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: 3 days ago

TLE from 3 days ago
0 SL-12 R/B(AUX MOTOR)
1 19755U 89001G   26170.80378785 -.00000046  00000-0  39231-3 0  9999
2 19755  65.2799   9.2969 5551881  76.8594 336.9779  4.25608160581228
Epoch: 2026-06-19T19:17Z
TLE epoch observation values (Epoch: 2026-06-19T19:17:27.270Z)
Latitude
0.00001°
Longitude
171.90745°
Altitude
3,487.225 km
Speed
7.486 km/s
True Right ascension
00h 37m 11s
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
23:20:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,633.831 km
Perigee altitude
775.738 km
Semi-major axis
16,082.921 km
Eccentricity
0.55519
Inclination
65.2799°
RAAN
9.2969°
Arg. of periapsis
76.8594°
True anomaly
283.33347°
Mean anomaly
336.9779°
Eccentric anomaly
314.15599°
Mean motion
1.06413 °/min
Orbital period
338.3 mins
BSTAR
0.00039231
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