Mission type | Communications |
---|---|
Operator | Intelsat |
COSPAR ID | 1970-003A |
SATCAT no. | 04297 |
Mission duration | 5 years (planned) |
Spacecraft properties | |
Manufacturer | TRW Inc. |
Launch mass | 293 kilograms (646 lb) |
BOL mass | 151 kilograms (333 lb) |
Power | 183 W |
Start of mission | |
Launch date | January 15, 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 | 0.00033[2] |
Perigee altitude | 35,773 kilometers (22,228 mi)[2] |
Apogee altitude | 35,801 kilometers (22,246 mi)[2] |
Inclination | 0.9°[2] |
Period | 1,436.1 minutes[2] |
Epoch | January 15, 1970[2] |
Intelsat III |
Intelsat III F-6 was a communications satellite owned by Intelsat. The satellite had an estimated useful life of 5 years.