Mathematical Problems in Engineering / 2009 / Article / Fig 2

Research Article

Some Initial Conditions for Disposed Satellites of the Systems GPS and Galileo Constellations

Figure 2

Time evolution of the eccentricity (a) and the critical angle (b). Initial conditions: a = 4.805  𝑅 𝑇 (30,647 km), e = 0.005, I = 56.06°, and other elements equal to zero. In the simulations, we consider only Sun and oblateness as disturbers.
510759.fig.002a
(a)
510759.fig.002b
(b)

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