Explanation:
Given:
orbital speed(s) = 5,434m/s
mass(m)=5.98*10^24kg
radius of earth (R)= 6400 km=6.4*10^6m
acceleration due to gravity =9.8m/s
we know ,
s= R*(√(g/(R+h)))
or, 5434=6.4*10^6(√(9.8/(6.4*10^6+h)))
or, 5434/6.4*10^6=√(9.8/(6.4*10^6+h))
or, 8.49*10^-4=√(9.8/(6.4*10^6+h))
squaring both the sides,we get,
or, 7.20*10^-7=9.8/(6.4*10^6+h)
or, 6.4*10^6+h=9.8/7.2*10^-7
or, 6.4*10^6+h=1.35*10^7
or, h=1.35*10^7-6.4*10^6
or, h=7.19*10^6m
Therefore, the distance of satellite from centre of earth is 6400km+7.19*10^6m=1.35*10^7m.
If answer is correct inform me because I am little confused.