OBJECT A, 57580 (Decayed)
Orbit data source: Space-Track
OBJECT A, 57580 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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57580 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 + 2 Pan, 0.5 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT A
1 57580U 23117A 25144.16779012 .11637947 25637-5 58038-3 0 9991
2 57580 97.4144 232.7843 0015917 264.3863 95.5622 16.41111729 99921Epoch: 2025-05-24T04:01Z
TLE epoch observation values (Epoch: 2025-05-24T04:01:37.066Z)
Latitude
0°
Longitude
-69.63267°
Altitude
167.125 km
Speed
7.805 km/s
True Right ascension
15h 31m 08s
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
21:26:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
170.06 km
Perigee altitude
149.247 km
Semi-major axis
6,537.791 km
Eccentricity
0.00159
Inclination
97.4144°
RAAN
232.7843°
Arg. of periapsis
264.3863°
True anomaly
95.7437°
Mean anomaly
95.5622°
Eccentric anomaly
95.65295°
Mean motion
4.10579 °/min
Orbital period
87.68 mins
BSTAR
0.00058038
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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 A 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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