The Orbital Dynamics of Synchronous Satellites: Irregular Motions in the 2 : 1 Resonance

Table 3

Values of the constant of integration 𝐶₁ for 𝑒=0.001, 𝐼=55^∘ and different values for semimajor axis.

𝑎(0)×10^3(m)	𝐶1×10^11(m^2/s)
26555.000	−1.467543158
26561.700	−1.467728282
26562.400	−1.467747623
26563.500	−1.467778013
26565.000	−1.467819454