OBJECT G, 51830 (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 G, 51830 was a satellite owned by Guodian Gaokeji (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.
51830 intel report (Beta)
OBJECT G details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 2 months ago |
| Origin | |
| Manufacturer | Shanghai ASES |
| Mission | Decayed Commercial Communications |
| Bus & Motor | STARLIGHTB, Unknown motor |
| Mass | 39 kg wet, 39 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, 0.5 m |
| Radar Cross Section | 0.195 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 2 months ago
0 OBJECT G
1 51830U 22019G 24257.48177505 .14461052 25176-5 17193-2 0 9990
2 51830 97.3866 343.0159 0014166 275.8825 84.0858 16.36270832141678Definitive object data (Epoch: 2024-09-13T11:33:45.364Z)
| Latitude | 0.00003° |
| Longitude | 176.62366° |
| Altitude | 178.044 km |
| Speed | 7.8 km/s |
| True Right ascension | 22h 52m 03s |
| 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 | 181.833 km |
| Perigee | 163.274 km |
| Semi-major axis | 6,550.69 km |
| Eccentricity | 0.0014166 |
| Inclination | 97.3866° |
| RAAN | 343.0159° |
| Arg. of periapsis | 275.8825° |
| True anomaly | 84.2473° |
| Mean anomaly | 84.0858° |
| Eccentric anomaly | 84.16654° |
| Mean motion | 4.09367 °/min |
| BSTAR | 0.0017193 |
| Period | 87.94 mins |
Other satellites on launch #19 in the year 2022 (2022-02-27 UTC)
OBJECT G 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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