DECAYED

OBJECT F, 56851 (Decayed)

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

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.

Not visible in the next 10 days
Identifier
56851, 2023-081F
Orbit
Decayed
Country
Flag of TBDTBD
Related business
None
Manufacturer
Unknown
Mission
Decayed Defense Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2023-06-07 (3 years ago)
Launch vehicle
LIJIAN-1
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Unknown
Shape & HBR
Box + 4 Pan, 4.0 m
Radar Cross Section
8.634 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last 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 16.41298238125991
Epoch: 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
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
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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Computing Atmospheric mass density...

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