SL-12 R/B(AUX MOTOR), 29682

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 29682 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
29682, 2006-062H
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: 1 week ago

TLE from 1 week ago
0 SL-12 R/B(AUX MOTOR)
1 29682U 06062H   25343.44481990  .00000128  00000-0  11840-2 0  9994
2 29682  65.1765  85.1626 5590212 261.3646  34.8942  4.25378267293502
Epoch: 2025-12-09T10:40Z
TLE epoch observation values (Epoch: 2025-12-09T10:40:32.439Z)
Latitude
-0.00009°
Longitude
-153.39331°
Altitude
5,716.765 km
Speed
6.415 km/s
True Right ascension
05h 40m 41s
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
00:00:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,704.511 km
Perigee altitude
716.645 km
Semi-major axis
16,088.715 km
Eccentricity
0.55902
Inclination
65.1765°
RAAN
85.1626°
Arg. of periapsis
261.3646°
True anomaly
98.73144°
Mean anomaly
34.8942°
Eccentric anomaly
63.57797°
Mean motion
1.06356 °/min
Orbital period
338.49 mins
BSTAR
0.001184
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