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Title: A spacecraft has these orbital elements: Post by: nimendrum on Mar 21, 2012 A spacecraft has these orbital elements:
Semimajor axis = 5740 km Eccentricity = 0.1 Inclination = 53° Right ascension of the ascending node = 345° Argument of perigee = 270° True anomaly = 183° What is peculiar about this orbit? Title: Re: A spacecraft has these orbital elements: Post by: chemb on Mar 22, 2012 Man, I wouldn't have the slightest clue, what should we be looking at here :thi:
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