SGPdotNET.Propagation.Sgp4 Class Reference

The Simplified General Perturbations (Model 4) propagator. More...

Public Member Functions
	Sgp4 (Tle tle)
	Constructor.
EciCoordinate	FindPosition (double tsince)
	Predicts the ECI position of a satellite at a time relative to the satellite's epoch.
EciCoordinate	FindPosition (DateTime date)
	Predicts the ECI position of a satellite at a specific date and time.

Public Attributes
readonly Orbit	Orbit
	The orbit information of the satellite.

Detailed Description

The Simplified General Perturbations (Model 4) propagator.

Constructor & Destructor Documentation

Sgp4()

SGPdotNET.Propagation.Sgp4.Sgp4 ( Tle  tle )

inline

Constructor.

Parameters

tle	The two-line element set to propogate

Member Function Documentation

FindPosition() [1/2]

EciCoordinate SGPdotNET.Propagation.Sgp4.FindPosition ( DateTime  date )

inline

Predicts the ECI position of a satellite at a specific date and time.

Parameters

date	the date and time to predict

Returns

The predicted position of the satellite at a specific date and time

FindPosition() [2/2]

EciCoordinate SGPdotNET.Propagation.Sgp4.FindPosition ( double  tsince )

inline

Predicts the ECI position of a satellite at a time relative to the satellite's epoch.

Parameters

tsince

Time since the satellite's epoch

Returns

The predicted position of the satellite at a time relative to the satellite's epoch

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The documentation for this class was generated from the following file:

• Src/CommonCore/TPG.GDK.CommonCore.Satellite/SgpNet/Propagation/SGP4.cs