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Good evening everyone, We know that the point of interest of any elliptical orbitiis located at the perigee... If I have the 6 orbital elements how to calculate the location on the earth surface (latitude and longitude) of this point????

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  • $\begingroup$ I'm sorry, I don't understand your question. Why is that the point of interest? What are you trying to get? $\endgroup$ – Rory Alsop Feb 14 at 10:42
  • $\begingroup$ The point of interest is the latitude and longitude of the perigee point which has been chosen during the design of orbit of satellite.. If I know the orbital elements how can I calculate the location on earth of this point? $\endgroup$ – Khaled Yassin Feb 15 at 14:13

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