OBJECT H, 43838 (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 H, 43838 was a satellite in LEO that was launched on Fri, 07 Dec 2018 UTC via a CHANG ZHENG 2D 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.
43838 intel report (Beta)
OBJECT H details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 4 months ago |
| Origin | |
| Manufacturer | Jiutian |
| Mission | Decayed Commercial Communications |
| Bus & Motor | CUBESAT 6U, Unknown motor |
| Mass | 10 kg wet, 10 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, 0.3 m |
| Radar Cross Section | 0.035 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 4 months ago
0 OBJECT H
1 43838U 18102H 24254.67329662 .32543562 25275-5 73064-3 0 9995
2 43838 97.3060 341.5296 0014505 255.1041 242.6528 16.45339038319066Definitive object data (Epoch: 2024-09-10T16:09:32.827Z)
| Latitude | 42.06573° |
| Longitude | -64.43626° |
| Altitude | 162.323 km |
| Speed | 7.81 km/s |
| True Right ascension | 11h 12m 32s |
| True Declination | 41° 52' 45" |
| 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 | 157.902 km |
| Perigee altitude | 138.968 km |
| Semi-major axis | 6,526.572 km |
| Eccentricity | 0.0014505 |
| Inclination | 97.306° |
| RAAN | 341.5296° |
| Arg. of periapsis | 255.1041° |
| True anomaly | 242.50528° |
| Mean anomaly | 242.6528° |
| Eccentric anomaly | 242.57903° |
| Mean motion | 4.11638 °/min |
| BSTAR | 0.00073064 |
| Orbital period | 87.46 mins |
Other satellites on launch #102 in the year 2018 (2018-12-07 UTC)
OBJECT H 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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