The Track type exposes the following members.
Methods
Name | Description | |
---|---|---|
![]() ![]() | CalcApsides(IOrbit, Double) |
Calculates an orbit's apogee and perigee information.
|
![]() ![]() | CalcApsides(IOrbit, Double, Double) |
Calculates an orbit's apogee and perigee information.
|
![]() ![]() | CalcAscendingNode |
Calculates the ascending node information of an orbit.
|
![]() ![]() | CalcDescendingNode |
Calculates the descending node information of an orbit.
|
![]() ![]() | CalcNodes |
Calculates the ascending and descending node information of an orbit.
|
![]() ![]() | CalcPassData(Site, Satellite, DateTime, DateTime, Boolean, Boolean) |
Calculate satellite pass data for a local horizon using a parallel algorithm.
The data includes rise time (AOS), set time (LOS), and optionally, the maximum
elevation (MAX) above the horizon.
|
![]() ![]() | CalcPassData(Site, Satellite, Double, Double, Boolean, Boolean) |
Calculate satellite pass data for a local horizon using a parallel algorithm.
The data includes rise time (AOS), set time (LOS), and optionally, the maximum
elevation (MAX) above the horizon.
|
![]() ![]() | CalcPassData(Station, Satellite, DateTime, DateTime, Boolean, Boolean, Boolean) |
Calculate satellite pass data for a local horizon and (optionally) pass segment data.
|
![]() ![]() | CalcPassData(Station, Satellite, Double, Double, Boolean, Boolean, Boolean) |
Calculate satellite pass data for a local horizon and (optionally) pass segment
data.
|
![]() ![]() | CoverageContour(Satellite, DateTime, Site, IBeamProfile, Int32, Boolean, Double) |
Calculates a coverage contour profile for a beam transmitted
from a satellite to a target location on Earth.
|
![]() ![]() | CoverageContour(Satellite, Double, Site, IBeamProfile, Int32, Boolean, Double) |
Calculates a coverage contour profile for a beam transmitted
from a satellite to a target location on Earth.
|
![]() ![]() | CoverageContourEci(Satellite, DateTime, Site, IBeamProfile, Int32, Boolean, Double) |
Calculates a coverage contour profile for a beam transmitted
from a satellite to a location on Earth.
|
![]() ![]() | CoverageContourEci(Satellite, Double, Site, IBeamProfile, Int32, Boolean, Double) |
Calculates a coverage contour profile for a beam transmitted
from a satellite to a location on Earth.
|
![]() ![]() | GroundTrack(Satellite, DateTime, DateTime, Double, Double) |
Returns the equidistant LAT/LON coordinates of a satellite ground track.
|
![]() ![]() | GroundTrack(Satellite, DateTime, DateTime, TimeSpan, Double) |
Returns the equal time-spaced LAT/LON coordinates of a satellite ground track.
|
![]() ![]() | GroundTrack(Satellite, Double, Double, Double, Double) |
Returns the equidistant LAT/LON coordinates of a satellite ground track.
|
![]() ![]() | GroundTrack(Satellite, Double, Double, TimeSpan, Double) |
Returns the equal time-spaced LAT/LON coordinates of a satellite ground track.
|
![]() ![]() | GroundTrackEcf(Satellite, DateTime, DateTime, Double, Double) |
Returns the equidistant Earth Centered Fixed coordinates of a satellite ground track.
|
![]() ![]() | GroundTrackEcf(Satellite, DateTime, DateTime, TimeSpan, Double) |
Returns the equal time-spaced Earth Centered Fixed coordinates of a satellite ground track.
|
![]() ![]() | GroundTrackEcf(Satellite, Double, Double, Double, Double) |
Returns the equidistant Earth Centered Fixed coordinates of a satellite ground track.
|
![]() ![]() | GroundTrackEcf(Satellite, Double, Double, TimeSpan, Double) |
Returns the equal time-spaced Earth Centered Fixed coordinates of a satellite ground track.
|
![]() ![]() | InSunlight(EciTime, WgsModel) |
Determines if an ECI coordinate point is illuminated by the sun.
|
![]() ![]() | InSunlight(Satellite, DateTime) |
Determines if a satellite is illuminated by the sun.
|
![]() ![]() | InSunlight(Satellite, Julian) |
Determines if a satellite is illuminated by the sun.
|
![]() ![]() | InSunlight(Site, DateTime, Double) |
Determines if a location on earth is illuminated by the sun.
|
![]() ![]() | InSunlight(Site, Julian, Double) |
Determines if a location on earth is illuminated by the sun.
|
![]() ![]() | IsoElevationCircle(Satellite, DateTime, Double, Double, Double) |
Calculates an elevation circle centered on a satellite subpoint.
|
![]() ![]() | IsoElevationCircle(Satellite, Double, Double, Double, Double) |
Calculates an elevation circle centered on a satellite subpoint.
|
![]() ![]() | IsoElevationCircle(Site, DateTime, Double, Double, Double, Double) |
Calculates an elevation circle centered on an earth site.
|
![]() ![]() | IsoElevationCircle(Site, Julian, Double, Double, Double, Double) |
Calculates an elevation circle centered on an earth site.
|
![]() ![]() | IsoElevationCircle(WgsModel, EciTime, Eci, Double, Double, Double) |
Calculates an elevation circle on an ellipsoid model.
|
![]() ![]() | IsoElevationCircleEcf(Satellite, DateTime, Double, Double, Double) |
Calculates an elevation circle centered on a satellite subpoint.
|
![]() ![]() | IsoElevationCircleEcf(Satellite, Double, Double, Double, Double) |
Calculates an elevation circle centered on a satellite subpoint.
|
![]() ![]() | IsoElevationCircleEcf(Site, DateTime, Double, Double, Double, Double) |
Calculates an elevation circle centered on an earth site.
|
![]() ![]() | IsoElevationCircleEcf(Site, Julian, Double, Double, Double, Double) |
Calculates an elevation circle centered on an earth site.
|
![]() ![]() | IsoElevationCircleEcf(WgsModel, EciTime, Eci, Double, Double, Double) |
Calculates an elevation circle on an ellipsoid model.
|
![]() ![]() | IsoElevationCircleEci(Satellite, DateTime, Double, Double, Double) |
Calculates an elevation circle centered on a satellite subpoint.
|
![]() ![]() | IsoElevationCircleEci(Satellite, Double, Double, Double, Double) |
Calculates an elevation circle centered on a satellite subpoint.
|
![]() ![]() | IsoElevationCircleEci(Site, DateTime, Double, Double, Double, Double) |
Calculates an elevation circle centered on an earth site.
|
![]() ![]() | IsoElevationCircleEci(Site, Julian, Double, Double, Double, Double) |
Calculates an elevation circle centered on an earth site.
|
![]() ![]() | IsoElevationCircleEci(WgsModel, EciTime, Eci, Double, Double, Double) |
Calculates an elevation circle on an ellipsoid model.
|
![]() ![]() | OrbitTrack(Satellite, DateTime, DateTime, Double) |
Returns the equidistant Earth Centered Inertial coordinates of a satellite orbit track.
|
![]() ![]() | OrbitTrack(Satellite, DateTime, DateTime, TimeSpan) |
Returns the equal time-spaced Earth Centered Inertial coordinates of a satellite orbit track.
|
![]() ![]() | OrbitTrack(Satellite, Double, Double, Double) |
Returns the equidistant Earth Centered Inertial coordinates of a satellite orbit track.
|
![]() ![]() | OrbitTrack(Satellite, Double, Double, TimeSpan) |
Returns the equal time-spaced Earth Centered Inertial coordinates of a satellite orbit track.
|
![]() ![]() | SolarSubpoint(WgsModel, DateTime, Double) |
Calculates the Sun's subpoint.
|
![]() ![]() | SolarSubpoint(WgsModel, Julian, Double) |
Calculates the Sun's subpoint.
|
![]() ![]() | SolarSubpointEcf(WgsModel, DateTime, Double) |
Calculates the Sun's subpoint.
|
![]() ![]() | SolarSubpointEcf(WgsModel, Julian, Double) |
Calculates the Sun's subpoint.
|
![]() ![]() | SolarSubpointEci(WgsModel, DateTime, Double) |
Calculates the Sun's subpoint.
|
![]() ![]() | SolarSubpointEci(WgsModel, Julian, Double) |
Calculates the Sun's subpoint.
|
![]() ![]() | SolarTerminator(WgsModel, DateTime, Double, Double) |
Calculates a set of points that define Earth's daylight terminator line.
|
![]() ![]() | SolarTerminator(WgsModel, Julian, Double, Double) |
Calculates a set of points that define Earth's daylight terminator line.
|
![]() ![]() | SolarTerminatorEcf(WgsModel, DateTime, Double, Double) |
Calculates a set of points that define Earth's daylight terminator line.
|
![]() ![]() | SolarTerminatorEcf(WgsModel, Julian, Double, Double) |
Calculates a set of points that define Earth's daylight terminator line.
|
![]() ![]() | SolarTerminatorEci(WgsModel, DateTime, Double, Double) |
Calculates a set of points that define Earth's daylight terminator line.
|
![]() ![]() | SolarTerminatorEci(WgsModel, Julian, Double, Double) |
Calculates a set of points that define Earth's daylight terminator line.
|
![]() ![]() | Subpoint(IOrbit, DateTime, Double) |
Returns the orbit subpoint at a given time.
|
![]() ![]() | Subpoint(IOrbit, Double, Double) |
Returns the orbit subpoint at a given time.
|
![]() ![]() | Subpoint(Satellite, DateTime, Double) |
Returns the satellite subpoint at a given time.
|
![]() ![]() | Subpoint(Satellite, Double, Double) |
Returns the satellite subpoint at a given time.
|
![]() ![]() | SubpointEcf(IOrbit, DateTime, Double) |
Returns the ECF coordinate of a satellite subpoint at a given time.
|
![]() ![]() | SubpointEcf(IOrbit, Double, Double) |
Returns the ECF coordinate of a satellite subpoint at a given time.
|
![]() ![]() | SubpointEcf(Satellite, DateTime, Double) |
Returns the ECF coordinate of a satellite subpoint at a given time.
|
![]() ![]() | SubpointEcf(Satellite, Double, Double) |
Returns the ECF coordinate of a satellite subpoint at a given time.
|