Respuesta :
Consider the attached ellipse. Let the sun be at the right focus. Then perihelion is at right vertex on the x-axis and aphelion is at the left vertex on the x-axis.
The distances:
- from perihelion to the sun in terms of ellipse is a-c;
- from aphelion to the sun in terms of ellipse is a+c.
Then
[tex]\left\{\begin{array}{l}a-c=741,000,000\\a+c=817,000,000\end{array}\right.[/tex]
Add these two equations:
[tex]2a=1,558,000,000 \\ \\a=779,000,000[/tex]
and subtract first equation from the second:
[tex]2c=76,000,000 \\ \\c=38,000,000.[/tex]
Note that [tex]b=\sqrt{a^2-c^2},[/tex] thus
[tex]b=\sqrt{779,000,000^2-38,000,000^2}=\sqrt{605,397,000,000,000,000}.[/tex]
The equation for the planet's orbit is
[tex]\dfrac{x^2}{a^2}+\dfrac{y^2}{b^2}=1\Rightarrow \dfrac{x^2}{606,841,000,000,000,000}+\dfrac{y^2}{605,397,000,000,000,000}=1.[/tex]
Answer:
The shape of planetary orbits follows from the observed fact that the force of gravity between two objects depends on the square of the distance between them. ... Ellipses are closed so the planets we see in elliptical orbits stick around.
Step-by-step explanation: