GEESAT 2-09, 58913
Orbit data source: Space-Track
GEESAT 2-09, 58913 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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58913 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 2-09
1 58913U 24023J 26171.45148517 .00001105 00000-0 16109-3 0 9996
2 58913 50.0049 339.0571 0021725 20.1819 339.9973 14.83240860129407Epoch: 2026-06-20T10:50Z
TLE epoch observation values (Epoch: 2026-06-20T10:50:08.318Z)
Latitude
-0.00007°
Longitude
-92.14354°
Altitude
605.378 km
Speed
7.566 km/s
True Right ascension
22h 36m 13s
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
21:50:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
635.073 km
Perigee altitude
604.667 km
Semi-major axis
6,998.007 km
Eccentricity
0.00217
Inclination
50.0049°
RAAN
339.0571°
Arg. of periapsis
20.1819°
True anomaly
339.91193°
Mean anomaly
339.9973°
Eccentric anomaly
339.95463°
Mean motion
3.7075 °/min
Orbital period
97.1 mins
BSTAR
0.00016109
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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 2-09 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 13:07:01.960Z | 210.495° SW | 2026-06-22 13:11:01.960Z | 143.497° SSE | 35.32° | 2026-06-22 13:15:01.960Z | 67.506° E |
| 6 mins | 2026-06-22 14:50:01.960Z | 276.575° WNW | 2026-06-22 14:53:01.960Z | 351.39° N | 32.328° | 2026-06-22 14:56:01.960Z | 42.493° NE |
| 5 mins | 2026-06-22 16:33:01.960Z | 322.908° NNW | 2026-06-22 16:35:01.960Z | 359.513° N | 20.829° | 2026-06-22 16:38:01.960Z | 45.454° ENE |
| 6 mins | 2026-06-22 18:15:01.960Z | 330.593° NNW | 2026-06-22 18:17:01.960Z | 10.079° NNE | 26.692° | 2026-06-22 18:21:01.960Z | 78.322° E |
| 7 mins | 2026-06-22 19:56:01.960Z | 301.111° NW | 2026-06-22 19:59:01.960Z | 230.236° WSW | 44.536° | 2026-06-22 20:03:01.960Z | 130.427° SE |
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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