A 5.00 kg satellite is launched from the north pole into a circular orbit 800 km above the surface of the earth. How much energy is required to achieve this orbit? (The following set of questions will guide you to the answer.) Me = 5.98x1024 kg; Re = 6.37x106 m. G = 6.67x10-11 N m2/ kg2. Note: The problem specifies that the satellite is being launched from the north pole so that we can ignore the initial circular motion and initial kinetic energy as it rotates once every day. In reality, space agencies choose to launch rockets from southern latitudes to take advantage of the initial velocity they have due to this motion. a. calculate the change in gravitational potential energy. (Give your answer in MJ.) b. What is the gravitational force on the satellite? (Give your answer in N.) c. What is the velocity of the satellite? (Give your answer in m/s.) Note: The weight force is equal to m v2/R. d. What is the kinetic energy in this orbit? (Give your answer in MJ.) e. how much total energy was needed to bring the satellite into this orbit? (Give your answer in MJ.)

Principles of Physics: A Calculus-Based Text
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Author:Raymond A. Serway, John W. Jewett
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Chapter11: Gravity, Planetary Orbits, And The Hydrogen Atom
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A 5.00 kg satellite is launched from the north pole into a circular orbit 800 km above the surface of the earth. How much energy is required to achieve this orbit? (The following set of questions will guide you to the answer.)

Me = 5.98x1024 kg; Re = 6.37x106 m. G = 6.67x10-11 N m2/ kg2.

Note: The problem specifies that the satellite is being launched from the north pole so that we can ignore the initial circular motion and initial kinetic energy as it rotates once every day. In reality, space agencies choose to launch rockets from southern latitudes to take advantage of the initial velocity they have due to this motion.

a. calculate the change in gravitational potential energy. (Give your answer in MJ.)

b. What is the gravitational force on the satellite? (Give your answer in N.)

c. What is the velocity of the satellite? (Give your answer in m/s.)

Note: The weight force is equal to m v2/R. 

d. What is the kinetic energy in this orbit? (Give your answer in MJ.)

e. how much total energy was needed to bring the satellite into this orbit? (Give your answer in MJ.)

 

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