SL-12 R/B(2), 29673

Orbit data source: Space-Track

SL-12 R/B(2), 29673 is space debris in MEO 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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SL-12 R/B(2) details

Identifier	29673, 2006-062D
Orbit	MEO
Last TLE update	1 day ago
Origin	Khrunichev (CIS)
Manufacturer	RKKE
Mission	Spacecraft
Bus & Motor	BLOK DM2, 11D58M
Mass	2,440 kg wet, 2,440 kg dry
Launch date (UTC)	2006-12-25 (18 years ago)
Launch vehicle	Unknown
Launch site	Tyuratam Missile And Space Complex (TTMTR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 6.3 m
Radar Cross Section	23.684 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 SL-12 R/B(2)
1 29673U 06062D   24360.38318275  .00000102  00000-0  00000-0 0  9996
2 29673  64.7016 211.6081 0026221 191.2912 168.8343  2.13404542140496

Epoch: 2024-12-25T09:11Z

Definitive object data (Epoch: 2024-12-25T09:11:46.989Z)

Latitude	0.09573°
Longitude	-20.66556°
Altitude	19,171.891 km
Speed	3.945 km/s
True Right ascension	14h 06m 37s
True Declination	0° 05' 44"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	64.54934°
Longitude	76.45141°
Altitude	19,125.76 km
Speed	3.954 km/s
Apparent Right ascension	21h 00m 22s
Apparent Declination	50° 25' 45"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	09:57:26
Azimuth	9.035° NNE
Elevation	1.209°
Doppler factor	1

Orbital elements

Apogee altitude	19,172.219 km
Perigee altitude	19,038.578 km
Semi-major axis	25,483.535 km
Eccentricity	0.0026221
Inclination	64.7016°
RAAN	211.6081°
Arg. of periapsis	191.2912°
True anomaly	168.8923°
Mean anomaly	168.8343°
Eccentric anomaly	168.86332°
Mean motion	0.53352 °/min
BSTAR	Unknown
Orbital period	674.76 mins