OBJECT AB, 62402
Orbit data source: Space-Track
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Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT AB, 62402 is a satellite in LEO that was launched on Sat, 21 Dec 2024 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.
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62402 intel report (Beta)
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OBJECT AB radio frequencies
OBJECT AB details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 16 hours ago |
| Origin | |
| Manufacturer | Montpellier |
| Mission | Operational Commercial Communications |
| Bus & Motor | CUBESAT 1U, Unknown motor |
| Mass | 1 kg wet, 1 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, 0.05 m |
| Radar Cross Section | 0.004 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 16 hours ago
0 OBJECT AB
1 62402U 24247AB 25035.59706850 .00026810 00000-0 11700-2 0 9996
2 62402 44.9906 117.2365 0004685 265.3936 94.6410 15.21731676 7000Epoch: 2025-02-04T14:19Z
Definitive object data (Epoch: 2025-02-04T14:19:46.718Z)
| Latitude | 0.00002° |
| Longitude | 127.29178° |
| Altitude | 500.877 km |
| Speed | 7.616 km/s |
| True Right ascension | 07h 48m 56s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 22.82815° |
| Longitude | -81.16338° |
| Altitude | 502.067 km |
| Speed | 7.616 km/s |
| Apparent Right ascension | 19h 08m 58s |
| Apparent Declination | -7° 41' 45" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 08:45:50 |
| Azimuth | 40.423° NE |
| Elevation | -51.18° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 505.447 km |
| Perigee altitude | 499 km |
| Semi-major axis | 6,880.361 km |
| Eccentricity | 0.0004685 |
| Inclination | 44.9906° |
| RAAN | 117.2365° |
| Arg. of periapsis | 265.3936° |
| True anomaly | 94.69451° |
| Mean anomaly | 94.641° |
| Eccentric anomaly | 94.66775° |
| Mean motion | 3.803 °/min |
| BSTAR | 0.00117 |
| Orbital period | 94.66 mins |
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Other satellites on launch #247 in the year 2024 (2024-12-21 UTC)
OBJECT AB 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-02-05 07:50:37.537Z | 190.674° SSW | 2025-02-05 07:52:37.537Z | 153.145° SSE | 22.373° | 2025-02-05 07:55:37.537Z | 92.495° ESE |
| 6 mins | 2025-02-05 09:29:37.537Z | 256.184° W | 2025-02-05 09:31:37.537Z | 293.064° NW | 42.847° | 2025-02-05 09:35:37.537Z | 64.428° ENE |
| 5 mins | 2025-02-05 11:09:37.537Z | 303.732° NW | 2025-02-05 11:11:37.537Z | 3.189° NNE | 31.54° | 2025-02-05 11:14:37.537Z | 63.946° ENE |
| 6 mins | 2025-02-05 12:48:37.537Z | 303.693° NW | 2025-02-05 12:50:37.537Z | 346.187° N | 37.431° | 2025-02-05 12:54:37.537Z | 93.457° ESE |
| 6 mins | 2025-02-05 14:27:37.537Z | 276.536° WNW | 2025-02-05 14:30:37.537Z | 195.589° SSW | 32.431° | 2025-02-05 14:33:37.537Z | 143.319° SSE |
Authenticating...
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