Question 1 Report
The effective potential energy, E, of a lunar satellite of mass, m, moving in an. elliptical orbit around the moon of mass, m, is given by
\[ E = \frac{K^2}{2m_1r^2} - \frac{Gm_1m_2}{r} \] where r is the distance of the satellite from the mooń and G is the universal gravitational constant of dimensions, \(M^{-1}L^3T^2\).
Ďetermine the dimensions of the angular momentum, K, of the satellite using dimensional analysis.
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