OBJECT F, 56851 (Decayed)
Orbit data source: Space-Track
OBJECT F, 56851 was a satellite in LEO that was launched on Wed, 07 Jun 2023 UTC via a LIJIAN-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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56851 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 OBJECT F
1 56851U 23081F 25249.27595955 .11320601 24892-5 55548-3 0 9992
2 56851 97.2923 332.7309 0015169 262.4727 97.4850 16.41298238125991Epoch: 2025-09-06T06:37Z
TLE epoch observation values (Epoch: 2025-09-06T06:37:22.905Z)
Latitude
-0.00002°
Longitude
-112.22665°
Altitude
166.915 km
Speed
7.805 km/s
True Right ascension
22h 10m 55s
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
23:30:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
169.069 km
Perigee altitude
149.236 km
Semi-major axis
6,537.289 km
Eccentricity
0.00152
Inclination
97.2923°
RAAN
332.7309°
Arg. of periapsis
262.4727°
True anomaly
97.6573°
Mean anomaly
97.485°
Eccentric anomaly
97.57115°
Mean motion
4.10626 °/min
Orbital period
87.67 mins
BSTAR
0.00055548
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Other satellites on launch #81 in the year 2023 (2023-06-07 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 F 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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