perturb::StateVector Struct Reference

Represents the output prediction from SGP4. More...

#include <perturb.hpp>

Public Attributes
JulianDate	epoch
	Time-stamp of the state vector.
Vec3	position
	Position in the TEME frame in [km].
Vec3	velocity
	Velocity in the TEME frame in [km/s].

Detailed Description

Represents the output prediction from SGP4.

Generated by Satellite::propagate method. The vectors are represented in the TEME (True Equator Mean Equinox) reference frame. Can be converted to classical orbital elements with the ClassicalOrbitalElements type.

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

• /github/workspace/include/perturb/perturb.hpp