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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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: 8 hours ago
TLE from 8 hours ago
0 GEESAT 2-04
1 58908U 24023D 25304.25835528 .00003888 00000-0 36734-3 0 9996
2 58908 49.9930 325.9073 0006512 224.4543 135.5878 14.95706120 95043Epoch: 2025-10-31T06:12Z
TLE epoch observation values (Epoch: 2025-10-31T06:12:01.896Z)
Latitude
-0.00003°
Longitude
-166.90599°
Altitude
583.966 km
Speed
7.568 km/s
True Right ascension
21h 43m 37s
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
09:45:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.477 km
Perigee altitude
576.414 km
Semi-major axis
6,959.082 km
Eccentricity
0.00065
Inclination
49.993°
RAAN
325.9073°
Arg. of periapsis
224.4543°
True anomaly
135.63999°
Mean anomaly
135.5878°
Eccentric anomaly
135.6139°
Mean motion
3.73865 °/min
Orbital period
96.29 mins
BSTAR
0.00036734
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-01 03:11:38.655Z | 175.311° S | 2025-11-01 03:14:38.655Z | 128.923° SE | 18.324° | 2025-11-01 03:16:38.655Z | 96.086° ESE |
| 7 mins | 2025-11-01 04:51:38.655Z | 244.168° WSW | 2025-11-01 04:54:38.655Z | 325.022° NNW | 43.859° | 2025-11-01 04:58:38.655Z | 52.754° ENE |
| 5 mins | 2025-11-01 06:33:38.655Z | 305.577° NW | 2025-11-01 06:35:38.655Z | 344.435° N | 23.218° | 2025-11-01 06:38:38.655Z | 37.336° NE |
| 5 mins | 2025-11-01 08:15:38.655Z | 335.483° NNW | 2025-11-01 08:17:38.655Z | 14.384° NNE | 20.718° | 2025-11-01 08:20:38.655Z | 59.355° ENE |
| 7 mins | 2025-11-01 09:55:38.655Z | 317.424° NNW | 2025-11-01 09:58:38.655Z | 29.441° NE | 37.194° | 2025-11-01 10:02:38.655Z | 103.075° ESE |
| 6 mins | 2025-11-01 11:36:38.655Z | 274.778° WNW | 2025-11-01 11:38:38.655Z | 235.244° WSW | 27.328° | 2025-11-01 11:42:38.655Z | 162.733° S |
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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