Some Initial Conditions for Disposed Satellites of the Systems GPS and Galileo Constellations
Figure 5
Time evolution of the osculating eccentricity (top) and the osculating critical angle (bottom) for a disposal GPS satellite. Note that the minimum of the eccentricity occurs when is crossing zero in decreasing direction (from positive to negative value) while maximum occurs when is crossing zero, but in increasing direction (from negative to positive value). Initial conditions: a = 3.5 RT (22,324 km), e = 0.005, I = 56.06°, and other elements equal to zero; IL = 28.58°.