| a | Orbit | [protected] |
| calculate_absolute_position(CPoint &new_position) | Orbit | |
| calculate_eccentricity(CPoint R, CPoint V) | Orbit | |
| calculate_new_position_in_orbit() | Orbit | |
| calculate_orbital_params(CPoint R, CPoint V) | Orbit | |
| dump() | Orbit | |
| e | Orbit | [protected] |
| e_vec | Orbit | [protected] |
| i | Orbit | [protected] |
| mu | Orbit | [protected] |
| n | Orbit | [protected] |
| n_vec | Orbit | [protected] |
| nu | Orbit | [protected] |
| omega | Orbit | [protected] |
| Orbit() | Orbit | [inline] |
| w | Orbit | [protected] |
| ~Orbit() | Orbit | [inline] |
1.4.5-20051010