3 The time period \(T\) of a satellite in circular orbit around a planet satisfies the equation
\(G M T ^ { 2 } = 4 \pi ^ { 2 } R ^ { 3 }\),
where
- \(G\) is the universal gravitational constant,
- \(M\) is the mass of the planet,
- \(\quad R\) is the radius of the orbital circle.
- Find the dimensions of \(G\).
A student suggests the following formula to model the approach speed between two orbiting bodies.
\(v = k G { } ^ { \alpha } { } ^ { \beta } { } _ { r } \gamma _ { m _ { 1 } } m _ { 2 } \left( m _ { 1 } + m _ { 2 } \right)\),
where