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
Last TLE update
8 hours ago
Origin
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 (35 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

TLE from 8 hours ago
0 SL-12 R/B(2)
1 21019U 90112D   25199.64045146 -.00000362  00000-0  00000-0 0  9994
2 21019  13.1932 340.4158 0027504 174.6828 129.0529  1.00024523116590
Epoch: 2025-07-18T15:22Z
TLE epoch observation values (Epoch: 2025-07-18T15:22:15.006Z)
Latitude
-10.93109°
Longitude
117.8505°
Altitude
35,931.526 km
Speed
3.067 km/s
True Right ascension
19h 00m 24s
True Declination
-10° 55' 13"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
12.23533°
Longitude
-119.35958°
Altitude
35,887.561 km
Speed
3.07 km/s
Apparent Right ascension
02h 55m 16s
Apparent Declination
6° 10' 09"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:28:07
Azimuth
314.899° NW
Elevation
-32.801°
Doppler factor
1
Orbital elements
Apogee altitude
35,973.205 km
Perigee altitude
35,740.878 km
Semi-major axis
42,235.178 km
Eccentricity
0.00275
Inclination
13.1932°
RAAN
340.4158°
Arg. of periapsis
174.6828°
True anomaly
129.29712°
Mean anomaly
129.0529°
Eccentric anomaly
129.17506°
Mean motion
0.25005 °/min
Orbital period
1,439.7 mins
BSTAR
0
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