Consider the TBP governing equation of motion in 3D. As mentioned, this equation governs the behavior of satellites or space vehicles in the Earth Centered Inertial Frame (ECI). TBP Governing Equation of Motion Si MEarh =398,600 km /s r(0) = 16001+ 5310J + 3800K (km) F(0) =-7.3501+ 0.4600J + 2.470K (km/s) Perform the following tasks: i. Use the initial condition of and arbitrary satellite given below to propagate its orbit for at least

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Consider the TBP governing equation of motion in 3D. As mentioned, this equation governs the
behavior of satellites or space vehicles in the Earth Centered Inertial Frame (ECI).
TBP Governing Equation of Motion
i HEarth =398,600 km³ /s?
r(0) = 16001+ 5310J+ 3800K (km)
ř(0)=-7.3501 + 0.4600J + 2.470K (km/s)
Perform the following tasks:
i. Use the initial condition of and arbitrary satellite given below to propagate its orbit for at least
one complete period (the orbit is closed). You can tabulate the position and velocity components
and magnitude with time for At = 100 Sec.
ii. Show (plot) the resulting satellite 3D trajectory for one complete period.
iii. Show the satellite ground track or its geographical position on the Earth surface. This can be
simply shown as a graph of the satellite latitude versus its longitude for one period. See the
sample given below.
Ground Tracker
60N
60N
40N
40N
20N
20N
20s
205
40s
60'S
100W
120°E
180E
M.ort
Transcribed Image Text:Consider the TBP governing equation of motion in 3D. As mentioned, this equation governs the behavior of satellites or space vehicles in the Earth Centered Inertial Frame (ECI). TBP Governing Equation of Motion i HEarth =398,600 km³ /s? r(0) = 16001+ 5310J+ 3800K (km) ř(0)=-7.3501 + 0.4600J + 2.470K (km/s) Perform the following tasks: i. Use the initial condition of and arbitrary satellite given below to propagate its orbit for at least one complete period (the orbit is closed). You can tabulate the position and velocity components and magnitude with time for At = 100 Sec. ii. Show (plot) the resulting satellite 3D trajectory for one complete period. iii. Show the satellite ground track or its geographical position on the Earth surface. This can be simply shown as a graph of the satellite latitude versus its longitude for one period. See the sample given below. Ground Tracker 60N 60N 40N 40N 20N 20N 20s 205 40s 60'S 100W 120°E 180E M.ort
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