Mission type | Communications |
---|---|
Operator | Intelsat |
COSPAR ID | 1969-064A |
SATCAT no. | 04051 |
Mission duration | 5 years planned Failed to orbit |
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 26, 1969, 02:06[1] | UTC
Rocket | Delta M |
Launch site | Cape Canaveral LC-17A |
End of mission | |
Deactivated | October 14, 1988 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Eccentricity | 0.07326 |
Perigee altitude | 252 kilometers (157 mi) |
Apogee altitude | 1,301 kilometers (808 mi) |
Inclination | 30.3° |
Period | 115.3 minutes |
Epoch | July 26, 1969 |
Intelsat III |
Intelsat III F-5 was a communications satellite intended to be operated by Intelsat. Launched towards geostationary orbit in 1969 it failed to achieve orbit.