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 (18 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: 3 days ago

TLE from 3 days ago
0 SL-12 R/B(AUX MOTOR)
1 32280U 07052F   26034.16441247 -.00000036  00000-0  11760-3 0  9991
2 32280  65.3368  10.7798 5632314 225.7259  71.5314  4.21923455187367
Epoch: 2026-02-03T03:56Z
TLE epoch observation values (Epoch: 2026-02-03T03:56:45.237Z)
Latitude
-0.00003°
Longitude
178.22254°
Altitude
11,840.641 km
Speed
4.373 km/s
True Right ascension
00h 43m 02s
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
00:25:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,909.33 km
Perigee altitude
687.21 km
Semi-major axis
16,176.407 km
Eccentricity
0.56323
Inclination
65.3368°
RAAN
10.7798°
Arg. of periapsis
225.7259°
True anomaly
134.37468°
Mean anomaly
71.5314°
Eccentric anomaly
102.97788°
Mean motion
1.05492 °/min
Orbital period
341.26 mins
BSTAR
0.0001176
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