Say you launch a rocket for rendezvous with the ISS.

You'll want to set the target orbital inclination and longitude of ascending node. These will ensure the rocket is in the plane of the ISS.

You'll also want to set the target altitude and velocity. These will ensure your rocket enters a stable orbit from which to transfer closer to the ISS.

Are there any other parameters you'd want to set? Would orbital eccentricity be important? If so, any comments on how you'd determine its appropriate value?

What about the argument of periapse and true anomaly? Would you set any of these? Comments on how to set them?