Spacecraft routinely use internal rotating wheels, such as reaction wheels and control moment gyroscopes, to alter and maintain their orientation in space via conservation of angular momentum.
The claim states that an electric vehicle (or spacecraft) in space can alter its orientation using rotating wheels as reaction control. Multiple retrieved papers (such as [3], [5], [9], and [11]) discuss spacecraft attitude control systems utilizing reaction wheels and control moment gyroscopes to manage orientation through internal momentum exchange without expelling mass. Thus, the evidence strongly supports the claim.