SL-12 R/B(AUX MOTOR), 28920

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 28920 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
28920, 2005-050F
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: 19 hours ago

TLE from 19 hours ago
0 SL-12 R/B(AUX MOTOR)
1 28920U 05050F   25318.19527735  .00004387  00000-0  17580-2 0  9994
2 28920  65.0154 144.8534 5859091 176.2209 191.8640  4.20813898306176
Epoch: 2025-11-14T04:41Z
TLE epoch observation values (Epoch: 2025-11-14T04:41:11.963Z)
Latitude
0.00006°
Longitude
21.01105°
Altitude
19,242.979 km
Speed
2.554 km/s
True Right ascension
09h 39m 24s
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
19,321.198 km
Perigee altitude
332.122 km
Semi-major axis
16,204.797 km
Eccentricity
0.58591
Inclination
65.0154°
RAAN
144.8534°
Arg. of periapsis
176.2209°
True anomaly
183.83067°
Mean anomaly
191.864°
Eccentric anomaly
187.48875°
Mean motion
1.05215 °/min
Orbital period
342.16 mins
BSTAR
0.001758
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