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Flying the Apollo 17 mission (was IMFD 5 base approach Q)
Hello experts,
I was wondering, when using the base approach program and adjust NUM to 0.000 I end up over the previously defined target base right at my very first revolution after orbit insertion, which is fine so far. However, is there a way I can also tell IFMD several hours before orbit insertion (planet approach phase), to have my orbit not only pass right over the target base but also that the apex* of the orbit will be over the target base as well?
*with apex I mean the point of the orbit with the highest latitude (halfway between the ascending node and descending node), here in my case it is a retrograde lunar orbit and at the apex my velocity vector would be pointing to heading of exactly 270°.
Any feedback appreciated.
Hello experts,
I was wondering, when using the base approach program and adjust NUM to 0.000 I end up over the previously defined target base right at my very first revolution after orbit insertion, which is fine so far. However, is there a way I can also tell IFMD several hours before orbit insertion (planet approach phase), to have my orbit not only pass right over the target base but also that the apex* of the orbit will be over the target base as well?
*with apex I mean the point of the orbit with the highest latitude (halfway between the ascending node and descending node), here in my case it is a retrograde lunar orbit and at the apex my velocity vector would be pointing to heading of exactly 270°.
Any feedback appreciated.
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