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4. A tracking station determines the following position and velocity vectors of a spacecraft in
the geocentric equatorial coordinate frame:
R = 10000 Î + 0j+ 10000 R km
V = 0f+ 6.5/ + 0R km/s
%3D
Find the satellite's COES and the flight path angle at that location.
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Transcribed Image Text:4. A tracking station determines the following position and velocity vectors of a spacecraft in the geocentric equatorial coordinate frame: R = 10000 Î + 0j+ 10000 R km V = 0f+ 6.5/ + 0R km/s %3D Find the satellite's COES and the flight path angle at that location.
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