GEESAT 1-05, 52789
Orbit data source: Space-Track
GEESAT 1-05, 52789 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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52789 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 1-05
1 52789U 22058E 25348.98378688 .00004350 00000-0 37979-3 0 9997
2 52789 49.9879 336.2494 0003000 101.0323 259.0959 14.98575805192567Epoch: 2025-12-14T23:36Z
TLE epoch observation values (Epoch: 2025-12-14T23:36:39.186Z)
Latitude
-0.00002°
Longitude
-101.80276°
Altitude
572.237 km
Speed
7.576 km/s
True Right ascension
22h 24m 59s
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
13:23:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.146 km
Perigee altitude
569.976 km
Semi-major axis
6,950.198 km
Eccentricity
0.0003
Inclination
49.9879°
RAAN
336.2494°
Arg. of periapsis
101.0323°
True anomaly
259.06215°
Mean anomaly
259.0959°
Eccentric anomaly
259.07902°
Mean motion
3.74582 °/min
Orbital period
96.11 mins
BSTAR
0.00037979
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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 1-05 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 01:22:20.652Z | 198.211° SSW | 2025-12-16 01:26:20.652Z | 121.396° SE | 27.751° | 2025-12-16 01:29:20.652Z | 74.221° E |
| 6 mins | 2025-12-16 03:03:20.652Z | 265.369° W | 2025-12-16 03:06:20.652Z | 345.062° N | 35.978° | 2025-12-16 03:09:20.652Z | 43.954° NE |
| 5 mins | 2025-12-16 04:45:20.652Z | 318.393° NNW | 2025-12-16 04:47:20.652Z | 356.319° N | 20.281° | 2025-12-16 04:50:20.652Z | 43.123° NE |
| 5 mins | 2025-12-16 06:26:20.652Z | 330.784° NNW | 2025-12-16 06:28:20.652Z | 8.857° NNE | 22.937° | 2025-12-16 06:31:20.652Z | 63.785° ENE |
| 7 mins | 2025-12-16 08:06:20.652Z | 308.391° NW | 2025-12-16 08:09:20.652Z | 23.327° NE | 44.095° | 2025-12-16 08:13:20.652Z | 118.837° 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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