SL-12 R/B(AUX MOTOR), 29680
Orbit data source: Space-Track
SL-12 R/B(AUX MOTOR), 29680 is space debris in HEO originally from a launch on Mon, 25 Dec 2006 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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29680 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SL-12 R/B(AUX MOTOR)
1 29680U 06062G   25303.03576029  .00000230  00000-0  52697-3 0  9991
2 29680  65.1545 118.2174 5699188 222.2190  76.1019  4.25863716190636Epoch: 2025-10-30T00:51Z
TLE epoch observation values (Epoch: 2025-10-30T00:51:29.689Z)
Latitude
0°
Longitude
66.7245°
Altitude
12,416.199 km
Speed
4.199 km/s
True Right ascension
07h 52m 47s
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
00:26:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,860.593 km
Perigee altitude
536.044 km
Semi-major axis
16,076.456 km
Eccentricity
0.56992
Inclination
65.1545°
RAAN
118.2174°
Arg. of periapsis
222.219°
True anomaly
137.85559°
Mean anomaly
76.1019°
Eccentric anomaly
107.2817°
Mean motion
1.06477 °/min
Orbital period
338.1 mins
BSTAR
0.00052697
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Other satellites on launch #62 in the year 2006 (2006-12-25 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. | 
|---|---|---|---|---|---|---|---|
| 238 mins | 2025-10-31 10:21:51.699Z | 154.587° SSE | 2025-10-31 12:29:51.699Z | 79.239° E | 43.337° | 2025-10-31 14:19:51.699Z | 35.391° NE | 
| 227 mins | 2025-10-31 16:38:51.699Z | 259.945° W | 2025-10-31 20:03:51.699Z | 19.368° NNE | 39.032° | 2025-10-31 20:25:51.699Z | 96.113° ESE | 
| 35 mins | 2025-11-01 01:28:51.699Z | 328.628° NNW | 2025-11-01 01:52:51.699Z | 300.302° NW | 16.932° | 2025-11-01 02:03:51.699Z | 265.807° W | 
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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| 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 ascending order | 
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