OBJECT R, 51839 (Decayed)
Orbit data source: Space-Track
OBJECT R, 51839 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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51839 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 OBJECT R
1 51839U 22019R 26157.35070802 .08475770 25153-5 75233-3 0 9998
2 51839 97.3544 255.4419 0013577 264.5878 95.3872 16.38904555238411Epoch: 2026-06-06T08:25Z
TLE epoch observation values (Epoch: 2026-06-06T08:25:01.172Z)
Latitude
-0.00007°
Longitude
-125.5805°
Altitude
172.816 km
Speed
7.802 km/s
True Right ascension
17h 01m 46s
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
21:57:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
174.409 km
Perigee altitude
156.641 km
Semi-major axis
6,543.662 km
Eccentricity
0.00136
Inclination
97.3544°
RAAN
255.4419°
Arg. of periapsis
264.5878°
True anomaly
95.54207°
Mean anomaly
95.3872°
Eccentric anomaly
95.46464°
Mean motion
4.10026 °/min
Orbital period
87.8 mins
BSTAR
0.00075233
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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 R 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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