OBJECT AK, 58289 (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 AK, 58289 was a satellite in SSO 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.
58289 intel report (Beta)
OBJECT AK details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 7 months ago |
| Origin | |
| Manufacturer | Hello Space |
| Mission | Decayed Commercial Technology |
| 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 + 2 Pan, 0.3 m |
| Radar Cross Section | 0.080 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 7 months ago
0 OBJECT AK
1 58289U 23174AK 24167.15955496 .03326691 28310-1 45560-2 0 9990
2 58289 97.4314 247.4797 0022483 266.0159 93.8555 16.10939344 33764Definitive object data (Epoch: 2024-06-15T03:49:45.548Z)
| Latitude | -0° |
| Longitude | -73.88744° |
| Altitude | 248.514 km |
| Speed | 7.757 km/s |
| True Right ascension | 16h 29m 55s |
| 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 | 255.997 km |
| Perigee altitude | 226.232 km |
| Semi-major axis | 6,619.252 km |
| Eccentricity | 0.0022483 |
| Inclination | 97.4314° |
| RAAN | 247.4797° |
| Arg. of periapsis | 266.0159° |
| True anomaly | 94.1125° |
| Mean anomaly | 93.8555° |
| Eccentric anomaly | 93.98401° |
| Mean motion | 4.03023 °/min |
| BSTAR | 0.004556 |
| Orbital period | 89.32 mins |
Other satellites on launch #174 in the year 2023 (2023-11-11 UTC)
OBJECT AK 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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