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Two satellite S(1) and S(2) revolve arou...

Two satellite `S_(1)` and `S_(2)` revolve around a planet in coplanar circular orbits in the opposite sense. The periods of revolutions are `T` and `eta T` respectively. Find the angular speed of `S_(2)` as observed by an astronouts in `S_(1)`, are observed by an astronaut in `S_(1)`, when they are closest to each other.

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The correct Answer is:
`omega = (2pi(eta^(2//3)+1))/(T(eta^(2//3)-1)]`
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