A Study about the Integration of the Elliptical Orbital Motion Based on a Special One-Parametric Family of Anomalies

Table 3

Number of steps to get a precision of |Δ𝑟|⃗<10⁻⁴ Km.

	𝑁	𝛼=0	𝛼=0.25	𝛼=0.5	𝛼=0.75	𝛼=1.0	𝛼(𝑒)
RK4	7084079	3292627	401504	251229	190193	158367	146393
RK8	305033	94362	14303	10833	9025	6840	6630