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: 5 days ago

TLE from 5 days ago
0 SL-12 R/B(AUX MOTOR)
1 29682U 06062H   25251.99473319  .00000017  00000-0 -37515-3 0  9994
2 29682  65.1704 116.8612 5565351 265.8890  32.2204  4.25375288289618
Epoch: 2025-09-08T23:52Z
TLE epoch observation values (Epoch: 2025-09-08T23:52:24.947Z)
Latitude
-0.00007°
Longitude
130.47548°
Altitude
5,198.426 km
Speed
6.641 km/s
True Right ascension
07h 47m 29s
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
09:53:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,664.642 km
Perigee altitude
756.68 km
Semi-major axis
16,088.798 km
Eccentricity
0.55654
Inclination
65.1704°
RAAN
116.8612°
Arg. of periapsis
265.889°
True anomaly
94.22957°
Mean anomaly
32.2204°
Eccentric anomaly
59.7717°
Mean motion
1.06355 °/min
Orbital period
338.49 mins
BSTAR
-0.00037515
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