OBJECT M, 51835 (Decayed)
Orbit data source: Space-Track
OBJECT M, 51835 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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51835 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 OBJECT M
1 51835U 22019M 26120.80150797 .14453301 25711-5 16849-3 0 9997
2 51835 97.3515 218.7383 0014909 270.1758 89.7838 16.49258376232763Epoch: 2026-04-30T19:14Z
TLE epoch observation values (Epoch: 2026-04-30T19:14:10.288Z)
Latitude
-0.00003°
Longitude
71.45254°
Altitude
144.532 km
Speed
7.819 km/s
True Right ascension
14h 34m 57s
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
21:52:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
147.798 km
Perigee altitude
128.368 km
Semi-major axis
6,516.22 km
Eccentricity
0.00149
Inclination
97.3515°
RAAN
218.7383°
Arg. of periapsis
270.1758°
True anomaly
89.95464°
Mean anomaly
89.7838°
Eccentric anomaly
89.86922°
Mean motion
4.12619 °/min
Orbital period
87.25 mins
BSTAR
0.00016849
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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 M 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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