OBJECT C, 51096 (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 C, 51096 was a satellite in LEO that was launched on Thu, 13 Jan 2022 UTC via an LAUNCHERONE launch vehicle from the Pegasus Launch, Western Range Air Space (WRAS). 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.
51096 intel report (Beta)
OBJECT C details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 4 months ago |
| Origin | |
| Manufacturer | Cornell |
| Mission | Decayed Amateur Technology |
| Bus & Motor | CUBESAT 3U, Unknown motor |
| Mass | 4 kg wet, 4 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, 0.3 m |
| Radar Cross Section | 0.035 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 4 months ago
0 OBJECT C
1 51096U 22003C 24229.64932609 .11828593 10716-4 32976-3 0 9992
2 51096 44.9174 335.3400 0006464 325.2105 34.8398 16.45189140145664Definitive object data (Epoch: 2024-08-16T15:35:01.774Z)
| Latitude | -0.00001° |
| Longitude | 136.06236° |
| Altitude | 148.561 km |
| Speed | 7.821 km/s |
| True Right ascension | 22h 21m 21s |
| 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 | 157.962 km |
| Perigee altitude | 149.518 km |
| Semi-major axis | 6,531.877 km |
| Eccentricity | 0.0006464 |
| Inclination | 44.9174° |
| RAAN | 335.34° |
| Arg. of periapsis | 325.2105° |
| True anomaly | 34.88214° |
| Mean anomaly | 34.8398° |
| Eccentric anomaly | 34.86097° |
| Mean motion | 4.11137 °/min |
| BSTAR | 0.00032976 |
| Orbital period | 87.56 mins |
Other satellites on launch #3 in the year 2022 (2022-01-13 UTC)
OBJECT C 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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