SL-12 R/B(2), 18634
Orbit data source: Space-Track
SL-12 R/B(2), 18634 is space debris in GEO originally from a launch on Thu, 10 Dec 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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18634 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SL-12 R/B(2)
1 18634U 87100D 25261.00610657 -.00000070 00000-0 00000-0 0 9997
2 18634 10.1648 321.6278 0017751 259.3589 113.1039 1.03399881142664
Epoch: 2025-09-18T00:08Z
TLE epoch observation values (Epoch: 2025-09-18T00:08:47.607Z)
Latitude
2.21379°
Longitude
-25.27094°
Altitude
34,960.276 km
Speed
3.104 km/s
True Right ascension
22h 16m 24s
True Declination
2° 12' 41"
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
18:28:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,006.231 km
Perigee altitude
34,859.569 km
Semi-major axis
41,311.037 km
Eccentricity
0.00178
Inclination
10.1648°
RAAN
321.6278°
Arg. of periapsis
259.3589°
True anomaly
113.29083°
Mean anomaly
113.1039°
Eccentric anomaly
113.19738°
Mean motion
0.25849 °/min
Orbital period
1,392.7 mins
BSTAR
0
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Other satellites on launch #100 in the year 1987 (1987-12-10 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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18634 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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