GEESAT 1-07, 52791
Orbit data source: Space-Track
GEESAT 1-07, 52791 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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52791 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 1-07
1 52791U 22058G 26171.39633963 .00000886 00000-0 14036-3 0 9999
2 52791 49.9872 186.6769 0012089 107.9360 252.2896 14.81395555220402Epoch: 2026-06-20T09:30Z
TLE epoch observation values (Epoch: 2026-06-20T09:30:43.744Z)
Latitude
-0.00001°
Longitude
135.38306°
Altitude
628.049 km
Speed
7.544 km/s
True Right ascension
12h 26m 42s
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
21:49:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
634.149 km
Perigee altitude
617.215 km
Semi-major axis
7,003.819 km
Eccentricity
0.00121
Inclination
49.9872°
RAAN
186.6769°
Arg. of periapsis
107.936°
True anomaly
252.1577°
Mean anomaly
252.2896°
Eccentric anomaly
252.22364°
Mean motion
3.70289 °/min
Orbital period
97.22 mins
BSTAR
0.00014036
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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 1-07 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 02:25:44.238Z | 194.266° SSW | 2026-06-23 02:28:44.238Z | 144.208° SSE | 28.337° | 2026-06-23 02:32:44.238Z | 74.134° E |
| 7 mins | 2026-06-23 04:07:44.238Z | 264.321° W | 2026-06-23 04:10:44.238Z | 346.236° N | 37.508° | 2026-06-23 04:14:44.238Z | 48.831° ENE |
| 5 mins | 2026-06-23 05:50:44.238Z | 315.609° NNW | 2026-06-23 05:52:44.238Z | 352.008° N | 21.87° | 2026-06-23 05:55:44.238Z | 40.79° NE |
| 6 mins | 2026-06-23 07:32:44.238Z | 325.899° NNW | 2026-06-23 07:35:44.238Z | 22.462° NNE | 24.22° | 2026-06-23 07:38:44.238Z | 68.941° E |
| 7 mins | 2026-06-23 09:14:44.238Z | 308.87° NW | 2026-06-23 09:17:44.238Z | 78.943° E | 43.749° | 2026-06-23 09:21:44.238Z | 119.904° 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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