GEESAT 2-03, 58907
Orbit data source: Space-Track
GEESAT 2-03, 58907 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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58907 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 GEESAT 2-03
1 58907U 24023C 26171.38392579 .00001744 00000-0 17130-3 0 9994
2 58907 50.0027 309.1363 0005839 48.6385 311.5060 14.97102096129804Epoch: 2026-06-20T09:12Z
TLE epoch observation values (Epoch: 2026-06-20T09:12:51.188Z)
Latitude
-0.00004°
Longitude
-97.67635°
Altitude
573.714 km
Speed
7.577 km/s
True Right ascension
20h 36m 32s
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
00:50:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.679 km
Perigee altitude
572.557 km
Semi-major axis
6,954.755 km
Eccentricity
0.00058
Inclination
50.0027°
RAAN
309.1363°
Arg. of periapsis
48.6385°
True anomaly
311.45587°
Mean anomaly
311.506°
Eccentric anomaly
311.48094°
Mean motion
3.74214 °/min
Orbital period
96.2 mins
BSTAR
0.0001713
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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 2-03 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 | 2026-06-22 14:24:24.162Z | 307.271° NW | 2026-06-22 14:27:24.162Z | 355.691° N | 19.914° | 2026-06-22 14:30:24.162Z | 43.367° NE |
| 6 mins | 2026-06-22 16:06:24.162Z | 328.542° NNW | 2026-06-22 16:08:24.162Z | 5.356° NNE | 24.019° | 2026-06-22 16:12:24.162Z | 74.448° E |
| 6 mins | 2026-06-22 17:47:24.162Z | 305.111° NW | 2026-06-22 17:49:24.162Z | 311.393° NW | 44.323° | 2026-06-22 17:53:24.162Z | 124.71° SE |
| 7 mins | 2026-06-23 11:05:24.162Z | 219.036° SW | 2026-06-23 11:08:24.162Z | 142.642° SSE | 41.733° | 2026-06-23 11:12:24.162Z | 61.441° ENE |
| 6 mins | 2026-06-23 12:46:24.162Z | 284.564° WNW | 2026-06-23 12:49:24.162Z | 349.285° N | 27.706° | 2026-06-23 12:52:24.162Z | 40.637° 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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