Time period of revolution of satellite T = 2π(r3/G*mE)1/2
So T2 = 4π2(r3/G*mE)
(G*mE)/r3 = 4π2/T2
So (4π/3)G*ρE = 4π2/T2
Then ρE = 3π/(T2*G) = 3π/[(90*60)2 * 6.66*10-11]
SO ρE = 4853 Kg/m3
Hope it clears. If still you have doubt you can ask me.
If you like answer then please approve it.