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 (38 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, Large (>1 m²)

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 19856U 89001H   26253.34906112 -.00000117  00000-0 -80935-5 0  9992
2 19856  65.1284 349.7415 5678827  19.9315 355.3773  4.25462445584153
Epoch: 2026-09-10T08:22Z
TLE epoch observation values (Epoch: 2026-09-10T08:22:38.880Z)
Latitude
-0.00014°
Longitude
-125.30316°
Altitude
721.167 km
Speed
9.356 km/s
True Right ascension
23h 18m 59s
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
04:28:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,843.722 km
Perigee altitude
573.149 km
Semi-major axis
16,086.573 km
Eccentricity
0.56788
Inclination
65.1284°
RAAN
349.7415°
Arg. of periapsis
19.9315°
True anomaly
339.92429°
Mean anomaly
355.3773°
Eccentric anomaly
349.38195°
Mean motion
1.06377 °/min
Orbital period
338.42 mins
BSTAR
-0.0000080935
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