Elliptical satellite orbit around the Earth

- Run the simulation. Calculate the speed necessary to travel in a circular
orbit with radius 8400 km, i.e. the distance from the center of the Earth
to the satellite when the simulation starts. Also find the period. Problems
with the calculations? Go to
**Parameters**and change the speed to the value that you calculated. Run the simulation to check if your value is correct.

- Change the speed back to 8100 m/s. Check
**View, Distance**and**View, Speed**. Stop the simulation when the satellite has the maximum distance from the Earth. Note the distance and the velocity. Then calculate this velocity using the known distance. Problems with the calculations?

- Make a sketch of the elliptical orbit. Draw acceleration vectors at some
points on the orbit with approximately correct directions and mutual lengths.
Check
**View, Acceleration vector**, run the simulation and compare with your drawing. Study the acceleration vectors and explain their directions. Which effect will the acceleration vector have on the velocity at various points on the orbit? (Consider the components of the vector along the orbit and perpendicular to the orbit.)

Comment to b: If the velocity and the distance are known in the point closest to the Earth, we may find

boththe velocity and distance in the farthest point. It turns out that

This is a special case of Kepler's third law, which follows from the law of conservation of angular momentum.