SL-6 R/B(2), 20666

Orbit data source: Space-Track

SL-6 R/B(2), 20666 is space debris in LEO originally from a launch on Thu, 21 Jun 1990 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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
20666, 1990-055D
Orbit
LEO
Last TLE update
6 hours ago
Origin
Manufacturer
NPO Energiya
Mission
Spacecraft
Bus & Motor
BLOK-L, Unknown motor
Mass
900 kg wet, 900 kg dry
Launch date (UTC)
1990-06-21 (35 years ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.6 m
Radar Cross Section
8.039 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 6 hours ago
0 SL-6 R/B(2)
1 20666U 90055D   25198.49081492  .00001533  00000-0  13048-3 0  9992
2 20666  62.7842 332.7303 0021766 199.8270 160.1985 15.02133052902845
Epoch: 2025-07-17T11:46Z
TLE epoch observation values (Epoch: 2025-07-17T11:46:46.409Z)
Latitude
-0.00001°
Longitude
-139.51894°
Altitude
576.377 km
Speed
7.565 km/s
True Right ascension
22h 10m 55s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
-18.39725°
Longitude
-150.20366°
Altitude
577.793 km
Speed
7.565 km/s
Apparent Right ascension
20h 20m 14s
Apparent Declination
-30° 01' 54"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
06:47:28
Azimuth
290.4° WNW
Elevation
-68.671°
Doppler factor
1
Orbital elements
Apogee altitude
574.242 km
Perigee altitude
544.043 km
Semi-major axis
6,937.279 km
Eccentricity
0.00218
Inclination
62.7842°
RAAN
332.7303°
Arg. of periapsis
199.827°
True anomaly
Unknown
Mean anomaly
160.1985°
Eccentric anomaly
Unknown
Mean motion
3.75629 °/min
Orbital period
95.84 mins
BSTAR
0.00013048
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