4. A tracking station determines the following position and velocity vectors of a spacecraft in the geocentric equatorial coordinate frame: R= 10000 I + 0/+10000 R km V = o1+ 6.5/ +0R km/s %3D %3D Find the satellite's COES and the flight path angle at that location.

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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 I + 0j+ 10000 R km
V = 01+ 6.5/ + OR km/s
%3D
Find the satellite's COES and the flight path angle at that location.
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 I + 0j+ 10000 R km V = 01+ 6.5/ + OR km/s %3D Find the satellite's COES and the flight path angle at that location.
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