Question

Consider an earth satellite moving with a speed 8200 m/s at perigee which is 340 km
above the earth's surface. Calculate distance to the satellite from the earth's surface when
it is at apogee. (Radius of earth is 6.4x100 m).
(a) 2340 km
(b) 4580 km
(c) 3520 km
(d) 1850 km

Answer 1

Answer:

4580 km this is the answer

Answer 2

Answer:

B or D my answer because 6.4x100m} {4580km}

or 1850 km