(a) The height above the earth's surface of the parking orbit is determined from the difference between the orbital radius and earth's radius (h = r - R).
(b) Velocity of the satellite of the earth is determined with a formula given as (2π/T)r.
The height above the earth's surface is calculated using the following formula;
[tex]T = \frac{2\pi r^{\frac{3}{2} }}{\sqrt{Gm} }[/tex]
where;
r = h + R
h = r - R
where;
The velocity of the satellite is determined using the formula below;
v = ωr
v = (2π/T)r
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