For the problem above, perform a quadrant check to determine which of the two possible

angles is the actual argument of perigee, $.$

Given: $e=0\mathrm{.}1469i+0\mathrm{.}1314j+0\mathrm{.}1066k($unitless$)$

From a known position and velocity vectors, determine orbit

a$.$ specific mechanical energy

b$.$ apogee altitude

c$.$ perigee altitude

Given: $r=3207i+5459j+2714kkm$ and $v=-6\mathrm{.}532i+0\mathrm{.}7835j+6\mathrm{.}142kk\frac{m}{s}$

From a known position and velocity vectors, determine the six classical orbital elements.

Given: $r=3207i+5459j+2714kkm$ and $v=-6\mathrm{.}532i+0\mathrm{.}7835j+6\mathrm{.}142kk\frac{m}{s}$