Struct Omm 

pub struct Omm {

    pub ccsds_omm_vers: String,
    pub creation_date: Option<String>,
    pub originator: Option<String>,
    pub object_name: Option<String>,
    pub object_id: Option<String>,
    pub center_name: Option<String>,
    pub ref_frame: Option<String>,
    pub time_system: Option<String>,
    pub mean_element_theory: Option<String>,
    pub epoch: OmmEpoch,
    pub mean_motion: f64,
    pub eccentricity: f64,
    pub inclination_deg: f64,
    pub ra_of_asc_node_deg: f64,
    pub arg_of_pericenter_deg: f64,
    pub mean_anomaly_deg: f64,
    pub ephemeris_type: i32,
    pub classification_type: String,
    pub norad_cat_id: u32,
    pub element_set_no: i32,
    pub rev_at_epoch: i64,
    pub bstar: f64,
    pub mean_motion_dot: f64,
    pub mean_motion_ddot: f64,
}

Canonical, format-agnostic OMM container.

Pure data: it knows nothing about KVN/XML/JSON serialization. The numeric element values use standard astrodynamic units (angles in degrees, mean motion in revolutions/day, its derivatives in rev/day^2 and rev/day^3, B* in inverse earth-radii) and are stored as directly parsed f64s, so every encoding decodes to the same value.

Fields

ccsds_omm_vers: String

creation_date: Option<String>

originator: Option<String>

object_name: Option<String>

object_id: Option<String>

International designator, CCSDS form (e.g. "1998-067A").

center_name: Option<String>

ref_frame: Option<String>

time_system: Option<String>

mean_element_theory: Option<String>

epoch: OmmEpoch

mean_motion: f64

Mean motion, revolutions per day.

eccentricity: f64

Eccentricity, dimensionless, in [0, 1).

inclination_deg: f64

Inclination, degrees.

ra_of_asc_node_deg: f64

Right ascension of the ascending node, degrees.

arg_of_pericenter_deg: f64

Argument of pericenter, degrees.

mean_anomaly_deg: f64

Mean anomaly, degrees.

ephemeris_type: i32

classification_type: String

norad_cat_id: u32

element_set_no: i32

rev_at_epoch: i64

bstar: f64

SGP4 drag term B*, inverse earth-radii.

mean_motion_dot: f64

First derivative of mean motion, rev/day^2.

mean_motion_ddot: f64

Second derivative of mean motion, rev/day^3.

Implementations

impl Omm

pub fn to_element_set(&self) -> Result<ElementSet, OmmError>

Convert the canonical OMM elements into the SGP4 ElementSet consumed by Satellite::from_elements.

The epoch is converted directly from the OMM calendar timestamp into SGP4’s split Julian date, preserving years outside the TLE pivot range. B* and the second mean-motion derivative are quantized onto the TLE assumed-decimal grid because those GP parameters originate in that field format.

Trait Implementations

impl Clone for Omm

fn clone(&self) -> Omm

Returns a duplicate of the value.

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

Performs copy-assignment from source.

impl Debug for Omm

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

Formats the value using the given formatter.

impl PartialEq for Omm

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

Tests for self and other values to be equal, and is used by ==.

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

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

impl StructuralPartialEq for Omm