a)
F = G M m / ( r + h) ^2
F = 6.67*10^-11* 639*5.98*10^24 / ( 6.38*10^6 + 11.6*10^6)^2
F = 788.4 N
======
b)
orbital speed of satellite
Vo^2 = GM / ( r + h)
Vo^2 = 6.67*10^-11* 5.98*10^24 / ( 11.6*10^6 + 6.38*10^6)
Vo = 4710 m/s
==========
c)
t = 2 pi ( r +h) / vo
t = 2*3.14* ( 6.38 + 11.6)*10^6 / 4710
t = 6.7 h
========
Comment in case any doubt, will reply for sure. Goodluck
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