Notice the small black mark?.. line?.. on the inboard tip? It is halfway between the leadouts.
Just as an ideal measure, consider the model as ONLY the CG spanwise, lengthwise, and from top to bottom. For ibest 'streamlined' flow, the fuselage should fly with the fuse centerline tangent to the flight path at the CG, no? That centerline meets the air at differing angles ahead of and aft of the CG. (The flip side of the flight path curve at the distances from the tangent point.) These angles are quite small, even when checked at the prop and at, e.g., the elevator hingeline...
Lines have drag - they make what Pete Soule' called an accelerated catenary - greater where the speed though the air is greater. (A caternary is the natural sag curve of a uniform load, on a uniform cable supported at its ends. Line drag is not uniform: it is affected by airspeed. Once lines go inside the structure, air drag no longer acts on that part. Well, duh...
The 'LINE...' programs allow (allowed?) estimating the curve AT the leadout guides. That angle, extended to the CG, creates no torque couple trying to rotate the fuse in yaw. If the extended angle points ahead of the CG, it tends to cause nose-in yaw, and vice versa. When control inputs are made, 'pull' is no longer equal on both lines, the yaw tendency appears, accordingly. But with close-set leadouts, the shift is (generally) slight. Other things correct, or counter, the tendency.
The lines should not bend due to the leadout placement, at neutral. The bellcrank pivot placement is irrelevant, but the 'aim' of the 'pull force' through the guides should go to the CG to reduce rubbing and bending.
The 'aim' might be adffected by relatively large changes of CG when flight trimming. Moving the guides to suit the CG can reduce or solve this.
So. without knowing more about the model's 'form' and conditions in that picture, we can't make any practical guesses or claims.
IMHO..