Returns the equidistant Earth Centered Inertial coordinates of a satellite orbit track.
Namespace: Zeptomoby.OrbitTools.TrackAssembly: Zeptomoby.OrbitTools.Track (in Zeptomoby.OrbitTools.Track.dll) Version: 1.5.0.0 (1.5.0.0)
Syntax
C# |
---|
public static IList<Eci> OrbitTrack(
this Satellite sat,
double t1,
double t2,
double kmSpacing
) |
Visual Basic |
---|
<ExtensionAttribute> _
Public Shared Function OrbitTrack ( _
sat As Satellite, _
t1 As Double, _
t2 As Double, _
kmSpacing As Double _
) As IList(Of Eci) |
Visual C++ |
---|
[ExtensionAttribute]
public:
static IList<Eci^>^ OrbitTrack(
Satellite^ sat,
double t1,
double t2,
double kmSpacing
) |
Parameters
- sat
- Type: Satellite
The satellite.
- t1
- Type: System..::..Double
The start time.
- t2
- Type: System..::..Double
The end time.
- kmSpacing
- Type: System..::..Double
The distance between points, in kilometers (approximate).
Return Value
A list of equidistant ECI coordinate points that define the location of the
satellite over the given time period.
Usage Note
In Visual Basic and C#, you can call this method as an instance method on any object of type
Satellite. When you use instance method syntax to call this method, omit the first parameter. For more information, see
or
.
See Also