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I am trying to simulate the launch of gravity assisted NASA satellites (specifically Galileo, Cassini, and Juno), but I am struggling to find the initial conditions for my simulation. I have tried searching NASA and JPL resources that I know of but am struggling to find the values or any values I can extrapolate from. For the style of simulation I am using the values I want are vx, vy, vz. Any direction or assistance would be appreciated.

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    $\begingroup$ This would fit better on "Space exploration" stackexchange. $\endgroup$ – James K Mar 29 '20 at 11:27

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