Vela 1BVela 1B |
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Operator | USAF |
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COSPAR ID | 1963-039C |
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SATCAT no. | 00692 |
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Mission duration | 6 months (planned) |
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Manufacturer | TRW |
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Launch mass | 150 kilograms (330 lb) |
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Power | 90 W |
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Launch date | October 17, 1963, 02:24 (1963-10-17UTC02:24Z) |
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Rocket | Atlas-LV3 Agena-D |
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Launch site | Cape Canaveral LC-13 |
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Reference system | Geocentric[1] |
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Regime | Highly Elliptical |
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Semi-major axis | 115,746.0 kilometres (71,921.2 mi) |
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Perigee altitude | 42,766.0 kilometres (26,573.6 mi) |
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Apogee altitude | 175,984.2 kilometres (109,351.5 mi) |
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Inclination | 28.7° |
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Period | 6,531.6 minutes |
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Epoch | June 3, 2018 (2018-06-03) |
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Instruments |
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X-ray/Charged Particle | Gamma ray/Charged Particle | Neutron Detectors |
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Vela 1B was a military satellite developed to detect nuclear detonations to monitor compliance with the 1963 Partial Test Ban Treaty by the Soviet Union.
- ^ N2YO.com. "VELA 1". N2YO.com. Retrieved June 3, 2018.
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: CS1 maint: numeric names: authors list (link)