OBJECT G, 57586 (Decayed)
Orbit data source: Space-Track
OBJECT G, 57586 was a Chinese satellite in LEO that was launched on Thu, 10 Aug 2023 UTC via a GUSHENXING 1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.
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57586 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.8 m
Radar Cross Section
2.000 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT G
1 57586U 23117G 25068.52792475 .22481099 25699-5 72925-3 0 9996
2 57586 97.4197 156.6561 0012324 276.0424 205.4674 16.43680646 88319Epoch: 2025-03-09T12:40Z
TLE epoch observation values (Epoch: 2025-03-09T12:40:12.698Z)
Latitude
57.88315°
Longitude
-8.95116°
Altitude
173.134 km
Speed
7.804 km/s
True Right ascension
23h 14m 14s
True Declination
57° 42' 51"
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
23:08:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
160.882 km
Perigee altitude
144.785 km
Semi-major axis
6,530.97 km
Eccentricity
0.00123
Inclination
97.4197°
RAAN
156.6561°
Arg. of periapsis
276.0424°
True anomaly
205.40676°
Mean anomaly
205.4674°
Eccentric anomaly
205.43707°
Mean motion
4.11222 °/min
Orbital period
87.54 mins
BSTAR
0.00072925
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Other satellites on launch #117 in the year 2023 (2023-08-10 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.OBJECT G Visibility
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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. |
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| This satellite is decayed. |
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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