DELTA 1 R/B(2), 11984
Orbit data source: Space-Track
DELTA 1 R/B(2), 11984 is space debris in LEO originally from a launch on Thu, 23 Mar 1967 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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11984 intel report (Beta)
DELTA 1 R/B(2) details
Identifier | |
Orbit | LEO |
Last TLE update | 9 hours ago |
Origin | |
Manufacturer | UTC |
Mission | Spacecraft |
Bus & Motor | FW4, Unknown motor |
Mass | 35 kg wet, 35 kg dry |
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 9 hours ago
0 DELTA 1 R/B(2)
1 11984U 67026C 24356.18680293 .00657297 -45081-5 38545-2 0 9998
2 11984 26.0383 70.8878 2073517 217.1096 126.6551 11.47266763533365
Epoch: 2024-12-21T04:28Z
Definitive object data (Epoch: 2024-12-21T04:28:59.773Z)
Latitude | 0.00001° |
Longitude | -86.6028° |
Altitude | 3,142.393 km |
Speed | 5.98 km/s |
True Right ascension | 04h 43m 33s |
True Declination | 0° 00' 00" |
Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
Latitude | 22.94016° |
Longitude | 32.31899° |
Altitude | 1,918.421 km |
Speed | 6.937 km/s |
Apparent Right ascension | 12h 25m 13s |
Apparent Declination | -17° 12' 25" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 12:47:06 |
Azimuth | 186.207° SSW |
Elevation | 32.65° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 3,652.695 km |
Perigee altitude | 207.286 km |
Semi-major axis | 8,308.128 km |
Eccentricity | 0.2073517 |
Inclination | 26.0383° |
RAAN | 70.8878° |
Arg. of periapsis | 217.1096° |
True anomaly | 142.93596° |
Mean anomaly | 126.6551° |
Eccentric anomaly | 135.04866° |
Mean motion | 2.86608 °/min |
BSTAR | 0.0038545 |
Orbital period | 125.61 mins |
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Other satellites on launch #26 in the year 1967 (1967-03-23 UTC)
INTELSAT 2-F3, 2717 |
DELTA 1 R/B(1), 2719 (Decayed) |
DELTA 1 R/B(2), 11984 |
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. |
---|---|---|---|---|---|---|---|
6 mins | 2024-12-21 13:45:05.391Z | 186.18° SSW | 2024-12-21 13:45:05.391Z | 186.18° SSW | 28.226° | 2024-12-21 13:51:05.391Z | 145.199° SSE |
24 mins | 2024-12-22 05:34:05.391Z | 175.181° S | 2024-12-22 05:45:05.391Z | 140.681° SSE | 18.542° | 2024-12-22 05:58:05.391Z | 105.099° ESE |
35 mins | 2024-12-22 07:44:05.391Z | 215.167° SW | 2024-12-22 08:02:05.391Z | 156.511° SSE | 32.454° | 2024-12-22 08:19:05.391Z | 98.815° ESE |
34 mins | 2024-12-22 10:00:05.391Z | 241.574° WSW | 2024-12-22 10:20:05.391Z | 174.834° S | 37.697° | 2024-12-22 10:34:05.391Z | 108.804° ESE |
27 mins | 2024-12-22 12:20:05.391Z | 257.129° W | 2024-12-22 12:36:05.391Z | 200.53° SSW | 34.654° | 2024-12-22 12:47:05.391Z | 130.532° SE |
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