OBJECT Q, 51838 (Decayed)
Orbit data source: Space-Track
OBJECT Q, 51838 was a satellite owned by Changguang WJ (CN) in LEO that was launched on Sun, 27 Feb 2022 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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51838 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 OBJECT Q
1 51838U 22019Q 25236.02825369 .13047705 25966-5 13718-3 0 9995
2 51838 97.3860 330.4152 0015287 261.9658 97.9912 16.49906820194576Epoch: 2025-08-24T00:40Z
TLE epoch observation values (Epoch: 2025-08-24T00:40:41.118Z)
Latitude
-0.00007°
Longitude
-12.31066°
Altitude
144.246 km
Speed
7.819 km/s
True Right ascension
22h 01m 39s
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
18:09:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
146.334 km
Perigee altitude
126.416 km
Semi-major axis
6,514.512 km
Eccentricity
0.00153
Inclination
97.386°
RAAN
330.4152°
Arg. of periapsis
261.9658°
True anomaly
98.16463°
Mean anomaly
97.9912°
Eccentric anomaly
98.07792°
Mean motion
4.12782 °/min
Orbital period
87.21 mins
BSTAR
0.00013718
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Other satellites on launch #19 in the year 2022 (2022-02-27 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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