DECAYED

OBJECT N, 56858 (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 N, 56858 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
56858, 2023-081N
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 N
1 56858U 23081N   25248.44781801  .11030718  24772-5  10008-2 0  9999
2 56858  97.2967 333.1874 0015267 265.3477  94.6078 16.38614757125941
Epoch: 2025-09-05T10:44Z
TLE epoch observation values (Epoch: 2025-09-05T10:44:51.476Z)
Latitude
-0.00003°
Longitude
-172.82294°
Altitude
173.561 km
Speed
7.802 km/s
True Right ascension
22h 12m 44s
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
23:27:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
176.286 km
Perigee altitude
156.303 km
Semi-major axis
6,544.432 km
Eccentricity
0.00153
Inclination
97.2967°
RAAN
333.1874°
Arg. of periapsis
265.3477°
True anomaly
94.78215°
Mean anomaly
94.6078°
Eccentric anomaly
94.69498°
Mean motion
4.09954 °/min
Orbital period
87.81 mins
BSTAR
0.0010008
Loading maneuver chart data...
Computing Atmospheric mass density...

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