GEESAT 2-04, 58908
Orbit data source: Space-Track
GEESAT 2-04, 58908 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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58908 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 2-04
1 58908U 24023D 26171.42432618 .00001790 00000-0 17481-3 0 9999
2 58908 49.9942 307.9406 0006013 52.3299 307.8189 14.97198034129811Epoch: 2026-06-20T10:11Z
TLE epoch observation values (Epoch: 2026-06-20T10:11:01.781Z)
Latitude
-0.00009°
Longitude
-113.45604°
Altitude
573.543 km
Speed
7.577 km/s
True Right ascension
20h 31m 45s
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
21:42:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.504 km
Perigee altitude
572.141 km
Semi-major axis
6,954.459 km
Eccentricity
0.0006
Inclination
49.9942°
RAAN
307.9406°
Arg. of periapsis
52.3299°
True anomaly
307.76444°
Mean anomaly
307.8189°
Eccentric anomaly
307.79167°
Mean motion
3.74238 °/min
Orbital period
96.2 mins
BSTAR
0.00017481
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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 2-04 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 12:02:38.950Z | 245.539° WSW | 2026-06-22 12:06:38.950Z | 359.237° N | 42.221° | 2026-06-22 12:09:38.950Z | 50.137° ENE |
| 5 mins | 2026-06-22 13:45:38.950Z | 313.12° NW | 2026-06-22 13:47:38.950Z | 354.769° N | 22.173° | 2026-06-22 13:50:38.950Z | 41.577° NE |
| 5 mins | 2026-06-22 15:26:38.950Z | 329.067° NNW | 2026-06-22 15:28:38.950Z | 5.086° NNE | 20.771° | 2026-06-22 15:31:38.950Z | 56.093° ENE |
| 6 mins | 2026-06-22 17:07:38.950Z | 321.402° NNW | 2026-06-22 17:09:38.950Z | 11.731° NNE | 37.76° | 2026-06-22 17:13:38.950Z | 104.033° ESE |
| 6 mins | 2026-06-22 18:47:38.950Z | 275.449° WNW | 2026-06-22 18:50:38.950Z | 213.363° SW | 25.447° | 2026-06-22 18:53:38.950Z | 166.545° S |
| 5 mins | 2026-06-23 10:26:38.950Z | 184.918° SSW | 2026-06-23 10:28:38.950Z | 140.665° SSE | 28.204° | 2026-06-23 10:31:38.950Z | 79.46° E |
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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