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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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: 2 days ago
TLE from 2 days ago
0 GEESAT 2-08
1 58912U 24023H 26171.47335100 .00001367 00000-0 19267-3 0 9991
2 58912 49.9909 338.0077 0003815 1.1926 358.9020 14.83262951129405Epoch: 2026-06-20T11:21Z
TLE epoch observation values (Epoch: 2026-06-20T11:21:37.526Z)
Latitude
-0.00006°
Longitude
-101.08617°
Altitude
616.918 km
Speed
7.553 km/s
True Right ascension
22h 32m 01s
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
23:20:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
622.473 km
Perigee altitude
617.133 km
Semi-major axis
6,997.94 km
Eccentricity
0.00038
Inclination
49.9909°
RAAN
338.0077°
Arg. of periapsis
1.1926°
True anomaly
358.90116°
Mean anomaly
358.902°
Eccentric anomaly
358.90158°
Mean motion
3.70756 °/min
Orbital period
97.1 mins
BSTAR
0.00019267
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-22 13:39:56.490Z | 232.081° WSW | 2026-06-22 13:43:56.490Z | 200.499° SSW | 44.626° | 2026-06-22 13:47:56.490Z | 56.995° ENE |
| 5 mins | 2026-06-22 15:23:56.490Z | 300.899° NW | 2026-06-22 15:25:56.490Z | 343.157° N | 26.365° | 2026-06-22 15:28:56.490Z | 37.34° NE |
| 6 mins | 2026-06-22 17:05:56.490Z | 322.678° NNW | 2026-06-22 17:07:56.490Z | 355.146° N | 20.947° | 2026-06-22 17:11:56.490Z | 56.913° ENE |
| 7 mins | 2026-06-22 18:47:56.490Z | 322.443° NNW | 2026-06-22 18:50:56.490Z | 35.447° NE | 33.94° | 2026-06-22 18:54:56.490Z | 96.895° ESE |
| 7 mins | 2026-06-22 20:28:56.490Z | 286.994° WNW | 2026-06-22 20:31:56.490Z | 228.261° WSW | 34.035° | 2026-06-22 20:35:56.490Z | 153.285° 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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