AviationTire General Navigation In-Flight Navigation Purposes of (FMS) Flight Management Systems Q 1 / 5

An aeroplanes flies from A (59° S 142W) to B (61° S 148W) with a TAS of 480 kt.
The autopilot is engaged and coupled with an Inertial Navigation System in which AB track is active. On route AB, true track:

varies by 10°
decreases by 6°
varies by 4°
increases by 5°