GEESAT 1-04, 52788
Orbit data source: Space-Track
GEESAT 1-04, 52788 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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52788 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: 6 hours ago
TLE from 6 hours ago
0 GEESAT 1-04
1 52788U 22058D 25347.04241760 .00007135 00000-0 63011-3 0 9992
2 52788 50.0045 347.4064 0002704 46.0132 314.1035 14.97246375192268Epoch: 2025-12-13T01:01Z
TLE epoch observation values (Epoch: 2025-12-13T01:01:04.880Z)
Latitude
-0.00001°
Longitude
-109.83931°
Altitude
574.649 km
Speed
7.575 km/s
True Right ascension
23h 09m 37s
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
05:21:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.052 km
Perigee altitude
574.291 km
Semi-major axis
6,954.308 km
Eccentricity
0.00027
Inclination
50.0045°
RAAN
347.4064°
Arg. of periapsis
46.0132°
True anomaly
314.08124°
Mean anomaly
314.1035°
Eccentric anomaly
314.09237°
Mean motion
3.7425 °/min
Orbital period
96.19 mins
BSTAR
0.00063011
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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 1-04 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 | 2025-12-13 07:50:15.424Z | 319.863° NNW | 2025-12-13 07:53:15.424Z | 9.118° NNE | 24.183° | 2025-12-13 07:56:15.424Z | 66.543° ENE |
| 7 mins | 2025-12-13 09:31:15.424Z | 304.987° NW | 2025-12-13 09:34:15.424Z | 327.602° NNW | 44.84° | 2025-12-13 09:38:15.424Z | 124.341° SE |
| 6 mins | 2025-12-14 02:50:15.424Z | 217.25° SW | 2025-12-14 02:53:15.424Z | 120.607° SE | 41.067° | 2025-12-14 02:56:15.424Z | 63.679° ENE |
| 6 mins | 2025-12-14 04:31:15.424Z | 287.44° WNW | 2025-12-14 04:33:15.424Z | 327.879° NNW | 27.778° | 2025-12-14 04:37:15.424Z | 42.753° NE |
| 4 mins | 2025-12-14 06:13:15.424Z | 327.908° NNW | 2025-12-14 06:15:15.424Z | 4.995° NNE | 19.44° | 2025-12-14 06:17:15.424Z | 38.995° NE |
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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