ATS-1 (Applications Technology Satellite 1) was the first experimental geostationary satellite, launched in 1966.[2][disputed (for: Syncom-3 was launched in 1964.) – discuss] Though intended as a communications satellite rather than as a weather satellite, it carried the Spin Scan Cloud Camera developed by Verner E. Suomi and Robert Parent at the University of Wisconsin. After entering a orbit at 23,000 mi (37,000 km) above Earth, initially in orbit over Ecuador, it transmitted weather images from the Western Hemisphere, as well as other data, to ground stations, including well as video feeds for television broadcasting. It took one of the first pictures of the Earth's full-disk (the first from a geostationary orbit), on December 11, 1966.[3]
"For the first time," historians would note later, "rapid-imaging of nearly an entire hemisphere was possible. We could watch, fascinated, as storm systems developed and moved and were captured in a time series of images. Today such images are an indispensable part of weather analysis and forecasting." [4]
![]() The ATS-1. | |
Mission type | Weather Satellite |
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Operator | NASA |
COSPAR ID | 1966-110A[1] |
SATCAT no. | 02608 |
Mission duration | 17 years |
Spacecraft properties | |
Bus | HS-306 |
Manufacturer | Hughes Aircraft |
Launch mass | 352 kilograms (776 lb) |
Start of mission | |
Launch date | December 7, 1966, 02:12:01 (1966-12-07UTC02:12:01Z) UTC |
Rocket | Atlas SLV-3 Agena-D |
Launch site | Cape Canaveral LC-12 |
End of mission | |
Last contact | April 1985 |
Orbital parameters | |
Reference system | Geocentric |
Regime | GEO |
Semi-major axis | 42,152.0 kilometres (26,192.0 mi) |
Eccentricity | 0.00013 |
Perigee altitude | 35,782.0 kilometres (22,233.9 mi) |
Apogee altitude | 35,793.0 kilometres (22,240.7 mi) |
Inclination | 3.6º |
Period | 1,435.5 minutes |
It was the first satellite to use frequency-division multiple access which accepted multiple independent signals and downlinked them in a single carrier. The spacecraft measured 56 inches (1,400 mm) in diameter, 57 inches (1,400 mm) high and weighed 750 lb (340 kg).[5]
The ATS-1 satellite was used during the 1967 international television broadcast Our World, providing a link between the United States and Australia during the program.
The ATS-1 would remain operational for more than 18 years, until April, 1985.[6]
This satellite was cylindrical, with a diameter of 142 cm (56 in) and a height of 135 cm (53 in); an additional 270 cm (110 in) in height was the engine cover. The surface was covered with solar panels, and the whole satellite was stabilized by rotation.
A total of fifteen experiments were conducted during the mission:[7]
Applications Technology Satellite Program | |
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Flown | |
Proposed |
|
← 1965 · Orbital launches in 1966 · 1967 → | |
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Kosmos 104 | OPS 2394 | OPS 7253 · OPS 3179 | Kosmos 105 | Kosmos 106 | OPS 1593 | Luna 9 | OPS 7291 | ESSA-1 | OPS 1439 | Kosmos 107 | Kosmos 108 | OPS 1184 · OPS 3011 · OPS 3031 | Dipason | Kosmos 109 | DS-K-40 No.2 | Kosmos 110 | ESSA-2 | Kosmos 111 | OPS 3488 | GATV-5003 | Gemini VIII | Kosmos 112 | OPS 0879 · OPS 0974 | Kosmos 113 | N-4 No.3 | OPS 1117 | Molniya-1 No.5 | OV1-4 · OV1-5 | OPS 0340 | Luna 10 | Kosmos 114 | OPS 1612 | Surveyor SD-3 | OAO-1 | OPS 0910 | Kosmos 115 | OV3-1 | Molniya 1-03 | Kosmos 116 | OPS 1508 | Kosmos 117 | Kosmos 118 | OPS 1950 · OPS 6785 | Nimbus 2 | Zenit-4 | GATV-5004 | OPS 0082 | OPS 1788 | Kosmos 119 | Explorer 32 | Surveyor 1 | ATDA | Gemini IX-A | OPS 1577 · OPS 1856 | OGO-3 | Kosmos 120 | OV3-4 | FTV-1351 · Secor 6 · ERS-16 | OPS 9311 · OPS 9312 · OPS 9313 · OPS 9314 · OPS 9315 · OPS 9316 · OPS 9317 · GGTS | Kosmos 121 | OPS 1599 | PAGEOS | Kosmos 122 | Explorer 33 | AS-203 | Proton 3 | Kosmos 123 | OPS 1850 | OV1-7 · OV1-8 | Kosmos 124 | GATV-5005 | Gemini X | Kosmos 125 | Kosmos 126 | OPS 3014 | OV3-3 | Kosmos 127 | OPS 1545 | Lunar Orbiter 1 | OPS 1832 · OPS 6810 | Pioneer 7 | OPS 2366 | FTV-1352 · Secor 7 · ERS-15 | Luna 11 | IDSCP 1 · IDSCP 2 · IDSCP 3 · IDSCP 4 · IDSCP 5 · IDSCP 6 · IDSCP 7 · GGTS | Kosmos 128 | GATV-5006 | Gemini XI | OPS 6026 | OPS 1686 · OPS 6874 | Zenit-2 No.40 | OPS 6026 | OPS 1686 · OPS 6874 | OGCh No.05L | Surveyor 2 | OPS 1703 | Ōsumi 1 | OPS 4096 | ESSA-3 | FTV-1583 · Secor 8 | OPS 2055 · OPS 5345 | Kosmos 129 | Molniya 1-04 | Kosmos 130 | Luna 12 | Surveyor SM-3 | Intelsat II F-1 | OV3-2 | OGCh No.06L | OPS 2070 · OPS 5424 | OPS 0855 · OV4-1R · OV4-1T · OV1-6 | Lunar Orbiter 2 | OPS 1866 | GATV-5001A | Gemini XII | Kosmos 131 | Strela-2 No.1 | Kosmos 132 | Kosmos 133 | Kosmos 134 | OPS 1890 | ATS-1 | OV1-9 · OV1-10 | Kosmos 135 | Soyuz 7K-OK No.1 | OPS 8968 | Biosatellite 1 | Kosmos 136 | Ōsumi 2 | Kosmos 137 | Luna 13 | OPS 1584 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
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