OBJECT AJ, 47445 (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 AJ, 47445 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.
47445 intel report (Beta)
OBJECT AJ radio frequencies
OBJECT AJ details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 6 days ago |
| Origin | |
| Manufacturer | TU Dresden |
| Mission | Decayed Amateur Science |
| Bus & Motor | CUBESAT 2U, Unknown motor |
| Mass | 2 kg wet, 2 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, Unknown HBR |
| Radar Cross Section | 0.025 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 6 days ago
0 OBJECT AJ
1 47445U 21006AJ 24320.07680123 .17272437 25045-5 27578-3 0 9997
2 47445 97.2621 23.7910 0008960 269.2652 90.7625 16.47927372212215Definitive object data (Epoch: 2024-11-15T01:50:35.626Z)
| Latitude | -0.00005° |
| Longitude | -58.50728° |
| Altitude | 148.148 km |
| Speed | 7.817 km/s |
| True Right ascension | 01h 35m 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 | 147.432 km |
| Perigee altitude | 135.749 km |
| Semi-major axis | 6,519.727 km |
| Eccentricity | 0.000896 |
| Inclination | 97.2621° |
| RAAN | 23.791° |
| Arg. of periapsis | 269.2652° |
| True anomaly | 90.86516° |
| Mean anomaly | 90.7625° |
| Eccentric anomaly | 90.81383° |
| Mean motion | 4.12286 °/min |
| BSTAR | 0.00027578 |
| Orbital period | 87.32 mins |
Other satellites on launch #6 in the year 2021 (2021-01-24 UTC)
OBJECT AJ 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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