Stationary satellites have been used for global commercial communication satellite system; however, they have several disadvantages so that orbit-controlled medium- altitude satellite system, and use of quasi-synchronous satellites with period of revolution (around earth) of less than 12 hr have been proposed previously; author, on other hand, points out that optimum satellite system involves equatorial orbit with period of 12 to 16 hr and proposes that global communication satellite system should employ this orbit.
CITATION STYLE
ONO K. (1968). GLOBAL COMMUNICATION SATELLITE SYSTEMS. Electronics & Communications in Japan (English Translation of Denshi Tsushin Gakkai Ronbunshi), 51(10), 79–80. https://doi.org/10.1007/978-3-319-23386-4_90
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