GEESAT 2-11, 58915
Orbit data source: Space-Track
GEESAT 2-11, 58915 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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58915 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 2-11
1 58915U 24023L 26171.46583429 .00001482 00000-0 20649-3 0 9996
2 58915 50.0012 338.8005 0019451 125.8421 234.4327 14.83265222129404Epoch: 2026-06-20T11:10Z
TLE epoch observation values (Epoch: 2026-06-20T11:10:48.082Z)
Latitude
-0.00006°
Longitude
-97.57995°
Altitude
627.514 km
Speed
7.542 km/s
True Right ascension
22h 35m 12s
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
21:47:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
633.406 km
Perigee altitude
606.183 km
Semi-major axis
6,997.931 km
Eccentricity
0.00195
Inclination
50.0012°
RAAN
338.8005°
Arg. of periapsis
125.8421°
True anomaly
234.25165°
Mean anomaly
234.4327°
Eccentric anomaly
234.34215°
Mean motion
3.70756 °/min
Orbital period
97.1 mins
BSTAR
0.00020649
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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 2-11 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 13:29:49.210Z | 220.437° SW | 2026-06-22 13:32:49.210Z | 132.151° SE | 42.7° | 2026-06-22 13:36:49.210Z | 60.58° ENE |
| 6 mins | 2026-06-22 15:11:49.210Z | 287.5° WNW | 2026-06-22 15:14:49.210Z | 352.41° N | 28.065° | 2026-06-22 15:17:49.210Z | 41.089° NE |
| 5 mins | 2026-06-22 16:54:49.210Z | 326.255° NNW | 2026-06-22 16:56:49.210Z | 1.984° NNE | 20.622° | 2026-06-22 16:59:49.210Z | 48.931° ENE |
| 6 mins | 2026-06-22 18:36:49.210Z | 329.046° NNW | 2026-06-22 18:38:49.210Z | 12.457° NNE | 30.404° | 2026-06-22 18:42:49.210Z | 87.48° E |
| 7 mins | 2026-06-22 20:17:49.210Z | 290.836° WNW | 2026-06-22 20:20:49.210Z | 211.052° SW | 39.022° | 2026-06-22 20:24:49.210Z | 143.347° 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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