发明名称 Ultrahigh altitude sun-synchronous orbit satellite system
摘要 An ultrahigh altitude sun-synchronous orbit satellite system having one or plural satellites orbiting the sun such that the satellites revolve around the earth in a substantially circular or elliptic motion at an altitude of several million kilometers from the earth, beyond the sphere of earth gravity influence. The satellites are placed on an orbital plane relative to both the sun and the earth and keep a distance and geometry between the satellites, sun and earth substantially constant. The satellite system performs any one of the services of space observation, global observation, and satellite communication. The satellites orbit the sun with both inclination and eccentricity distinct from those of the revolution of the earth and revolve around the earth with a sun synchronous property in which the local solar time is kept constant at a point on the surface of the earth directly beneath the satellite.
申请公布号 US7806369(B2) 申请公布日期 2010.10.05
申请号 US20040630087 申请日期 2004.06.22
申请人 JAPAN AEROSPACE EXPLORATION AGENCY 发明人 KAWAGUCHI JUNICHIRO
分类号 B64G1/10;B64G1/00;B64G1/24 主分类号 B64G1/10
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