Probably some kind of supercritical airfoil, somewhat like a modern airliner (these also have fairly high t/c ratios for a transonic wing).
What you observed on the F-22 is called conical camber, and yes the Su-57 has a similar geometry, albeit less pronounced. My guess is that this is related to the sweep angle (which is of course lower on the F-22), with more sweep requiring less camber. On the Concorde and Tu-144 SSTs the outer wings with lower sweep are also more dramatically cambered than the inboard, highly swept part.
One supersonic aircraft which didn't bother with any such complexities incidentally is the YF-23!