B) An artificial satellite is going around the earth at a
distance of 2400 km. Calculate the period of revolution and
orbital velocity.
Answers
Answered by
0
Answer:
Consider a satellite which is in a low orbit about the Earth at an altitude of 220 km above Earth's surface. Determine the orbital speed of this satellite. Use the information given below. The orbital speed can be found using v = SQRT(G*M/R).
follow me and mark my answers as brainliest
Similar questions