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CRCSS
Country: Australia. Spacecraft: Isis, CTS, FedSat.
1969 January 30 - . 06:46 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Thor. Launch Vehicle: Thor Delta E1.
- Isis 1 - . Payload: Isis A. Mass: 241 kg (531 lb). Nation: Canada. Agency: CRCSS. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Isis. USAF Sat Cat: 3669 . COSPAR: 1969-009A. Apogee: 3,458 km (2,148 mi). Perigee: 578 km (359 mi). Inclination: 88.40 deg. Period: 127.60 min. Ionospheric measurements; data correlated with measurements from Alouette 1. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .
1971 April 1 - . 02:57 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Thor. Launch Vehicle: Thor Delta E1.
- Isis 2 - . Payload: Isis B. Mass: 264 kg (582 lb). Nation: Canada. Agency: CRCSS. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Isis. USAF Sat Cat: 5104 . COSPAR: 1971-024A. Apogee: 1,424 km (884 mi). Perigee: 1,358 km (843 mi). Inclination: 88.20 deg. Period: 113.60 min. Ionospheric research. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .
1976 January 17 - . 23:27 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 2914.
- CTS 1 - .
Payload: Hermes. Mass: 500 kg (1,100 lb). Nation: Canada.
Agency: CRCSS.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: CTS.
Completed Operations Date: 1979-12-08 . USAF Sat Cat: 8585 . COSPAR: 1976-004A. Apogee: 35,840 km (22,260 mi). Perigee: 35,704 km (22,185 mi). Inclination: 12.80 deg. Period: 1,435.40 min.
Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Americas at 116 deg W in 1976-79; over the Pacific Ocean 142 deg W in 1979 As of 5 September 2001 located at 135.36 deg W drifting at 0.161 deg W per day. As of 2007 Mar 10 located at 131.55W drifting at 0.190W degrees per day.
2002 December 14 - . 23:04 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.
- FedSat - .
Mass: 58 kg (127 lb). Nation: Australia.
Agency: CSS.
Manufacturer: CRCSS.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: FedSat.
USAF Sat Cat: 27599 . COSPAR: 2002-056C. Apogee: 805 km (500 mi). Perigee: 791 km (491 mi). Inclination: 98.70 deg. Period: 100.80 min.
FedSat contained high-tech communication, space science, navigation and computing equipment and was intended to help bring broadband Internet services to remote parts of Australia. Data from its three-year mission was to be shared between Japan and Australia.
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