Take an illustrative elliptic Kepler orbit with semi-major axis , orbital eccentricity and gravitational parameter , in consistent dimensionless units. Its semi-minor axis is , mean motion is , and specific angular momentum magnitude is . About the attracting focus,The two sectors below each span , giving . Near periapsis the short radius sweeps a wide angle; near apoapsis the long radius sweeps a narrow angle. Constant areal velocity therefore does not require constant angular velocity or constant speed.
To compute the sectors without mistaking equal angles for equal times, parametrize the ellipse by eccentric anomaly :This follows by integrating . Kepler's equation gives , with mean anomaly measured from periapsis time . Consequently . The displayed sectors use mean anomaly intervals and , rather than equal eccentric anomaly increments.
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