DELTA 1 R/B(2) *, 11792
Orbit data source: Space-Track
DELTA 1 R/B(2) *, 11792 is space debris in HEO originally from a launch on Wed, 26 Oct 1966 UTC launched from the Air Force Eastern Test Range (AFETR). 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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11792 intel report (Beta)
DELTA 1 R/B(2) * details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 16 hours ago |
| Origin | |
| Manufacturer | Unknown |
| Mission | Spacecraft |
| Bus & Motor | Unknown |
| Mass | Unknown |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl, 1.5 m |
| Radar Cross Section | 0.687 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 16 hours ago
0 DELTA 1 R/B(2) *
1 11792U 66096C 25036.12268704 .00012922 00000-0 19474-1 0 9995
2 11792 17.9232 60.7045 6121340 323.1491 7.3571 3.73477960412509Epoch: 2025-02-05T02:56Z
Definitive object data (Epoch: 2025-02-05T02:56:40.16Z)
| Latitude | 0.00001° |
| Longitude | -118.95919° |
| Altitude | 996.169 km |
| Speed | 9.24 km/s |
| True Right ascension | 04h 02m 54s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 10.40695° |
| Longitude | 26.01576° |
| Altitude | 21,898.895 km |
| Speed | 2.341 km/s |
| Apparent Right ascension | 13h 06m 53s |
| Apparent Declination | 1° 58' 57" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 20:57:16 |
| Azimuth | 290.072° WNW |
| Elevation | -19.446° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 21,918.471 km |
| Perigee altitude | 429.791 km |
| Semi-major axis | 17,552.268 km |
| Eccentricity | 0.612134 |
| Inclination | 17.9232° |
| RAAN | 60.7045° |
| Arg. of periapsis | 323.1491° |
| True anomaly | 36.67156° |
| Mean anomaly | 7.3571° |
| Eccentric anomaly | 18.46622° |
| Mean motion | 0.93335 °/min |
| BSTAR | 0.019474 |
| Orbital period | 385.71 mins |
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Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)
| INTELSAT 2-F1, 2514 |
| DELTA 1 R/B(1), 2515 (Decayed) |
| DELTA 1 R/B(2) *, 11792 |
DELTA 1 R/B(2) * 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. |
|---|---|---|---|---|---|---|---|
| 246 mins | 2025-02-06 04:47:03.767Z | 205.853° SW | 2025-02-06 05:04:03.767Z | 142.61° SSE | 31.902° | 2025-02-06 08:53:03.767Z | 105.793° ESE |
| 295 mins | 2025-02-06 11:50:03.767Z | 265.966° W | 2025-02-06 13:35:03.767Z | 242.827° WSW | 29.863° | 2025-02-06 16:45:03.767Z | 187.972° SSW |
Authenticating...
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