SL-12 R/B(AUX MOTOR), 28919

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 28919 is space debris in HEO originally from a launch on Sun, 25 Dec 2005 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
28919, 2005-050E
Orbit
HEO
Country
Flag of CISCIS
Related business
Manufacturer
RKKE
Mission
Spacecraft
Bus & Motor
SOZ, Unknown motor
Mass
56 kg wet, 56 kg dry
Launch date (UTC)
2005-12-25 (20 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: 13 hours ago

TLE from 13 hours ago
0 SL-12 R/B(AUX MOTOR)
1 28919U 05050E   25318.46236220  .00000704  00000-0  11509-2 0  9992
2 28919  64.9401 140.5540 5751157 205.9718 107.8058  4.24217994307233
Epoch: 2025-11-14T11:05Z
TLE epoch observation values (Epoch: 2025-11-14T11:05:48.094Z)
Latitude
0.00002°
Longitude
-79.7159°
Altitude
15,965.984 km
Speed
3.31 km/s
True Right ascension
09h 22m 09s
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
20:40:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,009.608 km
Perigee altitude
470.156 km
Semi-major axis
16,118.019 km
Eccentricity
0.57512
Inclination
64.9401°
RAAN
140.554°
Arg. of periapsis
205.9718°
True anomaly
154.08473°
Mean anomaly
107.8058°
Eccentric anomaly
132.21195°
Mean motion
1.06066 °/min
Orbital period
339.41 mins
BSTAR
0.0011509
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