SL-12 R/B(AUX MOTOR), 29682
Orbit data source: Space-Track
SL-12 R/B(AUX MOTOR), 29682 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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29682 intel report (Beta)
SL-12 R/B(AUX MOTOR) details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 4 days ago |
| Origin | |
| Manufacturer | RKKE |
| Mission | Spacecraft |
| Bus & Motor | SOZ, Unknown motor |
| Mass | 56 kg wet, 56 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl, 1.1 m |
| Radar Cross Section | 0.660 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 4 days ago
0 SL-12 R/B(AUX MOTOR)
1 29682U 06062H 24357.04523106 .00000083 00000-0 14548-3 0 9999
2 29682 65.1725 206.3086 5554468 279.2299 24.9925 4.25369113278515Epoch: 2024-12-22T01:05Z
Definitive object data (Epoch: 2024-12-22T01:05:07.963Z)
| Latitude | -0.00023° |
| Longitude | 98.94608° |
| Altitude | 3,851.068 km |
| Speed | 7.292 km/s |
| True Right ascension | 13h 45m 16s |
| True Declination | 0° 00' 01" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 39.40984° |
| Longitude | -104.86874° |
| Altitude | 13,698.27 km |
| Speed | 3.867 km/s |
| Apparent Right ascension | 23h 37m 43s |
| Apparent Declination | 23° 39' 28" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:52:07 |
| Azimuth | 333.975° NNW |
| Elevation | -21.824° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 18,647.379 km |
| Perigee altitude | 774.26 km |
| Semi-major axis | 16,088.956 km |
| Eccentricity | 0.5554468 |
| Inclination | 65.1725° |
| RAAN | 206.3086° |
| Arg. of periapsis | 279.2299° |
| True anomaly | 80.91451° |
| Mean anomaly | 24.9925° |
| Eccentric anomaly | 49.01723° |
| Mean motion | 1.06353 °/min |
| BSTAR | 0.00014548 |
| Orbital period | 338.49 mins |
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Other satellites on launch #62 in the year 2006 (2006-12-25 UTC)
SL-12 R/B(AUX MOTOR) Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 159 mins | 2024-12-26 12:20:55.151Z | 130.175° SE | 2024-12-26 12:56:55.151Z | 68.045° E | 32.28° | 2024-12-26 14:59:55.151Z | 29.532° NE |
| 260 mins | 2024-12-26 18:06:55.151Z | 257.236° W | 2024-12-26 19:27:55.151Z | 344.274° N | 40.001° | 2024-12-26 22:26:55.151Z | 106.523° ESE |
| 201 mins | 2024-12-27 00:54:55.151Z | 327.656° NNW | 2024-12-27 03:16:55.151Z | 290.888° WNW | 36.191° | 2024-12-27 04:15:55.151Z | 222.442° SW |
Authenticating...
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