SL-12 R/B(AUX MOTOR), 20630

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 20630 is space debris in HEO originally from a launch on Sat, 19 May 1990 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
20630, 1990-045F
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)
1990-05-19 (36 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: 2 days ago

TLE from 2 days ago
0 SL-12 R/B(AUX MOTOR)
1 20630U 90045F   26171.38130311  .00000008  00000-0 -40410-4 0  9998
2 20630  65.0914 238.3974 5650479  42.6125 349.5810  4.32089392566153
Epoch: 2026-06-20T09:09Z
TLE epoch observation values (Epoch: 2026-06-20T09:09:04.588Z)
Latitude
-0.00008°
Longitude
-167.46238°
Altitude
1,269.683 km
Speed
8.901 km/s
True Right ascension
15h 53m 36s
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
23:08:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,540.02 km
Perigee altitude
547.021 km
Semi-major axis
15,921.658 km
Eccentricity
0.56505
Inclination
65.0914°
RAAN
238.3974°
Arg. of periapsis
42.6125°
True anomaly
317.5476°
Mean anomaly
349.581°
Eccentric anomaly
336.85657°
Mean motion
1.08034 °/min
Orbital period
333.23 mins
BSTAR
-0.00004041
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