An artificial satellite is moving in a circular orbit of radius 42250 km calvulate its speed if it takes 24 hours to revolve aronud earth
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The radius given in your question is slightly more than the radius of Geo stationary orbit. So practically its impossible to maintain or keep the satellite at that orbit with a time period 24 hours. The satellite will drop down to lower orbit.
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Hey there!
Given,
Radius (r) = 42250 km
Time (t) = 24 hours
Distance will equal to perimeter of the orbit
= 2πr
= 2π * 42250
Speed of artificial satelite
= 2π * 42250/24
= 11059 km/h
Hope It Helps You!
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