STEP-BY-STEP ANSWER:
Step 1: Recognize that satellites follow elliptical orbits, as described by Kepler's First Law.
Step 2: Use Kepler's Second Law, which states that a line joining a satellite and the central body sweeps out equal areas in equal times, to assess orbital speed variations.
Step 3: Apply Kepler's Third Law to relate the orbital period to the radius of the orbit.
Step 4: Solve for the desired orbital characteristic using the established relationships.
Final Answer: Kepler's Laws allow determination of orbital shape, speed variation, and period for a satellite by relating distance and time.