A satellite is orbiting in the equatorial plane with a period from perigee to the perigee of 12 h. If the eccentricity = 0.002, i = 0°, K1 = 66063.17 km2, μ = 3.99 x 1014 m3 / s2 and the earth's equatorial radius – 6378.14 km, the semi-major axis will be

A satellite is orbiting in the equatorial plane with a period from per

1.	A satellite is orbiting in the equatorial plane with a period from perigee to the perigee of 12 h. If the eccentricity = 0.002, i = 0°, K1 = 66063.17 km2, μ = 3.99 x 1014 m3 / s2 and the earth's equatorial radius – 6378.14 km, the semi-major axis will be
A.	34232 km
B.	30424 km
C.	26612 km
D.	22804 km
Answer» D. 22804 km