The position vector of the International Space Station `text{(S)}`, when visible above the horizon from a radar tracking location `text{(O)}` on the surface of Earth, is modelled by
`underset ~r(t) = 6800 sin(pi(1.3t-0.1))underset~i + (6800 cos(pi(1.3t-0.1))-6400)underset ~j`,
for `t in [0, 0.154]`,
where `underset ~i` is a unit vector relative to `text(O)` as shown and `underset ~j` is a unit vector vertically up from point `text(O)`. Time `t` is measured in hours and displacement components are measured in kilometres.
- Find the height, `h` km, of the space station above the surface of Earth when it is at point `text(P)`, directly above point `text(O)`.
- Give your answer correct to the nearest km. (1 mark)
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- Find the acceleration of the space station, and show that its acceleration is perpendicular to its velocity. (3 marks)
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- Find the speed of the space station in km/h.
- Give your answer correct to the nearest integer. (2 marks)
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- Find the equation of the path followed by the space station in cartesian form. (2 marks)
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- Find the times when the space station is at a distance of 1000 km from the radar tracking location `text(O)`.
- Give your answers in hours, correct to two decimal places. (3 marks)
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