OBJECT AG, 52424 (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 AG, 52424 was a satellite in LEO that was launched on Mon, 02 May 2022 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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.
52424 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 8 months ago |
| Origin | |
| Manufacturer | E-Space |
| 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 + 2 Pan, 1 m |
| Radar Cross Section | 0.126 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 8 months ago
0 OBJECT AG
1 52424U 22047AG 24206.95151229 .20960393 25598-5 41837-3 0 9992
2 52424 97.3573 301.7001 0016180 276.0889 203.9597 16.45792401125867Definitive object data (Epoch: 2024-07-24T22:50:10.661Z)
| Latitude | 59.32513° |
| Longitude | -151.49321° |
| Altitude | 170.236 km |
| Speed | 7.804 km/s |
| True Right ascension | 08h 56m 47s |
| True Declination | 59° 09' 37" |
| 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 | 157.795 km |
| Perigee altitude | 136.679 km |
| Semi-major axis | 6,525.374 km |
| Eccentricity | 0.001618 |
| Inclination | 97.3573° |
| RAAN | 301.7001° |
| Arg. of periapsis | 276.0889° |
| True anomaly | 203.88455° |
| Mean anomaly | 203.9597° |
| Eccentric anomaly | 203.92211° |
| Mean motion | 4.11751 °/min |
| BSTAR | 0.00041837 |
| Orbital period | 87.43 mins |
Other satellites on launch #47 in the year 2022 (2022-05-02 UTC)
OBJECT AG 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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