The position of an earth satellite is first determined to be Fi = 60001 + 10000.J + 2100km After two hours, ie, tz - 1 = 2h, the position vector is F, = -146001 - 25000 + 7000km Determine the orbital elements of the satellite. (Using the priteration method for solving Lambert's problem).
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The position of an earth satellite is first determined to be Fi = 60001 + 10000.J + 2100km After two hours, ie, tz - 1 = 2h, the position vector is F, = -146001 - 25000 + 7000km Determine the orbital elements of the satellite. (Using the priteration method for solving Lambert's problem).
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