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: 9 hours ago
TLE from 9 hours ago
0 SL-12 R/B(2)
1 21703U 91064B 26121.64130475 .00000018 00000-0 00000+0 0 9993
2 21703 13.3626 340.2770 0003192 13.4746 165.3004 0.99881574119684Epoch: 2026-05-01T15:23Z
TLE epoch observation values (Epoch: 2026-05-01T15:23:28.730Z)
Latitude
0.26312°
Longitude
68.66956°
Altitude
35,908.889 km
Speed
3.07 km/s
True Right ascension
10h 36m 26s
True Declination
0° 15' 46"
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
07:49:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,910.82 km
Perigee altitude
35,883.831 km
Semi-major axis
42,275.463 km
Eccentricity
0.00032
Inclination
13.3626°
RAAN
340.277°
Arg. of periapsis
13.4746°
True anomaly
165.30968°
Mean anomaly
165.3004°
Eccentric anomaly
165.30504°
Mean motion
0.2497 °/min
Orbital period
1,441.76 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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