SL-12 R/B(2), 28139
Orbit data source: Space-Track
SL-12 R/B(2), 28139 is space debris in GEO originally from a launch on Sun, 28 Dec 2003 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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28139 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 28139U 03060D 25304.76802385 -.00000029 00000-0 00000-0 0 9997
2 28139 13.3684 15.4100 0019834 226.4054 144.0007 1.00220002 79749Epoch: 2025-10-31T18:25Z
TLE epoch observation values (Epoch: 2025-10-31T18:25:57.260Z)
Latitude
2.427°
Longitude
68.84172°
Altitude
35,868.446 km
Speed
3.069 km/s
True Right ascension
01h 42m 33s
True Declination
2° 25' 28"
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
08:55:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,885.764 km
Perigee altitude
35,718.444 km
Semi-major axis
42,180.241 km
Eccentricity
0.00198
Inclination
13.3684°
RAAN
15.41°
Arg. of periapsis
226.4054°
True anomaly
144.13402°
Mean anomaly
144.0007°
Eccentric anomaly
144.06739°
Mean motion
0.25054 °/min
Orbital period
1,436.89 mins
BSTAR
0
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Other satellites on launch #60 in the year 2003 (2003-12-28 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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28139 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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