The length of time a satellite takes to orbit the earth depends on its:
A
launch speed
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B
mass
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C
distance from the earth
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D
weight
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E
orbital direction
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Solution
The correct option is C distance from the earth The length of time T taken by a satellite is given by ,
T=2π/R√(R+h)3g
where R= radius of earth , h= distance of satellite from earth,
it is clear from above relation that length of time T depends only upon h (distance of satellite from earth) .It does not depend upon mass,weight or orbital direction.