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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DELTA 1 R/B(2) * details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 20 hours 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 20 hours ago
0 DELTA 1 R/B(2) *
1 2971U 67094C 24284.13920322 .00006504 00000-0 21808-2 0 9993
2 2971 28.0826 155.9842 6593993 286.4775 14.4924 3.16918131540202Epoch: 2024-10-10T03:20Z
Definitive object data (Epoch: 2024-10-10T03:20:27.158Z)
| Latitude | 0.00034° |
| Longitude | 86.6932° |
| Altitude | 2,962.034 km |
| Speed | 8.062 km/s |
| True Right ascension | 10h 24m 08s |
| True Declination | 0° 00' 01" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | 23.49582° |
| Longitude | -148.23687° |
| Altitude | 24,080.834 km |
| Speed | 2.412 km/s |
| Apparent Right ascension | 19h 00m 51s |
| Apparent Declination | 19° 00' 12" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 17:24:18 |
| Azimuth | 128.166° SE |
| Elevation | 60.542° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 26,115.627 km |
| Perigee | 291.384 km |
| Semi-major axis | 19,581.643 km |
| Eccentricity | 0.6593993 |
| Inclination | 28.0826° |
| RAAN | 155.9842° |
| Arg. of periapsis | 286.4775° |
| True anomaly | 73.65887° |
| Mean anomaly | 14.4924° |
| Eccentric anomaly | 37.48299° |
| Mean motion | 0.79208 °/min |
| BSTAR | 0.0021808 |
| Period | 454.5 mins |
No data available
No data available
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: 39.9160978°, -105.1181434
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. |
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