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Suppose a probe satellite of mass m is released with some initial velocity Vo out in space, far away from some mystery planet of mass M. The
satellite is observed to speed up, whip around the mystery planet, and continue to off to infinity at angle of 90° relative to it's incoming path. What is the
eccentricity of the trajectory?
O e = 2
-3/2
e =
2
O e =
V2
°e =

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