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Physics
Physics
Problem
Show that for a satellite in a circular orbit of period
T
T
T
around Earth (mass
M
M
M
), the orbital radius
r
r
r
is given by
r
=
(
G
M
T
2
4
π
2
)
1
/
3
.
r = \left( \dfrac{G M T^{2}}{4\pi^{2}} \right)^{1/3}.
r
=
(
4
π
2
GM
T
2
)
1/3
.
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