OrbitalElements Class 
Namespace: AGI.Foundation.Coordinates
The OrbitalElements type exposes the following members.
Name  Description  

ComputeEccentricity 
Calculates the eccentricity of the orbit.
 
ComputeMeanMotion 
Calculates the mean motion of the orbit.
 
ComputePeriod 
Calculates the period of the orbit.
 
ComputeRadiusOfApoapsis 
Calculates the radius of apoapsis of the orbit.
 
ComputeRadiusOfPeriapsis 
Calculates the radius of periapsis of the orbit.
 
ComputeSemilatusRectum 
Calculates the semilatus rectum of the orbit.
 
ComputeSemimajorAxis 
Calculates the semimajor axis of the orbit.
 
ComputeTimeOfFlight 
Calculates the time of flight between two true anomalies.
 
ConvertEccentricAnomalyToMeanAnomaly 
Tries to convert the eccentric anomaly to the mean anomaly.
 
ConvertEccentricAnomalyToTimeFromPeriapsis 
Converts the eccentric anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
 
ConvertEccentricAnomalyToTrueAnomaly 
Converts the eccentric anomaly to the true anomaly.
 
ConvertHyperbolicAnomalyToMeanAnomaly 
Converts the hyperbolic anomaly to the mean anomaly.
 
ConvertHyperbolicAnomalyToTimeFromPeriapsis 
Converts the hyperbolic anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
 
ConvertHyperbolicAnomalyToTrueAnomaly 
Converts the hyperbolic anomaly to the true anomaly.
 
ConvertMeanAnomalyToEccentricAnomaly 
Converts the mean anomaly to the eccentric anomaly.
 
ConvertMeanAnomalyToHyperbolicAnomaly 
Tries to convert the mean anomaly to the hyperbolic anomaly.
 
ConvertMeanAnomalyToParabolicAnomaly 
Converts the mean anomaly to the parabolic anomaly.
 
ConvertMeanAnomalyToTimeFromPeriapsis 
Converts the mean anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
 
ConvertMeanAnomalyToTimeSincePreviousPeriapsis 
Converts the mean anomaly to the time of flight since the previous periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
 
ConvertMeanAnomalyToTimeUntilNextPeriapsis 
Converts the mean anomaly to the time of flight until the next periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
 
ConvertMeanAnomalyToTrueAnomaly 
Converts the mean anomaly to the true anomaly.
 
ConvertParabolicAnomalyToMeanAnomaly 
Converts the parabolic anomaly to the mean anomaly.
 
ConvertParabolicAnomalyToTimeFromPeriapsis 
Converts the parabolic anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
 
ConvertParabolicAnomalyToTrueAnomaly 
Converts the parabolic anomaly to the true anomaly.
 
ConvertTimeFromPeriapsisToEccentricAnomaly 
Converts the time from periapsis passage to eccentric anomaly. The value returned is signed and monotonic even for periodic orbits.
 
ConvertTimeFromPeriapsisToHyperbolicAnomaly 
Converts the time from periapsis passage to hyperbolic anomaly. The value returned is signed and monotonic.
 
ConvertTimeFromPeriapsisToMeanAnomaly 
Converts the time from periapsis passage to mean anomaly. The value returned is signed and monotonic even for periodic orbits.
 
ConvertTimeFromPeriapsisToParabolicAnomaly 
Converts the time from periapsis passage to parabolic anomaly. The value returned is signed and monotonic.
 
ConvertTimeFromPeriapsisToTrueAnomaly 
Converts the time from periapsis passage to true anomaly. The value returned is signed and monotonic even for periodic orbits.
 
ConvertTrueAnomalyToEccentricAnomaly 
Converts the true anomaly to the eccentric anomaly.
 
ConvertTrueAnomalyToHyperbolicAnomaly 
Converts the true anomaly to the hyperbolic anomaly.
 
ConvertTrueAnomalyToMeanAnomaly 
Converts the true anomaly to the mean anomaly.
 
ConvertTrueAnomalyToParabolicAnomaly 
Converts the true anomaly to the parabolic anomaly.
 
ConvertTrueAnomalyToTimeFromPeriapsis 
Converts the true anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
 
ConvertTrueAnomalyToTimeSincePreviousPeriapsis 
Converts the true anomaly to the time of flight since the previous periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
 
ConvertTrueAnomalyToTimeUntilNextPeriapsis 
Converts the true anomaly to the time of flight until the next periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
 
PerifocalToCartesianMatrix 
Calculates the transformation matrix from the perifocal axes to the inertial axes.
 
TryComputeEccentricity 
Tries to calculate the eccentricity of the orbit.
 
TryComputeMeanMotion 
Tries to calculate the mean motion of the orbit.
 
TryComputePeriod 
Tries to calculate the period of the orbit.
 
TryComputeRadiusOfApoapsis 
Tries to calculate the radius of apoapsis of the orbit.
 
TryComputeRadiusOfPeriapsis 
Tries to calculate the radius of periapsis of the orbit.
 
TryComputeSemilatusRectum 
Tries to calculate the semilatus rectum of the orbit.
 
TryComputeSemimajorAxis 
Tries to calculate the semimajor axis of the orbit.
 
TryComputeTimeOfFlight 
Tries to calculate the time of flight between two true anomalies.
 
TryConvertEccentricAnomalyToMeanAnomaly 
Tries to convert the eccentric anomaly to the mean anomaly.
 
TryConvertEccentricAnomalyToTimeFromPeriapsis 
Tries to convert the eccentric anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
 
TryConvertEccentricAnomalyToTrueAnomaly 
Tries to convert the eccentric anomaly to the true anomaly.
 
TryConvertHyperbolicAnomalyToMeanAnomaly 
Tries to convert the hyperbolic anomaly to the mean anomaly.
 
TryConvertHyperbolicAnomalyToTimeFromPeriapsis 
Tries to convert the hyperbolic anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
 
TryConvertHyperbolicAnomalyToTrueAnomaly 
Tries to convert the hyperbolic anomaly to the true anomaly.
 
TryConvertMeanAnomalyToEccentricAnomaly 
Tries to convert the mean anomaly to the eccentric anomaly.
 
TryConvertMeanAnomalyToHyperbolicAnomaly 
Tries to convert the mean anomaly to the hyperbolic anomaly.
 
TryConvertMeanAnomalyToParabolicAnomaly 
Tries to convert the mean anomaly to the parabolic anomaly.
 
TryConvertMeanAnomalyToTimeFromPeriapsis 
Tries to convert the mean anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
 
TryConvertMeanAnomalyToTimeSincePreviousPeriapsis 
Tries to convert the mean anomaly to the time of flight since the previous periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
 
TryConvertMeanAnomalyToTimeUntilNextPeriapsis 
Tries to convert the mean anomaly to the time of flight until the next periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
 
TryConvertMeanAnomalyToTrueAnomaly 
Tries to convert the mean anomaly to the true anomaly.
 
TryConvertParabolicAnomalyToMeanAnomaly 
Tries to convert the parabolic anomaly to the mean anomaly.
 
TryConvertParabolicAnomalyToTimeFromPeriapsis 
Tries to convert the parabolic anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
 
TryConvertParabolicAnomalyToTrueAnomaly 
Tries to convert the parabolic anomaly to the true anomaly.
 
TryConvertTimeFromPeriapsisToEccentricAnomaly 
Tries to convert the time from periapsis passage to eccentric anomaly. The value returned is signed and monotonic even for periodic orbits.
 
TryConvertTimeFromPeriapsisToHyperbolicAnomaly 
Tries to convert the time from periapsis passage to hyperbolic anomaly. The value returned is signed and monotonic.
 
TryConvertTimeFromPeriapsisToMeanAnomaly 
Tries to convert the time from periapsis passage to mean anomaly. The value returned is signed and monotonic even for periodic orbits.
 
TryConvertTimeFromPeriapsisToParabolicAnomaly 
Tries to convert the time from periapsis passage to parabolic anomaly. The value returned is signed and monotonic.
 
TryConvertTimeFromPeriapsisToTrueAnomaly 
Tries to convert the time from periapsis passage to true anomaly. The value returned is signed and monotonic even for periodic orbits.
 
TryConvertTrueAnomalyToEccentricAnomaly 
Tries to convert the true anomaly to the eccentric anomaly.
 
TryConvertTrueAnomalyToHyperbolicAnomaly 
Tries to convert the true anomaly to the hyperbolic anomaly.
 
TryConvertTrueAnomalyToMeanAnomaly 
Tries to convert the true anomaly to the mean anomaly.
 
TryConvertTrueAnomalyToParabolicAnomaly 
Tries to convert the true anomaly to the parabolic anomaly.
 
TryConvertTrueAnomalyToTimeFromPeriapsis 
True to convert the true anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
 
TryConvertTrueAnomalyToTimeSincePreviousPeriapsis 
Tries to convert the true anomaly to the time of flight since the previous periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
 
TryConvertTrueAnomalyToTimeUntilNextPeriapsis 
Tries to convert the true anomaly to the time of flight until the next periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
