DECAYED

OBJECT L, 56856 (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 L, 56856 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
56856, 2023-081L
Orbit
Decayed
Country
Flag of TBDTBD
Related business
Manufacturer
SECM?
Mission
Decayed Commercial Technology
Bus & Motor
Unknown
Mass
~80 kg wet, ~80 kg dry
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 L
1 56856U 23081L   25249.72267904  .18357823  25143-5  32851-3 0  9992
2 56856  97.2981 333.8676 0017366 262.2846  97.6485 16.46283875126106
Epoch: 2025-09-06T17:20Z
TLE epoch observation values (Epoch: 2025-09-06T17:20:39.469Z)
Latitude
-0.00001°
Longitude
87.65072°
Altitude
153.931 km
Speed
7.813 km/s
True Right ascension
22h 15m 28s
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
22:37:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
157.264 km
Perigee altitude
134.605 km
Semi-major axis
6,524.072 km
Eccentricity
0.00174
Inclination
97.2981°
RAAN
333.8676°
Arg. of periapsis
262.2846°
True anomaly
97.84567°
Mean anomaly
97.6485°
Eccentric anomaly
97.74709°
Mean motion
4.11875 °/min
Orbital period
87.41 mins
BSTAR
0.00032851
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|