OBJECT AE, 47441 (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 AE, 47441 was a satellite in LEO that was launched on Sun, 24 Jan 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.
47441 intel report (Beta)
OBJECT AE radio frequencies
OBJECT AE details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 6 months ago |
| Origin | |
| Manufacturer | ITUTR/ASELSN |
| Mission | Decayed Commercial Technology |
| Bus & Motor | CUBESAT 3U, Unknown motor |
| Mass | 4 kg wet, 4 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box + 2 Pan, 0.3 m |
| Radar Cross Section | 0.035 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 6 months ago
0 OBJECT AE
1 47441U 21006AE 24163.33992307 .16627094 24252-5 23736-3 0 9990
2 47441 97.2877 230.5397 0019040 190.9473 169.1419 16.47470004188335Definitive object data (Epoch: 2024-06-11T08:09:29.353Z)
| Latitude | -0.00003° |
| Longitude | -151.99515° |
| Altitude | 161.474 km |
| Speed | 7.802 km/s |
| True Right ascension | 15h 22m 09s |
| 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 | 155.215 km |
| Perigee altitude | 130.383 km |
| Semi-major axis | 6,520.936 km |
| Eccentricity | 0.001904 |
| Inclination | 97.2877° |
| RAAN | 230.5397° |
| Arg. of periapsis | 190.9473° |
| True anomaly | 169.1829° |
| Mean anomaly | 169.1419° |
| Eccentric anomaly | 169.16241° |
| Mean motion | 4.12172 °/min |
| BSTAR | 0.00023736 |
| Orbital period | 87.34 mins |
Other satellites on launch #6 in the year 2021 (2021-01-24 UTC)
OBJECT AE 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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