SL-12 R/B(AUX MOTOR), 32280

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 32280 is space debris in HEO originally from a launch on Fri, 26 Oct 2007 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
32280, 2007-052F
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)
2007-10-26 (19 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: 4 days ago

TLE from 4 days ago
0 SL-12 R/B(AUX MOTOR)
1 32280U 07052F   26126.12974669 -.00000024  00000-0  26886-3 0  9990
2 32280  65.2605 339.0119 5640694 221.0040  78.9741  4.21920878191244
Epoch: 2026-05-06T03:06Z
TLE epoch observation values (Epoch: 2026-05-06T03:06:50.114Z)
Latitude
-0.00001°
Longitude
68.3094°
Altitude
12,833.493 km
Speed
4.106 km/s
True Right ascension
22h 36m 03s
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
22:55:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,922.997 km
Perigee altitude
673.685 km
Semi-major axis
16,176.478 km
Eccentricity
0.56407
Inclination
65.2605°
RAAN
339.0119°
Arg. of periapsis
221.004°
True anomaly
139.04253°
Mean anomaly
78.9741°
Eccentric anomaly
109.44877°
Mean motion
1.05491 °/min
Orbital period
341.26 mins
BSTAR
0.00026886
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