Homework $2(1)$

Given:

Find $E_o($slide $20)$

Find $v_o($slide $21)$

Find $M_o$

Find time of flight from perigee

to $v_o$

Find time of flight from $v_o$ to $v=65$

Verify: Starting at $v_o,$ compute the

true anomaly after the time of flight

computed above.

Use MatLab to solve these. Show your code.Starting at $v_o,$ what is the true

anomaly after $2700$ seconds?

Starting at $v_o,$ what is the true

anomaly after exactly two orbit

periods?

What is the true anomaly after

$15000$ seconds?