OrbitalElement Class Reference

Inheritance diagram for OrbitalElement:

Collaboration diagram for OrbitalElement:

Classes
struct	Epoch

Public Member Functions
	OrbitalElement ()
	Default constructor.
	OrbitalElement (unsigned int id)
	Constructor from ID.
	OrbitalElement (const OrbitalElement &other)=default
	Copy constructor.
OrbitalElement &	operator= (const OrbitalElement &other)=default
	Copy assignemnt.
bool	isValid () const
	Returns true, if this represents a valid satellite information.
unsigned int	id () const
	Returns the NORAD catalog id.
const QString &	name () const
	Retunrs the name of the satellite.
const Epoch &	epoch () const
	Epoch of the orbital elements.
double	meanMotion () const
	Returns the mean motion.
double	meanMotionDerivative () const
	Returns the first derivative of the mean motion.
double	inclination () const
	Returns the inclination.
double	ascension () const
	Returns the right ascension of the ascending node.
double	eccentricity () const
	Returns the eccentricity.
double	perigee () const
	Returns the argument of perigee.
double	meanAnomaly () const
	Returns the mean anomaly.
unsigned int	revolutionNumber () const
	Returns the revolution number.

Static Public Member Functions
static OrbitalElement	fromCelesTrak (const QJsonObject &obj)

Protected Attributes
unsigned int	_id
QString	_name
Epoch	_epoch
double	_meanMotion
double	_meanMotionDerivative
double	_inclination
double	_ascension
double	_eccentricity
double	_perigee
double	_meanAnomaly
unsigned int	_revolutionNumber

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

• /builddir/build/BUILD/qdmr-0.12.1-build/qdmr-0.12.1/lib/orbitalelementsdatabase.hh
• /builddir/build/BUILD/qdmr-0.12.1-build/qdmr-0.12.1/lib/orbitalelementsdatabase.cc