DELTA 1 R/B(2) *, 2971
Orbit data source: Space-Track
DELTA 1 R/B(2) *, 2971 is space debris in HEO originally from a launch on Thu, 28 Sep 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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2971 intel report (Beta)
DELTA 1 R/B(2) * details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | UTC |
| Mission | Spacecraft |
| Bus & Motor | FW4, Unknown motor |
| Mass | ~40 kg wet, ~40 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, Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 DELTA 1 R/B(2) *
1 02971U 67094C 24355.32652166 .00006192 00000-0 30008-2 0 9996
2 02971 28.2089 116.9866 6576099 350.0402 1.4859 3.17892008542391Epoch: 2024-12-20T07:50Z
Definitive object data (Epoch: 2024-12-20T07:50:11.471Z)
| Latitude | 0.00004° |
| Longitude | -89.9717° |
| Altitude | 342.193 km |
| Speed | 9.911 km/s |
| True Right ascension | 07h 47m 52s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 14.13229° |
| Longitude | 61.35453° |
| Altitude | 21,939.309 km |
| Speed | 2.784 km/s |
| Apparent Right ascension | 18h 23m 08s |
| Apparent Declination | 6° 45' 54" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 15:15:21 |
| Azimuth | 115.408° SE |
| Elevation | 36.553° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 26,014.225 km |
| Perigee altitude | 312.716 km |
| Semi-major axis | 19,541.607 km |
| Eccentricity | 0.6576099 |
| Inclination | 28.2089° |
| RAAN | 116.9866° |
| Arg. of periapsis | 350.0402° |
| True anomaly | 9.51399° |
| Mean anomaly | 1.4859° |
| Eccentric anomaly | 4.33186° |
| Mean motion | 0.79452 °/min |
| BSTAR | 0.0030008 |
| Orbital period | 453.11 mins |
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Other satellites on launch #94 in the year 1967 (1967-09-28 UTC)
| INTELSAT 2-F4, 2969 |
| DELTA 1 R/B(1), 2970 (Decayed) |
| DELTA 1 R/B(2) *, 2971 |
| DELTA 1 DEB, 2972 (Decayed) |
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. |
|---|---|---|---|---|---|---|---|
| 236 mins | 2024-12-21 16:12:56.584Z | 115.437° SE | 2024-12-21 16:12:56.584Z | 115.437° SE | 30.768° | 2024-12-21 20:08:56.584Z | 140.53° SSE |
| 201 mins | 2024-12-22 12:51:56.584Z | 224.204° SW | 2024-12-22 13:00:56.584Z | 155.513° SSE | 39.405° | 2024-12-22 16:12:56.584Z | 108.979° ESE |
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