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   26171.19700953 -.00000068  00000-0  13692-3 0  9999
2 29680  65.1592  33.5804 5714748 210.9562  97.1352  4.25934809200563
Epoch: 2026-06-20T04:43Z
TLE epoch observation values (Epoch: 2026-06-20T04:43:41.623Z)
Latitude
-0°
Longitude
54.24797°
Altitude
14,857.115 km
Speed
3.571 km/s
True Right ascension
02h 14m 20s
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
23:18:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,882.789 km
Perigee altitude
510.261 km
Semi-major axis
16,074.662 km
Eccentricity
0.57147
Inclination
65.1592°
RAAN
33.5804°
Arg. of periapsis
210.9562°
True anomaly
149.09661°
Mean anomaly
97.1352°
Eccentric anomaly
124.21239°
Mean motion
1.06495 °/min
Orbital period
338.04 mins
BSTAR
0.00013692
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