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: 13 hours ago

TLE from 13 hours ago
0 SL-12 R/B(AUX MOTOR)
1 28920U 05050F   26043.67033953  .00001499  00000-0  10852-2 0  9993
2 28920  65.0228 111.1865 5832105 171.9709 204.6928  4.21410426309981
Epoch: 2026-02-12T16:05Z
TLE epoch observation values (Epoch: 2026-02-12T16:05:17.335Z)
Latitude
-0.00004°
Longitude
87.14832°
Altitude
18,906.772 km
Speed
2.629 km/s
True Right ascension
07h 24m 45s
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
07:17:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,253.259 km
Perigee altitude
369.479 km
Semi-major axis
16,189.506 km
Eccentricity
0.58321
Inclination
65.0228°
RAAN
111.1865°
Arg. of periapsis
171.9709°
True anomaly
188.07626°
Mean anomaly
204.6928°
Eccentric anomaly
195.66833°
Mean motion
1.05364 °/min
Orbital period
341.67 mins
BSTAR
0.0010852
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