To provide an orbit transition support device which is introduced in a geostationary transfer orbit GTO, and effectively supports orbit transition of a transition satellite.SOLUTION: An orbit transition support device 100 is introduced in a geostationary transfer orbit, and supports orbit transition of a transition satellite overtaking orbital altitude of a satellite constellation which is formed in the midway from perigee to apogee in the geostationary transfer orbit. A support information creation part 110 collects a forecast value of each orbit of a plurality of satellites which constitute the satellite constellation from orbit forecast information 51 in which a forecast value of an orbit of a space object 60 is set, and creates support information 111 which is used for support of orbit transition of the transition satellite. A support information display part 120 displays the support information 111 on display equipment 941.SELECTED DRAWING: Figure 9

    【課題】静止トランスファー軌道GTOに投入され遷移衛星の軌道遷移を効果的に支援することを目的とする。【解決手段】軌道遷移支援装置100は、静止トランスファー軌道に投入され、静止トランスファー軌道における近地点から遠地点に至る途中に形成された衛星コンステレーションの軌道高度を追い越す遷移衛星の軌道遷移を支援する。支援情報生成部110は、宇宙物体60の軌道の予報値が設定された軌道予報情報51から、衛星コンステレーションを構成する複数の衛星の各々の軌道の予報値を収集し、遷移衛星の軌道遷移の支援に用いる支援情報111を生成する。支援情報表示部120は、支援情報111を表示機器941に表示する。【選択図】図9


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    Title :

    ORBIT TRANSITION SUPPORT DEVICE, ORBIT TRANSITION SUPPORT METHOD, AND ORBIT TRANSITION SUPPORT PROGRAM


    Additional title:

    軌道遷移支援装置、軌道遷移支援方法、および軌道遷移支援プログラム


    Contributors:

    Publication date :

    2021-04-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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