For elliptical obits: the direction of the velocity of the satellite is (always, seldom, never) perpendicular to the net force acting upon the satellite. For circular obits: the direction of the velocity of the satellite is (always, seldom, never) perpendicular to the net force acting upon the satellite.

As per the orbits of the satellite and velocity in which they move is either seldom or always.

As we start to analyze the orbits of the satellites, in a circular orbit the satellite is always perpendicular to the net force of the speed of the object. As in the case of the elliptical orbits, the orbit is stretched. This tells us that are four points along the orbit. Thus the satellite is seldom perpendicular to the net force acting upon the satellite.

For elliptical orbits: seldom and always

Learn more about the elliptical orbits.

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