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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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 2-06
1 58910U 24023F 26171.43385260 .00004230 00000-0 31981-3 0 9996
2 58910 49.9884 284.1542 0005453 67.5296 292.6228 15.04221165130131Epoch: 2026-06-20T10:24Z
TLE epoch observation values (Epoch: 2026-06-20T10:24:44.864Z)
Latitude
-0.00001°
Longitude
-140.68128°
Altitude
552.993 km
Speed
7.587 km/s
True Right ascension
18h 56m 37s
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
23:18:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.445 km
Perigee altitude
550.884 km
Semi-major axis
6,932.802 km
Eccentricity
0.00055
Inclination
49.9884°
RAAN
284.1542°
Arg. of periapsis
67.5296°
True anomaly
292.56511°
Mean anomaly
292.6228°
Eccentric anomaly
292.59395°
Mean motion
3.75993 °/min
Orbital period
95.75 mins
BSTAR
0.00031981
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 13:49:24.119Z | 326.077° NNW | 2026-06-22 13:51:24.119Z | 0.433° NNE | 19.74° | 2026-06-22 13:54:24.119Z | 53.321° ENE |
| 6 mins | 2026-06-22 15:30:24.119Z | 325.547° NNW | 2026-06-22 15:32:24.119Z | 27.032° NE | 36.836° | 2026-06-22 15:36:24.119Z | 103.423° ESE |
| 5 mins | 2026-06-22 17:10:24.119Z | 267.292° W | 2026-06-22 17:12:24.119Z | 219.254° SW | 26.607° | 2026-06-22 17:15:24.119Z | 166.012° S |
| 5 mins | 2026-06-23 08:44:24.119Z | 175.194° S | 2026-06-23 08:46:24.119Z | 130.913° SE | 24.364° | 2026-06-23 08:49:24.119Z | 79.416° E |
| 6 mins | 2026-06-23 10:23:24.119Z | 260.392° W | 2026-06-23 10:26:24.119Z | 353.914° N | 37.633° | 2026-06-23 10:29:24.119Z | 46.596° ENE |
| 4 mins | 2026-06-23 12:05:24.119Z | 325.578° NNW | 2026-06-23 12:06:24.119Z | 345.827° N | 20.232° | 2026-06-23 12:09:24.119Z | 38.053° NE |
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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