If g∝1R3 (instead of 1R2), then the relation between time period of a satellite near earth's surface and radius R will be
T2∝R3
T∝R2
T2∝R
T∝R
Gravitational force provides the required centripetal forcemω2R=GMmR3⇒4π2T2=GMR4⇒T2∝R4⇒T∝R2