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: 9 hours ago

TLE from 9 hours ago
0 SL-12 R/B(AUX MOTOR)
1 36406U 10007G   26097.69699329 -.00000037  00000-0 -12529-4 0  9999
2 36406  64.6314 237.9387 5663686 329.4197   7.1636  4.23092161180245
Epoch: 2026-04-07T16:43Z
TLE epoch observation values (Epoch: 2026-04-07T16:43:40.220Z)
Latitude
-0.00005°
Longitude
151.04104°
Altitude
998.325 km
Speed
9.133 km/s
True Right ascension
15h 51m 42s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
07:40:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,913.483 km
Perigee altitude
623.562 km
Semi-major axis
16,146.659 km
Eccentricity
0.56637
Inclination
64.6314°
RAAN
237.9387°
Arg. of periapsis
329.4197°
True anomaly
30.33915°
Mean anomaly
7.1636°
Eccentric anomaly
16.23729°
Mean motion
1.05784 °/min
Orbital period
340.32 mins
BSTAR
-0.000012529
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