SL-12 R/B(2), 16339
Orbit data source: Space-Track
SL-12 R/B(2), 16339 is space debris in GEO originally from a launch on Fri, 15 Nov 1985 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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16339 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 SL-12 R/B(2)
1 16339U 85107F 25260.71923697 -.00000058 00000-0 00000-0 0 9996
2 16339 11.5096 324.5654 0017619 124.9482 232.5079 0.97493750124716
Epoch: 2025-09-17T17:15Z
TLE epoch observation values (Epoch: 2025-09-17T17:15:42.074Z)
Latitude
-0.54375°
Longitude
66.09936°
Altitude
36,629.493 km
Speed
3.043 km/s
True Right ascension
21h 27m 39s
True Declination
0° 32' 36"
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
22:01:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,660.5 km
Perigee altitude
36,509.107 km
Semi-major axis
42,962.941 km
Eccentricity
0.00176
Inclination
11.5096°
RAAN
324.5654°
Arg. of periapsis
124.9482°
True anomaly
232.34792°
Mean anomaly
232.5079°
Eccentric anomaly
232.42789°
Mean motion
0.24373 °/min
Orbital period
1,477.07 mins
BSTAR
0
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Other satellites on launch #107 in the year 1985 (1985-11-15 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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16339 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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