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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Edit Public Description
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: 7 hours ago
TLE from 7 hours ago
0 GEESAT 2-05
1 58909U 24023E 25304.31450409 .00004182 00000-0 45387-3 0 9997
2 58909 50.0052 334.3673 0008656 314.6354 45.3881 14.89931746 94942Epoch: 2025-10-31T07:32Z
TLE epoch observation values (Epoch: 2025-10-31T07:32:53.153Z)
Latitude
0.00002°
Longitude
-178.71487°
Altitude
594.457 km
Speed
7.566 km/s
True Right ascension
22h 17m 28s
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
09:43:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.948 km
Perigee altitude
592.869 km
Semi-major axis
6,977.045 km
Eccentricity
0.00087
Inclination
50.0052°
RAAN
334.3673°
Arg. of periapsis
314.6354°
True anomaly
45.45877°
Mean anomaly
45.3881°
Eccentric anomaly
45.42343°
Mean motion
3.72422 °/min
Orbital period
96.66 mins
BSTAR
0.00045387
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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 | 2025-11-01 04:38:19.121Z | 214.075° SW | 2025-11-01 04:42:19.121Z | 134.773° SE | 37.946° | 2025-11-01 04:46:19.121Z | 64.624° ENE |
| 7 mins | 2025-11-01 06:20:19.121Z | 276.323° WNW | 2025-11-01 06:23:19.121Z | 338.175° N | 31.207° | 2025-11-01 06:27:19.121Z | 45.583° ENE |
| 5 mins | 2025-11-01 08:03:19.121Z | 324.77° NNW | 2025-11-01 08:05:19.121Z | 1.383° NNE | 20.412° | 2025-11-01 08:08:19.121Z | 46.936° ENE |
| 6 mins | 2025-11-01 09:44:19.121Z | 324.824° NNW | 2025-11-01 09:47:19.121Z | 25.149° NE | 27.362° | 2025-11-01 09:50:19.121Z | 77.015° E |
| 7 mins | 2025-11-01 11:25:19.121Z | 298.786° NW | 2025-11-01 11:28:19.121Z | 220.582° SW | 43.708° | 2025-11-01 11:32:19.121Z | 133.731° 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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