what conditions must be met if a man-made satellite is to attain a circular orbit around the earth?(choose as many as apply)
AIt must be launched with a tangential speed of 0.
BIt must be launched with a tangential speed of 8 km/s.
CIt must be launched with a tangential speed greater than 8 km/s.
DIt must be launched horizontally at a distance over 150 kilometers above the earth.
EIt must be launched vertically with a speed of 8 km/s.
AIt must be launched with a tangential speed of 0.
BIt must be launched with a tangential speed of 8 km/s.
CIt must be launched with a tangential speed greater than 8 km/s.
DIt must be launched horizontally at a distance over 150 kilometers above the earth.
EIt must be launched vertically with a speed of 8 km/s.
