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.
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58930 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
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
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year 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
TLE epoch observation values (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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
03:56:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
122.994 km
Perigee altitude
108.353 km
Semi-major axis
6,493.81 km
Eccentricity
0.00113
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
Orbital period
86.8 mins
BSTAR
0.00012376
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Other satellites on launch #26 in the year 2024 (2024-02-09 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SL-4 R/B Visibility
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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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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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