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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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 2-03
1 58907U 24023C 25304.27175150 .00003863 00000-0 36585-3 0 9992
2 58907 50.0015 326.5121 0006313 221.9247 138.1213 14.95636114 95049Epoch: 2025-10-31T06:31Z
TLE epoch observation values (Epoch: 2025-10-31T06:31:19.329Z)
Latitude
-0.00007°
Longitude
-171.13707°
Altitude
584.218 km
Speed
7.568 km/s
True Right ascension
21h 46m 02s
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
09:45:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.555 km
Perigee altitude
576.768 km
Semi-major axis
6,959.298 km
Eccentricity
0.00063
Inclination
50.0015°
RAAN
326.5121°
Arg. of periapsis
221.9247°
True anomaly
138.16956°
Mean anomaly
138.1213°
Eccentric anomaly
138.14543°
Mean motion
3.73848 °/min
Orbital period
96.3 mins
BSTAR
0.00036585
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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 | 2025-11-01 03:31:37.261Z | 184.758° SSW | 2025-11-01 03:34:37.261Z | 130.529° SE | 23.989° | 2025-11-01 03:37:37.261Z | 80.778° E |
| 7 mins | 2025-11-01 05:11:37.261Z | 254.94° W | 2025-11-01 05:14:37.261Z | 318.774° NNW | 39.812° | 2025-11-01 05:18:37.261Z | 48.828° ENE |
| 5 mins | 2025-11-01 06:53:37.261Z | 307.307° NW | 2025-11-01 06:55:37.261Z | 341.624° N | 21.339° | 2025-11-01 06:58:37.261Z | 35.598° NE |
| 5 mins | 2025-11-01 08:35:37.261Z | 332.904° NNW | 2025-11-01 08:37:37.261Z | 11.351° NNE | 22.133° | 2025-11-01 08:40:37.261Z | 61.615° ENE |
| 7 mins | 2025-11-01 10:15:37.261Z | 312.033° NW | 2025-11-01 10:18:37.261Z | 17.658° NNE | 41.553° | 2025-11-01 10:22:37.261Z | 111.586° ESE |
| 4 mins | 2025-11-01 11:57:37.261Z | 255.358° W | 2025-11-01 11:58:37.261Z | 235.865° WSW | 21.246° | 2025-11-01 12:01:37.261Z | 181.984° 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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