The invention provides a space debris observation system, which comprises a low earth orbit observation satellite configured to observe a geosynchronous belt of 0-degree latitude in a near earth orbit so as to cooperatively observe a geosynchronous belt of a first longitude range; the inclined geosynchronous orbit observation satellite is configured to observe a geosynchronous belt in a second longitude range of 0-degree latitude on an inclined geosynchronous orbit; wherein the central point of the first longitude range is opposite to the backlight blind area, and the second longitude range comprises the backlight blind area.

    本发明提供了一种空间碎片观测系统,包括:低轨观测卫星,被配置为在近地轨道对0度纬度的地球同步带进行观测,以协同配合对第一经度范围的地球同步带进行观测;倾斜地球同步轨道观测卫星,被配置为在倾斜地球同步轨道上对0度纬度第二经度范围的地球同步带进行观测;其中,第一经度范围的中心点与逆光盲区相背,第二经度范围包括逆光盲区。


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    Title :

    Space debris observation system


    Additional title:

    空间碎片观测系统


    Contributors:
    ZHU YONGSHENG (author) / ZHENG ZHENZHEN (author) / ZHANG KEKE (author) / DU WEI (author) / DONG LEI (author) / WANG ZHILIANG (author) / WAN YUJUN (author) / MA CHEN (author) / ZHANG XIANG (author) / LI DONGNAN (author)

    Publication date :

    2022-10-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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