Answer:
Step-by-step explanation:
given,
time taken to complete the each orbit = 144 minutes
t = 144 x 60 = 8640 s
mass of the earth = 5.98 x 10²⁴ Kg
radius of earth,R = 6.38 x 10⁶ m
Using Kepler's 3rd law
r = 9.1 x 10⁶ m
the altitude of the satellite
H = r - R
H = 9.1 x 10⁶ - 6.38 x 10⁶
H = 2.72 x 10⁶ m