Far from the planet, the magnitude of angular momentum per unit mass is the magnitude of the cross product of position vector and velocity. The perpendicular distance from the incoming asymptote is the impact parameter , so
Choose at closest approach. The general solution of the differential equation in a, with , is
The specific orbital energy is
At infinity , giving . Thus the hyperbolic orbit has
A different zero of polar angle simply replaces by .
The incoming and outgoing asymptotes have radial directions and , where and . The incoming velocity points opposite its radial direction, so the deflection angle between incoming and outgoing velocities is . Hence
Putting gives

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