SL-4 R/B, 62031 (Decayed)
Orbit data source: Space-Track
SL-4 R/B, 62031 was space debris in LEO originally from a launch on Thu, 21 Nov 2024 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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62031 intel report (Beta)
SL-4 R/B details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 1 month ago |
| Origin | |
| Manufacturer | TsSKB-Progress |
| Mission | Decayed spacecraft |
| Bus & Motor | BLOK-I, RD-0980 |
| Mass | ~2,350 kg wet, 2,350 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 month ago
0 SL-4 R/B
1 62031U 24215B 24328.24398021 .11007155 12532-4 40279-3 0 9996
2 62031 51.6438 246.9269 0011875 76.8603 51.8089 16.43183118 288Epoch: 2024-11-23T05:51Z
Definitive object data (Epoch: 2024-11-23T05:51:19.89Z)
| Latitude | 37.81752° |
| Longitude | -121.24422° |
| Altitude | 155.505 km |
| Speed | 7.821 km/s |
| True Right ascension | 01h 57m 09s |
| True Declination | 37° 38' 09" |
| 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 | 165.637 km |
| Perigee altitude | 150.114 km |
| Semi-major axis | 6,536.013 km |
| Eccentricity | 0.0011875 |
| Inclination | 51.6438° |
| RAAN | 246.9269° |
| Arg. of periapsis | 76.8603° |
| True anomaly | 51.91595° |
| Mean anomaly | 51.8089° |
| Eccentric anomaly | 51.86241° |
| Mean motion | 4.10746 °/min |
| BSTAR | 0.00040279 |
| Orbital period | 87.65 mins |
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Other satellites on launch #215 in the year 2024 (2024-11-21 UTC)
| PROGRESS MS-29, 62030 |
| SL-4 R/B, 62031 (Decayed) |
SL-4 R/B Visibility forecast
Observer location: undefined°, undefined
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