SL-4 R/B, 61044 (Decayed)
Orbit data source: Space-Track
SL-4 R/B, 61044 was space debris in LEO originally from a launch on Wed, 11 Sep 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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61044 intel report (Beta)
SL-4 R/B details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 3 months ago |
| Origin | |
| Manufacturer | TsSKB-Progress |
| Mission | Decayed spacecraft |
| Bus & Motor | BLOK-I, RD-0110 |
| 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 3 months ago
0 SL-4 R/B
1 61044U 24162B 24257.35435400 .20508142 12653-4 36769-3 0 9991
2 61044 51.6564 237.6431 0005037 55.6763 97.7759 16.47424603 277Epoch: 2024-09-13T08:30Z
Definitive object data (Epoch: 2024-09-13T08:30:16.185Z)
| Latitude | 20.528° |
| Longitude | -79.8777° |
| Altitude | 146.94 km |
| Speed | 7.821 km/s |
| True Right ascension | 02h 42m 04s |
| True Declination | 20° 24' 17" |
| 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 | 149.939 km |
| Perigee altitude | 143.366 km |
| Semi-major axis | 6,524.789 km |
| Eccentricity | 0.0005037 |
| Inclination | 51.6564° |
| RAAN | 237.6431° |
| Arg. of periapsis | 55.6763° |
| True anomaly | 97.83308° |
| Mean anomaly | 97.7759° |
| Eccentric anomaly | 97.80449° |
| Mean motion | 4.11807 °/min |
| BSTAR | 0.00036769 |
| Orbital period | 87.42 mins |
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Other satellites on launch #162 in the year 2024 (2024-09-11 UTC)
| SOYUZ MS-26, 61043 |
| SL-4 R/B, 61044 (Decayed) |
SL-4 R/B Visibility forecast
Observer location: undefined°, undefined
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