DECAYED

OBJECT K, 54691 (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 K, 54691 was a satellite owned by HEAD (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
54691, 2022-167K
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
IMI/CAS
Mission
Decayed Commercial Communications
Bus & Motor
WN100, Unknown motor
Mass
40 kg wet, 40 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 + 2 Pan, 1.0 m
Radar Cross Section
0.223 m², Medium (>0.1 m² and < 1m²)

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

TLE from 1 month ago
0 OBJECT K
1 54691U 22167K   26136.41992729  .12221728  26477-5  47460-3 0  9994
2 54691  97.5460 326.2890 0011677 276.4525  83.5446 16.42889174192115
Epoch: 2026-05-16T10:04Z
TLE epoch observation values (Epoch: 2026-05-16T10:04:41.717Z)
Latitude
-0.00003°
Longitude
-59.02197°
Altitude
160.529 km
Speed
7.81 km/s
True Right ascension
21h 45m 09s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
21:31:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.567 km
Perigee altitude
147.31 km
Semi-major axis
6,533.076 km
Eccentricity
0.00117
Inclination
97.546°
RAAN
326.289°
Arg. of periapsis
276.4525°
True anomaly
83.67758°
Mean anomaly
83.5446°
Eccentric anomaly
83.61109°
Mean motion
4.11023 °/min
Orbital period
87.59 mins
BSTAR
0.0004746
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
|