Satellite Communication Tutorial Orbit

Q1. Calculate the radius of orbit (in SI units) for a earth satellite in a Medium Earth orbit, where the earth's rotational period is 8664 seconds. Q2. An artificial earth satellite is in an elliptical orbit which brings it to an altitude of 1250 km at perigee and out to an altitude of 5000 km at apogee. Calculate the velocity of the satellite at both perigee and apogee. Q3. A satellite in earth orbit passes through its apogee point at an altitude of 2000 km above the earth's surface and at a velocity of 7,850 m/s. Calculate the perigee altitude of the satellite. Q4. A satellite in earth orbit has a semi-major axis of 6,700 km and an eccentricity of 0.01. Calculate the satellite's altitude at both perigee and apogee. Q5. Find the velocity of the GPS satellite. For Solution you can click below link https://drive.google.com/file/d/1xql0Z2xIjUGKHNgSN5S5xKzBDwHMSUnB/view?usp=sharing