SL-12 R/B(AUX MOTOR), 33384

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 33384 is space debris in HEO originally from a launch on Thu, 25 Sep 2008 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
33384, 2008-046G
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)
2008-09-25 (17 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: 10 hours ago

TLE from 10 hours ago
0 SL-12 R/B(AUX MOTOR)
1 33384U 08046G   26062.27823031  .00000044  00000-0  35825-3 0  9995
2 33384  65.3476  74.0757 5632411 241.4210  51.3747  4.23394167269418
Epoch: 2026-03-03T06:40Z
TLE epoch observation values (Epoch: 2026-03-03T06:40:39.098Z)
Latitude
0.00006°
Longitude
172.83638°
Altitude
8,711.197 km
Speed
5.305 km/s
True Right ascension
04h 56m 14s
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
20:44:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,850.883 km
Perigee altitude
670.679 km
Semi-major axis
16,138.918 km
Eccentricity
0.56324
Inclination
65.3476°
RAAN
74.0757°
Arg. of periapsis
241.421°
True anomaly
118.67234°
Mean anomaly
51.3747°
Eccentric anomaly
83.43439°
Mean motion
1.0586 °/min
Orbital period
340.07 mins
BSTAR
0.00035825
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