| a | Orbit | |
| Compute(const Vector &dr, const Vector &dv, const double mu) | Orbit | |
| Compute(const Body &b, const Body &ref_b) | Orbit | |
| e | Orbit | |
| GetE() const | Orbit | |
| i | Orbit | |
| M | Orbit | |
| mu | Orbit | |
| omega_node | Orbit | |
| omega_pericenter | Orbit | |
| Orbit() | Orbit | [inline] |
| Period() const | Orbit | [inline] |
| RelativePosVel(Vector &relative_position, Vector &relative_velocity) const | Orbit |
1.4.7