SL-12 R/B(2), 13630
Orbit data source: Space-Track
SL-12 R/B(2), 13630 is space debris in GEO originally from a launch on Wed, 20 Oct 1982 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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13630 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 SL-12 R/B(2)
1 13630U 82103E 25348.86341704 -.00000283 00000-0 00000-0 0 9996
2 13630 7.7021 303.0827 0011210 194.9016 352.4295 1.00400460119657Epoch: 2025-12-14T20:43Z
TLE epoch observation values (Epoch: 2025-12-14T20:43:19.232Z)
Latitude
-0.97491°
Longitude
95.70762°
Altitude
35,703.494 km
Speed
3.079 km/s
True Right ascension
08h 41m 13s
True Declination
0° 58' 26"
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
13:25:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,798.832 km
Perigee altitude
35,704.377 km
Semi-major axis
42,129.741 km
Eccentricity
0.00112
Inclination
7.7021°
RAAN
303.0827°
Arg. of periapsis
194.9016°
True anomaly
352.41255°
Mean anomaly
352.4295°
Eccentric anomaly
352.42103°
Mean motion
0.25099 °/min
Orbital period
1,434.31 mins
BSTAR
0
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Other satellites on launch #103 in the year 1982 (1982-10-20 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. |
|---|---|---|---|---|---|---|---|
| SL-12 R/B(2) is likely not visible in the next few days. |
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13630 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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