Understanding How much orbit energy
For an elliptic orbit the specific orbital energy is the negative of the additional energy required to accelerate a mass of one kilogram to escape velocity (parabolic orbit). For a hyperbolic orbit, it is equal to the excess energy compared to that of a parabolic orbit.
In the , the specific orbital energy $${\displaystyle \varepsilon }$$ (or specific vis-viva energy) of twois the constant quotient of their(the sum of their mutual
ISSThehas anof 91.74 minutes (5504 s), hence bythe semi-major axis of its orbit is 6,738 km.The specific orbital energy associated with this orbit is −29.6.
For an elliptic orbit the rate of change of the specific orbital energy with respect to a change in the semi-major axis is $${\displaystyle {\frac {\mu }{2a^{2}}}}$$ where• $${\displaystyle \mu ={G}(m_{1}+m_{2})}$$ is the
Assume:• a is the acceleration due to(the time-rate at whichis spent)• g is.
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