8. A spacecraft is in an elliptical orbit around the earth. At the time t=0 hours, it is at its apogee (highest point), 1000 km above the earth's surface. It is at its perigee (lowest point), 100 km above the surface 50 minutes later. Assuming that distance from the earth varies sinusoldally with time, write an equation and find the first 3 positive values of t for which the spacecraft is 200 km from the surface. Apogee Perigee

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Chapter1: Units, Trigonometry. And Vectors
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A spacecraft is in an elliptical orbit around the earth. At th etime t = 0 hours, it is at its apogee (highest point), 1000 km above the earth's surface. It is at its perigee (lowest point), 100 km above the surface 50 minutes later. Assuming that distance from the earth varies sinusoidally with time, write an equation and find the first 3 positive values of t for which the spacecraft is 200 km from the surface. 

8. A spacecraft is in an elliptical orbit around the earth. At the time t=0 hours, it is at its apogee (highest
point), 1000 km above the earth's surface. It is at its perigee (lowest point), 100 km above the surface
50 minutes later. Assuming that distance from the earth varies sinusoldally with time, write an equation
and find the first 3 positive values of t for which the spacecraft is 200 km from the surface.
Apogee
Perigee
Transcribed Image Text:8. A spacecraft is in an elliptical orbit around the earth. At the time t=0 hours, it is at its apogee (highest point), 1000 km above the earth's surface. It is at its perigee (lowest point), 100 km above the surface 50 minutes later. Assuming that distance from the earth varies sinusoldally with time, write an equation and find the first 3 positive values of t for which the spacecraft is 200 km from the surface. Apogee Perigee
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