OBJECT N, 43843 (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 N, 43843 was a satellite in LEO that was launched on Fri, 07 Dec 2018 UTC launched 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.
43843 intel report (Beta)
OBJECT N details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 7 months ago |
| Origin | |
| Manufacturer | CALT |
| Mission | Decayed spacecraft |
| Bus & Motor | Unknown |
| Mass | 1 kg wet, 1 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Cone, 0.2 m |
| Radar Cross Section | 0.025 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 7 months ago
0 OBJECT N
1 43843U 18102N 24140.97272243 .06998283 25122-5 16865-2 0 9991
2 43843 97.4385 238.5864 0016795 268.5926 91.3443 16.29064881302051Definitive object data (Epoch: 2024-05-19T23:20:43.217Z)
| Latitude | -0.00011° |
| Longitude | 10.28997° |
| Altitude | 198.567 km |
| Speed | 7.787 km/s |
| True Right ascension | 15h 54m 20s |
| 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 | 202.912 km |
| Perigee altitude | 180.843 km |
| Semi-major axis | 6,570.015 km |
| Eccentricity | 0.0016795 |
| Inclination | 97.4385° |
| RAAN | 238.5864° |
| Arg. of periapsis | 268.5926° |
| True anomaly | 91.53669° |
| Mean anomaly | 91.3443° |
| Eccentric anomaly | 91.4405° |
| Mean motion | 4.07562 °/min |
| BSTAR | 0.0016865 |
| Orbital period | 88.33 mins |
Other satellites on launch #102 in the year 2018 (2018-12-07 UTC)
OBJECT N 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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