SL-12 R/B(2), 20266

Orbit data source: Space-Track

SL-12 R/B(2), 20266 is space debris in GEO originally from a launch on Thu, 28 Sep 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
20266, 1989-081D
Orbit
GEO
Country
Flag of CISCIS
Related business
Manufacturer
NPO Energiya
Mission
Spacecraft
Bus & Motor
BLOK DM, Unknown motor
Mass
2,440 kg wet, 2,440 kg dry
Launch date (UTC)
1989-09-28 (36 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.1 m
Radar Cross Section
23.597 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 SL-12 R/B(2)
1 20266U 89081D   25312.51649345 -.00000291  00000-0  00000+0 0  9994
2 20266  12.1283 334.3640 0025652 124.2385  60.3428  1.00613733117133
Epoch: 2025-11-08T12:23Z
TLE epoch observation values (Epoch: 2025-11-08T12:23:45.034Z)
Latitude
-1.02728°
Longitude
-74.8011°
Altitude
35,637.981 km
Speed
3.082 km/s
True Right ascension
10h 36m 19s
True Declination
-1° 01' 34"
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
21:35:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,799.928 km
Perigee altitude
35,584.091 km
Semi-major axis
42,070.147 km
Eccentricity
0.00257
Inclination
12.1283°
RAAN
334.364°
Arg. of periapsis
124.2385°
True anomaly
60.59865°
Mean anomaly
60.3428°
Eccentric anomaly
60.47068°
Mean motion
0.25153 °/min
Orbital period
1,431.27 mins
BSTAR
0
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