Multiplying the tangential equation of motion by gives
Therefore is constant. It is the signed specific angular momentum; reverse the angular orientation if necessary to take for a nonradial orbit. Set and denote differentiation with respect to by a prime. Then
Substitution into the radial equation of motion and division by give the Binet equation
Its general solution is . Write and , where . This produces the Kepler orbit
Here is the orbital eccentricity, and points toward periapsis when . Only portions with describe positive radial distances. The expression assumes ; a zero-angular momentum trajectory is radial and must be treated separately.
Choose the gravitational potential energy to vanish at infinity. The total mechanical energy is
Put and . From part (i), and . Consequently
and the angular terms cancel against the gravitational potential energy:
For a nonradial Kepler orbit, negative, zero and positive mechanical energy correspond respectively to , and .
At infinity, the meteorite's incoming asymptote has speed and perpendicular distance from the Earth’s centre. The magnitude of its specific angular momentum is the magnitude of . On the asymptote, this is , so conservation of angular momentum gives . Its mechanical energy at infinity is . Comparing with part (ii) gives
For this Kepler orbit is a hyperbola. The smallest occurs at periapsis, where . Thus
The middle equality follows by substituting . A trajectory entering the Earth satisfies , equivalently
Therefore the sufficient collision condition is
This is gravitational focusing: Newtonian gravity increases the collision radius measured at infinity. Equality is the ideal grazing trajectory, which touches the surface; a strict inequality penetrates it. For the incoming motion is radial and collides, with as the limiting value of the above expression.

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