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numbers, the other with the equations. Put a box around the answer to each part. 1. An objects circular orbital velocity vc around the earth can be calculated using the equation , where ve is the circular orbital velocity, μ-3.98601 E5 km3/s, is the earths gravitational parameter, and r is the distance of the object from the earths center. Some commercial satellites, like DirecTV, are in an orbit where they take one sidereal day (23h 56m 4.09s) to orbit the earth. This makes it so that the satellite appears to be stationary to an observer on the earths surface, which also takes one sidereal day to rotate about its axis That is a good situation because each receiving antenna only needs to be aimed once, which is a lot easier than tracking a satellite. This type of orbit is called geosynchronous (since it is synchronized with geo-earth) and is abbreviated GEO, for Geosynchronous Earth Orbit. (a) Using ONLY the circular orbital velocity equation given above AND knowledge about the circumference of a circle, calculate the required GEO orbital radius rceo, in km.(b) For this to work, what angle must the orbit have with respect to the equator? (c) Calculate the GEO satellites circular orbital velocity y^-ceo around the earth, in km/s (d) Explain why a sidereal day is not exactly 24h 0m 0s

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