Struct sgp4::tle::TLE

pub struct TLE {
    pub name: String,
    pub sat_number: u32,
    pub classification: char,
    pub int_designator: String,
    pub epoch_year: u16,
    pub epoch_day: f64,
    pub first_mean_motion: f64,
    pub second_mean_motion: f64,
    pub bstar: f64,
    pub tle_version: u16,
    pub i: f64,
    pub raan: f64,
    pub e: f64,
    pub omega: f64,
    pub mean_anomaly: f64,
    pub mean_motion: f64,
    pub revolution_number: u32,
}

Satellite elements from a TLE file

Read "Two Line Element" files that are a standard way of distributing defined orbits.

Fields

name	Name of the object
sat_number	The Satellite Catalog Number, a sequential 5-digit number assigned by United States Space Command to all Earth orbiting satellites.
classification	Classification (U=Unclassified)
int_designator	International Designator
epoch_year	Epoch Year
epoch_day	Epoch Day
first_mean_motion	First Time Derivative of the Mean Motion
second_mean_motion	Second Time Derivative of Mean Motion
bstar	BSTAR drag term
tle_version	Element set number (Incremented when a new TLE is generated for this object)
i	Inclination
raan	Right ascension of the ascending node
e	Eccentricity
omega	Argument of perigee
mean_anomaly	Mean Anomaly
mean_motion	Mean Motion (revolutions per day)
revolution_number	Revolution number at epoch (revolutions)