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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 GEESAT 1-04
1 52788U 22058D 26171.41139668 .00000881 00000-0 13967-3 0 9998
2 52788 50.0029 188.1620 0009456 164.0376 196.0861 14.81407081220408Epoch: 2026-06-20T09:52Z
TLE epoch observation values (Epoch: 2026-06-20T09:52:24.673Z)
Latitude
-0.00001°
Longitude
131.43278°
Altitude
631.793 km
Speed
7.54 km/s
True Right ascension
12h 32m 38s
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
21:57:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
632.266 km
Perigee altitude
619.02 km
Semi-major axis
7,003.78 km
Eccentricity
0.00095
Inclination
50.0029°
RAAN
188.162°
Arg. of periapsis
164.0376°
True anomaly
196.05611°
Mean anomaly
196.0861°
Eccentric anomaly
196.0711°
Mean motion
3.70292 °/min
Orbital period
97.22 mins
BSTAR
0.00013967
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 10:58:34.845Z | 284.656° WNW | 2026-06-22 11:02:34.845Z | 219.641° SW | 26.03° | 2026-06-22 11:05:34.845Z | 170.237° S |
| 7 mins | 2026-06-23 02:48:34.845Z | 200.491° SSW | 2026-06-23 02:51:34.845Z | 128.28° SE | 34.595° | 2026-06-23 02:55:34.845Z | 66.849° ENE |
| 7 mins | 2026-06-23 04:29:34.845Z | 268.984° W | 2026-06-23 04:32:34.845Z | 322.874° NNW | 33.621° | 2026-06-23 04:36:34.845Z | 44.129° NE |
| 5 mins | 2026-06-23 06:13:34.845Z | 323.879° NNW | 2026-06-23 06:15:34.845Z | 1.019° NNE | 21.243° | 2026-06-23 06:18:34.845Z | 45.863° ENE |
| 6 mins | 2026-06-23 07:55:34.845Z | 330.049° NNW | 2026-06-23 07:57:34.845Z | 8.521° NNE | 26.483° | 2026-06-23 08:01:34.845Z | 77.067° E |
| 7 mins | 2026-06-23 09:36:34.845Z | 302.171° NW | 2026-06-23 09:39:34.845Z | 270.835° WNW | 44.308° | 2026-06-23 09:43:34.845Z | 129.18° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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