Initially a satellite of \( 100 \, \text{kg} \) is in a circular orbit of radius \( 1.5 R_E \). This satellite can be moved to a circular orbit of radius \( 3 R_E \) by supplying \( \alpha \times 10^{6} \, \text{J} \) of energy. The value of \( \alpha \) is ______________.
\( \big(\text{Take Radius of Earth } R_E = 6 \times 10^{6} \, \text{m} \text{ and } g = 10 \, \text{m}/\text{s}^{2} \big) \)