SL-12 R/B(2), 20028

Orbit data source: Space-Track

SL-12 R/B(2), 20028 is space debris in MEO originally from a launch on Wed, 31 May 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
20028, 1989-039E
Orbit
MEO
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)
1989-05-31 (37 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
23.684 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(2)
1 20028U 89039E   25344.59336119 -.00000050  00000-0  00000+0 0  9991
2 20028  65.0187 315.6765 0008628 286.0941 287.0722  2.13485199270300
Epoch: 2025-12-10T14:14Z
TLE epoch observation values (Epoch: 2025-12-10T14:14:26.406Z)
Latitude
-29.73791°
Longitude
-142.09371°
Altitude
19,102.203 km
Speed
3.956 km/s
True Right ascension
10h 04m 18s
True Declination
-29° 41' 47"
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
17:02:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,120.95 km
Perigee altitude
19,076.986 km
Semi-major axis
25,477.105 km
Eccentricity
0.00086
Inclination
65.0187°
RAAN
315.6765°
Arg. of periapsis
286.0941°
True anomaly
286.97766°
Mean anomaly
287.0722°
Eccentric anomaly
287.02493°
Mean motion
0.53373 °/min
Orbital period
674.5 mins
BSTAR
0
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