SL-12 R/B(AUX MOTOR), 36116

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 36116 is space debris in HEO originally from a launch on Mon, 14 Dec 2009 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
36116, 2009-070F
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)
2009-12-14 (17 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: 2 days ago

TLE from 2 days ago
0 SL-12 R/B(AUX MOTOR)
1 36116U 09070F   26171.37791192  .00000062  00000-0  12597-3 0  9994
2 36116  64.9824 205.7667 5598545 299.8065  16.2468  4.35653834101173
Epoch: 2026-06-20T09:04Z
TLE epoch observation values (Epoch: 2026-06-20T09:04:11.589Z)
Latitude
0.00006°
Longitude
161.13725°
Altitude
2,138.842 km
Speed
8.273 km/s
True Right ascension
13h 43m 06s
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
00:50:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,321.701 km
Perigee altitude
591.438 km
Semi-major axis
15,834.706 km
Eccentricity
0.55985
Inclination
64.9824°
RAAN
205.7667°
Arg. of periapsis
299.8065°
True anomaly
60.37481°
Mean anomaly
16.2468°
Eccentric anomaly
34.34314°
Mean motion
1.08925 °/min
Orbital period
330.5 mins
BSTAR
0.00012597
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