TwoBodyStateTransitionMatrixPropagator Properties |
The TwoBodyStateTransitionMatrixPropagator type exposes the following members.
Properties| Name | Description | |
|---|---|---|
 | Epoch |
Gets or sets the Julian date at which the initial conditions are defined.
|
| GravitationalParameter |
Gets or sets the gravitational parameter for the central body around which to propagate.
|
| InitialConditions |
Gets or sets the orbital state of the spacecraft at the Epoch.
|
| IsFrozen |
Gets a value indicating whether this object is frozen. A frozen object cannot be modified and an
ObjectFrozenException will be thrown if an attempt is made to do so.
(Inherited from DefinitionalObject.) |
See Also