Presumably the Ariane 5 rocket launched the James Webb Space Telescope into an elliptical orbit with its apogee at the L2 point. Such an orbit’s period is about 70 days, i.e. the journey to L2 should take 35 days. Is the reason for it taking only 30 days due to the Coriolis Effect or is the trajectory something other than a simple orbit?
I am of course, for simplicity, viewing the above orbit in a rotating frame of reference centred on the Sun-Earth barycentre and rotating at the Earth’s orbital angular velocity.