The ratio of the orbital speeds of two satellites of the earth if the satellites are at heights 6400 km and 19200 km from the surface of the Earth. (Radius of the earth =6400 km.) :
A
√2:1
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B
√3:1
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C
2:1
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D
3:1
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Solution
The correct option is A√2:1 Orbital Speed is given by: V∝1√R Hence, V1V2=√R2R1 V1V2=√19200+64006400+6400 V1V2=√2