Struct sgp4_rs::ClassicalOrbitalElements

pub struct ClassicalOrbitalElements {
    pub semilatus_rectum: Length,
    pub semimajor_axis: Length,
    pub eccentricity: f64,
    pub inclination: Angle,
    pub raan: Angle,
    pub argument_of_perigee: Angle,
    pub true_anomaly: Angle,
    pub mean_anomaly: Angle,
    pub argument_of_latitude: Angle,
    pub true_longitude: Angle,
    pub longitude_of_periapsis: Angle,
}

A Keplerian orbital element set.

This structure contains all of the “classical” orbital elements as derivable from a TLE. We lean on the uom crate to provide safe dimensional types which help to avoid bugs related to mixing units of measure.

Fields

semilatus_rectum: Length

semimajor_axis: Length

eccentricity: f64

inclination: Angle

raan: Angle

argument_of_perigee: Angle

true_anomaly: Angle

mean_anomaly: Angle

argument_of_latitude: Angle

true_longitude: Angle

longitude_of_periapsis: Angle

Trait Implementations

impl Clone for ClassicalOrbitalElements

fn clone(&self) -> ClassicalOrbitalElements

Returns a copy of the value.

fn clone_from(&mut self, source: &Self)

Performs copy-assignment from source.

impl Debug for ClassicalOrbitalElements

fn fmt(&self, f: &mut Formatter<'_>) -> Result

Formats the value using the given formatter.

impl From<StateVector> for ClassicalOrbitalElements

fn from(sv: StateVector) -> Self

Converts to this type from the input type.

impl PartialEq<ClassicalOrbitalElements> for ClassicalOrbitalElements

fn eq(&self, other: &ClassicalOrbitalElements) -> bool

This method tests for self and other values to be equal, and is used by ==.

fn ne(&self, other: &Rhs) -> bool

This method tests for !=. The default implementation is almost always sufficient, and should not be overridden without very good reason.

impl Copy for ClassicalOrbitalElements

impl StructuralPartialEq for ClassicalOrbitalElements