GEESAT 2-08, 58912
Orbit data source: Space-Track
GEESAT 2-08, 58912 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Fri, 02 Feb 2024 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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58912 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: 8 hours ago
TLE from 8 hours ago
0 GEESAT 2-08
1 58912U 24023H 25304.26202638 .00004808 00000-0 51742-3 0 9991
2 58912 49.9897 333.8298 0013487 277.4441 82.4967 14.89947004 94938Epoch: 2025-10-31T06:17Z
TLE epoch observation values (Epoch: 2025-10-31T06:17:19.079Z)
Latitude
-0.00003°
Longitude
-160.30871°
Altitude
597.429 km
Speed
7.563 km/s
True Right ascension
22h 15m 19s
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
09:43:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.273 km
Perigee altitude
589.453 km
Semi-major axis
6,977 km
Eccentricity
0.00135
Inclination
49.9897°
RAAN
333.8298°
Arg. of periapsis
277.4441°
True anomaly
82.64996°
Mean anomaly
82.4967°
Eccentric anomaly
82.57333°
Mean motion
3.72426 °/min
Orbital period
96.66 mins
BSTAR
0.00051742
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Other satellites on launch #23 in the year 2024 (2024-02-02 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 2-08 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-01 05:01:20.449Z | 228.278° WSW | 2025-11-01 05:04:20.449Z | 128.704° SE | 44.473° | 2025-11-01 05:08:20.449Z | 57.996° ENE |
| 6 mins | 2025-11-01 06:43:20.449Z | 295.718° NW | 2025-11-01 06:45:20.449Z | 336.026° NNW | 26.618° | 2025-11-01 06:49:20.449Z | 43.589° NE |
| 5 mins | 2025-11-01 08:25:20.449Z | 324.843° NNW | 2025-11-01 08:27:20.449Z | 359.148° N | 20.698° | 2025-11-01 08:30:20.449Z | 48.66° ENE |
| 7 mins | 2025-11-01 10:06:20.449Z | 320.528° NNW | 2025-11-01 10:09:20.449Z | 22.474° NNE | 32.627° | 2025-11-01 10:13:20.449Z | 92.922° ESE |
| 7 mins | 2025-11-01 11:47:20.449Z | 288.624° WNW | 2025-11-01 11:50:20.449Z | 223.843° SW | 36.093° | 2025-11-01 11:54:20.449Z | 149.136° SSE |
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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