i have a question.....
design all orbital elements:
a, b, c, e, E, ralpha, inc, omega, tv, and T ?
given:
r, v, mue
mue (u) : 398600 km3/ s2
r (vector) : [in matrix form] [10000
7000
3000] km
v (vector) : in matrix form [ 8.5
2.3
4 ] km/s
...............................................................
i know how to solv in normally but not in matrix form...
so i hope any one can help me