SL-12 R/B(2), 18446
Orbit data source: Space-Track
SL-12 R/B(2), 18446 is space debris in GEO originally from a launch on Wed, 28 Oct 1987 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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18446 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 SL-12 R/B(2)
1 18446U 87091D 26251.00707122 -.00000273 00000-0 00000-0 0 9996
2 18446 10.6734 325.2027 0023310 267.9558 211.7270 1.00151362130832Epoch: 2026-09-08T00:10Z
TLE epoch observation values (Epoch: 2026-09-08T00:10:10.953Z)
Latitude
9.27184°
Longitude
95.56847°
Altitude
35,902.468 km
Speed
3.068 km/s
True Right ascension
05h 40m 46s
True Declination
9° 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
07:53:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,919.771 km
Perigee altitude
35,723.036 km
Semi-major axis
42,199.541 km
Eccentricity
0.00233
Inclination
10.6734°
RAAN
325.2027°
Arg. of periapsis
267.9558°
True anomaly
211.58688°
Mean anomaly
211.727°
Eccentric anomaly
211.65691°
Mean motion
0.25037 °/min
Orbital period
1,437.87 mins
BSTAR
0
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Other satellites on launch #91 in the year 1987 (1987-10-28 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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18446 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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