Getting satellite exp
[link to documentation (https://rhodesmill.org/skyfield/toc.html)]
study about
free space propagation model frisyw separate atenuation models Know how to calculate them separatly and know which function calculate whats then sum all attenuation up
Trying to get the real altitude between observer and sat
Should satellite be a class ?
Thing is I don't know if the library I'm using is good enough
and if my angle calculations are good.
I can get infos from satellites TLE and know even how to download
and manipulate many of them - I didnt implement it because my computer
was going to explode.
I still don't know what is wrong with the attenuation rechnungen but I think
the problem is in the values I choose...
Or the problem is my PC, because even the example is not working.
-> calculate.py
Mixes realtime with the first attenuation example:
https://itu-rpy.readthedocs.io/en/latest/quickstart.html
and
https://rhodesmill.org/skyfield/earth-satellites.html
''' from skyfield.api import EarthSatellite, load from datetime import datetime
ts = load.timescale() line1 = '1 01520U 65065H 24004.88423715 .00000109 00000+0 19149-3 0 9994' line2 = '2 01520 89.9593 128.8254 0070679 106.6182 14.1898 13.36021334843288' satellite = EarthSatellite(line1, line2, 'Calisto', ts) print(satellite) '''
''' active_stations_url = 'http://celestrak.org/NORAD/elements/stations.txt' satellites = load.tle_file(active_stations_url) print('Loaded', len(satellites), 'satellites') '''
Make global time = load.timescale
then after use t = time.now()