SL-12 R/B(AUX MOTOR), 28920
Orbit data source: Space-Track
SL-12 R/B(AUX MOTOR), 28920 is space debris in HEO originally from a launch on Sun, 25 Dec 2005 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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28920 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 SL-12 R/B(AUX MOTOR)
1 28920U 05050F 26043.67033953 .00001499 00000-0 10852-2 0 9993
2 28920 65.0228 111.1865 5832105 171.9709 204.6928 4.21410426309981Epoch: 2026-02-12T16:05Z
TLE epoch observation values (Epoch: 2026-02-12T16:05:17.335Z)
Latitude
-0.00004°
Longitude
87.14832°
Altitude
18,906.772 km
Speed
2.629 km/s
True Right ascension
07h 24m 45s
True Declination
0° 00' 00"
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
07:17:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,253.259 km
Perigee altitude
369.479 km
Semi-major axis
16,189.506 km
Eccentricity
0.58321
Inclination
65.0228°
RAAN
111.1865°
Arg. of periapsis
171.9709°
True anomaly
188.07626°
Mean anomaly
204.6928°
Eccentric anomaly
195.66833°
Mean motion
1.05364 °/min
Orbital period
341.67 mins
BSTAR
0.0010852
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Other satellites on launch #50 in the year 2005 (2005-12-25 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(AUX MOTOR) Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 45 mins | 2026-02-13 04:44:56.160Z | 119.664° SE | 2026-02-13 04:53:56.160Z | 101.564° ESE | 42.453° | 2026-02-13 05:29:56.160Z | 35.233° NE |
| 86 mins | 2026-02-13 09:57:56.160Z | 269.942° W | 2026-02-13 11:12:56.160Z | 340.591° N | 27.726° | 2026-02-13 11:23:56.160Z | 41.35° NE |
| 158 mins | 2026-02-14 01:35:56.160Z | 134.081° SE | 2026-02-14 03:36:56.160Z | 92.925° ESE | 36.446° | 2026-02-14 04:13:56.160Z | 38.267° NE |
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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