A spacecraft is currently orbiting around the Earth with the following characteristics (in Earth-Centered Mean J2000 Equatorial frame): a = 3R N = 45° e = 0.40 i = 28.5° 0 = 235° W = 90° a) Determine ř and ū in both ê-ôp-ħ and î-Ô-h frame. Also determine r, v, y, 0*, M, E, t – tp.
A spacecraft is currently orbiting around the Earth with the following characteristics (in Earth-Centered Mean J2000 Equatorial frame): a = 3R N = 45° e = 0.40 i = 28.5° 0 = 235° W = 90° a) Determine ř and ū in both ê-ôp-ħ and î-Ô-h frame. Also determine r, v, y, 0*, M, E, t – tp.
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Transcribed Image Text:A spacecraft is currently orbiting around the Earth with the following characteristics (in
Earth-Centered Mean J2000 Equatorial frame):
= 3R
N = 45°
e = 0.40
i = 28.5°
0 = 235°
w = 90°
a) Determine and ī in both ê-p-ħ and î-Ô-ĥħ frame. Also determine r, v, y, 0*, M, E,
ー tp.
t -
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