Initial state interface for J2/J4 perturbation propagators.
![]() | Options for modeling elliptical motion. |
![]() | This property is deprecated. Use the OrbitEpoch property to configure orbit state epoch. Epoch. Uses DateFormat Dimension. |
![]() | Get the smart epoch component to configure the orbit state epoch. |
![]() | The propagation frame |
![]() | Representation. |
![]() | Returns supported propagation frames |