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)
SL-12 R/B(AUX MOTOR) details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 1 day 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 1 day ago
0 SL-12 R/B(AUX MOTOR)
1 29680U 06062G 24360.22378961 .00000113 00000-0 33397-3 0 9995
2 29680 65.1549 228.2555 5622851 237.7858 55.5245 4.25820765177487Epoch: 2024-12-25T05:22Z
Definitive object data (Epoch: 2024-12-25T05:22:15.422Z)
| Latitude | -0.00002° |
| Longitude | 53.47524° |
| Altitude | 9,338.225 km |
| Speed | 5.093 km/s |
| True Right ascension | 15h 13m 02s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 32.16933° |
| Longitude | 69.94976° |
| Altitude | 16,630.774 km |
| Speed | 3.141 km/s |
| Apparent Right ascension | 17h 13m 39s |
| Apparent Declination | 21° 36' 60" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:54:14 |
| Azimuth | 60.977° ENE |
| Elevation | -0.331° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 18,739.594 km |
| Perigee altitude | 659.25 km |
| Semi-major axis | 16,077.559 km |
| Eccentricity | 0.5622851 |
| Inclination | 65.1549° |
| RAAN | 228.2555° |
| Arg. of periapsis | 237.7858° |
| True anomaly | 122.30329° |
| Mean anomaly | 55.5245° |
| Eccentric anomaly | 87.71546° |
| Mean motion | 1.06467 °/min |
| BSTAR | 0.00033397 |
| Orbital period | 338.13 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. |
|---|---|---|---|---|---|---|---|
| 47 mins | 2024-12-26 11:29:02.508Z | 44.616° NE | 2024-12-26 11:54:02.508Z | 37.021° NE | 11.179° | 2024-12-26 12:16:02.508Z | 29.96° NE |
| 242 mins | 2024-12-26 15:01:02.508Z | 170.385° S | 2024-12-26 16:34:02.508Z | 85.672° E | 44.373° | 2024-12-26 19:03:02.508Z | 41.694° NE |
| 224 mins | 2024-12-26 21:31:02.508Z | 280.123° WNW | 2024-12-27 00:52:02.508Z | 40.946° NE | 42.853° | 2024-12-27 01:15:02.508Z | 123.594° SE |
| 41 mins | 2024-12-27 05:58:02.508Z | 330.897° NNW | 2024-12-27 06:24:02.508Z | 312.634° NW | 13.213° | 2024-12-27 06:39:02.508Z | 291.813° WNW |
Authenticating...
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