OBJECT N, 51836 (Decayed)
Orbit data source: Space-Track
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT N, 51836 was a satellite owned by Wuhan daxue (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.
51836 intel report (Beta)
OBJECT N details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 3 months ago |
| Origin | |
| Manufacturer | Wuhan daxue |
| Mission | Decayed Commercial Imaging |
| Bus & Motor | QMX, Unknown motor |
| Mass | 19.2 kg wet, 19.2 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box + 1 Pan, 0.9 m |
| Radar Cross Section | 0.207 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 3 months ago
0 OBJECT N
1 51836U 22019N 24304.75401821 .18937816 25286-5 63928-3 0 9990
2 51836 97.4016 33.5379 0011429 290.3678 69.6395 16.43601568149073Definitive object data (Epoch: 2024-10-30T18:05:47.173Z)
| Latitude | -0.00003° |
| Longitude | 82.54437° |
| Altitude | 156.904 km |
| Speed | 7.814 km/s |
| True Right ascension | 02h 14m 09s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee altitude | 160.507 km |
| Perigee altitude | 145.578 km |
| Semi-major axis | 6,531.179 km |
| Eccentricity | 0.0011429 |
| Inclination | 97.4016° |
| RAAN | 33.5379° |
| Arg. of periapsis | 290.3678° |
| True anomaly | 69.76235° |
| Mean anomaly | 69.6395° |
| Eccentric anomaly | 69.70092° |
| Mean motion | 4.11203 °/min |
| BSTAR | 0.00063928 |
| Orbital period | 87.55 mins |
Other satellites on launch #19 in the year 2022 (2022-02-27 UTC)
OBJECT N Visibility forecast
Observer location: undefined°, undefined
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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