SL-12 R/B(AUX MOTOR), 29680

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 29680 is space debris in HEO originally from a launch on Mon, 25 Dec 2006 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
29680, 2006-062G
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)
2006-12-25 (19 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 29680U 06062G   26123.06391164 -.00000074  00000-0  11824-3 0  9994
2 29680  65.1514  51.0859 5713751 213.3497  92.1914  4.25929822198518
Epoch: 2026-05-03T01:32Z
TLE epoch observation values (Epoch: 2026-05-03T01:32:01.965Z)
Latitude
-0.00006°
Longitude
167.11411°
Altitude
14,360.685 km
Speed
3.695 km/s
True Right ascension
03h 24m 22s
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
18:10:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,881.385 km
Perigee altitude
511.918 km
Semi-major axis
16,074.788 km
Eccentricity
0.57138
Inclination
65.1514°
RAAN
51.0859°
Arg. of periapsis
213.3497°
True anomaly
146.70891°
Mean anomaly
92.1914°
Eccentric anomaly
120.42159°
Mean motion
1.06494 °/min
Orbital period
338.05 mins
BSTAR
0.00011824
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