OBJECT B, 60455 (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 B, 60455 was an Indian satellite in LEO that was launched on Fri, 16 Aug 2024 UTC via an SSLV launch vehicle from the Sirharikota (SRI). 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.
60455 intel report (Beta)
OBJECT B radio frequencies
OBJECT B details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 2 months ago |
| Origin | |
| Manufacturer | SRICK |
| Mission | Decayed spacecraft |
| Bus & Motor | SR0, Unknown motor |
| Mass | 0.2 kg wet, 0.2 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Unknown |
| Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 2 months ago
0 OBJECT B
1 60455U 24147B 24306.95056519 .14569292 41128-5 32600-2 0 9995
2 60455 37.3538 162.9853 0013229 282.3917 77.5393 16.28877097 11746Definitive object data (Epoch: 2024-11-01T22:48:48.832Z)
| Latitude | -0.00001° |
| Longitude | 139.06982° |
| Altitude | 192.812 km |
| Speed | 7.794 km/s |
| True Right ascension | 10h 51m 56s |
| True Declination | 0° 00' 00" |
| 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 | 207.265 km |
| Perigee altitude | 189.864 km |
| Semi-major axis | 6,576.701 km |
| Eccentricity | 0.0013229 |
| Inclination | 37.3538° |
| RAAN | 162.9853° |
| Arg. of periapsis | 282.3917° |
| True anomaly | 77.68737° |
| Mean anomaly | 77.5393° |
| Eccentric anomaly | 77.61333° |
| Mean motion | 4.06941 °/min |
| BSTAR | 0.00326 |
| Orbital period | 88.47 mins |
Other satellites on launch #147 in the year 2024 (2024-08-16 UTC)
| EOS-8, 60454 |
| OBJECT B, 60455 (Decayed) |
| OBJECT C, 60456 |
| OBJECT D, 60457 |
OBJECT B 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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