SL-12 R/B(2), 23883

Orbit data source: Space-Track

SL-12 R/B(2), 23883 is space debris in GEO originally from a launch on Sat, 25 May 1996 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.

Not visible in the next 10 days

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Identifier	23883, 1996-034D
Orbit	GEO
Last TLE update	10 hours ago
Origin	RVSN (CIS)
Manufacturer	RKKE
Mission	Spacecraft
Bus & Motor	BLOK DM, Unknown motor
Mass	2,440 kg wet, 2,440 kg dry
Launch date (UTC)	1996-05-25 (29 years ago)
Launch vehicle	Unknown
Launch site	Tyuratam Missile And Space Complex (TTMTR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 6.27 m
Radar Cross Section	23.597 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 10 hours ago

0 SL-12 R/B(2)
1 23883U 96034D   25093.83378100 -.00000075  00000-0  00000-0 0  9998
2 23883  15.2555   1.1591 0030342  91.5318  87.0374  0.97944472103239

Epoch: 2025-04-03T20:00Z

Definitive object data (Epoch: 2025-04-03T20:00:38.678Z)

Latitude	0.27477°
Longitude	47.5755°
Altitude	36,445.474 km
Speed	3.051 km/s
True Right ascension	12h 00m 33s
True Declination	0° 16' 28"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-10.10921°
Longitude	-172.21239°
Altitude	36,541.847 km
Speed	3.044 km/s
Apparent Right ascension	21h 33m 33s
Apparent Declination	-13° 59' 20"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	11:22:25
Azimuth	50.312° ENE
Elevation	-54.781°
Doppler factor	1

Orbital elements

Apogee altitude	36,582.816 km
Perigee altitude	36,322.9 km
Semi-major axis	42,830.995 km
Eccentricity	0.0030342
Inclination	15.2555°
RAAN	1.1591°
Arg. of periapsis	91.5318°
True anomaly	87.38469°
Mean anomaly	87.0374°
Eccentric anomaly	87.21104°
Mean motion	0.24485 °/min
BSTAR	Unknown
Orbital period	1470.27 mins