SL-12 R/B(AUX MOTOR), 19856

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 19856 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
19856, 1989-001H
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: 18 hours ago

TLE from 18 hours ago
0 SL-12 R/B(AUX MOTOR)
1 19856U 89001H   25350.39522283 -.00000095  00000-0  56373-4 0  9999
2 19856  65.1226  85.6152 5670696  32.8585 352.1803  4.25427816572757
Epoch: 2025-12-16T09:29Z
TLE epoch observation values (Epoch: 2025-12-16T09:29:07.252Z)
Latitude
-0.00011°
Longitude
-141.93187°
Altitude
1,008.561 km
Speed
9.12 km/s
True Right ascension
05h 42m 30s
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
02:42:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,832.015 km
Perigee altitude
586.609 km
Semi-major axis
16,087.449 km
Eccentricity
0.56707
Inclination
65.1226°
RAAN
85.6152°
Arg. of periapsis
32.8585°
True anomaly
327.00627°
Mean anomaly
352.1803°
Eccentric anomaly
342.30447°
Mean motion
1.06368 °/min
Orbital period
338.45 mins
BSTAR
0.000056373
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