OBJECT P, 51837 (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 P, 51837 was a Chinese satellite 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.
51837 intel report (Beta)
OBJECT P details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 2 months ago |
| Origin | |
| Manufacturer | Changsha Tianyi |
| Mission | Decayed Commercial Science |
| Bus & Motor | CUBESAT 6U?, Unknown motor |
| Mass | 14 kg wet, 14 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box + 2 Pan, 1 m |
| Radar Cross Section | 0.126 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 2 months ago
0 OBJECT P
1 51837U 22019P 24251.77527469 .18198306 25886-5 20618-3 0 9999
2 51837 97.3859 338.7352 0011792 272.7734 87.2220 16.49764729140900Definitive object data (Epoch: 2024-09-07T18:36:23.733Z)
| Latitude | -0.00009° |
| Longitude | 72.3077° |
| Altitude | 142.856 km |
| Speed | 7.821 km/s |
| True Right ascension | 22h 34m 56s |
| 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 | 144.432 km |
| Perigee | 129.067 km |
| Semi-major axis | 6,514.886 km |
| Eccentricity | 0.0011792 |
| Inclination | 97.3859° |
| RAAN | 338.7352° |
| Arg. of periapsis | 272.7734° |
| True anomaly | 87.35698° |
| Mean anomaly | 87.222° |
| Eccentric anomaly | 87.28949° |
| Mean motion | 4.12746 °/min |
| BSTAR | 0.00020618 |
| Period | 87.22 mins |
Other satellites on launch #19 in the year 2022 (2022-02-27 UTC)
OBJECT P 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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