#2
What is the altitude above Earth's surface of a satellite with an orbital speed of 6.5 km/s?
The universal gravitational force equation
Fg = 6.67 * 10^-11 * (m1 * m2) ÷ r^2
m1 = mass of Earth = 5.98 * 10^24 kg
m2 = mass of satellite
Radius of Earth = 6.38 * 10^6 m
r = distance from the center of the Earth to the satellite
Fg = 6.67 * 10^-11 * (5.98 * 10^24 * m2) ÷ r^2
Assuming the orbit is circular,
Force centripetal = ( mass of satellite * velocity^2) ÷ radius
velocity = 6,500 m/s
Force centripetal = (m2 * 6500^2) ÷ r
Force of Universal gravitation = Force centripetal
6.67 * 10^-11 * (5.98 * 10^24 * m2) ÷ r^2 = (m2 * 6500^2) ÷ r
Divide both sides by m2
(6.67 * 10^-11 * 5.98 * 10^24) ÷ r^2 = 6500^2 ÷ r
Multiply both sides by r
(6.67 * 10^-11 * 5.98 * 10^24) ÷ r = 6500^2
r = 9.44 * 10^6
r = distance from the center of the earth to the satellite
Radius of Earth = 6.38 * 10^6 m
Altitude = 9.44 * 10^6 – 6.38 * 10^6 = 3.06 *10^6 m