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Statistics
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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Abolfazl Shirazi
. All Rights Reserved.