A satellite close to earth is in orbit above the equator with a period of rotation of 1.5 hrs. If it is above a point P on the equator at some time, it will be above P again after time
1.5 hrs
1.6 hrs. if it is rotating from west to east.
24/17 hrs. if it is rotating from west to east
24/17 hrs. if it is rotating from east to west.
Let = the angular velocity of earth above its axis =
Let = angular velocity, of satellite.
For a satellite rotating from west to east. (same as earth), the relative angular velocity
Time period of rotation relative to earth =
Now for a satellite rotating from east to west (opposite to earth) the relative angular velocity
. Time period of rotation relative to earth =