I am working on a project where we need to find an optimal


I am working on a project where we need to find an optimal transfer for a spacecraft from LEO to the L4 LaGrange point in the Earth-Moon system. In order to calculate the delta V for the arrival at the LaGrange point, we need to know the "velocity" of the LaGrange point as the moon orbits the Earth. How would you calculate this velocity (in 3-D)?

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Physics: I am working on a project where we need to find an optimal
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