GEESAT 2-06, 58910
Orbit data source: Space-Track
GEESAT 2-06, 58910 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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58910 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 2-06
1 58910U 24023F 25304.24183225 .00008968 00000-0 71241-3 0 9994
2 58910 49.9889 313.1073 0006265 232.2112 127.8266 15.01058029 95212Epoch: 2025-10-31T05:48Z
TLE epoch observation values (Epoch: 2025-10-31T05:48:14.306Z)
Latitude
-0.00006°
Longitude
-173.74144°
Altitude
566.848 km
Speed
7.578 km/s
True Right ascension
20h 52m 25s
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
568.748 km
Perigee altitude
560.049 km
Semi-major axis
6,942.535 km
Eccentricity
0.00063
Inclination
49.9889°
RAAN
313.1073°
Arg. of periapsis
232.2112°
True anomaly
127.88328°
Mean anomaly
127.8266°
Eccentric anomaly
127.85494°
Mean motion
3.75203 °/min
Orbital period
95.95 mins
BSTAR
0.00071241
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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 2-06 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 02:44:19.477Z | 187.118° SSW | 2025-11-01 02:47:19.477Z | 127.329° SE | 25.472° | 2025-11-01 02:50:19.477Z | 77.815° E |
| 6 mins | 2025-11-01 04:24:19.477Z | 261.092° W | 2025-11-01 04:27:19.477Z | 347.524° N | 37.804° | 2025-11-01 04:30:19.477Z | 45.55° ENE |
| 4 mins | 2025-11-01 06:06:19.477Z | 320.192° NNW | 2025-11-01 06:08:19.477Z | 0.174° NNE | 20.448° | 2025-11-01 06:10:19.477Z | 34.094° NE |
| 5 mins | 2025-11-01 07:47:19.477Z | 336.132° NNW | 2025-11-01 07:49:19.477Z | 16.906° NNE | 22.048° | 2025-11-01 07:52:19.477Z | 65.219° ENE |
| 6 mins | 2025-11-01 09:27:19.477Z | 313.059° NW | 2025-11-01 09:30:19.477Z | 71.946° E | 41.146° | 2025-11-01 09:33:19.477Z | 113.279° SE |
| 4 mins | 2025-11-01 11:08:19.477Z | 254.028° W | 2025-11-01 11:09:19.477Z | 235.252° WSW | 19.42° | 2025-11-01 11:12:19.477Z | 183.8° SSW |
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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