Geo-synchronous satellites in quasi-equatorial orbits
    1.
    发明授权
    Geo-synchronous satellites in quasi-equatorial orbits 失效
    地质同步卫星在均匀轨道中

    公开(公告)号:US3836969A

    公开(公告)日:1974-09-17

    申请号:US19208371

    申请日:1971-10-26

    Applicant: RCA CORP

    Inventor: BOND D HOLMAN J

    CPC classification number: H04B7/19 B64G1/1007 B64G1/1085 B64G1/242

    Abstract: The method of the selection of launch conditions for a satellite at substantially synchronous altitude above the earth in a slightly inclined orbit relative to the equatorial plane of the earth to limit the inclination that may be induced by perturbations for significantly long periods of time without the need of orbit adjusting means (north-south station keeping means) aboard the satellite. One or more such satellites are arranged in a communication system in cooperation with at least one ground station. In a two-satellite system a communication channel is continuously operated between at least one satellite and the ground station notwithstanding solar outages.

    D R A W I N G

    Abstract translation: {PG,1

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