!,@, (i) r₁ = (8800.00 ƒ) km and v = (0.943736 -6.31469 k) km/s and i (ii). r₁ = (3818.14 i +8148.07 +504.90k)km, r₂ = (3533.28 +8280.22 +525.91 k) km r₁=(-3969.52 i +8512.67 +821.75 k) km.

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Determine the classical orbital elements (a, e, i, 2, w, f,) for
(1) L, = (8800.00 ) km and v, = (0.943736 i-6.31469 k) km/s and
%3D
%3D
(ii). r, = (3818.14 i+8148.07 j+504.90 k) km, r, = (3533.28 i +8280.22 j +525.91k) km
r =(-3969.52 î + 8512.67 j + 821.75 k) km.
Assume u= 3.986 x 10° km /s? (i.e., geocentric orbits)
Transcribed Image Text:Determine the classical orbital elements (a, e, i, 2, w, f,) for (1) L, = (8800.00 ) km and v, = (0.943736 i-6.31469 k) km/s and %3D %3D (ii). r, = (3818.14 i+8148.07 j+504.90 k) km, r, = (3533.28 i +8280.22 j +525.91k) km r =(-3969.52 î + 8512.67 j + 821.75 k) km. Assume u= 3.986 x 10° km /s? (i.e., geocentric orbits)
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