For a circular Orbit F = ma
m1ms
m1v12
2 r1
G ----------- =
---------- and v1
= ----------
r12
r1
T1
Substituting v1 and canceling m1.
ms
4 2 r1 2
ms 4 2
r1
G ------ =
------------ Simplifying
G ------ = ------------
r12
r1T12
r12
T12
Rearranging to get r and T on one side and all
other terms on the other side. Repeat the equation for 2nd
period.
T12
4 2
T22 4 2
T12 T22
----- = ---------- and ----- =
---------- Since G, ms,
and are
constants -----
= -------
r13 G ms
r23 G ms
r13
r23
This can be rearranged to get
T12
r13
----- = -------
T22 r23
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