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 (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: 19 hours ago

TLE from 19 hours ago
0 SL-12 R/B(AUX MOTOR)
1 36116U 09070F   25348.83476767  .00000084  00000-0  57909-3 0  9998
2 36116  64.9639 275.9214 5643662 308.3162  13.1773  4.35611945 93003
Epoch: 2025-12-14T20:02Z
TLE epoch observation values (Epoch: 2025-12-14T20:02:03.926Z)
Latitude
-0.00006°
Longitude
-108.36057°
Altitude
1,620.501 km
Speed
8.632 km/s
True Right ascension
18h 23m 35s
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
13:25:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,394.714 km
Perigee altitude
520.434 km
Semi-major axis
15,835.711 km
Eccentricity
0.56437
Inclination
64.9639°
RAAN
275.9214°
Arg. of periapsis
308.3162°
True anomaly
51.74579°
Mean anomaly
13.1773°
Eccentric anomaly
28.71131°
Mean motion
1.08915 °/min
Orbital period
330.53 mins
BSTAR
0.00057909
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