Question #1068c
1 Answer
Jun 5, 2016
Explanation:
Let
m->"Mass of satellite" M->"Mass of Earth" R->"Radius of Earth" =6400km h->"Height of the orbit from surface of the Earth" =900km v->"Orbiting speed of the satellite" G->"Gravitational constant" g->"Acceleration due to gravity" =9.8xx10^-3kms^-2
Now we know
Now inserting the values in equation (1) we get