An artificial satellite is moving around earth in a circular orbit with speed equal to one fourth
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Escape velocity = 2gR−−−−√1/4
th escape velocity = 2gR
−−−−√/4 = gR/8
−−−√=GM/8R
−−−−−−−√orbital speed = GM/r
−−−−−√so r= 8R
hope it's help you
================
th escape velocity = 2gR
−−−−√/4 = gR/8
−−−√=GM/8R
−−−−−−−√orbital speed = GM/r
−−−−−√so r= 8R
hope it's help you
================
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