DELTA 1 R/B, 979
Orbit data source: Space-Track
DELTA 1 R/B, 979 is space debris in LEO originally from a launch on Fri, 22 Jan 1965 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 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 15 hours ago |
| Origin | |
| Manufacturer | ABL |
| Mission status | Unknown |
| Mission | Unknown |
| Bus & Motor | ALTAIR, Unknown motor |
| Mass | 60 kg wet, 60 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Radar Cross Section | 0.47 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 15 hours ago
0 DELTA 1 R/B
1 00979U 65004B 24251.43181059 .00001075 00000-0 13551-2 0 9995
2 00979 96.4168 48.6272 1140033 232.2286 117.0112 12.15126900636877Epoch: 2024-09-07T10:21Z
Definitive object data (Epoch: 2024-09-07T10:21:48.434Z)
| Latitude | -0.00003° |
| Longitude | -93.81469° |
| Altitude | 2,106.4 km |
| Speed | 6.642 km/s |
| True Right ascension | 03h 14m 30s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | -76.7929° |
| Longitude | 58.0494° |
| Altitude | 812.99 km |
| Speed | 7.825 km/s |
| Apparent Right ascension | 07h 06m 58s |
| Apparent Declination | -67° 48' 39" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 17:48:32 |
| Azimuth | 194.736° SSW |
| Elevation | -60.113° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 2,521.942 km |
| Perigee | 700.335 km |
| Semi-major axis | 7,989.275 km |
| Eccentricity | 0.1140033 |
| Inclination | 96.4168° |
| RAAN | 48.6272° |
| Arg. of periapsis | 232.2286° |
| True anomaly | 127.87608° |
| Mean anomaly | 117.0112° |
| Eccentric anomaly | 122.51899° |
| Mean motion | 3.03936 °/min |
| BSTAR | 0.0013551 |
| Period | 118.45 mins |
No data available
Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)
| TIROS 9, 978 |
| DELTA 1 R/B, 979 |
| DELTA 1 DEB, 1312 |
| DELTA 1 DEB, 1313 |
| DELTA 1 DEB, 27720 |
DELTA 1 R/B 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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