-0.6762894988059998, 15.338576316833496, "VIS/IR Radiometer/Imaging Spectrometer MWIR/TIR Detector Material CMT"]
+[-2.4549922943115234, 13.151769638061523, "Hyperspectral Imager Usable Bands 137"]
+[-2.4537320137023926, 13.18005657196045, "Hyperspectral Imager Data Storage 134 MByte"]
+[-2.448838949203491, 13.188565254211426, "Hyperspectral Imager Data Transfer Time 6-30 s"]
+[-0.6932835578918457, 12.289984703063965, "Proton Monitor Intercomparison In-orbit results"]
+[0.5796880722045898, 12.026191711425781, "Sensor Testing For satellite applications"]
+[1.4889988899230957, 21.199838638305664, "Instrument Mass 137 kg"]
+[1.6288477182388306, 23.21164894104004, "Instrument Power Consumption (Daytime) 350 W"]
+[1.621732234954834, 23.221994400024414, "Instrument Power Consumption (Nighttime) 220 W"]
+[2.545559883117676, 22.695035934448242, "Instrument Observation Time Day time"]
+[0.2382964789867401, 13.79179859161377, "Calibration Model Purpose Establishes a mathematical model that describes the relationship between the position of the CCRR and the position of the return beam on the sensor"]
+[-2.233046293258667, 11.058466911315918, "Image Processing Algorithm Function Determines where the center of the beam on the lateral detector is"]
+[-2.3746511936187744, 11.181540489196777, "Image Processing Tool Function Applied to the detector image to simulate a circularly symmetric FOV"]
+[2.682648181915283, 12.254382133483887, "Beam Shape Reference Function Used to determine the quality of the laser beam and monitor potential degradation of the beam shape over the mission lifetime"]
+[3.4574437141418457, 10.623196601867676, "Traveling Wave Tube Amplifier Component Type Amplifier"]
+[3.4784982204437256, 10.55704402923584, "Driving Amplifier Component Type Amplifier"]
+[-1.5181353092193604, 8.516593933105469, "Input Matrix Component Type Matrix"]
+[-1.547120451927185, 8.474566459655762, "Output Matrix Component Type Matrix"]
+[-1.5132097005844116, 8.74942684173584, "Waveguide switches Component Type Switch"]
+[-0.9986186623573303, 8.031710624694824, "Fire Product Meeting Date July 2014"]
+[5.019608020782471, -4.47469425201416, "Satellite Operational Acceptance Date Sept. 16, 2014"]
+[-2.227522373199463, 7.098343849182129, "Global Gridded Products Publication Year 2010"]
+[-6.627043724060059, 9.93331241607666, "Antenna System Control Subsystem Distributed embedded control subsystem"]
+[-1.9159183502197266, 8.802916526794434, "Tile Control Unit Quantity 12"]
+[-5.029139041900635, 8.657271385192871, "Transmit Receive Controller Quantity 288"]
+[-5.636482238769531, 15.879745483398438, "Quicklook Processor/Near Real-time SAR Processor Device Type cPCI computer system, and a COTS-based DSP (Digital Signal Processor)"]
+[-8.623371124267578, 13.817194938659668, "Parameter Spatial Resolution (km) 25"]
+[-8.407820701599121, 13.763578414916992, "Parameter Range of Values 3 - 25"]
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+[-8.521087646484375, 13.684586524963379, "Parameter Absolute Accuracy \u00b1 2 m/s"]
+[-8.593510627746582, 13.77950382232666, "Parameter Spatial Resolution (km) 25"]
+[-8.470658302307129, 13.70453929901123, "Parameter Range of Values 0 - 100"]
+[-8.647074699401855, 13.505914688110352, "Parameter Quantization Levels 1"]
+[-8.569945335388184, 13.710987091064453, "Parameter Absolute Accuracy \u00b1 12%"]
+[-8.619457244873047, 13.80518627166748, "Parameter Spatial Resolution (km) 25"]
+[-8.470588684082031, 13.704553604125977, "Parameter Range of Values 0 - 100"]
+[-8.614641189575195, 13.53857707977295, "Parameter Quantization Levels 1"]
+[-8.494853973388672, 13.717336654663086, "Parameter Absolute Accuracy \u00b1 12.5 km"]
+[-8.600363731384277, 13.794523239135742, "Parameter Spatial Resolution (km) 25"]
+[-8.456543922424316, 13.719977378845215, "Parameter Range of Values 0 - 25"]
+[-8.583511352539062, 13.567858695983887, "Parameter Quantization Levels 0,5,10,15,20, \u226525"]
+[-8.54224967956543, 13.705470085144043, "Parameter Absolute Accuracy \u00b1 5 mm/hr"]
+[-8.60049057006836, 13.787656784057617, "Parameter Spatial Resolution (km) 25"]
+[-8.45750904083252, 13.709156036376953, "Parameter Range of Values 0 - 1"]
+[-8.568830490112305, 13.595250129699707, "Parameter Quantization Levels 0.05"]
+[-8.503937721252441, 13.704440116882324, "Parameter Absolute Accuracy \u00b1 0.1 kg/m 2"]
+[-8.60354995727539, 13.813796997070312, "Parameter Spatial Resolution (km) 25"]
+[-8.479132652282715, 13.704413414001465, "Parameter Range of Values 0 - 80"]
+[-8.607604026794434, 13.54527473449707, "Parameter Quantization Levels 0.10"]
+[-8.525153160095215, 13.696576118469238, "Parameter Absolute Accuracy \u00b1 2.0 kg/m 2"]
+[-8.60427474975586, 13.807382583618164, "Parameter Spatial Resolution (km) 25"]
+[-8.45857048034668, 13.715751647949219, "Parameter Range of Values 0 - 25"]
+[-8.5679292678833, 13.581533432006836, "Parameter Quantization Levels 0,5,10,15,20,\u226525"]
+[-8.52756404876709, 13.692159652709961, "Parameter Absolute Accuracy \u00b1 5 mm/hr"]
+[-8.622917175292969, 13.814449310302734, "Parameter Spatial Resolution (km) 50"]
+[-8.472332954406738, 13.717023849487305, "Parameter Range of Values 0 - 60%"]
+[-8.627875328063965, 13.525664329528809, "Parameter Quantization Levels 1"]
+[-8.602459907531738, 13.791807174682617, "Parameter Spatial Resolution (km) 25"]
+[-8.450039863586426, 13.685663223266602, "Parameter Range of Values 180 - 340 K"]
+[-8.629693984985352, 13.52413272857666, "Parameter Quantization Levels 1"]
+[-8.602606773376465, 13.792073249816895, "Parameter Spatial Resolution (km) 25"]
+[-8.453225135803223, 13.731759071350098, "Parameter Range of Values 0 - 50 cm"]
+[-8.622398376464844, 13.531891822814941, "Parameter Quantization Levels 1"]
+[-8.534682273864746, 13.68187427520752, "Parameter Absolute Accuracy \u00b1 3 cm"]
+[-8.602625846862793, 13.791868209838867, "Parameter Spatial Resolution (km) 25"]
+[-8.485709190368652, 13.675687789916992, "Parameter Range of Values 12 types"]
+[-8.641544342041016, 13.83117389678955, "Parameter Spatial Resolution (km) 25"]
+[-8.479832649230957, 13.70290756225586, "Parameter Range of Values 0 - 100%"]
+[-8.636224746704102, 13.518288612365723, "Parameter Quantization Levels 1"]
+[-8.506765365600586, 13.701897621154785, "Parameter Absolute Accuracy \u00b1 20%"]
+[-7.492374420166016, 5.973535537719727, "Panchromatic Camera Spectral Range 450-900 nm"]
+[-7.499393939971924, 5.9579620361328125, "Panchromatic Camera Spatial Resolution 200-300 m"]
+[-7.490256309509277, 5.973028182983398, "Panchromatic Camera Swath \u00b1 700 km"]
+[-3.8549506664276123, 6.912723541259766, "Data Collection System Uplink Frequency 401.55 MHz"]
+[-3.0732226371765137, 4.313456058502197, "Spacecraft Prime Contractor Airbus"]
+[-3.8595378398895264, 3.717270851135254, "Rover Designed and Built by Airbus"]
+[-0.9566674828529358, 8.156042098999023, "Manipulating Arm Purpose Transfer the samples from the SFR to the Mars Ascent Vehicle (MAV)"]
+[6.419617176055908, 7.328276634216309, "Satellite Component Field of View (FOV) Unobstructed"]
+[6.416355609893799, 7.329948902130127, "Satellite Component Beam Pointing Direction Not specified"]
+[3.7270336151123047, 17.701515197753906, "Payload Component Data Transfer LCT to modulators through the DPU (Data Processing Unit)"]
+[-1.147367000579834, 7.854968547821045, "Device Signal Generation Generate the corresponding RF (Radio Frequency) signal"]
+[2.705965042114258, -3.240938663482666, "Satellite Communication System Link Availability Always available"]
+[2.720883369445801, -3.255866050720215, "Satellite Communication System Link Availability Immediately when they need it"]
+[4.050465106964111, 13.900229454040527, "Laser Altimeter System Mission Lifetime 2018 to 2022"]
+[-3.1474759578704834, 1.777496337890625, "Atmospheric Mission Operation Period 2018 to 2022"]
+[-3.122131586074829, 1.8081917762756348, "Atmospheric Mission Operation Period 2018 to 2022"]
+[-3.1675896644592285, 1.7718549966812134, "Atmospheric Mission License to Operate Through February 2018, perhaps longer"]
+[-2.102102041244507, 11.454808235168457, "Cloud-Aerosol Transport System License to Operate Through February 2018, perhaps longer"]
+[-4.936044216156006, 9.770379066467285, "Receiver Frequency 1 2036.25 MHz"]
+[-4.944536209106445, 9.77296257019043, "Receiver Frequency 2 401.25 MHz"]
+[-4.945864677429199, 9.780136108398438, "Receiver Precision <5 cm"]
+[-4.9441375732421875, 9.779594421386719, "Receiver Function Measure Doppler shift"]
+[-2.003901720046997, 8.069941520690918, "System Programmable Yes"]
+[-1.9350554943084717, 8.099798202514648, "System Recovery Actions Reconfigurations or mode change"]
+[-1.9408760070800781, 8.108514785766602, "System Telemetry Information Reconfiguration flags, current configuration flags, failures reported through dedicated event packages"]
+[-1.926308274269104, 8.125017166137695, "System Design Verification Standalone or integrated GNC/FDIR test environments"]
+[-13.83069133758545, -2.253618001937866, "X-ray Telescope Observation Target Galaxy Clusters, Active Galactic Nuclei, X-ray Sources, Double Stars, Supernovae, Neutron Stars"]
+[-13.86299991607666, -2.2182655334472656, "X-ray Telescope Observation Plan Discover many X-ray sources, including double stars and the remains of stellar explosions (supernovae). Rare objects such as isolated neutron stars"]
+[-2.1461169719696045, 2.908831834793091, "Space Observatory Launch Date 21 June"]
+[-13.890400886535645, -2.2550806999206543, "X-ray Telescope Observation Point L2"]
+[1.3866230249404907, 5.395112037658691, "Spacecraft Bus Weight 350 kg"]
+[2.2969040870666504, -2.5740270614624023, "Satellite Budget $88 million"]
+[5.10813045501709, -3.9596357345581055, "Satellite Launch Date Mid-2022"]
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+[2.2791433334350586, -1.9510623216629028, "Satellite Ground Control Center Location New Zealand"]
+[2.2111093997955322, -2.5736711025238037, "Satellite Ground Control Center Budget $16 million"]
+[2.768115758895874, -1.7869666814804077, "Satellite Payload Provider Ball Aerospace"]
+[3.0583066940307617, -2.2616384029388428, "Satellite Launch Provider Not yet been selected"]
+[2.560244083404541, -2.2186219692230225, "Satellite Ground Communications Commercial ground communications companies"]
+[-5.269341945648193, 7.950196743011475, "Communication System Downlink Frequency X-band"]
+[-5.325530052185059, 7.982245445251465, "Communication System Uplink Frequency S-band"]
+[-6.676231861114502, 9.944600105285645, "Antennas Quantity Two"]
+[-5.2669525146484375, 7.8134379386901855, "Communication System Modulation Scheme Digital QPSK"]
+[-5.236423492431641, 7.84648323059082, "Communication System Encoding Scheme Concatenated external Reed Solomon (255,223) encoder and an internal convolutional (7,1/2) encoder with an interleaving depth of 5"]
+[-5.290133476257324, 7.945635795593262, "Communication System TX Power Likely need to be increased to close the link at apogee"]
+[-1.495348572731018, 11.370844841003418, "Lidar Sensor Data Accuracy Meter-level"]
+[-1.5956621170043945, 11.277607917785645, "Lidar Sensor Bandwidth Up to 250 MHz"]
+[-1.6235394477844238, 11.266508102416992, "Lidar Sensor Analysis Resolution ~ 1.5 m (vertically) within each 100 m diameter footprint"]
+[-1.591795802116394, 11.28442096710205, "Lidar Sensor Observation Duration Over 80 hours"]
+[2.3239808082580566, -1.7982994318008423, "Satellite Archive Location ASF (Alaska Satellite Facility)"]
+[2.5622012615203857, -2.6606476306915283, "Satellite Archive Size Exceeds 1.5 PB (1015 Byte)"]
+[3.1082839965820312, -0.49276068806648254, "Satellite Sensor Complement Active and passive instruments"]
+[2.8245460987091064, -1.7243430614471436, "Satellite Operation All sensors operated at the same time, over the same region of the ocean"]
+[2.5806210041046143, -3.9298136234283447, "Satellite URL http://www.uzay.tubitak.gov.tr/tubitakUzay/en/newsArchive/gk-2.php"]
+[2.579998731613159, -3.912095546722412, "Satellite URL https://iafastro.directory/iac/proceedings/IAC-19/IAC"]
+[2.5929300785064697, -3.9433836936950684, "Satellite URL http://blog.gezgin.gov.tr/?p=1898"]
+[-7.393564701080322, 2.8722751140594482, "Cosmic Ray Detector Events Collected 54 billion"]
+[-7.389874458312988, 2.86917781829834, "Cosmic Ray Detector Events Analyzed 41 billion"]
+[-7.39088773727417, 2.8726072311401367, "Cosmic Ray Detector Positron Fraction Energy Range 0.5 to 500 GeV"]
+[-7.397218704223633, 2.8679091930389404, "Cosmic Ray Detector Energy at Which Fraction Starts to Increase 8 GeV"]
+[-7.373175144195557, 2.894524335861206, "Cosmic Ray Detector Identified Electrons and Positrons 10 million"]
+[0.5131663680076599, 9.45017147064209, "Attitude Control and Determination System Attitude Determination Error \u2264 10 \u00b5rad (2\u03c3) per axis"]
+[0.5469281673431396, 9.445352554321289, "Attitude Control and Determination System Control Error \u2264 1200 \u00b5rad (3\u03c3) per axis"]
+[0.5330538153648376, 9.467796325683594, "Attitude Control and Determination System Relative Pointing Error \u2264 0.03 \u00b5rad/1.5 ms (3\u03c3); and \u2264 0.06 \u00b5rad/3.0 ms (3\u03c3)"]
+[2.1372721195220947, -1.7426973581314087, "Satellite IMU and Star Trackers Mounting On the thermally controlled sensor plate on the MSI"]
+[2.159644365310669, -1.604419231414795, "Satellite Star Tracker Noises Consideration By covariance tuning"]
+[-0.5066496133804321, 1.1950219869613647, "Satellite Orbit Altitude 686 km"]
+[-0.5331166982650757, 1.2352513074874878, "Satellite Orbit Inclination 98.13\u00ba"]
+[-5.149676322937012, 7.943800926208496, "Telecommunications Subsystem Downlink Data Rate 9.6 or 38.4 kbit/s"]
+[-5.172690391540527, 7.9058637619018555, "Telecommunications Subsystem Uplink Data Rate 9.6 kbit/s"]
+[-5.0732421875, 7.905747890472412, "Telecommunications Subsystem X-band Downlink Data Rate 30 Mbit/s"]
+[1.6829980611801147, 10.622673034667969, "Image Transmission Units Signal Power 5 W (+37 dBm)"]
+[1.6722667217254639, 10.532145500183105, "Image Transmission Units Modulation QPSK (Quadra-Phase Shift Keying)"]
+[2.1230790615081787, -0.922282338142395, "Satellite Sensor Signal-to-Noise Ratio High"]
+[2.067723512649536, -0.8821817636489868, "Satellite Sensor Image Quality High"]
+[2.8256895542144775, 13.712967872619629, "Optical Device Configuration Corner cube"]
+[2.78800368309021, 13.728255271911621, "Optical Device Mirror Planes Orientation Perpendicular to each other"]
+[2.8110063076019287, 13.70900821685791, "Optical Device Intersection Point Location Outside the mirror device"]
+[2.791487455368042, 13.679201126098633, "Optical Device Round-Trip Path Length Twice the distance between the beam starting point and a plane normal to the beam direction and intersecting the vertex"]
+[2.90725040435791, -1.6188665628433228, "Satellite Mission Objectives Formation flying demonstration, Equipment qualification, Development, design and validation principles for formation flight, Relative dynamics experiments, Guest payload"]
+[3.7548537254333496, 17.733062744140625, "Payload Length About 150 m"]
+[3.7304325103759766, 17.703346252441406, "Payload Type Distributed over the Formation"]
+[1.9721269607543945, -2.2082836627960205, "Satellite Formation Control 6DOF with thrusters"]
+[2.086446762084961, -2.018338918685913, "Satellite Collision Avoidance Realistic demonstration"]
+[2.965731143951416, -1.4550468921661377, "Satellite Mission Nuclear Spectroscopic Telescope Array"]
+[-0.5499401092529297, 3.1067299842834473, "Pulsar Distance from Earth 50 million light years"]
+[-0.6089991927146912, 3.165067434310913, "Pulsar Luminosity 1,000 times more than the maximum thought possible for an accreting neutron star"]
+[-0.6033385396003723, 3.187957286834717, "Pulsar Energy Emission Same amount of energy as our sun does in 3.5 years in one second"]
+[-0.607289731502533, 3.1512277126312256, "Pulsar Distance from Earth About 12 million light-years away"]
+[-0.5948114395141602, 3.1621243953704834, "Pulsar Brightness 10 times less than NGC 5907 ULX"]
+[2.753246784210205, 22.5224666595459, "Instrument Detection Efficiency Unknown"]
+[2.734656572341919, 22.805784225463867, "Instrument Event Detection Thresholds Unknown"]
+[2.3754262924194336, 22.346452713012695, "Instrument Background Albedo 80%"]
+[2.6833016872406006, 22.27845001220703, "Instrument Detection Efficiency Map Shown in Figure 66"]
+[-0.008730722591280937, -1.9916292428970337, "Satellite Operation RMS Absolute Error 1-2 m"]
+[-0.0033228257670998573, -1.9983985424041748, "Satellite Operation Standard Deviation of Error (Along-track) 0.2-0.4 m"]
+[0.023860802873969078, -1.9950159788131714, "Satellite Operation Standard Deviation of Error (Slant-range) 0.1-0.3 m"]
+[-0.9222387075424194, 6.758080959320068, "Process Start Date 2004"]
+[-0.8835609555244446, 6.763854503631592, "Process Focus Coordinating orders for maritime GoC users"]
+[1.853948712348938, -1.3060797452926636, "Satellite Geomagnetic Field Data Capture High-Precision"]
+[-4.510283470153809, 12.110064506530762, "Magnetometer Calibration Unknown"]
+[-0.8151917457580566, 11.61718463897705, "Detector Device Type Deep-depletion, frame-transfer CCD"]
+[-0.8764330148696899, 11.621179580688477, "Detector Array Size 2048 (H) x 2048 (V)"]
+[-0.8794407844543457, 11.672815322875977, "Detector Die Size 32 (W) x 64 (H) mm"]
+[-0.791267454624176, 11.621689796447754, "Detector Pixel Size 15 x 15 \u00b5m"]
+[-0.8341964483261108, 11.578168869018555, "Detector Area 20.4 cm2"]
+[-0.806627631187439, 11.598674774169922, "Detector Output Circuit Single-stage MOSFET"]
+[0.3205224573612213, -4.121973514556885, "Satellite Platform Mass ~100 kg"]
+[0.1303996741771698, -4.046079635620117, "Satellite Platform Envelope Dimensions 0:65 m x 0:65 m x 0:72 m"]
+[0.11634261906147003, -4.042492866516113, "Satellite Platform Downlink, uplink 2 Mbit/s (S-band), 19.2 kbit/s"]
+[0.29597702622413635, -4.109187126159668, "Satellite Platform Payload Mass ~40 kg"]
+[0.16098463535308838, -4.047971725463867, "Satellite Platform Payload Power 8 W"]
+[0.11319530010223389, -4.043597221374512, "Satellite Platform Pointing Knowledge ~2.5\u00ba"]
+[0.10074200481176376, -4.041506290435791, "Satellite Platform \u0394V Up to 6 m/s"]
+[-3.0924630165100098, 1.667043924331665, "Satellite Mission URL http://www.jpl.nasa.gov/news/fact_sheets/genesis.pdf"]
+[-3.2230381965637207, 1.7219491004943848, "Satellite Mission Conference Date March 13-17, 2000"]
+[0.6847506761550903, 9.31084156036377, "Attitude Determination and Control Subsystem Attitude Control Provider BCT XACT"]
+[0.6787480711936951, 9.319397926330566, "Attitude Determination and Control Subsystem Integrated Components Star trackers, IMU, and RWAs"]
+[0.6583191752433777, 9.324010848999023, "Attitude Determination and Control Subsystem Interface Can interface with thrusters"]
+[-1.451574683189392, 7.31805944442749, "Docking Equipment Manufacturer Boeing"]
+[-1.3226814270019531, 6.189510345458984, "Manufacturer Location Santa Barbara, California"]
+[-1.3441736698150635, 6.302525997161865, "Manufacturer Product Canister, frame and solar array blanket"]
+[2.781353712081909, -1.917230486869812, "Satellite Schematic Diagram Not Applicable"]
+[-5.233619689941406, 7.759791374206543, "Communication System Protocol DVB-S2"]
+[-5.265090465545654, 7.882288455963135, "Communication System Type Unknown"]
+[-4.982316493988037, 2.9029128551483154, "Space Telescope Observation Target TOI-4329"]
+[-4.943721294403076, 2.900338649749756, "Space Telescope Monitoring Target Planetary Systems"]
+[-3.098334789276123, 2.4451889991760254, "Mission Purpose Provide much tighter constraints on planet in-spiral"]
+[0.04907849058508873, 7.098791599273682, "Experiment Cloud Top Imaging Resolution Near \u00bc km"]
+[0.13995972275733948, 7.183578014373779, "Experiment Wavelength 8.5 \u00b5m"]
+[0.14270444214344025, 7.184115886688232, "Experiment Detector Array Approximately 80,000 detectors"]
+[3.7895636558532715, -2.6221349239349365, "Satellite Image Capture Frequency Every 30 minutes"]
+[-3.416867733001709, 4.182526588439941, "Comet Estimated Ejected Material About one million kilograms"]
+[-3.4370646476745605, 4.170125484466553, "Comet Potential Crater Size Around 20 meters (about 65 feet) across"]
+[-3.532890796661377, 4.184986591339111, "Comet Dust Trail A field of larger debris that traces the comet\u2019s orbital path as it travels around the sun"]
+[7.298389911651611, 12.425887107849121, "Satellite Instrument Unknown Unknown"]
+[7.225576400756836, 12.37608528137207, "Satellite Instrument URL http://www.aip.de/People/ASchwope/papers/eROSITA_SPIE_2006.pdf"]
+[1.4418343305587769, 10.821954727172852, "Pushbroom Scanner # satellites to collect 106 sqkm/day @ 50 cm GSD 1"]
+[-2.57513427734375, 11.45298957824707, "Push Framer # satellites to collect 106 sqkm/day @ 50 cm GSD 75"]
+[1.4491506814956665, 10.799744606018066, "Pushbroom Scanner Satellite lifetime >10 years"]
+[-2.583599090576172, 11.481436729431152, "Push Framer Satellite lifetime <<5 years"]
+[1.488811731338501, 10.792867660522461, "Pushbroom Scanner Amortized unit cost $100 million"]
+[-2.5765492916107178, 11.437600135803223, "Push Framer Amortized unit cost $5 million"]
+[1.4263566732406616, 10.793431282043457, "Pushbroom Scanner Annualized cost to collect 10 6  km 2 /day < $10 million"]
+[-2.5462045669555664, 11.37153148651123, "Push Framer Annualized cost to collect 10 6  km 2 /day > $75 million"]
+[-1.8344708681106567, 12.15824031829834, "Infrared Camera Application Earth Observation"]
+[-5.886862754821777, 16.000476837158203, "Synthetic Aperture Radar Design Wide swath, high resolution, full polarimetric"]
+[-0.6400312185287476, 9.442152976989746, "Spacecraft Component Diameter 50 mm"]
+[-0.6804514527320862, 9.452200889587402, "Spacecraft Component Size 1.04 Rs"]
+[-0.9959113001823425, 11.297163009643555, "CCD Detector Pixel Size 15 \u00b5m"]
+[2.607933759689331, 14.266045570373535, "Optical Instrument Effective Focal Length 1150 mm"]
+[2.5846564769744873, 14.263731956481934, "Optical Instrument Overall Length 700 mm"]
+[2.8235857486724854, -1.1249622106552124, "Satellite Purpose Demonstrate several technologies critical for the CanX-4/5 formation flying mission"]
+[2.023073434829712, -2.392051935195923, "Satellite Propulsion System Custom cold-gas propulsion system"]
+[1.8208510875701904, -2.183427572250366, "Satellite Reaction Wheel 30 mNms nanosatellite reaction wheel"]
+[1.5919219255447388, -2.136126756668091, "Satellite Attitude Control System Three-axis stabilised momentum-bias attitude control system"]
+[2.4395391941070557, -1.7150908708572388, "Satellite GPS Receiver Commercially available"]
+[7.294629096984863, 12.422651290893555, "Satellite Instrument Swath Coverage 88\u00ba N over the Arctic, and about 79.6\u00ba S over the Antarctic"]
+[7.246267795562744, 12.382929801940918, "Satellite Instrument Viewing Angle Away from the sun"]
+[-9.940978050231934, 5.8702616691589355, "Search and Rescue System Status and Developments Meeting Date 25 \u2013 29 January 2015"]
+[-0.8866977095603943, 0.201324462890625, "Satellite System First Space Test Date Jan. 23, 2013"]
+[-0.9634547829627991, 6.394818305969238, "Publication Issue 21 Date Feb. 2009"]
+[-3.334681272506714, 8.511615753173828, "Memory Device Programming Time 700 \u00b5s per 4 kbyte data"]
+[-3.312385082244873, 8.518017768859863, "Memory Device Erase Time 2 ms per block (64 pages)"]
+[-3.2974092960357666, 8.490540504455566, "Memory Device Interface Eight bit interface"]
+[-3.3041155338287354, 8.49853229522705, "Memory Device Maximum Operating Frequency 40 MHz"]
+[2.6005733013153076, -1.5952143669128418, "Satellite Ground-level Changes Data Provider ESA (European Space Agency) Sentinel-1 satellite"]
+[2.582608222961426, -1.2291778326034546, "Satellite Water Loss Data Provider NASA\u2019s Gravity Recovery and Climate Experiment (GRACE) and GRACE-FO satellites"]
+[-0.5759059190750122, 4.974342346191406, "Region Groundwater Pumping Percentage More than 80% in drought years"]
+[0.4580964744091034, 4.523558616638184, "Natural Phenomenon Minimum Extent Below 4.0 million km2 (1.54 million square miles)"]
+[0.47091493010520935, 4.517433166503906, "Natural Phenomenon Lowest 14 Ice Extents All occurred in the past 14 years"]
+[0.47613686323165894, 4.511869430541992, "Natural Phenomenon Regional Variations Inhibit melting in different parts of the Arctic"]
+[-1.6125984191894531, 1.4720063209533691, "Data Relay System Service Types Optical and Ka-band"]
+[2.6670596599578857, 13.813875198364258, "Optical Intersatellite Links Type Bi-directional"]
+[2.7418580055236816, -2.8290233612060547, "Ka-band Intersatellite Links Type Bi-directional"]
+[-5.447601795196533, 7.068972110748291, "Return link Direction From LEO user to GEO"]
+[-5.438029766082764, 7.03597354888916, "Forward link Direction From GEO to the LEO user"]
+[-0.9568620920181274, 9.822867393493652, "Rocket Reusability Fully and rapidly reusable"]
+[-0.9495370388031006, 9.829215049743652, "Rocket Launches Planned At least a dozen"]
+[-0.9585650563240051, 9.822096824645996, "Rocket First Stage Landing Land safely on Earth to be refueled and fly again"]
+[-0.9739773273468018, 9.818375587463379, "Rocket Boosters First Stage Recovery Via an unprecedented precision guided landing on an ocean-going \"drone\""]
+[2.976264715194702, -1.4178482294082642, "Satellite Mission Overview Lightning Study"]
+[5.30918025970459, -4.487865447998047, "Satellite Launch Date March 1, 2011"]
+[2.5806028842926025, -3.9399054050445557, "Satellite URL http://www.cnes.fr"]
+[-5.227618217468262, 7.677398681640625, "Communication System Data Download Capacity Few hundred Mbit per day"]
+[-5.53830623626709, 9.511255264282227, "Frequency Band Telemetry Bit Rates Hundred of kbit/s"]
+[-5.534709453582764, 9.514710426330566, "Frequency Band Telemetry Bit Rates Few Mbit/s"]
+[-5.493743896484375, 9.527750968933105, "Frequency Band Telemetry Possible for telemetry"]
+[-5.545586109161377, 9.510396957397461, "Frequency Band Spectral Recommended Occupation Bandwidth 6 MHz maximum"]
+[-5.534075736999512, 9.504561424255371, "Frequency Band TC (TeleCommanding) capacity Increase"]
+[2.358393430709839, -1.7956374883651733, "Satellite Device Type 3U CubeSat"]
+[2.2186038494110107, -2.5386970043182373, "Satellite Spectrometer Channels 12"]
+[2.8144302368164062, -2.4542760848999023, "Satellite Spectrometer Frequency Near 90 and 206 GHz"]
+[2.7993247509002686, -2.475301742553711, "Satellite Spectrometer Frequency Near 118 GHz"]
+[2.744375228881836, -2.406751871109009, "Satellite Spectrometer Frequency Near 183 GHz"]
+[2.6722214221954346, -1.189155101776123, "Satellite Target Applications Measurement of surface deformation of vegetated terrain, soil moisture, land cover classification, crop type discrimination, Polar ice sheets and ice caps monitoring, sea-ice conditions monitoring, European maritime situational awareness"]
+[2.6189050674438477, -1.7235676050186157, "Satellite SAR Interferometry Capability Yes"]
+[2.8858799934387207, -1.519165277481079, "Satellite Control Application Software Developed and delivered by SPACEBEL"]
+[-5.251813888549805, 7.830821514129639, "Communication System Channel Speed 9600 bit/s"]
+[-4.760097980499268, 9.2628173828125, "Transmitter Frequency 2.4 GHz"]
+[-4.226674556732178, 7.353644371032715, "Data Rates Options 24, 48, or 96 kbit/s"]
+[-3.3835673332214355, 8.551715850830078, "Memory Capacity 4 MByte"]
+[-1.0776846408843994, 7.986210823059082, "Deorbiting Mechanism Principle Cross-sectional drag increase of the spacecraft by unfolding a triangular sail on two deployed booms"]
+[2.161459445953369, -1.442798137664795, "Satellite Main Instrument Coronagraph"]
+[2.3670692443847656, -1.4973903894424438, "Satellite Carried Device Occulting Disk"]
+[-1.2133550643920898, 6.962286472320557, "Assembly Manufacturing Location SENER Aeroespacial facility in Bilbao (Spain)"]
+[0.24670977890491486, 11.550681114196777, "Sensor System Purpose Allow one satellite to lock onto the other"]
+[2.585341215133667, -1.718428134918213, "Satellite Polarimetric Data Unknown"]
+[2.051405668258667, -1.1101019382476807, "Satellite Radar Remote Sensing Contribution to radar remote sensing"]
+[3.091928482055664, -1.6291016340255737, "Satellite Agency ISRO"]
+[2.523825168609619, -1.5173883438110352, "Satellite Event Floods in Indonesia, February 2015"]
+[3.22113037109375, 2.3855884075164795, "Satellite Subsystem Margins of Safety 8.5 g\u2019s in two directions simultaneously, 12 g\u2019s in each of three directions individually"]
+[6.3335394859313965, 7.40931510925293, "Satellite Component Ultimate Factor of Safety 1.4"]
+[6.328141212463379, 7.4046101570129395, "Satellite Component Safety Factor 2.0"]
+[3.2208642959594727, 2.3778021335601807, "Satellite Subsystem Sine Burst Levels Up to 14.4 g"]
+[2.2230050563812256, 22.19733238220215, "Instrument Measurement Total Solar Irradiance"]
+[2.2412824630737305, 22.231443405151367, "Instrument Measurement Total Solar Irradiance"]
+[0.15499503910541534, 7.19136381149292, "Experiment Sponsor NASA/GRC"]
+[0.18096740543842316, 7.227071285247803, "Experiment Developer NASA/GRC"]
+[-5.440818786621094, 9.066810607910156, "SDR (Software Defined Radio) Frequency Range UHF to S-band"]
+[-5.398451805114746, 9.022668838500977, "SDR (Software Defined Radio) Function Receives and decodes GPS signals"]
+[-5.35783576965332, 9.024120330810547, "SDR (Software Defined Radio) Function Supports precise ranging measurements"]
+[-5.427274703979492, 9.039340019226074, "SDR (Software Defined Radio) Compatibility CubeSat standard compatible version"]
+[-5.423538684844971, 9.04480266571045, "SDR (Software Defined Radio) Frequency Range UHF to S-band"]
+[2.88655161857605, -1.0305883884429932, "Satellite Purpose Vertical structure and distribution of precipitation"]
+[2.89113187789917, -1.0391249656677246, "Satellite Purpose Soil moisture and ocean salinity"]
+[2.9095306396484375, -1.014718770980835, "Satellite Purpose Soil moisture and ocean salinity"]
+[2.9434804916381836, -1.0193170309066772, "Satellite Purpose Soil moisture and ocean salinity"]
+[2.897376775741577, -0.9791076183319092, "Satellite Purpose Ocean surface evaporation, snow, ice and soil moisture"]
+[-1.3582745790481567, 6.901857376098633, "Model Nature Bursty or pulsed"]
+[-1.3640965223312378, 6.918834686279297, "Model Nature Quasi-periodic"]
+[-1.3604053258895874, 6.927393436431885, "Model Nature Ground signatures of bursty reconnection turning on and off at the magnetopause"]
+[0.6402695178985596, 12.148001670837402, "Sensor Sensor Quantity 8"]
+[0.5246161818504333, 12.191293716430664, "Sensor Sensor #1 Radius 42 mm"]
+[0.4897640347480774, 12.233479499816895, "Sensor Sensor #2 Radius 52 mm"]
+[0.6367623805999756, 12.0211820602417, "Sensor PCB Technology Flex-rigid"]
+[0.7333178520202637, 11.999058723449707, "Sensor Mounting Set of screws and spacers"]
+[-0.9509027600288391, 9.816725730895996, "Rocket Performance 2.3 t in a reference 700 km polar orbit"]
+[-0.9612525105476379, 9.802844047546387, "Rocket Capability 1.5 t"]
+[3.72426176071167, 17.696809768676758, "Payload Affiliation Italian space agency ASI"]
+[3.7409353256225586, 17.710153579711914, "Payload Quantity 6"]
+[-3.557655096054077, 4.385743618011475, "Spacecraft Launch Date November 6, 2014"]
+[-2.9756674766540527, 4.1674346923828125, "Spacecraft Orbit Altitude 504 km"]
+[-2.981931686401367, 4.156230926513672, "Spacecraft Orbit Inclination 97.4\u00ba"]
+[-3.2615342140197754, 4.277604579925537, "Spacecraft Local Time on Descending Node 11:00 hours"]
+[16.777816772460938, 6.918093681335449, "Microsatellite Mass 50 kg"]
+[16.773405075073242, 6.913453102111816, "Microsatellite Mass 60 kg"]
+[16.810213088989258, 6.884547710418701, "Microsatellite Mass 49 kg"]
+[16.77106475830078, 6.924232006072998, "Microsatellite Mass 49 kg"]
+[-5.885594367980957, 16.00266456604004, "L-band synthetic aperture radar Quantity 1"]
+[-6.7909016609191895, 10.04649829864502, "Antenna Diameter 79 cm"]
+[1.7357110977172852, 22.05060577392578, "Instrument Footprint 35 km"]
+[2.081568717956543, 22.37894058227539, "Instrument Accuracy of Water Vapor Measurement 0.2 gm/cm2"]
+[2.0492682456970215, 22.438745498657227, "Instrument Range of Water Vapor Measurement 0.2 to 6.0 gm/cm2"]
+[1.901727557182312, 22.281845092773438, "Instrument Uncertainty of Altimeter Height Data Corrections 1.2 cm"]
+[-13.85954475402832, -2.168433666229248, "X-ray Telescope Energy Range Broad"]
+[-13.898499488830566, -2.2445104122161865, "X-ray Telescope Penetration Depth Deeper into the region around the black hole"]
+[-1.1723241806030273, 3.0658931732177734, "Celestial Object Spin Rate Can be determined conclusively"]
+[-1.1611430644989014, 3.052549123764038, "Celestial Object Accretion Disk Formation Formed as their gravity pulls matter inward"]
+[5.1424078941345215, -4.477731227874756, "Satellite Reentry Date Nov. 12, 2002"]
+[3.1301918029785156, -1.87538480758667, "Satellite Mission Success 100%"]
+[0.5893276929855347, 12.065999984741211, "Sensor First Data Transmission Date Aug. 1, 2000"]
+[0.6883271336555481, 12.003252983093262, "Sensor Launch Date July 19, 2000"]
+[1.7964612245559692, 22.09479331970215, "Instrument Spatial Resolution 15-50 km"]
+[1.7904103994369507, 22.083032608032227, "Instrument Spatial Resolution 4-50 km"]
+[1.8169020414352417, 22.093461990356445, "Instrument Spatial Resolution 2-5 km"]
+[2.1787939071655273, 22.487607955932617, "Instrument Sensitivity 0.1-0.2 K"]
+[2.128849506378174, 22.57129669189453, "Instrument Sensitivity 0.3-0.5 K"]
+[2.054973840713501, 22.655195236206055, "Instrument Sensitivity 0.5 dB"]
+[1.1252515316009521, -1.3687996864318848, "Satellite Swath Width Over 1000 km"]
+[4.2207207679748535, -2.523195266723633, "Satellite Revisit Time 2-3 days"]
+[0.5332040190696716, -1.463423490524292, "Satellite Orbit Altitude 645 km"]
+[0.9587304592132568, -4.399441242218018, "Satellite Total Mass 1300-1500 kg"]
+[2.7389559745788574, -2.7050063610076904, "Satellite Instantaneous Data Rate Approximately 27 Mbps"]
+[2.5833635330200195, -2.247997999191284, "Satellite Daily Data Volume 291.6GB"]
+[2.7161061763763428, -2.7821106910705566, "Satellite Downlink Data Rate 750 Mbps"]
+[4.026583671569824, -2.7339110374450684, "Satellite Total Data Downlink Time About 52 minutes per day"]
+[-1.6705490350723267, 11.232507705688477, "Lidar Deployment Date April 2012"]
+[-1.702881932258606, 11.25686264038086, "Lidar Scanning Rate 20 Hz"]
+[-1.6706849336624146, 11.22705078125, "Lidar Off-nadir Scanning Angle ~15\u00ba"]
+[-1.6720774173736572, 11.238912582397461, "Lidar Wavelength 532 nm"]
+[-1.6798537969589233, 11.23383617401123, "Lidar PRF (Pulse Repetition Frequency) 5 kHz"]
+[-1.6829109191894531, 11.226110458374023, "Lidar Footprint 1 m"]
+[-1.6900384426116943, 11.184221267700195, "Lidar Scanning Swath Width ~250 m"]
+[-2.7923784255981445, 15.279775619506836, "Microwave Radiometer & Scatterometer Radiometer Type Pushbroom-type polarimetric microwave radiometer in L-band"]
+[-2.783147096633911, 15.347270965576172, "Microwave Radiometer & Scatterometer Scatterometer Type S-band scatterometer"]
+[-2.817671060562134, 15.270350456237793, "Microwave Radiometer & Scatterometer Radiometer Objective Measure the microwave brightness temperatures of the ocean surface"]
+[-2.784278154373169, 15.319499015808105, "Microwave Radiometer & Scatterometer Scatterometer Objective Measure the surface roughness"]
+[2.8132619857788086, 13.742191314697266, "Optical Device Stability Requirement Up to 16 years"]
+[2.7921080589294434, 13.719388961791992, "Optical Device Operation Requirement 24/7 for five years for the initial mission, with a possible six to seven years of extended mission after that"]
+[2.792926788330078, 13.691849708557129, "Optical Device Frequency Stabilization One wavelength and a perfect beam out to 15 decimal places of accuracy"]
+[2.797940254211426, 13.707840919494629, "Optical Device Technology Monolithic laser oscillator technology"]
+[2.2050530910491943, -1.5537288188934326, "Satellite Instrument Synthetic Aperture Radar"]
+[2.2065112590789795, -1.49720299243927, "Satellite Instrument Multibeam Thermal-Infrared Instrument"]
+[2.267916679382324, 22.105764389038086, "Instrument Measurement Height-resolved cloud movements"]
+[2.165956974029541, 22.061981201171875, "Instrument Measurement Sea-surface temperature differences"]
+[-0.8026885390281677, 0.13702528178691864, "Satellite System Communication Technology Laser technology"]
+[5.049124240875244, -4.377595901489258, "Satellite User Commissioning Review Date July 16, 2020"]
+[2.595694065093994, -2.3306832313537598, "Satellite Communication Method Laser communication"]
+[3.184152603149414, -1.776484727859497, "Satellite Manufacturer OHB System"]
+[2.8378214836120605, -1.6318268775939941, "Satellite Laser Terminals Developer Tesat-Spacecom and the DLR German Space Administration"]
+[1.57305908203125, -1.823655605316162, "Satellite Polarimetric Observation Technique Compact (or hybrid) polarimetry"]
+[1.761674404144287, -2.041752576828003, "Satellite Polarimetric Information Not enough compared to that of full-pol."]
+[1.36920166015625, -1.587774634361267, "Satellite Swath of Compact Polarimetry Wider than that of full-pol."]
+[11.875711441040039, 5.2834577560424805, "3U CubeSat Mass ~10 kg"]
+[11.82137393951416, 5.335962295532227, "3U CubeSat Ground Station Montsec Observatory (OAdM)"]
+[11.863348007202148, 5.310343265533447, "3U CubeSat Ground Station Location Sant Esteve de la Sarga, in the Pallars Juss\u00e0"]
+[-1.4469202756881714, 13.368069648742676, "Solar Panels Size 19 meter x 6 meter"]
+[-1.4515451192855835, 13.361364364624023, "Solar Panels Electricity Production More than 120 kW"]
+[-1.4439971446990967, 13.356463432312012, "Solar Panels Power Increase 20 to 30 percent"]
+[-2.115401029586792, 4.314021587371826, "Space Station Power Source Solar Panels"]
+[-2.133676767349243, 4.310880184173584, "Space Station Purpose Conducting experiments and research in microgravity environment"]
+[-13.755717277526855, -2.3659260272979736, "X-ray Astronomy Satellite Launch Date 2018"]
+[-13.839211463928223, -2.2533559799194336, "X-ray Astronomy Satellite URL http://www.mpe.mpg.de/6686210/news-20170120"]
+[-13.812041282653809, -2.2628843784332275, "X-ray Astronomy Satellite URL http://www.mpe.mpg.de/450698/news"]
+[-14.106640815734863, -2.4348304271698, "X-ray Astronomy Satellite URL http://www.mpe.mpg.de/6541082/eROSITA_Bulletin7.pdf"]
+[-13.8095121383667, -2.3306713104248047, "X-ray Astronomy Satellite URL http://www.russianspaceweb.com/spektr-rg-launch-attempt2.html"]
+[-1.597154974937439, 4.109591007232666, "Ground Segment Components CCC (Command and Control Center), Network of S-band satellite tracking stations, TETX (Telemetry Earth Terminal X-band), Communication network, Mission Center, ICARE Data Processing and Management Center"]
+[2.7896292209625244, -2.470137119293213, "Satellite Tracking Stations Frequency 2 GHz"]
+[-0.872498095035553, 5.034330368041992, "Receiving Station Location Toulouse"]
+[-3.332304000854492, 7.243424415588379, "Data Processing and Management Center Location USTL (Universit\u00e9 des Sciences et Techniques de Lille), Lille, France"]
+[1.723818063735962, -1.8509992361068726, "Satellite Model Assembly State In the assembly state"]
+[5.080777645111084, -4.350670337677002, "Satellite Model Availability Date 2009"]
+[5.282472610473633, -4.2611541748046875, "Satellite Launch Date 2010"]
+[-4.370510101318359, 0.20250023901462555, "GPS Receiver Power Supply Voltage 3.3 VDC"]
+[-4.362259864807129, 0.20354677736759186, "GPS Receiver Current About 0.15 A"]
+[-4.36346960067749, 0.19262269139289856, "GPS Receiver Power Consumption About 0.5 W"]
+[-4.358687877655029, 0.1980697363615036, "GPS Receiver Dimensions 41 mm x 71 mm x 13 mm"]
+[-4.365799427032471, 0.19934557378292084, "GPS Receiver Mass About 22 g"]
+[-4.3662943840026855, 0.19473496079444885, "GPS Receiver Sampling Rate 1/60 Hz"]
+[-4.367180824279785, 0.2005152702331543, "GPS Receiver Data Rate Up to 1 Hz"]
+[-0.46158528327941895, 3.6547372341156006, "Planetary System Number of Planets 2"]
+[-2.688161611557007, 11.721294403076172, "Imager Bands 3"]
+[-2.644498348236084, 11.677056312561035, "Imager Image Generation Simultaneous"]
+[-3.0078041553497314, 4.179433345794678, "Spacecraft Orbit GEO (geostationary)"]
+[-2.616689920425415, 11.646161079406738, "Imager Orbital Altitude About 35,786 km"]
+[-2.6888132095336914, 11.698568344116211, "Imager Nominal Position 0o longitude"]
+[0.5092151165008545, 12.281301498413086, "Sensor Wavelength 322 nm"]
+[0.5208198428153992, 12.329564094543457, "Sensor Wavelength 350 nm"]
+[0.48020172119140625, 12.301130294799805, "Sensor Wavelength 603 nm"]
+[0.4463217854499817, 12.293069839477539, "Sensor Wavelength 675 nm"]
+[0.4877728819847107, 12.296090126037598, "Sensor Wavelength 760 nm"]
+[0.4758918881416321, 12.208081245422363, "Sensor Spatial Resolution 0.5 km"]
+[0.4603721797466278, 12.230586051940918, "Sensor Spatial Resolution 0.5 km"]
+[0.4824577867984772, 12.210223197937012, "Sensor Spatial Resolution 0.75 km"]
+[0.4660300314426422, 12.233274459838867, "Sensor Spatial Resolution 0.75 km"]
+[0.4708458483219147, 12.212955474853516, "Sensor Spatial Resolution 0.75 km"]
+[6.245085716247559, 7.495589256286621, "Satellite Component Number of Earth observation satellites More than 16"]
+[6.340521812438965, 7.40234899520874, "Satellite Component Service Tracking, monitoring and control of satellites"]
+[-1.161971926689148, 4.448163032531738, "Ground Station Number 3"]
+[2.567521333694458, -1.7196906805038452, "Satellite Data Processing Location GSFC"]
+[-0.1455133855342865, 13.60288143157959, "Measurement Device Reconnection Duration Hours"]
+[1.9091451168060303, 10.70822811126709, "Imaging Device Reconnection Duration Hours"]
+[2.0469439029693604, -1.3654919862747192, "Satellite Parameter Measurement Movement of water based on variations of Earth\u2019s gravity field"]
+[3.4381778240203857, -2.520583152770996, "Satellite Measurement Frequency Month to month"]
+[2.5302093029022217, -1.2478505373001099, "Satellite Data Integration With data from the original GRACE mission (2002-2017) and with current and historical ground-based observations"]
+[2.0204033851623535, -1.2705274820327759, "Satellite Parameter Measurement State of soil moisture and groundwater"]
+[3.4552581310272217, -2.51582932472229, "Satellite Measurement Frequency Month to month"]
+[2.4363698959350586, -1.1553257703781128, "Satellite Data Integration With other ground-based observations using a numerical model of water and energy processes at the land surface"]
+[-0.8182014226913452, 11.620152473449707, "Detector Rigidity Evaluation Relative Error \u0394R/R"]
+[-0.7857837677001953, 11.671639442443848, "Detector Curvature Determination Error \u0394R/R"]
+[-0.825337290763855, 11.609158515930176, "Detector Lever Arm Length ~ 1 m to ~ 4 m"]
+[-0.8268344402313232, 11.555644035339355, "Detector Rigidity Resolution Unknown"]
+[-3.6301844120025635, 12.744072914123535, "Particle Detector Magnet Type Superconducting"]
+[-3.6363682746887207, 12.759316444396973, "Particle Detector Magnet Type Permanent"]
+[-3.6455771923065186, 12.756938934326172, "Particle Detector Data Collection Time 18 years"]
+[-5.214271545410156, 7.958678722381592, "Communication System Components 1.8-m Main Reflector (MR), four separate feed horns, and calibration targets"]
+[-2.123141288757324, 5.386760711669922, "Deployment System Function Stows the MR and deploys it to the on-orbit configuration"]
+[-0.6888805031776428, 8.361956596374512, "Mechanism Functions Conical scanning, signal transfer and power distribution through internal slip rings"]
+[-1.8137818574905396, 8.559943199157715, "Electronics Subsystem Function Provides the interface to the spacecraft and is responsible for MWI control"]
+[5.268963813781738, -4.068568229675293, "Satellite Launch Date 2016"]
+[5.263087272644043, -4.099532127380371, "Satellite Launch Date 2016"]
+[3.82338285446167, -2.654655694961548, "Satellite Network Revisit Times Few hours or less"]
+[3.1332623958587646, -1.888297200202942, "Satellite Testing Status In the process of final testing and checkout"]
+[3.0765552520751953, -1.8120001554489136, "Satellite Testing Status In the process of final testing and checkout"]
+[-13.52637004852295, -2.0314598083496094, "X-ray Observatory Energy Range 8 to 24 keV"]
+[-13.547430038452148, -2.036699056625366, "X-ray Observatory Energy Range 0.5 to 7 keV"]
+[-0.5982295274734497, 1.299088954925537, "Orbit Synopticity and a mix of sun-synchronous and mid-inclination orbits Requirement"]
+[-0.6015160083770752, 1.300806999206543, "Orbit \u00b150\u00b0 latitude Population distribution"]
+[0.5242399573326111, 12.204062461853027, "Sensor Lens f1.4/85 Zeiss lens"]
+[0.493052214384079, 12.14730167388916, "Sensor Field of View 28.6\u00ba"]
+[0.47408658266067505, 12.263557434082031, "Sensor Image Diameter 43 mm"]
+[0.728176474571228, 12.075169563293457, "Sensor Detector Areas Two"]
+[0.544543445110321, 12.096491813659668, "Sensor Detector Types CMOS detector, smaller CMOS sensor"]
+[0.5875106453895569, 12.117616653442383, "Sensor Science Sensor Integration Times Longer"]
+[5.155104637145996, -4.474526405334473, "Satellite On-Orbit Thermal Analysis Date Oct. 10-13, 2012"]
+[5.172418117523193, -4.479118347167969, "Satellite On-Orbit Experiment Date Oct. 1-5, 2012"]
+[-2.0750837326049805, 5.949620723724365, "Flight Test Date Unknown"]
+[-3.046776294708252, 4.350549697875977, "Spacecraft Purpose Safe, Reliable Human Transport to Deep Space"]
+[-3.541194200515747, 4.373419761657715, "Spacecraft Test Date June 19, 2014"]
+[1.8284571170806885, 22.774564743041992, "Instrument Proton Energy Range Above ~75 MeV"]
+[2.750370502471924, 22.761768341064453, "Instrument Threshold Energy Unknown"]
+[2.5671730041503906, 22.429548263549805, "Instrument Equivalent Shieldings Different for each floor"]
+[2.6819331645965576, 22.28914451599121, "Instrument Shielding Different for each floor at right angles to the sensors"]
+[2.4674861431121826, 22.273591995239258, "Instrument Shielding In first approximation, the same for all the floors in the rest of directions"]
+[-0.8444052934646606, 0.17024774849414825, "Satellite System Integration Objective Integrate separate meteorological programs into a single program"]
+[-0.8409819006919861, 0.15742915868759155, "Satellite System Reporting Structure Tri-agency office reporting through NOAA to an Executive Committee of representatives from DOC, DoD and NASA"]
+[2.5416860580444336, 22.65399932861328, "Instrument Detection Threshold 25"]
+[2.5707502365112305, 23.47527313232422, "Instrument False Event Rate Less than 100 events/sec"]
+[-0.37723076343536377, 3.777636766433716, "Planet Type Sub-Earth"]
+[-0.3529380261898041, 3.8122105598449707, "Planet Transit Period Ultrashort"]
+[2.8404674530029297, 22.062583923339844, "Instrument Goal Provide closely spaced observations of surface wind speed and direction"]
+[2.0428049564361572, 22.41324806213379, "Instrument Wind Speed Accuracy 2 m/s or 10%"]
+[1.925927996635437, 22.266637802124023, "Instrument Wind Speed Range 3-16 m/s"]
+[2.161604642868042, 22.242267608642578, "Instrument Wind Direction Accuracy 20\u00ba"]
+[-4.745473861694336, 9.265207290649414, "Transmitter Bandwidth 320 MHz"]
+[-4.751522541046143, 9.250222206115723, "Transmitter Time-Delay Resolution 3.125 ns"]
+[2.649527072906494, 23.66952133178711, "Instrument Operating Frequency 13.56 GHz"]
+[1.6786490678787231, 23.168054580688477, "Instrument Chirp Signal Peak Power 2 kW"]
+[1.683349609375, 21.95733642578125, "Instrument Swath Width 2.4 to 12 km"]
+[-1.4977201223373413, 16.88490867614746, "Altimeter Uncompressed Pulse Width 3.2 \u00b5s"]
+[-1.50375497341156, 16.899911880493164, "Altimeter Compressed Pulse Width 3.125 ns"]
+[-1.4948192834854126, 16.88397789001465, "Altimeter Height Measurement Precision 10 cm (rms)"]
+[-1.50020432472229, 16.90029525756836, "Altimeter Significant Wave Height Estimate Accuracy 0.5 m or 10%"]
+[-1.5073542594909668, 16.901262283325195, "Altimeter Ocean Backscatter Coefficient Accuracy 1 dB"]
+[-3.0927045345306396, 2.0912601947784424, "Robotic Mission Purpose Pioneer techniques for storing and replenishing cryogenic spacecraft fuel"]
+[-1.477222204208374, 9.516213417053223, "Fuel/Propellant Properties Produces high thrust or acceleration"]
+[-0.768775999546051, 8.696887016296387, "Coolant Properties Keeps spacecraft operational and can prolong their lifespan by years"]
+[-1.939518690109253, 9.452361106872559, "Fuel Source Benefit Minimizes the amount of fuel spacecraft are required to carry from Earth's surface"]
+[-4.2157745361328125, 7.405023097991943, "Data Forwarding Mechanism Function Forward data from the EDRS GEO satellite to the target LEO satellite"]
+[-3.202810764312744, 7.314506530761719, "Data Processing and Control Center Function Process forward tasking data request"]
+[-3.240244150161743, 7.379682540893555, "Data Processing and Control Center Function Stop internal processing if request is deleted"]
+[-3.1987524032592773, 7.388866424560547, "Data Processing and Control Center Function Generate and execute FOP to delete the commands from the on-board time-tag TC buffer"]
+[-2.6640615463256836, 11.664095878601074, "Imager Objectives Hurricane track & intensity forecast"]
+[-2.1529946327209473, 12.651443481445312, "Solar Ultra Violet Imager Objectives Power blackout forecasts due to solar flares"]
+[-13.556763648986816, -2.0068891048431396, "Extreme Ultra Violet and X-ray Irradiance Sensor Objectives Solar flare warnings for communications and navigation"]
+[1.437723159790039, 2.311211109161377, "Geostationary Lightning Mapper Objectives Thunderstorm & tornado warning lead time, Aviation flight route planning"]
+[-2.974127769470215, 4.238838195800781, "Space Environmental In-Situ Suite Objectives Energetic particle forecasts"]
+[-4.526358604431152, 12.091211318969727, "Magnetometer Objectives Not specified"]
+[6.341725826263428, 7.408300876617432, "Satellite Component Offset Angle 42\u00ba"]
+[1.6507331132888794, 21.93913459777832, "Instrument Swath Width About 600 km"]
+[1.785080075263977, 22.119888305664062, "Instrument Spatial Resolution at 37 GHz About 22 km"]
+[1.825393557548523, 22.131223678588867, "Instrument Spatial Resolution at 6.6 GHz About 100 km"]
+[2.2135539054870605, 22.356473922729492, "Instrument Sea Surface Temperature Accuracy 2 K"]
+[2.0732152462005615, 22.41008758544922, "Instrument Wind Speed Measurements Accuracy 2 m/s"]
+[1.5182859897613525, 21.234891891479492, "Instrument Mass 53.9 kg"]
+[1.6260697841644287, 23.218679428100586, "Instrument Power Consumption ~60 W"]
+[0.45429444313049316, 4.518319606781006, "Environmental Phenomenon Date Spring 2021"]
+[0.43996790051460266, 4.530028343200684, "Environmental Phenomenon Date 16 January 2021"]
+[0.4798749089241028, 4.520754337310791, "Environmental Phenomenon Date 14 December 2020"]
+[0.501923143863678, 4.543507099151611, "Environmental Phenomenon Date 11 November 2020"]
+[1.5122137069702148, 5.420992851257324, "Satellite Bus Diameter 2.10 m"]
+[1.5113002061843872, 5.420977592468262, "Satellite Bus Length 3.195 m"]
+[1.5112638473510742, 5.425179481506348, "Satellite Bus Spin Configuration Dual-spin at 100 rpm"]
+[1.5162112712860107, 5.424500465393066, "Satellite Bus Dry Mass 322 kg"]
+[1.5059329271316528, 5.422465801239014, "Satellite Bus Launch Mass 696 kg"]
+[1.5017036199569702, 5.4304022789001465, "Satellite Bus Design Life 5 years"]
+[1.5028700828552246, 5.423305988311768, "Satellite Bus RF Communications S-band"]
+[1.5147029161453247, 5.420910835266113, "Satellite Bus RF Communications L-band"]
+[-2.1389808654785156, 5.51627779006958, "Deployment System Quantity 4"]
+[0.7208519577980042, -1.176005482673645, "Satellite Altitude ~325 km"]
+[0.7188488841056824, -2.2913002967834473, "Satellite Inclination ~51.6\u00ba"]
+[11.205875396728516, 5.342966556549072, "CubeSat Quantity of Femtosatellites About 250"]
+[11.16020679473877, 5.265934467315674, "CubeSat Mass ~5.5 kg"]
+[11.514093399047852, 5.738908290863037, "CubeSat Size 2U"]
+[11.506637573242188, 5.717225074768066, "CubeSat Size 1U"]
+[0.9937673211097717, -4.400106430053711, "Satellite Mass 764 kg (including fuel)"]
+[2.055926561355591, -0.6147249937057495, "Satellite Power 693 W (EOL)"]
+[0.977890133857727, -4.317713737487793, "Satellite Propellant 81 kg, N 2 H 4"]
+[1.048384428024292, -2.0690441131591797, "Satellite Pointing Accuracy 0.12\u00ba, 0.02\u00ba"]
+[1.401047945022583, -1.2898939847946167, "Satellite Position Knowledge of Imagery 9 m"]
+[0.9866659641265869, -2.175999164581299, "Satellite Pointing Agility Roll 10\u00ba in 25 s and 30\u00ba in 45 s, pitch 45\u00ba in 60 s"]
+[-5.351253032684326, 7.974065780639648, "Communication System Frequency S-band"]
+[-5.198605060577393, 7.769524574279785, "Communication System Data Rate 4 kbit/s uplink, 1.6 Mbit/s downlink"]
+[-3.866224527359009, 7.944357395172119, "Data Storage Capacity 41 Gbit on SSR (Solid State Recorder)"]
+[-3.209165096282959, 4.244126796722412, "Spacecraft Imaging Frequency Every three hours"]
+[-3.1186442375183105, 4.195361137390137, "Spacecraft Data Availability Rapidly made public through NASA\u2019s Mikulski Archive for Space Telescopes (MAST)"]
+[-1.1691772937774658, 3.035327434539795, "Celestial Object Normal Activity Driven by sunlight vaporizing the ices near the surface of the nucleus"]
+[2.100802183151245, -2.6765682697296143, "Satellite Orbits Per Day 15"]
+[4.201991081237793, -2.7986373901367188, "Satellite Communication Pass Duration 8 to 10 minutes"]
+[1.1513912677764893, -1.374288558959961, "Satellite Maximum Elevation Varies"]
+[0.7319320440292358, -1.1745924949645996, "Satellite Pass Elevation Sequence High, Low, High"]
+[3.510063409805298, -2.537400484085083, "Satellite High-Elevation Pass Selection Once per day"]
+[2.447530508041382, 22.772424697875977, "Instrument Band Number 1, 2, 3, 4, 5, 6, 7, 8"]
+[2.1039280891418457, 22.63878059387207, "Instrument Spectral Band (\u00b5m) 0.402 - 0.422, 0.433 - 0.453, 0.480 - 0.500, 0.511 - 0.529, 0.555 - 0.575, 0.660 - 0.680, 0.745 - 0.785, 0.845 - 0.885"]
+[2.0333735942840576, 22.687360763549805, "Instrument Bandwidth (\u00b5m) 0.020, 0.020, 0.020, 0.018, 0.020, 0.020, 0.040, 0.040"]
+[2.034764528274536, 22.52118492126465, "Instrument Radiance (W/m/sr/\u00b5m) 145, 150, 130, 120, 90, 60, 40, 20"]
+[2.2634034156799316, 22.684669494628906, "Instrument SNR 450, 500, 500, 500, 500, 500, 500, 450"]
+[2.2067601680755615, 22.527202606201172, "Instrument NEDT 3.55 - 3.88, 8.25 - 8.80, 10.3 - 11.4, 11.4 - 12.7"]
+[2.2051119804382324, 22.359140396118164, "Instrument IFOV 0.85 mrad (~700 m)"]
+[2.4216601848602295, 22.48996925354004, "Instrument Quantization 10-bit/pixel"]
+[2.120090961456299, 22.190855026245117, "Instrument Scanning angle ~\u00b140\u00ba (1400 km)"]
+[2.092238664627075, 22.15790367126465, "Instrument Tilting angle -20\u00ba, 0\u00ba, +20\u00ba"]
+[2.1637930870056152, 22.666027069091797, "Instrument Polarization sensitivity Band 1 \u2264 5%, Band 2-8 \u2264 2%"]
+[-1.628861904144287, 9.632364273071289, "Ion Engine System Maximum Power Consumption < 20 W"]
+[-1.6139010190963745, 9.625140190124512, "Ion Engine System Instrument Mass < 6.2 kg"]
+[-1.6223970651626587, 9.676639556884766, "Ion Engine System Vibration Tolerance > 20 G rms"]
+[-1.6437687873840332, 9.572223663330078, "Ion Engine System Shock Tolerance > 1000 G srs"]
+[-1.6197521686553955, 9.638922691345215, "Ion Engine System Operation Temperature -25\u00ba to 55\u00baC"]
+[-0.27406710386276245, 10.271561622619629, "Tracking System Tracking Task Completion Date November 2, 2010"]
+[-3.3087546825408936, 4.249444007873535, "Spacecraft Circumlunar Flight Duration 150 days"]
+[-3.004718065261841, 4.214460372924805, "Spacecraft Elliptical Lunar Orbit 100 km x 15 km (apoapsis x periapsis)"]
+[-3.0000691413879395, 4.189183235168457, "Spacecraft Preliminary Circular Lunar Orbit 100 km x 100 km"]
+[-3.320657730102539, 4.363861560821533, "Spacecraft Midway Correction Control October 2, 2010"]
+[-3.0693697929382324, 4.290362358093262, "Spacecraft Midway Correction Control 490 N"]
+[16.88430404663086, 6.841517925262451, "Microsatellites Objective Evaluate new technologies in the high radiation dose environment of GTO"]
+[16.915863037109375, 6.807675361633301, "Microsatellites Technologies Tested Advanced structural materials, radiation hardened computers, sensors, solar cells, vibration suppression on a cryogenic cooler, measurements of the ion and electron environment, spacecraft charging, and microelectronics"]
+[2.243279457092285, 22.723478317260742, "Instrument Gain Stability Far slower than the MWIR and LWIR channels"]
+[0.23475034534931183, 13.798583984375, "Calibration Device Observation Frequency Approximately every two weeks"]
+[-3.097599983215332, 2.4429078102111816, "Mission Tool Definition and Upload Any time during the mission life"]
+[1.7533828020095825, 10.926482200622559, "Imaging Mode Images Collected 30-second Mesoscale, 5-minute CONUS, 10-minute Full Disk"]
+[1.1476573944091797, -0.753383219242096, "Satellite Size 10 cm x 10 cm x 34 cm"]
+[0.9991230964660645, -4.403580665588379, "Satellite Mass 5.5 kg"]
+[-2.0119566917419434, 8.638160705566406, "Electronic System Components Three main PCBs \u2013 EPS, C&DH, and Backplane"]
+[-2.042055368423462, 8.644149780273438, "Electronic System CPU PIC32"]
+[-2.0579702854156494, 8.612552642822266, "Electronic System Memory microSD (2 GB), and 3Mbit FRAM"]
+[-2.1276514530181885, 8.673849105834961, "Electronic System Bus Power Less than 50 mA (without radios)"]
+[-2.0588300228118896, 8.636914253234863, "Electronic System Battery Capacity 80 Whr"]
+[1.7201368808746338, -2.0138492584228516, "Satellite Attitude Control Permanent magnets and hysteresis rods"]
+[2.0932986736297607, -2.176229476928711, "Satellite Solar Panels Fixed body mounted triple junction"]
+[-2.1306521892547607, 8.67876148223877, "Electronic System Radios 1 Microhard 2420, 1 Stensat beacon"]
+[-5.354016304016113, 2.783752918243408, "Telescope Aperture 35 cm"]
+[2.605764627456665, 13.992194175720215, "Optical Alignment System Degrees-of-freedom 6"]
+[2.6040523052215576, 13.916078567504883, "Optical Alignment System Mechanism Actuators"]
+[2.606555938720703, 13.885293960571289, "Optical Alignment System Adjustment  Misalignment"]
+[6.316231727600098, 7.426761150360107, "Satellite Component Attachment Cylindrical tube"]
+[2.654874801635742, -1.8322625160217285, "Satellite Proximity to Payload Net payload"]
+[2.4313066005706787, -1.831344485282898, "Satellite Proximity to Payload VBN sensor and ISL"]
+[-7.576677322387695, 5.884782314300537, "Cameras Attachment Optimization Provide the best possible view of all of the demonstrations"]
+[-0.8492620587348938, 0.16346518695354462, "Satellite System Follow-up System RADARSAT-2"]
+[-0.8629056811332703, 0.18974359333515167, "Satellite System Launch Timeframe 2012-14"]
+[-0.809456467628479, 0.1514105647802353, "Satellite System Ground Segment Architecture Modular distributed system"]
+[-0.8399719595909119, 0.15938560664653778, "Satellite System Technology Up to date"]
+[2.926778793334961, -1.4530528783798218, "Satellite Mission High-resolution optical reconnaissance and Earth observation"]
+[3.106114387512207, -1.5382018089294434, "Satellite Mission Type Dual use - civil and defense"]
+[2.4084436893463135, -1.9559012651443481, "Satellite Ground Stations One fixed and one mobile"]
+[-0.20294131338596344, 15.447832107543945, "Spectrometer Detector CCD array"]
+[-0.128490149974823, 15.533425331115723, "Spectrometer Components Photodiode array, visible light cameras, calibration lamp, optics and baffling"]
+[-1.1643595695495605, 8.683424949645996, "Canister Components Canister extension ring, HMDA"]
+[-2.2062065601348877, 8.26449966430664, "Interface Components HH Remote Interface Unit (HRIU), LEP (Lower End Plate) electronics"]
+[-2.2941527366638184, 8.327383995056152, "Remote Interface Unit Power Source HH avionics"]
+[2.7630960941314697, 22.370481491088867, "Instrument Data Recording On triggering alerts only"]
+[2.742154359817505, 22.353660583496094, "Instrument Data Recording On triggering alerts only"]
+[2.756068229675293, 22.34524917602539, "Instrument Data Recording On triggering alerts only"]
+[2.7740423679351807, 22.296117782592773, "Instrument Data Recording On triggering alerts only"]
+[2.279020309448242, 22.4832820892334, "Instruments Relative Time Accuracy Less than 10 ns"]
+[2.2026748657226562, 22.5219783782959, "Instruments Absolute Time Accuracy Less than 1 ms"]
+[2.7014875411987305, 22.63694953918457, "Instruments Data Download Up to about 2 GB of high-resolution data (event mode) will be downloaded per day"]
+[-3.490203857421875, 4.373979568481445, "Spacecraft Test Flight Date Fall 2014"]
+[-3.514256477355957, 4.390471458435059, "Spacecraft Crew Module Launch Date Dec. 2014"]
+[-2.725567102432251, 15.31014633178711, "Scanning Multichannel Microwave Radiometer Measurement Goals Obtain all-weather measurements of ocean surface temperature and wind speed"]
+[-2.7166974544525146, 15.299534797668457, "Scanning Multichannel Microwave Radiometer Measurement Results The instrument has produced the first global maps of surface temperature together with maps of wind speed"]
+[-2.6919732093811035, 15.290106773376465, "Scanning Multichannel Microwave Radiometer Measurement Goals Obtain integrated liquid water and water vapour content in the atmosphere"]
+[-2.6760990619659424, 15.309497833251953, "Scanning Multichannel Microwave Radiometer Measurement Results Water vapour measurements proved to be at least as accurate as radiosondes"]
+[-2.7261157035827637, 15.304464340209961, "Scanning Multichannel Microwave Radiometer Measurement Results Liquid water in clouds and rain was mapped globally"]
+[-2.6908676624298096, 15.294191360473633, "Scanning Multichannel Microwave Radiometer Instrument Function Provide necessary corrections for the SeaSat altimeter and scatterometer measurements"]
+[-2.6968138217926025, 15.28420352935791, "Scanning Multichannel Microwave Radiometer Instrument Function Accurate corrections were provided for both instruments"]
+[1.6291543245315552, 22.17690658569336, "Instrument Dimensions 7.6 cm x 7.6 cm x 7.1 cm"]
+[1.5289263725280762, 21.253225326538086, "Instrument Mass ~ 0.850 kg"]
+[1.6141319274902344, 23.232563018798828, "Instrument Power Consumption 1.3 W"]
+[-0.36720195412635803, 8.36155891418457, "Composite Sheet Power Consumption 5.3 W"]
+[-0.6248330473899841, 8.467325210571289, "Composite Sheet Components Layer of polymer matrix composite with a thin strip of shape memory alloy on each side"]
+[1.6488685607910156, 6.960940837860107, "Flexible Interconnect Thickness <0.25 mm"]
+[16.849712371826172, 6.857392311096191, "Microsatellite Manufacturer CNES"]
+[16.88818359375, 6.830129146575928, "Microsatellite Operator CNES"]
+[3.4330430030822754, 13.42746639251709, "Laser Intersatellite Terminal Development Funding DLR German Aerospace Center"]
+[3.49407696723938, -2.5569193363189697, "Satellite Laser Beam Link Frequency Up to 15 times per day"]
+[2.649045467376709, -2.6933960914611816, "Satellite Laser Beam Link Speed 600 Mbit/s"]
+[2.6241095066070557, -2.6435654163360596, "Satellite Laser Terminal Speed 1.8 Gbit/s"]
+[-1.6194336414337158, 1.480944275856018, "Data Relay System Data Relay Capacity Up to 50 TB a day"]
+[4.916540622711182, -2.4329543113708496, "Satellite Operational Lifetime At least 15 years"]
+[2.0933125019073486, -2.725192070007324, "Satellite Number of Satellites 4"]
+[2.1080615520477295, -2.726459264755249, "Satellite Number of Satellites in Operation 2"]
+[2.2265994548797607, -2.4328536987304688, "Satellite Backup Satellite 1"]
+[2.9933085441589355, 22.535715103149414, "Instrument Manufacturer Airbus Defence and Space in France"]
+[1.7047053575515747, 6.937890529632568, "Communication Device Manufacturer Tesat Spacecom GmbH"]
+[1.7167003154754639, 6.939237594604492, "Communication Device Function Transmit data via laser to satellites in geostationary orbit"]
+[2.783243179321289, 22.291606903076172, "Instruments Objective Measure changes in optical transmission, thermal absorption and emission"]
+[2.800859212875366, 22.318668365478516, "Instruments Function Measure the effects of erosion from quartz windows and re-deposition of material onto nearby optics"]
+[2.8307125568389893, 22.197683334350586, "Instruments Function Detect changes in thermal control paint coefficients of heat gain / loss based on exposure"]
+[-3.410231113433838, 4.306458473205566, "Space Probe Close Flyby Date December 13, 2012"]
+[-1.1561371088027954, 3.0480732917785645, "Celestial Body Size ~ 5 km in length"]
+[0.4370630979537964, 12.268115043640137, "Sensor Array Size 512 x 2 pixel"]
+[1.892951488494873, 10.714622497558594, "Imaging Device Band MWIR (Midwave Infrared)"]
+[1.8830541372299194, 10.715760231018066, "Imaging Device Band TIR (Thermal Infrared)"]
+[4.70229434967041, -2.494405746459961, "Spaceborne Service Monitoring Duration Less than three years"]
+[-2.9317383766174316, 1.9244258403778076, "Spaceborne Service Forest Cover Loss 5-6 per cent to just 0.06 per cent"]
+[-4.602625370025635, -3.1282362937927246, "Exoplanet Orbit Period 9 hours"]
+[-4.567629814147949, -3.095479965209961, "Exoplanet Number of Summers and Winters 2 each"]
+[-4.55871057510376, -3.0931613445281982, "Exoplanet Temperature Difference Almost 1,500\u00ba F (800\u00ba C)"]
+[-4.567408084869385, -3.0926589965820312, "Exoplanet Transit Lopsided"]
+[-4.552885055541992, -3.0769145488739014, "Exoplanet Transit Begins near the star's bright poles and then blocks less and less light as it travels over the star's dimmer equator"]
+[6.285942077636719, 7.455431938171387, "Satellite Component Backup Active"]
+[3.7204833030700684, 22.972820281982422, "Instrument Activation Date 11 June 2018"]
+[7.32053279876709, 12.445910453796387, "Satellite Instrument Unknown Unknown"]
+[-2.221072196960449, 2.866908550262451, "Space-based Observatory Mission Status Feasible for final technology development and design before adoption"]
+[-2.21860671043396, 2.8699800968170166, "Space-based Observatory Formation Three spacecraft flying in a triangular formation with 2.5-million kilometre-long sides"]
+[-2.215597152709961, 2.867802381515503, "Space-based Observatory Mission Lifetime Cycle Phase Phase A"]
+[1.0405776500701904, -2.0407021045684814, "Satellite Pointing Accuracy 0.01\u00ba"]
+[0.9702049493789673, -4.383366107940674, "Satellite Mass ~1220 kg"]
+[-1.500518798828125, 13.425393104553223, "Solar Array Size 9.29 m2"]
+[-1.4879655838012695, 13.409156799316406, "Solar Array Power 2.2 kW"]
+[-3.5207204818725586, 6.790406227111816, "Data Types UltraRapid, Rapid, Final"]
+[-3.521969795227051, 6.790783405303955, "Data Average Latency About 4 hours, 17 hours, 12 days"]
+[-1.8848778009414673, 6.910386085510254, "Software Run Frequency Once per day"]
+[-1.9570149183273315, 6.927794933319092, "Software Orbit File Generation Period 24 hours"]
+[-1.928659200668335, 6.899989604949951, "Software Orbit File Latency About 48 hours"]
+[-1.9318149089813232, 6.903820037841797, "Software Orbit File Latency About 24 hours"]
+[4.664099216461182, -2.5983822345733643, "Satellite Mission Duration 1 year"]
+[-0.8443982005119324, 7.674265384674072, "Object Size Basketball-size"]
+[-1.9590661525726318, 8.170515060424805, "Containment System Purpose Ensure that the precious samples reach the Earth\u2019s surface intact"]
+[-1.9137662649154663, 7.388059616088867, "Review Board Recommendations Provided to NASA"]
+[-1.3252246379852295, 6.049496650695801, "Agency Confirmation Decision Date 2033"]
+[-1.8500704765319824, 6.812482833862305, "Pathfinder Launch Date September 13, 2012"]
+[-1.857923984527588, 6.915239334106445, "Pathfinder Communication Issues Spring/Summer of 2013"]
+[-1.8517094850540161, 6.817318439483643, "Pathfinder Launch Date November 20, 2013"]
+[-1.8796806335449219, 6.977652549743652, "Pathfinder Attitude Control Full set of reaction wheels"]
+[-1.8523343801498413, 6.931032180786133, "Pathfinder Imager More sensitive"]
+[-3.0581953525543213, 20.238019943237305, "Spectral Band Center Wavelength 14.71 \u00b5m (680 cm -1)"]
+[-2.9030721187591553, 20.149513244628906, "Spectral Band Bandwidth 0.281 \u00b5m (13 cm -1)"]
+[-2.6773626804351807, 20.379663467407227, "Spectral Band NEDT at 300 K 1.5 K"]
+[-3.0819954872131348, 19.87712860107422, "Spectral Band Principal Absorbing Constituents CO2"]
+[-3.007089376449585, 20.191356658935547, "Spectral Band Center Wavelength 14.37 \u00b5m (696 cm -1)"]
+[-2.877963066101074, 20.155061721801758, "Spectral Band Bandwidth 0.268 \u00b5m (13 cm -1)"]
+[-2.6840455532073975, 20.376489639282227, "Spectral Band NEDT at 300 K 1 K"]
+[-3.0836029052734375, 19.874977111816406, "Spectral Band Principal Absorbing Constituents CO2"]
+[-3.0137758255004883, 20.19408416748047, "Spectral Band Center Wavelength 14.06 \u00b5m (711 cm -1)"]
+[-2.9137380123138428, 20.110822677612305, "Spectral Band Bandwidth 0.256 \u00b5m (13 cm -1)"]
+[-2.6758973598480225, 20.38235855102539, "Spectral Band NEDT at 300 K 0.5 K"]
+[-3.0841243267059326, 19.874088287353516, "Spectral Band Principal Absorbing Constituents CO2"]
+[-3.0196094512939453, 20.207138061523438, "Spectral Band Center Wavelength 13.96 \u00b5m (733 cm -1)"]
+[-2.878204822540283, 20.14856719970703, "Spectral Band Bandwidth 0.298 \u00b5m (16 cm -1)"]
+[-2.668142080307007, 20.388057708740234, "Spectral Band NEDT at 300 K 0.5 K"]
+[-3.0840377807617188, 19.87465476989746, "Spectral Band Principal Absorbing Constituents CO2"]
+[-3.02545428276062, 20.21299934387207, "Spectral Band Center Wavelength 13.37 \u00b5m (749 cm -1)"]
+[-2.891122341156006, 20.1473331451416, "Spectral Band Bandwidth 0.286 \u00b5m (16 cm -1)"]
+[-2.6715729236602783, 20.386659622192383, "Spectral Band NEDT at 300 K 0.5 K"]
+[-3.096588134765625, 19.805810928344727, "Spectral Band Principal Absorbing Constituents CO2"]
+[-3.057321786880493, 20.23794937133789, "Spectral Band Center Wavelength 12.66 \u00b5m (790 cm -1)"]
+[-2.901489019393921, 20.14405059814453, "Spectral Band Bandwidth 0.481 \u00b5m (30 cm -1)"]
+[-2.678107738494873, 20.37830924987793, "Spectral Band NEDT at 300 K 0.3 K"]
+[-3.083646297454834, 19.874290466308594, "Spectral Band Principal Absorbing Constituents Water vapor"]
+[-3.0680992603302, 20.261371612548828, "Spectral Band Center Wavelength 12.02 \u00b5m (832 cm -1)"]
+[-2.88642954826355, 20.15299415588379, "Spectral Band Bandwidth 0.723 \u00b5m (50 cm -1)"]
+[-2.6365222930908203, 20.413436889648438, "Spectral Band NEDT at 300 K 0.15 K"]
+[-3.0914711952209473, 19.842041015625, "Spectral Band Principal Absorbing Constituents Water vapor"]
+[-3.0177955627441406, 20.197423934936523, "Spectral Band Center Wavelength 11.03 \u00b5m (907 cm -1)"]
+[-2.8867011070251465, 20.143110275268555, "Spectral Band Bandwidth 0.608 \u00b5m (50 cm -1)"]
+[-2.6394104957580566, 20.415395736694336, "Spectral Band NEDT at 300 K 0.15 K"]
+[-3.0954599380493164, 19.841327667236328, "Spectral Band Principal Absorbing Constituents Window"]
+[-3.016395092010498, 20.196826934814453, "Spectral Band Center Wavelength 9.71 \u00b5m (1030 cm -1)"]
+[-2.9055874347686768, 20.152610778808594, "Spectral Band Bandwidth 0.235 \u00b5m (25 cm -1)"]
+[-2.6904664039611816, 20.37201690673828, "Spectral Band NEDT at 300 K 0.2 K"]
+[-3.099350690841675, 19.841699600219727, "Spectral Band Principal Absorbing Constituents Ozone"]
+[-3.0033390522003174, 20.185306549072266, "Spectral Band Center Wavelength 7.43 \u00b5m (1425 cm -1)"]
+[-2.893676280975342, 20.160686492919922, "Spectral Band Bandwidth 0.304 \u00b5m (55 cm -1)"]
+[-2.6998705863952637, 20.367177963256836, "Spectral Band NEDT at 300 K 0.2 K"]
+[-3.1149630546569824, 19.824390411376953, "Spectral Band Principal Absorbing Constituents Water vapor"]
+[-3.015711545944214, 20.197891235351562, "Spectral Band Center Wavelength 7.02 \u00b5m (1425 cm -1)"]
+[-2.8992629051208496, 20.14322853088379, "Spectral Band Bandwidth 0.394 \u00b5m (80 cm -1)"]
+[-2.6936981678009033, 20.369873046875, "Spectral Band NEDT at 300 K 0.2 K"]
+[-3.095069408416748, 19.840129852294922, "Spectral Band Principal Absorbing Constituents Water vapor"]
+[-3.0172293186187744, 20.233104705810547, "Spectral Band Center Wavelength 6.51 \u00b5m (1535 cm -1)"]
+[-2.841409921646118, 20.083179473876953, "Spectral Band Bandwidth 0.255 \u00b5m (60 cm -1)"]
+[-3.0396323204040527, 4.264301300048828, "Spacecraft Data Source High-energy X-ray data"]
+[-3.1095926761627197, 4.299302101135254, "Spacecraft Purpose Take focused pictures of the cosmos in high-energy X-ray light"]
+[2.759486436843872, -1.8945633172988892, "Satellite Cloud Detection Scheme Unknown"]
+[5.317294120788574, -4.423717021942139, "Satellite Launch Date January 2017"]
+[-0.9935060739517212, 9.420494079589844, "Rocket Component Quantity 4"]
+[-0.9778990149497986, 9.487688064575195, "Rocket Component Configuration X-wing"]
+[-0.9893258810043335, 9.515735626220703, "Rocket Component Function Control the stage's lift vector"]
+[-1.0065796375274658, 9.52155876159668, "Rocket Component Independence Each fin moves independently for roll, pitch and yaw"]
+[-5.3027024269104, 2.804316759109497, "Telescope URL http://constellation.gsfc.nasa.gov/resources/Published_Papers/HighResolutionXrayTelescopes2010.pdf"]
+[2.6837809085845947, 14.352657318115234, "Optical Instrument Light-Tight Requirement Three-bounce"]
+[-1.22544527053833, 8.61115550994873, "Component Function Allow venting after launch"]
+[-0.6189206838607788, 9.415996551513672, "Spacecraft Component Material Aluminum"]
+[-0.6309953927993774, 9.412635803222656, "Spacecraft Component Material Aluminum"]
+[1.0727473497390747, -4.4302215576171875, "Satellite Total Mass 7.5 kg"]
+[-5.473764419555664, 2.7919247150421143, "Telescope Strehl Ratio < 0.5 at wavelength of 450 nm"]
+[-5.360709190368652, 2.799006223678589, "Telescope Strehl Ratio > 0.8 at near infrared band"]
+[-5.460524082183838, 2.7199370861053467, "Telescope Design Nearly diffraction-limited system close to the near-infrared band"]
+[-5.458978176116943, 2.7277536392211914, "Telescope Spot Size Smaller than the pixel size of the detector"]
+[-8.146404266357422, 8.823123931884766, "Electric Power Subsystem Maximum Power 65 W"]
+[-8.137038230895996, 8.823461532592773, "Electric Power Subsystem Average On-Orbit Power 42-52 W"]
+[-8.149965286254883, 8.825039863586426, "Electric Power Subsystem Voltage 28 V and 5 V"]
+[-8.145309448242188, 8.824053764343262, "Electric Power Subsystem Battery Type 6 Ah NiCd batteries at 28 V"]
+[-5.156762599945068, 7.944339752197266, "Communication Subsystem Frequency Bands S-band, UHF/VHF bands"]
+[2.1914143562316895, 13.385751724243164, "Optical Sensor Sensor Type Core sensor of OCTS heritage"]
+[2.1965014934539795, 13.401385307312012, "Optical Sensor Image Credit JAXA"]
+[2.2219626903533936, 13.371282577514648, "Optical Sensor Observation Scheme Figure 7"]
+[5.319833278656006, -2.189692735671997, "Satellite Design Life 5 years"]
+[1.923712968826294, 10.721456527709961, "Imaging Device Precision-Pointing Accuracy 0.01\u00ba"]
+[-1.709050178527832, 8.877427101135254, "Control System Components Combination flywheel and magnetic control coil system"]
+[1.8802763223648071, 10.719182968139648, "Imaging Device Geographical Mapping Accuracy Automatic"]
+[5.250732421875, -4.416746616363525, "Satellite Launch Date 26 July 2013"]
+[3.194826364517212, -1.538475751876831, "Satellite Mission Type EO"]
+[3.0496020317077637, -1.5730304718017578, "Satellite Mission Owner ISRO (Indian Space Research Organisation)"]
+[2.9143128395080566, -1.180726170539856, "Satellite Mission Purpose Provide enhanced meteorological observations and monitoring of land and ocean for weather forecasting and disaster warning"]
+[1.000985026359558, -4.407553195953369, "Satellite Mass 63 kg"]
+[0.959152102470398, -4.365349769592285, "Satellite Payload Mass 17 kg"]
+[2.0870907306671143, -0.5426021814346313, "Satellite Average Power 12 W"]
+[1.745184063911438, -1.757668137550354, "Satellite Orbit Average Power 14-27 W"]
+[1.5672385692596436, -2.2689599990844727, "Satellite Spin Stabilization 3 rpm"]
+[1.073443055152893, -2.1165404319763184, "Satellite Coarse Attitude Knowledge \u00b15\u00ba"]
+[5.065363883972168, -2.326815128326416, "Satellite Design Life One year"]
+[-2.606553554534912, 11.780048370361328, "Advanced Baseline Imager Development Date Nov. 3-5, 2009"]
+[-2.6473827362060547, 11.701506614685059, "Advanced Baseline Imager Presentation Date Jan. 17-21, 2010"]
+[-2.698564291000366, 11.691879272460938, "Advanced Baseline Imager URL http://www.goes-r.gov/education/docs/Factsheet_ABI_v6.pdf"]
+[2.719534397125244, 22.44403076171875, "Instrument Type Multiple direction/polarisation radiometers"]
+[5.33789587020874, -4.466780185699463, "Satellite Launch Date May 27, 2012"]
+[-3.635784864425659, 12.765275955200195, "Particle Detector Dark Matter Detection Unknown"]
+[-3.658101797103882, 12.765067100524902, "Particle Detector Antimatter Detection Unknown"]
+[-3.6409337520599365, 12.747584342956543, "Particle Detector Hypothesis After the Big Bang, identical amounts of matter and antimatter were created"]
+[0.6327068209648132, 12.031947135925293, "Sensor Technology CCD 4720 from E2V"]
+[0.5765735507011414, 12.023916244506836, "Sensor Operation Mode NIMO (Non Inverted Mode Operation)"]
+[0.575526237487793, 11.95140552520752, "Sensor Cooling System Two-stage TEC (Thermoelectric Cooler)"]
+[0.5362014770507812, 12.104412078857422, "Sensor Module Type Photometer"]
+[0.6214023232460022, 12.056816101074219, "Sensor Module Operation Plugged into the MEXIC module"]
+[-2.4376862049102783, 13.117486953735352, "High-Resolution Multispectral Scanner Manufacturer ISDE (Institute of Space Device Engineering, Moscow)"]
+[-2.4274070262908936, 13.107576370239258, "High-Resolution Multispectral Scanner Type Sensor"]
+[-0.4842223525047302, 5.858506679534912, "Unknown Unknown Unknown"]
+[2.835775136947632, -1.2410441637039185, "Satellite Mission Purpose Provide images for distinguishing crop types and data on plant indices"]
+[4.745387554168701, -4.489902496337891, "Satellite Image Capture Date March 2021"]
+[4.618625164031982, -4.578221797943115, "Satellite Image Capture Date April 8, 2022"]
+[2.1775357723236084, -1.4785146713256836, "Satellite High-resolution optical imager Onboard"]
+[2.663412570953369, -1.2101306915283203, "Satellite Objective Continuously providing optical observations of land and coastlines"]
+[1.4036966562271118, -3.1068482398986816, "Satellites Objectives Radar mapping of land and sea, air quality, and sea-surface topography and temperature"]
+[6.7453107833862305, 6.953620433807373, "Satellite Component Unknown Unknown"]
+[-1.863796591758728, 14.82510757446289, "Radiometer Purpose Measurement of the solar constant"]
+[-1.8138664960861206, 14.917609214782715, "Radiometer Objective Measurement of the absolute value of the total solar irradiance (and long-term variations)"]
+[3.7170300483703613, 22.98863410949707, "Instrument Comparison Date 11 January 2019"]
+[-1.0581151247024536, 7.699490547180176, "Device Conference Date July 22-27, 2012"]
+[2.627589464187622, -1.3057045936584473, "Satellite Surveillance Capabilities All-weather, day/night persistent surveillance"]
+[-1.218389630317688, 6.76027250289917, "Project Capabilities Near real-time ship detection, arctic land surveillance, environmental sensing, maritime surveillance radar beam optimization"]
+[0.8068969249725342, -1.1225178241729736, "Satellite Measurement Depth Up to 140 feet (43 meters)"]
+[2.6710822582244873, -1.1492159366607666, "Satellite Application Investigate coastal ecosystems, measure mangrove forests, measure sea level rise in coastal regions, improve nearshore bathymetry maps"]
+[2.66365647315979, -1.4163581132888794, "Satellite Data Presentation AGU meeting"]
+[-2.6972451210021973, 8.762086868286133, "Module Components Atmel's high speed ADC (Analog Digital Converter) & demultiplexer and a Xilinx XQVR-600 FPGA-based BAQ and formatter"]
+[-2.0061874389648438, 7.4927077293396, "Hardware Components Motherboard-daughterboard configuration using a single 80C32 microcontroller, a Xilinx XQVR-600 FPGA, a Mil-STD-1553B based control processor and 3 I/O modules along with its power supply"]
+[-1.6426348686218262, 14.761273384094238, "Calorimeter Module Section 648 mm x 648 mm"]
+[-1.7015327215194702, 14.816033363342285, "Calorimeter Module Depth 18 mm"]
+[-1.6323015689849854, 14.798235893249512, "Calorimeter Module Rotation 90\u00ba"]
+[-0.8227049112319946, 11.586549758911133, "Detector Pixels per PMT 4"]
+[-1.5848965644836426, 14.803889274597168, "Calorimeter Elementary Cell Size 648 mm x 9 mm"]
+[-5.335560321807861, 2.693909168243408, "Telescope Location Happy Jack, Arizona"]
+[-5.433821201324463, 2.7460343837738037, "Telescope Image Source Sloan Digital Sky Survey"]
+[-6.737419605255127, 10.007152557373047, "Antenna Area 23 m2"]
+[-4.743357181549072, 9.245630264282227, "Transmitter Mounting Location On the mast"]
+[-4.756497859954834, 9.261372566223145, "Transmitter Antenna Type Helical"]
+[-3.571277141571045, 4.417759418487549, "Spacecraft Launch Date June 27 (UTC), 1978"]
+[-3.0255682468414307, 4.168323516845703, "Spacecraft Orbit Type Non-sun-synchronous near circular polar orbit"]
+[-3.0074801445007324, 4.186551570892334, "Spacecraft Orbit Inclination 108\u00ba"]
+[-3.02144193649292, 4.221489429473877, "Spacecraft Apogee 799 km"]
+[-3.0317702293395996, 4.23952579498291, "Spacecraft Perigee 775 km"]
+[-3.1927340030670166, 4.250326633453369, "Spacecraft Orbit Period 101 minutes"]
+[-3.2676002979278564, 4.286013126373291, "Spacecraft Repeat Cycle 17 days"]
+[0.4113107919692993, 12.358721733093262, "Sensor Channel frequencies AIS #1: 161.975 MHz, AIS #2: 162.025 MHz AIS #3: 156.775 MHz, AIS #4: 156.825 MHz"]
+[0.5091103911399841, 12.199748039245605, "Sensor Minimum receiver sensitivity -112 dBm"]
+[0.39311298727989197, 12.37830638885498, "Sensor Sampling rate 76.8 kHz"]
+[0.7885278463363647, 12.08041000366211, "Sensor Mass 7 kg"]
+[0.4913730025291443, 12.232467651367188, "Sensor Size 1050 mm x 800 mm x 800 mm"]
+[5.518699645996094, -4.398000240325928, "Satellite Launch Date 7 September 2018"]
+[1.3966445922851562, -2.557084798812866, "Satellite Orbit Type Sun-synchronous"]
+[0.628093957901001, -1.4988157749176025, "Satellite Orbit Altitude 780 km"]
+[0.7232366800308228, -2.2678003311157227, "Satellite Orbit Inclination 98.6\u00ba"]
+[3.890455484390259, -3.0056135654449463, "Satellite LTDN 10:30 \u00b130 min"]
+[5.275428295135498, -4.286954402923584, "Satellite Launch Date 10 June 2020"]
+[2.79654598236084, 22.34243392944336, "Instrument Mounting Location Japanese Experiment Module's Exposed Facility"]
+[-3.0917694568634033, 2.4196155071258545, "Mission Demonstration Transfer and long-term storage of liquid methane in microgravity"]
+[-3.1035170555114746, 2.4267914295196533, "Mission Importance Enable long duration journeys to destinations, such as the Moon and Mars"]
+[0.3886256515979767, 12.399452209472656, "Sensor Center Frequency 10.6 GHz"]
+[0.9329328536987305, 12.20533275604248, "Sensor Number of Passbands 1"]
+[0.4063490629196167, 12.390372276306152, "Sensor Bandwidth 100 MHz"]
+[0.5154260396957397, 12.095415115356445, "Sensor Effective FOV 89 x 198 km"]
+[0.44087305665016174, 12.256322860717773, "Sensor Pixel Size 32 x 32 km"]
+[0.4874069392681122, 12.24914264678955, "Sensor Sensitivity 0.5 K/pixel"]
+[0.7305070161819458, 12.076818466186523, "Sensor Approx. Peak Sensitivity Altitude Unknown"]
+[0.3962368965148926, 12.408113479614258, "Sensor Center Frequency 18.7 GHz"]
+[0.9627254605293274, 12.221139907836914, "Sensor Number of Passbands 1"]
+[0.3949319124221802, 12.397439002990723, "Sensor Bandwidth 200 MHz"]
+[0.48428255319595337, 12.174997329711914, "Sensor Effective FOV 52 x 16 km"]
+[0.4462488293647766, 12.263412475585938, "Sensor Pixel Size 32 x 32 km"]
+[0.525518000125885, 12.177334785461426, "Sensor Sensitivity 0.4 K/pixel"]
+[0.6575343012809753, 12.070693969726562, "Sensor Approx. Peak Sensitivity Altitude Unknown"]
+[0.38546034693717957, 12.383326530456543, "Sensor Center Frequency 23.8 GHz"]
+[0.9523051977157593, 12.217902183532715, "Sensor Number of Passbands 1"]
+[0.35444948077201843, 12.449308395385742, "Sensor Bandwidth 400 MHz"]
+[0.5236189961433411, 12.155458450317383, "Sensor Effective FOV 42 x 94 km"]
+[0.3703427314758301, 12.296412467956543, "Sensor Pixel Size 32 x 32 km"]
+[0.5427045822143555, 12.168482780456543, "Sensor Sensitivity 0.3 K/pixel"]
+[0.6609190106391907, 12.063204765319824, "Sensor Approx. Peak Sensitivity Altitude Unknown"]
+[0.38069137930870056, 12.424606323242188, "Sensor Center Frequency 31.5 GHz"]
+[0.9403982162475586, 12.21383285522461, "Sensor Number of Passbands 1"]
+[0.3857203423976898, 12.431260108947754, "Sensor Bandwidth 1000 MHz"]
+[0.4582984745502472, 12.178927421569824, "Sensor Effective FOV 35 x 76 km"]
+[0.42242661118507385, 12.27857494354248, "Sensor Pixel Size 32 x 32 km"]
+[0.5499984622001648, 12.154052734375, "Sensor Sensitivity 0.3 K/pixel"]
+[0.6472083330154419, 12.079192161560059, "Sensor Approx. Peak Sensitivity Altitude Unknown"]
+[0.39744558930397034, 12.402827262878418, "Sensor Center Frequency 36.5 GHz"]
+[0.9646598696708679, 12.206594467163086, "Sensor Number of Passbands 1"]
+[0.36797550320625305, 12.474603652954102, "Sensor Bandwidth 1000 MHz"]
+[0.456455796957016, 12.123677253723145, "Sensor Effective FOV 30 x 67 km"]
+[0.37860050797462463, 12.310214042663574, "Sensor Pixel Size 32 x 32 km"]
+[0.5388090014457703, 12.195746421813965, "Sensor Sensitivity 0.3 K/pixel"]
+[0.6449559926986694, 12.135690689086914, "Sensor Approx. Peak Sensitivity Altitude Unknown"]
+[0.3945716321468353, 12.399199485778809, "Sensor Center Frequency 42 GHz"]
+[0.9935222268104553, 12.217470169067383, "Sensor Number of Passbands 1"]
+[0.37582120299339294, 12.439562797546387, "Sensor Bandwidth 1000 MHz"]
+[0.4662224352359772, 12.168288230895996, "Sensor Effective FOV 26 x 60 km"]
+[0.408658504486084, 12.32265567779541, "Sensor Pixel Size 32 x32 km"]
+[0.5006735324859619, 12.259922981262207, "Sensor Sensitivity 0.4 K/pixel"]
+[0.6681156754493713, 12.089241981506348, "Sensor Approx. Peak Sensitivity Altitude Unknown"]
+[0.3601391613483429, 12.4386625289917, "Sensor Center Frequency 48 GHz"]
+[0.9572587013244629, 12.216389656066895, "Sensor Number of Passbands 1"]
+[0.37824705243110657, 12.437225341796875, "Sensor Bandwidth 1000 MHz"]
+[0.4728214144706726, 12.157576560974121, "Sensor Effective FOV 24 x 43 km"]
+[0.4140503704547882, 12.288759231567383, "Sensor Pixel Size 32 x 32 km"]
+[0.5687735080718994, 12.275596618652344, "Sensor Sensitivity 0.4 K/pixel"]
+[0.6190814971923828, 12.11005973815918, "Sensor Approx. Peak Sensitivity Altitude Unknown"]
+[6.258072376251221, 7.475624084472656, "Satellite Component Size Large"]
+[3.410254955291748, 10.639095306396484, "Traveling Wave Tube Amplifier Power 20 W"]
+[6.1624531745910645, 7.574065685272217, "Satellite Component Quantity 2"]
+[-0.8348120450973511, 11.575867652893066, "Detector Type Gamma-radiation"]
+[0.4685029685497284, 12.222298622131348, "Sensor Resolution 0.550 km"]
+[-0.8403260707855225, 11.678956031799316, "Detector Best Energy Resolution Temperature Below -60\u00ba C"]
+[-0.8398112654685974, 11.596582412719727, "Detector Gain Levels 16 discrete levels"]
+[-4.640945911407471, 8.280919075012207, "Mixed Signal ASIC Number of Parallel Readout Channels 128"]
+[-4.487988471984863, 8.268744468688965, "Mixed Signal ASIC Digital Registers 16 x 64 bit"]
+[-4.44354248046875, 8.321751594543457, "Mixed Signal ASIC Functional Blocks Current source to bias the pnCCD JFET, JFET preamplifier for pnCCD signal amplification, Programmable RC low pass for bandwidth limitation, Eight-fold correlated double sampling filter, Sample and hold stage, 128 to 1 multiplexer, Output buffer, On-chip digital sequencer (16 x 64 bit), Serial programming interface with LVDS, Option of integrated bias current DACs (digital analog converters)"]
+[1.441169261932373, -1.0774372816085815, "Satellite Body Structure Octagonal prism, 40 cm in diameter and a height of 25 cm"]
+[1.5461339950561523, -2.245328664779663, "Satellite Attitude Control Spin-stabilized at 5 rpm with the spin-axis normal to the orbital plane"]
+[2.083083152770996, -0.5091227889060974, "Satellite Power Average power of 10 W"]
+[2.0087828636169434, -1.3846993446350098, "Satellite Battery NiMH batteries of 2.4 Ah capacity"]
+[0.9441633820533752, -4.368282794952393, "Satellite Mass 12 kg"]
+[5.063767433166504, -2.326504707336426, "Satellite Design Life One year"]
+[2.6155529022216797, 14.290876388549805, "Optical Instrument Diameter 3 cm"]
+[2.6025853157043457, 14.283300399780273, "Optical Instrument Focal Length 12 cm"]
+[-1.0164963006973267, 7.779121398925781, "Device Aperture 35 mm"]
+[-1.0027869939804077, 7.816554069519043, "Device Dimensions 50 mm x 5 \u03bcm"]
+[2.6311635971069336, 13.44815444946289, "Optical Component Density 300 lines/mm"]
+[2.652214288711548, 14.265887260437012, "Optical Instrument Array Size 1024 x 1024 pixels"]
+[2.6148598194122314, 14.293336868286133, "Optical Instrument Pixel Size 24 \u03bcm x 24 \u03bcm"]
+[-3.806142807006836, 6.9142866134643555, "Data Collection Resolution 10 meters"]
+[3.9723451137542725, -2.79656720161438, "Satellite Imaging Period Contemporary"]
+[-3.3143389225006104, 6.895673751831055, "Cloud Computing Platform Open Platform Yes"]
+[-3.8029277324676514, 6.931879997253418, "Data Collection Cost-Effective Yes"]
+[-3.79008150100708, 6.925860404968262, "Data Collection Deployment Method From boats and ships"]
+[-1.5851455926895142, 1.4900487661361694, "Optical Data Relay Link Components Data electronics, laser and fiber amplifiers, computer, mechanisms, beam expander optics"]
+[-1.5840343236923218, 1.4634476900100708, "Optical Data Relay Link Voltage Conversion Yes"]
+[6.331149101257324, 7.4064459800720215, "Satellite Component Heat Transport System Collecting power to be dissipated externally to the LCT"]
+[2.758354663848877, -3.2675323486328125, "Communication Satellite Data Transmission Rate Up to 1.8 Gbit/s"]
+[2.900717258453369, -3.3671302795410156, "Communication Satellite Launch Date Days away from July 26, 2019"]
+[1.7421165704727173, -0.5682072639465332, "Imaging Satellites Resolution Up to 80 cm"]
+[1.7046663761138916, -0.5883501768112183, "Imaging Satellites Inclination 53 degrees"]
+[1.7191280126571655, -0.5611063241958618, "Imaging Satellites Resolution 50-centimeter"]
+[1.7344558238983154, -0.5925601124763489, "Imaging Satellites Resolution One-meter"]
+[1.889667272567749, 10.728376388549805, "Imaging Device Focal Length 2.5 cm"]
+[1.9272520542144775, 10.717238426208496, "Imaging Device Cant Angle 26\u00ba from the vertical"]
+[1.9089604616165161, 10.730334281921387, "Imaging Device Swath 2770 km"]
+[1.9412602186203003, 10.748064994812012, "Imaging Device Resolution at Nadir 1.5 km"]
+[1.9098268747329712, 10.720974922180176, "Imaging Device Resolution at Edge of Swath 5.5 km"]
+[2.646775245666504, 21.97565460205078, "Instrument Function Furnished cloud-height profiles"]
+[-3.8767313957214355, 7.922199249267578, "Data Storage Device Capacity Stored pictures of the entire northern hemisphere each day"]
+[3.1434755325317383, -1.4074057340621948, "Satellite Mission Prospecting for Lunar Water Ice"]
+[1.6769529581069946, -0.420767605304718, "Satellite Imaging System Imaging Capability 8 minutes per orbit"]
+[1.7134073972702026, -0.42073142528533936, "Satellite Imaging System Imaging Areas One 3000 km x 24 km continuous strip, two 100 km x 24 km stereo pairs, four 100 km x 24 km strips, or eight scenes"]
+[-0.1794070601463318, 9.486197471618652, "Inertial Reference Frame - -"]
+[-0.5576694011688232, 9.162087440490723, "Coordinate Frame - -"]
+[-0.5687388181686401, 9.131500244140625, "Coordinate Frame X-axis orientation to the station longitude for GOES -"]
+[-0.7347555160522461, 8.97299861907959, "Reference Frame Defined by the velocity vector and nadir -"]
+[-0.6598145365715027, 9.114727020263672, "Reference Frame Relative to the spacecraft body axis frame -"]
+[-0.5611132979393005, 9.142282485961914, "Coordinate Frame Ideal Geosynchronous orbit located at the GOES east or GOES west station longitude -"]
+[1.4204272031784058, -3.902728319168091, "Satellite Mass 495 kg"]
+[1.1627323627471924, -2.091416835784912, "Satellite Pointing Capability \u00b145\u00ba from nadir in any direction"]
+[1.086198091506958, -2.106222629547119, "Satellite Pointing Rate 1\u00ba/s (average)"]
+[1.0645848512649536, -1.9863401651382446, "Satellite Pointing Accuracy Better than 0.05\u00ba (3\u03c3)"]
+[-6.748112201690674, 10.021245002746582, "Antenna Data Rate 800 Mbit/s"]
+[2.092651128768921, -0.5121017098426819, "Satellite Power > 1300 W (SAP power), 400 W (payload power)"]
+[1.1659162044525146, -0.7775706648826599, "Satellite Size Approximately 2.5 m x 3.5 m x 3.2 m (deployed)"]
+[5.280756950378418, -2.1711738109588623, "Satellite Design Life 3 years (goal of 5 years of operations)"]
+[2.1884031295776367, 22.19801902770996, "Instrument Observation Field Tilt Capability \u00b140\u00ba"]
+[2.109241008758545, 22.677366256713867, "Instrument Spectral Band 0.42-0.50 \u00b5m"]
+[2.3871381282806396, 22.319515228271484, "Instrument Optical System Catadioptric Schmidt optical system (telescope)"]
+[2.060076951980591, 22.46457290649414, "Instrument Radiometric Absolute Accuracy \u00b110%"]
+[2.193443536758423, 22.506938934326172, "Instrument Onboard Calibration Accuracy \u00b15%"]
+[2.611520290374756, 22.44060707092285, "Instrument CCDs 5,000 and 10,000 detector elements"]
+[1.5264060497283936, 21.24198341369629, "Instrument Mass 250 kg"]
+[1.659029483795166, 23.19207000732422, "Instrument Power 300W"]
+[1.8096991777420044, 22.11862564086914, "Instrument Laser Pulses Distance 480 km"]
+[1.8182145357131958, 22.29031753540039, "Instrument Telescope Diameter 0.8 m"]
+[1.5482252836227417, 21.298551559448242, "Instrument Telescope Mass 20.8 kg"]
+[-0.01065409742295742, 10.337886810302734, "Alignment Monitoring and Control System Testing Duration Several weeks"]
+[2.750166893005371, 22.161930084228516, "Instrument Testing Location Temperature-controlled vacuum chamber at Goddard"]
+[4.264566898345947, -2.7866005897521973, "Satellite Orbit Period Order of 8-12 years"]
+[4.586060523986816, -2.6723897457122803, "Satellite Short-term Oscillations Period Six months"]
+[1.3761019706726074, -2.156031608581543, "Satellite Earth/Moon Stray Light ~106 times lower than in low-Earth orbit"]
+[2.6223862171173096, -2.6414740085601807, "Satellite Data Rates at Perigee ~100 Mbit s-1"]
+[4.094133377075195, -2.681551218032837, "Satellite Launch Windows 20 days per lunation"]
+[1.414320945739746, -2.0620710849761963, "Satellite Pointing Stability Excellent"]
+[3.049663543701172, -1.9929053783416748, "Satellite Operations Single 4 hr downlink & repoint every 2 weeks"]
+[4.930110931396484, -2.455585241317749, "Satellite Lifetime Several decades above GEO (>6.6 RE)"]
+[1.8841506242752075, 10.741265296936035, "Imaging Device Imaging Time Dawn to dusk throughout the day"]
+[-1.935265302658081, 8.105929374694824, "System Cost Less than previous constellation cost"]
+[6.382295608520508, 7.357828617095947, "Satellite Component Resolution 30 cm"]
+[-0.5356859564781189, 1.2308387756347656, "Satellite Orbit Apogee 804.6 km"]
+[-0.5374140739440918, 1.2364497184753418, "Satellite Orbit Perigee 789.0 km"]
+[-0.542322039604187, 1.2396705150604248, "Satellite Orbit Orbital Period 100.8 min"]
+[-0.5358152985572815, 1.2420783042907715, "Satellite Orbit Ground Repeat Cycle 41 days"]
+[-5.239073753356934, 7.7752509117126465, "Communication System AVNIR (M) Data Rate 60 Mbit/s"]
+[-5.1088762283325195, 7.721469402313232, "Communication System AVNIR (P) Data Rate 60 Mbit/s"]
+[-5.18572473526001, 7.781562328338623, "Communication System OCTS Data Rate 3.0 Mbit/s"]
+[-5.217803478240967, 7.82500696182251, "Communication System Polder Data Rate 0.882 Mbit/s"]
+[-5.191856861114502, 7.781455039978027, "Communication System IMG Data Rate 0.9 Mbit/s"]
+[-5.180126190185547, 7.777127265930176, "Communication System ILAS Data Rate 0.517 Mbit/s"]
+[-5.234304904937744, 7.771203517913818, "Communication System NSCAT Data Rate 2.9 kbit/s"]
+[-5.2501983642578125, 7.761044025421143, "Communication System TOMS Data Rate 0.7 kbit/s"]
+[-5.268780708312988, 7.983660697937012, "Communication System Uplink Frequency 2.0 GHz"]
+[-5.337859630584717, 8.05816650390625, "Communication System Downlink Frequency 2.2 GHz"]
+[-5.224822998046875, 7.8182172775268555, "Communication System Command Bit Rate 500 bit/s"]
+[2.021395444869995, -1.6123549938201904, "Satellite Acquisition Modes Snapshot mode (10 km x 10 km), StripMap mode, Skew mode"]
+[4.24484920501709, -2.82918381690979, "Satellite Acquisition Request Acceptance Time Until 30 minutes before uplink"]
+[2.842376232147217, -1.8333643674850464, "Satellite Operator Action Nominally no operator action is required"]
+[2.831860065460205, -1.9603813886642456, "Satellite High-energy source Unknown"]
+[2.5702319145202637, -1.4802290201187134, "Satellite X-ray emission source First identified in the 1970s"]
+[2.5891056060791016, -1.5551995038986206, "Satellite X-ray emission source Detected"]
+[2.5546882152557373, -1.5292930603027344, "Satellite X-ray emission source Detected"]
+[2.5829036235809326, -1.550140619277954, "Satellite X-ray emission source Realized it was the same object as this likely pulsar"]
+[2.977085828781128, -1.3767489194869995, "Satellite Mission Gravity Recovery and Climate Experiment Follow-On"]
+[-0.9528183341026306, 9.836240768432617, "Rocket Launch Date Early 2018"]
+[-1.3676502704620361, 6.075283527374268, "Company Number of Satellites 5"]
+[2.9536385536193848, 22.334228515625, "Instrument Affiliation CEA (Commissariat Energie Atomique - or the Atomic Energy Commission of France) + Tohoku University and Riken University (Japan)"]
+[2.895771026611328, 21.999618530273438, "Instrument Objectives To identify and characterize the TLEs (sprites, halos, elves, etc.), to locate the source regions of TLEs over the world, to identify and characterize the strongest lightning flashes, and to trigger other TARANIS instruments which may point out associated events"]
+[2.4111316204071045, 22.555566787719727, "Instrument Quantity 2 MicroCameras"]
+[2.350787401199341, 22.525876998901367, "Instrument Quantity 4 photometers"]
+[-2.14115571975708, 2.891643762588501, "Observatory Gravitational Wave Detection Low-frequency"]
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+[-2.1141960620880127, 2.942538261413574, "Observatory Cosmic Horizon Expands"]
+[-2.152235507965088, 2.9092462062835693, "Observatory Structure Mapping First hundred million years of the history of the Universe"]
+[-1.9163331985473633, 14.86758804321289, "Radiometer Instrument Objective Measure the temperature and humidity profiles"]
+[-1.9718255996704102, 14.830248832702637, "Radiometer Instrument Ground Resolution 10 km"]
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+[3.0414505004882812, 22.79985237121582, "Instrument Unknown Unknown"]
+[2.9881081581115723, -2.094963312149048, "Satellite Unknown Unknown"]
+[0.029206516221165657, 13.435503005981445, "Metrology System Quantity 1"]
+[0.02639499120414257, 13.447467803955078, "Metrology System Quantity 8+8"]
+[-5.237332344055176, 7.936065673828125, "Communication System Quantity 2 x Rx-Tx + 4 x antennas"]
+[-0.09972820430994034, 9.210090637207031, "Navigation System Quantity 2 x receivers + 2 x Antennas"]
+[0.5570844411849976, 9.44130802154541, "Attitude Determination and Control System Quantity 3 x Optical Heads + 2 x electronics"]
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+[0.49530765414237976, 9.472501754760742, "Attitude Determination and Control System Quantity Two 3-axes Inertial Rate Sensors"]
+[-1.5908533334732056, 9.672941207885742, "Propulsion System Quantity 2 x 8 x 1N Monopropellant, 2 x 12 x 10 mN Cold Gas"]
+[0.5212234258651733, 9.46463394165039, "Attitude Determination and Control System Quantity Pyramid of 4 units"]
+[-7.542248725891113, 5.848897933959961, "Camera Housing Material Titanium"]
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+[-7.548065185546875, 5.906441688537598, "Camera Surrounding Temperature +20\u00baC"]
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+[3.744893789291382, 17.734195709228516, "Payload Vibration Isolation >20 dB"]
+[3.744028091430664, 17.705821990966797, "Payload Vibration Suppression >20 dB"]
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+[3.7344679832458496, 17.70987892150879, "Payload Steering Rate 2 Hz"]
+[-0.34117230772972107, 6.600195407867432, "Test Bed Components MDIM (Meteoroid and Debris Impact Monitor) and the Meteoroid Impact Sensor of BMDO"]
+[-0.6653605699539185, 8.447998046875, "Structural Component Thickness 30 mm"]
+[-0.5779028534889221, 8.312142372131348, "Structural Component Material Machined aluminum"]
+[-0.7390435338020325, 8.388059616088867, "Structural Component Mounts ISS deployment specific mounts"]
+[-0.686884880065918, 8.441444396972656, "Structural Component Revert Thickness Thicker"]
+[2.6668293476104736, -1.322157382965088, "Satellite Data Collection During and after the eruption"]
+[2.655665874481201, -1.4522101879119873, "Satellite Data Sharing With colleagues around the world, including disaster response agencies"]
+[3.2203171253204346, -1.5169155597686768, "Satellite Mission Type Non-EO"]
+[5.095616340637207, -3.981609344482422, "Satellite Launch Date 2024"]
+[5.048042297363281, -4.096287727355957, "Satellite End of Life Date 2026"]
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+[5.078100681304932, -3.935865640640259, "Satellite Launch Date 2024"]
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+[-0.8395889401435852, 12.708828926086426, "Standard Radiation Environment Monitor Manufacturer Contraves"]
+[-0.8337010741233826, 12.675514221191406, "Standard Radiation Environment Monitor URL http://www.oerlikon.com/ecomaXL/get_blob.php?name=SREM_Brochure&download=1"]
+[4.922530174255371, -4.311845302581787, "Satellite Groundwater Storage Measurement Date March 29, 2021"]
+[4.815950870513916, -4.051570415496826, "Satellite Groundwater Storage Comparison Period 1948-2010"]
+[-0.6765215992927551, 5.068538665771484, "Country Lowest Water Storage Levels Timeframe 15 years"]
+[-0.6904734373092651, 5.090610980987549, "Country Precipitation Deficit 48 percent lower than the average for 1981-2010"]
+[2.7190284729003906, -1.180024266242981, "Satellite Objective Retrieve the atmosphere column-averaged CO2 dry air mole fraction (XCO2) with precisions of 1% (4 ppm) on national and global scales"]
+[2.749340295791626, -1.0975735187530518, "Satellite Scientific Goal Improve the understanding on the global CO2 distribution and its contribution to the climate change, and also to monitor the CO2 variation on seasonal time scales"]
+[-4.8800201416015625, 9.720991134643555, "Test Receiver Receiver Type Dual-mode receiver"]
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+[-4.844606399536133, 9.691754341125488, "Test Receiver Manufacturer NovAtel Inc."]
+[-5.033387660980225, 2.8672590255737305, "Space-based Telescopes Mission Date Aug. 10-15, 2013"]
+[-5.067217826843262, 2.875901460647583, "Space-based Telescopes URL http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=2991&context=smallsat"]
+[-5.125503063201904, 2.879185676574707, "Space-based Telescopes URL of presentation http://digitalcommons.usu.edu/cgi/viewcontent.cgi?filename=0&article=2991&context=smallsat&type=additional"]
+[-6.6713337898254395, 9.937616348266602, "Antenna Number of Beams 126"]
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+[-6.706263542175293, 9.971598625183105, "Antenna Polarizations Both"]
+[-2.9858129024505615, 4.218371391296387, "Spacecraft Pointing Accuracy 20 arcseconds"]
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+[0.5021747350692749, 9.373047828674316, "Attitude Control System Pointing Accuracy < 5 arcsec"]
+[0.4656200110912323, 9.376731872558594, "Attitude Control System Actuation Three magnetic-torquer coils and four reaction wheels"]
+[-5.423982620239258, 8.102557182312012, "Communication System Frequency Band S-band"]
+[-4.704695224761963, 9.061580657958984, "Transceiver Manufacturer Vulcan Wireless"]
+[-4.704572677612305, 9.047733306884766, "Transceiver Safe Mode Uplink Data Rate 4 kbit/s"]
+[-4.711984157562256, 9.077524185180664, "Transceiver Safe Mode Downlink Data Rate 10 kbit/s"]
+[-4.699841022491455, 9.043377876281738, "Transceiver Nominal Mode Uplink Data Rate 32 kbit/s"]
+[-4.712992191314697, 9.06595230102539, "Transceiver Nominal Mode Downlink Data Rate 1 Mbit/s"]
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+[-0.9125142097473145, 11.616364479064941, "Detection Algorithm Operation Detects targets with a high probability of detection while allowing a rather large number of false alarms"]
+[-0.8904528021812439, 11.541394233703613, "Detection Algorithm Operation Uses an adaptive nonparametric CFAR detection scheme that does not involve the theoretical modeling of clutter statistics"]
+[2.2444047927856445, -1.3875881433486938, "Satellite Imagery Collection 80 million km2"]
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+[-0.744209349155426, 12.654631614685059, "Space Radiation Monitor Parameters Measured Total Ionization Doze (TID), Single Event Upsets (SEUs), Single Event Latchups (SELs), HEH fluence"]
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+[-5.243722438812256, 7.483977794647217, "File Transfer Protocol Supported Links One-way and two-way"]
+[-5.293290138244629, 7.678014755249023, "Network Time Protocol Functionality Maintain the processor clock and provide accurate time stamps"]
+[-5.231041431427002, 7.6000471115112305, "Network Time Protocol Hardware Simple PC104 computer clock, no thermal control, no 1 PPS source"]
+[0.7175950407981873, -1.1506775617599487, "Satellite Altitude 368 km"]
+[2.083991765975952, -2.5822103023529053, "Satellite RCS Reversely for NDO tracking 4 times"]
+[0.8864372968673706, -1.3711458444595337, "Satellite Atmospheric Drag Estimated to be greater than the actual one"]
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+[6.251004695892334, 7.483639717102051, "Satellite Component Pixel Size Requirement Small"]
+[6.327349662780762, 7.413033485412598, "Satellite Component Signal Requirement Must be enough"]
+[6.2930474281311035, 7.4480671882629395, "Satellite Component Blur Requirement Must be kept in bounds"]
+[5.2792205810546875, -4.398045539855957, "Satellite Launch Date December 2016"]
+[4.9508514404296875, -4.209200859069824, "Satellite Calibration Completion Date Summer of 2017"]
+[2.7221410274505615, -1.5181431770324707, "Satellite XCO2 Retrieval Algorithm IAPCAS"]
+[-3.1201164722442627, 7.48453950881958, "Algorithm Purpose Application of TanSat XCO2 Retrieval Algorithm in GOSAT Observations"]
+[5.133090019226074, -4.315473556518555, "Satellite XCO2 Maps Date April and July 2017"]
+[-3.668440818786621, 8.04728889465332, "Solid-State Recorder Capacity 64 Gbit"]
+[-5.63166618347168, 8.180953025817871, "Communication Band Downlink Rate 60 Mbit/s"]
+[1.781571388244629, 6.865718841552734, "Communication Device TC Rate 20 kbit/s"]
+[1.768607258796692, 6.879851818084717, "Communication Device TM Rate 25-384 kbit/s"]
+[14.65427017211914, 7.782218933105469, "Nanosatellite Mass Approximately 10 kg"]
+[14.461557388305664, 7.7515974044799805, "Nanosatellite Orbit Altitude Approximately 550 km"]
+[-0.8978782296180725, -10.05384349822998, "Constellation Orbit Altitude Approximately 500 km"]
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+[2.14365816116333, 22.273923873901367, "Instrument Scan Width 144\u00ba"]
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+[2.7548511028289795, 22.39046287536621, "Instrument Data Transmission Asynchronous"]
+[-1.1502723693847656, 7.202944755554199, "Front Door Assembly Function Protect the instrument against dust particles"]
+[-1.1612976789474487, 7.03176212310791, "Front Door Assembly Operation Several shot closing/opening of the entrance aperture"]
+[-1.1078187227249146, 7.223660945892334, "Front Door Assembly Redundancy One-shot wax actuator"]
+[-13.735173225402832, -2.333543300628662, "X-ray Telescope Survey Date December 9, 2020"]
+[-13.881379127502441, -2.2428910732269287, "X-ray Telescope Survey Map Feature Huge circular structure of hot gas below the plane of the Milky Way"]
+[-2.5539727210998535, 11.859113693237305, "Optical Imager Image Taking Condition Nanosatellite\u2019s view must not be obstructed by the Earth or moon"]
+[-2.416447639465332, 12.112293243408203, "Optical Imager Sun Constraint The sun constraint shown in Figure 10"]
+[-1.7959659099578857, 8.777456283569336, "Control Box Function Command & control of the complete instrument, image data processing"]
+[-1.7101680040359497, 8.775134086608887, "Control Box Interface Handling Towards the spacecraft, housekeeping data acquisition, automatic image data acquisition & processing, execution of autonomous measurement sequences"]
+[0.5389969944953918, 12.156523704528809, "Sensing Method Sensitivity Few nrad/\u221aHz"]
+[2.660076379776001, 14.210860252380371, "Optical Bench Rigidly Mounted Yes"]
+[-1.002138614654541, 7.7282609939575195, "Device Directly Controlled by and only depends on the steering mirror The angle of the local oscillator beam w.r.t. the optical bench"]
+[-1.3199450969696045, 6.896735668182373, "Technology Optimization Contributions Size, mass, and power"]
+[-3.043653726577759, 15.076208114624023, "Microwave Monolithic Integrated Circuit Design and Production Location India"]
+[-2.2983906269073486, 7.435390949249268, "On-Board Computer Architecture ERC32 PM"]
+[3.698024272918701, 17.718164443969727, "Payload Data Handling System Data Compression From 1.3 Gbit/s to 450 Mbit/s"]
+[1.0264663696289062, -4.407154560089111, "Satellite Mass ~ 1200 kg"]
+[1.5235044956207275, 21.240278244018555, "Instrument Mass 275 kg"]
+[3.7596774101257324, 17.73232078552246, "Payload Mass 35 kg"]
+[-2.2067275047302246, 4.060628414154053, "Hydrazine Mass 80 kg"]
+[2.083991289138794, -0.5605411529541016, "Satellite Power 1250 W max"]
+[1.6513006687164307, 23.170568466186523, "Instrument Power 170 W"]
+[3.7360401153564453, 17.717670440673828, "Payload Power < 100 W"]
+[5.185183525085449, -2.2654917240142822, "Satellite Design Life 7.25 years"]
+[-2.3823671340942383, 4.079204559326172, "Hydrazine Operational Life 12 years"]
+[-3.8363466262817383, 7.903790473937988, "Data Storage Data Storage Method Encrypted, digital format"]
+[-1.135817050933838, 4.482009410858154, "Ground Stations Data Relay Method Commercial communications satellites"]
+[5.384544372558594, -4.398880958557129, "Satellite First Launch Date September 11, 1976"]
+[4.37791109085083, -2.790595531463623, "Satellite Recovery Date A few months later"]
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+[-3.3499670028686523, 8.032001495361328, "Signal Processing Implementation On-board in real time and on the ground in the data processor"]
+[-5.007640361785889, 8.639623641967773, "Transmit/Receive Modules Peak Power >150W"]
+[-6.7416605949401855, 9.966767311096191, "Antennas Size One of the largest"]
+[-1.7038763761520386, 8.370250701904297, "Electronics Technology Cutting edge"]
+[-1.9016863107681274, 8.070560455322266, "System Requirement Demanding"]
+[0.6128817796707153, 9.357151985168457, "Attitude Determination and Control Subsystem Manufacturer Adcole Maryland Aerospace"]
+[0.7069944143295288, 9.293477058410645, "Attitude Determination and Control Subsystem Stabilization Three-axis"]
+[0.6696985960006714, 9.310064315795898, "Attitude Determination and Control Subsystem Pointing Control Better than a tenth of a degree"]
+[0.6984372138977051, 9.294950485229492, "Attitude Determination and Control Subsystem Pointing Solution Update Rate 10 Hz"]
+[0.5863434076309204, 12.028366088867188, "Sensor Mounting Opposite side of the spacecraft from the X-ray telescope's optics"]
+[5.229149341583252, -4.453531265258789, "Satellite Launch Date Dec 23, 2019"]
+[2.847119092941284, -1.058404803276062, "Satellite Purpose Monitor water resources, agriculture, urban growth, and land use, with a large focus on the preservation of the Amazon rainforest"]
+[-3.0931060314178467, 2.4233739376068115, "Mission Total Duration Over six hours"]
+[0.5814802646636963, -1.4590967893600464, "Satellite Orbit Altitude ~300 x 860 km"]
+[0.6449410319328308, -2.330779552459717, "Satellite Orbit Inclination ~28\u00ba"]
+[-3.0994961261749268, 2.4110913276672363, "Mission Second Deployment Batch Altitude 720 km"]
+[-3.1114110946655273, 2.484769344329834, "Mission Second Deployment Batch Inclination 24\u00ba"]
+[0.5730834007263184, -1.5229241847991943, "Satellite Initial Orbit Altitude 720 km"]
+[0.5448799133300781, -1.4975645542144775, "Satellite Final Orbit Altitude ~520-550 km"]
+[0.6836798787117004, -2.309648036956787, "Satellite Final Orbit Inclination 24\u00ba"]
+[2.6087348461151123, -1.772011399269104, "Satellite Flight Selection NASA's CubeSat Launch Initiative (CSLI)"]
+[2.54801869392395, -1.8078022003173828, "Satellite Flight Selection NASA's CubeSat Launch Initiative (CSLI)"]
+[-0.21848389506340027, 6.994325637817383, "Investigations Lead Johns Hopkins University Applied Physics Laboratory"]
+[11.290711402893066, 5.503922939300537, "CubeSat University Aarhus University in Denmark"]
+[5.281521797180176, -4.2648844718933105, "Satellite Launch Date September 2021"]
+[2.070404529571533, -2.7813022136688232, "Satellite Number of Satellites 6"]
+[5.131974220275879, -3.9673190116882324, "Satellite Planned Launch Quarter First quarter of 2021"]
+[4.847452163696289, -3.534396171569824, "Satellite Second Launch Timing Approximately three to six months after the first launch"]
+[-2.288480758666992, 6.258977890014648, "Focal Plane Array Number of FPMs 6"]
+[-2.272817850112915, 6.249931335449219, "Focal Plane Array Number of Pan bands 2"]
+[-2.272167205810547, 6.268087387084961, "Focal Plane Array Number of MS bands 4"]
+[2.0262835025787354, -1.9662153720855713, "Satellite Focus Mechanism Active/passive thermal control mechanism"]
+[2.679347276687622, -2.013765573501587, "Satellite Data Transmission Subsystem PDTS"]
+[-0.8100154995918274, 11.586310386657715, "Detector Number of Elements 8"]
+[-0.8166043162345886, 11.56727123260498, "Detector Number of Detector Elements 4"]
+[-0.8188114166259766, 11.599669456481934, "Detector Type InSb (Indium Antimonide) photodiode"]
+[-0.8084635138511658, 11.547446250915527, "Detector Type Photo-conductive HgCdTe (Mercury Cadmium Telluride) detectors"]
+[-0.7885945439338684, 11.606780052185059, "Detector IGFOV 112 \u00b5rad"]
+[-0.8176355957984924, 11.597116470336914, "Detector IGFOV 224 \u00b5rad"]
+[-0.8211297392845154, 11.56221866607666, "Detector Pixel Size 4 km per side"]
+[-0.8561187386512756, 11.633980751037598, "Detector Pixel Size 8 km on a side"]
+[2.903672933578491, 22.330644607543945, "Instrument Major Contribution Provided by Germany"]
+[1.1412070989608765, -0.720156192779541, "Satellite Dimensions Approximately 3 m x 2 m x 0.8 m"]
+[0.9986922740936279, -4.367824554443359, "Satellite Mass Around 580 kg"]
+[14.476625442504883, 7.68690299987793, "Nanosatellite Development Purpose Educational tool and a technology testbed"]
+[14.521485328674316, 7.678346157073975, "Nanosatellite Radiation Environment Analysis Implemented"]
+[14.495490074157715, 7.698197364807129, "Nanosatellite Responsive Exploitation of Space Low-cost"]
+[-2.1520512104034424, 7.6085357666015625, "Avionics Board Processor 32 bit ARM Cortex-M3"]
+[-2.151324510574341, 7.622608661651611, "Avionics Board Memory Flash for in-flight reprogramming (dual redundant)"]
+[-2.1608223915100098, 7.579528331756592, "Avionics Board FPGA For flow-through error correction in case of a radiation upset on the memory"]
+[-2.205453872680664, 7.5772881507873535, "Avionics Board Data Storage MicroSD card"]
+[-2.161043167114258, 7.595822811126709, "Avionics Board Function Controls both magnetometers and samples connected sensors"]
+[-2.1620399951934814, 7.615302085876465, "Avionics Board Function Contains both sun and nadir sensors"]
+[-1.3134955167770386, 9.43680477142334, "N/A N/A N/A"]
+[-1.2740262746810913, 9.414030075073242, "N/A N/A N/A"]
+[2.836430549621582, -1.0535110235214233, "Satellite Purpose Measure changes in gravitational pull"]
+[2.6644985675811768, -1.7682843208312988, "Satellite Operation Orbit Earth and measure changes in mass below"]
+[2.6017322540283203, -2.0495259761810303, "Satellite Designation GOES-17"]
+[2.133829355239868, -1.992271900177002, "Satellite Operational Location GOES-West"]
+[1.6754846572875977, -1.575949788093567, "Satellite Coverage Area Western U.S., Alaska, Hawaii and the Pacific Ocean"]
+[2.3479676246643066, -1.424282193183899, "Satellite Instruments Earth-sensing, lightning-detecting, solar imaging and space weather monitoring instruments"]
+[2.407548666000366, -1.1882567405700684, "Satellite Data and Imagery Near-realtime on severe weather events such as thunderstorms, tornadoes, hurricanes and flash floods, as well as hazards like fog, aerosols, dust storms, volcanic eruptions and forest fires"]
+[2.6197307109832764, 13.508455276489258, "Optical Element Transmit Beam Waist Radius 2.5 mm"]
+[2.6401100158691406, 13.474756240844727, "Optical Element Receive Aperture Radius 4 mm"]
+[2.666738510131836, 13.47107982635498, "Optical Element Laser Power 25 mW"]
+[2.638831853866577, 13.46129322052002, "Optical Element Laser Wavelength 1064 nm"]
+[2.6415998935699463, 13.454497337341309, "Optical Element Satellite Separation 270 km"]
+[2.635573148727417, 13.464731216430664, "Optical Element Transmission Efficiency for Receive Path 97%"]
+[2.6425437927246094, 13.514598846435547, "Optical Element Transmit Efficiency 50%"]
+[2.6542725563049316, 13.470795631408691, "Optical Element Effective Received Power (a) ~200 pW"]
+[2.6522066593170166, 13.450119018554688, "Optical Element Effective Received Power (b) > 25 pW"]
+[2.0768792629241943, -1.2241110801696777, "Satellite Measurement Capability Trace individual waves"]
+[0.7888555526733398, -1.1969343423843384, "Satellite Bathymetry Visibility Up to 25 meters"]
+[1.8790826797485352, -1.1944094896316528, "Satellite Tree Height Measurement Global"]
+[5.230219841003418, -3.759505033493042, "Satellite Launch Year 2018"]
+[2.795949935913086, -1.0073856115341187, "Satellite Purpose Make detailed global elevation measurements, including over Earth's frozen regions"]
+[-0.3477896749973297, 8.279292106628418, "Ice Sheet Average Annual Ice Loss 200 gigatons"]
+[-0.3091851472854614, 8.232470512390137, "Ice Sheet Average Annual Ice Loss 118 gigatons"]
+[3.7577052116394043, 17.745807647705078, "Payload Data Loss Varies"]
+[3.7295968532562256, 17.710735321044922, "Payload Data Exceeded minimum requirements"]
+[0.09684310108423233, -4.040053844451904, "Satellite Platform Fault Tolerant Features SEE immunity, innovative error mitigation techniques, sophisticated three-level FDIR policy, redundancy on all critical functions"]
+[0.1229814738035202, -4.033222198486328, "Satellite Platform Data Handling Functionality On-board data handling functionality exploits the advantages of the reliable hot redundant CAN networking with built-in error detection mechanisms and a ruggedized and fail-safe harness"]
+[-6.99698543548584, 11.216038703918457, "Phased Array Type L-band Aperture Radar-2 Imagery Acquisition Date June 27, 2014"]
+[2.2690963745117188, 22.1922550201416, "Instrument Altitude Data Acquired by PRISM aboard ALOS-2"]
+[1.0534592866897583, 0.6801460981369019, "Advanced Land Observing Satellite Attitude Control System Status Shifted to the regular operation mode"]
+[2.021512031555176, -1.2211313247680664, "Satellite Measurement Capabilities Density, temperature, and winds of ions and neutrals"]
+[2.3899428844451904, 22.094493865966797, "Instrument Measurement Capabilities Neutral and ion density, temperature, wind and composition"]
+[0.5977380871772766, -1.5948878526687622, "Satellite Orbit Altitude 600 and 700 km"]
+[4.117732048034668, -2.457144260406494, "Satellite Repeat Intervals Six to 30 days"]
+[2.848740339279175, -1.9185556173324585, "Satellite Wavelengths Unknown"]
+[2.7133755683898926, -1.9469808340072632, "Satellite Ground Deformation Measurement Unknown"]
+[0.6444591283798218, 12.24459171295166, "Sensor Spectral Bands 5"]
+[0.4939480721950531, 12.235685348510742, "Sensor Spectral Range 0.755 - 14.29 \u00b5m"]
+[0.6966279745101929, 11.959752082824707, "Sensor Cross-track Coverage \u00b135\u00b0"]
+[0.556208074092865, 12.047586441040039, "Sensor Along-track Coverage \u00b140\u00b0"]
+[0.6484241485595703, 12.223604202270508, "Sensor Spectral Bands 5"]
+[0.4891107380390167, 12.266142845153809, "Sensor Spectral Range 0.333 - 1.675 \u00b5m"]
+[0.47974464297294617, 12.224982261657715, "Sensor Spatial Resolution 460 - 920 m at nadir"]
+[0.5276894569396973, 12.136772155761719, "Sensor Swath 1000 km"]
+[-6.771089553833008, 10.030622482299805, "Antenna Dimensions 2.1 m x 10.7 m"]
+[1.5253342390060425, -2.3184478282928467, "Satellite Stabilization 3-axis stabilized"]
+[0.6924801468849182, 9.263113021850586, "Attitude Control Subsystem Propulsion Hot gas jets"]
+[0.64606773853302, 9.305159568786621, "Attitude Control Subsystem Stabilization Gyro reference unit"]
+[0.5145412087440491, 9.535353660583496, "Attitude Sensor Accuracy Most accurate ones for three-dimensional orientation measurements"]
+[-3.3395872116088867, 7.4623823165893555, "Data Processing Purpose Combine measurements from several different sensors to obtain a better result"]
+[-3.3939859867095947, 7.497686386108398, "Data Processing Method Combining measurements from several different sensors"]
+[-3.297322988510132, 7.495790958404541, "Data Processing Output Estimate of the gyro angular rate bias"]
+[0.3833360970020294, 12.382379531860352, "Sensor Measurement Frequency High-frequency"]
+[6.31983757019043, 7.413207054138184, "Satellite Component Structure Triangular"]
+[6.357665538787842, 7.377392768859863, "Satellite Component Structure Cuboid"]
+[6.326479434967041, 7.411999702453613, "Satellite Component Location Inside the cuboid module"]
+[6.330671310424805, 7.4019951820373535, "Satellite Components Location Inside the cuboid module"]
+[6.294063091278076, 7.444308280944824, "Satellite Components Location On one of the shear webs and the exterior surface of the triangular bottom deck"]
+[6.304530143737793, 7.437360763549805, "Satellite Component Location Inside the main cylinder"]
+[6.3206095695495605, 7.416701316833496, "Satellite Component Location On a circular deck in a tetrahedral configuration"]
+[2.882235288619995, -2.044455051422119, "Satellite Operational Status Yes"]
+[2.7615649700164795, -1.1614196300506592, "Satellite Purpose Weather observation"]
+[2.76381254196167, -1.7534791231155396, "Satellite Operators Russian Federal Space Agency (Roskosmos) and Federal Service for Hydrometeorology and Environmental Monitoring of Russia (Roshydromet)"]
+[5.188037872314453, -4.4968953132629395, "Satellite Reentry Date April 26, 2002"]
+[1.2516746520996094, -1.3497673273086548, "Satellite Solar Maximum Double-peaked"]
+[2.4958837032318115, -2.2722597122192383, "Satellite Orbital Decay Occurred"]
+[2.8369576930999756, 22.763721466064453, "Instrument Operational Timelines Continuous Full Disk (CFD), Flex Mode (aka Storm Watch)"]
+[2.6841790676116943, 22.412490844726562, "Instrument Images Collected 5-minute Full Disk images"]
+[2.734757423400879, 22.392261505126953, "Instrument Images Collected 30-second Mesoscale, 5-minute CONUS, 15-minute Full Disk"]
+[2.3512494564056396, 22.670198440551758, "Instrument Space Look Observation Frequency At least every 30 seconds"]
+[2.455024242401123, 22.956954956054688, "Instrument Blackbody Observation Frequency At least every 15 minutes"]
+[2.353548049926758, 22.734893798828125, "Instrument Visible Stars Observation Frequency On average at least every 100 s"]
+[2.3441100120544434, 22.733739852905273, "Instrument IR Stars Observation Frequency On average at least every 300 s"]
+[-1.1688711643218994, 3.056399345397949, "Celestial Object Material Consumption Rate Phenomenal"]
+[-1.16356360912323, 3.0643796920776367, "Celestial Object X-ray Blocking Property Acts like lead paneling"]
+[0.7060796618461609, -4.144720077514648, "Satellite Launch Mass ~4,990 kg"]
+[1.6379611492156982, -2.2472774982452393, "Satellite Orbit Geostationary orbit of 35,786 km above Earth"]
+[5.474628448486328, -4.505896091461182, "Satellite Launch Date March 1, 2018"]
+[2.6850624084472656, -2.387423276901245, "Satellite Launch Vehicle Atlas V 541 rocket"]
+[2.5533556938171387, 22.784616470336914, "Instrument Threshold-to-Noise Ratio Unknown"]
+[2.3894245624542236, 22.66735076904297, "Instrument Total Noise Varies by several counts over small spatial scales"]
+[2.4816386699676514, 22.753271102905273, "Instrument Global Detection Threshold 25 counts"]
+[2.3027565479278564, 22.786928176879883, "Instrument False Event Rate Below 100 events/s"]
+[2.531780958175659, 13.898725509643555, "Optical Filter SRF (Solar Rejection Filter) Spectral Width ~30 nm FWHM"]
+[2.5556938648223877, 13.9666166305542, "Optical Filter SBF (Solar Blocking Filter) Spectral Width ~3 nm FWHM"]
+[2.5233497619628906, 14.0490140914917, "Optical Filter NBF (Narrow Band Filter) Spectral Width ~1 nm FWHM"]
+[2.7202064990997314, 22.895156860351562, "Instrument Frame Rate Unknown"]
+[2.9574532508850098, 22.78995704650879, "Instrument CCD Well Depth Unknown"]
+[0.6800141334533691, -4.125722408294678, "Satellite Launch Mass 2350 kg"]
+[0.7329937815666199, -4.159494876861572, "Satellite Launch Mass 2480 kg"]
+[4.427797317504883, -2.5581295490264893, "Satellite Earth-to-Moon Cruise Time 12 days"]
+[4.38286828994751, -2.61899995803833, "Satellite Earth-to-Moon Cruise Time 5 days"]
+[0.6126998066902161, -1.5203968286514282, "Satellite Lunar Working Orbit 200 km x 200 km"]
+[0.5552862286567688, -1.5732134580612183, "Satellite Lunar Working Orbit 100 km x 100 km"]
+[1.5103715658187866, -1.1525462865829468, "Satellite Spatial Resolution 120 m"]
+[1.4827542304992676, -1.1573339700698853, "Satellite Spatial Resolution 7 m ( 100 km altitude) 1.3 m ( 15 km altitude)"]
+[2.629948854446411, -2.1195921897888184, "Satellite TT&C S-band"]
+[2.498884439468384, -2.22607421875, "Satellite TT&C S -band, X-band"]
+[3.0859451293945312, -1.647607684135437, "Satellite Extended Mission Crash into the Moon surface"]
+[3.103900909423828, -1.5984501838684082, "Satellite Extended Mission Earth-Sun L2 mission followed by a deep-space mission"]
+[-1.3931434154510498, 8.614289283752441, "Electronic Component Number of Active Modules (Flash) 2"]
+[-1.3710225820541382, 8.581768989562988, "Electronic Component Number of Active Modules (SDRAM) 10"]
+[-1.3599799871444702, 8.628671646118164, "Electronic Component Data Retention Mode Function Store user data and refresh and scrub for error detection and correction"]
+[-4.7457194328308105, 9.291775703430176, "Transmitter Wavelength 830 nm"]
+[-4.732277870178223, 9.248350143432617, "Transmitter Output Power 1.5 W"]
+[-4.736374378204346, 9.240449905395508, "Transmitter Beam Divergence 1 mrad"]
+[-0.9805145859718323, 7.798905372619629, "Device Diameter 8 mm"]
+[-1.0293623208999634, 7.70334529876709, "Device Mass 3 kg"]
+[-0.9915016293525696, 7.730209827423096, "Device Power Consumption 4 W"]
+[-1.1530252695083618, 4.4513936042785645, "Ground Station Diameter 100 cm"]
+[-1.1403653621673584, 4.472078323364258, "Ground Station FOV \u00b11.5\u00ba"]
+[-5.455355644226074, 7.680483341217041, "Communication Data Rate 100 Mbit/s"]
+[-5.466447830200195, 7.80518102645874, "Communication Bit Rate Error < 10 -6"]
+[-5.426794528961182, 7.811337471008301, "Communication Signal Format NRZ (Non-Return Zero)"]
+[-5.489260196685791, 7.830745220184326, "Communication Modulation IM/DD (Intensity Modulation / Direct Detection)"]
+[6.265716075897217, 7.458477020263672, "Satellite Component Mass 32 kg"]
+[6.396610736846924, 7.3436150550842285, "Satellite Component Volume 0.8 m x 0.5 m x 0.25 m"]
+[6.306762218475342, 7.433826446533203, "Satellite Component Power Consumption 50 W"]
+[6.311568260192871, 7.430056095123291, "Satellite Component Data Quantization 12 bit"]
+[6.316223621368408, 7.4290242195129395, "Satellite Component Data Rate 883 kbit/s"]
+[6.5146942138671875, 7.257578372955322, "Satellite Component FOV (Field of View) \u00b1 43\u00ba along track; \u00b1 51\u00ba cross track"]
+[6.316009044647217, 7.422814846038818, "Satellite Component Swath Width 2400 km"]
+[6.3740410804748535, 7.369812965393066, "Satellite Component Ground Resolution 6 km x 7 km"]
+[-4.57806396484375, -3.07775616645813, "Exoplanet Size Three times Earth\u2019s size"]
+[-4.579225063323975, -3.106107234954834, "Exoplanet Orbital Period 10 days"]
+[-4.564274787902832, -3.0783705711364746, "Exoplanets Size A little over four times larger than Earth"]
+[-4.581858158111572, -3.110517740249634, "Exoplanets Orbital Period Exceeding 17 days"]
+[-4.56887149810791, -3.0851633548736572, "Exoplanet Size About twice Earth\u2019s size"]
+[-4.578303337097168, -3.1042723655700684, "Exoplanet Orbital Period 13 hours"]
+[-4.5700907707214355, -3.095100164413452, "Exoplanet UV Light Intensity 400 times more than Earth"]
+[-4.565629959106445, -3.0916824340820312, "Exoplanet UV Light Intensity Around 22,000 times more than Earth"]
+[7.252683639526367, 12.463241577148438, "Spacecraft Instrument System Control Module (SCM) 1 unit"]
+[7.292601108551025, 12.438204765319824, "Spacecraft Instrument Test Modules (TM) 5 units"]
+[7.312183856964111, 12.460813522338867, "Spacecraft Instrument Test Modules (TM) LEO environmental monitor module, a \u201dram\u201d (direction in face of flight) calorimeter module, a \u201dwake\u201d (direction at the rear of flight) calorimeter module, a Temperature-controlled Quartz Crystal Microbalance (TQCM)/actinometer module, and a solar photovoltaic module"]
+[-6.768270969390869, 10.02537727355957, "Antenna Size 9.9 m (azimuth) x 2.9 m (elevation)"]
+[-6.736713409423828, 10.014708518981934, "Antenna Number of Radiation Elements 1,080"]
+[-6.7200026512146, 9.985630989074707, "Antenna Number of TRMs 180"]
+[-6.815659999847412, 9.936841011047363, "Antenna Peak Radiation Power 3,300 W with three panels for Spotlight mode and Ultra-Fine mode, or 5,100 W with full aperture for High sensitive mode, Fine mode and ScanSAR mode"]
+[-6.741272449493408, 10.031137466430664, "Antenna Number of Antenna Partitions in Receive 2"]
+[6.405342102050781, 7.471591949462891, "Satellite Component Pointing Accuracy 0.5\u00ba in roll, pitch and yaw"]
+[6.337801933288574, 7.410887241363525, "Satellite Component Telemetered Data Accuracy 0.2\u00ba in all axes"]
+[6.382324695587158, 7.368069171905518, "Satellite Component Function Provide pitch and roll references viewing the Earth's horizon and pitch and roll fine control"]
+[0.4293234944343567, 9.385475158691406, "Attitude Control Method Function Maintain yaw attitude"]
+[0.5921779870986938, 11.98837661743164, "Sensor Function Determine accurately the yaw orientation"]
+[-8.144648551940918, 8.823497772216797, "Electrical Power Subsystem Power Output 28 \u00b14 VDC"]
+[-8.16597843170166, 8.819583892822266, "Electrical Power Subsystem Design Philosophy Provide functional redundancy"]
+[1.3479278087615967, -2.079301118850708, "Satellite Fine Pointing Control Detect 55 Cancri e via the transit method"]
+[1.2329468727111816, -0.9361245632171631, "Satellite Telescope Size 2.4-inch (6-centimeter)"]
+[1.23681640625, -0.9371017217636108, "Satellite Telescope Size 5.9-inch (15-centimeter)"]
+[-4.562467098236084, -3.0835607051849365, "Exoplanet Light Blocking 0.04% of its host star's light"]
+[-1.3232311010360718, 6.864829063415527, "Technology Development Pre-developed by ESA, NASA and the LISA consortium of ESA member states"]
+[-1.3105719089508057, 6.8662238121032715, "Technology Development Pre-developed by ESA, NASA and the LISA consortium of ESA member states"]
+[-1.2929657697677612, 6.835265636444092, "Technology Development Pre-developed by ESA, NASA and the LISA consortium of ESA member states"]
+[0.55550616979599, 12.10928726196289, "Sensor Development Pre-developed by ESA, NASA and the LISA consortium of ESA member states"]
+[5.190308570861816, -4.597416877746582, "Satellite Launch Date Dec. 18, 2004"]
+[3.048910140991211, -2.255314350128174, "Satellite Launch Mass Unknown"]
+[0.6610329747200012, -4.117284297943115, "Satellite Launch Mass 4200 kg"]
+[16.92038917541504, 6.801735877990723, "Microsatellites Objective Analysis of the electromagnetic environment (military use)"]
+[16.91193389892578, 6.803195476531982, "Microsatellites Bus Myriade microsatellite bus of CNES"]
+[0.9731881022453308, 9.152423858642578, "Attitude and Orbit Control System Stabilization 3-axis"]
+[1.00836980342865, 9.145397186279297, "Attitude and Orbit Control System Short Term Stability 56 \u00b5rad"]
+[0.9739420413970947, 9.170391082763672, "Attitude and Orbit Control System Long Term Stability 112 \u00b5rad"]
+[0.7226706743240356, 11.950019836425781, "Sensors Purpose Provide higher accuracies for image processing"]
+[0.8199223279953003, 11.839662551879883, "Sensors Purpose Used for initial attitude acquisitions and other maneuvers"]
+[-5.715904235839844, 9.324441909790039, "Radio RSSI Parameter Value"]
+[5.431070804595947, -4.48902702331543, "Satellite Launch Date April 28, 2008"]
+[1.7277753353118896, -1.6348401308059692, "Satellite Uplink Margins Sufficient"]
+[2.5798261165618896, -1.8526498079299927, "Satellite Operating System CANOE"]
+[2.4787864685058594, -1.8935482501983643, "Satellite Bootloader-1 (BL1) Pre-programmed EPROM"]
+[2.655064821243286, -1.9841021299362183, "Satellite Ground Station Contact Second pass after deployment"]
+[1.5126807689666748, 5.4229416847229, "Satellite Bus Mass Approximately 80 kg"]
+[1.5182825326919556, 5.417646408081055, "Satellite Bus Dimensions 52.4 cm by 52.4 cm by 62 cm"]
+[-2.396543264389038, 7.319504737854004, "Onboard Computer Data Rate 19.2kbps"]
+[1.7549834251403809, -2.0626885890960693, "Satellite Attitude Control System ST-16 star tracker, three reaction wheels, Smart Solar Panels"]
+[-3.053161382675171, 7.69713830947876, "Processing Unit Purpose Lower cost, more energy efficiency and longer battery life"]
+[2.6133997440338135, 14.293167114257812, "Optical Instrument Mirror Material Silicon Carbide"]
+[2.627570867538452, 14.31977367401123, "Optical Instrument Mirror Mounting Angle 45\u00b0"]
+[2.6362106800079346, 14.343116760253906, "Optical Instrument Swing Angle \u00b14.5\u00b0 (mechanical)"]
+[2.6621882915496826, 14.36444091796875, "Optical Instrument Field of Regard \u00b16\u00b0"]
+[2.6109371185302734, 14.368642807006836, "Optical Instrument Earth's Surface Angle from GEO 17.4\u00b0"]
+[2.6413381099700928, 14.31458568572998, "Optical Instrument Ground Distance per Step 8 km"]
+[0.6387315392494202, 12.017359733581543, "Sensor Integration Location INVAP facility in Bariloche, Argentina"]
+[-2.1550769805908203, 2.9030165672302246, "Observatory Environmental Testing Location INPE/LIT facility in Sao Jose dos Campos, Brazil"]
+[5.320346355438232, -4.481532573699951, "Satellite Launch Date July 2009"]
+[4.9535088539123535, -2.405702829360962, "Satellite Operational Lifetime 5 years"]
+[4.083334922790527, 13.93288803100586, "Advanced Topographic Laser Altimeter System Measurement Method Sending pulses of light to Earth\u2019s surface and measuring how long it takes individual photons to return to the satellite"]
+[4.081652641296387, 13.934369087219238, "Advanced Topographic Laser Altimeter System Measurement Accuracy Within a billionth of a second"]
+[1.645189881324768, -1.62716543674469, "Satellite Coverage More southern latitudes than ever before"]
+[2.4128706455230713, 23.391620635986328, "Instrument Power Cycle Frequency 4 times a second"]
+[-0.8911137580871582, 11.539383888244629, "Detector Mounting On a PCB (Printed Circuit Board) along with 4 operational amplifiers"]
+[-2.444089651107788, 8.817697525024414, "Converter Resolution 14 bit"]
+[-1.2199807167053223, 8.561062812805176, "Components Qualification Space qualified"]
+[3.626699209213257, 13.249765396118164, "Laser Background Measurement Make a background measurement 4 times a second"]
+[1.6884735822677612, 6.887683391571045, "Communication Device Uplink Power 32 dBm"]
+[1.7314330339431763, 6.916715145111084, "Communication Device Orbit Geostationary"]
+[1.6457842588424683, 6.959505558013916, "Communication Device Orbital Period 24 hours"]
+[-0.8074191212654114, 0.13103699684143066, "Satellite System Function Provide first responders with highly accurate locations"]
+[-5.88598108291626, 15.993075370788574, "Synthetic Aperture Radar Polarimetry Modes Single, dual, quad (full-pol.), compact (or hybrid)"]
+[-5.890419006347656, 15.998684883117676, "Synthetic Aperture Radar PRF of full-pol. mode Doubled as that of single/dual-pol."]
+[-5.915022850036621, 16.02853775024414, "Synthetic Aperture Radar Range Coverage of full-pol. in fine mode 30 km"]
+[-5.928228855133057, 16.014204025268555, "Synthetic Aperture Radar Range Coverage of single/dual-pol. in fine mode 70 km"]
+[-2.565997362136841, 8.355104446411133, "Capture Technology Use In space"]
+[-2.568608522415161, 8.336699485778809, "Capture Technology Use In space"]
+[-2.5619354248046875, 8.337507247924805, "Capture Technology Use In space"]
+[-1.9268133640289307, 8.120373725891113, "System Purpose Testing net technologies on the ground"]
+[-0.6394844055175781, 6.7465410232543945, "Study Purpose Examining attitude estimation and non-cooperative approach using a visual and infrared system"]
+[-0.679085910320282, 6.717606544494629, "Study Purpose Examined trade-offs for different ADR technologies, especially including flexible link capture systems"]
+[-0.07171259820461273, 9.511467933654785, "Vision-Based relative Navigation Development Status Currently being developed"]
+[-5.384616851806641, 8.809136390686035, "RF Communications Frequency Band S-band"]
+[-4.74070930480957, 9.267338752746582, "Transmitter Data Rate 800 Mbit/s"]
+[-4.750170707702637, 9.270112037658691, "Transmitter Modulation 16-QAM (Quadrature Amplitude Modulation)"]
+[-6.670579433441162, 9.994367599487305, "Antenna Pointing Mechanism Mass 4.4 kg"]
+[-6.659740447998047, 10.010262489318848, "Antenna Pointing Mechanism Pointing Accuracy Better than 0.1\u00ba"]
+[-6.678390026092529, 9.987467765808105, "Antenna Pointing Mechanism Maximum Slew Rate 4\u00ba/s"]
+[-6.6330742835998535, 9.969432830810547, "Antenna Pointing Mechanism Acceleration Rate 0.4\u00ba s-2"]
+[-7.573212623596191, 5.887086868286133, "Cameras Field of View 65\u00ba x 54 \u00ba"]
+[-7.553711414337158, 5.9094109535217285, "Cameras Field of View 17\u00ba x 14\u00ba"]
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+[0.046992283314466476, 9.226967811584473, "Pointing Control Device Control Loop Frequency 20 Hz"]
+[-5.379125595092773, 2.907418727874756, "Optical Telescope Assembly Estimated Total Conductance of Bipods 0.015 W/K"]
+[-3.098893880844116, 1.6975431442260742, "Satellite Mission Catalogue Content Confirmed and characterized planets in habitable zones with known mean densities, compositions, and evolutionary ages/stages"]
+[-3.110013246536255, 1.678369164466858, "Satellite Mission Target Earth-sized planets and super-Earths"]
+[-2.0630147457122803, 2.917513847351074, "Astrophysical Observatory Orbit Halo orbit around L2 Lagrange point"]
+[-1.1920894384384155, 4.465478897094727, "Ground Station Quantity 3"]
+[-14.146890640258789, -2.410287618637085, "X-ray Telescope Developer IKI RAN"]
+[-13.982954978942871, -2.300137758255005, "X-ray Telescope Developer Max Planck Institute for Extraterrestrial Physics (MPE) in Germany"]
+[-1.07750403881073, 4.516598224639893, "Ground Station Location Australia, Spain and Argentina"]
+[-2.568507432937622, 4.307230472564697, "Space Environmental Effects Experiment Purpose Researching and characterizing the MEO space weather effects on spacecraft electronics and materials"]
+[-3.152667999267578, 1.6996006965637207, "Satellite Mission Purpose Provide an important database for future designers of space missions intended to operate in the MEO environment"]
+[-3.1486589908599854, 1.7086011171340942, "Satellite Mission Technology Planning System Inc. (PSI) Network Data Acquisition System (NDAS)"]
+[1.836403727531433, 10.6920166015625, "Imaging Technology Field of View 21.2\u00b0 squared"]
+[1.8200745582580566, 10.704751968383789, "Imaging Technology Angular Resolution Coarser than Wolter optics"]
+[1.7765281200408936, 10.657833099365234, "Imaging Technology Angular Resolution Finer than MPO"]
+[7.336236000061035, 12.463337898254395, "Satellite Instrument Orbit Geostationary"]
+[7.285760402679443, 12.390719413757324, "Satellite Instrument Observation Frequency About every 30 minutes"]
+[7.289309024810791, 12.411438941955566, "Satellite Instrument Observation Range About 50 to 400 miles in altitude"]
+[-1.4173625707626343, 4.328326225280762, "Ground System TLE Update Frequency Twice per day"]
+[-1.4685027599334717, 4.333510875701904, "Ground System Elevation Angle for Downlink 90\u00ba"]
+[-3.204148292541504, 1.7746480703353882, "Mission Planning System Image Acquisition Order Acceptance Time Before AOS -30 minutes"]
+[-3.185936212539673, 1.8415309190750122, "Mission Planning System Product Delivery Time Within an hour from imagery acquisition"]
+[-0.48198315501213074, 5.859288692474365, "Unknown Unknown Unknown"]
+[2.028271436691284, 22.6324462890625, "Instrument Emission Wavelength 30.4 nm"]
+[1.9065725803375244, 22.836421966552734, "Instrument Emission Energy 40.8 eV"]
+[2.1005876064300537, 22.55531883239746, "Instrument Scattered Emission Wavelength 121.6 nm"]
+[2.077373743057251, 22.677074432373047, "Instrument Scattered Emission Energy 10.2 eV"]
+[2.7499477863311768, 22.27138328552246, "Instrument Background Due to energetic particles striking the detector"]
+[0.45191311836242676, 12.038558006286621, "Sensor Data Collection Method Sweeping perpendicular to the groundtrack"]
+[-0.6248728632926941, -0.006690697744488716, "Satellite Architecture Design Dual-spinner design"]
+[-1.6199806928634644, 1.4854869842529297, "Data Relay System Operational Date July 12, 2012"]
+[3.729198932647705, 17.706449508666992, "Payload Operational Date Oct.12-16, 2015"]
+[7.308578014373779, 12.439874649047852, "Satellite Instrument Data Processing Acquiring, processing, analyzing, archiving and distributing scientific data"]
+[-3.348257541656494, 7.3983988761901855, "Data Processing Segment Function Automatically retrieves raw downlink files of Aquarius science data from the CONAE database and processes this data into time-ordered salinity data files"]
+[1.5215938091278076, 21.2396183013916, "Instrument Mass 225 kg"]
+[1.6040174961090088, 23.238014221191406, "Instrument Power Consumption 270 W"]
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+[5.384857654571533, -4.273462295532227, "Satellite Launch Date 1982"]
+[2.166666269302368, -2.7533843517303467, "Satellite Number on Order for the Air Force 13"]
+[2.0598859786987305, -2.82210636138916, "Satellite Number of Long-life Follow-on Satellites 9"]
+[0.9225669503211975, -4.326930999755859, "Satellite Liftoff Mass 2,704 kg"]
+[0.04054269194602966, 13.395553588867188, "Metrology System Individual Focal Length 1600 mm"]
+[-0.04796003922820091, 13.447521209716797, "Metrology System Accuracy Requirement Within 50 \u00b5m"]
+[6.3860578536987305, 7.357602119445801, "Satellite Component Material Aluminum"]
+[1.052300214767456, 9.140835762023926, "Attitude & Orbit Control Subsystem Reaction Wheels Quantity 4"]
+[1.059265375137329, 9.136591911315918, "Attitude & Orbit Control Subsystem Reaction Wheels Capacity 0.12 Nms"]
+[1.0711381435394287, 9.132134437561035, "Attitude & Orbit Control Subsystem Hydrazine Tank Capacity 4.7 kg"]
+[-8.140983581542969, 8.824278831481934, "Electric Power Subsystem Solar Array Power 180 W EOL"]
+[-8.145174980163574, 8.823636054992676, "Electric Power Subsystem Li-ion Battery Capacity 15 Ah BOL"]
+[-2.234328508377075, 9.044037818908691, "Power & Control Distribution Unit On-board computer T805, 1 Gbit DRAM/EDAC, 8 Mbit Flash EEPROM"]
+[-2.2680556774139404, 9.070611000061035, "Power & Control Distribution Unit S-band transceivers Data Rate 20 kbit/s TC"]
+[-2.2403547763824463, 9.041662216186523, "Power & Control Distribution Unit S-band transceivers Data Rate 25-384 kbit/s TM"]
+[6.262744903564453, 7.4796295166015625, "Satellite Component X band downlink Data Rate 60 Mbit/s"]
+[6.325287818908691, 7.417932987213135, "Satellite Component Storage memory Capacity 64 to 79 Gbit BOL"]
+[0.6867957711219788, -4.125059604644775, "Satellite Launch Mass 116 kg"]
+[1.1331202983856201, -2.0636582374572754, "Satellite Agility \u00b130\u00ba roll in 90 s"]
+[1.3546401262283325, -1.3086670637130737, "Satellite Localization Performance 300 m CE90"]
+[-1.937915325164795, 6.882964134216309, "Software Function Process Satellite Derived Bathymetry data, assess accuracy, and output as .BAG files"]
+[-1.9828572273254395, 6.869527816772461, "Software Function Automatically extract seafloor depth measurements from ICESat-2 laser data"]
+[1.5905061960220337, -1.2012826204299927, "Satellite Green Laser Altimeter Accuracy Gauging seafloor depths down to 100 feet below the surface"]
+[2.4666829109191895, -1.2768501043319702, "Satellite Primary Design Polar ice elevation and tree canopy measurements"]
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+[1.4193171262741089, -1.043108582496643, "Satellite Target Size Smaller than 1 pixel in camera image"]
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+[-5.157236099243164, 7.82996940612793, "Communication Experiment Type Laser"]
+[0.5902664661407471, -1.451438307762146, "Satellite Orbit Altitude 19,000 to 24,000 kilometers"]
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+[3.7332711219787598, 17.713903427124023, "Payload Downlink Frequency Band 2226 MHz (S-band)"]
+[3.750462532043457, 17.710798263549805, "Payload Quantity 17"]
+[3.789924144744873, 17.757465362548828, "Payload Quantity 6"]
+[3.7415523529052734, 17.7080135345459, "Payload Quantity 2"]
+[-13.493147850036621, -2.006223440170288, "X-ray Observatory Observation Objective Study the supernova"]
+[-13.881476402282715, -2.2777392864227295, "Ultraluminous X-ray source Observation Duration 10 days"]
+[-13.810300827026367, -2.1870055198669434, "Ultraluminous X-ray source Observation Frequency Multiple times in quick succession"]
+[1.9174352884292603, 10.730069160461426, "Imaging Device Field of View 15 degrees"]
+[1.8938367366790771, 10.727371215820312, "Imaging Device Synchronization Accuracy 10 millionths of a second"]
+[1.896179437637329, 10.718423843383789, "Imaging Device Filter Optimized for the near-infrared LED light"]
+[-0.4217210114002228, 6.774657726287842, "Test Equipment Spacing 30 m intervals"]
+[-0.38066375255584717, 6.770564079284668, "Test Equipment Length 33-m long"]
+[2.172144889831543, -1.8403565883636475, "Satellite Form Factor 12U CubeSat"]
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+[0.08413506299257278, 4.653890132904053, "Volcano Elevation 1592 m"]
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+[-0.46592313051223755, 5.0131120681762695, "Caldera North to South 25 km"]
+[-0.48975497484207153, 5.052094459533691, "Caldera East to West 18 km"]
+[-1.619450569152832, 9.640473365783691, "Propulsion System Power Range 56-80 W"]
+[-1.6060755252838135, 9.683812141418457, "Propulsion System Voltage Range 28-37 V"]
+[-1.6301668882369995, 9.693219184875488, "Propulsion System Thrust 0.66-1.24 mN"]
+[-1.6162312030792236, 9.683097839355469, "Propulsion System Isp 1,400-2,640 s"]
+[-1.6148680448532104, 9.675432205200195, "Propulsion System \u0394V Capability 2.9 km/s"]
+[-3.617037296295166, 12.744874954223633, "Particle Detector Energy Range 0.5 to 350 GeV"]
+[-3.6251628398895264, 12.746627807617188, "Particle Detector Observation Fraction decreases with increasing energy from 0.5 to 10 GeV"]
+[-3.653938055038452, 12.737196922302246, "Particle Detector Observation Fraction increases steadily between 10 GeV to ~250 GeV"]
+[-3.660722255706787, 12.739715576171875, "Particle Detector Observation Slope of the positron fraction decreases by an order of magnitude from 20 to 250 GeV"]
+[-3.647226572036743, 12.755149841308594, "Particle Detector Observation Spectrum appears to flatten above 250 GeV"]
+[-1.3107682466506958, 9.445563316345215, "N/A N/A N/A"]
+[1.9777787923812866, 22.348312377929688, "Instrument Measurement Accuracy \u00b1 10 cm"]
+[2.017167568206787, 22.38166046142578, "Instrument Wave Height Measurement Accuracy \u00b1 10% or 0.5 m, whichever is greater"]
+[2.0635180473327637, 22.536514282226562, "Instrument Backscatter Coefficient Measurement Accuracy \u00b1 1.0 dB"]
+[3.1391453742980957, 22.94358253479004, "Instrument Status Unsuccessful"]
+[2.53006911277771, 22.852046966552734, "Instrument Monitoring Duration At least 30 days"]
+[3.582655429840088, 13.855966567993164, "Laser Ranging Interferometer Switch On Date July 2, 2018"]
+[3.5790529251098633, 13.854290008544922, "Laser Ranging Interferometer Purpose Precision distance measurements in space"]
+[3.6146914958953857, 13.86460018157959, "Laser Ranging Interferometer Management JPL and the Max Planck Institute for Gravitational Physics (Albert Einstein Institute)"]
+[-3.115081310272217, 4.264326095581055, "Spacecraft Design Constraint VBS mounted on the OSC"]
+[-3.0751352310180664, 4.370224475860596, "Spacecraft Maximum Fuel Budget Unknown"]
+[-3.120915651321411, 4.290929794311523, "Spacecraft Maximum Number of Admissible Thruster Firings Unknown"]
+[-3.061429977416992, 4.306422710418701, "Spacecraft Maximum Admissible Heat Load Unknown"]
+[-3.041900157928467, 4.033721446990967, "Spacecraft Non-cooperative Mode Operation Not during eclipses, when large shadows are cast on the CSC, or in the case specular reflections on the CSC cause the sunlight to mirror back to the OSC"]
+[-3.037214994430542, 4.223105430603027, "Spacecraft Maximum Angular Limit Away from Sun-pointing Direction Unknown"]
+[-3.043308734893799, 4.242984294891357, "Spacecraft Low Thrust Propulsion Requires advanced guidance techniques for hops"]
+[-3.1607582569122314, 4.2314887046813965, "Spacecraft Control Authority in Forced-motion Phases Limited"]
+[6.354725360870361, 7.380834102630615, "Satellite Component Manufacturer SI (Satrec Initiative Co. Ltd.)"]
+[-1.7221705913543701, 6.631809234619141, "Program Purpose Technology Transfer Program"]
+[-1.7139915227890015, 6.607527732849121, "Program Participants ~10 young engineers and scientists from UAE"]
+[-3.260065793991089, 5.429998397827148, "Launcher Anomaly Date January 25, 2018"]
+[-3.2593932151794434, 5.433656215667725, "Launch Vehicles Launch Campaigns Continuing"]
+[2.282597541809082, 22.14876365661621, "Instrument Measurement Changes in salinity"]
+[3.173197031021118, 22.968297958374023, "Instrument Status Fully operative"]
+[3.182699680328369, 22.985355377197266, "Instrument Status Fully operative"]
+[3.198045253753662, 22.9915771484375, "Instrument Status Fully operative"]
+[3.2054412364959717, 22.99510383605957, "Instrument Status Fully operative"]
+[-0.7388454079627991, 5.542572021484375, "Bridge Total Length 2,164 m"]
+[-0.7024365067481995, 5.511444091796875, "Bridge Length over the Bosporus 1,408 m"]
+[-0.7597430944442749, 5.524488925933838, "Bridge Tower Height (European side) 322 m"]
+[-0.7062098383903503, 5.5038981437683105, "Bridge Tower Height (Asian side) 318 m"]
+[-0.7128781080245972, 5.538639545440674, "Bridge Number of Highway Lanes 8"]
+[-0.7194702625274658, 5.529382705688477, "Bridge Number of Railway Lanes 2"]
+[-5.3461198806762695, 2.7567996978759766, "Telescope Delay Measurement 30,000 km"]
+[-1.179709792137146, 3.336491107940674, "Black Hole Weight 3 million Earths"]
+[-1.1217128038406372, 3.2983508110046387, "Supermassive Black Hole Weight 200 million times the mass of our Sun"]
+[-0.5306722521781921, 8.297730445861816, "Support Structure Purpose Ensure system rigidity and required first eigenfrequency of the COB"]
+[-0.4780660569667816, 8.320503234863281, "Support Structure Purpose Minimize the mechanical constraints resulting from temperature gradients"]
+[-0.5201485753059387, 8.288008689880371, "Support Structure Purpose Minimize the transfer of OBA deformations to the coronagraph structure"]
+[-0.5186034440994263, 8.289007186889648, "Support Structure Purpose Minimize the thermal conductive leaks between the COB and the OBA"]
+[-1.9333288669586182, 6.890924453735352, "Software Compatibility Model-Based Systems Engineering (MBSE) artifacts"]
+[-1.8667179346084595, 7.981846809387207, "System Model Tool Cameo Enterprise Architecture"]
+[-1.8491690158843994, 8.143333435058594, "Integrated System Model Function Define the spacecraft structure, model functionality, and requirements"]
+[-13.860719680786133, -2.012129306793213, "X-ray Telescope Energy Range > 25 keV"]
+[-13.692695617675781, -2.314845561981201, "X-ray Telescope Discovery Date Feb. 28, 2017"]
+[-13.785599708557129, -2.3073196411132812, "X-ray Telescope URL http://www.jpl.nasa.gov/news/news.php?feature=6760&utm_source=iContact&utm_medium=email&utm_campaign=NASAJPL&utm_content=daily20170228-2"]
+[2.1661765575408936, 22.57274055480957, "Instrument Imaging Wavelength Far ultraviolet light"]
+[2.3621089458465576, 22.229299545288086, "Instrument Observation Range Entire Western Hemisphere"]
+[2.8869171142578125, 21.950672149658203, "Instrument Purpose Track changes in the ionosphere\u2019s temperature, density and composition"]
+[3.6859774589538574, 22.965560913085938, "Instrument Operational Date July 1987"]
+[2.8069441318511963, 22.505205154418945, "Instrument DMSP Missions F-8, F-10, F-11, F-12, F-13, F-14, F-15"]
+[-2.0489134788513184, 12.623624801635742, "Solar Ultraviolet Imager Instrument Delivery Date Oct. 2013"]
+[-2.0060553550720215, 12.644073486328125, "Solar Ultraviolet Imager Integration Date 2014"]
+[-13.688094139099121, -2.0588340759277344, "Extreme Ultra Violet and X-ray Irradiance Sensor Not specified Not specified"]
+[1.7018760442733765, 6.945454120635986, "Communication Device Manufacturer Airbus subsidiary Tesat Spacecom"]
+[1.7633699178695679, 6.885983467102051, "Communication Device Data Relay More than 10,000 successful links to the European Union\u2019s Copernicus Sentinels-1 and -2"]
+[1.7518489360809326, 6.903386116027832, "Communication Device Data Relay Relaying in excess of 500 TB of the Earth observers\u2019 findings"]
+[1.669925570487976, 6.980685234069824, "Communication Device Integration Date March 2017"]
+[1.6530616283416748, 7.002403259277344, "Communication Device Number of Tests More than 90"]
+[1.635777235031128, 6.94813346862793, "Communication Device Test Type Thermal vacuum test"]
+[-0.9012220501899719, -10.019492149353027, "Satellite Constellation Image Revisit Rate Up to 15 times per day"]
+[-0.9500069618225098, -9.997544288635254, "Satellite Constellation Monitoring Capabilities High-agility point collects for monitoring targets and large-area collects for mapping missions"]
+[-0.9477874636650085, -10.004429817199707, "Satellite Constellation Mission Focus Vehicle navigation, Environmental sustainability, Global connectivity, Disaster response, National security"]
+[-4.253618240356445, 7.373989582061768, "Data Transmission Link Direction EDRS to LEO, LEO to EDRS, or bidirectional"]
+[-4.27495002746582, 7.41500997543335, "Data Transmission Link Speed Unknown"]
+[-2.119633674621582, 5.898527145385742, "Flight Operations Execution Time Unknown"]
+[-2.0649752616882324, 5.8633222579956055, "Flight Operations Execution Time Unknown"]
+[5.2851033210754395, -4.43195915222168, "Satellite Launch Date 15 December 2017"]
+[4.395174980163574, -3.361287832260132, "Satellite Launch Time 15:36 UTC"]
+[2.6271588802337646, -2.404696226119995, "Satellite Launch Vehicle SpaceX-13 Falcon 9FT"]
+[2.779066801071167, -2.2514500617980957, "Satellite Launch Site Cape Canaveral Air Force Station, SLC-40"]
+[-4.681811332702637, 9.064486503601074, "COTS Transceiver Frequency S-band"]
+[0.5951876044273376, -1.4591281414031982, "Satellite Orbit Altitude ~400 km"]
+[0.7582119703292847, -2.2092692852020264, "Satellite Orbit Inclination 51.6\u00b0"]
+[-0.27448031306266785, 10.17955207824707, "Tracking Device Nanosatellite CanX-2"]
+[14.474352836608887, 7.694282054901123, "Nanosatellite Orbit Operations Duration Two Years"]
+[-2.9879565238952637, 16.166555404663086, "Scatterometer Function Return estimates of backscatter power"]
+[-2.9823286533355713, 16.171113967895508, "Scatterometer Component Unknown Unknown"]
+[-2.98069429397583, 16.181718826293945, "Scatterometer Component Unknown Unknown"]
+[-4.2407684326171875, 8.84925651550293, "Signal Generator Function Generate the high-power radar transmit signal"]
+[3.4787018299102783, 10.560796737670898, "Power Amplifier Function Generate the high-power radar transmit signal"]
+[-3.3958911895751953, 7.378963470458984, "Data Processing System Function Perform digital data processing of the received signal"]
+[-13.833381652832031, -2.1640079021453857, "X-ray Telescope Imaging High-energy X-rays"]
+[-13.804837226867676, -2.2630553245544434, "X-ray Telescope Imaging Lower-energy X-ray light"]
+[-0.5547013878822327, 8.175885200500488, "Structure X-ray Emission Glows with lower-energy X-ray light"]
+[-3.0368001461029053, 9.59658145904541, "Battery Assembly Cell Type Lithium-ion 18650"]
+[-2.94266414642334, 9.569171905517578, "Battery Assembly Voltage Range 24 V to 32.8 V"]
+[-2.9603230953216553, 9.59109878540039, "Battery Assembly End-of-life Capacity 47 Whr"]
+[-2.5965654850006104, 9.60878849029541, "Power Source Number of Strings 8"]
+[-2.610023021697998, 9.600519180297852, "Power Source Number of Cells per String 7"]
+[-3.6283493041992188, 12.75566577911377, "Particle Detector Dark Matter Particle Mass 80 GeV/c2"]
+[-3.5960605144500732, 12.800118446350098, "Particle Detector Dark Matter Particle Mass Approximately 40 and 60 GeV/c2"]
+[-3.644132375717163, 12.755157470703125, "Particle Detector Particles Collected 100 billion"]
+[1.6186002492904663, 7.011297702789307, "Communication Device Frequency Band Ka-band"]
+[5.325529098510742, -4.559474468231201, "Satellite Launch Date June 2-8, 2013"]
+[1.2860673666000366, -1.169382095336914, "Small Satellite Program Start Year 1994"]
+[1.2824898958206177, -1.3812025785446167, "Small Satellite Program Objectives Provide an environment for frequent, inexpensive, on-orbit demonstrations of emerging space system technologies and to accelerate their transition into operational use"]
+[1.3041242361068726, -1.4283541440963745, "Small Satellite Launch Options STS (Shuttle) or with multi-service launch systems"]
+[-2.592181444168091, 9.621235847473145, "Power Source Dimensions 3.73 m x 1.8 m"]
+[-3.124441146850586, 9.669265747070312, "Battery Capacity 89 Ah"]
+[5.254475116729736, -2.231412887573242, "Satellite Design Life Seven years"]
+[1.3994640111923218, -1.0739368200302124, "Satellite Resolution 3 m"]
+[0.7335222363471985, -1.425141453742981, "Satellite Ground Track Tolerance Better than \u00b1 5km, with a goal of \u00b1 1km"]
+[2.6303412914276123, -2.0967321395874023, "Satellite Fuel Monopropellant hydrazine"]
+[2.148000478744507, -2.3928112983703613, "Satellite Thrusters Six 1 N thrusters"]
+[1.9803143739700317, -2.510802984237671, "Satellite Fuel Budget Enough for extensive COLA manoeuvres and de-orbit services"]
+[8.955479621887207, 8.511608123779297, "Satellite Payload Data Rate 640 Mbit/s"]
+[-4.284224033355713, 7.3673176765441895, "Data Transmission Maximum Data Rate 170 Mbit/s"]
+[1.1220719814300537, 13.206195831298828, "Modulation Technique Modulation Type QPSK (Quadrature Phase Shift Keying)"]
+[-4.2545623779296875, 7.378321170806885, "Data Transmission Data Rate 320 Mbit/s"]
+[-4.242168426513672, 7.365407466888428, "Data Transmission Data Rate 320 Mbit/s"]
+[0.897541344165802, 14.80247974395752, "Instrumentation Magnet Power Source Superfluid helium"]
+[0.893826425075531, 14.794137001037598, "Instrumentation Magnet Temperature 1.8\u00ba C above absolute zero"]
+[0.9058740139007568, 14.79741096496582, "Instrumentation Thermal-Vacuum Testing Location ESA's the LSS (Large Space Simulator)"]
+[-5.281029224395752, 2.6985859870910645, "Telescope Discovery Date 14 April 2021"]
+[-5.210607051849365, 2.660118579864502, "Telescope NASA Feature Date 12 February 2021"]
+[-2.5325567722320557, 12.205008506774902, "High resolution optical imagers Instrument type High resolution optical imagers"]
+[-2.540569543838501, 12.178093910217285, "High resolution optical imagers Measurement domain Land"]
+[-2.5388896465301514, 12.211044311523438, "High resolution optical imagers Measurement category Multi-purpose imagery (land)"]
+[-0.8269908428192139, 11.577695846557617, "Detector Quantity 7"]
+[-0.9747313261032104, 11.486693382263184, "Detector Purpose Accurate spectroscopy of X-rays as well as imaging with high time resolution"]
+[-0.8375239968299866, 11.7175874710083, "Detector Thickness 450 \u00b5m"]
+[-0.8241304755210876, 11.597946166992188, "Detector X-ray Photon Detection Efficiency At least 90% in the energy band from 0.3 keV to 10 keV"]
+[-1.3803763389587402, 8.956853866577148, "Function Maximum Frame Rate Up to 200 X-ray images per second"]
+[2.8433804512023926, -3.3571503162384033, "Communication Satellite Presentation Date Oct. 11-13, 2005"]
+[2.86958909034729, -3.3849899768829346, "Communication Satellite Presentation Date Feb. 15, 2006"]
+[2.8301854133605957, -3.3437254428863525, "Communication Satellite Conference Date Oct. 2-6, 2006"]
+[2.7294342517852783, 21.624332427978516, "Science Instrument Development Status Unknown"]
+[0.8981016874313354, 10.460188865661621, "Digital Mapping System Image Color White, gray, black or navy"]
+[0.9194897413253784, 10.460841178894043, "Digital Mapping System Image Source NASA, Nathan Kurtz"]
+[-13.854536056518555, -2.139437198638916, "X-ray Telescope Energy Band 3 to 79 keV"]
+[-13.879043579101562, -2.251366376876831, "X-ray Telescope Sensitivity Improvement More than 100-fold"]
+[-13.901144027709961, -2.2108922004699707, "X-ray Telescope Scientific Objectives Probe the obscured AGN activity, study the population of hard X-ray-emitting compact objects, study the non-thermal radiation in young supernova remnants, observe blazars"]
+[0.517512321472168, 10.912534713745117, "Image Sensor Data Readout Serial"]
+[-2.542827606201172, 8.889444351196289, "Analog Digital Converters Bit Resolution 16 bit"]
+[-2.779299020767212, 7.459440231323242, "Field-Programmable Gate Array Data Processing Spacewire packets"]
+[-2.8483965396881104, 7.499041557312012, "Field-Programmable Gate Array CCD Synchronization Yes"]
+[-2.7936017513275146, 15.23546028137207, "Microwave Radiometer Operating Frequencies 6.6 GHz, 10.7 GHz, 18.0 GHz, 21.0 GHz, 37.0 GHz"]
+[-2.8145976066589355, 15.24093246459961, "Microwave Radiometer Swath Width Approximately 600 km"]
+[-2.872403383255005, 15.232810974121094, "Microwave Radiometer Spatial Resolution Ranged from 22 km at 37 GHz to 100 km at 6.6 GHz"]
+[-2.8416876792907715, 15.244101524353027, "Microwave Radiometer Antenna Type Parabolic reflector"]
+[-2.8252193927764893, 15.258552551269531, "Microwave Radiometer Antenna Offset 42\u00b0 from the nadir"]
+[-2.811492443084717, 15.24944019317627, "Microwave Radiometer Sea Surface Temperature Accuracy 2 K"]
+[-2.839146375656128, 15.219993591308594, "Microwave Radiometer Wind Speed Measurement Accuracy 2 m/s for winds ranging from 7 m/s to about 50 m/s"]
+[-1.4962708950042725, 16.897863388061523, "Altimeter Position Accuracy 0.1 m"]
+[-1.5108230113983154, 16.905893325805664, "Altimeter Backscatter Coefficient Accuracy 1.0 dB"]
+[-1.49936842918396, 16.89876937866211, "Altimeter Wave Height Measurement Accuracy 10% or 0.5 m, whichever was greater"]
+[-1.507562279701233, 16.90342140197754, "Altimeter Operating Frequency 13.56 GHz"]
+[-1.47221040725708, 16.867671966552734, "Altimeter Swath Width Varies from 2.4 to 12 km"]
+[-13.855005264282227, -2.2044320106506348, "X-ray Telescope Development Location MPE"]
+[-5.359750747680664, 2.704025983810425, "Telescope Development Location Russia"]
+[-13.48344612121582, -2.036947727203369, "X-ray Observatory Launch Date March 2019"]
+[-5.73110294342041, 9.287461280822754, "Radio System Integration Date May 29"]
+[-5.272359848022461, 2.6976726055145264, "Telescopes Electric Tests Date May 3 to May 21"]
+[1.747661828994751, -1.284647822380066, "Satellite Monitoring Area 24 x 96\u00ba strips of the sky"]
+[3.781993865966797, -2.6117146015167236, "Satellite Camera Capture Interval Every 10 minutes"]
+[3.7873778343200684, -2.6190834045410156, "Satellite Fast Mode Brightness Measurement Interval Every 20 seconds"]
+[4.613391399383545, -2.6939194202423096, "Satellite Extended Mission Duration Until September 2022"]
+[2.6304869651794434, 13.474759101867676, "Optical Component Number of mirror modules 7"]
+[2.635164737701416, 13.43505859375, "Optical Component Degree of nesting (mirror shells/module) 54"]
+[2.636016607284546, 13.469231605529785, "Optical Component Focal length 1600 mm"]
+[2.6327366828918457, 13.422826766967773, "Optical Component Largest mirror diameter 358 mm"]
+[2.637935161590576, 13.39735221862793, "Optical Component Smallest mirror diameter 76 mm"]
+[2.6092636585235596, 13.415719985961914, "Optical Component Micro-roughness < 0.5 nm"]
+[2.64414119720459, 13.458885192871094, "Optical Component Energy range ~0.2 to 10 keV"]
+[2.692380905151367, 13.367883682250977, "Optical Component Energy resolution 138 eV @ 6 keV"]
+[2.618997097015381, 13.440021514892578, "Optical Component Coating Gold (> 50 nm)"]
+[2.625640392303467, 13.417008399963379, "Optical Component FOV (Filed of View) 61 arcmin"]
+[-5.382447242736816, 2.757357120513916, "Telescope Structure Dimensions ~ 1.9 m in diameter x 3.25 m in hight"]
+[-5.381547451019287, 2.7505264282226562, "Telescope Total mass ~ 750 kg"]
+[-5.405440330505371, 2.7141363620758057, "Telescope Power 405 W"]
+[-7.57166051864624, 5.878966808319092, "Camera Image Area Dimensions 3 cm x 3 cm"]
+[-7.525387287139893, 5.910655975341797, "Camera Pixel Size 75 \u00b5m by 75 \u00b5m"]
+[-7.542244911193848, 5.90562105178833, "Camera Number of Pixels 384 x 384"]
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+[-1.2744643688201904, 8.575456619262695, "Component Power Dissipation 50 \u00b5W/pixel"]
+[-1.2106541395187378, 8.610164642333984, "Component Leakage Current Negligible"]
+[-1.910463571548462, 8.13817024230957, "System Function Measure deposited energy and arrival time for each event, enable depth of interaction measurement"]
+[1.5238150358200073, -2.3594679832458496, "Satellite Orbit Earth-trailing heliocentric orbit about 50 million km from Earth"]
+[0.7933968305587769, -1.47466242313385, "Satellite Inter-spacecraft Separation 2.5 million km"]
+[5.052736282348633, -3.863504648208618, "Satellite Launch 2034"]
+[4.963521957397461, -2.4320921897888184, "Satellite Lifetime Four years, with possible six-year extension"]
+[3.073505401611328, -1.5479423999786377, "Satellite Type of mission L-class mission"]
+[-3.881401538848877, 7.9391188621521, "Data Storage Data Distribution Capacity Over 2.5 TB per day per satellite"]
+[-1.6161189079284668, 4.0921525955200195, "Ground Segment Routine Activities Nominal activities related to the provision of the link service, management of payload configuration and maintenance activities"]
+[-2.0689761638641357, 8.061925888061523, "System Architecture Layer 1 Components Commanding front-end and automation engine"]
+[-2.0686872005462646, 8.108109474182129, "System Architecture Layer 2 Components LMS (Link Management System) and interface to the MOC"]
+[-1.9471536874771118, 8.094676971435547, "System Autonomy Fully autonomous"]
+[-1.138718843460083, 4.460728168487549, "Ground Station Orbit Determination Frequency Twice per day"]
+[-1.944209337234497, 8.125990867614746, "System TLE Maintenance 5.5 hours to 10 hours"]
+[-1.925730586051941, 8.14177131652832, "System TLE Generation By mean processing of a 6 lap orbit"]
+[-1.9253556728363037, 8.05408000946045, "System TLE Accuracy Low distance difference of the appropriate time zone"]
+[0.9687899947166443, -4.319638729095459, "Satellite Mass 3500 kg"]
+[2.292581081390381, -2.340510606765747, "Satellite Launcher Thrust 1340 t"]
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+[4.473663806915283, -2.775956869125366, "Satellite Test Duration Two weeks"]
+[4.4275431632995605, -2.6783254146575928, "Satellite Acoustic Test Duration Two days"]
+[3.0869944095611572, -1.666785478591919, "Satellite Principal Scientific Investigator Dr Steven C. Wofsy"]
+[5.012670040130615, -3.857177734375, "Satellite Launch Schedule 2021"]
+[2.6237905025482178, -1.7677010297775269, "Satellite Payload DigitalGlobe"]
+[11.906455993652344, 5.2700653076171875, "3U CubeSat Mass 4 kg"]
+[16.798219680786133, 6.900508880615234, "Microsatellite Mass ~100 kg"]
+[2.41520357131958, 22.3577823638916, "Instrument Parameter Detect plasma densities and particle fluxes of 10 MeV energy range near the Earth"]
+[-0.5003790855407715, 15.539738655090332, "NIR Imaging Spectrometer Purpose Star formation history"]
+[11.889423370361328, 5.285261154174805, "3U CubeSat project Mass 4 kg"]
+[11.79737663269043, 5.318592548370361, "6U CubeSats Quantity Two"]
+[-0.11131460964679718, 9.215457916259766, "Navigation System Technology Cameras and LiDaR"]
+[-2.5983808040618896, 8.341883659362793, "Capture Technology Speed 20 m/s"]
+[-0.6131884455680847, 1.3155027627944946, "De-orbit Technology Function Speed de-orbit into the Earth\u2019s atmosphere"]
+[5.059162616729736, -4.441032409667969, "Satellite Deployment Date 20 June 2018"]
+[2.9502041339874268, -1.7074387073516846, "Satellite Consortium Surrey Space Center at the University of Surrey and co-funded by the EC (European Commission)"]
+[2.298448085784912, -2.7504656314849854, "Satellite Deployment Mission Count 13"]
+[2.3816089630126953, -2.0067338943481445, "Satellite Deployment Type Doublewide"]
+[5.176877498626709, -3.9894251823425293, "Satellite Mission Start Year 2003"]
+[-0.33530256152153015, 4.977782249450684, "Subglacial Lakes Draining Period Frequency Third time since the original ICESat mission began measuring elevation changes on the ice sheet\u2019s surface in 2003"]
+[-0.3881930112838745, 5.039579391479492, "Lakes Outlines Change Gradually as water enters and leaves the reservoirs"]
+[2.3773880004882812, -1.2194147109985352, "Satellite Data Detection Lakes filling and draining"]
+[-7.5842461585998535, 5.859208106994629, "Camera Image Resolution 1.6 km"]
+[2.558762788772583, -1.5926554203033447, "Satellite Camera Activation Signal from the OBC"]
+[2.5860753059387207, -1.9039298295974731, "Satellite Camera Activation Command from the ground station"]
+[0.6806642413139343, 12.00684642791748, "Sensor Mounting Location OSC"]
+[0.7652914524078369, 11.994099617004395, "Sensor Mounting Location CSC"]
+[0.7001843452453613, 11.995892524719238, "Sensor Mounting Location OSC"]
+[0.5973067283630371, 11.951590538024902, "Sensor Function Computing the relative position and velocity during perigee pass based on GPS measurements"]
+[-5.572022914886475, 7.0624775886535645, "Communication Link Function Range measurement and transfer of data between the two S/C"]
+[0.8160474300384521, 12.051800727844238, "Sensor Quantity 3 on each S/C"]
+[0.6771364212036133, 12.097744941711426, "Sensor Quantity Two on each S/C"]
+[0.797258734703064, 12.098772048950195, "Sensor Quantity 1 of each on each S/C"]
+[-0.4651376008987427, 8.653976440429688, "Actuator Quantity 12 on the OSC"]
+[-0.45621177554130554, 8.664039611816406, "Actuator Quantity 8 on the CSC"]
+[-0.4599166214466095, 8.658778190612793, "Actuator Quantity 4 on each S/C"]
+[2.8943285942077637, 22.589757919311523, "Instrument Program Sentinel-2"]
+[0.8525696396827698, 12.045364379882812, "Sensor Quantity 4 (2 in the head and 2 close to the ADC)"]
+[-0.9403806328773499, 7.866184711456299, "Device Temperature Control Zones Front tube of the COB, Equipment Box of the COB"]
+[1.1691304445266724, -0.6864619255065918, "Satellite Size 3 m x 3 m x 0.8 m"]
+[0.9821166396141052, -4.411136627197266, "Satellite Mass ~600 kg"]
+[1.4923990964889526, -2.4051430225372314, "Satellite Orbit Co-planar polar orbit"]
+[0.7354640960693359, -1.1663804054260254, "Satellite Altitude ~490 km"]
+[1.0227129459381104, -1.282396674156189, "Satellite Spacing 220 km"]
+[-0.948434591293335, -10.012621879577637, "Satellite Constellation Imaging Frequency 6 times at \u226450cm, 10 times at \u22641m, 14 times at <\u22641.3m"]
+[-0.9496979117393494, -10.01064682006836, "Satellite Constellation Visits/Day \u226516 at 1.3m"]
+[-0.6022137403488159, 1.297456979751587, "Orbit Type Descending Node Time 10:30"]
+[-1.8262245655059814, 14.887384414672852, "Radiometer Look Angle 39\u00ba"]
+[-1.9059182405471802, 14.870672225952148, "Radiometer Spectral Bands 0.5-0.6, 0.6-0.7, 0.7-0.8, 0.8-1.1, and 10.4 - 12.6 \u00b5m"]
+[-1.8530056476593018, 14.949207305908203, "Radiometer Spatial Resolution 170 m (in VIS) and 600 m (TIR)"]
+[-1.9335246086120605, 14.896707534790039, "Radiometer Swath 600 km"]
+[-1.8985540866851807, 14.870482444763184, "Radiometer Potential Repeat Cycle 3-5 days"]
+[-1.8963887691497803, 14.8694486618042, "Radiometer Orbit Repeat Cycle 21 days"]
+[-1.8942172527313232, 14.889092445373535, "Radiometer Scan Rate 50 lines/s in channels 1-4 and 12.5 lines/s in channel 5"]
+[-1.856146216392517, 14.835956573486328, "Radiometer Absolute Radiometric Error 1%"]
+[-1.9020922183990479, 14.865050315856934, "Radiometer Signal-to-Noise Ratio (SNR) 80 dB"]
+[-1.934556484222412, 14.799605369567871, "Radiometer Noise Equivalent Temperature 0.5 K"]
+[-1.939488410949707, 14.91246223449707, "Radiometer Data Quantization 8 bits"]
+[-1.896394968032837, 14.89022159576416, "Radiometer Mass 21kg"]
+[-1.9037444591522217, 14.875237464904785, "Radiometer Downlink Limitations Four out of five bands may be downlinked simultaneously"]
+[0.5020819306373596, 9.373146057128906, "Attitude Control System Sun-pointed Attitude Acquisition Time Within 150 seconds"]
+[-2.9911458492279053, 4.219078540802002, "Spacecraft Subsystem On-orbit Maximum Battery Voltage Within 0.13 V of the predicted value"]
+[-2.894216299057007, 4.0954484939575195, "Spacecraft Subsystem On-orbit Measured Solar Array Power Approximately 5 W greater than the predicted value"]
+[-6.650378227233887, 9.95856761932373, "Antenna System Reflector Dimension 65 cm"]
+[-6.592105388641357, 9.9008150100708, "Antenna System Calibration Target Temperature Difference 50-60 K"]
+[-6.629832744598389, 9.932120323181152, "Antenna System Drum Rotation Continuous"]
+[2.869292974472046, 22.711891174316406, "Instrument Flight Performance Analysis Unknown"]
+[3.6906492710113525, 22.95985984802246, "Instrument Publication Date 2009"]
+[2.6277084350585938, 14.294865608215332, "Optical Instrument Calibration Focus Bright X-ray sources"]
+[-13.728425025939941, -2.329227924346924, "X-ray Telescope First Snapshots Date June 28, 2012"]
+[-13.688233375549316, -2.3151772022247314, "X-ray Telescope Mast Deployment Date June 21, 2012"]
+[-13.889886856079102, -2.256680965423584, "X-ray Telescope Mast Length Lengthy"]
+[-13.847413063049316, -2.192117214202881, "X-ray Telescope Ability See the highest energy X-rays in the universe"]
+[2.5504190921783447, -2.0890727043151855, "Satellite Calibration and Validation Unknown"]
+[4.9737067222595215, -4.608675003051758, "Satellite Workshop Date March 26-28, 2014"]
+[2.8058571815490723, 22.477094650268555, "Instrument Type Data collection"]
+[2.862487554550171, 22.404687881469727, "Instrument Type High resolution optical imagers"]
+[2.8218376636505127, 22.340030670166016, "Instrument Type Multispectral and Panchromatic Wide-Scan Camera"]
+[2.775074005126953, 22.42136573791504, "Instrument Type Multi-spectral radiometers"]
+[2.9416396617889404, -1.4134082794189453, "Satellite Mission Global CO2 Observation and Monitoring"]
+[5.0314154624938965, -4.545226573944092, "Satellite Symposium Date June 25-29, 2012"]
+[5.0125322341918945, -4.566700458526611, "Satellite Symposium Date June 25-29, 2012"]
+[-1.9257951974868774, 14.857139587402344, "Radiometer Frequency Band L-band"]
+[-2.994877338409424, 16.178180694580078, "Scatterometer Measurement Surface Roughness"]
+[2.344468355178833, 22.18021583557129, "Instrument Measurement Polarized reflectance in VIS/NIR"]
+[2.6782445907592773, 22.177122116088867, "Instrument Observation Earth's target reflectance from 12 directions during a single S/C pass"]
+[2.6546571254730225, 23.12354850769043, "Instrument Operation Modes Two dynamic modes for high SNR and wide dynamic range"]
+[2.3608455657958984, 22.74934959411621, "Instrument Measurement Channels 15 channels (three channels for each polarized band)"]
+[1.63468599319458, 21.91663360595703, "Instrument Swath Width 1440 km x 2200 (across-track) km"]
+[1.7770131826400757, 22.080522537231445, "Instrument Ground Spatial Resolution 7 km x 6 km at nadir"]
+[2.321214437484741, 22.97722625732422, "Instrument Data Rate 0.882 Mbit/s"]
+[2.589101552963257, 22.51055145263672, "Instrument Quantization 12-bit"]
+[-4.489280700683594, 15.912171363830566, "Radar Pulse Transmit Frequency 14.599 GHz"]
+[-4.506274223327637, 15.93237590789795, "Radar Swath Width 500 km"]
+[2.056856870651245, 22.663387298583984, "Instrument Wavelengths 0.49 \u00b5m - 0.94 \u00b5m, 10.5 \u00b5m - 12.5 \u00b5m"]
+[1.87578547000885, 22.06641960144043, "Instrument Nadir Angular Resolution 2.3 km and 4.4 km"]
+[1.6916910409927368, 21.96114730834961, "Instrument Swath Width 2280 km"]
+[0.7624425292015076, -2.2440345287323, "Satellite Orbit Inclination 108\u00b0"]
+[0.7150598168373108, -1.627647876739502, "Satellite Apogee 799 km"]
+[0.6949369311332703, -1.5887027978897095, "Satellite Perigee 775 km"]
+[4.1265549659729, -2.890402317047119, "Satellite Orbit Period 101 minutes"]
+[4.2078423500061035, -2.5366878509521484, "Satellite Repeat Cycle 17 days"]
+[4.181105136871338, -2.493558883666992, "Satellite Subcycle 3 days"]
+[-5.24915885925293, 7.865984916687012, "Communication System Modulation Asynchronous GMSK"]
+[-5.405969142913818, 8.167923927307129, "Communication System Downlink Frequency 2.207 GHz"]
+[-5.232822895050049, 7.851670265197754, "Communication System Data Rate 100 kbit/s"]
+[-5.286128997802734, 8.032198905944824, "Communication System Uplink Frequency 1.767 GHz"]
+[-5.236416816711426, 7.904273986816406, "Communication System Self-management Required"]
+[-5.285216331481934, 7.920581340789795, "Communication System Low Overhead Required"]
+[-5.220911502838135, 7.829347133636475, "Communication System Bandwidth Demand Increased"]
+[-5.148889064788818, 7.866005897521973, "Communication System Raw Data Rates Increased"]
+[-5.199714660644531, 7.841325283050537, "Communication System Challenge Major"]
+[-3.1088063716888428, 1.6852147579193115, "Satellite Missions Time Reference GNSS systems"]
+[0.7169467806816101, 12.00721549987793, "Sensor Power Status On"]
+[0.7592709064483643, 12.041839599609375, "Sensor Observation Target Sun"]
+[-5.864831447601318, 15.982852935791016, "Synthetic Aperture Radar Architecture Front-end and back-end"]
+[3.023219347000122, 22.622303009033203, "Instrument Section Components Instrument Control Module (ICM), Chirp and Timing Generator (CTG), Digitiser Modules (DGR), Power Conditioning Modules (PCM)"]
+[2.7144806385040283, 22.679983139038086, "Instrument Section Number of Digitiser modules 6"]
+[2.7358860969543457, 23.266088485717773, "Instrument Section Functions Digital conversion of the radar echoes, digital beamforming, SCan On Receive, decimation, data compression, packetization"]
+[3.6472537517547607, 22.23703384399414, "Instrument Component Protection Function Blocks Sun light"]
+[3.6345767974853516, 22.244483947753906, "Instrument Component Heating Power Lower than 0.5 W"]
+[3.646519422531128, 22.23722267150879, "Instrument Component Motor Type Limited angle DC brushless torque motor"]
+[3.62431001663208, 22.24482536315918, "Instrument Component Spring Function Closes the shutter when unpowered"]
+[3.630009889602661, 22.239490509033203, "Instrument Component Control System Control loops and position encoder"]
+[-7.400013446807861, 2.8691701889038086, "Cosmic Ray Detector Installation Date May 2011"]
+[-7.397871494293213, 2.8695528507232666, "Cosmic Ray Detector Repair Date January 25, 2020"]
+[-7.428574085235596, 2.8589868545532227, "Cosmic Ray Detector Service Date December 3, 2019"]
+[0.5318031311035156, 9.456727027893066, "Attitude Determination and Control System Pointing Accuracy \u00b1.14 arcsec (1\u03c3)"]
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+[5.369044303894043, -4.412393093109131, "Satellite Launch Date 19.1.1964"]
+[3.1105387210845947, -2.3087713718414307, "Satellite Reentry Date Unknown"]
+[2.892364025115967, -2.040107011795044, "Satellite Comments Also known as Ops-3367"]
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+[-3.907517194747925, 15.639044761657715, "Imaging microwave radars Instrument type Imaging microwave radars"]
+[-3.9356346130371094, 15.661412239074707, "Imaging microwave radars Measurement domain Atmosphere, Ocean, Land, Snow & Ice"]
+[-3.9186785221099854, 15.631032943725586, "Imaging microwave radars Measurement category Multi-purpose imagery (ocean), Multi-purpose imagery (land), Vegetation, Albedo and reflectance, Landscape topography, Ocean topography/currents, Sea ice cover, edge and thickness, Soil moisture, Snow cover, edge and depth, Ocean surface winds, Atmospheric Winds, Ocean wave height and spectrum, Ice sheet topography"]
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+[0.8084104061126709, -2.1641929149627686, "Satellite Latitude 88 degrees south"]
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+[2.1270251274108887, -1.46371591091156, "Satellite Instrument Optimization Procedures Ensure the laser is pointing at the precisely correct angle and lasing at the precisely correct wavelength"]
+[-1.6208635568618774, 1.4829024076461792, "Data Relay System First Quasi-Real-Time Demonstration Date Feb. 29, 2016"]
+[2.604201555252075, -1.3862591981887817, "Satellite Product Contents 25-m spaced annual global mosaics (using orthorectified slope corrected SAR)"]
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+[2.6770832538604736, -1.3952677249908447, "Satellite Product Soil moisture To be generated from PolSAR data"]
+[2.5741827487945557, -1.2676916122436523, "Satellite Product Sea ice identification Creates monthly ScanSAR mosaics for both polar regions and temporal changes for glacier movement"]
+[2.5227980613708496, -1.3602744340896606, "Satellite Product Wind speed distribution LMOD (L-band modulation function) developed for PALSAR will be improved by using the dual-polarized PALSAR-2"]
+[2.7235782146453857, -1.3121225833892822, "Satellite Product Sensitivity research for disasters Time-series SAR data (amplitude), PolSAR and InSAR (coherence) will be combined to detect the best combination for each disaster"]
+[2.6616008281707764, -1.407284140586853, "Satellite Product Fire scar Using time-differentiation of the slope-corrected HV, fire risk areas will be detected"]
+[8.517626762390137, 13.942585945129395, "Lidar Instrument Wavelengths 532 nm and 1064 nm"]
+[8.51745891571045, 13.942684173583984, "Lidar Instrument Data Product Delivery Time Within 12 hours"]
+[8.518268585205078, 13.94384479522705, "Lidar Instrument Laser Operation Time Over 24 continuous hours"]
+[-3.196814775466919, 4.565414905548096, "Cargo spacecraft Departure Date Feb. 10, 2015"]
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+[-0.7015683650970459, 3.258549928665161, "Star Tracker Probability 99.9%"]
+[2.6264281272888184, -3.1846845149993896, "Communications Satellite Propulsion All-electric"]
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+[0.58084636926651, 12.136655807495117, "Sensor Manufacturer LASP (Laboratory for Atmospheric and Space Physics) at the University of Colorado, Boulder, CO"]
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+[1.3999600410461426, 2.6998071670532227, "Defense Meteorological Support Program Satellite Unveiling Date December 20, 2017"]
+[-3.1601502895355225, 1.8148090839385986, "Airborne Mission Resumption Date Late March 2018"]
+[-7.528566837310791, 5.874276161193848, "Camera Product Line Compact & versatile cameras"]
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+[-7.396492958068848, 2.8675763607025146, "Cosmic Ray Detector Antiproton Flux Unknown"]
+[-7.412573337554932, 2.842850685119629, "Cosmic Ray Detector Antiproton-to-Proton Flux Ratio Unknown"]
+[-7.403202056884766, 2.8624637126922607, "Cosmic Ray Detector Properties of Elementary Particle Fluxes Unknown"]
+[2.2406110763549805, 22.232072830200195, "Instrument Measurement Type Methane in the atmosphere"]
+[2.3581581115722656, 22.652315139770508, "Instrument Spectrum Short-wave infrared (SWIR)"]
+[2.139122247695923, 22.231813430786133, "Instrument Measurement Light absorbed by methane"]
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+[2.733246326446533, -1.5876461267471313, "Satellite Operator MethaneSAT LLC"]
+[5.093474388122559, -3.9760918617248535, "Satellite Launch Date 2023"]
+[5.016308307647705, -4.347151756286621, "Laser Telecommunication Satellite Launch Date Feb. 1, 2016"]
+[5.35880708694458, -4.376951217651367, "Satellite Launch Date 6 August 2019"]
+[-13.50749397277832, -2.0106804370880127, "X-ray Observatory Energy Range 1 to 7 keV"]
+[-13.91864013671875, -2.12743878364563, "X-ray Telescope Energy Range 68 to 78 keV"]
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+[-13.881547927856445, -2.2197656631469727, "X-ray Telescope Spatial Resolution Approximately 10 times greater than previous missions"]
+[-13.913385391235352, -2.2245090007781982, "X-ray Telescope Sensitivity More than 100 times greater than previous missions"]
+[4.6878156661987305, -4.53354549407959, "Satellite Image Capture Date 27 October 2017"]
+[0.6824244856834412, -1.376285433769226, "Satellite Relative Speed Up to 28,000 km per hour"]
+[5.277310848236084, -3.77516508102417, "Satellite Launch Year 2018"]
+[-5.272922039031982, 7.912247180938721, "Communication System Partnership ESA and Airbus"]
+[16.926025390625, 6.789715766906738, "Imaging Microsatellite Launch Date July 29, 2009"]
+[16.916648864746094, 6.795219898223877, "Imaging Microsatellite Launch Site Baikonur, Kazakhstan"]
+[16.908275604248047, 6.811635971069336, "Imaging Microsatellite Launch Provider ISC (International Space Company) Kosmotras of Moscow, Russia"]
+[16.819887161254883, 6.882975101470947, "Imaging Microsatellite Mass 12 kg"]
+[0.955475926399231, -4.3956122398376465, "Satellite Mass 23.5 kg"]
+[5.228647232055664, -4.035623550415039, "Satellite Program Initiation Year 1977"]
+[4.925715923309326, -3.650278091430664, "Satellite Start of Operations 1985"]
+[4.64495849609375, -2.846771717071533, "Satellite Planned Observation Continuation At least until 2000"]
+[2.681211233139038, -1.1562403440475464, "Satellite Applications Observation of the state of agricultural crops, assessment of hydrological conditions, forest and tundra fires, pollution monitoring"]
+[-5.321187496185303, 2.723451614379883, "Telescope Mirror Modules 7"]
+[-5.426149845123291, 2.738938808441162, "Telescope Mirror Shells per Module 54"]
+[-5.39666748046875, 2.7792623043060303, "Telescope Mirror Module Configuration Compact hexagonal with 1300 mm diameter"]
+[-9.909002304077148, 7.395928859710693, "Mirror Manufacturing Shape Negative of the final reflective surface of the mirror"]
+[0.9822477102279663, -1.0633550882339478, "Satellite Melt Pond Depth About 80 cm"]
+[1.1099307537078857, -0.8643597960472107, "Satellite Melt Pond Size As big as Olympic-sized swimming pools, or bigger"]
+[2.4199228286743164, -1.324134111404419, "Satellite Melt Pond Detection Automatic"]
+[5.278880596160889, -4.481761932373047, "Satellite Launch Date Nov. 20, 2017"]
+[4.643455505371094, -2.5987961292266846, "Satellite Primary Mission Duration Three months"]
+[4.61652946472168, -2.6319682598114014, "Satellite Extended Mission Duration Nearly two years"]
+[2.8035457134246826, -1.6739994287490845, "Satellite Program Manager Lorraine Fesq"]
+[3.108834981918335, -1.5873039960861206, "Satellite Principal Investigator MIT's Sara Seager"]
+[4.691736221313477, -2.6139605045318604, "Satellite Operation Duration 1 year"]
+[3.037630081176758, -1.509028434753418, "Satellite Partnership NASA and the German Research Center for Geosciences (GFZ)"]
+[2.795985221862793, -1.831055998802185, "Satellite Operation Center German Space Operations Center in Oberpfaffenhofen, Germany"]
+[3.708422899246216, 17.68319320678711, "Payload Activation Date August 7 - 8, 2013"]
+[3.7340147495269775, 17.702280044555664, "Payload Performance Satisfactory"]
+[3.703214645385742, 17.660898208618164, "Payload Image Quality Good"]
+[0.9721385836601257, -2.1224448680877686, "Satellite Final Geostationary Orbital Location 82\u00ba East longitude"]
+[0.5501638054847717, -1.362626552581787, "Satellite GEO Altitude 35,786 km"]
+[-0.4151434302330017, -0.4097638726234436, "Satellite Deployment Mechanism CubeSat Capacity 18"]
+[-3.078460454940796, 4.6029205322265625, "Cargo Spacecraft Return Cargo Capacity More than 1800 kg"]
+[-3.2022759914398193, 4.500038146972656, "Cargo Spacecraft Deorbit Burn Duration Up to 10 minutes"]
+[-3.1234662532806396, 4.515980243682861, "Cargo Spacecraft Reentry Duration About 30 minutes"]
+[3.2084803581237793, 2.372236728668213, "Satellite Subsystem Thruster Type 1N hydrazine"]
+[3.221566915512085, 2.368046522140503, "Satellite Subsystem Propellant Tank Capacity 20 liter"]
+[3.2253153324127197, 2.3769819736480713, "Satellite Subsystem Propellant Quantity 10 kg"]
+[3.2231080532073975, 2.375777244567871, "Satellite Subsystem Uplink Data Rate 2 k bit/s"]
+[3.223389148712158, 2.377393960952759, "Satellite Subsystem Downlink Data Rate 8.192 kbit/s"]
+[3.221104383468628, 2.374539852142334, "Satellite Subsystem X-band Link Data Rate 64Mbit/s"]
+[3.2018051147460938, 2.3929286003112793, "Satellite Subsystem Onboard Storage Capacity 128 Gbit"]
+[-3.828974962234497, 6.852282524108887, "Data Collection Platforms Number of Services 1000"]
+[-3.8189449310302734, 6.857224941253662, "Data Collection Platforms Transmission Time About 10 seconds"]
+[-3.823491334915161, 6.857736587524414, "Data Collection Platforms Type Combination of `alert' and `self-timed' DCPs"]
+[-3.2017509937286377, 7.528288841247559, "Algorithm Cloud Discrimination Processing Time Longer than using CAI-2"]
+[-0.00973831582814455, 9.324999809265137, "Intelligent Pointing System Usage Used for the intelligent pointing system"]
+[-1.4161866903305054, 10.823471069335938, "Cloud Discrimination Usage Used for cloud discrimination except thin cirrus"]
+[7.28136682510376, 12.410035133361816, "Satellite Instrument Band 2.0 \u00b5m"]
+[2.125248670578003, 22.557716369628906, "Instrument Bands 0.67, 0.87 and 1.60 \u00b5m"]
+[2.8100805282592773, 22.144166946411133, "Instrument Environmental Testing Passed"]
+[1.6197545528411865, 22.1864013671875, "Instrument Size Less than 10 x 10 x 8 cm"]
+[2.876793384552002, 22.02619743347168, "Instrument Purpose Space weather in-orbit demonstration"]
+[-2.4516148567199707, 8.325423240661621, "Capture System Mass and Volume Low"]
+[-2.487760305404663, 8.36485767364502, "Capture System Firing Speed High"]
+[-2.4444239139556885, 8.30258846282959, "Capture System Development Risk Low"]
+[-2.4954729080200195, 8.321290016174316, "Capture System Cost Low"]
+[-0.18495886027812958, 15.596724510192871, "Spectrometer Spectral Range 80 to 170 nm"]
+[-0.1420295089483261, 15.559968948364258, "Spectrometer Spectral Resolution 1.5 nm or less"]
+[-0.027443943545222282, 15.493803024291992, "Spectrometer IFOV 0.1\u00ba vertical and 2.4\u00ba horizontal"]
+[-0.12950679659843445, 15.4420804977417, "Spectrometer FOR 30\u00ba x 2.4\u00ba"]
+[-0.11650107055902481, 15.5256929397583, "Spectrometer Scanning Range 10\u00ba - 40\u00ba below of spacecraft horizon (y-direction)"]
+[-0.06825008243322372, 15.509380340576172, "Spectrometer Scanning Rate Up to 6\u00ba per second"]
+[-0.11452629417181015, 15.5350341796875, "Spectrometer Sensitivity 0.5 counts per second per Rayleigh at 83.4 nm"]
+[-3.8408877849578857, 7.955657005310059, "Data Storage Capacity 2.4 Tbit"]
+[-5.172654151916504, 7.724228382110596, "Communication System Data Rate 560 Mbit/s"]
+[-5.2287821769714355, 7.7815752029418945, "Communication System Uplink Data Rate 64 kbit/s"]
+[-5.184207439422607, 7.775256156921387, "Communication System Downlink Data Rate 2 Mbit/s"]
+[-1.1642762422561646, 4.476356506347656, "Ground Station Quantity 4"]
+[3.4446399211883545, 13.431930541992188, "Laser Communication Terminal Manufacturer Tesat-Spacecom"]
+[0.9925375580787659, -4.3467206954956055, "Satellite Mass 500 kg"]
+[0.9958710074424744, -4.374547004699707, "Satellite Mass 180 kg (Chaser/Servicer), 20 kg (Target/Client)"]
+[0.9579412937164307, -4.397724628448486, "Satellite Mass 15 kg"]
+[2.0809743404388428, -2.7196130752563477, "Satellite Quantity 3"]
+[2.6273529529571533, -2.285968065261841, "Satellite Communication Bands Ku-band, S-band"]
+[5.337818622589111, -4.3891496658325195, "Satellite Launch Date 19.11965"]
+[5.083548545837402, -4.424100875854492, "Satellite Reentry Date 13.7.1979"]
+[2.765296697616577, -1.9595441818237305, "Satellite Also known as Ops-7040"]
+[3.734104633331299, -1.6100341081619263, "Satellite Housekeeping Mode Nominal"]
+[2.2198257446289062, -1.6778841018676758, "Satellite Battery Status Fully charged"]
+[0.6716284155845642, -2.1802477836608887, "Satellite Temperature Range 20-40\u00baC"]
+[-0.8787294626235962, 5.046066761016846, "Station Location NTU"]
+[-0.8903210163116455, 5.011207103729248, "Station Antennas UHF/VHF high-gain cross Yagi-Uda antennas"]
+[6.74560022354126, 6.953031063079834, "Satellite Component Unknown Unknown"]
+[2.9745724201202393, -2.0978310108184814, "Satellite Unknown Unknown"]
+[-6.702786445617676, 9.977448463439941, "Antenna Frequency Bands L1/L2"]
+[-6.698261737823486, 9.974285125732422, "Antenna Gain Greater than \u2013 4 dBic for elevations > 5\u00b0"]
+[-6.6854472160339355, 9.961604118347168, "Antenna Polarization RHCP (Right Hand Circular Polarization)"]
+[-6.68548583984375, 9.956504821777344, "Antenna Function Receive the strongly attenuated signals coming from the GPS constellation during their occultation time window"]
+[-1.0825194120407104, 7.65451192855835, "Device Type Unknown"]
+[4.092888832092285, 13.932826042175293, "Airborne Laser Altimeter Wavelengths 532 nm and 1064 nm"]
+[4.0870680809021, 13.922369003295898, "Airborne Laser Altimeter Laser Pulses ~1.5 ns"]
+[4.102084159851074, 13.935482025146484, "Airborne Laser Altimeter Maximum View Angle \u00b11 km"]
+[5.297773838043213, -4.282168388366699, "Satellite Launch Date 2017\u20132018"]
+[2.602403402328491, -2.2335102558135986, "Satellite Consortium Size More than 350 scientists and engineers"]
+[2.9047374725341797, -1.518093228340149, "Satellite CCDs Procurement Study of the CCDs procurement was issued by ESA"]
+[-2.6498804092407227, 9.370835304260254, "Power Supply Voltage range (V) 800~1,100"]
+[-2.623793125152588, 9.337916374206543, "Power Supply Current range (A) 0.2~0.6"]
+[-2.621274709701538, 9.342840194702148, "Power Supply Ripple (%) 5"]
+[-2.6238460540771484, 9.331320762634277, "Power Supply Regulation (%) \u00b13"]
+[-2.621368408203125, 9.315163612365723, "Power Supply Maximum Power (W) 660"]
+[-2.6256158351898193, 9.3350830078125, "Power Supply Voltage range (V) 400~500"]
+[-2.6666202545166016, 9.373322486877441, "Power Supply Current range (A) 0.001~0.1"]
+[-2.637303590774536, 9.330489158630371, "Power Supply Ripple (%) 5"]
+[-2.643362522125244, 9.328160285949707, "Power Supply Regulation (%) \u00b15"]
+[-2.6242189407348633, 9.335555076599121, "Power Supply Maximum Power (W) 5.5"]
+[2.32351016998291, 22.54313087463379, "Instrument Stability Requirement High signal-to-noise ratio and long-term photometric stability"]
+[-3.333603620529175, 4.236815452575684, "Spacecraft Mission Lifetime Up to 8.5 years"]
+[2.348848581314087, 22.167137145996094, "Instrument Thermal Environment Requirement Stable measurements over long periods of time (months)"]
+[-5.300187110900879, 3.0487453937530518, "Telescope Array Energy Range 2-3 keV, 3-5 keV"]
+[-5.312439441680908, 3.1229588985443115, "Telescope Array X-ray Source Distance 12 million light years"]
+[-0.7562662363052368, 3.1123061180114746, "Stellar Remnant Energy Output About 10 million suns"]
+[-2.58392333984375, 9.628854751586914, "Power Source Articulation 2-axis"]
+[0.9754635095596313, -4.374294757843018, "Satellite Total Mass 123.7 kg"]
+[2.0718188285827637, -0.564744234085083, "Satellite Power 330 W (EOL, 100 W average)"]
+[1.9687690734863281, -0.7094083428382874, "Satellite Bus Voltage 28 V"]
+[-3.095338821411133, 9.657198905944824, "Battery Capacity 4 Ah"]
+[-3.0662808418273926, 7.615662574768066, "Central Processing Unit Model RAD6000"]
+[5.112661361694336, -2.283963203430176, "Satellite Design Life 1 year + 3 months extension"]
+[0.47848939895629883, 9.434903144836426, "Attitude Determination Device Type Star tracker"]
+[0.4913375973701477, 9.454802513122559, "Attitude Determination Device Type Interferometric fiber optic gyro"]
+[0.48514893651008606, 9.375598907470703, "Attitude Control Device Quantity Three"]
+[-1.7442513704299927, 8.762665748596191, "Secondary Control Device Quantity Three"]
+[1.8978688716888428, 8.601672172546387, "Subsystem Solid State Storage 380 MByte"]
+[1.89737069606781, 8.598283767700195, "Subsystem Data Rates 20 MByte/s"]
+[-1.6513079404830933, 8.365264892578125, "System Component Function Control and synchronise the camera electronics, the SPS, the thermal control and the mechanisms control"]
+[-1.6384460926055908, 8.415417671203613, "System Component Function Integrated interfaces and instrument control/monitoring functions"]
+[-2.893345355987549, 7.798264503479004, "Processing Core Function Achieve on-board data compression"]
+[-5.2047438621521, 7.859452247619629, "Communication Architecture Function Attach to the running system by a flexible and glitch-free on-chip communication architecture"]
+[-2.39691162109375, 9.1914701461792, "Power System Solar Arrays Power Over 330 W"]
+[-2.3503310680389404, 9.176370620727539, "Power System Battery Packs Capacity 14.4 Ah"]
+[-0.6465714573860168, 9.420899391174316, "Space Component Manufacturer MAXAR"]
+[-1.3427112102508545, 6.097343444824219, "Company CEO Dan Jablonsky"]
+[-1.3483694791793823, 6.084349155426025, "Company Cost Savings $60 million"]
+[-1.3337699174880981, 6.095733642578125, "Company Business Unit SSL"]
+[1.6346087455749512, -2.3282856941223145, "Satellite Design Objective Achieve specific orbit with high accuracy"]
+[1.2219717502593994, -0.9458717703819275, "Satellite CCR Diameter 25 mm"]
+[1.1668146848678589, -0.8604472875595093, "Satellite CCR Diameter 37.5 mm"]
+[2.7808005809783936, -1.6875662803649902, "Satellite CCRs COTS components"]
+[-2.027655839920044, 8.552814483642578, "Ancillary Electronics Module Function Data acquisition and treatment, temperature control"]
+[-2.065138816833496, 8.558634757995605, "Ancillary Electronics Module Signal Inputs 8 differential signals from light sensors, 2 temperature signals"]
+[-2.088348627090454, 8.58583927154541, "Ancillary Electronics Module Signal Output 2 signals"]
+[-2.1730034351348877, 8.558082580566406, "Ancillary Electronics Module ADC Bit Depth 16 bit"]
+[-2.0638785362243652, 8.563112258911133, "Ancillary Electronics Module ADC Cadence 40 samples/s"]
+[6.289246082305908, 7.438328742980957, "Satellite Module Mechanical, Thermal and TED Qualification Completed"]
+[-2.4069137573242188, 8.32486343383789, "Service Module Development Start Phase 2"]
+[-0.3469572961330414, 6.8608784675598145, "Assembly, Integration and Test Modularity Parallelize activities and reduce the lead time"]
+[-0.37587419152259827, 6.832150459289551, "Assembly, Integration and Test Accessibility Reactive in case of troubleshooting"]
+[-0.3886466920375824, 6.762841701507568, "Assembly, Integration and Test Alignment Performance Achieved through adequate alignment strategies and accuracies"]
+[2.770577907562256, 13.717857360839844, "Optical Device Spacer Material ULE"]
+[2.789304256439209, 13.68010425567627, "Optical Device Spacer Length 77.5 mm"]
+[2.7894339561462402, 13.695528984069824, "Optical Device Finesse About 10,000"]
+[2.7817342281341553, 13.695327758789062, "Optical Device Finesse About 10,000"]
+[2.5050864219665527, 22.543283462524414, "Instrument Measurement Record 40 years"]
+[2.6519930362701416, 22.650737762451172, "Instrument Measurement Record Unknown"]
+[4.633375644683838, -2.441671848297119, "Satellite Mission Operations Center Support 3 years"]
+[3.7007882595062256, 22.96962547302246, "Instrument Arrival Date at NASA/KSC August 4, 2017"]
+[3.680845022201538, 22.960107803344727, "Instrument NASA Responsibility Start Date October 1, 2015"]
+[3.6670749187469482, 22.963884353637695, "Instrument Delta-Critical Design Review Completion Date July 2015"]
+[-5.417048931121826, 2.7195937633514404, "Telescope Development Location Goddard Space Flight Center"]
+[-0.08219966292381287, 13.573665618896484, "Measurement System Development Location Jet Propulsion Laboratory"]
+[-1.616217851638794, 9.67370891571045, "Propulsion System Development Location Jet Propulsion Laboratory"]
+[-2.2098660469055176, 7.109508514404297, "Management System Development Location University of Florida"]
+[3.5884921550750732, 13.265144348144531, "Laser Beams Color Blue, green, and purple"]
+[2.5895936489105225, -1.6484639644622803, "Satellite Synthetic Aperture Radar (SAR) Unknown"]
+[2.364733934402466, -1.4036026000976562, "Satellite Radar Image Acquired on May 18, 2021"]
+[-0.8294891119003296, 16.41967010498047, "Fourier Transform Spectrometer LTAN 13:00 \u00b1 0:15 hr"]
+[-0.823950469493866, 16.418842315673828, "Fourier Transform Spectrometer Orbital altitude 613 km"]
+[-0.8319809436798096, 16.42451286315918, "Fourier Transform Spectrometer Revisit time 3 days"]
+[-0.8298590779304504, 16.421358108520508, "Fourier Transform Spectrometer Coverage Cross-track: \u00b135\u00ba, Along-track: \u00b140\u00ba"]
+[-0.8318904042243958, 16.42300033569336, "Fourier Transform Spectrometer IFOV 10.5 km"]
+[-0.8287174105644226, 16.420360565185547, "Fourier Transform Spectrometer Sampling duration 4 s"]
+[-0.8310725688934326, 16.425247192382812, "Fourier Transform Spectrometer Spectral resolution 0.2 cm -1"]
+[-0.823082685470581, 16.415727615356445, "Fourier Transform Spectrometer SNR >400 (Band 1) >300 (Band 2 to 5) @SZA=30\u00ba, albedo=0.3) >300"]
+[-2.6365058422088623, 11.702550888061523, "Imager LTAN 13:00 \u00b1 0:15 hr"]
+[-2.6538729667663574, 11.687427520751953, "Imager Orbital altitude 666 km"]
+[-2.6658756732940674, 11.668240547180176, "Imager Revisit time 3 days"]
+[-2.64304518699646, 11.696362495422363, "Imager Coverage Cross-track: \u00b135\u00ba, Along-track: \u00b120\u00ba"]
+[-2.654827833175659, 11.682486534118652, "Imager IFOV 10.5 km"]
+[-2.649379253387451, 11.671789169311523, "Imager Sampling duration 4 s"]
+[-2.6428370475769043, 11.705290794372559, "Imager Spectral resolution 0.2 cm -1"]
+[-2.6426331996917725, 11.70783519744873, "Imager SNR >300"]
+[-2.2820775508880615, 11.740549087524414, "Cloud and Aerosol Imager Spectroscopic System Band pass filter"]
+[-2.377676486968994, 11.769401550292969, "Cloud and Aerosol Imager Spatial resolution 1 km"]
+[-2.3659863471984863, 11.698074340820312, "Cloud and Aerosol Imager Spatial resolution 500 m"]
+[-2.314696788787842, 11.660544395446777, "Cloud and Aerosol Imager Spatial resolution 1500 m"]
+[0.10499636828899384, -4.035928726196289, "Satellite Platform Design Principle Accommodates the majority of the platform avionics and equipments in the lower half of the spacecraft, with the upper half of the spacecraft primarily dedicated to accommodating the RemoveDebris payloads"]
+[0.11722280830144882, -4.0225372314453125, "Satellite Platforms Design Principles Use of mature, well developed non space specific protocols such as CAN (Controller Area Network)and LIN (Local Interconnect Network), On board autonomy, Robustness and redundancy, The use of COTS (Commercial-off-the-Shelf) components and technologies, Modularity, Low recurrent costs at unit level"]
+[1.7398754358291626, 6.909066677093506, "Communication Device Uplink Frequency 450MHz"]
+[1.7798466682434082, 6.860103607177734, "Communication Device Uplink Data Rate 9.6 kbit/s"]
+[1.7196630239486694, 6.9121832847595215, "Communication Device Uplink Data Rate 16 kbit/s with FEC (Forward Error Correction)"]
+[1.7092812061309814, 6.929385185241699, "Communication Device Downlink Frequency 468 MHz"]
+[1.766697645187378, 6.880325794219971, "Communication Device Downlink Data Rate 3 Mbit/s"]
+[-1.2586039304733276, 9.38499927520752, "N/A N/A N/A"]
+[-1.5897624492645264, 12.21267032623291, "Infrared Focal Plane Array (FPA) Pixel Size 25 \u00b5m square"]
+[-1.5728955268859863, 12.184480667114258, "Infrared Focal Plane Array (FPA) NEDT 40 mK"]
+[-1.5225259065628052, 12.188689231872559, "Infrared Focal Plane Array (FPA) Optics f/1"]
+[-1.6401410102844238, 12.17073917388916, "Infrared Focal Plane Array (FPA) Drive and Readout Circuits Similar to those of the commercial IR camera"]
+[-13.924193382263184, -2.1383419036865234, "X-ray Telescope Energy Level Up to 11 keV"]
+[-13.57149887084961, -2.0534775257110596, "X-ray Phenomenon Shift Blue-shifted"]
+[-13.85770320892334, -2.263904333114624, "X-ray Telescope Number of Detected Sources About one million"]
+[-0.9672200679779053, 11.181476593017578, "Award Recipient Prize Silver casting of the T. E. S. T. sculpture"]
+[-2.600393295288086, 9.610851287841797, "Power Source Power 750 W (600 W average)"]
+[-3.0455002784729004, 4.271286487579346, "Spacecraft Type 3-axis stabilized"]
+[-3.272158145904541, 4.2388434410095215, "Spacecraft Design Life 2 years"]
+[-3.29398250579834, 4.226390361785889, "Spacecraft Lifetime ~10 years"]
+[-13.904688835144043, -2.2632153034210205, "X-ray Telescope Number of Mirrors 2"]
+[-13.907041549682617, -2.2429263591766357, "X-ray Telescope Detector Type Cadmium-zinc-telluride pixel detectors"]
+[-13.883199691772461, -2.249706506729126, "X-ray Telescope Detector-Mirror Separation 10 m"]
+[-14.045103073120117, -2.341120481491089, "X-ray Telescope Mast Length 10 m"]
+[-5.403921127319336, 2.7723405361175537, "Telescope Deployment Mechanism Trusses and hinges"]
+[-5.476665496826172, 2.714467763900757, "Telescope Stray Light Mitigation Baffles"]
+[-5.4003801345825195, 2.7465832233428955, "Telescope Alignment Mechanism Fine precision mechanism"]
+[-5.248388767242432, 2.7241246700286865, "Telescope Patent Date June 1, 2007"]
+[-3.0754902362823486, 7.291904926300049, "Collision Risk Assessment & Mitigation System Data Filters PoC, miss distance, time to TCA"]
+[-1.5235813856124878, 7.069847106933594, "Tool Alert Method Email"]
+[-5.369049072265625, 7.772724151611328, "Communication Method Content Excel spreadsheet with CM data and value-added analysis results including PoC and delta-V tradespace"]
+[-7.573054790496826, 5.880578517913818, "Camera N/A N/A"]
+[-7.603437423706055, 5.849178791046143, "Camera N/A N/A"]
+[3.453272819519043, 8.12723445892334, "X- and \u03b3-ray detectors Photon Energy Range 20 keV \u2013 10 MeV"]
+[3.4569389820098877, 8.13277816772461, "X- and \u03b3-ray detectors Relativistic e- Energy Range 1 MeV \u2013 10 MeV"]
+[-0.839063823223114, 11.607805252075195, "e- detectors Energy Range 70 keV \u2013 4 MeV"]
+[-4.4866838455200195, 12.12980842590332, "Triaxial search coil magnetometer Frequency Range 5Hz \u2013 20kHz"]
+[-5.501449108123779, 9.570964813232422, "MF Frequency Range 10kHz \u2013 1MHz"]
+[-6.716470241546631, 9.985230445861816, "LF-E (Low Frequency-Electric) antenna Frequency Range DC\u20131 MHz"]
+[-6.72601842880249, 9.993172645568848, "HF-E antenna Frequency Range 100 kHz \u2013 35 MHz"]
+[-2.0255606174468994, 7.391113758087158, "Operating System Type Open-source"]
+[-5.285622596740723, 7.487166881561279, "Protocol Purpose Data transport errors correction in LEO satellite links"]
+[-3.1846461296081543, 7.501784801483154, "Algorithm Purpose Routing in the network layer protocol"]
+[-5.179409503936768, 7.467598915100098, "Network Feature Automatically make use of ground stations or other satellites when available to reach a given target"]
+[1.0823781490325928, 0.7102199792861938, "Earth Observation Satellite Purpose Monitoring greenhouse gases such as methane, ozone, water vapour, carbon monoxide and nitrogen dioxide levels"]
+[1.056693434715271, 0.7391088604927063, "Earth Observation Satellite Owner Japan Aerospace Exploration Agency (JAXA)"]
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+[-0.8610102534294128, 12.60877513885498, "Radiation Monitor Electron Detector Surface Area 25 mm2"]
+[-0.8280977010726929, 12.652216911315918, "Radiation Monitor Photon Detector Surface Area 150 mm2"]
+[-0.8309100866317749, 12.638763427734375, "Radiation Monitor Mass 3 kg"]
+[-0.8511212468147278, 12.677689552307129, "Radiation Monitor Power Consumption 5 W"]
+[-0.8743099570274353, 12.71852970123291, "Radiation Monitor Data Output 20 kByte/orbit"]
+[2.797353744506836, 13.719889640808105, "Optical Device Range Accuracy Few centimetres"]
+[-1.730149745941162, 16.987293243408203, "Radar Altimeter Data Management Center Wallops Flight Center, VA"]
+[-2.6958060264587402, 15.329750061035156, "Scanning Multichannel Microwave Radiometer Data Management Center JPL"]
+[-5.891278266906738, 16.012897491455078, "Synthetic Aperture Radar Data Management Center JPL"]
+[-2.994981050491333, 16.187074661254883, "SeaSat-A Scatterometer System Data Management Center LaRC (Langley Research Center)"]
+[-1.4979490041732788, 14.85547924041748, "Visible and Infrared Radiometer Data Management Center GSFC"]
+[0.1385549008846283, 7.182147026062012, "Experiment Module Patch Content Antimicrobial hydrogel"]
+[-1.9886939525604248, 8.029251098632812, "Nutrient Delivery System Delivery System Type Passive"]
+[-1.085729718208313, 5.423615455627441, "Plant Growth Facility Purpose Cultivate leafy greens"]
+[2.634218692779541, 14.345995903015137, "Optical Instrument Mirror Tilt Approximately 4.5\u00ba"]
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+[2.8178091049194336, -1.087038278579712, "Satellite Purpose Measure the density of molecular oxygen in the thermosphere"]
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+[0.906934380531311, -1.2436935901641846, "Satellite Distance Between Disc and Satellite 150 m"]
+[3.023128032684326, -1.5972766876220703, "Satellite Principal Investigator Andrei Zhukov"]
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+[1.7402245998382568, 22.202442169189453, "Instrument Diameter 2 cm"]
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+[2.1239564418792725, -1.8306491374969482, "PolSAR Inversion Rate Validity Criterion 5%"]
+[2.17193865776062, -1.8604398965835571, "PolSAR Soil Moisture Measurement Period April to October"]
+[2.026381015777588, -1.8432376384735107, "PolSAR Soil Moisture Measurement Error 6.2 to 8.5 volume percent"]
+[6.402967929840088, 7.338294982910156, "Satellite Component Functions Launch the laser beam to other S/C, superimpose the received beam and the local oscillator on the PRFs, convert the optical heterodyne signal to electrical signal, enable the beam steering, enable closed loop beam steering, image the OBA entrance aperture and the FSM onto the PRFs"]
+[6.30780553817749, 7.426101207733154, "Satellite Component Features Ultra-stable fiber injector (FIA), beam fine steering mirror (FSM), imaging optics, photoreceiver frontends (PRFs) with the quadrant photodiodes"]
+[2.833038091659546, -1.5090653896331787, "Satellite Mission Objective Collection of high precision scalar magnetic data"]
+[5.267584800720215, -4.057098388671875, "Satellite Launch Year 2011"]
+[4.113764762878418, -3.3247737884521484, "Satellite Data Gap Mid July 2006 through June 2007"]
+[1.922189474105835, -2.044347047805786, "Satellite Lack of Attitude Control Resulted in an almost total lack of GPS timing information"]
+[-8.628655433654785, 13.522475242614746, "Propagator Positional Error 1000 m"]
+[-0.5868210196495056, 1.2818902730941772, "Orbit Refinement Orbital Accuracy \u2264 50 m"]
+[-1.224356770515442, 11.006038665771484, "Cloud Discrimination Instrument Parameter Value"]
+[-3.5332021713256836, 6.7551703453063965, "Data Cloud-Contaminated Value"]
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+[-1.7206902503967285, 6.591516017913818, "Program Program Name SAR/GLONASS"]
+[-1.7288671731948853, 6.624607086181641, "Program Program Name SAR/Galileo"]
+[-4.464352130889893, 8.287732124328613, "MEO Local User Terminals Ground System Component MEOLUTs"]
+[-1.696732759475708, 5.341355323791504, "Mission Control Centers Ground System Component MCCs"]
+[1.5308750867843628, 21.2406005859375, "Instrument Mass 32 kg"]
+[1.5957096815109253, 22.197322845458984, "Instrument Size 80 cm x 50 cm x 25 cm"]
+[1.6136744022369385, 23.226863861083984, "Instrument Power Consumption 50 W in imaging mode (mean power of 29 W)"]
+[2.290924072265625, 22.93621253967285, "Instrument Data Rate 883 kbit/s"]
+[-0.7520347237586975, 3.184361219406128, "Star System Eclipsing Sextuply"]
+[-1.4275705814361572, 6.902977466583252, "Model Projection Orthographic, centered at 90\u00ba West, 30\u00ba North"]
+[-1.4021437168121338, 6.9332075119018555, "Model Magnetization Dominance Areas of negative magnetization are dominated by magnetizations in directions oblique and opposite to that of the present Earth's field"]
+[-1.3920172452926636, 6.944770812988281, "Model Long-wavelength Magnetizations Dominated by the continent-ocean contrast"]
+[-1.3281315565109253, 6.903369426727295, "Model Short wavelength Magnetizations Dominated by seafloor spreading"]
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+[0.7345064878463745, -1.2095355987548828, "Satellite Mean Altitude About 650 km"]
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+[4.035404682159424, -2.8616769313812256, "Satellite Period 97 minutes"]
+[0.6925607323646545, -1.1404720544815063, "Satellite Altitude 835 km"]
+[0.6236485242843628, -2.3806962966918945, "Satellite Inclination 98.7\u00ba"]
+[4.026254653930664, -2.926581621170044, "Satellite Period 101.2 minutes"]
+[-5.0549492835998535, 2.8931782245635986, "Space Telescope Design Concept On-axis, two-mirror, and two-lens corrector system"]
+[-5.104239463806152, 2.885662794113159, "Space Telescope Optical Performance Limits to some extent the optical performance with regard to maximum swath width, MTF degradation, and stray light problems"]
+[-4.934133052825928, 2.920008420944214, "Space Telescope Advantages Low-cost, stable, easier to collimate"]
+[-2.2085702419281006, 5.838696002960205, "Formation Flying Demonstration Mission Unknown Unknown"]
+[-2.196887969970703, 5.852056503295898, "Formation Flying Demonstration Mission Unknown Unknown"]
+[-0.8430168032646179, 11.64285659790039, "Detector Array Size 1.3 mega pixel (1280 x 1024)"]
+[-0.7558056712150574, 11.560392379760742, "Detector Pixel Size 6.7 \u00b5m x 6.7 \u00b5m"]
+[-0.81790691614151, 11.587752342224121, "Detector ROIC Size 640 x 480 pixels"]
+[-0.8371660709381104, 11.606740951538086, "Detector Focal Plane Size 4.3 mm x 3.2 mm"]
+[1.523132085800171, 21.26978874206543, "Instrument Total Mass 120g"]
+[1.8740020990371704, 22.229812622070312, "Instrument Resolution 273.7 m"]
+[1.914084792137146, 22.07305145263672, "Instrument Trace H 175.2 km"]
+[1.8811635971069336, 22.037569046020508, "Instrument Trace V 131.4 km"]
+[-13.847196578979492, -2.20353102684021, "X-ray Telescope Calibration Unknown"]
+[1.853711485862732, -1.4741644859313965, "Satellite Localization Capability Rapid"]
+[1.7055095434188843, -1.4759135246276855, "Satellite Localization Very precise"]
+[1.6856416463851929, -1.330061912536621, "Satellite Localization Larger"]
+[1.8146485090255737, 22.130739212036133, "Instrument Localization Area Large"]
+[-3.4479923248291016, 7.996049880981445, "Signal Processing Method Method Piecewise linear method with cascade amplification"]
+[-3.431381940841675, 8.038856506347656, "Signal Processing Method Number of Bands 4"]
+[-3.4260425567626953, 8.033855438232422, "Signal Processing Method Application Automatic observation of objects with large radiance differences (ocean colour and land vegetation)"]
+[-3.398080825805664, 8.073543548583984, "Signal Processing Method Dynamic Range Wide"]
+[-1.0871851444244385, 5.436977386474609, "Facility Location Suitland, MD"]
+[-1.112472653388977, 5.424805164337158, "Facility Location Wallops, VA"]
+[-1.0993984937667847, 5.425698280334473, "Facility Location Fairmont, WV"]
+[-1.2603203058242798, 9.144163131713867, "Gas Separation Technology Material Calcium-silicate (C-S)"]
+[-1.4302310943603516, 9.12158489227295, "Gas Separation Technology Pore Size 100 nanometers or smaller"]
+[-2.920637369155884, 4.604608058929443, "Spacecraft Payload Capacity More than 400 kg"]
+[-3.1411936283111572, 1.7100600004196167, "Satellite Mission Detectable Binaries Dozens"]
+[-3.1413116455078125, 1.6980072259902954, "Satellite Mission Sensitivity Milky Way systems"]
+[-3.848231554031372, 7.93889045715332, "Data Storage Use Storing larger quantities of data"]
+[-3.65878963470459, 7.576483249664307, "Data Recorder Qualification Program Radiation tests, assembly qualification, construction analysis, electrical characterization, reliability tests like burn-in, destructive physical analysis, stress and life tests"]
+[-7.577115535736084, 5.884855270385742, "Camera Quantity 4"]
+[-0.64622962474823, 9.44896411895752, "Spacecraft Component Design Standard NanoRacks 6U deployer ICD"]
+[-0.6503773927688599, 9.42794132232666, "Spacecraft Component Quantity 2"]
+[-1.1732169389724731, 8.602949142456055, "Dispenser Component Design Feature Engages with tabs"]
+[-0.5980798006057739, 9.49447250366211, "Spacecraft Component Mounting Location Internal components"]
+[6.3383331298828125, 7.404730319976807, "Satellite Component Diameter 4 meters"]
+[11.264954566955566, 5.482260227203369, "CubeSat Mission Type Astronomy"]
+[11.241134643554688, 5.469376087188721, "CubeSat Mission Type Space Weather Science"]
+[11.305770874023438, 5.529940605163574, "CubeSat Mission Type Technology Demonstration"]
+[0.6241070032119751, -1.4272410869598389, "Satellite Orbit Altitude 550 km"]
+[0.6891478300094604, -2.2801480293273926, "Satellite Orbit Inclination 97.6\u00ba"]
+[-0.3469347357749939, 3.803541660308838, "Planet Distance from Earth 80 light-years"]
+[-0.3582732677459717, 3.789564609527588, "Planet Host Star Diameter Roughly 11,000 miles (18,000 km)"]
+[-0.365805447101593, 3.7811038494110107, "Planet Host Star Age Up to 10 billion years old"]
+[-0.40710222721099854, 3.6968562602996826, "Planet Host Star Type White dwarf"]
+[-0.42848828434944153, 3.6868207454681396, "Planet Host Star System Triple star system"]
+[-0.35269981622695923, 3.7936670780181885, "Planet Origin Distance At least 50 times farther away from its present location"]
+[-0.8604732155799866, 7.830394268035889, "Charge Coupled Devices Exposure Time 2 seconds"]
+[-3.340116024017334, 7.314454078674316, "Data Handling Unit Data Product Subarrays (nominally 10 x 10 pixels)"]
+[-1.0847277641296387, 7.584300994873047, "Device Data Processing Extracts subarrays from each 2 min summed image, compresses them and stores them in the SSB"]
+[-3.6890313625335693, 8.036276817321777, "Solid State Buffer Data Storage Stores subarrays and full frame images"]
+[4.993480205535889, -4.1684465408325195, "From SSB Downlink Frequency Every 13.7 days at perigee"]
+[-6.799620628356934, 10.057032585144043, "Antenna Panel Size 2 m x 2 m"]
+[-6.786192417144775, 10.047595977783203, "Antenna Tile Size 1 m x 1 m"]
+[-6.829573154449463, 10.08970832824707, "Antenna Number of Radiating Elements per Tile 24 x 24"]
+[-6.739881992340088, 10.003832817077637, "Antenna Number of Radiating Element Groups per Tile 24"]
+[-6.754538536071777, 10.035574913024902, "Antenna Number of T/R Modules per Group 2"]
+[1.523574709892273, -2.29970645904541, "Satellite Spacecraft Stabilization Three-axis stabilized"]
+[5.002420902252197, -2.3807613849639893, "Satellite Spacecraft Design Life 5-7 years"]
+[1.747361421585083, -1.76790452003479, "Satellite Observation Efficiency 85%"]
+[-2.6288933753967285, 11.703703880310059, "Imager Number of Channels 14"]
+[-2.648008346557617, 11.68626880645752, "Imager Spatial Resolution 0.5-4 km"]
+[-2.655681610107422, 11.662792205810547, "Imager Full Disk Imaging Time 15 minutes"]
+[-1.9285353422164917, 14.844320297241211, "Radiometer Number of Channels 5"]
+[-1.880517601966858, 14.855169296264648, "Radiometer Spatial Resolution 1.25-5 km"]
+[-1.9071351289749146, 14.851820945739746, "Radiometer Full Disk Imaging Time 30 minutes"]
+[-2.463186740875244, 14.08387565612793, "Infrared Sounder Number of Channels 913"]
+[-2.491042137145996, 14.108796119689941, "Infrared Sounder Spectral Resolution 0.8 to 1.6 cm -1"]
+[-2.5039491653442383, 14.08847713470459, "Infrared Sounder Spatial Resolution 16 km"]
+[-2.6797914505004883, 11.716597557067871, "Imager SSP Resolution 7.8 km"]
+[-0.7690547108650208, 12.469104766845703, "Space Environment Monitor Device Type High energy particles"]
+[1.698644757270813, 6.948673725128174, "Communication Device Manufacturer L-3 Communications Inc."]
+[-2.1052498817443848, 7.749258518218994, "Avionics System Manufacturer SEAKR Engineering Inc."]
+[-2.092414140701294, 7.7301530838012695, "Computer System Manufacturer Planning Systems Inc. (PSI)"]
+[1.683148980140686, 6.942581653594971, "Communication Devices Quantity Multiple"]
+[-6.71117639541626, 9.979499816894531, "Antennas Quantity 6"]
+[-6.625394344329834, 9.891826629638672, "Antennas Quantity 2"]
+[1.1338343620300293, 13.206880569458008, "Signal Modulation Carrier frequency (MHz) 1176.45"]
+[1.1216853857040405, 13.195769309997559, "Signal Modulation Data/Pilot Data"]
+[1.1359148025512695, 13.208362579345703, "Signal Modulation Carrier frequency (MHz) 1176.45"]
+[1.1260844469070435, 13.191916465759277, "Signal Modulation Data/Pilot Pilot"]
+[1.1458425521850586, 13.211935043334961, "Signal Modulation Carrier frequency (MHz) 1207.14"]
+[1.1239556074142456, 13.198718070983887, "Signal Modulation Data/Pilot Data"]
+[1.1343514919281006, 13.207019805908203, "Signal Modulation Carrier frequency (MHz) 1207.14"]
+[1.1260088682174683, 13.193620681762695, "Signal Modulation Data/Pilot Pilot"]
+[1.1244499683380127, 13.198370933532715, "Signal Modulation Carrier frequency (MHz) 1278.750"]
+[1.129250168800354, 13.200724601745605, "Signal Modulation Data/Pilot Classified"]
+[1.1243921518325806, 13.200078964233398, "Signal Modulation Carrier frequency (MHz) 1278.750"]
+[1.1274983882904053, 13.198349952697754, "Signal Modulation Data/Pilot Data"]
+[1.1267781257629395, 13.202692031860352, "Signal Modulation Carrier frequency (MHz) 1278.750"]
+[1.1344833374023438, 13.192816734313965, "Signal Modulation Data/Pilot Pilot"]
+[1.139608383178711, 13.20980453491211, "Signal Modulation Carrier frequency (MHz) 1575.420"]
+[1.1318860054016113, 13.202391624450684, "Signal Modulation Data/Pilot Classified"]
+[1.1353206634521484, 13.207563400268555, "Signal Modulation Carrier frequency (MHz) 1575.420"]
+[1.125336766242981, 13.194172859191895, "Signal Modulation Data/Pilot Data"]
+[1.1338859796524048, 13.207972526550293, "Signal Modulation Carrier frequency (MHz) 1575.420"]
+[1.1374567747116089, 13.182833671569824, "Signal Modulation Data/Pilot Pilot"]
+[0.5264697074890137, 11.977185249328613, "Environmental Anomaly Sensor Objective To demonstrate on-orbit autonomous monitoring of the S/C environment and to provide \u201calerts\u201d when satellite charging, SEUs or other radiation events are likely"]
+[0.46461260318756104, 12.064860343933105, "Environmental Anomaly Sensor Data Request Time 72 hours"]
+[0.485338032245636, 12.026678085327148, "Environmental Anomaly Sensor Output Alerts/warnings in terms of a series of ascending order flags, indicating the likelihood and severity of the forthcoming anomalies"]
+[1.7037277221679688, -1.1843132972717285, "Satellite Imaging Resolution 2 m (panchromatic), 8 m (multispectral)"]
+[2.8731985092163086, 22.086469650268555, "Instrument Purpose Imager of Sprites and Upper Atmospheric Lightning"]
+[1.9094949960708618, -1.481826663017273, "Satellite Daily Image Coverage Taiwan and the surrounding region"]
+[1.8328135013580322, -2.147941827774048, "Satellite Orbiting Object Earth"]
+[2.6166608333587646, 21.917434692382812, "Instrument Function Measure how long it takes for light to bounce off the ice and return to the instruments\u2019 sensors"]
+[2.8839683532714844, 21.97574806213379, "Instrument Purpose Calculate the distance between the aircraft or the satellite and the ice surface"]
+[2.8736279010772705, 21.975048065185547, "Instrument Purpose Measure ice height"]
+[2.0938382148742676, -2.6451587677001953, "Satellite Number of Laser Beams 6"]
+[2.7970805168151855, -1.000096082687378, "Satellite Purpose Measure ice height"]
+[2.638216972351074, 13.452170372009277, "Optical Component Purpose Separate VNIR spectral domain into the ten bands B1 to B9"]
+[2.6480913162231445, 13.444869995117188, "Optical Component Purpose Prevent stray light effects"]
+[-1.3989179134368896, 8.611632347106934, "Electronic Component Provides Electrical Interfaces to Detectors Power supply, bias voltages, clock and video signals"]
+[-1.3486779928207397, 8.61323070526123, "Electronic Component Purpose Process the video signals delivered by the FEEs : digitization on 12 bits, numerical processing, compression and image CCSDS packet generation"]
+[-3.5857412815093994, 4.405062198638916, "Spacecraft Launch Date Dec. 2014"]
+[-3.5284502506256104, 4.381947994232178, "Spacecraft Testing Date April 11, 2014"]
+[-3.0134623050689697, 3.95991587638855, "Crew Capsule Test Flight Date Fall 2014"]
+[6.344777584075928, 7.392076015472412, "Satellite Component Built-in Radio System Yes"]
+[6.337914943695068, 7.408918380737305, "Satellite Component SD Card Capacity Pair of SD Cards"]
+[5.2709760665893555, -4.427437782287598, "Satellite Launch Date December 6, 2015"]
+[4.4306864738464355, -3.3934030532836914, "Satellite Launch Time 21:44:57 UTC"]
+[2.7286274433135986, -2.287465810775757, "Satellite Launch Vehicle ULA Atlas-V-401"]
+[2.854830026626587, -2.339843273162842, "Satellite Launch Site SLC-41 (Space Launch Complex-41) at CCAFS (Cape Canaveral Air Force Station), FL"]
+[2.578416347503662, -3.9058749675750732, "Satellite URL http://www.wmo-sat.info/oscar/satellites/view/467"]
+[0.8056135177612305, -1.735823392868042, "Satellite Configuration Field of Regard 500 km"]
+[-2.8063249588012695, 15.281798362731934, "Microwave Radiometer & Scatterometer Objectives Understanding ocean circulation, global water cycle and climate interaction. Soil moisture over Argentina Global sea salinity measurements & Retrieval of soil moisture from Aquarius over Argentina"]
+[-0.3984755277633667, 12.238327980041504, "New Infrared Sensor Technology Objectives Hot spot events, sea surface temperature measurements Monitoring of hot spots caused by biomass fires and volcanic eruptions, estimation of fire radiative power Measurements of sea surface temperature"]
+[-2.7972419261932373, 15.248563766479492, "Microwave Radiometer Objectives Precipitable water, winds speed, sea ice concentration, water vapor, cloud liquid water Measurements of precipitable water and sea surface wind speed (which will enhance the results of Aquarius measurements). Measurements of water vapor, cloud liquid water and sea ice concentration"]
+[-7.497047424316406, 5.962881565093994, "High Sensitivity Camera Objectives Urban lights, electric storms, polar regions, snow cover Measurements of light intensity (urban areas, detection of electric storms, snow coverage, detection of fishing boats and aurora studies)"]
+[-3.7934341430664062, 6.920525550842285, "Data Collection System Objectives Collection of data from the ground segment Collect environmental measured parameters (e.g. meteorological)"]
+[-1.6937437057495117, 14.683317184448242, "Radio Occultation Sounder for Atmosphere Objectives Atmospheric properties Measurements of atmospheric temperature, pressure profiles, and water vapor content"]
+[-1.0731666088104248, 9.762310981750488, "ICARE & SODAD Objectives Effects of cosmic radiation in electronic devices, distribution of micro-particles and space debris Measure the high-energy radiation environment (ICARE). Measure the size distribution of micro- particles and space debris (SODAD)"]
+[-0.5504750609397888, 7.180120468139648, "Technological Demonstration Package Objectives Technology demonstration Position, velocity and time inertial angular velocity determination"]
+[-3.223660707473755, 14.598587036132812, "Interferometric Microwave Imager Frequency Bands L/S/C"]
+[-3.2266361713409424, 14.583418846130371, "Interferometric Microwave Imager Mission Water Cycle Observation"]
+[-1.5563781261444092, 12.82436752319336, "Coronagraph Field of View Unprecedented"]
+[-1.5465284585952759, 12.816248893737793, "Coronagraph Scientific Objectives Understand the physical processes that govern the quiescent solar corona and determine space weather"]
+[2.6459338665008545, 22.47348976135254, "Instrument Bias Negatively biased"]
+[1.790769100189209, 22.78668785095215, "Instrument Energy Range ~100 eV to 14 keV"]
+[2.0824313163757324, 22.42341423034668, "Instrument Resolution 5.2%"]
+[-1.9297332763671875, 6.856810092926025, "Software Function Tracks the solar wind flow speed and autonomously adjusts the energy range"]
+[2.9427356719970703, 22.549484252929688, "Instruments Operation Period Since shortly after launch in August 2001 until August 4, 2004"]
+[2.9083425998687744, 21.952789306640625, "Instrument Purpose Detect the solar wind regime"]
+[0.06156347319483757, 15.343342781066895, "Electron Spectrometer Sensor Head Heritage SWEPAM-E and BAM-E flown on the ACE and the Ulysses missions"]
+[0.058826297521591187, 15.342246055603027, "Electron Spectrometer Field of View 10\u00ba-170\u00ba with respect to the spin axis by 30\u00ba in azimuth"]
+[0.12348182499408722, 15.286700248718262, "Electron Spectrometer Energy Steps 24"]
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+[0.03089543804526329, 15.394694328308105, "Electron Spectrometer Energies Sampled Per Spin 4"]
+[-0.827237606048584, 12.52812671661377, "Yeast Radiation Biosensor Mission Measure effects of space radiation on DNA"]
+[3.0224599838256836, -1.5089008808135986, "Satellite Mission Perform proximity operations with the ICPS post-disposal and record imagery of engineering and historical significance \u2014 as well as of the Earth and moon"]
+[11.791643142700195, 5.285685062408447, "6U CubeSat Propulsion System Inert water"]
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+[2.9878642559051514, -1.432475209236145, "Satellite Mission Help scientists understand the quantity of hydrogen-bearing materials in cold traps in permanently shaded lunar craters"]
+[-3.052442789077759, 4.27052640914917, "Spacecraft Sensor Miniature high-temperature MWIR (Mid-Wave Infrared) sensor"]
+[-3.6300315856933594, 12.761404037475586, "Particle Detector Dark Matter Particle Mass 1 TeV"]
+[-3.646071195602417, 12.762269020080566, "Particle Detector Positron Fraction Unknown"]
+[-3.6398935317993164, 12.7637300491333, "Particle Detector Anti-proton Fraction Unknown"]
+[-1.5899301767349243, 4.1092000007629395, "Ground Segment Components Mission management, product generation, product distribution, enterprise management"]
+[-1.0215355157852173, 4.969876766204834, "Remote Backup Facility Function Provide backup facility"]
+[-3.3229918479919434, 7.428335189819336, "Advanced Weather Information Processing System Distribution Subset of product generation element"]
+[6.184640407562256, 7.554810047149658, "Satellite Component Quantity 1 per CubeSat"]
+[1.695909857749939, 6.950850009918213, "Communication Device Function Communicate with the platform"]
+[11.341914176940918, 5.54144287109375, "CubeSat Communication Does not have a communication link directly with Earth"]
+[11.272406578063965, 5.498168468475342, "CubeSat Additional Board Control of the air valve and the CGG system"]
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+[-5.812109470367432, 15.963343620300293, "Synthetic Aperture Radar (SAR) Monitoring Vegetation, ice and oceans"]
+[-5.847996234893799, 16.059988021850586, "Synthetic Aperture Radar (SAR) Launch Date Mid-2027"]
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+[-2.599074125289917, 4.046811103820801, "Space Phenomenon Magnetic Reconnection Occurs at one or more places along the dayside magnetopause"]
+[-2.6330318450927734, 4.043998718261719, "Space Phenomenon Charged Particle Flow From the magnetosheath flow along the newly opened magnetic field lines into the cusps"]
+[4.851568222045898, -4.463742733001709, "Satellite Image Acquisition Date October 8, 2019"]
+[3.6932222843170166, -2.566448450088501, "Satellite Image Acquisition Frequency Almost every 24 days"]
+[-0.4662816822528839, 4.918818473815918, "Island Height More than 120 meters over the surrounding terrain"]
+[-3.05568528175354, 4.420690536499023, "Sailing Ship Number of People 40"]
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+[-7.574950218200684, 5.876935958862305, "Camera FOV \u00b128.63\u00ba"]
+[-7.506565093994141, 5.935853958129883, "Camera Ground Resolution 55 m"]
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+[-7.578037261962891, 5.8888444900512695, "Camera MTF > 0.65 at 38.5 lp/mm"]
+[-7.508621692657471, 5.840915679931641, "Camera Global MTF > 0.23 at 38.5 lp/mm for B13, B14 and B15 bands, and > 0.18 at 38.5 lp/mm for B16 band"]
+[-7.6144561767578125, 5.833765029907227, "Camera Distortion < 3.0%"]
+[-7.565239429473877, 5.88218355178833, "Camera Polarization Sensitivity < 7.0 %"]
+[-7.597308158874512, 5.858972549438477, "Camera Field Illumination Constant within \u00b1 3.0%"]
+[-7.527872562408447, 5.918219089508057, "Camera Band-to-Band Registration < 5.2 \u00b5m"]
+[-7.519481658935547, 5.942711353302002, "Camera Mean Temperature of Operation 17.5\u00baC"]
+[-7.558582782745361, 5.894435882568359, "Camera Temperature Range 15\u00baC \u2013 20\u00baC"]
+[-1.5970715284347534, 8.211545944213867, "Robotic System Life on Station 2 years"]
+[-1.5344783067703247, 8.283892631530762, "Robotic System Cryogenic Liquid Methane Transfer Objective"]
+[-1.637060523033142, 8.310832023620605, "Robotic System Maintain Cryogen Fluid Mass 6 months"]
+[2.885281562805176, 21.98269271850586, "Instrument Purpose Observe Earth to detect smoke and fires, as well as measure crop transevaporation"]
+[-1.8415294885635376, 7.854307651519775, "Task Purpose In-space assessment of fiducials (decals) with unique patterns that enhance machine vision algorithms and aid in autonomous rendezvous and tool positioning"]
+[-0.9563580751419067, 7.722399711608887, "Medical Device Usage Vein scans"]
+[-0.6114951968193054, 6.809503078460693, "Research Study Purpose Investigates cardiovascular health in space"]
+[-3.0470693111419678, 4.312183380126953, "Spacecraft Unpressurized Trunk New pair of solar arrays"]
+[5.326030731201172, -4.452882289886475, "Satellite Mission Start Date October 30, 2019"]
+[-0.6281419992446899, 3.2149970531463623, "Stars Physical Properties Mass, size and age"]
+[-0.61976557970047, 3.222132682800293, "Star Evolutionary State Red-giant phase"]
+[0.561470091342926, 4.656293869018555, "Phenomenon Effect Brought the planet inward from its original, wider orbit"]
+[-7.396919250488281, 2.865898609161377, "Cosmic Ray Detector Proton-to-Helium Flux Ratio Decreases with rigidity"]
+[-7.390782833099365, 2.8701326847076416, "Cosmic Ray Detector Be/B Ratio Increases with energy"]
+[-7.3982157707214355, 2.8674564361572266, "Cosmic Ray Detector Age of Cosmic Rays in the Galaxy ~12 million years"]
+[-7.397498607635498, 2.8692946434020996, "Cosmic Ray Detector B/C Flux Ratio Well described by a single power law B/C= kRd with d = -0.333\u00b10.015"]
+[-3.621382236480713, 12.732368469238281, "Particle Detector Energy Range 1 GV to 1.8 TV"]
+[-3.6627652645111084, 12.788100242614746, "Particle Detector Energy Range 2 GV to 3 TV"]
+[-3.612421751022339, 12.75101089477539, "Particle Detector Energy Range 1 GeV to 500 GeV"]
+[-3.612995147705078, 12.748749732971191, "Particle Detector Energy Range 1 GeV to 350 GeV"]
+[-3.633282423019409, 12.733579635620117, "Particle Detector Energy Range 0.5 Gev to 700 GeV"]
+[-3.6099088191986084, 12.748845100402832, "Particle Detector Energy Range 0.5 GV to 500 GV"]
+[0.10632497072219849, -4.03797721862793, "Satellite Platform In-Orbit Lifetime Up to 10 years"]
+[0.10664388537406921, -4.038166522979736, "Satellite Platform Equipment Selection Minimum Class 2 EEE parts, with compatibility to Class 1 in most cases"]
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+[0.09776530414819717, -4.038042068481445, "Satellite Platform FDIR Concept Hierarchically structured and can easily be adapted to specific mission needs"]
+[11.284279823303223, 5.429206371307373, "CubeSat Ejection Velocity Low"]
+[-1.1051421165466309, 7.778182029724121, "Device Locking Mechanism Flip-out"]
+[11.040046691894531, 5.217514991760254, "CubeSat Deorbiting Yes"]
+[-7.549368858337402, 5.904704570770264, "Camera Resolution High-resolution"]
+[-0.8080736994743347, 12.672111511230469, "Space Radiation Monitor Measurement Ionizing dose of charged particles"]
+[0.6514595150947571, 9.32876968383789, "Attitude Control Subsystem Components Coarse Sun Sensors (CSS), Fine Sun Sensors (FSS), Magnetometers (MAG), Fiber-optical Gyros (Gyro), Star Sensors (STS)"]
+[-3.0431125164031982, 7.668427467346191, "Central Processing Unit Type Radiation-tolerant processor"]
+[6.241718769073486, 7.49956750869751, "Satellite Component Number of Normal Cameras 24"]
+[6.204176425933838, 7.537631988525391, "Satellite Component Number of Fast Cameras 2"]
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+[-2.297262191772461, 7.43289041519165, "On-Board Computer Processor Type Advanced commercial FPGA"]
+[-2.698962926864624, 9.450502395629883, "Power Generation Type Improved triple junction cell, ultra triple junction cell"]
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+[-2.7003633975982666, 9.438592910766602, "Power Generation Location Five sides of the nanosatellite, sun-facing -Z surface of the spacecraft"]
+[-3.379149913787842, 7.2041850090026855, "Data Handling System PROMs Capacity 32 kbyte"]
+[-3.362370491027832, 7.227159023284912, "Data Handling System Buffering Capacity Three days worth of science data"]
+[-3.354541778564453, 7.190476417541504, "Data Handling System Cycle Time 60 s"]
+[-3.3832898139953613, 7.213903427124023, "Data Handling System Sub-Experiment Allotment Time 5 seconds"]
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+[1.5855224132537842, -1.5111539363861084, "Satellite Mode Imaging Area 530 km x 500 km"]
+[-6.767374038696289, 10.019641876220703, "Antenna Failure Date 2012"]
+[-2.3789024353027344, 9.180790901184082, "Power System Maximum Depth Of Discharge 1% outside of eclipse and 8% during eclipse"]
+[-1.7198091745376587, 9.280487060546875, "Fuel System Remaining Fuel More than 120 kg"]
+[-1.8258001804351807, 9.201129913330078, "Fuel System Average Consumption per Burn 0.011 kg"]
+[2.0608389377593994, -0.5708082318305969, "Satellite Maximum Power Draw 65.5 W"]
+[2.089174747467041, -0.5179668664932251, "Satellite Peak Power Collection 122 W"]
+[2.116528034210205, -0.565332293510437, "Satellite Power Storage 160 W-hr"]
+[2.65281343460083, -1.7425670623779297, "Satellite Flight Software F\u2019 (pronounced F prime) framework from JPL"]
+[-0.1951770782470703, 11.538928985595703, "Environmental Scanner Function Provide essential knowledge about surrounding space"]
+[-0.08908369392156601, 11.61699104309082, "Environmental Scanner Objectives Develop and demonstrate on-orbit, autonomous, compact, light weight, low-power instrumentation to monitor the environment around a spacecraft, and to provide alerts whenever the environment is likely to cause any of the following anomalies: surface charging, deep dielectric charging, single event upsets (SEU's), or radiation dose effects"]
+[11.282591819763184, 5.5181779861450195, "CubeSat Manufacturer PIST (Pakistan Institute of Space Technology)"]
+[11.518484115600586, 5.728076457977295, "CubeSat Size 3U"]
+[-0.7853073477745056, 7.886307239532471, "FemtoSat Size 1.5U"]
+[-0.9828252196311951, 7.784662246704102, "FemtoSat Size 2.5U"]
+[-0.9446200728416443, 7.746068000793457, "FemtoSat Size 1U"]
+[-1.0758241415023804, 7.712253093719482, "PocketQube Size 2.5U"]
+[14.686266899108887, 7.820980072021484, "Nanosatellite Mass 3.5 kg"]
+[14.610593795776367, 7.6852192878723145, "Nanosatellite Size 3U"]
+[14.695882797241211, 7.81979513168335, "Nanosatellite Mass 4 kg"]
+[14.690606117248535, 7.812615871429443, "Nanosatellite Mass 4 kg"]
+[11.516889572143555, 5.74724817276001, "CubeSat Size 2U"]
+[11.180049896240234, 5.417585849761963, "CubeSat Manufacturer EXA (Ecuadorian Civilian Space Agency)"]
+[0.5207781791687012, 12.231193542480469, "Electric Field Sensor Frequency Range 100 kHz to 30 MHz"]
+[0.5212332606315613, 12.154252052307129, "Electric Field Sensor Sensor Type Double-wire Hertz dipole"]
+[0.5643061995506287, 12.16347885131836, "Electric Field Sensor Antenna Preamp Equipped"]
+[-3.032567262649536, 7.78992223739624, "Data Processor Signal Depth 12 bit"]
+[-3.0160508155822754, 7.763186931610107, "Data Processor Sampling Frequency 80 MHz"]
+[0.8308032751083374, -4.269251346588135, "Satellite Mass 14 kg"]
+[1.1419621706008911, -0.7348365783691406, "Satellite Size About the size of a boot box"]
+[2.087751626968384, -0.5764613747596741, "Satellite Power Requirement None from the rocket"]
+[-1.3099846839904785, 5.472691535949707, "Office Location NASA/MSFC (Marshall Space Flight Center) in Huntsville, Alabama"]
+[-1.071815848350525, 7.850879192352295, "Adapter Location Between the ICPS (Interim Cryogenic Propulsion Stage) and Orion"]
+[-1.774879813194275, 8.49018669128418, "Electronics Digital Conversion 12 bit"]
+[-2.095477819442749, 8.742866516113281, "Electrical Architecture Mass Memory Capacity 64 Gbit"]
+[-2.181187152862549, 8.44077205657959, "Interface Control Module Function Housekeeping"]
+[0.7293359041213989, -1.2283000946044922, "Satellite Ground Path Height Measurement Every 2.3 feet (70 cm)"]
+[2.018331527709961, -1.4439529180526733, "Satellite Data Coverage Continuous around the globe"]
+[2.1312966346740723, -1.217951774597168, "Satellite Laser Instrument Can directly measure both the height of the top of the melt pond and of the ice below"]
+[2.4125916957855225, 13.955693244934082, "Microchannel Plate Coating KBr"]
+[2.2872681617736816, 13.936113357543945, "Microchannel Plate Diameter 40 mm"]
+[-4.507098197937012, 12.067333221435547, "Magnet Surface Field 144.6 mT"]
+[-3.6154937744140625, 12.749957084655762, "Particle Suppression System Proton Suppression Factor 105"]
+[-3.6327412128448486, 12.757061958312988, "Particle Suppression System Electron Suppression More than protons"]
+[-1.320363998413086, 6.1899495124816895, "Personnel Working Depth Shallow water"]
+[-1.2025072574615479, 6.602169990539551, "Survey Method Efficiency Inefficient in shallow waters"]
+[-0.8258565068244934, 5.2637248039245605, "Survey Boundary Water Depth 3.5 meters (11 feet)"]
+[-0.8207629919052124, 5.276832103729248, "Survey Boundary Extension Can extend significant distances from shore"]
+[5.381002426147461, -4.3905839920043945, "Satellite Launch Date January 1975"]
+[4.997453689575195, -3.868194103240967, "Satellite Operation Period 26 June - 10 October 1978"]
+[4.979240417480469, -3.7774622440338135, "Satellite Data Utilization Project Period 1979-1982"]
+[-0.7187901735305786, 3.2516987323760986, "Star Tracker Purpose Precise reconstruction of the direction of arrival of high energy gamma rays"]
+[-5.108459949493408, 2.780029296875, "Astro Mapper Responsibility Providing real-time information for compensating the large uncertainties in the ISS flight attitude and the structural degrees of freedom"]
+[-0.0753650888800621, 15.513020515441895, "Spectrometer Purpose Look for antimatter in cosmic rays above the atmosphere"]
+[3.2252326011657715, 2.3755125999450684, "Satellite Subsystem Performance On-Orbit"]
+[3.2219936847686768, 2.374154567718506, "Satellite Subsystem Operation ASTERIA"]
+[-2.647568941116333, 11.700350761413574, "Imager Panchromatic Spatial Resolution 2.5 m"]
+[-2.6261768341064453, 11.714737892150879, "Imager Multispectral Spatial Resolution 5 m"]
+[-2.651935577392578, 11.680359840393066, "Imager Swath Width 20 km"]
+[-2.689702033996582, 11.626482963562012, "Imager Field of View 720 km"]
+[-2.6607396602630615, 11.66275691986084, "Imager Global Coverage Time Four months"]
+[-2.668658494949341, 11.682707786560059, "Imager Revisit Time Four days"]
+[-0.5928730368614197, 1.2787598371505737, "Orbit Inclination 98.13\u00b0"]
+[-0.5889564156532288, 1.2877206802368164, "Orbit Altitude 686 km"]
+[-0.6144947409629822, 1.3048028945922852, "Orbit Orbital Period 97.7 minutes"]
+[1.1615458726882935, -0.9063953161239624, "Satellite Diameter 1.2 m"]
+[1.1086204051971436, -1.0159227848052979, "Satellite Height 1.35 m"]
+[0.6841831207275391, -4.117064952850342, "Satellite Launch Mass 200 kg"]
+[5.357605457305908, -2.1705198287963867, "Satellite Design Life Five years"]
+[2.7400143146514893, 22.626663208007812, "Instrument Anomalies Present"]
+[3.042309045791626, -1.2178897857666016, "Satellite Mission Goal Provide policy makers with observed and analyzed data on climate changes"]
+[3.0273215770721436, -1.5224257707595825, "Satellite Mission Requirements Defined by MOE, NIES, and JAXA"]
+[2.9408411979675293, -2.107391119003296, "Satellite Mission Date Unknown"]
+[2.5743961334228516, -3.9309959411621094, "Satellite URL https://www.nasa.gov/feature/goddard/2021/nasa-s-tess-discovers-stellar-siblings-host-teenage-exoplanets"]
+[1.961885929107666, 22.70265007019043, "Instrument Kinetic Energy of Atomic Hydrogen 0.3 eV"]
+[1.8420684337615967, 22.914249420166016, "Instrument Kinetic Energy of Iron (Fe) ~18 eV"]
+[-0.1488969773054123, 15.588703155517578, "Spectrometer Incident Flux Energy Spread \u0394Einc of approximately 18 eV"]
+[-0.1624983847141266, 15.542853355407715, "Spectrometer Mass Resolution 1/50"]
+[-0.024702461436390877, 15.532156944274902, "Spectrometer Final Energy Ef 900 eV"]
+[2.9061620235443115, 22.430540084838867, "Instruments Accelerators Two-aperture ion optic lenses"]
+[2.5761959552764893, 22.274362564086914, "Instrument Photo Image credit: NASA, Debora McCallum"]
+[-7.560909748077393, 5.913116931915283, "Camera Spectral Measurement Broad band"]
+[-7.560572624206543, 5.898468971252441, "Camera Function Maximize the contrast between the TLE and lightning events"]
+[2.879042387008667, 21.99446678161621, "Instrument Purpose Earth observation"]
+[2.893404960632324, 22.00176239013672, "Instrument Purpose Earth observation"]
+[2.8952910900115967, 22.027278900146484, "Instrument Purpose Earth observation"]
+[2.877598524093628, 22.0218448638916, "Instrument Purpose Earth observation"]
+[2.9047224521636963, 22.00075340270996, "Instrument Purpose Earth observation"]
+[2.6337907314300537, 13.452156066894531, "Optical Component Beam Collimation Maintains approximately the same diameter"]
+[2.6469686031341553, 13.417242050170898, "Optical Component Captures the laser beam Yes"]
+[-3.4775502681732178, 8.232954978942871, "Signal Processor Processes the return signal Yes"]
+[8.518414497375488, 13.94298267364502, "Lidar Instrument Operating Mode Mode 2 (532 & 1064 nm backscatter)"]
+[8.517864227294922, 13.94273853302002, "Lidar Instrument Laser Wavelengths 355, 532, 1064 nm"]
+[8.517589569091797, 13.94230842590332, "Lidar Instrument Image Coverage From 30 \u00ba North to 30 \u00ba South"]
+[8.517220497131348, 13.942312240600586, "Lidar Instrument Particle Heights 4 -5 km, 16 km, closer to the ground"]
+[-13.783300399780273, -2.246375799179077, "X-ray Telescope Survey Duration 4 years"]
+[-13.763409614562988, -2.2495486736297607, "X-ray Telescope Survey Duration 2.5 years"]
+[-13.860638618469238, -2.118929862976074, "X-ray Telescope Energy Band 0.3\u201311 keV"]
+[-13.904101371765137, -2.1380674839019775, "X-ray Telescope Energy Band Up to 30 keV"]
+[-1.9014396667480469, 8.092799186706543, "System Performance Excellent"]
+[-1.8809130191802979, 8.106974601745605, "System Performance Nominal"]
+[-1.90651535987854, 8.110506057739258, "System Performance Nominal"]
+[-1.2349169254302979, 8.605962753295898, "Component Charring Consistent with expectations"]
+[-1.909221887588501, 8.081036567687988, "System Performance As expected"]
+[-1.2559853792190552, 8.564225196838379, "Component Pressure Maintained"]
+[-1.9322919845581055, 8.105310440063477, "System Performance As expected"]
+[-1.8980180025100708, 8.05886459350586, "System Performance Successful"]
+[3.0626323223114014, -1.5226925611495972, "Satellite Mission Type Small-scale planetary missions"]
+[2.854074239730835, -1.0412046909332275, "Satellite Purpose Provide useful scientific data"]
+[3.1974146366119385, -1.7551392316818237, "Satellite Manufacturer Morehead State University, NASA/GSFC, Busek Company"]
+[16.982898712158203, 6.733456134796143, "Microsatellite Launch Date 29 July 2009"]
+[16.87364959716797, 6.842570781707764, "Microsatellite Agency INTA"]
+[16.901599884033203, 6.822793006896973, "Microsatellite Mission Type Non-EO"]
+[16.969369888305664, 6.747103214263916, "Microsatellite Launch Date 29 July 2009"]
+[16.968624114990234, 6.748001575469971, "Microsatellite Launch Date 29 July 2009"]
+[2.6459217071533203, 14.280223846435547, "Optical Instrument Image Size 24\u00ba x 24\u00ba"]
+[2.59381103515625, 14.261173248291016, "Optical Instrument 50% Ensquared-Energy Half-Width 15 \u00b5m (one pixel or 0.35 arcmin)"]
+[2.6272993087768555, 14.32308578491211, "Optical Instrument Accessory Function Reduces the effects of scattered light from the Earth and Moon"]
+[1.7395685911178589, -1.358911156654358, "Satellite Temporal Resolution High"]
+[1.681681513786316, -1.2837579250335693, "Satellite Spatial Resolution High"]
+[2.2370619773864746, -2.5387094020843506, "Satellite Red Edge Bands 3"]
+[2.8106865882873535, -1.1524075269699097, "Satellite Application Plant health monitoring"]
+[-3.0369644165039062, 7.021575927734375, "Command and Data Handling System Total Mass 8 kg"]
+[-3.0384480953216553, 7.047277450561523, "Command and Data Handling System Peak Power 66W (allocated), 34W (measured @ 30\u00baC) at 28V"]
+[-3.018026351928711, 6.997076988220215, "Command and Data Handling System Dimensions 27.5 cm x 20 cm x 17.5 cm"]
+[-3.083188533782959, 7.080035209655762, "Command and Data Handling System Processor Speed 1500 MIPS"]
+[-3.027595043182373, 7.052839279174805, "Command and Data Handling System Volatile Mass Storage 10 GByte"]
+[-3.0402724742889404, 7.027202129364014, "Command and Data Handling System Serial Interfaces 12"]
+[-3.0294175148010254, 7.028071880340576, "Command and Data Handling System Power Supply Card Conditioning raw 28 V spacecraft power to conditioned supply voltages for ECS components"]
+[-0.9566859602928162, 11.724093437194824, "Detector Array Type Pushbroom"]
+[1.615086317062378, 10.722428321838379, "Imaging Parameter Value 15 m"]
+[1.626867413520813, 10.714284896850586, "Imaging Parameter Value 50-60 m"]
+[1.6077269315719604, 10.717309951782227, "Imaging Parameter Value 15 km"]
+[1.6175897121429443, 10.71290111541748, "Imaging Parameter Range 400-1000 nm"]
+[1.6665806770324707, 10.716336250305176, "Imaging Parameter Value 500 Hz"]
+[1.5920472145080566, 10.716743469238281, "Imaging Parameter Value 10 bit"]
+[-5.377744197845459, 2.7888805866241455, "Telescope Diameter 150 mm"]
+[-5.419678211212158, 2.809237003326416, "Telescope Type Cassegrain reflective telescope with correcting lenses (a catadioptric optical system)"]
+[-5.32959508895874, 2.826686382293701, "Telescope Parameter Value 1.38\u00ba"]
+[-5.2917633056640625, 2.7656431198120117, "Telescope Parameter Value 24 \u00b5rad"]
+[1.6556085348129272, 10.724868774414062, "Imaging Parameter Value > 100 (peak)"]
+[-0.4273655414581299, 14.512443542480469, "Imaging Instrument Mass ~ 10 kg"]
+[-1.9100677967071533, 14.848365783691406, "Radiometer Frequency L-/S-/C-band"]
+[-1.9413796663284302, 14.894288063049316, "Radiometer Resolution 15 - 50 km"]
+[-1.8508708477020264, 14.809700012207031, "Radiometer Reflector Size 6 m x 6 m"]
+[-3.338878870010376, 14.532926559448242, "Microwave Radiometric Imager Frequency 6.8 to 150 GHz"]
+[-3.4531209468841553, 14.41234302520752, "Microwave Radiometric Imager Resolution Unfocused SAR"]
+[-2.986192226409912, 16.125865936279297, "Dual-frequency Polarised Scatterometer Resolution 2 - 5 km"]
+[-3.0013208389282227, 16.11460304260254, "Dual-frequency Polarised Scatterometer Swath 1000 km"]
+[-2.9459311962127686, 16.086685180664062, "Dual-frequency Polarised Scatterometer Reflector Size 1.8 m diameter"]
+[-5.550960540771484, 2.9321441650390625, "Photomultiplier Tube Signal Range From a few photo-electrons for MIP to ~ 105 photo-electrons for electromagnetic showers"]
+[-2.0926706790924072, 8.6675386428833, "Electronic System Power Consumption Limited to 100 W"]
+[-2.295257329940796, 15.071642875671387, "Electromagnetic Calorimeter Energy Measurement Range 1 GeV to few TeV"]
+[-2.333299398422241, 15.101957321166992, "Electromagnetic Calorimeter Angular Resolution < 1\u00ba @ E > 50 GeV"]
+[-2.3408613204956055, 15.09431266784668, "Electromagnetic Calorimeter Gamma Efficiency > 90% above 2 GeV"]
+[-2.7778851985931396, 14.204734802246094, "Sounder Scene Spacing 480 km for the earlier instruments, 50 km for the lower atmosphere and 75 km altitude for the upper atmosphere measurements"]
+[-2.7863898277282715, 14.201059341430664, "Sounder Frequency 85 GHz was changed to 91 GHz"]
+[-2.7847890853881836, 14.191411972045898, "Sounder Channel 8 at 150 GHz"]
+[-2.7946829795837402, 14.186080932617188, "Sounder Scan Rate 31.9 scans/min (or 1.88 s/scan)"]
+[3.8701388835906982, -2.5367586612701416, "Satellite Ground Segment Development Completion Almost a decade after launch"]
+[2.618548631668091, -2.151454448699951, "Satellite TT&C Stations Completion Two decades after completion of the TT&C (Telemetry, Tracking, and Command) stations originally installed for RADARSAT-1"]
+[2.3588650226593018, -1.522735357284546, "Satellite SAR Processor Upgrade New and improved image products"]
+[1.4071414470672607, -2.0019097328186035, "Satellite Ground Processed Orbit Determination Accuracy Improvement Significant ground processed orbit determination accuracy improvement"]
+[2.3683435916900635, -2.158904790878296, "Satellite X-band SAR Data Reception Stations 26 sites"]
+[-3.0188300609588623, 4.332014560699463, "6U Spacecraft Purpose Understand the radiation environment in the region of space around Earth"]
+[11.220270156860352, 5.374207019805908, "CubeSat Purpose Demonstrate the technology for low-cost and very small spacecraft to explore the lunar surface"]
+[11.244635581970215, 5.475744724273682, "CubeSat Purpose Demonstrate the ability to perform operations in close proximity of the ICPS"]
+[2.5612237453460693, -2.0959341526031494, "Satellite Bus Type Block 5D-3"]
+[1.7517222166061401, -2.061911106109619, "Satellite Attitude Control System Advanced"]
+[2.4578909873962402, -2.2024219036102295, "Satellite Onboard Computer Memory Increased"]
+[1.8327618837356567, -2.2528915405273438, "Satellite Command Link Rate Higher"]
+[1.9308634996414185, -1.5543322563171387, "Satellite Battery Capacity Increased"]
+[4.448987007141113, -2.536590814590454, "Satellite Onboard Autonomy 60 days"]
+[1.4030169248580933, -2.535451889038086, "Satellite Orbit Type Sun-synchronous"]
+[0.7097707986831665, -1.149341106414795, "Satellite Altitude 811 - 853 km"]
+[0.6484702825546265, -2.3374855518341064, "Satellite Inclination 98.9\u00ba"]
+[4.045714855194092, -2.8636960983276367, "Satellite Period 101.6 minutes"]
+[0.7125435471534729, -1.1599373817443848, "Satellite Altitude 271.5 km and 216.8 km"]
+[0.6819143891334534, -1.1945111751556396, "Satellite Altitude 250 km, 240 km, 230 km, 181.1 km, and 167.4 km"]
+[0.7734590768814087, -1.1515663862228394, "Satellite Altitude 180 km"]
+[3.1327764987945557, -1.714314579963684, "Satellite Operation Gas jet is turned on in addition to the ion engines to withstand the drag"]
+[-5.856370449066162, 16.000391006469727, "Synthetic Aperture Radar Launch Date 2023"]
+[-5.861946105957031, 15.969717025756836, "Synthetic Aperture Radar Ground Level Measurement Resolution Higher than Sentinel-1"]
+[-5.860014915466309, 15.988490104675293, "Synthetic Aperture Radar Dataset Combination GRACE Follow-On data"]
+[-3.594778060913086, 4.408722877502441, "Spacecraft Launch Date June 3, 2021"]
+[-3.5887699127197266, 4.439207077026367, "Spacecraft Docking Date June 5"]
+[-3.396383047103882, 4.247836112976074, "Spacecraft Duration at Space Station About a month"]
+[0.07708922773599625, 7.1305999755859375, "Experiment Measurement Delays in GPS signals through the atmosphere"]
+[5.163480281829834, -4.460071563720703, "Satellite Occultation Trials January 2009 to June 2009"]
+[2.1441941261291504, -2.0270025730133057, "Satellite Attitude Demonstration Operations Third quarter of 2008"]
+[1.4188666343688965, 7.030811309814453, "Communication Equipment LEO-to-ground Communication Link Speed 5.625 Gbit/s"]
+[1.450561761856079, 7.023584365844727, "Communication Equipment GEO-to-ground Communication Link Speed 2.8 Gbit/s"]
+[1.364161491394043, 7.067459583282471, "Communication Equipment Orbit Altitude 786 km"]
+[1.3238147497177124, 7.1024675369262695, "Communication Equipment Orbit Inclination 98.5\u00ba"]
+[1.3400611877441406, 7.077475547790527, "Communication Equipment Revolutions per Day 14+3/10"]
+[1.3580907583236694, 7.063786029815674, "Communication Equipment Local Time at Descending Node 10:30 hours"]
+[1.4362226724624634, 7.011847496032715, "Communication Equipment Revisit Cycle 5 day"]
+[3.3278005123138428, 0.46046003699302673, "Satellite Program Critical Design Review Completion Date April"]
+[3.328253746032715, 0.460134893655777, "Satellite Program Milestone B Certification Date May 15"]
+[3.3247382640838623, 0.4610440731048584, "Satellite Program Program Manager Lt. Col. Wilfredo Ruiz"]
+[2.4571681022644043, 22.84478187561035, "Instrument Number of Bands 8 (threshold), 12 (goal)"]
+[2.0610077381134033, 22.64597511291504, "Instrument Band Wavelengths 0.64\u00b10.05, 1.61\u00b10.03; 3.9\u00b10.1; 6.15\u00b10.45; 7.0\u00b10.2; 10.7\u00b10.5; 12.0\u00b10.5; 13.3\u00b10.3"]
+[1.523047924041748, 21.236738204956055, "Instrument Mass <125 kg"]
+[1.6671290397644043, 23.17821502685547, "Instrument Power <256 W"]
+[2.006545305252075, 22.42706298828125, "Instrument Volume <0.8 m 3"]
+[2.881551742553711, 23.03982925415039, "Instrument Lifetime 10 years"]
+[3.4508237838745117, 13.446864128112793, "Laser Communication Terminal Design/Qualification Approach Identical for GEO and LEO application"]
+[-0.7565485239028931, 8.855772018432617, "Heat Transfer System Interface Temperature Between -10\u00baC and +15\u00baC"]
+[2.7926809787750244, 22.450389862060547, "Instrument Type Other"]
+[2.518110990524292, 22.106386184692383, "Instrument Measurement Domain Atmosphere, Ocean, Land, Gravity and Magnetic Fields, Snow & Ice"]
+[2.781146764755249, 22.518848419189453, "Instrument Type Imaging microwave radars"]
+[2.5281617641448975, 22.26144790649414, "Instrument Measurement Domain Ocean imagery and water leaving spectral radiance, Land surface imagery, Vegetation type, Fire fractional cover, Earth surface albedo, Land surface temperature, Land surface topography, Wind vector over sea surface (horizontal), Sea-ice cover, Snow cover, Soil moisture at the surface, Iceberg fractional cover, Sea-ice type, Glacier motion, Sea-ice sheet topography, Oil spill cover, Crustal Motion, Above Ground Biomass (AGB), Active Fire Detection, Snow melting status (wet/dry)"]
+[4.212975978851318, -2.5219576358795166, "Satellite Revisit Rate 5 days"]
+[2.661529541015625, -1.163084864616394, "Satellite Objective Provide remote sensing images to observe and monitor vegetation, deforestation in the Amazon region, water resources, agriculture, urban growth, land use and education"]
+[-3.2247865200042725, 14.611654281616211, "Interferometric Microwave Imager Frequencies L-, S-, C-band 6.8, 10.65, 18.7, 23.8, 37, 89, 150 GHz X-band, Ku-band"]
+[-3.2196595668792725, 14.589557647705078, "Interferometric Microwave Imager Mean Spatial Resolution 15~50 km 4~50 km 2~5 km"]
+[-3.2440106868743896, 14.596477508544922, "Interferometric Microwave Imager Swath Width >1000 km > 1000 km > 1000 km"]
+[-3.219947099685669, 14.611588478088379, "Interferometric Microwave Imager Sensitivity 0.1~0.2 K 0.3~0.5 K 0.5 dB"]
+[-3.2447822093963623, 14.5838623046875, "Interferometric Microwave Imager Polarisation Mode Full-polarisation Full-polarisation for selected frequencies Full-polarisation"]
+[-3.2339351177215576, 14.58332633972168, "Interferometric Microwave Imager Temporal Resolution 2-3 days 2-3 days 2-3 days"]
+[-3.255678176879883, 14.581205368041992, "Interferometric Microwave Imager Reflector Size 9 m x 6 m"]
+[-3.2436187267303467, 14.587181091308594, "Interferometric Microwave Imager Objective Provide an advanced measurement capability on soil moisture and ocean salinity parameters from space"]
+[0.6153842210769653, 9.341635704040527, "Attitude Control Subsystem Sensor Type 3-axis magnetic sensor"]
+[0.2550947070121765, 12.371898651123047, "Coarse Solar Sensors Sensor Type GaAs cells and experimental porous Si cells"]
+[0.26408275961875916, 12.359429359436035, "Coarse Solar Sensors Accuracy 0.2\u00ba"]
+[-5.916140556335449, 15.98004150390625, "Synthetic Aperture Radar Wavelength 9.6 cm"]
+[-5.901771068572998, 16.023012161254883, "Synthetic Aperture Radar Frequency 3.13 GHz"]
+[-5.904016971588135, 16.00840187072754, "Synthetic Aperture Radar Incidence-angle Range 20-55\u00ba"]
+[-2.0863037109375, 7.573297023773193, "Printed Circuit Board Dimensions 75 mm by 65 mm"]
+[7.463981628417969, 12.59681510925293, "Satellite Instrument Observation Date November 4-5, 2018"]
+[7.393178462982178, 12.537761688232422, "Satellite Instrument Observation Date December 10, 2019"]
+[5.005436897277832, -4.4394707679748535, "Satellite Observation Date December 10, 2019"]
+[0.5914451479911804, 4.096284866333008, "Atmospheric Region Altitude Range 50 to 400 miles"]
+[-3.6690149307250977, 12.727198600769043, "Particle Detector Experiment Start Date September 2011"]
+[-3.6383895874023438, 12.767897605895996, "Particle Detector Collaboration AMS Collaboration"]
+[2.0150887966156006, -1.8685516119003296, "Satellite Observation Band 171 \u00c5"]
+[4.839813709259033, -4.4694719314575195, "Satellite Image Date Nov. 6, 1999"]
+[5.235753059387207, -4.399413585662842, "Satellite Extended Mission Start Date April 1999"]
+[0.876001238822937, -1.2760021686553955, "Satellite Loop Span 30 or more times the diameter of planet Earth"]
+[-4.218212127685547, 9.090350151062012, "Digital Chirp Generator Bandwidth 0-75 MHz"]
+[-3.670245409011841, 7.6387505531311035, "Data Acquisition and Compression Subsystem Signal Quantization 8 bit I/Q"]
+[-3.6764638423919678, 7.611028671264648, "Data Acquisition and Compression Subsystem Data Compression Algorithm Real-time flexible BAQ (Block Adaptive Quantization)"]
+[2.8577334880828857, -3.346616268157959, "Communication Satellite Launch Date 24 July 2019"]
+[2.6926605701446533, -3.2664496898651123, "Communication Satellite Orbit Position Geostationary orbit at 31\u00b0 East"]
+[-5.29615592956543, 7.820643424987793, "Communication Network Data Transmission Rate 1.8 Gbit/s"]
+[2.7770488262176514, -3.315206527709961, "Communication Satellite Number of Laser Terminals 3"]
+[-1.705991506576538, 9.330363273620605, "Blow-down System Propellant Hydrazine"]
+[-1.7730090618133545, 9.224527359008789, "Blow-down System \u0394V 80 m/s"]
+[-1.6927987337112427, 9.329460144042969, "Blow-down System Thruster Thrust 1 N"]
+[0.9793296456336975, -4.382033348083496, "Satellite Mass ~165 kg"]
+[1.1281722784042358, -0.730484664440155, "Satellite Size 98 cm x 107 cm x 115 cm"]
+[5.096780300140381, -2.292586326599121, "Satellite Design Life 2 years"]
+[-5.219677925109863, 7.780877113342285, "Communication System Mass Memory Capacity 16 Gbit"]
+[-5.1918134689331055, 7.765293121337891, "Communication System Downlink Data Rate 16.8 Mbit/s"]
+[-5.148830890655518, 7.725159168243408, "Communication System Data Volume ~ 4 GB/day"]
+[1.1815602779388428, -0.7992823719978333, "Satellite Size 0.10 x 0.20 x 0.30 m"]
+[0.9804384708404541, -4.402205944061279, "Satellite Mass 11 kg"]
+[2.1051597595214844, -0.712721586227417, "Satellite Power Source Body-mounted solar panels, two deployable panels, 48 Watt-hour batteries"]
+[2.733293294906616, -1.9514126777648926, "Satellite Onboard Computer ARM A8 Linux-based"]
+[2.6717965602874756, -2.725687026977539, "Satellite Data Rate 19.2kbps"]
+[2.5121548175811768, -2.1638283729553223, "Satellite Ka-Band Terminal Second-generation"]
+[2.731311559677124, -2.7633345127105713, "Satellite Downlink Data Rate 10 and 40Mbps"]
+[3.9832844734191895, -2.7515902519226074, "Satellite Ground Station Passes 11 minutes"]
+[2.1333160400390625, 13.578991889953613, "Lens Material Radiation resistant glasses"]
+[2.1481058597564697, 13.577079772949219, "Lens Composition Doublet, lens, doublet"]
+[2.5655908584594727, 13.833407402038574, "Optical Filter Quantity 4 polarizes and 2 filters"]
+[2.568727731704712, 13.978679656982422, "Optical Filter Wavelength Range 540 nm \u2013 590 nm"]
+[2.5616254806518555, 14.000435829162598, "Optical Filter Center Wavelength 587.6 nm"]
+[-0.6405788660049438, 9.440014839172363, "Spacecraft Component Length 10 m"]
+[-0.6316436529159546, 9.426780700683594, "Spacecraft Component Type Single articulating"]
+[0.48413750529289246, 9.491891860961914, "Attitude Sensing Device Type Multi-head"]
+[1.7143551111221313, 6.939611911773682, "Communication Device Location Malindi, Kenya"]
+[1.0621501207351685, 9.134228706359863, "Attitude and Orbit Determination and Control Subsystem Stabilization 3-axis"]
+[1.0628407001495361, 9.131693840026855, "Attitude and Orbit Determination and Control Subsystem Actuators Four reaction wheels and three magnetorquers"]
+[1.0395684242248535, 9.15139102935791, "Attitude and Orbit Determination and Control Subsystem Off-nadir Body-pointing Capability \u00b130\u00ba in all directions"]
+[-5.5075578689575195, 2.891613245010376, "Telescope and Imager Focal Length 225 mm"]
+[-5.531539440155029, 2.9267759323120117, "Telescope and Imager Aperture 85 mm"]
+[-5.533852577209473, 2.833635091781616, "Telescope and Imager Resolution 29 \u00b5rad/pixel"]
+[-5.552119731903076, 2.9091506004333496, "Telescope and Imager Resolution 6.100/pixel"]
+[-5.493983268737793, 2.871534824371338, "Telescope and Imager Resolution 2.9 m/pixel"]
+[-5.497674465179443, 2.875450611114502, "Telescope and Imager Field Size 2.08\u00ba x 1.67\u00ba"]
+[-5.544802188873291, 2.944129228591919, "Telescope and Imager Design Two-mirror telescope"]
+[-5.507216453552246, 2.856485605239868, "Telescope and Imager Payload Size 1.5U"]
+[-0.9033995866775513, 6.215808868408203, "Website Copyright 2024"]
+[0.3985866904258728, 12.298116683959961, "Sensor Resolution 10 km2"]
+[0.5102800726890564, 12.217949867248535, "Sensor Observation Frequency Every 10 minutes"]
+[0.4794682264328003, 12.179545402526855, "Sensor Field of Regard Sixth of North America"]
+[0.7138510346412659, 12.020200729370117, "Sensor Principal Investigator Kelly Chance"]
+[2.1090800762176514, -2.636950969696045, "Satellite Laser Beams 6"]
+[2.1838886737823486, -1.3995805978775024, "Satellite Ability Detect the seafloor up to 30 m below the surface"]
+[2.4583542346954346, -1.2760438919067383, "Satellite Ability Detect the top of the canopy and the forest floor below"]
+[0.8035459518432617, -1.2036851644515991, "Satellite Height 500 km in space"]
+[2.7841367721557617, -1.0208189487457275, "Satellite Purpose Precisely measure the height of ice and track how it changes over time"]
+[0.7145553827285767, -1.1504939794540405, "Satellite Snow Depth 5 cm (2 inches) in October, 17 cm (6.7 in) in April"]
+[0.6699186563491821, -1.1950769424438477, "Satellite Snow Depth 14 cm (5.5 inches) in October, 27 cm (10.6 inches) in April"]
+[1.6419579982757568, -1.1464580297470093, "Satellite Laser Altimeter Height Measurement Down to about an inch"]
+[1.949562430381775, -1.5160715579986572, "Satellite Laser Altimeter 10,000 pulses of light each second"]
+[1.9518078565597534, -1.2838780879974365, "Satellite Laser Altimeter Records the length of time it takes to make that round trip"]
+[6.327011585235596, 7.4156012535095215, "Satellite Component Material Aluminum honeycomb sandwich panels"]
+[6.35567045211792, 7.388748645782471, "Satellite Component Material Machined aluminum"]
+[-2.5854427814483643, 9.631627082824707, "Power Source Location Three of the four side panels"]
+[6.361264705657959, 7.376680850982666, "Satellite Component Contents Magnetometers, magnetorquers, reaction wheels, gyros, on-board computers, GPS receiver, X50 avionics stack, and batteries"]
+[1.1261382102966309, -0.7180867791175842, "Satellite Structure Dimensions 1.6 m side length, 2.4 m in height"]
+[1.062912106513977, -1.937381386756897, "Satellite Pointing Accuracy < 0.7 km (0.12\u00ba)"]
+[1.0510308742523193, -1.9730602502822876, "Satellite Position Knowledge < 70 m (0.02\u00ba)"]
+[1.7906155586242676, -1.9746906757354736, "Satellite Attitude and Orbit Control Subsystem Components Star sensors, gyroscopes, IRU (Inertial Reference Unit)"]
+[-1.1563916206359863, 5.491662502288818, "Facility Number of Systems 7"]
+[-1.1070702075958252, 5.4595112800598145, "Facility Operator Requirement 4"]
+[-1.0826530456542969, 5.45885705947876, "Facility Image Delivery Time Within one hour after data acquisition"]
+[2.4871292114257812, -1.7409857511520386, "Satellite Image Acquisition Request Available"]
+[-3.0526227951049805, 1.708303451538086, "Earth Observation Mission Operational Period Until 2026-2028"]
+[-5.884611129760742, 16.00853157043457, "Synthetic Aperture Radar Mission Phase Preliminary design phase"]
+[-5.880967140197754, 16.017494201660156, "Synthetic Aperture Radar Frequency L-band"]
+[-5.935476779937744, 16.044443130493164, "Synthetic Aperture Radar Synergy Works in synergy with other Copernicus SAR-based space elements operating at a different frequency"]
+[-10.264565467834473, 9.978279113769531, "Accelerometers Sensitivity Ultra-sensitive"]
+[-0.470574289560318, 5.851552486419678, "Unknown Unknown Unknown"]
+[-5.162605285644531, 8.947936058044434, "RF Module Peak Pulse Power +6 dBm"]
+[-5.126829147338867, 8.9329195022583, "RF Module Center Frequency 5.405 GHz"]
+[-5.165687561035156, 8.96180534362793, "RF Module Maximum Bandwidth 100 MHz"]
+[-5.160740852355957, 8.921893119812012, "RF Module Peak Pulse Output Power (High Power Mode) +40 dBm (10 watts)"]
+[-5.139683723449707, 8.951903343200684, "RF Module Peak Pulse Output Power (Low Power Mode) +38 dBm (6.3 W)"]
+[-5.153387546539307, 8.941662788391113, "RF Module RF Receive Interfaces HP and VP 50 ohm"]
+[5.009027004241943, -4.341427803039551, "Satellite Mission Date 17-19 November 2015"]
+[2.5759167671203613, -3.927313804626465, "Satellite URL http://www.lares-mission.com/LARES_2.asp"]
+[-5.317917823791504, 2.7208845615386963, "Telescope Launch Date Unknown"]
+[3.161632537841797, 22.499675750732422, "Instrument Website http://smsc.cnes.fr/SCARAB/"]
+[3.00740909576416, 22.48805046081543, "Instrument Website http://www.lmd.polytechnique.fr/~Scarab/english/Orbs.htm"]
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+[-1.7386085987091064, 8.466666221618652, "Electronics Function Controls other heaters"]
+[-1.0005089044570923, 7.6895341873168945, "Emergency Device Frequency 121.5/243 MHz"]
+[-0.9884476065635681, 7.62308931350708, "Emergency Device Alert Signal Frequency 406.025 MHz"]
+[-0.9687074422836304, 7.6309895515441895, "Emergency Device Power Source Battery-powered"]
+[-0.9423509240150452, 7.643120765686035, "Emergency Device Usage Maritime applications"]
+[-0.9634609222412109, 7.6550397872924805, "Emergency Device Activation Can be activated in times of trouble to send out help signals"]
+[4.740193843841553, -4.50916051864624, "Satellite Image Capture Date 28 December 2021"]
+[4.618949890136719, -4.568702697753906, "Satellite Image Capture Date 18 December 2021"]
+[4.653434753417969, -4.536754131317139, "Satellite Image Capture Date June 17, 2022"]
+[-1.9300850629806519, 7.334384918212891, "Workstation Application SCPS software"]
+[-3.219650983810425, 4.393917560577393, "Spacecraft Internet Protocol (IP) address Unknown"]
+[-3.1664438247680664, 4.263362884521484, "Spacecraft First spacecraft to have an Internet Protocol (IP) address 1996"]
+[4.666792392730713, -4.543948173522949, "Satellite Image Capture Date March 2018 and March 2022"]
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+[-0.43180862069129944, 5.151147842407227, "Reservoir Current Elevation Just a few meters from the 'minimum power pool'"]
+[2.9772539138793945, -1.3451642990112305, "Satellite Mission Detect the slight signs of change that may foretell an eruption"]
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+[4.415426254272461, -2.6851139068603516, "Satellite Data Collection Duration 518 days"]
+[3.8014578819274902, -2.538886547088623, "Satellite Geographical Position Visit Frequency Every 4 days"]
+[4.547725677490234, -2.6536917686462402, "Satellite Time to Reach Same Altitude About 3 months"]
+[0.677687406539917, -1.268224835395813, "Satellite Altitude Range for Data Collection ~588 km to ~706 km"]
+[-0.12422844022512436, 12.68075180053711, "Sun Sensor FOV (Field of View) Unknown"]
+[-0.12400174885988235, 12.667119026184082, "Sun Sensor Pointing Accuracy Unknown"]
+[-0.14398151636123657, 12.685087203979492, "Sun Sensor Data Format Analog or digital"]
+[-0.16417114436626434, 12.685918807983398, "Sun Sensor Size and Mass Unknown"]
+[2.1483757495880127, -2.093514919281006, "Satellite Attitude Determination and Control Strategies Unknown"]
+[-5.29494571685791, 7.905078887939453, "Communication System Meeting Date October 14th, 2008"]
+[5.295467853546143, -4.50520658493042, "Satellite Launch Date Dec. 7, 2001"]
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+[2.6342506408691406, -2.0597622394561768, "Satellite Tandem Setup Completed Sept. 16, 2002"]
+[1.8509016036987305, -1.1569050550460815, "Satellite Topography Measurement Data High-resolution"]
+[-1.9897971153259277, 7.552716255187988, "Hardware Material Titanium"]
+[-1.9419662952423096, 7.52349853515625, "Hardware Material BK7G18"]
+[-1.9413940906524658, 7.478005886077881, "Hardware Purpose Achieve low thermal noise and high beam pointing stability"]
+[2.111487627029419, -2.157034158706665, "Satellite Control Center Location DLR in Oberpfaffenhofen"]
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+[-1.0908857583999634, 4.531177997589111, "Data Ground Stations Number of Stations Two"]
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+[2.51080060005188, 22.470136642456055, "Instrument Detection Efficiency Maximize"]
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+[-0.8266900777816772, 0.1439715474843979, "Satellite System Detection Capability Near-instantaneous"]
+[-0.8321108818054199, 0.1513233780860901, "Satellite System Tracking Capability Almost instantaneous"]
+[-0.8705223202705383, 0.1843312382698059, "Satellite System Operational Alerts Availability 2014-2016"]
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+[-7.534657001495361, 5.907808780670166, "Digital Camera Lens 400 mm"]
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+[-0.8679314851760864, 5.197617530822754, "City Population 5.4 million in 2012"]
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+[0.5089273452758789, 9.56265926361084, "Attitude Sensor Field of View 33.5\u00ba x 23.5\u00ba"]
+[0.5500401854515076, 9.385879516601562, "Attitude Control Algorithm Spacecraft Spin Rate 1 revolution in 37.5 seconds"]
+[16.980836868286133, 6.741588115692139, "Microsatellite Launch Date Sept. 26, 2016"]
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+[4.1514573097229, -2.6372008323669434, "Satellite Orbit Repeat Cycle 91 days"]
+[5.438803672790527, -4.407958984375, "Satellite Launch Date September 2018"]
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+[3.155599594116211, -1.8239834308624268, "Satellite Science Team Lead Lori Magruder"]
+[4.668147087097168, -2.586278200149536, "Satellite Flight Operations 7 years"]
+[-6.664247989654541, 9.92585563659668, "Antenna Unit Failure 2012"]
+[-3.087301254272461, 9.651351928710938, "Battery Outage Duration Approximately 12 hours"]
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+[-3.213982343673706, 7.356038570404053, "Data Handling Unit Interface BDH unit"]
+[3.6816911697387695, 17.724353790283203, "Payload Controller Function Transmit beam definition command and switching sequence definitions to the active antenna"]
+[-1.9037846326828003, 8.864741325378418, "Tile Control Unit Function Control the beam pointing and the beam setting in a tile"]
+[-5.245580673217773, 2.8771259784698486, "Solar Telescope Field of View 1/10th of the solar disk"]
+[-5.233224391937256, 2.7954835891723633, "Solar Telescope Temporal Cadence About 20-30 seconds"]
+[-5.255056381225586, 2.8023810386657715, "Solar Telescope Memory Compression 12 bit JPEG compression"]
+[-5.224079132080078, 2.8634774684906006, "Solar Telescope Image Quality Dependent upon wavelength and required image quality"]
+[-3.0521392822265625, 4.326159954071045, "Spacecraft Stack Components Conical CM (Crew Module), and a cylindrical SM (Service Module)"]
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+[-2.823260545730591, 4.510075092315674, "Crew Module Function Houses and transports NASA's astronauts during spaceflight missions"]
+[-2.466808557510376, 8.408438682556152, "Service Module Function Contains Orion's propulsion, power and life support systems"]
+[-1.1913516521453857, 7.885956764221191, "Adaptor Function Connects Orion to the launch vehicle"]
+[6.360945701599121, 7.387341499328613, "Satellite Component Battery Type Ni-Cd"]
+[6.358755588531494, 7.445395469665527, "Satellite Component Technology Monocrystalline silicon panels"]
+[6.278257369995117, 7.464738845825195, "Satellite Component Efficiency 15%"]
+[6.288918972015381, 7.4465508460998535, "Satellite Component Efficiency 24%"]
+[6.306673049926758, 7.428554534912109, "Satellite Component Capacity 4Ah"]
+[0.9505823850631714, -4.410069942474365, "Satellite Mass 10 kg"]
+[-13.915194511413574, -2.1162161827087402, "X-ray Telescope Energy Range Greater than 10 keV"]
+[-13.932229995727539, -2.2380385398864746, "X-ray Telescope Total Effective Area Unknown"]
+[-13.709267616271973, -2.263697862625122, "X-ray Telescope Launch Date Q1 2012"]
+[-13.874186515808105, -2.2490899562835693, "X-ray Telescope Mission Status Operational"]
+[-13.932978630065918, -2.2791748046875, "X-ray Telescope Program NASA's Explorer Program"]
+[-2.635559558868408, 9.635744094848633, "Power Source Type Rechargeable"]
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+[-3.0253653526306152, 4.330752849578857, "Spacecraft Structure Type Novel"]
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+[-2.573202133178711, 9.693961143493652, "Energy Source Orientation 40\u00ba ahead of the +Y axis and 40\u00ba behind the -Y axis"]
+[-2.5878090858459473, 9.707696914672852, "Energy Source Tracking 360\u00ba about the axis"]
+[-1.743841528892517, 8.466251373291016, "Electronics Function Process signals from sun sensors and control the array drive motor speed"]
+[-0.7479991912841797, 11.540643692016602, "Position Detector Recording Frequency High"]
+[-0.8875680565834045, 11.63952922821045, "Detector Detection Type Single incoming X-ray photons"]
+[-1.9383211135864258, 8.148064613342285, "System Compatibility Not work with an integrating detector"]
+[0.24732598662376404, 13.802078247070312, "Calibration Device Calibration Process Inserting the ISS orbit attitude information in terms of yaw pitch and roll in the NightPod computer"]
+[0.19167564809322357, 13.765801429748535, "Calibration Device Operational Modes Manual mode, other operational modes"]
+[8.491888999938965, 15.222429275512695, "Camera Mount Mode Function Manually pointing the camera to specific targets and making single-shot pictures"]
+[-1.6955938339233398, 9.312018394470215, "Plasma System Gas Xenon"]
+[-1.4230464696884155, 9.531564712524414, "Thruster Component Flight Test First"]
+[-1.7691841125488281, 9.184967041015625, "Gas Flow Control System Development First flight test"]
+[0.4603712856769562, 9.373278617858887, "Attitude Control System Backup For the magnetorquers for control of S/C precession"]
+[1.0688836574554443, 9.138642311096191, "Attitude and Orbit Control Subsystem Pointing \u00b1 0.05\u00b0 (3\u03c3)"]
+[1.0550391674041748, 9.141325950622559, "Attitude and Orbit Control Subsystem Drift Rate \u00b1 3.0 x 10 -4 \u00ba/s"]
+[1.0688680410385132, 9.135656356811523, "Attitude and Orbit Control Subsystem Sun Sensor 4\u03c0 sun sensor"]
+[1.0749053955078125, 9.129724502563477, "Attitude and Orbit Control Subsystem Magnetometer Magnetometer"]
+[1.0387250185012817, 9.160603523254395, "Attitude and Orbit Control Subsystem IRU Inertial Reference Unit"]
+[1.0944132804870605, 9.10855484008789, "Attitude and Orbit Control Subsystem Star Sensor Star sensor"]
+[1.0595754384994507, 9.140861511230469, "Attitude and Orbit Control Subsystem Earth Sensor Earth sensor"]
+[1.0569684505462646, 9.133893966674805, "Attitude and Orbit Control Subsystem DSS Digital Sun Sensor"]
+[1.0730644464492798, 9.13060188293457, "Attitude and Orbit Control Subsystem SPSS Solar Panel Sun Sensor"]
+[1.078928828239441, 9.131007194519043, "Attitude and Orbit Control Subsystem Thrusters Eight 11 N canted thrusters"]
+[1.0610872507095337, 9.134231567382812, "Attitude and Orbit Control Subsystem Central Thruster One (1) central 11 N thruster"]
+[1.081615686416626, 9.101519584655762, "Attitude and Orbit Control Subsystem Reaction Wheels 4 reaction wheels"]
+[1.0677380561828613, 9.14184856414795, "Attitude and Orbit Control Subsystem Magnetic Torquers Magnetic torquers of 60.0 Am2 capacity"]
+[1.1084635257720947, 9.114969253540039, "Attitude and Orbit Control Subsystem Sun Sensors, Star Sensors, Magnetometer Provide attitude data in the form of absolute attitude errors"]
+[1.1023083925247192, 9.112222671508789, "Attitude and Orbit Control Subsystem Magnetometer, 4\u03c0 Sun Sensor, Temperature Sensor Data are processed in the OBC"]
+[5.3579206466674805, -4.276543140411377, "Satellite Launch Date 2007"]
+[-1.6462558507919312, 5.283030033111572, "Marine Security Operations Centers Locations Halifax and Esquimalt"]
+[-1.6895334720611572, 5.320479869842529, "Marine Security Operations Centers Agencies Department of National Defence (DND), the Royal Canadian Mounted Police, Canada Border Services Agency, the Canadian Coast Guard, the Department of Fisheries and Oceans and Transport Canada"]
+[-3.132683515548706, 1.7349517345428467, "Satellite Mission Formation Flying Operation Phase Duration 7 orbits"]
+[-3.1474461555480957, 1.7010347843170166, "Satellite Mission Relative Drift Velocity 50-60 cm/s"]
+[-3.129920721054077, 1.704933524131775, "Satellite Mission Safe Orbit Range < 1 km"]
+[3.452124834060669, 13.369599342346191, "Laser Transmitter Development Date Feb. 15-18, 2010"]
+[3.6171836853027344, 22.956396102905273, "Instrument Publication Date 2012"]
+[-1.2350664138793945, 6.873049736022949, "Presentation URL http://www.scribd.com/doc/76177455/ICESat-2-ND-Presentation-4-18-11"]
+[1.5013649463653564, -1.4916733503341675, "Satellite Mode Swath 105 to 170 km"]
+[1.545082449913025, -1.4101319313049316, "Satellite Mode Resolution 5 m"]
+[1.6403391361236572, -1.5250362157821655, "Satellite Modes Coverage From 49.54\u00ba to 54.2\u00ba"]
+[1.6226288080215454, -1.546127200126648, "Satellite Modes Range Resolution 1.9 m"]
+[3.758871078491211, 17.7326717376709, "Payload Anomaly Occurrence Decrease About 40%"]
+[-5.860838413238525, 16.01582908630371, "Synthetic Aperture Radar Operation Ground-based"]
+[-1.4018160104751587, 4.356709003448486, "Ground-based operational software system Function Plan user image acquisition requests and generate spacecraft payload sequencing commands"]
+[-2.746251106262207, 7.074023723602295, "Command Sequence Generator Function Generate configuration and timing information and the beam parameters for conducting the SAR payload operations"]
+[-4.374765872955322, 0.18087850511074066, "GPS Receiver Operation Modes C/A and P code, P-codeless (cross-correlation)"]
+[-4.366505146026611, 0.19139915704727173, "GPS Receiver Tracking Dual-frequency code and cross-correlation, data output of up to eight GPS satellites simultaneously"]
+[-4.377116680145264, 0.21377074718475342, "GPS Receiver Sampling Rate 10 Hz"]
+[-4.366731643676758, 0.19271785020828247, "GPS Receiver Mass 4 kg"]
+[-4.401778697967529, 0.164787158370018, "GPS Receiver Power 7-15 W"]
+[1.1767606735229492, 22.101037979125977, "Pushbroom Instrument Spectral Bands 4 bands in the VIS/NIR region"]
+[1.1689544916152954, 22.084562301635742, "Pushbroom Instrument Pixels per Line 21800 pixels/line"]
+[1.2233011722564697, 22.076343536376953, "Pushbroom Instrument Swath 950 km"]
+[1.1979414224624634, 22.093442916870117, "Pushbroom Instrument Spatial Resolution 50 m"]
+[1.1575548648834229, 22.083980560302734, "Pushbroom Instrument Application Monitor vegetation and the coastal zone"]
+[2.583453893661499, -1.6538034677505493, "Satellite Data Distribution Service Available"]
+[-3.614678144454956, 7.081793785095215, "Data Access System Concept Meteosat missions can be combined by the user to provide an integrated data access system"]
+[1.4197947978973389, 2.7330331802368164, "Meteorological Data Dissemination Distribution Potential Particularly across Africa and the Middle East"]
+[-2.4365198612213135, 9.085836410522461, "Power Processing Unit Primary Input Voltage 100 V"]
+[-2.2491090297698975, 9.079736709594727, "Power Control and Conditioning Unit Input Voltage Range 24 V to 32 V"]
+[-1.0995433330535889, 7.677488803863525, "Devices Power Efficiency 90%"]
+[14.521662712097168, 7.682803630828857, "Nanosatellite Manufacturer UTIAS/SFL"]
+[14.528495788574219, 7.682132720947266, "Nanosatellite Manufacturer Aalborg University, Denmark"]
+[14.52375602722168, 7.689001560211182, "Nanosatellite Manufacturer University of Applied Science, Aachen, Germany"]
+[14.493494987487793, 7.662836074829102, "Nanosatellite Manufacturer Technical University of Delft, The Netherlands"]
+[14.530502319335938, 7.6827311515808105, "Nanosatellite Manufacturer Nihon University, Japan"]
+[14.507283210754395, 7.687272071838379, "Nanosatellite Manufacturer Tokyo Institute of Technology (TITech), Japan"]
+[14.515299797058105, 7.692851543426514, "Nanosatellite Manufacturer COM DEV / UTIAS/SFL, Toronto, Canada"]
+[14.489364624023438, 7.658051490783691, "Nanosatellite Manufacturer OHB-System, Bremen, Germany"]
+[14.695236206054688, 7.809848785400391, "Nanosatellite Mass 7 kg"]
+[-5.364845275878906, 2.799734354019165, "Telescope Purpose Study X-ray light"]
+[-5.249714374542236, 3.1389572620391846, "Spectroscopic Telescope Array Manufacturer NASA"]
+[-5.419023513793945, 2.7382662296295166, "Telescope Manufacturer European Space Agency"]
+[2.668659210205078, 22.34771156311035, "Instrument Type Imaging multi-spectral radiometers (vis/IR)"]
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+[2.8541347980499268, 22.4946231842041, "Instrument Type Space environment"]
+[2.85343337059021, 22.480987548828125, "Instrument Type Data collection"]
+[2.7434985637664795, 22.376340866088867, "Instrument Type Lightning sensors"]
+[2.8121562004089355, 22.426029205322266, "Instrument Type Magnetic field"]
+[-7.576582431793213, 5.8798441886901855, "Camera Imaging X-rays"]
+[-0.8062012195587158, 3.20241641998291, "Galaxy Cluster Plasma Temperature Around 50 million degrees"]
+[-0.7933399081230164, 3.225062370300293, "Galaxy Cluster Sky Area Roughly the size of two full Moons"]
+[-0.8022387623786926, 3.2362399101257324, "Galaxy Cluster Sky Area Roughly the size of four full Moons"]
+[2.7118310928344727, 21.92024803161621, "Research Instrument Objective Observe the natural upward lightning discharge phenomena toward the ionosphere on top of the troposphere"]
+[2.7236735820770264, 21.749074935913086, "Research Instrument Requirements Determine the location and timing of luminous phenomena above thunder clouds, obtain a global survey of upper atmospheric optical flash transients"]
+[4.713483810424805, -2.557105541229248, "Satellite Mission Duration 17 years"]
+[5.410241603851318, -4.310600757598877, "Satellite Launch Date December 2016"]
+[5.099240303039551, -3.9028286933898926, "Satellite Planned Launch Year 2033"]
+[-4.239116668701172, 15.763467788696289, "Radar Instrument Delivery Date 3 December 2020"]
+[-4.249500274658203, 15.75469970703125, "Radar Instrument URL https://www.airbus.com/en/newsroom/press-releases/2020-12-airbus-to-deliver-radar-instrument-for-new-copernicus-rose-l"]
+[-0.6402161717414856, 9.442606925964355, "Spacecraft Component Quantity 2"]
+[-0.9439965486526489, 7.740753650665283, "Medical Device Purpose Medical Imaging"]
+[-1.0641953945159912, 7.689576625823975, "Device Purpose Provide tactile and visual feedback to astronauts during robotic operations"]
+[-3.431533098220825, 7.079562664031982, "Data Analysis Tool Signal Repeating Interval 36 days"]
+[2.647136688232422, 22.160837173461914, "Instrument Location Magellan Telescope in Chile"]
+[4.507992744445801, -2.6879971027374268, "Satellite Monitoring Duration Two years"]
+[2.0538790225982666, -2.7779428958892822, "Satellite Number of Small Planets to Deliver Information 50"]
+[-3.9026525020599365, 7.959372520446777, "Data Storage Capability 300 Gbit"]
+[-4.226562976837158, 7.197842597961426, "Data Downlink Maximum Data Rate 640 Mbit/s"]
+[-4.3395161628723145, 7.185182571411133, "Data Downlink Polarizations RHCP and LHCP"]
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+[-0.506445050239563, 15.523425102233887, "Imaging Spectroradiometer Image Acquisition Date Unknown"]
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+[0.061354681849479675, 8.337691307067871, "Crystal Growth Investigation Protein LRRK2 (Leucine-Rich Repeat Kinase 2)"]
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+[2.5873889923095703, -1.6169589757919312, "Satellite Data Access Free"]
+[1.845526933670044, -1.2381470203399658, "Satellite Imaging Capacity More than 250,000 km2 of the ocean in less than a minute"]
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+[-3.6226017475128174, 7.012458324432373, "Data Platform Function Provides near real-time monitoring of fishing activity"]
+[-3.568809747695923, 6.994271278381348, "Data Platform Function Addresses dark vessel detection and supports maritime enforcement initiatives"]
+[-0.03188936412334442, 7.579646110534668, "Material Science Demonstration Objective Monitor the changes in sample thickness as a result of atomic oxygen erosion"]
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+[1.3994654417037964, 5.391854763031006, "Spacecraft Bus Components AM (Avionics Module), PM (Payload Module) structure, harness, ESPA (EELV Secondary Payload Adapter) ring"]
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+[5.2719244956970215, -2.2185935974121094, "Satellite Design Life Seven years"]
+[5.25836181640625, -2.2274389266967773, "Satellite Design Life Seven years"]
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+[5.153499603271484, -3.969303607940674, "Satellite Replacement Year 2025"]
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+[-3.0890228748321533, 2.434441566467285, "Mission Management NASA's Goddard Space Flight Center"]
+[-0.8780470490455627, 3.2999918460845947, "Galaxy X-ray Sources Extremely bright"]
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+[2.5436928272247314, -1.5220333337783813, "Satellite Dataset Availability Public download"]
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+[0.12059768289327621, 7.17565393447876, "Experiment Purpose Provide advance power technology for the Starshine 3 Satellite"]
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+[-2.2427115440368652, 7.023769378662109, "Intelligence Platform Capability Observe, analyze and act on global events"]
+[-2.216526746749878, 7.035597801208496, "Intelligence Platform Imagery Access More than 10 high-resolution imaging spacecraft"]
+[-2.209977865219116, 7.037208080291748, "Intelligence Platform Real-time Image Acquisition Available"]
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+[-1.5217190980911255, 13.454221725463867, "Solar Array Deployment Process Install the electrical cables and drive the final two bolts"]
+[-1.1768025159835815, 8.622461318969727, "Component Width 1.2 mm"]
+[-1.219878077507019, 8.598295211791992, "Component Width 1.6 mm"]
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+[-3.4474425315856934, 6.844219207763672, "Data Product Integration Times User-defined or variable"]
+[-3.424302577972412, 6.794708251953125, "Data Product Integration Not conducted on the spacecraft"]
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+[0.2565661072731018, 11.574947357177734, "Sensor System Absolute Calibration IR yes (10 bit), VIS no (pre-launch, drifts)"]
+[3.7978506088256836, 17.774349212646484, "Payload Thermal Channels Unknown"]
+[3.7126009464263916, 17.68608856201172, "Payload Model MODTRAN"]
+[0.6060426831245422, 12.0565185546875, "Sensor Function Verify the safe centering of the entrance pupil of the coronagraph into the shadow cone of the occulting disc"]
+[0.478744238615036, 11.91828441619873, "Sensor Function Signal to the satellite (CSC) that the umbra moves out of the nominal position range of the SPS"]
+[-5.882920265197754, 16.02224349975586, "Synthetic Aperture Radar Emergency Observation Date November 13, 2016"]
+[-0.12060399353504181, 11.321220397949219, "Forest Early Warning System Monitoring Frequency Once every 45 days"]
+[1.0412400960922241, 0.7500826716423035, "Advanced Land Observing Satellite-2 Launch Date Between 2009 and 2012"]
+[-6.973270416259766, 11.211280822753906, "Active Phased Array Radar Capability Beam steering, multi-beam operations, large bandwidth and high efficiency"]
+[-4.998998641967773, 8.679728507995605, "Transmit/Receive Module Size 170 mm x 70 mm x 20 mm"]
+[-3.293779134750366, 8.737743377685547, "Memory Module Quantity 2"]
+[-3.294973373413086, 8.735176086425781, "Memory Module Quantity 2"]
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+[-1.0731151103973389, 7.712796211242676, "Device Quantity 1"]
+[-3.3172945976257324, 8.77047061920166, "Memory Module Quantity 3"]
+[-1.0876514911651611, 7.676980972290039, "Device Quantity 4"]
+[-2.538571834564209, 9.316418647766113, "Power Converter Quantity 2"]
+[-1.8472940921783447, 7.635498046875, "Board Quantity 10"]
+[-1.8757168054580688, 7.546067237854004, "Board Quantity 18"]
+[-1.0842828750610352, 7.70878791809082, "Device Number of Light Emitters 3"]
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+[-1.0752978324890137, 7.709089756011963, "Device Data Delivery Not usable onboard in real time"]
+[-1.023078203201294, 7.728456020355225, "Device Use Requirement Coronagraph fully operational, door open, and then with the entrance pupil in the umbra or low penumbra"]
+[5.019525051116943, -2.385859251022339, "Satellite Expected Lifetime Five years"]
+[7.361670017242432, 12.480436325073242, "Satellite Instrument Bandwidth 20 nm"]
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+[7.276965618133545, 12.400007247924805, "Satellite Instrument Comments/Observations Polarization moved to 490 nm"]
+[7.279250144958496, 12.400965690612793, "Satellite Instrument Saturation Level 1.1"]
+[7.304896354675293, 12.460027694702148, "Satellite Instrument Band Center 490 nm"]
+[7.266467094421387, 12.406346321105957, "Satellite Instrument Band Center 565 nm"]
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+[7.365048408508301, 12.526288986206055, "Satellite Instrument Band Center 670P nm"]
+[7.3095269203186035, 12.486024856567383, "Satellite Instrument Band Center 865P nm"]
+[7.270151138305664, 12.471908569335938, "Satellite Instrument Band Center 763 nm"]
+[7.312546253204346, 12.468461036682129, "Satellite Instrument Band Center 765 nm"]
+[7.216506004333496, 12.539566040039062, "Satellite Instrument Band Center 910 nm"]
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+[-2.2200448513031006, 8.418163299560547, "Interface Control Unit Power Lines +3.3 V, +5 V, \u00b115 V, \u00b148 V"]
+[-10.264874458312988, 9.979584693908691, "Accelerometer Maximum Acceleration Control Range \u00b12.5 x 10-4ms-2"]
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+[-10.264994621276855, 9.979347229003906, "Accelerometer Measurement Range YACC and ZACC axes \u00b15 x 10-5ms-2"]
+[0.9212889671325684, -4.413207054138184, "Satellite Mass 12 kg"]
+[1.12333345413208, -4.265428066253662, "Communications Satellite Mass 12 kg"]
+[1.2431994676589966, -4.18168830871582, "Communications Satellite Mass 10 kg"]
+[1.0049198865890503, -4.414876937866211, "Scientific Satellite Mass 15 kg"]
+[16.70330238342285, 6.932093143463135, "Technology Minisatellite Mass 110 kg"]
+[-3.1497654914855957, 1.7182037830352783, "Satellite Mission Mission Conception Year 2003"]
+[-3.1482691764831543, 1.6980431079864502, "Satellite Mission Primary Funding AFRL"]
+[-0.535244882106781, 1.2335447072982788, "Satellite Orbit Longer Spacecraft Contact Periods Than in LEO"]
+[-0.5298095941543579, 1.2381572723388672, "Satellite Orbit Uninterrupted Earth Coverage Attractive for a number of observation services"]
+[2.475752830505371, -1.1416199207305908, "Satellite Data Usage Detect the movement of water on Earth based on variations of Earth\u2019s gravity field"]
+[1.5070606470108032, -1.151507019996643, "Satellite Data Resolution 1/8th degree of latitude, or about 8.5 miles"]
+[2.4552268981933594, -1.1586456298828125, "Satellite Data Output Time-varying maps of the distribution of water at three depths: surface soil moisture, root zone soil moisture, and shallow groundwater"]
+[2.6270415782928467, 22.734554290771484, "Instrument Ranging Noise Requirement Unknown"]
+[2.788770914077759, 13.674781799316406, "Optical Device Beam Splitter Unknown"]
+[6.3561248779296875, 7.443289279937744, "Satellite Component FDIR Strategy Fault Detection Isolation and Recovery"]
+[5.051644802093506, -4.321944713592529, "Satellite Operational Date Feb. 2015"]
+[5.220264434814453, -4.124629974365234, "Satellite Collaboration Start Date 2003"]
+[2.356449842453003, -1.0790150165557861, "Satellite Imagery Objective Provide medium resolution satellite imagery as well as expertise to identify locust breeding areas"]
+[-0.9704322814941406, -9.983932495117188, "Satellite Constellation Number of Satellites 6"]
+[-0.9510865211486816, -10.02299976348877, "Satellite Constellation Resolution Sub 30 cm"]
+[-0.9261342883110046, -10.021209716796875, "Satellite Constellation Launch Date 2021"]
+[1.1029928922653198, 0.6418843269348145, "Earth Observation Satellites Imaging Capability To be replaced"]
+[2.6418490409851074, 22.482580184936523, "Instrument Data Products Survey level X-ray and microdosimeter measurements"]
+[2.7121565341949463, 22.34282875061035, "Instrument Data Telemetry All survey data and roughly 1/3 of X-ray imaging data"]
+[2.683582067489624, 22.188915252685547, "Instrument Observation Type Line-of-sight observations"]
+[-3.4442214965820312, 6.845158576965332, "Data Product Energy Band 1/4 keV (R12)"]
+[-3.6333916187286377, 7.203117847442627, "Data Distribution System Storage Capacity Seven days"]
+[-3.7287216186523438, 7.197388648986816, "Data Distribution System Interface Type Subscription-based and ad hoc data requests"]
+[-3.591803550720215, 7.192945957183838, "Data Distribution System API Application Programming Interface"]
+[-3.6618082523345947, 7.234806060791016, "Data Distribution System Interface Type Sectorized cloud and moisture imagery directly to the NWS via the AWIPS interface"]
+[-3.727933406829834, 7.195302486419678, "Data Distribution System Interface Type High availability, low latency distribution channel"]
+[-3.6392290592193604, 7.24086332321167, "Data Distribution System Product Sectorization Parameters Geographic coordinate corner points, Map projection, Spatial resolution, Bit depth, ABI channel, Periodicity"]
+[1.4009720087051392, -2.5356028079986572, "Satellite Orbit Type Sun-synchronous orbit"]
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+[0.6367290616035461, -2.351327657699585, "Satellite Inclination 98.8\u00ba"]
+[4.017704486846924, -2.870335102081299, "Satellite Period 101.1 minutes"]
+[1.4052456617355347, -2.5572457313537598, "Satellite Orbit Type Sun-synchronous orbit"]
+[0.7289994955062866, -1.1215685606002808, "Satellite Altitude 816.3 km"]
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+[4.001755237579346, -2.8988332748413086, "Satellite Period 101.1 minutes"]
+[5.387152194976807, -4.4480366706848145, "Satellite Launch Date November 11, 2016"]
+[3.273960828781128, -1.7497087717056274, "Satellite Manufacturer Maxar company SSL (Space Systems Loral)"]
+[2.6321983337402344, -2.4299490451812744, "Satellite Launch Vehicle Falcon-9"]
+[-3.1497557163238525, 1.7050366401672363, "Polar Survey Mission Duration Eleven Years"]
+[1.8201887607574463, 22.139413833618164, "Instrument Test Range About 12,270 km"]
+[2.139867067337036, 22.525484085083008, "Instrument Accuracy About 10-9"]
+[1.350538730621338, -3.0468969345092773, "Satellites Test Range 12,270 km"]
+[-3.094871759414673, 2.3836710453033447, "Demonstration Mission Cost Low"]
+[-0.38664713501930237, 15.539706230163574, "Imaging Spectroradiometer Ocean Color Information Assists with operational use of maritime patrol aircraft, ships, submarines and sonar performance prediction"]
+[-3.457667827606201, 7.532619476318359, "Automated Identification System Device Type Mixed ship and shore-based broadcast transponder system"]
+[-3.3831429481506348, 7.5132246017456055, "Automated Identification System Operating Band VHF maritime band"]
+[-3.437119483947754, 7.399600505828857, "Automated Identification System Information Broadcast Ship identification, position, heading, ship length, beam, type, draught and hazardous cargo information"]
+[2.4995369911193848, -1.5527713298797607, "Satellite Function Ship detection with SAR imagery"]
+[0.09600473195314407, 7.234933376312256, "Experiment Facility Mass ~435 kg"]
+[-0.4352693557739258, 7.181312084197998, "Sample Cartridge Assembly Gravity Conditions Earth-gravity (1g) and microgravity (\u00b5g)"]
+[0.14349892735481262, 15.328214645385742, "Spectrometer IFOV Unknown"]
+[-0.3907910883426666, 15.469505310058594, "Multi-angle Imaging SpectroRadiometer Spectral Bands 0.45, 0.56, 0.67 and 0.87 \u00b5m"]
+[-0.3730202615261078, 15.501574516296387, "Multi-angle Imaging SpectroRadiometer Band Wavelength 0.67 and 0.87 \u00b5m"]
+[2.979555368423462, -1.27508544921875, "Satellite Mission Goal Detect and study exoplanets"]
+[2.4074466228485107, -1.8659729957580566, "Satellite Transit Signal Detection Method Measurement of the so-called transit signal"]
+[2.23057222366333, -1.8929792642593384, "Satellite Transit Signal Study Method Further information about the planet's bulk properties can be determined by studying the transit signal"]
+[1.5286900997161865, 10.98713207244873, "Virtual Reality Display Purpose Estimate the distance to an object, length of an object and orientation of their bodies in space"]
+[1.4770698547363281, 10.962479591369629, "Virtual Reality Display Sponsor Canadian Space Agency (CSA)"]
+[0.4966212213039398, 9.562424659729004, "Attitude Sensors Quantity 2"]
+[0.5112447142601013, 9.587746620178223, "Attitude Sensors Quantity 2"]
+[-1.4511572122573853, 9.528401374816895, "Thrusters Quantity 4"]
+[-1.4609259366989136, 9.545994758605957, "Thrusters Thrust 10 N"]
+[-1.5008118152618408, 9.544182777404785, "Thrusters Quantity 2"]
+[-1.4554004669189453, 9.553911209106445, "Thrusters Thrust 2 N"]
+[0.9966602325439453, -4.3236613273620605, "Satellite Dry Mass 322 kg"]
+[0.7183499336242676, -4.1330342292785645, "Satellite Launch Mass 696 kg"]
+[5.301631450653076, -2.20379376411438, "Satellite Design Life 5 years"]
+[1.1474636793136597, -0.9503238797187805, "Satellite Diameter 2.10 m"]
+[2.1087870597839355, -0.5098844766616821, "Satellite Electrical Power 200 W"]
+[1.5497976541519165, -2.2577884197235107, "Satellite Stabilization Spin-stabilized (100 rpm)"]
+[3.221240520477295, -1.796329379081726, "Satellite Manufacturer Aerospatiale of Cannes (France)"]
+[3.0742061138153076, -1.6866458654403687, "Satellite Prime Contractor ESA (later Alcatel Space)"]
+[3.026707410812378, -1.6839028596878052, "Satellite Consortium European subcontractors"]
+[-0.33968719840049744, 8.216649055480957, "Alloy Density 9050 kg/m3"]
+[-0.3559240400791168, 8.22298812866211, "Alloy Yield 1031 MPa"]
+[-0.3293071985244751, 8.204500198364258, "Alloy E 220-230 GPa"]
+[-0.3252332806587219, 8.217148780822754, "Alloy Hardness 32 HRC"]
+[-0.3351340889930725, 8.225789070129395, "Alloy Density 8190 kg/m3"]
+[-0.3287029564380646, 8.220365524291992, "Alloy Yield 1034 MPa"]
+[-0.33269500732421875, 8.21649169921875, "Alloy E 195-200 GPa"]
+[-0.3381769061088562, 8.205253601074219, "Alloy Hardness >33.4 HRC"]
+[-2.4059743881225586, 7.331068992614746, "Onboard Computer Microprocessor 10 MIPS T805"]
+[-2.375786304473877, 7.319037914276123, "Onboard Computer Power Consumption < 6 W"]
+[-2.4106764793395996, 7.2648444175720215, "Onboard Computer Mass 3 kg"]
+[-1.8184568881988525, 14.926578521728516, "Optoelectronic Scanning Radiometer Spectral Range 0.42 - 0.89 \u00b5m"]
+[-1.8563220500946045, 14.919756889343262, "Optoelectronic Scanning Radiometer Spatial Resolution ~16 m"]
+[-1.8581547737121582, 14.914288520812988, "Optoelectronic Scanning Radiometer Swath Width 80 km"]
+[0.7144510746002197, 12.228982925415039, "Sensor Component Type Bi-alkali"]
+[0.7496923208236694, 12.248479843139648, "Sensor Component Material Glass"]
+[0.5038919448852539, 12.330146789550781, "Sensor Component Diameter 7 mm"]
+[0.6452230215072632, 12.298333168029785, "Sensor Component Wavelength 427.8 nm"]
+[0.6012937426567078, 12.279501914978027, "Sensor Component Signal Type Pulse"]
+[0.5880813002586365, 12.2614107131958, "Sensor Component Power 0.5 W"]
+[0.5789555311203003, 12.312296867370605, "Sensor Component Temperature Range -30\u00ba - -20\u00ba C"]
+[2.71291184425354, 22.283199310302734, "Instrument Debris Shield Removed and jettisoned"]
+[2.7198448181152344, 22.338607788085938, "Instrument Cooling Pipes Housed in the service channel"]
+[2.7861764430999756, 22.556848526000977, "Instrument Data Cable Connected"]
+[-5.393606662750244, 2.948934555053711, "Telescope Observation Type Infrared"]
+[-0.35796889662742615, 3.788269519805908, "Planet Size No more than 14 times Jupiter\u2019s size"]
+[-5.496422290802002, 2.704615354537964, "Telescope Detection Capability Water and carbon dioxide"]
+[-5.366270542144775, 2.7812163829803467, "Telescope Number of Transits for Observation 5"]
+[0.4651232063770294, 12.25120735168457, "Sensor Measurement Ambient electron density and temperatures, ambient ion density, average ion temperature and molecular weight"]
+[0.5003765225410461, 12.135823249816895, "Sensor Data Volume 12 MByte/satellite-day"]
+[0.4585948884487152, 12.451342582702637, "Electron Sensor Type Langmuir probe"]
+[0.33041220903396606, 12.293139457702637, "Ion Sensor Type Planar aperture, planar collector sensor"]
+[0.6525123119354248, 12.021839141845703, "Sensor Components Langmuir probe, planar collector, plasma drift meter, scintillation meter"]
+[2.481125831604004, 22.790691375732422, "Instrument Duty Cycle 100%"]
+[2.360445976257324, 22.892969131469727, "Instrument Data Rate 3 kbit/s"]
+[2.3109421730041504, 22.844785690307617, "Instrument Data Volume 18 Mbit/orbit"]
+[2.5878677368164062, 22.832164764404297, "Instrument Data Storage Up to 12 hours"]
+[1.5163745880126953, 21.228086471557617, "Instrument Mass 40 kg"]
+[1.615807056427002, 23.219837188720703, "Instrument Maximum Power Use 70 W"]
+[2.851116895675659, -1.942591667175293, "Satellite Orbit Transfer Status Ongoing"]
+[-1.3856602907180786, 6.912530422210693, "Empirical Model Atmosphere Statistical Comparisons and Scientific Issues"]
+[0.9201616644859314, 10.455425262451172, "Digital Mapping System Data Collection Thousands of high-resolution photographs during a single flight"]
+[0.9490047097206116, 10.46192455291748, "Digital Mapping System Camera Position Mounted on the belly of the plane"]
+[0.9229912757873535, 10.453516006469727, "Digital Mapping System Data Use Helps scientists identify features that are also detected by radar, laser, and gravity instruments"]
+[3.905489206314087, 8.978529930114746, "Space Shuttle Payload Mass 11,200 kg"]
+[3.928521156311035, 8.986905097961426, "Space Shuttle Orbit Average Altitude 320 km"]
+[3.9078009128570557, 8.979026794433594, "Space Shuttle Orbit Inclination 51.6\u00ba"]
+[3.9166629314422607, 8.9552001953125, "Space Shuttle Total Orbits 185"]
+[3.9168028831481934, 8.986289024353027, "Space Shuttle Mission Duration 11 days and 19 hours"]
+[-8.059874534606934, 8.821259498596191, "Power Subsystem Component Quantity 3"]
+[-8.0950345993042, 8.817090034484863, "Power Subsystem Component Manufacturer STI (SpaceTech GmbH Immenstaad), Germany"]
+[-8.03858757019043, 8.853119850158691, "Power Subsystem Component Components Photovoltaic assembly, solar panel deployment mechanisms, PDM (Pyro Drive Module) electronics"]
+[-2.882357120513916, 15.180716514587402, "Microwave Radiometer Frequencies 6.6 GHz, 10.7 GHz, 18.0 GHz, 21.0 GHz, 37.0 GHz"]
+[-2.8316571712493896, 15.257902145385742, "Microwave Radiometer Radiometer Type Dicke-type"]
+[6.366003513336182, 7.379148483276367, "Satellite Component Material Graphite epoxy"]
+[6.370603084564209, 7.368863105773926, "Satellite Component Type Momentum compensation devices"]
+[6.3553338050842285, 7.380625247955322, "Satellite Component Contents Input and reference switching networks, the mixer-IF preamplifiers, and the Gunn local oscillators"]
+[0.6173356175422668, 11.866127967834473, "Sensor Function Provide attitude information"]
+[0.5670580863952637, 11.946891784667969, "Sensor Function Close-up maneuvering"]
+[2.6168172359466553, 21.86703109741211, "Instrument Function Take images of the Sun's corona"]
+[-1.296472430229187, 6.871461868286133, "Technology Function Demonstrate a high-precision formation flight in space"]
+[0.9506431818008423, -4.395561218261719, "Satellite Mass 23.5 kg"]
+[0.9850073456764221, -4.372834205627441, "Satellite Mass ~ 190 kg"]
+[1.021864891052246, -4.419609546661377, "Satellite Mass ~ 96 kg"]
+[0.9681506156921387, -4.360148906707764, "Satellite Mass ~ 96 kg"]
+[0.893785834312439, -4.449267387390137, "Satellite Mass 12 kg"]
+[0.9422500133514404, -4.425839900970459, "Satellite Mass 12 kg"]
+[-3.262594223022461, 1.755491852760315, "Satellite Mission Mission Date July 31-Aug. 4, 2006"]
+[-3.244551420211792, 1.6841412782669067, "Satellite Mission Workshop Date May 15-17, 2006"]
+[1.3410582542419434, 7.077114105224609, "Communication Equipment Signal Type 16 QAM"]
+[-1.3977338075637817, 4.31050968170166, "Ground System Antenna Diameter 4.6 m"]
+[-1.4478073120117188, 4.334993362426758, "Ground System Functions Mission control, mission planning, ground station, mission data processing and GIS"]
+[-2.8572747707366943, 15.215958595275879, "Microwave Radiometer Frequency Eight"]
+[-2.8289356231689453, 15.2227201461792, "Microwave Radiometer Polarization Dual"]
+[-2.825897693634033, 15.247292518615723, "Microwave Radiometer Scanning Rate 40 rpm"]
+[-2.8173611164093018, 15.245918273925781, "Microwave Radiometer Incidence Angle Approximately 55\u00ba"]
+[-2.8920083045959473, 15.359369277954102, "Microwave Radiometer Antenna Diameter 2.0 m"]
+[-2.831378936767578, 15.243428230285645, "Microwave Radiometer Antenna Type Offset Parabolic"]
+[-2.8387773036956787, 15.236005783081055, "Microwave Radiometer Antenna Mass Nearly 200 kg"]
+[1.6509987115859985, 22.195106506347656, "Instrument Size 1.47 m long x 0.93 m wide x 0.62 m high"]
+[1.5149754285812378, 21.22537612915039, "Instrument Mass 44 kg"]
+[2.0559585094451904, 22.553646087646484, "Instrument Mirror Shape Defect Few tens of a \u00b5m"]
+[-0.9258061051368713, -10.040057182312012, "Satellite Constellation Number of Satellites Up to 100"]
+[-0.9629095196723938, -10.015461921691895, "Satellite Constellation Funds Raised 2.4 million euros ($2.8 million)"]
+[-1.057131290435791, -10.1029691696167, "Satellite Constellation Funds Needed $35 million to deploy an initial 16 satellites by the end of 2022"]
+[-7.561444282531738, 5.895885467529297, "Camera Application Earth Observation"]
+[-7.559051990509033, 5.88913106918335, "Camera Development Date Oct. 4-8, 2010"]
+[-7.529414176940918, 5.933061599731445, "Camera Presentation Date June 2-8, 2013"]
+[-3.003744125366211, 4.46825647354126, "Spacecraft Cargo Capacity 3,356 kg"]
+[-2.1203110218048096, 4.323410511016846, "Space Station Crew Size Three-person"]
+[-2.117713451385498, 4.310911178588867, "Space Station Arrival Date Monday (Nov. 19)"]
+[-13.489524841308594, -2.027513027191162, "X-ray Observatory Measurement Date Unknown"]
+[-13.473905563354492, -1.9995484352111816, "X-ray Observatory Measurement Date Unknown"]
+[-13.51750659942627, -2.0464813709259033, "X-ray Observatory Launch Date June 2012"]
+[-13.532503128051758, -2.076831340789795, "X-ray Observatory Mission Duration More than eight months"]
+[-13.482734680175781, -2.015106439590454, "X-ray Observatory Science Goals Mapping of the central regions of our Milky Way galaxy, studying the remnants of exploded stars in our galaxy, and surveys of several well-studied extragalactic fields"]
+[-4.134230613708496, 15.709288597106934, "Imaging Radar Studied Phenomena Surface waves, internal waves, currents, upwelling, shoals, sea ice, wind, and rainfall"]
+[2.914661169052124, 21.918811798095703, "Instrument Purpose Produced the first global view of the variability of the surface geostrophic currents"]
+[5.188272953033447, -3.8725500106811523, "Satellite Planning Start Year 1972"]
+[2.7760167121887207, -1.1457051038742065, "Satellite Objectives Collect data on sea-surface winds, sea-surface temperatures, wave heights, ocean topography, internal waves, atmospheric water, and sea ice properties"]
+[1.5223673582077026, 5.429131507873535, "Satellite Bus Variant DMSP Block-5D military satellite bus"]
+[2.4089603424072266, -1.9141488075256348, "Satellite Design Resembled in appearance conventional Earth-oriented satellites of this period"]
+[2.5260279178619385, -1.7852064371109009, "Satellite Sections Three sections: a square precision-mounting platform, a five-sided equipment-support module, a circular reaction and control-equipment support structure"]
+[-3.1498794555664062, 14.744210243225098, "Interferometric Microwave Sounder Instrument Overview and Recent Progress Unknown"]
+[-6.649906635284424, 10.062274932861328, "Antenna Design, Position Error Analysis and Adjustment Unknown"]
+[1.4365720748901367, 2.326580762863159, "Geostationary Lightning Imager Development and Evaluation of detection algorithm Unknown"]
+[0.47051188349723816, 12.248088836669922, "Sensor Detection Area Size 8 cm x 8 cm"]
+[-7.47225284576416, 5.992167949676514, "Camera Image Format JPEG"]
+[-7.584667205810547, 5.926992416381836, "Camera Image Resolution 640 x 480 pixels"]
+[-7.553138256072998, 5.896099090576172, "Camera Pixel Size 1.6 km"]
+[4.345248699188232, -3.001310110092163, "Satellite Release Time 29 minutes after liftoff"]
+[4.305877685546875, -2.9209609031677246, "Satellite Separation Time 33 minutes after liftoff"]
+[5.2798686027526855, -3.9738168716430664, "Satellite Launch Date 2018"]
+[1.8215426206588745, -2.2774388790130615, "Satellite Orbit Type Geostationary orbit"]
+[0.4712075889110565, -1.4846875667572021, "Satellite Orbit Altitude 35,876 km"]
+[0.8634397387504578, -2.171172618865967, "Satellite Orbit Location 31\u00baE"]
+[2.6470391750335693, 14.370892524719238, "Optical Instrument Temperature Stability \u00b12\u00b0C"]
+[-0.3921426832675934, 8.20566177368164, "Mechanical Structure Material Aluminum alloy"]
+[2.6451256275177, 14.369817733764648, "Optical Instrument Support Components SPS (Shadow Position Sensor), FDA (Front Door Assembly), entrance objective, IO (Internal Occulter) with field stop"]
+[-0.6457439064979553, 8.34354019165039, "Structured Parallelepiped Components Relay lens(es), FPA and its radiator, filter wheel and the Lyot stop assemblies, shutter mechanisms, venting systems"]
+[-1.5679298639297485, 9.664280891418457, "Propulsion Unit Operation Produces iodine vapor via sublimation"]
+[-1.5875836610794067, 9.702274322509766, "Propulsion Unit Control Scheme Works best for long-duration, steady-state maneuvers"]
+[-1.6403447389602661, 9.74324893951416, "Propulsion Unit Response Time Can be slow"]
+[1.487310528755188, -2.402022123336792, "Satellite Deployment Orbit Sun-synchronous circular orbit of 720 km with an inclination of 24\u00ba"]
+[0.9973540306091309, -4.364475727081299, "Satellite Mass 280 kg"]
+[3.739470958709717, 17.713550567626953, "Payload Stack Total Mass 3700 kg"]
+[-0.9629745483398438, 7.8385515213012695, "Device Volume 125 mm x 180 mm x 165 mm"]
+[-1.0193573236465454, 7.728318214416504, "Device Mass ~ 2 kg"]
+[-1.002037763595581, 7.732247829437256, "Device Power Consumption < 4.5 W"]
+[1.533918857574463, -1.0928821563720703, "Satellite Resolution 1-meter"]
+[1.6773713827133179, -1.729628562927246, "Satellite Geolocation Accuracy Improved"]
+[2.840435743331909, -2.0683841705322266, "Satellite On-orbit Lifetime Unknown"]
+[2.8740017414093018, -1.1594369411468506, "Imagery Service Tasking Available"]
+[-0.1396682858467102, 11.165210723876953, "Event Monitoring Service Revisit Times Very short"]
+[7.270660400390625, 12.442124366760254, "Satellite Instrument Science Goals Observe and model the processes that relate salinity variations to climatic changes in the global cycling of water"]
+[7.291018486022949, 12.427301406860352, "Satellite Instrument Measurement Sea Surface Salinity"]
+[7.288081169128418, 12.421219825744629, "Satellite Instrument Measurement Sea Surface Temperature"]
+[7.27681303024292, 12.506362915039062, "Satellite Instrument Determination Sea Surface Density"]
+[7.318241119384766, 12.41323184967041, "Satellite Instrument Regulation 3-dimensional ocean circulation"]
+[-1.1477686166763306, 15.110932350158691, "Imaging multi-spectral radiometers (vis/IR) Instrument type Imaging multi-spectral radiometers (vis/IR)"]
+[-2.5333335399627686, 12.220243453979492, "High resolution optical imagers Instrument type High resolution optical imagers"]
+[2.221855640411377, -1.5286017656326294, "Satellite Exoplanet Survey Detects planets via the transit method"]
+[-2.242682456970215, 2.8916685581207275, "Infrared Observatory Retired Recently retired"]
+[-4.566855430603027, -3.0890328884124756, "Exoplanet Type Presence Hints at the presence of even younger hot Jupiters"]
+[1.7447614669799805, -1.6123183965682983, "Satellite Coverage Lunar nearside, function of latitude, several times of day"]
+[1.7853015661239624, -1.1288540363311768, "Satellite Measurement Diurnal variation in OH absorption"]
+[1.7881146669387817, -1.1047559976577759, "Satellite Measurement C-, H-, O-, and S-bearing volatiles"]
+[1.7337826490402222, -1.0741645097732544, "Satellite Measurement 3 \u00b5m band absorption by several forms of water"]
+[2.834306478500366, 22.098848342895508, "Instrument Observation Method Solar occultation"]
+[2.2488369941711426, 22.238595962524414, "Instrument Measurement Components of solar light absorbed"]
+[2.217228651046753, 22.264095306396484, "Instrument Measurement Resolves solar light into spectra"]
+[2.802476406097412, 22.09796142578125, "Instrument Observation Provides information on the altitude distribution of the light-absorbing substances"]
+[2.5753557682037354, 22.094623565673828, "Instrument Image Navigation Ground processing algorithms to decompress, calibrate and navigate the image samples"]
+[1.9753419160842896, 22.362276077270508, "Instrument Pixel Size 14 \u00b5rad"]
+[2.035334587097168, 22.533763885498047, "Instrument Quaternion Uncertainty ~ 100 \u00b5rad"]
+[2.1110830307006836, 22.477325439453125, "Instrument Attitude Rate Measurements < 20 \u00b5rad drift over 15 minutes"]
+[1.9141535758972168, 22.228988647460938, "Instrument Spacecraft Position 35 m in-track, 35 m cross-track and 70 m radial over 15 minutes"]
+[1.995151162147522, 22.389080047607422, "Instrument Spacecraft Velocity < 6 cm/sec uncertainty per axis"]
+[-0.718413233757019, 3.2603487968444824, "Star Tracker Quantity 1"]
+[0.5225054621696472, 9.365553855895996, "Attitude Control System Quantity 3"]
+[-1.4698091745376587, 13.365646362304688, "Solar Panels Quantity 5"]
+[-3.0978646278381348, 7.645425796508789, "Processing Unit Type ARM M0+"]
+[2.5066046714782715, -2.335195302963257, "Satellite Data Storage 1TB"]
+[2.4294068813323975, -2.172806978225708, "Satellite Daily Imaging Capacity 1.2 TB"]
+[1.1956555843353271, -1.340356707572937, "Satellite Ground Coverage Area 150 million square Kilometres"]
+[2.662295341491699, -2.6658008098602295, "Satellite Ka-Band Link 170 Mbps"]
+[-3.235527753829956, 1.702492594718933, "Satellite Mission Launch Date May 2018"]
+[-3.1236534118652344, 1.6791644096374512, "Satellite Mission Purpose Measure the change in the mass of water across the planet"]
+[-3.1447808742523193, 1.7122974395751953, "Satellite Mission Data Usage Track drought across the United States"]
+[-3.145296573638916, 1.6902432441711426, "Satellite Mission Data Usage Measure mass changes in the thick ice sheets of Greenland and Antarctica"]
+[-0.7542986273765564, 3.1815567016601562, "Star System Orbital Period 51.4 days"]
+[-0.735580325126648, 3.1913740634918213, "Star System Average Distance about 61 million km"]
+[-0.5765336751937866, 3.2815675735473633, "Star Size 4.3 times bigger than the Sun"]
+[-0.5983933806419373, 3.2473201751708984, "Star Surface Temperature around 17,500 \u00baF (9,700\u00baC)"]
+[-0.6121037006378174, 3.218595504760742, "Star Brightness five times fainter than the primary star"]
+[-0.5913619995117188, 3.2330219745635986, "Star Size most likely half the primary\u2019s size"]
+[-0.6209717988967896, 3.2114717960357666, "Star Surface Temperature 40% hotter than the Sun"]
+[4.684657573699951, -4.154587268829346, "TDE Discovery Date Unknown"]
+[4.901939392089844, -4.309484958648682, "TDE Publication Date 26 September 2019"]
+[4.620809078216553, -4.054553508758545, "TDE Journal The Astrophysical Journal"]
+[-5.400230884552002, 2.75673508644104, "Telescope Capability Focusing high-energy X-rays into sharp pictures"]
+[-5.463468074798584, 2.774651288986206, "Telescope Function Revealing what lies around the most buried supermassive black holes"]
+[-5.3709025382995605, 2.6463851928710938, "Telescope Function Seeing through the gas and dust around black holes"]
+[1.5510772466659546, -1.5915474891662598, "Satellite Technique Accuracy Sub-mm"]
+[1.767721176147461, -1.6009528636932373, "Satellite Technique Purpose Polar motion determination"]
+[1.5445679426193237, -1.7022961378097534, "Satellite Technique Purpose Inertial direction of the Earth rotation vector determination"]
+[3.5884954929351807, 13.823602676391602, "International Laser Ranging Service Target Signature Error 1 mm"]
+[-1.0360968112945557, 7.705429553985596, "Device Swath 105 km"]
+[-1.956425666809082, 14.922467231750488, "Radiometer Spectral Bands 2"]
+[-1.8748449087142944, 14.855746269226074, "Radiometer Spectral Range 0.58 - 1.0 \u00b5m"]
+[-1.9385862350463867, 14.899847030639648, "Radiometer Resolution 240 m"]
+[-1.9349335432052612, 14.88137435913086, "Radiometer Swath 1380 km"]
+[-2.1781864166259766, 2.8832404613494873, "Space Observatory Expected Launch Date 2034"]
+[-2.176992893218994, 2.8888046741485596, "Space Observatory Sensitivity Lower frequency than LIGO"]
+[-2.18408465385437, 2.880540132522583, "Space Observatory Detector Type Gravitational Waves"]
+[-0.8624555468559265, 12.480098724365234, "Radiation Shield Thickness 2 cm"]
+[-0.8675286173820496, 12.551312446594238, "Radiation Shield Extension Above Detector 20 cm"]
+[-0.8747081756591797, 12.50484561920166, "Radiation Shield Opening Angle 16\u00ba"]
+[2.6303601264953613, 13.444808959960938, "Optical Component Opening Diameter 4\u00ba"]
+[-0.8183341026306152, 11.602795600891113, "Detector Performance Assumption Use of depth-of-interaction measurement to reject interactions in the back of the detector"]
+[7.363340854644775, 12.489304542541504, "Satellite Instrument Average Concentration of Antarctic Sea Ice November 2016"]
+[2.528911590576172, -2.0888116359710693, "Satellite Anomaly Resolution Closed"]
+[2.535961866378784, -1.5283061265945435, "Satellite Power Failure Within the command and control system"]
+[2.6125435829162598, -1.9905890226364136, "Satellite Command Processor Unreachable"]
+[1.3477472066879272, -1.9967973232269287, "Satellite Pointing Accuracy Degrades"]
+[4.917916774749756, -4.369035243988037, "Satellite Image Reception Date December 27, 2019"]
+[2.222142219543457, -2.0438897609710693, "Satellite Ground Station Location Cuiaba, MT"]
+[2.5606980323791504, -1.4843335151672363, "Satellite Raw Data Processing Location S\u00e3o Jos\u00e9 dos Campos, SP"]
+[4.446364879608154, -2.714945077896118, "Satellite Commissioning Phase Duration About three months"]
+[-2.1326310634613037, 11.48945426940918, "Cloud-Aerosol Transport System URL http://www.nasa.gov/mission_pages station/research/experiments/1037.html"]
+[-1.0085643529891968, 8.150466918945312, "Robotic Arm Task Execution Carry out tasks using a suite of three primary tools"]
+[-1.595248818397522, 7.0900421142578125, "Tool Operation Operates smaller specialized tools to prepare for the fluid transfer"]
+[-1.568878412246704, 7.007789134979248, "Tool Operation Uses a hose to connect the tank filled with liquid methane to the empty tank"]
+[-7.559327125549316, 5.891120433807373, "Robotic Camera Monitoring Make sure tools are properly positioned"]
+[1.3862017393112183, 10.555427551269531, "Imaging System Function Taking snapshots of targets of interest"]
+[1.3093996047973633, 10.51279067993164, "Imaging System Function Perform star-tracking experiments"]
+[2.6357715129852295, 22.173131942749023, "Instrument Objective Detect the greenhouse gas constituents in the near-infrared spectrum using earthshine spectra"]
+[0.19453127682209015, 7.189907073974609, "Science Experiment Function Performs refractive radio occultation measurements of the Earth's atmosphere and monitors the auroral activity"]
+[0.027546992525458336, 7.457787036895752, "Material Science Demonstration Experiment Function Measures the surface degradation of a material sample exposed to the space environment"]
+[-5.225030422210693, 7.880982398986816, "Communication System Function Allows satellites to dynamically transfer data"]
+[-2.7367758750915527, 7.958365440368652, "Fault-Tolerant Processor Processor Configuration Reconfigurable"]
+[-2.583430290222168, 7.671126365661621, "FPGA Interface 16-bit PC/104 bus"]
+[-2.4327244758605957, 7.449255466461182, "FPGA Programming Interface JTAG (Joint Test Action Group)"]
+[-2.6118581295013428, 7.888607501983643, "Fault-Tolerant Processor Configuration TMR (Triple-Modular Redundant) computer"]
+[-2.6938207149505615, 7.921767234802246, "Fault-Tolerant Processor Operation Focus Recording SEEs near the SAA (South Atlantic Anomaly)"]
+[-3.559868097305298, 7.663503170013428, "Compression Engine Data Type JPEG imagery of the VISIM data"]
+[2.726992130279541, -1.8403775691986084, "Satellite Calibration and Validation Phase Ongoing"]
+[1.8685379028320312, -1.6830881834030151, "Satellite Radiometric Calibration CEOS network Tuz G\u00f6l\u00fc (Salt Lake) in Turkey"]
+[1.7079981565475464, -1.5259984731674194, "Satellite Geometric Calibration Yearly basis"]
+[3.0028562545776367, -1.8575077056884766, "Satellite Operational Capacity Above mission specified parameters"]
+[-0.9115654826164246, -10.048377990722656, "Satellite Constellation Daily Revisit Average daily revisit"]
+[-0.9445461630821228, -10.013104438781738, "Satellite Constellation Daily Access Daily access to 95% of the world"]
+[-0.9700811505317688, -9.990262031555176, "Satellite Constellation Mission Development Start 2005"]
+[-0.981865644454956, -9.96966552734375, "Satellite Constellation Satellite Launches Planned 2018"]
+[3.1805882453918457, -2.406205415725708, "Satellite Launch Date Unknown"]
+[5.063127517700195, -4.351573944091797, "Satellite Testing Date 29 September 2020"]
+[5.1125569343566895, -4.345849990844727, "Satellite Instrument Installation Date 1 July 2019"]
+[5.242988586425781, -4.459114074707031, "Satellite Launch Date July 2014"]
+[2.7316734790802, -1.4498956203460693, "Satellite Mission Type Meteorological"]
+[2.6787757873535156, -1.549775242805481, "Satellite Operation Global observations of the Earth\u2019s surface and atmosphere"]
+[1.4251282215118408, 2.7287161350250244, "Meteorological Satellite Launch Date 6 June 2021"]
+[1.4832258224487305, 2.7243149280548096, "Meteorological Satellite URL https://space.oscar.wmo.int/satellites/view/fy_4b"]
+[2.5713229179382324, -3.935468912124634, "Satellite URL https://fy4.nsmc.org.cn/nsmc/en/theme/FY4A.html"]
+[-0.99522864818573, 6.474492073059082, "Document Date 2 June 2018"]
+[-6.99532413482666, 11.215394020080566, "Phased Array Antenna Size 1510 mm x 990 mm x 1530 mm"]
+[-6.998008728027344, 11.215453147888184, "Phased Array Antenna Mass 183 kg"]
+[-6.994438171386719, 11.205288887023926, "Phased Array Antenna Aperture Size 649 mm x 539 mm"]
+[-6.996211528778076, 11.207563400268555, "Phased Array Antenna Frequency (Ka-band) 18 GHz (17.7-18.8)"]
+[-6.992868900299072, 11.213241577148438, "Phased Array Antenna Bandwidth 1.1 GHz"]
+[-6.995338439941406, 11.216997146606445, "Phased Array Antenna No of Radiation Elements 128"]
+[-6.996329307556152, 11.211530685424805, "Phased Array Antenna Polarization Linear (V, H)"]
+[-6.99611759185791, 11.211141586303711, "Phased Array Antenna FOV (Field of View) 8\u00ba in azimuth 7\u00ba in elevation"]
+[-6.998025417327881, 11.215925216674805, "Phased Array Antenna No of Beams 2"]
+[-6.994263172149658, 11.21401309967041, "Phased Array Antenna EIRP \u2265 54.6 dBW/ 1 beam \u2265 52.1 dBW/ 2 beams"]
+[-6.996978282928467, 11.212567329406738, "Phased Array Antenna Directive Gain 37.8 dBi at \u03b8=0"]
+[-6.995337963104248, 11.217788696289062, "Phased Array Antenna Phase Shift Bit Number 5"]
+[-6.99406623840332, 11.21979808807373, "Phased Array Antenna Operating Mode SS-TDMA"]
+[-6.986588954925537, 11.225831985473633, "Phased Array Antenna Beam Hopping Time \u2264 10 \u00b5s at SS-TDMA"]
+[-6.99365758895874, 11.211870193481445, "Phased Array Antenna Beam Steering Range 8\u00ba (half cone angle)"]
+[-6.9956536293029785, 11.212944030761719, "Phased Array Antenna Power Consumption \u2264 750 W"]
+[-6.998110294342041, 11.223917961120605, "Phased Array Antenna Operating Temperature 0~70\u00baC -10~70\u00baC"]
+[2.3238673210144043, 22.16958999633789, "Instrument Calibration Process Correcting systematic errors in the measurements"]
+[2.2671444416046143, 22.18196678161621, "Instrument Calibration Procedure Calibrated separately"]
+[-0.9326575398445129, 11.889287948608398, "Surface Charge Detector Mass 0.6 kg"]
+[-0.9454036355018616, 11.88781452178955, "Surface Charge Detector Power 2 W"]
+[-0.9420161247253418, 11.885359764099121, "Surface Charge Detector Dimensions about 100 mm x 150 mm x 30 mm"]
+[-0.9230172038078308, 11.922560691833496, "Surface Charge Detector Objective Non-contact measurement of surface potentials"]
+[-2.559203624725342, 11.889289855957031, "Optical Imager Development Date July 5-12, 2009"]
+[-1.0796988010406494, 7.586893558502197, "Device Progress Date Aug. 26-27, 2007"]
+[-1.72755765914917, 16.98495101928711, "Radar Altimeter Mass 93.8 kg"]
+[-1.7327656745910645, 16.98919105529785, "Radar Altimeter Power Consumption 177 W"]
+[-1.7146176099777222, 16.984909057617188, "Radar Altimeter Height Bias 0.0 \u00b1 0.07 m"]
+[-1.709571123123169, 16.97032928466797, "Radar Altimeter Echo Samples Spacing 3.125 ns"]
+[-1.783884048461914, 16.957189559936523, "Radar Altimeter Waveform Sampling Bandwidth 312.5 kHz"]
+[-5.172207832336426, 7.782983303070068, "Communication System Data Rate Up to 24 Mbit/s"]
+[-5.130926609039307, 7.805032730102539, "Communication System Data Rate Up to 6.5 Mbit/s"]
+[-1.2128968238830566, 4.522871971130371, "Earth Station Purpose Establish telecommunications in disaster areas"]
+[-1.2251534461975098, 4.423630714416504, "Earth Station Mobility Can be used while being moved in off-road and all-weather conditions"]
+[2.7469310760498047, 23.418821334838867, "Instrument Development and Operations 1996"]
+[-1.7063186168670654, 6.590546607971191, "Program Participating Countries and Organizations Canada (CRC), France (CNES), Russia (ROSHYDROMET), and the USA (NOAA)"]
+[-1.7373031377792358, 6.620458126068115, "Program Ground Segment Providers 24"]
+[-1.7369142770767212, 6.608100891113281, "Program Local User Terminals (LUTs) Over 40"]
+[-1.7027111053466797, 6.592859268188477, "Program Participants Associated with the Management 9"]
+[-1.7408943176269531, 6.601438522338867, "Program New Home of the Program Office Montreal, Canada"]
+[-1.761324167251587, 6.615017414093018, "Program Formal Understanding with ISRO Concerning the long-term provision of INSAT GEOSAR services"]
+[-1.7473236322402954, 6.583901405334473, "Program Phased Out Devices 121.5 and 243 MHz emergency beacons"]
+[-2.2556087970733643, 2.8373870849609375, "Space-based gravitational-wave observatory Launch Date 2034"]
+[-0.8288854956626892, 3.1509106159210205, "Stellar Remnants Primary Temperature Nearly 50,000 K"]
+[-0.791334867477417, 3.1219046115875244, "Stellar Remnants Primary Mass About three times as massive as the secondary"]
+[-1.1621073484420776, 3.0620217323303223, "Celestial Object Orbital Period 6.91 minutes"]
+[-7.6019673347473145, 5.8656392097473145, "Camera Data Transmission Rate 4 Mbit/s"]
+[-7.589240550994873, 5.8675947189331055, "Camera Transmission Success Most cases"]
+[-7.593412399291992, 5.863230228424072, "Camera Transmission Failure Cases with obstacles such as buildings, pedestrian overpasses and utility poles"]
+[0.23424629867076874, 13.77829360961914, "Calibration Subsystem Calibration Sources Gray lamps and blackbodies"]
+[0.26152873039245605, 13.734423637390137, "Calibration Subsystem Thermal Control Continuous"]
+[0.24687816202640533, 13.785165786743164, "Calibration Subsystem Usage Turned on during the calibration session (typically once per day)"]
+[0.2802053391933441, 13.778733253479004, "Calibration Subsystem Usage Once per month"]
+[0.2549965977668762, 13.769705772399902, "Calibration Subsystem Status Damaged on the ScaRaB/Meteor-3-7 mission"]
+[-1.5002106428146362, 16.899654388427734, "Altimeter Pulse Time Interval Measurement Precision ~ 5 ns"]
+[-1.4859567880630493, 16.88880729675293, "Altimeter Footprint Diameter 100 m"]
+[-1.509915828704834, 16.90910530090332, "Altimeter TVR Total Vertical Roughness"]
+[-1.4864392280578613, 16.888755798339844, "Altimeter Tree Height Measurement Possible"]
+[0.5696460604667664, -1.520045518875122, "Satellite Orbit Altitude 1336 km"]
+[4.147552967071533, -2.815284252166748, "Satellite Orbit Period 112.4 min"]
+[0.6985226273536682, -2.2750275135040283, "Satellite Orbit Inclination 66.039\u00ba"]
+[4.109219074249268, -2.460706949234009, "Satellite Repeat Period About 10-day"]
+[-1.126772165298462, 4.475954532623291, "Ground Station Measurement Technique Satellite Laser Ranging"]
+[-1.1193575859069824, 4.483931541442871, "Ground Station Measurement Technique DORIS"]
+[-4.3666253089904785, 0.19177928566932678, "GPS Receiver Tracking Method Track the satellite"]
+[-5.109927177429199, 8.039522171020508, "Communication System Tracking Method Track the spacecraft"]
+[6.17753791809082, 7.567223072052002, "Satellite Component Revolution Count 1216"]
+[6.212562561035156, 7.581162452697754, "Satellite Component Slewing Angle 9\u00ba"]
+[6.296590805053711, 7.442273139953613, "Satellite Component Step Size 1120 \u00b5rad"]
+[6.358094215393066, 7.385870933532715, "Satellite Component Time 200 ms"]
+[6.359238147735596, 7.375847339630127, "Satellite Component Interruption Frequency Every 30 minutes"]
+[0.556911289691925, -2.012634038925171, "Satellite Parameter Maximum Pointing Error 0.064\u00b0"]
+[-0.14932715892791748, 13.51308536529541, "Signal Measurement Average Level -46.4 dBm"]
+[-0.09119504690170288, 13.446578025817871, "Signal Measurement C/N0 47.4 dB"]
+[2.384329080581665, -2.143169403076172, "Satellite Test Data Rate 18 Mbit/s"]
+[2.487579822540283, -2.153460741043091, "Satellite Test Expected Data Rate 24 Mbit/s"]
+[3.61112642288208, 13.269760131835938, "Laser Frequency Locking On-board reference cavity"]
+[3.610672950744629, 13.292773246765137, "Laser Frequency Offset Chosen such that after picking up once more the Doppler shift (with the same sign) on the way back to S/C 1, the beat note between the light arriving back at S/C 1 and the local, stabilized, laser at S/C 1 is in the sensitive frequency range of the phasemeter (approximately 2 - 15 MHz)"]
+[2.225072145462036, 23.100900650024414, "Instrument Sensitive Frequency Range Approximately 2 - 15 MHz"]
+[0.7522737979888916, 11.923639297485352, "Sensors Type Dual axis"]
+[0.8155535459518433, 11.93283462524414, "Sensor Type Triaxial"]
+[-0.0797438770532608, 9.872584342956543, "Inertial Measurement Units Quantity 3"]
+[0.5916010141372681, 11.978941917419434, "Sensor Purpose Fine-attitude determination"]
+[0.4882315695285797, 9.387864112854004, "Attitude Actuation Quantity 3"]
+[0.4869471788406372, 9.40352725982666, "Attitude Actuation Maximum Speed 3,400 RPM"]
+[0.4981934130191803, 9.402490615844727, "Attitude Actuation Nominal Torque Setting 1mNm"]
+[0.42914149165153503, 9.467425346374512, "Attitude Actuation Maximum Power 0.7 W"]
+[1.027701497077942, -2.055384397506714, "Satellite Pointing Accuracy 1.0\u00ba"]
+[0.9904255270957947, -2.122502326965332, "Satellite Attitude Determination Accuracy 0.1\u00b0"]
+[-3.099622964859009, 9.665983200073242, "Battery Capacity 30 Ah"]
+[-2.5915112495422363, 9.372895240783691, "Power Generation System Efficiency 28.5% at BOL"]
+[-2.589536428451538, 9.351374626159668, "Power Generation System Technology Triple junction GaAs cell"]
+[-2.582472562789917, 9.365673065185547, "Power Generation System Type Fixed, single wing, three panel"]
+[-0.8529648780822754, 0.16725395619869232, "Satellite System Development Start Date April 9, 2014"]
+[-0.8634750843048096, 0.17580150067806244, "Satellite System Project Status Presentation Date May 5-7, 2014"]
+[-0.8485583662986755, 0.16713961958885193, "Satellite System Contract Award Date May 20, 2014"]
+[1.3977630138397217, -2.560030937194824, "Satellite Orbit Type Super-synchronous"]
+[0.8450287580490112, -1.7523484230041504, "Satellite Orbit Perigee 300 km"]
+[0.7162140011787415, -1.6219441890716553, "Satellite Orbit Apogee 60,000 km"]
+[0.7301985025405884, -2.334184169769287, "Satellite Orbit Inclination 27\u00ba"]
+[1.92146635055542, -1.6399961709976196, "Satellite Detector Energy Range keV to MeV"]
+[1.4328641891479492, 2.7733306884765625, "Weather Satellite Launch Date Dec. 10, 2016"]
+[1.424401879310608, 2.7622640132904053, "Weather Satellite Launch Date 2 June 2021"]
+[-6.653993129730225, 9.857551574707031, "Antenna Configuration Typical"]
+[1.690802812576294, 6.951018333435059, "Communication Device Signal Processing Capability Phase shift keyed (PSK) and more general linear phase modulated (PM) signals, either spread or non-spread"]
+[1.6907578706741333, 6.9474334716796875, "Communication Device Coherent Tracking Capability Symbols, carrier and, when necessary, PN code"]
+[1.7590488195419312, 6.8792548179626465, "Communication Device Maximum Data Rate 1 Mbit/s"]
+[1.78409743309021, 6.8777618408203125, "Communication Device Data Rates Up to 5 Mbit/s"]
+[-2.97189998626709, 4.195362091064453, "Spacecraft Body Pointing Function \u00b130\u00ba in the roll axis"]
+[-3.169667959213257, 4.272532939910889, "Spacecraft Attitude Manoeuvring Time Up to 2 minutes from the Earth pointing attitude to right- or left-looking"]
+[-3.236964702606201, 4.212007522583008, "Spacecraft Attitude Manoeuvring Time Up to 3 minutes from right- to left-looking (or from left- to right-looking)"]
+[0.4913431406021118, 9.413959503173828, "Attitude Control Device Output Torque More than 0.9 Nm"]
+[0.4973198175430298, 9.409683227539062, "Attitude Control Device Maximum Momentum 40 Nms"]
+[0.5022958517074585, 9.385527610778809, "Attitude Control Device Maximum Attitude Rate 0.7\u00ba/s in roll axis"]
+[5.3152031898498535, -4.502758979797363, "Satellite Reprogramming Date May 2013"]
+[4.915960311889648, -4.553342342376709, "Satellite Image Acquisition Date May 6, 2013"]
+[2.3476674556732178, -1.3772900104522705, "Satellite Image Content Vancouver harbor, Canada"]
+[-0.1181514784693718, 9.194182395935059, "Vibration Control Device Purpose Provide an ultra-quiet environment for sensitive optical sensors, laser transmitters, and other detection and measurement devices"]
+[-0.15022137761116028, 9.15942668914795, "Vibration Control Device Configuration Hexapod (Stuart platform)"]
+[-0.005574987269937992, 9.242725372314453, "Vibration Control Device Degrees of Freedom Six"]
+[-0.08021863549947739, 9.192605972290039, "Vibration Control Device Purpose Steering about any or all of the three rotational axes"]
+[3.012749195098877, 22.07508659362793, "Instrument Mission Goal Study the boundary layer between Earth and space"]
+[2.825881004333496, 22.376014709472656, "Instrument Lead Richard W. Eastes of UCF (University of Central Florida)"]
+[3.7013232707977295, 22.975318908691406, "Instrument Launch Date 2017"]
+[-0.25841864943504333, 15.695988655090332, "Spectrometer Spectral Range 450-1000 nm"]
+[-0.11226318776607513, 15.492287635803223, "Spectrometer Spectral Sampling Interval 1.2 nm \u2013 16 nm"]
+[-0.15035752952098846, 15.537259101867676, "Spectrometer Dispersion Element Direct vision prism"]
+[-0.14538130164146423, 15.579808235168457, "Spectrometer F Number 3.0"]
+[-0.1255810260772705, 15.512314796447754, "Spectrometer Magnification 1:1"]
+[-0.13949918746948242, 15.55246639251709, "Spectrometer Proto-Flight Model Components Entrance slit assembly, front-side optical system, dispersing assembly and back-side optical system"]
+[-7.45316743850708, 6.002751350402832, "Camera Design and Performance Not provided"]
+[-7.581726551055908, 5.880957126617432, "Camera CCDs Not provided"]
+[-2.6970443725585938, 9.431402206420898, "Power Generation Number of Panels 6"]
+[-1.2388266324996948, 6.998056411743164, "Drive Assembly Roll Bias Compensation \u00b1 36\u00b0"]
+[-2.960097312927246, 9.54505443572998, "Battery System Battery Type NiH2"]
+[-2.935157299041748, 9.528579711914062, "Battery System Capacity 70 AH"]
+[7.288148403167725, 12.447123527526855, "Satellite Instrument Cirrus Cloud Properties Derived"]
+[-1.29921555519104, 4.446972846984863, "Ground-Based Instrument Network Validation Tool Used"]
+[-2.491598129272461, 12.570273399353027, "Spectral Imager Spectral Bands 13"]
+[-2.4853768348693848, 12.584765434265137, "Spectral Imager Spatial Sampling Distance 10 m, 20 m, 60 m"]
+[-2.2829010486602783, 6.274825572967529, "Focal Plane Array Filters 10"]
+[-2.2874245643615723, 6.250865459442139, "Focal Plane Array Pitch 7.5-15 \u00b5m"]
+[-2.279846668243408, 6.25732946395874, "Focal Plane Array Pixels 31,152-15,576"]
+[-2.308497667312622, 6.287900447845459, "Focal Plane Array Temperature 293K"]
+[-2.280054807662964, 6.260501861572266, "Focal Plane Array TDI Stage 1 for 2 lines"]
+[-2.2733118534088135, 6.266729354858398, "Focal Plane Array TDI Stage 1 for 2 lines, 2 additional lines for pixel deselection"]
+[-6.69326114654541, 9.900137901306152, "Antenna Signal Down-Conversion IF"]
+[-1.5733919143676758, 8.145137786865234, "Unit Digitizer 8 bit"]
+[2.2746706008911133, -2.3989598751068115, "Satellite BAQ Option 2-6 bits"]
+[-5.9214186668396, 8.441814422607422, "Channel Data Output Rate 31.25 MHz"]
+[-6.7103095054626465, 9.987398147583008, "Antenna PRF 2800-3700 Hz"]
+[-3.671332359313965, 7.120744228363037, "Data Archive Availability Public"]
+[-1.6596509218215942, 5.343754291534424, "Mission Operations Center Location UCB/SSL"]
+[-1.1230181455612183, 5.555210113525391, "Communication Facility Operator ASI (Agenzia Spaziale Italiana)"]
+[-1.1235148906707764, 4.4595255851745605, "Ground Station Location Visibility Once per 90 minute orbit"]
+[-1.1245157718658447, 4.463296413421631, "Ground Station Location Command Preparation Time Up to 12 hours"]
+[-3.2765069007873535, 5.4291887283325195, "Launch Vehicle Payload Capability 1750 kg in 600 km SSPO"]
+[-3.2794737815856934, 5.436399936676025, "Launch Vehicle Payload Capability 1425 kg for the Sub-GTO (Sub Geosynchronous Transfer Orbit) of 284 km x 21,000 km"]
+[-3.2694337368011475, 5.427340984344482, "Launch Vehicle Liquid Propellant Capacity 2.5 tons"]
+[-3.2782464027404785, 5.45601749420166, "Launch Vehicle Heaviest Satellite Mass 1858 kg"]
+[2.1863842010498047, -2.6989715099334717, "Satellite Camera Quantity 4"]
+[1.4440807104110718, -1.1266396045684814, "Satellite Sky Section Size 24 x 96 degree"]
+[4.4168853759765625, -2.68835711479187, "Satellite Observation Duration 27 days"]
+[0.7916684746742249, -1.6056081056594849, "Satellite Maximum Distance to Stars 300 light-years"]
+[1.3769093751907349, 7.062406063079834, "Communication Equipment Antenna Diameter 2.4 m"]
+[1.4124926328659058, 7.042575836181641, "Communication Equipment Antenna Diameter 5 m"]
+[-5.325343132019043, 7.73795747756958, "Communication Network Speed 622 Mbit/s"]
+[-5.316175937652588, 7.768149375915527, "Communication Network Speed 1244 Mbit/s"]
+[-5.796702861785889, 9.348618507385254, "Radio Antenna Type Dual patch antennas"]
+[-6.816462516784668, 10.081628799438477, "Antenna Antenna Size 21 m"]
+[-5.7772064208984375, 9.356141090393066, "Radio Antenna Data Rate 128 kbit/s with the 34 m DSN antennas and 64 kbit/s with the MSU 21 m Ground Station"]
+[-5.776455879211426, 9.364631652832031, "Radio Weight 0.875 kg"]
+[-5.742515563964844, 9.34218692779541, "Radio Output Power 4 W"]
+[-0.7656602263450623, 11.548442840576172, "Detector Light Sensor Silicon Photomultipliers (SiPMs)"]
+[-0.8194151520729065, 11.601415634155273, "Detector Sensitivity Main prompt emission energy of GRBs"]
+[-0.8067578077316284, 11.613140106201172, "Detector Field-of-View Wide"]
+[-0.8463438153266907, 11.623064041137695, "Detector Effective Area Falloff Approximately cosine"]
+[-1.885554313659668, 14.91934585571289, "Scanning Radiometer Optical System Catoptric"]
+[-1.866381049156189, 14.94803524017334, "Scanning Radiometer Scanning Method Mechanical rotating with a mirror"]
+[-1.8638319969177246, 14.912763595581055, "Scanning Radiometer IR Detector Temperature 100 K"]
+[-1.8341758251190186, 14.955826759338379, "Scanning Radiometer Calibration Methods Solar and internal lamp for VNIR, deep space and black body for IR"]
+[2.2967607975006104, 22.266422271728516, "Instrument Detector Format 640 x 480 pixels"]
+[1.9087454080581665, 22.153165817260742, "Instrument Spatial Resolution 200 m (ALOS-2), 130 m (CALET)"]
+[1.6154067516326904, 22.186838150024414, "Instrument Size 110 mm x 180 mm x 230 mm"]
+[1.6235454082489014, 23.22357177734375, "Instrument Power Consumption <20 W"]
+[-4.490481853485107, 8.288254737854004, "Local User Terminal Location Bangalore"]
+[-1.6720305681228638, 5.351631164550781, "Mission Control Center Location Unknown"]
+[-1.354097604751587, 5.366928577423096, "Centers Locations Mumbai, Kolkata, Delhi and Chennai"]
+[-1.2894083261489868, 6.1858134269714355, "Organizations Activities Search and rescue"]
+[-1.7030576467514038, 5.354013919830322, "Mission Control Center Communication Linked to the RCCs and other international MCCs through automatic telex and Aeronautical Fixed Telecommunication Network (AFTN)"]
+[5.171016693115234, -2.2853164672851562, "Satellite Operational Lifetime 10 years"]
+[4.925466060638428, -2.4150853157043457, "Satellite On-Orbit Spare Lifetime 5 years"]
+[2.7282776832580566, -1.0836427211761475, "Satellite Purpose Geostationary meteorological imager"]
+[1.073500633239746, -4.45920991897583, "Satellite Mass 60.7 kg"]
+[2.1373026371002197, -0.5689893364906311, "Satellite Power 54 W (40 W average load)"]
+[1.485746145248413, -2.3441154956817627, "Satellite Stabilization Gravity gradient boom and active magnetic torquing"]
+[-5.501702785491943, 3.2342069149017334, "Star Imager Camera Power 37 W EOL"]
+[-3.1032395362854004, 9.665143013000488, "Battery Capacity 6 Ah"]
+[5.166172981262207, -2.2474873065948486, "Satellite Design Life At least one year (three year goal)"]
\ No newline at end of file