OBJECT F, 51829 (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 F, 51829 was a satellite owned by Weina (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.
51829 intel report (Beta)
OBJECT F details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 2 months ago |
| Origin | |
| Manufacturer | Weina |
| Mission | Decayed Commercial Imaging |
| Bus & Motor | MN200, Unknown motor |
| Mass | 240 kg wet, 240 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box + Cyl + 2 Pan, 5 m |
| Radar Cross Section | 2.585 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 2 months ago
0 OBJECT F
1 51829U 22019F 24257.89891422 .17016459 26093-5 24644-3 0 9993
2 51829 97.3972 344.8493 0011072 260.7498 99.2554 16.48290570141761Definitive object data (Epoch: 2024-09-13T21:34:26.188Z)
| Latitude | -0° |
| Longitude | 27.87581° |
| Altitude | 148.273 km |
| Speed | 7.816 km/s |
| True Right ascension | 22h 59m 23s |
| 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 | 147.855 km |
| Perigee | 133.42 km |
| Semi-major axis | 6,518.775 km |
| Eccentricity | 0.0011072 |
| Inclination | 97.3972° |
| RAAN | 344.8493° |
| Arg. of periapsis | 260.7498° |
| True anomaly | 99.3806° |
| Mean anomaly | 99.2554° |
| Eccentric anomaly | 99.318° |
| Mean motion | 4.12377 °/min |
| BSTAR | 0.00024644 |
| Period | 87.3 mins |
Other satellites on launch #19 in the year 2022 (2022-02-27 UTC)
OBJECT F 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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