SL-12 R/B(AUX MOTOR), 23402

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 23402 is space debris in HEO originally from a launch on Sun, 20 Nov 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
23402, 1994-076G
Orbit
HEO
Country
Flag of CISCIS
Related business
Manufacturer
RKKE
Mission
Spacecraft
Bus & Motor
SOZ, Unknown motor
Mass
Wet unknown, ~60 kg dry
Launch date (UTC)
1994-11-20 (32 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.6 m
Radar Cross Section
0.660 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 SL-12 R/B(AUX MOTOR)
1 23402U 94076G   26295.28340563 -.00000025  00000-0  56851-4 0  9999
2 23402  65.4076 255.4865 5581379 112.5847 314.0758  4.27498821495171
Epoch: 2026-10-22T06:48Z
TLE epoch observation values (Epoch: 2026-10-22T06:48:06.246Z)
Latitude
0.00003°
Longitude
122.73186°
Altitude
7,656.984 km
Speed
5.653 km/s
True Right ascension
17h 01m 54s
True Declination
0° 00' 00"
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
01:51:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,607.29 km
Perigee altitude
707.316 km
Semi-major axis
16,035.44 km
Eccentricity
0.55814
Inclination
65.4076°
RAAN
255.4865°
Arg. of periapsis
112.5847°
True anomaly
247.5122°
Mean anomaly
314.0758°
Eccentric anomaly
282.90453°
Mean motion
1.06886 °/min
Orbital period
336.81 mins
BSTAR
0.000056851
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