A
aphh
Guest
<p>I'm trying to figure out what is needed to get some orbital parameters of a satellite by observing the satellite in the sky.<br /><br /> Here is the basic schematic for a best case scenario, where the observer has unobstructed both horizons, sun is perpendicular to the satellite's orbit and the satellite passes directly overhead:<br /><br /><br /> <img src="http://sitelife.space.com/ver1.0/Content/images/store/13/8/8dae2b3a-c1a6-4319-a892-c412b6359552.Medium.jpg" alt="" /><br /><br />The blue area is the visible portion of the satellite's orbit in the best case scenario. Knowing the altitude makes it possible to calculate the time it takes for the satellite to complete the visible arc.</p><p>Let's say the satellite is the ISS, and you are in a position to get a direct overhead pass. The visible arc would then be 2 * ((6375km / (6375km + 330km) * cos^-1)) = 36 degrees.</p><p>If one orbit takes 5441 seconds to complete, then the visible pass would take 544 seconds in optimal conditions.</p><p>How far the satellite is when the visible pass begins in this scenario is (xkm)^2 + (6375km)^2 = (6705km)^2. Solving the x gives 2076 kilometers distance to the satellite when the visible pass begins or ends.</p><p>The length of the visible arc in this case is 2pi * 6705km / 10 = 4212km (because the visible arc is one tenth of the full circle in this scenario). </p><p>This is for a satellite, who's orbital parameters are known. The next step would be to determine the orbital parameters by observing how long it takes for the satellite to complete the visible pass.</p><p>For this we need reference points in the sky, stars. By observing how long it takes for the satellite to go between two fixed reference points in the sky should allow us to determine the time it takes for the satellite to complete one complete orbit and thus the mean altitude. </p>