GEESAT 2-02, 58906
Orbit data source: Space-Track
GEESAT 2-02, 58906 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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58906 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 2-02
1 58906U 24023B 25304.28480139 .00004164 00000-0 45180-3 0 9994
2 58906 49.9992 334.5440 0010722 311.7307 48.2717 14.89942820 94930Epoch: 2025-10-31T06:50Z
TLE epoch observation values (Epoch: 2025-10-31T06:50:06.840Z)
Latitude
0.00005°
Longitude
-167.8159°
Altitude
593.686 km
Speed
7.567 km/s
True Right ascension
22h 18m 10s
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
09:45:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
606.355 km
Perigee altitude
591.394 km
Semi-major axis
6,977.012 km
Eccentricity
0.00107
Inclination
49.9992°
RAAN
334.544°
Arg. of periapsis
311.7307°
True anomaly
48.36348°
Mean anomaly
48.2717°
Eccentric anomaly
48.31758°
Mean motion
3.72425 °/min
Orbital period
96.66 mins
BSTAR
0.0004518
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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 2-02 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-01 03:54:37.667Z | 182.389° SSW | 2025-11-01 03:57:37.667Z | 135.636° SSE | 21.444° | 2025-11-01 04:00:37.667Z | 85.838° E |
| 7 mins | 2025-11-01 05:35:37.667Z | 251.435° W | 2025-11-01 05:38:37.667Z | 348.854° N | 41.859° | 2025-11-01 05:42:37.667Z | 51.419° ENE |
| 5 mins | 2025-11-01 07:17:37.667Z | 305.718° NW | 2025-11-01 07:19:37.667Z | 341.181° N | 22.633° | 2025-11-01 07:22:37.667Z | 35.404° NE |
| 5 mins | 2025-11-01 08:59:37.667Z | 327.603° NNW | 2025-11-01 09:01:37.667Z | 2.251° NNE | 21.968° | 2025-11-01 09:04:37.667Z | 55.461° ENE |
| 7 mins | 2025-11-01 10:40:37.667Z | 314.959° NW | 2025-11-01 10:43:37.667Z | 31.252° NE | 40.214° | 2025-11-01 10:47:37.667Z | 108.185° ESE |
| 6 mins | 2025-11-01 12:21:37.667Z | 274.738° WNW | 2025-11-01 12:24:37.667Z | 218.706° SW | 24.411° | 2025-11-01 12:27:37.667Z | 171.46° 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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