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CS-3
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Class: Communications. Destination: Geosynchronous Orbit. Nation: Japan. Agency: TSCJ(Sakura). To continue communications services provided by the communications satellite 2 (CS-2). To meet increasing and diversifying demands for communications. To develop technologies for communications satellites. Launch vehicle H18F. Launching organization NASDA. Typical orbit: 35787 km x 35789 km at 0 degrees inclination. Mass: 1,100 kg (2,400 lb). Associated Launch Vehicle: H-1. CS-3 Chronology
Bibliography and Further Reading - McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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