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: 13 hours ago

TLE from 13 hours ago
0 SL-12 R/B(AUX MOTOR)
1 19856U 89001H   26074.01164022  .00000117  00000-0  45036-3 0  9992
2 19856  65.1563  53.9339 5673551  28.6292 353.2688  4.25442516576523
Epoch: 2026-03-15T00:16Z
TLE epoch observation values (Epoch: 2026-03-15T00:16:45.715Z)
Latitude
-0.00013°
Longitude
-122.89763°
Altitude
907.483 km
Speed
9.202 km/s
True Right ascension
03h 35m 40s
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
17:38:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,836.02 km
Perigee altitude
581.853 km
Semi-major axis
16,087.074 km
Eccentricity
0.56736
Inclination
65.1563°
RAAN
53.9339°
Arg. of periapsis
28.6292°
True anomaly
331.28293°
Mean anomaly
353.2688°
Eccentric anomaly
344.68027°
Mean motion
1.06372 °/min
Orbital period
338.43 mins
BSTAR
0.00045036
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