GEESAT 1-03, 52787
Orbit data source: Space-Track
GEESAT 1-03, 52787 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Thu, 02 Jun 2022 UTC via a CHANG ZHENG 2C launch vehicle from the Xichang Space Center, China (XSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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52787 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GWCG
Mission
Operational Commercial Navigation
Bus & Motor
GPS100, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 GEESAT 1-03
1 52787U 22058C 26171.40397159 .00000905 00000-0 14269-3 0 9990
2 52787 49.9857 186.5338 0007658 118.0547 242.1165 14.81384839220418Epoch: 2026-06-20T09:41Z
TLE epoch observation values (Epoch: 2026-06-20T09:41:43.145Z)
Latitude
-0.00005°
Longitude
132.48491°
Altitude
628.009 km
Speed
7.544 km/s
True Right ascension
12h 26m 08s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
00:54:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.08 km
Perigee altitude
620.353 km
Semi-major axis
7,003.853 km
Eccentricity
0.00077
Inclination
49.9857°
RAAN
186.5338°
Arg. of periapsis
118.0547°
True anomaly
242.03897°
Mean anomaly
242.1165°
Eccentric anomaly
242.07773°
Mean motion
3.70286 °/min
Orbital period
97.22 mins
BSTAR
0.00014269
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Other satellites on launch #58 in the year 2022 (2022-06-02 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GEESAT 1-03 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-23 02:36:51.621Z | 203.906° SW | 2026-06-23 02:40:51.621Z | 125.172° SE | 32.687° | 2026-06-23 02:43:51.621Z | 72.818° E |
| 7 mins | 2026-06-23 04:18:51.621Z | 267.686° W | 2026-06-23 04:21:51.621Z | 326.786° NNW | 34.819° | 2026-06-23 04:25:51.621Z | 45.442° ENE |
| 6 mins | 2026-06-23 06:01:51.621Z | 311.847° NW | 2026-06-23 06:04:51.621Z | 3.66° NNE | 21.156° | 2026-06-23 06:07:51.621Z | 46.75° ENE |
| 6 mins | 2026-06-23 07:44:51.621Z | 332.086° NNW | 2026-06-23 07:46:51.621Z | 12.002° NNE | 26.017° | 2026-06-23 07:50:51.621Z | 76.721° E |
| 7 mins | 2026-06-23 09:25:51.621Z | 303.608° NW | 2026-06-23 09:28:51.621Z | 282.363° WNW | 44.857° | 2026-06-23 09:32:51.621Z | 126.541° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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