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.

Not visible in the next 10 days
Identifier
23683, 1995-054D
Orbit
GEO
Country
Flag of CISCIS
Related business
Manufacturer
RKKE
Mission
Spacecraft
Bus & Motor
BLOK DM, Unknown motor
Mass
2,440 kg wet, 2,440 kg dry
Launch date (UTC)
1995-10-11 (30 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.1 m
Radar Cross Section
23.597 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 SL-12 R/B(2)
1 23683U 95054D   26039.29020318 -.00000371  00000-0  00000+0 0  9991
2 23683  14.9805   0.0865 0017495  98.3556 266.1580  1.00214985111081
Epoch: 2026-02-08T06:57Z
TLE epoch observation values (Epoch: 2026-02-08T06:57:53.554Z)
Latitude
1.11135°
Longitude
121.39033°
Altitude
35,807.308 km
Speed
3.074 km/s
True Right ascension
00h 17m 03s
True Declination
1° 06' 37"
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
19:09:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,877.288 km
Perigee altitude
35,729.694 km
Semi-major axis
42,181.628 km
Eccentricity
0.00175
Inclination
14.9805°
RAAN
0.0865°
Arg. of periapsis
98.3556°
True anomaly
265.958°
Mean anomaly
266.158°
Eccentric anomaly
266.058°
Mean motion
0.25053 °/min
Orbital period
1,436.96 mins
BSTAR
0
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