By what percent ,the energy of the satellite has to be increased to shift it from an orbit of radius ’r’ to ‘3r’
66.7%
33.3%
15%
20.3%
TE=−Gmm2r;ΔTE=Gmm21r1-1r2 TE%=ΔTETE×100%=Gmm21r1-1r2Gmm2r1×100%=1r-13r1r×100%=3-13r1r×100%=23×100=66.7%