Helper method to assign a new orbit state using Equinoctial representation
| [Visual Basic .NET] |
|---|
|
| [C#] |
|---|
|
| [Managed C++] |
|---|
|
| [Java] |
|---|
|
| [Unmanaged C++] |
|---|
|
- ECoordinateSystem
- SemiMajorAxis
- H
- K
- P
- Q
- MeanLon








| AGI STK Util 11 | Send comments on this topic. |
| AssignEquinoctialRetrograde Method (IAgOrbitState) | |
| See Also | |
![]() ![]() |
| [Visual Basic .NET] |
|---|
|
| [C#] |
|---|
|
| [Managed C++] |
|---|
|
| [Java] |
|---|
|
| [Unmanaged C++] |
|---|
|