SL-12 R/B(AUX MOTOR), 37144

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 37144 is space debris in HEO originally from a launch on Thu, 02 Sep 2010 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
37144, 2010-041H
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)
2010-09-02 (15 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 37144U 10041H   26034.29327579  .00000093  00000-0  38809-3 0  9997
2 37144  64.7856 139.8188 5643084 314.2348  11.4024  4.24860807 99638
Epoch: 2026-02-03T07:02Z
TLE epoch observation values (Epoch: 2026-02-03T07:02:19.028Z)
Latitude
-0.0001°
Longitude
-99.24558°
Altitude
1,502.531 km
Speed
8.742 km/s
True Right ascension
09h 19m 14s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
12:43:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,810.046 km
Perigee altitude
637.283 km
Semi-major axis
16,101.801 km
Eccentricity
0.56431
Inclination
64.7856°
RAAN
139.8188°
Arg. of periapsis
314.2348°
True anomaly
45.80254°
Mean anomaly
11.4024°
Eccentric anomaly
25.13644°
Mean motion
1.06226 °/min
Orbital period
338.9 mins
BSTAR
0.00038809
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