pylupnt.TLE

class pylupnt.TLE

Two-line element set describing a satellite’s mean orbital elements.

property arg_perigee

Argument of perigee [deg].

property bstar

B* drag term [1/R_EARTH].

property eccentricity

Eccentricity [-].

property epoch_day

Day of year and fraction of the epoch [day].

property epoch_tai

Epoch [s TAI].

property epoch_year

Last two digits of the epoch year [yr].

static from_file(filename: str) → list[pylupnt._pylupnt.TLE]

Parse all TLEs from a file, returning a list.

static from_lines(line1: str, line2: str, line3: str) → pylupnt._pylupnt.TLE

Parse a TLE from a name line plus the two element lines.

property inclination

Inclination [deg].

property mean_anomaly

Mean anomaly [deg].

property mean_motion

Mean motion [revs/day].

property name

Satellite name.

property prn

PRN / catalog number.

property raan

Right ascension of the ascending node [deg].