Answer:
The answer is the fourth option, 5.
"For a satellite orbit, the Earth with an elliptical orbit modeled by..." the maximum distance between the satellite and the Earth is
D= 510 km. Option B. This is further explained below.
<h3>What is Kepler Orbit?</h3>
Generally, In the study of astrodynamics, an ellipse of the satellite is often referred to as a Kepler Orbit
The function of the elliptical orbit is
![\frac{(x-h)^2}{a^2}+\frac{(x-k)^2}{b^2}=1](https://tex.z-dn.net/?f=%5Cfrac%7B%28x-h%29%5E2%7D%7Ba%5E2%7D%2B%5Cfrac%7B%28x-k%29%5E2%7D%7Bb%5E2%7D%3D1)
compared to
![\frac{(x^2)^2}{47334400}+\frac{(y^2)^2}{43956900}=1](https://tex.z-dn.net/?f=%5Cfrac%7B%28x%5E2%29%5E2%7D%7B47334400%7D%2B%5Cfrac%7B%28y%5E2%29%5E2%7D%7B43956900%7D%3D1)
Hence
a = √(47,334,400 km²)
a= 6,880 km.
In conclusion, The distance of the satellite above the Earth's surface.
D = a - r
D= 6,880 km - 6,370 km
D= 510 km
Read more about elliptical orbit
at brainly.com/question/13999216
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Answer:
B, C, D and E. A and F are incorrect
Step-by-step explanation:
Her Grandson Travis. Walter asks what she has done. Ruth is in the kitchen, Travis runs in and Mama tells Travis she went out and bought a house