SL-12 R/B(2), 23270

Orbit data source: Space-Track

SL-12 R/B(2), 23270 is space debris in GEO originally from a launch on Wed, 21 Sep 1994 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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Identifier
23270, 1994-060D
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)
1994-09-21 (31 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: 15 hours ago

TLE from 15 hours ago
0 SL-12 R/B(2)
1 23270U 94060D   26023.47970657  .00000027  00000-0  00000-0 0  9990
2 23270  14.3014 351.1725 0006334 157.6259  25.1242  1.00059193114093
Epoch: 2026-01-23T11:30Z
TLE epoch observation values (Epoch: 2026-01-23T11:30:46.647Z)
Latitude
-0.68104°
Longitude
-121.63783°
Altitude
35,821.694 km
Speed
3.074 km/s
True Right ascension
11h 35m 29s
True Declination
0° 40' 49"
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
03:42:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,874.017 km
Perigee altitude
35,820.526 km
Semi-major axis
42,225.408 km
Eccentricity
0.00063
Inclination
14.3014°
RAAN
351.1725°
Arg. of periapsis
157.6259°
True anomaly
25.15504°
Mean anomaly
25.1242°
Eccentric anomaly
25.13962°
Mean motion
0.25014 °/min
Orbital period
1,439.2 mins
BSTAR
0
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