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If a satellite is moved from one stable circular orbit to a farther stable circular orbit, then the following quantity increasesA. Linear orbital speedB. Gravitational forceC. Centripetal accelerationsD. Gravitational P.E.

Answer» Correct Answer - D
Orbital speed `v_(c )=sqrt((GM)/(r ))`,
Gravitational force `prop (1)/(r^(2))`, c.p. acceleration `=(v^(2))/(r )`
All the three decrease as the orbital radius is increased. But the gravitational P.E. `= -(GMm)/(r )`.
It is given that `r_(2)gt r_(1)`. Hence the P.E. will increase, because of the -ve sign.


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