A satellite in a circular orbit of radius \(r_1 = 7000\;\text{km}\) around Earth needs to transfer to a circular orbit of radius \(r_2 = 42000\;\text{km}\) (geostationary orbit) using a Hohmann transfer.
- Calculate the velocity at each circular orbit.
- Calculate the two velocity changes (\(\Delta v_1\) and \(\Delta v_2\)) needed for the Hohmann transfer.
- Calculate the transfer time.
- Why is the Hohmann transfer the most fuel-efficient two-impulse transfer?
(Use \(M_{\text{Earth}} = 5.97 \times 10^{24}\;\text{kg}\), \(G = 6.674 \times 10^{-11}\;\text{N}\!\cdot\!\text{m}^2/\text{kg}^2\))