SL-12 R/B(AUX MOTOR), 32281
Orbit data source: Space-Track
SL-12 R/B(AUX MOTOR), 32281 is space debris in HEO originally from a launch on Fri, 26 Oct 2007 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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32281 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 SL-12 R/B(AUX MOTOR)
1 32281U 07052G 25303.46789089 .00000025 00000-0 56099-3 0 9993
2 32281 65.3223 21.1944 5678624 213.5168 92.3551 4.23717686278189Epoch: 2025-10-30T11:13Z
TLE epoch observation values (Epoch: 2025-10-30T11:13:45.772Z)
Latitude
-0.00008°
Longitude
173.73927°
Altitude
14,396.238 km
Speed
3.697 km/s
True Right ascension
01h 24m 49s
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
23:06:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,912.565 km
Perigee altitude
592.541 km
Semi-major axis
16,130.69 km
Eccentricity
0.56786
Inclination
65.3223°
RAAN
21.1944°
Arg. of periapsis
213.5168°
True anomaly
146.54013°
Mean anomaly
92.3551°
Eccentric anomaly
120.41394°
Mean motion
1.05941 °/min
Orbital period
339.81 mins
BSTAR
0.00056099
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Other satellites on launch #52 in the year 2007 (2007-10-26 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. |
|---|---|---|---|---|---|---|---|
| 89 mins | 2025-11-02 03:20:01.510Z | 74.752° E | 2025-11-02 03:40:01.510Z | 65.398° ENE | 31.288° | 2025-11-02 04:49:01.510Z | 30.046° NE |
| 247 mins | 2025-11-02 06:49:01.510Z | 208.928° SW | 2025-11-02 09:35:01.510Z | 303.78° NW | 40.853° | 2025-11-02 10:56:01.510Z | 52.603° ENE |
| 64 mins | 2025-11-02 15:49:01.510Z | 326.148° NNW | 2025-11-02 16:44:01.510Z | 256.274° W | 43.027° | 2025-11-02 16:53:01.510Z | 172.984° S |
| 127 mins | 2025-11-03 01:12:01.510Z | 80.323° E | 2025-11-03 02:28:01.510Z | 56.09° ENE | 21.169° | 2025-11-03 03:19:01.510Z | 30.777° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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