SL-12 R/B(2), 32278

Orbit data source: Space-Track

SL-12 R/B(2), 32278 is space debris in MEO originally from a launch on Fri, 26 Oct 2007 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	32278, 2007-052D
Orbit	MEO
Last TLE update	2 days 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)	2007-10-26 (17 years ago)
Launch vehicle	Unknown
Launch site	Tyuratam Missile And Space Complex (TTMTR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 7.1 m
Radar Cross Section	26.008 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 days ago

0 SL-12 R/B(2)
1 32278U 07052D   24359.92576177 -.00000056  00000-0  00000+0 0  9994
2 32278  65.8524 333.4394 0017479 201.1051 340.0248  2.13394124133705

Epoch: 2024-12-24T22:13Z

Definitive object data (Epoch: 2024-12-24T22:13:05.816Z)

Latitude	-1.02215°
Longitude	86.68617°
Altitude	19,065.524 km
Speed	3.961 km/s
True Right ascension	10h 15m 32s
True Declination	-1° 01' 14"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-64.80618°
Longitude	-165.98802°
Altitude	19,120.222 km
Speed	3.955 km/s
Apparent Right ascension	18h 48m 47s
Apparent Declination	-64° 11' 09"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	10:19:02
Azimuth	146.409° SSE
Elevation	-51.321°
Doppler factor	1

Orbital elements

Apogee altitude	19,150.732 km
Perigee altitude	19,061.644 km
Semi-major axis	25,484.325 km
Eccentricity	0.0017479
Inclination	65.8524°
RAAN	333.4394°
Arg. of periapsis	201.1051°
True anomaly	339.95624°
Mean anomaly	340.0248°
Eccentric anomaly	339.99053°
Mean motion	0.5335 °/min
BSTAR	Unknown
Orbital period	674.79 mins