SL-12 R/B(AUX MOTOR), 23403

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 23403 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
23403, 1994-076H
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 23403U 94076H   26170.97982336 -.00000027  00000-0  45073-3 0  9993
2 23403  65.5422 320.8942 5579280 109.5164 315.7773  4.27492881490807
Epoch: 2026-06-19T23:30Z
TLE epoch observation values (Epoch: 2026-06-19T23:30:56.738Z)
Latitude
-1.07322°
Longitude
59.45344°
Altitude
7,363.452 km
Speed
5.759 km/s
True Right ascension
21h 21m 33s
True Declination
-1° 04' 12"
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
23:07:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,604.137 km
Perigee altitude
710.742 km
Semi-major axis
16,035.577 km
Eccentricity
0.55793
Inclination
65.5422°
RAAN
320.8942°
Arg. of periapsis
109.5164°
True anomaly
249.42408°
Mean anomaly
315.7773°
Eccentric anomaly
284.88276°
Mean motion
1.06885 °/min
Orbital period
336.81 mins
BSTAR
0.00045073
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