The invention provides a star sensor sub-low temperature independent thermal control device of an orbit transfer vehicle. The device comprises an imported star sensor A, a domestic star sensor B, thermistors (2), heaters (3), light shields (4), F46 films (5), an S781 white paint thermal control coating (6), mounting supports (7), a self support (8), heat insulation pads (8), a plurality of layers of heat insulation components (10) and thermal protection layers (11). Thermal resistance between stars and the star sensors is increased through the heat insulation pads, heat leakage compensation is greatly reduced, and a foundation is laid for independent temperature control over the star sensors. According to the sub-low temperature design requirement, the S781 white paint thermal control coating is adopted to increase the temperature adaptability of a star sensor motive track. The heat insulation components and the protection layers are adopted, and the radiation influence of a 25N engine on the imported star sensor A is effectively prevented. The device is convenient to implement, high in reliability and adaptability and small in total occupied resource, and the heat radiation of the engine can be effectively prevented.