Research Article
A Note on the Use of Generalized Sundman Anomalies in the Numerical Integration of the Elliptical Orbital Motion
Table 2
Optimal
for
  
in
 Km
and in
.
| | | | | | | | |
| 0.00 | 1.539 | | | 0.50 | 1.671 | | | 0.05 | 1.561 | | | 0.55 | 1.681 | | | 0.10 | 1.578 | | | 0.60 | 1.692 | | | 0.15 | 1.593 | | | 0.65 | 1.704 | | | 0.20 | 1.606 | | | 0.70 | 1.718 | | | 0.25 | 1.618 | | | 0.75 | 1.735 | | | 0.30 | 1.630 | | | 0.80 | 1.757 | | | 0.35 | 1.640 | | | 0.85 | 1.790 | | | 0.40 | 1.650 | | | 0.90 | 1.847 | | | 0.45 | 1.661 | | | 0.95 | 1.917 | | |
|
|