A satellite of mass M orbits the earth with period T. A second satellite of mass 2M
is at the same radial distance from the center of the earth as the first satellite. What is the
period of the second satellite?
A. 1
2T
B. T
C. 2T
D. 4T
"G\\frac{Mm}{r^2}=m\\omega_1^2r"
"G\\frac{M2m}{r^2}=2m\\omega_2^2r" . So, we have
"\\omega_1^2\/\\omega_2^2=1\\to \\omega_1=\\omega_2\\to T_1=T_2=T"
B. T . Answer
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