Mission type | Communications |
---|---|
Operator | Intelsat |
COSPAR ID | 1970-032A |
SATCAT no. | 04376 |
Mission duration | 5 years (planned) |
Spacecraft properties | |
Manufacturer | TRW Inc. |
Launch mass | 647 kilograms (1,426 lb) |
BOL mass | 151 kilograms (333 lb) |
Power | 183 W |
Start of mission | |
Launch date | April 23, 1970, 00:46:12 (1970-04-23UTC00:46:12Z) UTC |
Rocket | Thor Delta M 559/D78 |
Launch site | Cape Canaveral LC-17A |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 124° W (current position) |
Semi-major axis | 42,146 kilometers (26,188 mi) |
Perigee altitude | 35,760.4 kilometers (22,220.5 mi) |
Apogee altitude | 35,789.9 kilometers (22,238.8 mi) |
Inclination | 4.9° |
Period | 1,435.1 minutes |
Epoch | May 29, 2018 |
Intelsat III← Intelsat III F-6Intelsat III F-8 → |
Intelsat III F-7 was an American communications satellite owned by Intelsat. The satellite had an estimated useful life of 5 years.
Design
The seventh of eight Intelsat III satellites to be launched, Intelsat III F-7 was built by TRW. It was a 647-kilogram (1,426 lb) spacecraft equipped with two transponders to be powered by body-mounted solar cells generating 183 watts of power. It had a design life of five years and carried an SVM-2 apogee motor for propulsion.
Launch
Intelsat III F-7 was launched by a Delta M rocket, flying from Launch Complex 17A at the Cape Canaveral Air Force Station.
See also
References
- McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved May 29, 2018.
- ^ Real Time Satellite Tracking, N2YO.com. "INTELSAT 3 F-7". Retrieved May 29, 2018.
{{cite web}}
: CS1 maint: numeric names: authors list (link) - Wade, Mark. "Intelsat 3". Encyclopedia Astronautica. Archived from the original on February 23, 2002. Retrieved May 29, 2018.
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