SL-12 R/B(2), 21703
Orbit data source: Space-Track
SL-12 R/B(2), 21703 is space debris in GEO originally from a launch on Fri, 13 Sep 1991 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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21703 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 SL-12 R/B(2)
1 21703U 91064B 26065.72544876 -.00000308 00000-0 00000+0 0 9996
2 21703 13.4072 340.6730 0003169 0.1630 230.5887 0.99900806119122Epoch: 2026-03-06T17:24Z
TLE epoch observation values (Epoch: 2026-03-06T17:24:38.772Z)
Latitude
-10.34296°
Longitude
145.02824°
Altitude
35,901.03 km
Speed
3.07 km/s
True Right ascension
14h 02m 35s
True Declination
-10° 19' 58"
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
10:25:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,905.295 km
Perigee altitude
35,878.504 km
Semi-major axis
42,270.036 km
Eccentricity
0.00032
Inclination
13.4072°
RAAN
340.673°
Arg. of periapsis
0.163°
True anomaly
230.56065°
Mean anomaly
230.5887°
Eccentric anomaly
230.57467°
Mean motion
0.24974 °/min
Orbital period
1,441.48 mins
BSTAR
0
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Other satellites on launch #64 in the year 1991 (1991-09-13 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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21703 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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