SL-12 R/B(AUX MOTOR), 19755

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 19755 is space debris in HEO originally from a launch on Tue, 10 Jan 1989 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
19755, 1989-001G
Orbit
HEO
Country
Flag of CISCIS
Related business
Manufacturer
NPO Energiya
Mission
Spacecraft
Bus & Motor
SOZ, Unknown motor
Mass
Wet unknown, ~60 kg dry
Launch date (UTC)
1989-01-10 (37 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: 12 hours ago

TLE from 12 hours ago
0 SL-12 R/B(AUX MOTOR)
1 19755U 89001G   25350.65146809 -.00000066  00000-0 -60738-3 0  9990
2 19755  65.2667  72.7264 5524490  86.3869 331.9511  4.25601684573349
Epoch: 2025-12-16T15:38Z
TLE epoch observation values (Epoch: 2025-12-16T15:38:06.842Z)
Latitude
0.00001°
Longitude
112.6793°
Altitude
4,412.739 km
Speed
7.008 km/s
True Right ascension
04h 50m 57s
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
02:44:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,590.045 km
Perigee altitude
819.867 km
Semi-major axis
16,083.093 km
Eccentricity
0.55245
Inclination
65.2667°
RAAN
72.7264°
Arg. of periapsis
86.3869°
True anomaly
273.63079°
Mean anomaly
331.9511°
Eccentric anomaly
306.50986°
Mean motion
1.06412 °/min
Orbital period
338.31 mins
BSTAR
-0.00060738
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