GEESAT 2-01, 58905
Orbit data source: Space-Track
GEESAT 2-01, 58905 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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58905 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 2-01
1 58905U 24023A 25304.29924409 .00004187 00000-0 45436-3 0 9996
2 58905 49.9954 334.3988 0008149 289.4991 70.5069 14.89934945 94939Epoch: 2025-10-31T07:10Z
TLE epoch observation values (Epoch: 2025-10-31T07:10:54.689Z)
Latitude
-0.00004°
Longitude
-173.17478°
Altitude
596.791 km
Speed
7.564 km/s
True Right ascension
22h 17m 35s
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
09:32:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.585 km
Perigee altitude
593.214 km
Semi-major axis
6,977.037 km
Eccentricity
0.00081
Inclination
49.9954°
RAAN
334.3988°
Arg. of periapsis
289.4991°
True anomaly
70.59496°
Mean anomaly
70.5069°
Eccentric anomaly
70.55093°
Mean motion
3.72423 °/min
Orbital period
96.66 mins
BSTAR
0.00045436
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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 2-01 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 | 2025-11-01 04:15:50.076Z | 198.298° SSW | 2025-11-01 04:19:50.076Z | 122.4° SE | 28.772° | 2025-11-01 04:22:50.076Z | 74.568° E |
| 6 mins | 2025-11-01 05:57:50.076Z | 269.041° W | 2025-11-01 05:59:50.076Z | 314.662° NW | 36.04° | 2025-11-01 06:03:50.076Z | 45.588° ENE |
| 5 mins | 2025-11-01 07:39:50.076Z | 315.015° NNW | 2025-11-01 07:41:50.076Z | 350.657° N | 21.253° | 2025-11-01 07:44:50.076Z | 40.274° NE |
| 5 mins | 2025-11-01 09:21:50.076Z | 332.363° NNW | 2025-11-01 09:23:50.076Z | 11.367° NNE | 24.251° | 2025-11-01 09:26:50.076Z | 65.106° ENE |
| 6 mins | 2025-11-01 11:02:50.076Z | 308.633° NW | 2025-11-01 11:05:50.076Z | 91.869° ESE | 43.232° | 2025-11-01 11:08:50.076Z | 119.555° SE |
| 4 mins | 2025-11-01 12:44:50.076Z | 247.903° W | 2025-11-01 12:45:50.076Z | 230.712° WSW | 17.488° | 2025-11-01 12:48:50.076Z | 186.689° 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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