Satellite tracking - Dynamics, Angular velocity, Circular motion

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The discussion revolves around solving a problem related to satellite tracking, specifically calculating when a satellite in a circular orbit will pass through the beam of a tracking antenna. The satellite orbits 1600 km above Earth and takes two hours to complete an orbit, while the antenna is aimed 30 degrees above the horizon. Participants emphasize the importance of using trigonometry to find the necessary angles and distances, with suggestions to apply the sine rule for calculations. The complexity arises from understanding the geometry involved, particularly in determining the angles at the center of the Earth and the relationship between the satellite's position and the tracking station. Ultimately, the discussion highlights the collaborative effort to clarify trigonometric concepts and solve the problem effectively.
  • #31
Coto said:
Overkill :). And this only finds a velocity which can be found using the data of the problem in a more direct manner.

What can I say other than I'm a nerd and yes I'm proud of it :)
 

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