SL-12 R/B(2), 21019

Orbit data source: Space-Track

SL-12 R/B(2), 21019 is space debris in GEO originally from a launch on Thu, 20 Dec 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.

Not visible in the next 10 days
Identifier
21019, 1990-112D
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)
1990-12-20 (36 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.6 m
Radar Cross Section
23.597 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 21019U 90112D   26269.96455396 -.00000177  00000-0  00000-0 0  9994
2 21019  12.8080 337.3645 0025870 188.9269 276.0043  1.00011173120953
Epoch: 2026-09-26T23:08Z
TLE epoch observation values (Epoch: 2026-09-26T23:08:57.462Z)
Latitude
12.38381°
Longitude
89.33141°
Altitude
35,847.886 km
Speed
3.073 km/s
True Right ascension
05h 29m 20s
True Declination
12° 22' 18"
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
02:09:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,970.076 km
Perigee altitude
35,751.532 km
Semi-major axis
42,238.941 km
Eccentricity
0.00259
Inclination
12.808°
RAAN
337.3645°
Arg. of periapsis
188.9269°
True anomaly
275.70938°
Mean anomaly
276.0043°
Eccentric anomaly
275.85685°
Mean motion
0.25002 °/min
Orbital period
1,439.89 mins
BSTAR
0
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