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M: +2.00/-0.66

A satellite is orbiting in the equatorial plane with a period from perigee to perigee of 12h. If the eccentricity = 0.002, i = 0o, K1 = 66063.17 km2, μ = 3.99 × 1014 m3/s2 and the earth’s equatorial radius = 6378.14 km, the semi-major axis will be

[ESE 2019 Paper 2 (Technical) ECE]
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