Perhaps the angle between the two vectors must be 90 degrees? It might not be the perigee point. Just figured it out by playing with the perigee angle..the northernmost point will remain 90 degrees from the ascending node. What do you guys think?
Homework Statement
A satellite is orbiting Earth with a period time of T=110 min.
At the ascending node, the state vector of the satellite is rAN =[4500 7100 ?]T km
At the northernmost latitude, the state vector of the satellite is rn=[1700 ? 7000]T km. The question marks imply that the...