Mission type | Communications |
---|---|
Operator | Intelsat |
COSPAR ID | 1970-055A |
SATCAT no. | 04478 |
Mission duration | 5 years (planned) Launch failure |
Spacecraft properties | |
Manufacturer | TRW |
Launch mass | 293 kilograms (646 lb) |
BOL mass | 151 kilograms (333 lb) |
Power | 183 W |
Start of mission | |
Launch date | July 23, 1970, 00:16:03[1] | UTC
Rocket | Delta M |
Launch site | Cape Canaveral LC-17A |
Orbital parameters | |
Reference system | Geocentric[2] |
Regime | Geostationary[2] |
Eccentricity | 0.24386[2] |
Perigee altitude | 19,400 kilometers (12,100 mi)[2] |
Apogee altitude | 36,030 kilometers (22,390 mi)[2] |
Inclination | 13.3°[2] |
Period | 1,043.0 minutes[2] |
Epoch | July 23, 1970[2] |
Intelsat III |
Intelsat III F-8 was a communications satellite owned by Intelsat. The satellite had an estimated useful life of 5 years.