GEESAT 1-09, 52793
Orbit data source: Space-Track
GEESAT 1-09, 52793 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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52793 intel report (Beta)
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Edit Public Description
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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 GEESAT 1-09
1 52793U 22058J 25348.93947693 .00003819 00000-0 33600-3 0 9991
2 52793 49.9984 337.2689 0006653 161.5757 198.5429 14.98586505192596Epoch: 2025-12-14T22:32Z
TLE epoch observation values (Epoch: 2025-12-14T22:32:50.806Z)
Latitude
-0.00008°
Longitude
-84.78806°
Altitude
576.194 km
Speed
7.572 km/s
True Right ascension
22h 29m 04s
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
13:22:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.65 km
Perigee altitude
567.402 km
Semi-major axis
6,950.163 km
Eccentricity
0.00067
Inclination
49.9984°
RAAN
337.2689°
Arg. of periapsis
161.5757°
True anomaly
198.51867°
Mean anomaly
198.5429°
Eccentric anomaly
198.53079°
Mean motion
3.74585 °/min
Orbital period
96.11 mins
BSTAR
0.000336
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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 1-09 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-16 01:55:18.909Z | 218.768° SW | 2025-12-16 01:59:18.909Z | 136.182° SSE | 40.171° | 2025-12-16 02:03:18.909Z | 62.618° ENE |
| 6 mins | 2025-12-16 03:37:18.909Z | 284.657° WNW | 2025-12-16 03:39:18.909Z | 324.577° NNW | 28.394° | 2025-12-16 03:43:18.909Z | 42.483° NE |
| 4 mins | 2025-12-16 05:19:18.909Z | 327.636° NNW | 2025-12-16 05:21:18.909Z | 5.012° NNE | 19.312° | 2025-12-16 05:23:18.909Z | 38.719° NE |
| 5 mins | 2025-12-16 07:00:18.909Z | 333.699° NNW | 2025-12-16 07:02:18.909Z | 19.774° NNE | 27.487° | 2025-12-16 07:05:18.909Z | 77.6° E |
| 6 mins | 2025-12-16 08:40:18.909Z | 294.994° NW | 2025-12-16 08:43:18.909Z | 182.681° SSW | 41.149° | 2025-12-16 08:46:18.909Z | 138.026° SSE |
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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