OBJECT C, 44488 (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 C, 44488 was a satellite owned by Guoxing (CN) in LEO that was launched on Sat, 17 Aug 2019 UTC via a JIELONG-1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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.
44488 intel report (Beta)
OBJECT C details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 1 month ago |
| Origin | |
| Manufacturer | Weina |
| Mission | Decayed Commercial Technology |
| Bus & Motor | MN10, Unknown motor |
| Mass | ~20 kg wet, ~20 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box + 3 Pan, 1 m |
| Radar Cross Section | 0.225 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 1 month ago
0 OBJECT C
1 44488U 19052C 24319.98751478 .17349390 25414-5 44692-3 0 9998
2 44488 97.3701 40.4158 0010034 275.6713 84.3445 16.45152244290595Definitive object data (Epoch: 2024-11-14T23:42:01.276Z)
| Latitude | -0.00005° |
| Longitude | -9.65135° |
| Altitude | 154.752 km |
| Speed | 7.814 km/s |
| True Right ascension | 02h 41m 39s |
| 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 | 155.481 km |
| Perigee altitude | 142.383 km |
| Semi-major axis | 6,527.069 km |
| Eccentricity | 0.0010034 |
| Inclination | 97.3701° |
| RAAN | 40.4158° |
| Arg. of periapsis | 275.6713° |
| True anomaly | 84.45894° |
| Mean anomaly | 84.3445° |
| Eccentric anomaly | 84.40172° |
| Mean motion | 4.11591 °/min |
| BSTAR | 0.00044692 |
| Orbital period | 87.47 mins |
Other satellites on launch #52 in the year 2019 (2019-08-17 UTC)
| OBJECT A, 44486 |
| OBJECT B, 44487 |
| OBJECT C, 44488 (Decayed) |
OBJECT C 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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