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

Table 4

Values of the constant of integration 𝐶₁ for 𝑒=0.05, 𝐼=10^∘, and different values for semimajor axis.

𝑎(0)×10^3(m)	𝐶1×10^11(m^2/𝑠)
26555.000	−1.045724331
26565.000	−1.045921210
26568.000	−1.045980267
26574.000	−1.046098370