Given, MA=200kg,MB=400kg,HA=600km,HB=1600km and ‌‌RA=RE+HA=6400+600=7000kmRB=RE+HB=6400+1600=8000km Let TA,TB,ωA,ωB,RA and RB be the time period, angular frequencies and radii of satellites A and B, respectively. Force on satellite A,FA=mAωA2RA=‌