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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Edit Public Description
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 25255.47647837 -.00000116 00000-0 00000-0 0 9992
2 18446 11.1855 327.5056 0023420 256.0478 101.4965 1.00254578127218
Epoch: 2025-09-12T11:26Z
TLE epoch observation values (Epoch: 2025-09-12T11:26:07.731Z)
Latitude
-0.42641°
Longitude
162.1°
Altitude
35,811.28 km
Speed
3.073 km/s
True Right ascension
21h 41m 25s
True Declination
0° 25' 34"
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
17:53:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,891.194 km
Perigee altitude
35,693.667 km
Semi-major axis
42,170.568 km
Eccentricity
0.00234
Inclination
11.1855°
RAAN
327.5056°
Arg. of periapsis
256.0478°
True anomaly
101.75933°
Mean anomaly
101.4965°
Eccentric anomaly
101.62793°
Mean motion
0.25063 °/min
Orbital period
1,436.39 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
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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