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
Last TLE update
8 months 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
Shape & HBR
Cyl, 4.5 m
Radar Cross Section
21.560 m², Large (>1 m²)
Expand to show TLE details & history
TLE from 8 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
No trajectory is available.
Visualization observer readout
No trajectory is available.
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)
SL-4 R/B Visibility
Observer location: undefined°, undefined°
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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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Authenticating...
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