Two satellites, A and B, have masses m and 2m respectively. A is in a circular orbit of radius R, and B is in a circular orbit of radius 2R around the earth. The ratio of their kinetic energies, `T_(A)//T_(B)`, is :A. `(1)/(2)`B. 1C. 2D. `sqrt((1)/(2))`

Two satellites, A and B, have masses m and 2m respectively. A is in a

1.	Two satellites, A and B, have masses m and 2m respectively. A is in a circular orbit of radius R, and B is in a circular orbit of radius 2R around the earth. The ratio of their kinetic energies, `T_(A)//T_(B)`, is :A. `(1)/(2)`B. 1C. 2D. `sqrt((1)/(2))`
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Two satellites, A and B, have masses m and 2m respectively. A is in a circular orbit of radius R, and B is in a circular orbit of radius 2R around the earth. The ratio of their kinetic energies, `T_(A)//T_(B)`, is :A. `(1)/(2)`B. 1C. 2D. `sqrt((1)/(2))`

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