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
Taizhou Xingkong
Mission
Operational Commercial Navigation
Bus & Motor
GEESAT1, 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: 18 hours ago
TLE from 18 hours ago
0 GEESAT 2-04
1 58908U 24023D 25249.33174109 .00003268 00000-0 31611-3 0 9995
2 58908 49.9903 225.2257 0006806 6.2135 353.8891 14.95239216 86821Epoch: 2025-09-06T07:57Z
TLE epoch observation values (Epoch: 2025-09-06T07:57:42.43Z)
Latitude
-0.00003°
Longitude
120.13179°
Altitude
577.467 km
Speed
7.576 km/s
True Right ascension
15h 00m 54s
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
18:02:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.131 km
Perigee altitude
577.657 km
Semi-major axis
6,960.531 km
Eccentricity
0.00068
Inclination
49.9903°
RAAN
225.2257°
Arg. of periapsis
6.2135°
True anomaly
353.88079°
Mean anomaly
353.8891°
Eccentric anomaly
353.88495°
Mean motion
3.73749 °/min
Orbital period
96.32 mins
BSTAR
0.00031611
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Other satellites on launch #23 in the year 2024 (2024-02-02 UTC)
GEESAT 2-04 Visibility forecast
Observer location: undefined°, undefined°
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-07 03:29:55.958Z | 293.31° NW | 2025-09-07 03:32:55.958Z | 343.283° N | 23.19° | 2025-09-07 03:35:55.958Z | 36.918° NE |
| 5 mins | 2025-09-07 05:12:55.958Z | 334.322° NNW | 2025-09-07 05:14:55.958Z | 12.815° NNE | 20.67° | 2025-09-07 05:17:55.958Z | 58.511° ENE |
| 7 mins | 2025-09-07 06:52:55.958Z | 316.964° NNW | 2025-09-07 06:55:55.958Z | 24.107° NE | 36.94° | 2025-09-07 06:59:55.958Z | 102.169° ESE |
| 6 mins | 2025-09-07 08:33:55.958Z | 276.744° WNW | 2025-09-07 08:36:55.958Z | 210.304° SW | 27.56° | 2025-09-07 08:39:55.958Z | 163.185° S |
| 6 mins | 2025-09-08 00:13:55.958Z | 184.873° SSW | 2025-09-08 00:15:55.958Z | 145.757° SSE | 26.557° | 2025-09-08 00:19:55.958Z | 74.626° 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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Authenticating...
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