Achievable orbit from launch location

jeudi 31 octobre 2013

Hi Astro gurus,



Is there any limitation on the inclination of the achievable orbit because of the latitude of the launch location? For example, latitude of Baikonur is roughly 46° E. Does that limit somehow the inclinations of the orbits that can be achieved from Baikonur?



I think there should be no limitation as it should be possible to achieve any velocity vector at some position, & hence any possible set of orbital elements should be possible. More so, if a ballistic missile can hit target in any direction, it means different sets of orbital elements are possible.






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