GEESAT 2-10, 58914
Orbit data source: Space-Track
GEESAT 2-10, 58914 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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58914 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 2-10
1 58914U 24023K 25304.29207492 .00004166 00000-0 45227-3 0 9997
2 58914 49.9952 334.3456 0007921 280.0614 79.9433 14.89925726 94938Epoch: 2025-10-31T07:00Z
TLE epoch observation values (Epoch: 2025-10-31T07:00:35.273Z)
Latitude
-0°
Longitude
-170.63998°
Altitude
597.752 km
Speed
7.563 km/s
True Right ascension
22h 17m 22s
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
09:32:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.455 km
Perigee altitude
593.402 km
Semi-major axis
6,977.066 km
Eccentricity
0.00079
Inclination
49.9952°
RAAN
334.3456°
Arg. of periapsis
280.0614°
True anomaly
80.03269°
Mean anomaly
79.9433°
Eccentric anomaly
79.98799°
Mean motion
3.72421 °/min
Orbital period
96.66 mins
BSTAR
0.00045227
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Other satellites on launch #23 in the year 2024 (2024-02-02 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GEESAT 2-10 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 04:05:49.082Z | 186.422° SSW | 2025-11-01 04:08:49.082Z | 131.015° SE | 25.484° | 2025-11-01 04:11:49.082Z | 80.153° E |
| 6 mins | 2025-11-01 05:46:49.082Z | 260.355° W | 2025-11-01 05:49:49.082Z | 353.37° N | 38.66° | 2025-11-01 05:52:49.082Z | 46.4° ENE |
| 5 mins | 2025-11-01 07:28:49.082Z | 310.117° NW | 2025-11-01 07:30:49.082Z | 345.239° N | 21.807° | 2025-11-01 07:33:49.082Z | 37.33° NE |
| 5 mins | 2025-11-01 09:10:49.082Z | 329.531° NNW | 2025-11-01 09:12:49.082Z | 5.745° NNE | 23.025° | 2025-11-01 09:15:49.082Z | 59.86° ENE |
| 7 mins | 2025-11-01 10:51:49.082Z | 312.019° NW | 2025-11-01 10:54:49.082Z | 49.609° ENE | 42.645° | 2025-11-01 10:58:49.082Z | 114.779° SE |
| 4 mins | 2025-11-01 12:33:49.082Z | 254.737° W | 2025-11-01 12:34:49.082Z | 236.432° WSW | 20.361° | 2025-11-01 12:37:49.082Z | 185.051° 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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