OBJECT Q, 54751 (Decayed)
Orbit data source: Space-Track
OBJECT Q, 54751 was a satellite owned by Changguang WJ (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.
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54751 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changguang WJ
Mission
Decayed Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
42 kg wet, 42 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
2.000 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT Q
1 54751U 22167Q 25150.43247673 .07419421 26595-5 85623-3 0 9996
2 54751 97.6074 320.3733 0014247 256.9785 102.9922 16.36535842137737Epoch: 2025-05-30T10:22Z
TLE epoch observation values (Epoch: 2025-05-30T10:22:45.989Z)
Latitude
0.00002°
Longitude
-83.50562°
Altitude
180.386 km
Speed
7.797 km/s
True Right ascension
21h 21m 29s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:23:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
181.187 km
Perigee altitude
162.524 km
Semi-major axis
6,549.992 km
Eccentricity
0.00142
Inclination
97.6074°
RAAN
320.3733°
Arg. of periapsis
256.9785°
True anomaly
103.15122°
Mean anomaly
102.9922°
Eccentric anomaly
103.07171°
Mean motion
4.09432 °/min
Orbital period
87.93 mins
BSTAR
0.00085623
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Other satellites on launch #167 in the year 2022 (2022-12-09 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT Q Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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