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nimendrum nimendrum
wrote...
Posts: 3
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12 years ago
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?
Source  Sellers, Understanding Space.
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wrote...
12 years ago
Man, I wouldn't have the slightest clue, what should we be looking at here Thinking Face
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