SL-4 R/B, 58930 (Decayed)
Orbit data source: Space-Track
SL-4 R/B, 58930 was space debris in LEO originally from a launch on Fri, 09 Feb 2024 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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.
Focus sentinelFocus sentinel
58930 intel report (Beta)
SL-4 R/B details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 6 months ago |
| Origin | |
| Manufacturer | TsSKB-Progress |
| Mission | Decayed spacecraft |
| Bus & Motor | BLOK-I, RD-0110 |
| Mass | Wet unknown, 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 6 months ago
0 SL-4 R/B
1 58930U 24027B 24162.59689719 .31737778 23207-5 12376-3 0 9993
2 58930 96.7292 60.1188 0011273 241.5955 203.7505 16.57784045 19392Epoch: 2024-06-10T14:19Z
Definitive object data (Epoch: 2024-06-10T14:19:31.917Z)
| Latitude | 81.83811° |
| Longitude | -109.07122° |
| Altitude | 139.148 km |
| Speed | 7.826 km/s |
| True Right ascension | 00h 20m 58s |
| True Declination | 81° 47' 06" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -68.30346° |
| Longitude | 1.42084° |
| Altitude | 9,649.381 km |
| Speed | 4.637 km/s |
| Apparent Right ascension | 04h 51m 48s |
| Apparent Declination | -69° 20' 39" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 13:10:28 |
| Azimuth | 206.227° SW |
| Elevation | -48.965° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 122.994 km |
| Perigee altitude | 108.353 km |
| Semi-major axis | 6,493.81 km |
| Eccentricity | 0.0011273 |
| Inclination | 96.7292° |
| RAAN | 60.1188° |
| Arg. of periapsis | 241.5955° |
| True anomaly | 203.69854° |
| Mean anomaly | 203.7505° |
| Eccentric anomaly | 203.72451° |
| Mean motion | 4.14757 °/min |
| BSTAR | 0.00012376 |
| Orbital period | 86.8 mins |
Loading maneuver chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #26 in the year 2024 (2024-02-09 UTC)
| COSMOS 2575, 58929 |
| SL-4 R/B, 58930 (Decayed) |
SL-4 R/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. |
|---|
Authenticating...
Click to sort rows by NORAD ID header in ascending order | Click to sort rows by Common name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
|---|