GEESAT 2-05, 58909
Orbit data source: Space-Track
GEESAT 2-05, 58909 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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58909 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 2-05
1 58909U 24023E 26171.45861763 .00001194 00000-0 17189-3 0 9993
2 58909 50.0061 339.1947 0011007 77.2913 282.9255 14.83268439129406Epoch: 2026-06-20T11:00Z
TLE epoch observation values (Epoch: 2026-06-20T11:00:24.563Z)
Latitude
-0.00001°
Longitude
-94.5806°
Altitude
617.856 km
Speed
7.552 km/s
True Right ascension
22h 36m 46s
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
21:39:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.486 km
Perigee altitude
612.081 km
Semi-major axis
6,997.92 km
Eccentricity
0.0011
Inclination
50.0061°
RAAN
339.1947°
Arg. of periapsis
77.2913°
True anomaly
282.80253°
Mean anomaly
282.9255°
Eccentric anomaly
282.86402°
Mean motion
3.70757 °/min
Orbital period
97.1 mins
BSTAR
0.00017189
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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 2-05 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 13:17:48.187Z | 215.911° SW | 2026-06-22 13:21:48.187Z | 139.519° SSE | 39.132° | 2026-06-22 13:25:48.187Z | 64.185° ENE |
| 6 mins | 2026-06-22 15:00:48.187Z | 282.026° WNW | 2026-06-22 15:03:48.187Z | 352.339° N | 30.263° | 2026-06-22 15:06:48.187Z | 41.803° NE |
| 5 mins | 2026-06-22 16:43:48.187Z | 324.807° NNW | 2026-06-22 16:45:48.187Z | 1.003° NNE | 20.664° | 2026-06-22 16:48:48.187Z | 47.066° ENE |
| 6 mins | 2026-06-22 18:25:48.187Z | 330.391° NNW | 2026-06-22 18:27:48.187Z | 11.718° NNE | 28.227° | 2026-06-22 18:31:48.187Z | 82.352° E |
| 7 mins | 2026-06-22 20:06:48.187Z | 296.697° NW | 2026-06-22 20:09:48.187Z | 213.042° SW | 42.817° | 2026-06-22 20:13:48.187Z | 136.287° 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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