Expand description
§Satellite
Modular set of functions for SGP4 and SDP4 propagation of TLEs.
Modules§
Structs§
- EcfVec3
- EciVec3
- Geodetic
Location - Look
Angles - Range
Err - SatRec
- Satellite record containing description of orbit.
- Sgp4
Result - Topocentric
Enums§
Functions§
- degrees_
lat - degrees_
long - degrees_
to_ radians - doppler_
factor - ecf_
to_ eci - ecf_
to_ look_ angles - eci_
to_ ecf - eci_
to_ geodetic - geodetic_
to_ ecf - get_
constants - gstime
- jday
- jday_
date - propagate
- propagate_
date - radians_
lat - radians_
long - radians_
to_ degrees - sgp4
- twoline2satrec
- Return a Satellite imported from two lines of TLE data.Provide the two TLE lines as strings
longstr1andlongstr2,and select which standard set of gravitational constants you wantby providinggravity_constants:sgp4.propagation.wgs72- Standard WGS 72 modelsgp4.propagation.wgs84- More recent WGS 84 modelsgp4.propagation.wgs72old- Legacy support for old SGP4 behaviorNormally, computations are made using letious recent improvementsto the algorithm. If you want to turn some of these off and goback into “afspc” mode, then setafspc_modetoTrue.