OBJECT AL, 58290 (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 AL, 58290 was a satellite in LEO that was launched on Sat, 11 Nov 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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.
58290 intel report (Beta)
OBJECT AL radio frequencies
OBJECT AL details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 6 months ago |
| Origin | |
| Manufacturer | Hello Space |
| Mission | Decayed Commercial Communications |
| Bus & Motor | POCKETQUBE 2P, Unknown motor |
| Mass | 0.5 kg wet, 0.5 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, 0.1 m |
| Radar Cross Section | 0.008 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 6 months ago
0 OBJECT AL
1 58290U 23174AL 24170.19749364 .08885996 24693-5 37822-2 0 9994
2 58290 97.4332 251.0314 0018195 262.7426 97.1795 16.22404648 34263Definitive object data (Epoch: 2024-06-18T04:44:23.45Z)
| Latitude | -0.0001° |
| Longitude | -86.98799° |
| Altitude | 217.779 km |
| Speed | 7.775 km/s |
| True Right ascension | 16h 44m 07s |
| 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 | 221.85 km |
| Perigee altitude | 197.876 km |
| Semi-major axis | 6,588 km |
| Eccentricity | 0.0018195 |
| Inclination | 97.4332° |
| RAAN | 251.0314° |
| Arg. of periapsis | 262.7426° |
| True anomaly | 97.38631° |
| Mean anomaly | 97.1795° |
| Eccentric anomaly | 97.28291° |
| Mean motion | 4.05894 °/min |
| BSTAR | 0.0037822 |
| Orbital period | 88.69 mins |
Other satellites on launch #174 in the year 2023 (2023-11-11 UTC)
OBJECT AL 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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