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: 1 day ago

TLE from 1 day ago
0 SL-12 R/B(AUX MOTOR)
1 28920U 05050F   25259.94030575  .00002968  00000-0  11374-2 0  9990
2 28920  64.9967 166.5980 5868823 178.9055 183.5742  4.20406473303729
Epoch: 2025-09-16T22:34Z
TLE epoch observation values (Epoch: 2025-09-16T22:34:02.416Z)
Latitude
Longitude
-168.03479°
Altitude
19,350.386 km
Speed
2.531 km/s
True Right ascension
11h 06m 23s
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
20:37:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,353.58 km
Perigee altitude
320.676 km
Semi-major axis
16,215.265 km
Eccentricity
0.58688
Inclination
64.9967°
RAAN
166.598°
Arg. of periapsis
178.9055°
True anomaly
181.14943°
Mean anomaly
183.5742°
Eccentric anomaly
182.25256°
Mean motion
1.05113 °/min
Orbital period
342.49 mins
BSTAR
0.0011374
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