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Homa - Online Space Orbit SimulatorHoma - Online Space Orbit Simulator

Orbit Simulation

Eccentricity:
e
 Semimajor Axis (km):
a
 True Anomaly (deg):
θ
Inclination (deg):
i
 Argument of Perigee (deg):
ω
 Right Ascension (deg):
Ω






Homa is optimized for learning orbital mechanics and analyzing space orbits. Results are constantly reviewed to avoid errors, but full correctness of all contents cannot be warranted.
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