SL-12 R/B(AUX MOTOR), 36115

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 36115 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
36115, 2009-070E
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 36115U 09070E   26171.45706227  .00000076  00000-0  48917-3 0  9997
2 36115  65.2612 245.9720 5592384 267.0512  31.2561  4.26802036256123
Epoch: 2026-06-20T10:58Z
TLE epoch observation values (Epoch: 2026-06-20T10:58:10.180Z)
Latitude
-0.00006°
Longitude
172.76003°
Altitude
4,998.301 km
Speed
6.727 km/s
True Right ascension
16h 23m 53s
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
23:20:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,652.164 km
Perigee altitude
697.366 km
Semi-major axis
16,052.902 km
Eccentricity
0.55924
Inclination
65.2612°
RAAN
245.972°
Arg. of periapsis
267.0512°
True anomaly
93.10166°
Mean anomaly
31.2561°
Eccentric anomaly
58.60787°
Mean motion
1.06712 °/min
Orbital period
337.36 mins
BSTAR
0.00048917
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