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: 17 hours ago

TLE from 17 hours ago
0 SL-12 R/B(AUX MOTOR)
1 19856U 89001H   25257.78088474  .00000032  00000-0  41509-3 0  9991
2 19856  65.1267 118.7048 5663087  37.1882 351.1591  4.25417645568812
Epoch: 2025-09-14T18:44Z
TLE epoch observation values (Epoch: 2025-09-14T18:44:28.441Z)
Latitude
0.0001°
Longitude
-156.40465°
Altitude
1,148.229 km
Speed
9.009 km/s
True Right ascension
07h 54m 50s
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
04:04:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,820.178 km
Perigee altitude
598.961 km
Semi-major axis
16,087.707 km
Eccentricity
0.56631
Inclination
65.1267°
RAAN
118.7048°
Arg. of periapsis
37.1882°
True anomaly
323.18053°
Mean anomaly
351.1591°
Eccentric anomaly
340.1316°
Mean motion
1.06366 °/min
Orbital period
338.45 mins
BSTAR
0.00041509
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