GEESAT 1-06, 52790
Orbit data source: Space-Track
GEESAT 1-06, 52790 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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52790 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 1-06
1 52790U 22058F 25348.93854503 .00003736 00000-0 33741-3 0 9999
2 52790 50.0055 338.1687 0005150 105.3429 254.8084 14.97610296192559Epoch: 2025-12-14T22:31Z
TLE epoch observation values (Epoch: 2025-12-14T22:31:30.290Z)
Latitude
-0.00008°
Longitude
-83.55185°
Altitude
575.77 km
Speed
7.574 km/s
True Right ascension
22h 32m 40s
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
13:22:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.625 km
Perigee altitude
571.464 km
Semi-major axis
6,953.182 km
Eccentricity
0.00052
Inclination
50.0055°
RAAN
338.1687°
Arg. of periapsis
105.3429°
True anomaly
254.75146°
Mean anomaly
254.8084°
Eccentric anomaly
254.77993°
Mean motion
3.74341 °/min
Orbital period
96.17 mins
BSTAR
0.00033741
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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 1-06 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 | 2025-12-16 01:55:23.176Z | 214.452° SW | 2025-12-16 01:58:23.176Z | 164.101° S | 37.82° | 2025-12-16 02:02:23.176Z | 65.34° ENE |
| 5 mins | 2025-12-16 03:37:23.176Z | 289.042° WNW | 2025-12-16 03:39:23.176Z | 338.889° N | 29.782° | 2025-12-16 03:42:23.176Z | 38.759° NE |
| 4 mins | 2025-12-16 05:19:23.176Z | 333.864° NNW | 2025-12-16 05:20:23.176Z | 352.775° N | 19.36° | 2025-12-16 05:23:23.176Z | 43.078° NE |
| 6 mins | 2025-12-16 06:59:23.176Z | 325.834° NNW | 2025-12-16 07:02:23.176Z | 29.085° NE | 26.528° | 2025-12-16 07:05:23.176Z | 78.984° E |
| 6 mins | 2025-12-16 08:40:23.176Z | 295.873° NW | 2025-12-16 08:42:23.176Z | 253.065° W | 42.481° | 2025-12-16 08:46:23.176Z | 134.975° 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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