GEESAT 2-09, 58913
Orbit data source: Space-Track
GEESAT 2-09, 58913 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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58913 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: 10 hours ago
TLE from 10 hours ago
0 GEESAT 2-09
1 58913U 24023J 25303.90467075 .00004626 00000-0 49867-3 0 9993
2 58913 50.0042 336.1471 0016389 281.5950 78.3151 14.89931012 94883Epoch: 2025-10-30T21:42Z
TLE epoch observation values (Epoch: 2025-10-30T21:42:43.552Z)
Latitude
-0.00005°
Longitude
-28.99117°
Altitude
596.4 km
Speed
7.564 km/s
True Right ascension
22h 24m 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
02:55:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
610.345 km
Perigee altitude
587.476 km
Semi-major axis
6,977.048 km
Eccentricity
0.00164
Inclination
50.0042°
RAAN
336.1471°
Arg. of periapsis
281.595°
True anomaly
78.49909°
Mean anomaly
78.3151°
Eccentric anomaly
78.40709°
Mean motion
3.72422 °/min
Orbital period
96.66 mins
BSTAR
0.00049867
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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 2-09 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 | 2025-10-31 07:40:08.759Z | 295.583° NW | 2025-10-31 07:43:08.759Z | 340.971° N | 22.611° | 2025-10-31 07:47:08.759Z | 44.591° NE |
| 6 mins | 2025-10-31 09:23:08.759Z | 327.354° NNW | 2025-10-31 09:25:08.759Z | 1.708° NNE | 22.22° | 2025-10-31 09:29:08.759Z | 65.046° ENE |
| 7 mins | 2025-10-31 11:04:08.759Z | 314.284° NW | 2025-10-31 11:07:08.759Z | 29.157° NE | 40.723° | 2025-10-31 11:11:08.759Z | 109.064° ESE |
| 5 mins | 2025-10-31 12:46:08.759Z | 261.475° W | 2025-10-31 12:48:08.759Z | 219.737° SW | 23.859° | 2025-10-31 12:51:08.759Z | 172.75° S |
| 7 mins | 2025-11-01 04:28:08.759Z | 202.231° SSW | 2025-11-01 04:31:08.759Z | 137.664° SSE | 34.134° | 2025-11-01 04:35:08.759Z | 67.889° E |
| 7 mins | 2025-11-01 06:09:08.759Z | 271.103° WNW | 2025-11-01 06:12:08.759Z | 336.613° NNW | 33.778° | 2025-11-01 06:16:08.759Z | 46.272° ENE |
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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