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)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
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
Shape & HBR
Cyl, 4.5 m
Radar Cross Section
21.560 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months 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
TLE epoch observation values (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
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
23:18:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
165.637 km
Perigee altitude
150.114 km
Semi-major axis
6,536.013 km
Eccentricity
0.00119
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
Orbital period
87.65 mins
BSTAR
0.00040279
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Other satellites on launch #215 in the year 2024 (2024-11-21 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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