Answer:
the centripetal force on the satellite in the larger orbit is _one fourth_ as that on the satellite in the smaller orbit.
Explanation:
Mass of satellite, m
orbit radius of first, r1 = r
orbit radius of second, r2 Â = 2r
Centripetal force is given by
[tex]F= \frac{mv^{2}}{r}[/tex]
Where v be the orbital velocity, which is given by
[tex]v=\sqrt{gr}[/tex]
So, the centripetal force is given by
[tex]F= \frac{mgr}}{r}}=mg[/tex]
where, g bet the acceleration due to gravity
[tex]g=\frac{GM}{r^{2}}[/tex]
So, the centripetal force
[tex]F= \frac{GMm}}{r^{2}}}[/tex]
Gravitational force on the satellite having larger orbit
[tex]F= \frac{GMm}{4r^{2}}[/tex] .... (1)
Gravitational force on the satellite having smaller orbit
[tex]F'= \frac{GMm}{r^{2}}[/tex] .... (2)
Comparing (1) and (2),
F' = 4 F
So, the centripetal force on the satellite in the larger orbit is _one fourth_ as that on the satellite in the smaller orbit.