DELTA 1 R/B, 979
Orbit data source: Space-Track
DELTA 1 R/B, 979 is space debris in SSO 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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979 intel report (Beta)
DELTA 1 R/B details
Identifier | |
Orbit | SSO |
Last TLE update | 19 hours ago |
Origin | |
Manufacturer | ABL |
Mission | Spacecraft |
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 |
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 19 hours ago
0 DELTA 1 R/B
1 00979U 65004B 25002.25923356 .00000466 00000-0 59988-3 0 9992
2 00979 96.4309 109.3019 1139053 338.0829 17.4997 12.15285532651065
Epoch: 2025-01-02T06:13Z
Definitive object data (Epoch: 2025-01-02T06:13:17.779Z)
Latitude | 0.00002° |
Longitude | -86.16291° |
Altitude | 758.779 km |
Speed | 7.865 km/s |
True Right ascension | 07h 17m 12s |
True Declination | 0° 00' 00" |
Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
Latitude | -77.32941° |
Longitude | -55.82635° |
Altitude | 1,056.567 km |
Speed | 7.588 km/s |
Apparent Right ascension | 12h 31m 16s |
Apparent Declination | -62° 41' 40" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 01:28:53 |
Azimuth | 163.94° S |
Elevation | -65.637° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 2,520.385 km |
Perigee altitude | 700.502 km |
Semi-major axis | 7,988.58 km |
Eccentricity | 0.1139053 |
Inclination | 96.4309° |
RAAN | 109.3019° |
Arg. of periapsis | 338.0829° |
True anomaly | 22.03193° |
Mean anomaly | 17.4997° |
Eccentric anomaly | 19.69964° |
Mean motion | 3.03976 °/min |
BSTAR | 0.00059988 |
Orbital period | 118.43 mins |
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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: 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. |
---|---|---|---|---|---|---|---|
11 mins | 2025-01-03 06:03:36.590Z | 122.74° SE | 2025-01-03 06:07:36.590Z | 72.069° E | 30.552° | 2025-01-03 06:14:36.590Z | 4.484° NNE |
10 mins | 2025-01-03 08:01:36.590Z | 220.591° SW | 2025-01-03 08:05:36.590Z | 278.286° WNW | 28.849° | 2025-01-03 08:11:36.590Z | 332.576° NNW |
23 mins | 2025-01-03 18:23:36.590Z | 25.451° NE | 2025-01-03 18:34:36.590Z | 95.655° ESE | 35.581° | 2025-01-03 18:46:36.590Z | 160.189° S |
24 mins | 2025-01-03 20:20:36.590Z | 2.055° NNE | 2025-01-03 20:31:36.590Z | 280.452° WNW | 41.432° | 2025-01-03 20:44:36.590Z | 213.513° SW |
14 mins | 2025-01-03 22:19:36.590Z | 339.141° N | 2025-01-03 22:25:36.590Z | 308.178° NW | 17.799° | 2025-01-03 22:33:36.590Z | 271.651° WNW |
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