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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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: 2 days ago
TLE from 2 days ago
0 GEESAT 2-10
1 58914U 24023K 26171.43575847 .00001152 00000-0 16686-3 0 9997
2 58914 49.9958 338.9407 0009640 10.2723 349.8410 14.83252436129392Epoch: 2026-06-20T10:27Z
TLE epoch observation values (Epoch: 2026-06-20T10:27:29.531Z)
Latitude
-0.00007°
Longitude
-86.58282°
Altitude
612.981 km
Speed
7.558 km/s
True Right ascension
22h 35m 45s
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
21:54:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.581 km
Perigee altitude
613.089 km
Semi-major axis
6,997.972 km
Eccentricity
0.00096
Inclination
49.9958°
RAAN
338.9407°
Arg. of periapsis
10.2723°
True anomaly
349.82149°
Mean anomaly
349.841°
Eccentric anomaly
349.83125°
Mean motion
3.70753 °/min
Orbital period
97.1 mins
BSTAR
0.00016686
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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 2-10 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 12:43:53.499Z | 195.239° SSW | 2026-06-22 12:47:53.499Z | 128.155° SE | 26.79° | 2026-06-22 12:50:53.499Z | 78.343° E |
| 7 mins | 2026-06-22 14:25:53.499Z | 260.07° W | 2026-06-22 14:28:53.499Z | 332.297° NNW | 38.732° | 2026-06-22 14:32:53.499Z | 48.356° ENE |
| 5 mins | 2026-06-22 16:08:53.499Z | 313.03° NW | 2026-06-22 16:10:53.499Z | 348.902° N | 22.009° | 2026-06-22 16:13:53.499Z | 39.135° NE |
| 6 mins | 2026-06-22 17:50:53.499Z | 325.857° NNW | 2026-06-22 17:53:53.499Z | 21.762° NNE | 23.776° | 2026-06-22 17:56:53.499Z | 67.589° E |
| 7 mins | 2026-06-22 19:32:53.499Z | 311.09° NW | 2026-06-22 19:35:53.499Z | 76.317° E | 42.736° | 2026-06-22 19:39:53.499Z | 117.684° SE |
| 4 mins | 2026-06-22 21:14:53.499Z | 256.768° W | 2026-06-22 21:16:53.499Z | 221.344° SW | 19.401° | 2026-06-22 21:18:53.499Z | 190.101° 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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