ARGUMENT OF PERIGEE

w



 

The Argument of Perigee (w) is defined as the angle within the satellite orbit plane that is measured from the Ascending Node (W) to the perigee point (p) along the satellite's direction of travel.

The value of the Argument of Perigee can be anywhere from 0 to 360 degrees.




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Argument of Perigee Was Last Modified On May 23, 2010