Particle spectra at low Earth orbits

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Date & Time
Orbit parameters | Select Satellite
Mean motion:
Inclination (i):
Right Ascension
of ascending node:
Eccentricity (e):
Argument of perigee
at epoch (ω):
Mean anomaly from
perigee at epoch (M0):
Orbit decay rate:
Display results:
If you choose later than 1st of March 2020, you will get experimental not tested model results for GOES16 and if you choose earlier than 2010, you will get untested results for goes 6-11