OBJECT F, 44843 (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, 44843 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.
44843 intel report (Beta)
OBJECT F details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 5 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 5 months ago
0 OBJECT F
1 44843U 19087F 24214.51925386 .07037054 25919-5 86399-3 0 9995
2 44843 97.5018 48.1624 0009226 264.5765 95.4480 16.36199226260085Definitive object data (Epoch: 2024-08-01T12:27:43.533Z)
| Latitude | 0° |
| Longitude | -89.37631° |
| Altitude | 179.756 km |
| Speed | 7.798 km/s |
| True Right ascension | 03h 12m 38s |
| 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 | 178.794 km |
| Perigee altitude | 166.706 km |
| Semi-major axis | 6,550.887 km |
| Eccentricity | 0.0009226 |
| Inclination | 97.5018° |
| RAAN | 48.1624° |
| Arg. of periapsis | 264.5765° |
| True anomaly | 95.55323° |
| Mean anomaly | 95.448° |
| Eccentric anomaly | 95.50062° |
| Mean motion | 4.09348 °/min |
| BSTAR | 0.00086399 |
| Orbital period | 87.94 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 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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