GEESAT 1-08, 52792
Orbit data source: Space-Track
GEESAT 1-08, 52792 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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52792 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: 15 hours ago
TLE from 15 hours ago
0 GEESAT 1-08
1 52792U 22058H 25348.98514484 .00004021 00000-0 36537-3 0 9991
2 52792 49.9934 336.1797 0002320 69.2575 290.8617 14.97180640192579Epoch: 2025-12-14T23:38Z
TLE epoch observation values (Epoch: 2025-12-14T23:38:36.514Z)
Latitude
-0.00004°
Longitude
-102.36268°
Altitude
575.585 km
Speed
7.575 km/s
True Right ascension
22h 24m 43s
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
13:24:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.99 km
Perigee altitude
574.763 km
Semi-major axis
6,954.513 km
Eccentricity
0.00023
Inclination
49.9934°
RAAN
336.1797°
Arg. of periapsis
69.2575°
True anomaly
290.83686°
Mean anomaly
290.8617°
Eccentric anomaly
290.84928°
Mean motion
3.74234 °/min
Orbital period
96.2 mins
BSTAR
0.00036537
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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 1-08 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-16 01:26:16.567Z | 197.697° SSW | 2025-12-16 01:29:16.567Z | 140.654° SSE | 29.969° | 2025-12-16 01:32:16.567Z | 77.675° E |
| 6 mins | 2025-12-16 03:07:16.567Z | 269.975° W | 2025-12-16 03:09:16.567Z | 312.373° NW | 34.277° | 2025-12-16 03:13:16.567Z | 44.76° NE |
| 5 mins | 2025-12-16 04:49:16.567Z | 321.51° NNW | 2025-12-16 04:51:16.567Z | 359.898° N | 20.124° | 2025-12-16 04:54:16.567Z | 44.878° NE |
| 5 mins | 2025-12-16 06:30:16.567Z | 331.568° NNW | 2025-12-16 06:32:16.567Z | 10.541° NNE | 23.588° | 2025-12-16 06:35:16.567Z | 65.583° ENE |
| 7 mins | 2025-12-16 08:10:16.567Z | 306.934° NW | 2025-12-16 08:13:16.567Z | 12.468° NNE | 44.582° | 2025-12-16 08:17:16.567Z | 121.181° 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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