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 day ago

TLE from 1 day ago
0 SL-12 R/B(AUX MOTOR)
1 29682U 06062H   26033.22024220  .00000026  00000-0  45139-3 0  9992
2 29682  65.1822  66.0291 5601979 258.6859  36.6264  4.25384026295835
Epoch: 2026-02-02T05:17Z
TLE epoch observation values (Epoch: 2026-02-02T05:17:08.926Z)
Latitude
-0.00002°
Longitude
-145.66649°
Altitude
6,030.932 km
Speed
6.283 km/s
True Right ascension
04h 24m 09s
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
17:28:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,723.211 km
Perigee altitude
697.648 km
Semi-major axis
16,088.566 km
Eccentricity
0.5602
Inclination
65.1822°
RAAN
66.0291°
Arg. of periapsis
258.6859°
True anomaly
101.39197°
Mean anomaly
36.6264°
Eccentric anomaly
65.93321°
Mean motion
1.06357 °/min
Orbital period
338.48 mins
BSTAR
0.00045139
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