Be that as it may, Kepler clearly demonstrated the validity of Newton's Laws, especially "... that Uniform Circular Motion applies to all objects that maintain a constant velocity magnitude but constantly change velocity direction. Since the direction is always changing, a centripetal acceleration must be present. Centripetal acceleration is the acceleration caused by centripetal force and directed toward the center of the circle radially.
Mathematically, a = v^2/r, where a is the centripetal acceleration, v is the velocity (magnitude only), and r is the radius (the distance of the object from the center of the circle. By using the previous equation for acceleration, the centripetal force on an object equals the mass times the velocity squared divided by the radius. Mathematically, F = mv^2/r, where F is the centripetal force, m is the mass of the object, v is the velocity, and r is the radius. Centripetal force is not a true force; therefore, it is called a psuedoforce. Though the direction of the velocity changes, the magnitude of the velocity is constant for an object in uniform circular motion. The acceleration of an object in circular motion is equal to v^2/r, the acceleration according to uniform gravitation is equal to Gm/r^2, therefore Gm/r^2 = v^2/r, or v = sqrt (Gm/r), where G is the constant for gravitation, m is the mass of the object, r is the radius, and v is the velocity�s magnitude. This equation only applies to satellites and celestial bodies affected by gravity. (Source: NASA -Orbital Mechanics).
There is no linear acceleration along an orbital flight path, but only acceleration in the direction of its motion. This acceleration is centripetal acceleration, because the direction of travel is always inwards towards the center of the circular orbit.