GEESAT 2-01, 58905
Orbit data source: Space-Track
GEESAT 2-01, 58905 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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58905 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 2-01
1 58905U 24023A 26171.44371947 .00001171 00000-0 16897-3 0 9998
2 58905 49.9962 339.0085 0005094 44.3034 315.8311 14.83262610129391Epoch: 2026-06-20T10:38Z
TLE epoch observation values (Epoch: 2026-06-20T10:38:57.362Z)
Latitude
-0.00002°
Longitude
-89.38878°
Altitude
617.032 km
Speed
7.553 km/s
True Right ascension
22h 36m 02s
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
21:34:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
623.368 km
Perigee altitude
616.239 km
Semi-major axis
6,997.94 km
Eccentricity
0.00051
Inclination
49.9962°
RAAN
339.0085°
Arg. of periapsis
44.3034°
True anomaly
315.79041°
Mean anomaly
315.8311°
Eccentric anomaly
315.81076°
Mean motion
3.70756 °/min
Orbital period
97.1 mins
BSTAR
0.00016897
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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 2-01 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 12:55:29.165Z | 203.5° SW | 2026-06-22 12:59:29.165Z | 137.877° SSE | 31.278° | 2026-06-22 13:03:29.165Z | 70.371° E |
| 6 mins | 2026-06-22 14:38:29.165Z | 271.964° WNW | 2026-06-22 14:40:29.165Z | 317.052° NNW | 35.238° | 2026-06-22 14:44:29.165Z | 44.903° NE |
| 5 mins | 2026-06-22 16:21:29.165Z | 323.705° NNW | 2026-06-22 16:23:29.165Z | 2.071° NNE | 21.207° | 2026-06-22 16:26:29.165Z | 45.717° ENE |
| 5 mins | 2026-06-22 18:03:29.165Z | 333.216° NNW | 2026-06-22 18:05:29.165Z | 13.365° NNE | 25.319° | 2026-06-22 18:08:29.165Z | 67.398° ENE |
| 7 mins | 2026-06-22 19:44:29.165Z | 305.557° NW | 2026-06-22 19:47:29.165Z | 61.552° ENE | 44.927° | 2026-06-22 19:51:29.165Z | 123.711° 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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