Functions
template<typename T >
T	EGXPhys::Apoapsis (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis of an orbiting body. More...

template<typename T >
T	EGXPhys::Apocenter (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis of an orbiting body. More...

template<typename T >
T	EGXPhys::Apofocus (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis of an orbiting body. More...

template<typename T >
T	EGXPhys::Apogalacticon (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around a galaxy. More...

template<typename T >
T	EGXPhys::Apobothron (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around a black hole. More...

template<typename T >
T	EGXPhys::Aponigricon (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around a black hole. More...

template<typename T >
T	EGXPhys::Apastron (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around a star. More...

template<typename T >
T	EGXPhys::Aphelion (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around the Sun. More...

template<typename T >
T	EGXPhys::Apohermion (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Mercury. More...

template<typename T >
T	EGXPhys::Apocytherion (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Venus. More...

template<typename T >
T	EGXPhys::Apogee (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Earth. More...

template<typename T >
T	EGXPhys::Apolune (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Moon. More...

template<typename T >
T	EGXPhys::Apocynthion (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Moon. More...

template<typename T >
T	EGXPhys::Aposelene (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Moon. More...

template<typename T >
T	EGXPhys::Apoareion (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Mars. More...

template<typename T >
T	EGXPhys::Apozene (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Jupiter. More...

template<typename T >
T	EGXPhys::Apojove (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Jupiter. More...

template<typename T >
T	EGXPhys::Apochron (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Saturn. More...

template<typename T >
T	EGXPhys::Apokrone (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Saturn. More...

template<typename T >
T	EGXPhys::Aposaturnium (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Saturn. More...

template<typename T >
T	EGXPhys::Apouranion (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Uranus. More...

template<typename T >
T	EGXPhys::Apoposeidon (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Neptune. More...

template<typename T >
T	EGXPhys::Apohadion (const T &orbitalEccentricity, const T &semiMajorAxisInm)
	Calculates apoapsis around Pluto. More...

Detailed Description

Calculates apoapsis of an orbiting body.

Function Documentation

◆ Apastron()

template<typename T >

T EGXPhys::Apastron	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around a star.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apastron for the orbiting body.

See also: Apoapsis() for more info.

◆ Aphelion()

template<typename T >

T EGXPhys::Aphelion	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around the Sun.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Aphelion for the orbiting body.

See also: Apoapsis() for more info.

◆ Apoapsis()

template<typename T >

T EGXPhys::Apoapsis	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis of an orbiting body.

The apoapsis is the distance at which an orbiting object is farthest away from the body it is orbiting.

\[r=a(1+e)\]

See https://en.wikipedia.org/wiki/Apsis

Equation taken from http://mathworld.wolfram.com/Apoapsis.html

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apoapsis for the orbiting body.

See also: Apocenter() alternative name.; Apofocus() alternative name.; Apogalacticon() apoapsis around a galaxy.; Apobothron() apoapsis around a black hole.; Aponigricon() apoapsis around a black hole.; Apastron() apoapsis around a star.; Aphelion() apoapsis around the Sun.; Apohermion() apoapsis around Mercury.; Apocytherion() apoapsis around Venus.; Apogee() apoapsis around Earth.; Apolune() apoapsis around Moon.; Apocynthion() apoapsis around Moon.; Aposelene() apoapsis around Moon.; Apoareion() apoapsis around Mars.; Apozene() apoapsis around Jupiter.; Apojove() apoapsis around Jupiter.; Apochron() apoapsis around Saturn.; Apokrone() apoapsis around Saturn.; Aposaturnium() apoapsis around Saturn.; Apouranion() apoapsis around Uranus.; Apoposeidon() apoapsis around Neptune.; Apohadion() apoapsis around Pluto.

◆ Apoareion()

template<typename T >

T EGXPhys::Apoareion	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Mars.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apoareion for the orbiting body.

See also: Apoapsis() for more info.

◆ Apobothron()

template<typename T >

T EGXPhys::Apobothron	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around a black hole.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apobothron for the orbiting body.

See also: Apoapsis() for more info.; Aponigricon() alternative name.

◆ Apocenter()

template<typename T >

T EGXPhys::Apocenter	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis of an orbiting body.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apocenter for the orbiting body.

See also: Apoapsis() for more info.; Apofocus() alternative name.

◆ Apochron()

template<typename T >

T EGXPhys::Apochron	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Saturn.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apochron for the orbiting body.

See also: Apoapsis() for more info.; Apochron() alternative name.; Aposaturnium() alternative name.

◆ Apocynthion()

template<typename T >

T EGXPhys::Apocynthion	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Moon.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apocynthion for the orbiting body.

See also: Apoapsis() for more info.; Apolune() alternative name.; Aposelene() alternative name.

◆ Apocytherion()

template<typename T >

T EGXPhys::Apocytherion	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Venus.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apocytherion for the orbiting body.

See also: Apoapsis() for more info.

◆ Apofocus()

template<typename T >

T EGXPhys::Apofocus	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis of an orbiting body.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apofocus for the orbiting body.

See also: Apoapsis() for more info.; Apocenter() alternative name.

◆ Apogalacticon()

template<typename T >

T EGXPhys::Apogalacticon	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around a galaxy.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apogalacticon for the orbiting body.

See also: Apoapsis() for more info.

◆ Apogee()

template<typename T >

T EGXPhys::Apogee	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Earth.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apogee for the orbiting body.

See also: Apoapsis() for more info.

◆ Apohadion()

template<typename T >

T EGXPhys::Apohadion	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Pluto.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apohadion for the orbiting body.

See also: Apoapsis() for more info.

◆ Apohermion()

template<typename T >

T EGXPhys::Apohermion	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Mercury.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apohermion for the orbiting body.

See also: Apoapsis() for more info.

◆ Apojove()

template<typename T >

T EGXPhys::Apojove	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Jupiter.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apojove for the orbiting body.

See also: Apoapsis() for more info.; Apozene() alternative name.

◆ Apokrone()

template<typename T >

T EGXPhys::Apokrone	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Saturn.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apokrone for the orbiting body.

See also: Apoapsis() for more info.; Apochron() alternative name.; Aposaturnium() alternative name.

◆ Apolune()

template<typename T >

T EGXPhys::Apolune	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Moon.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apolune for the orbiting body.

See also: Apoapsis() for more info.; Apocynthion() alternative name.; Aposelene() alternative name.

◆ Aponigricon()

template<typename T >

T EGXPhys::Aponigricon	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around a black hole.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Aponigricon for the orbiting body.

See also: Apoapsis() for more info.; Apobothron() alternative name.

◆ Apoposeidon()

template<typename T >

T EGXPhys::Apoposeidon	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Neptune.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apoposeidon for the orbiting body.

See also: Apoapsis() for more info.

◆ Aposaturnium()

template<typename T >

T EGXPhys::Aposaturnium	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Saturn.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Aposaturnium for the orbiting body.

See also: Apoapsis() for more info.; Apochron() alternative name.; Apokrone() alternative name.

◆ Aposelene()

template<typename T >

T EGXPhys::Aposelene	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Moon.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Aposelene for the orbiting body.

See also: Apoapsis() for more info.; Apolune() alternative name.; Apocynthion() alternative name.

◆ Apouranion()

template<typename T >

T EGXPhys::Apouranion	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Uranus.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apouranion for the orbiting body.

See also: Apoapsis() for more info.

◆ Apozene()

template<typename T >

T EGXPhys::Apozene	(	const T &	orbitalEccentricity,
		const T &	semiMajorAxisInm
	)

Calculates apoapsis around Jupiter.

Parameters

orbitalEccentricity	\( e\ (dimensionless)\) Eccentricity of the orbit. Eccentricity is the amount by which an objects orbit around another body deviates from a perfect circle. e=0 is circular, 0<e<1 is elliptical and e>1 is hyperbola. See https://en.wikipedia.org/wiki/Orbital_eccentricity.
semiMajorAxisInm	\( a\ (m)\) Semi-major axis of the orbit in meters. This is the line segment from the center of the orbit to the widest point in the perimiter. See https://en.wikipedia.org/wiki/Semi-major_and_semi-minor_axes.

Returns: \( r\ (m)\) Apozene for the orbiting body.

See also: Apoapsis() for more info.; Apojove() alternative name.

Functions

Detailed Description

Function Documentation

◆ Apastron()

◆ Aphelion()

◆ Apoapsis()

◆ Apoareion()

◆ Apobothron()

◆ Apocenter()

◆ Apochron()

◆ Apocynthion()

◆ Apocytherion()

◆ Apofocus()

◆ Apogalacticon()

◆ Apogee()

◆ Apohadion()

◆ Apohermion()

◆ Apojove()

◆ Apokrone()

◆ Apolune()

◆ Aponigricon()

◆ Apoposeidon()

◆ Aposaturnium()

◆ Aposelene()

◆ Apouranion()

◆ Apozene()