SL-12 R/B(AUX MOTOR), 36406

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 36406 is space debris in HEO originally from a launch on Mon, 01 Mar 2010 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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Identifier
36406, 2010-007G
Orbit
HEO
Country
Flag of CISCIS
Related business
Manufacturer
RKKE
Mission
Spacecraft
Bus & Motor
SOZ, Unknown motor
Mass
56 kg wet, 56 kg dry
Launch date (UTC)
2010-03-01 (16 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.6 m
Radar Cross Section
0.660 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 SL-12 R/B(AUX MOTOR)
1 36406U 10007G   25339.79054683  .00000062  00000-0  74319-3 0  9996
2 36406  64.6530 282.0210 5664582 333.3882   6.1874  4.23082355175041
Epoch: 2025-12-05T18:58Z
TLE epoch observation values (Epoch: 2025-12-05T18:58:23.246Z)
Latitude
0.00005°
Longitude
-77.42256°
Altitude
902.197 km
Speed
9.211 km/s
True Right ascension
18h 48m 00s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
04:24:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,915.317 km
Perigee altitude
622.222 km
Semi-major axis
16,146.907 km
Eccentricity
0.56646
Inclination
64.653°
RAAN
282.021°
Arg. of periapsis
333.3882°
True anomaly
26.43345°
Mean anomaly
6.1874°
Eccentric anomaly
14.08688°
Mean motion
1.05781 °/min
Orbital period
340.32 mins
BSTAR
0.00074319
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