OBJECT E, 44842 (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 E, 44842 was a satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Sat, 07 Dec 2019 UTC via a KUAIZHOU-1A launch vehicle from the Taiyaun Space Center, China (TSC). 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.
44842 intel report (Beta)
OBJECT E details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 9 months ago |
| Origin | |
| Manufacturer | GUOG? |
| Mission | Decayed Commercial Imaging |
| Bus & Motor | CUBESAT 6U?, Unknown motor |
| Mass | 8 kg wet, 8 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, 0.3 m |
| Radar Cross Section | 0.080 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 9 months ago
0 OBJECT E
1 44842U 19087E 24091.02873833 .07848714 25368-5 16623-2 0 9995
2 44842 97.4763 279.3477 0007439 271.5628 88.4815 16.30832210241101Definitive object data (Epoch: 2024-03-31T00:41:22.991Z)
| Latitude | 0.00004° |
| Longitude | 80.11268° |
| Altitude | 193.415 km |
| Speed | 7.79 km/s |
| True Right ascension | 18h 37m 23s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight 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 | 192.011 km |
| Perigee altitude | 182.243 km |
| Semi-major axis | 6,565.264 km |
| Eccentricity | 0.0007439 |
| Inclination | 97.4763° |
| RAAN | 279.3477° |
| Arg. of periapsis | 271.5628° |
| True anomaly | 88.56672° |
| Mean anomaly | 88.4815° |
| Eccentric anomaly | 88.52411° |
| Mean motion | 4.08004 °/min |
| BSTAR | 0.0016623 |
| Orbital period | 88.23 mins |
Other satellites on launch #87 in the year 2019 (2019-12-07 UTC)
| OBJECT A, 44838 (Decayed) |
| OBJECT B, 44839 (Decayed) |
| OBJECT C, 44840 (Decayed) |
| OBJECT D, 44841 (Decayed) |
| OBJECT E, 44842 (Decayed) |
| OBJECT F, 44843 (Decayed) |
| KZ-1A R/B, 44844 (Decayed) |
OBJECT E 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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