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.
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21019 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 SL-12 R/B(2)
1 21019U 90112D 25260.80878385 .00000050 00000-0 00000-0 0 9993
2 21019 13.1401 339.9780 0027659 178.6598 189.3573 1.00011440117216
Epoch: 2025-09-17T19:24Z
TLE epoch observation values (Epoch: 2025-09-17T19:24:38.924Z)
Latitude
1.79859°
Longitude
59.59229°
Altitude
35,974.934 km
Speed
3.064 km/s
True Right ascension
23h 10m 56s
True Declination
1° 47' 48"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:26:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,977.554 km
Perigee altitude
35,743.897 km
Semi-major axis
42,238.862 km
Eccentricity
0.00277
Inclination
13.1401°
RAAN
339.978°
Arg. of periapsis
178.6598°
True anomaly
189.30594°
Mean anomaly
189.3573°
Eccentric anomaly
189.3316°
Mean motion
0.25002 °/min
Orbital period
1,439.88 mins
BSTAR
0
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Other satellites on launch #112 in the year 1990 (1990-12-20 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SL-12 R/B(2) Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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SL-12 R/B(2) is likely not visible in the next few days. |
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21019 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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