The path of a satellite orbiting the earth causes the satell
Solution
Let the position nof the satellite be denoted by S and let the perpendicular from S to the ground meet the line BA at P. Also, let the satellite be h miles above the ground ans let PA = x miles.
Then in the right angled SPA, we have tan 870 = h/x so that h = x tan 870 = 19.0811x…(1). Similarly, considering the right angled SPB, we have tan 84.20 = h/(x+65) so that h = (x+65) tan 84.20= (x+65)*9.8448 or, h = 9.8448x+ 639.9120...(2). Now, on subtracting the 2nd equation from the 1st equation, we get 19.0811x -9.8448x -639.9120 = 0 or, 9.2363x = 639.9120 so that x = 639.9120/9.2363 =69.2823. Then, from the 1st equation, we get h =19.0811*69.2823 = 1321.9823.Further, in the right angled SPA, we have sin 870 = h/SA so that SA = h sin 870 = 1321.9823*0.9986 = 1320.1706.
Thus, the satellite is 1320.17 miles from station A.
Also, the satellite is 1321.98 miles above the ground.
