OBJECT L, 43859 (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 L, 43859 was a satellite owned by NASA GRC (US) in LEO that was launched on Sun, 16 Dec 2018 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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.
43859 intel report (Beta)
OBJECT L details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 5 months ago |
| Origin | |
| Manufacturer | NASA GRC |
| Mission | Decayed Civil Technology |
| Bus & Motor | CUBESAT 3U, Unknown motor |
| Mass | 2.91 kg wet, 2.91 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box + 4 Pan, 0.6 m |
| Radar Cross Section | 0.066 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 5 months ago
0 OBJECT L
1 43859U 18104L 24194.91423858 .09173232 -15042-5 34830-3 0 9999
2 43859 84.9829 254.0101 0013879 258.4364 101.5385 16.42702273311208Definitive object data (Epoch: 2024-07-12T21:56:30.213Z)
| Latitude | 0° |
| Longitude | -6.39948° |
| Altitude | 163.766 km |
| Speed | 7.807 km/s |
| True Right ascension | 16h 56m 02s |
| 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 | 164.406 km |
| Perigee altitude | 146.27 km |
| Semi-major axis | 6,533.475 km |
| Eccentricity | 0.0013879 |
| Inclination | 84.9829° |
| RAAN | 254.0101° |
| Arg. of periapsis | 258.4364° |
| True anomaly | 101.69427° |
| Mean anomaly | 101.5385° |
| Eccentric anomaly | 101.61639° |
| Mean motion | 4.10986 °/min |
| BSTAR | 0.0003483 |
| Orbital period | 87.59 mins |
Other satellites on launch #104 in the year 2018 (2018-12-16 UTC)
OBJECT L 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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