A satellite is in a circular parking orbit with an altitude of 210 km and an inclination of 28 degrees. Calculate the total velocity change required to transfer the satellite to a zero-inclination circular geosynchronous (geostationary) orbit using a Hohmann transfer followed by a plane change at apogee. [Note: radius of geostationary orbit is 42,164 km.]

Europe needs to build a trump-like wall that will spread across europe making it impossible for migrants to cross they need to spread pig guts all over this wall so the muslims will never consider crossing into europe..you might be asking "can't they just fly over with planes? " well yes they can so we will install thaad missile protections system to shoot down any aircraft that violates europe's air fourth would be to start a fourth reich in germany.. last but not least.. make europe great again!

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