SL-12 R/B(2), 23683
Orbit data source: Space-Track
SL-12 R/B(2), 23683 is space debris in GEO originally from a launch on Wed, 11 Oct 1995 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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23683 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
RKKE
Mission
Spacecraft
Bus & Motor
BLOK DM, Unknown motor
Mass
2,440 kg wet, 2,440 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 3.1 m
Radar Cross Section
23.597 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SL-12 R/B(2)
1 23683U 95054D 25241.67323203 -.00000335 00000-0 00000-0 0 9997
2 23683 14.9598 1.3729 0019089 100.9595 250.8388 1.00290654109447Epoch: 2025-08-29T16:09Z
TLE epoch observation values (Epoch: 2025-08-29T16:09:27.247Z)
Latitude
-2.17319°
Longitude
132.74871°
Altitude
35,808.033 km
Speed
3.073 km/s
True Right ascension
23h 32m 55s
True Declination
-2° 10' 16"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
16:03:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,862.752 km
Perigee altitude
35,701.792 km
Semi-major axis
42,160.409 km
Eccentricity
0.00191
Inclination
14.9598°
RAAN
1.3729°
Arg. of periapsis
100.9595°
True anomaly
250.63234°
Mean anomaly
250.8388°
Eccentric anomaly
250.73555°
Mean motion
0.25072 °/min
Orbital period
1,435.87 mins
BSTAR
0
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Other satellites on launch #54 in the year 1995 (1995-10-11 UTC)
SL-12 R/B(2) Visibility
Observer location: undefined°, undefined°
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23683 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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