DECAYED

OBJECT C, 54684 (Decayed)

Orbit data source: Space-Track

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

OBJECT C, 54684 was a satellite owned by CAMSAT (CN) in LEO that was launched on Fri, 09 Dec 2022 UTC via a JIELONG-3 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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
54684, 2022-167C
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
CAMSAT
Mission
Decayed Amateur Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2022-12-09 (4 years ago)
Launch vehicle
JIELONG-3
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.105 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year ago
0 OBJECT C
1 54684U 22167C   25064.68183564  .08547514  26414-5  93170-3 0  9992
2 54684  97.5856 230.7463 0011725 277.2083  82.7881 16.37185507124845
Epoch: 2025-03-05T16:21Z
TLE epoch observation values (Epoch: 2025-03-05T16:21:50.599Z)
Latitude
-0.00004°
Longitude
-178.38193°
Altitude
175.586 km
Speed
7.801 km/s
True Right ascension
15h 22m 59s
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
21:28:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
177.798 km
Perigee altitude
162.442 km
Semi-major axis
6,548.257 km
Eccentricity
0.00117
Inclination
97.5856°
RAAN
230.7463°
Arg. of periapsis
277.2083°
True anomaly
82.92142°
Mean anomaly
82.7881°
Eccentric anomaly
82.85476°
Mean motion
4.09595 °/min
Orbital period
87.89 mins
BSTAR
0.0009317
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