Satellite orbit Perigee Line of apsides Vernal equinox Equator Equator Nodal line Ascending Node Use the figure above to determine the Cartesian coordinates (X, Y, Z) of the satellite f: the distance from the center of the Earth to the satellite is 26560.000 km and the orbit is circular in shape. Determine (X, Y, Z) of the satellite for the following cases: Position 1 Position 2 Position 3 Position 4 Ω Ω i 210.0 90.0 20.0 19.0 142.0 f i Ω f 0.0 14.0 25.0 45.0 6.0 9.0 | 81.0 180.0 | 0.0 | 30.0 61.0 Satellite orbit
Satellite orbit Perigee Line of apsides Vernal equinox Equator Equator Nodal line Ascending Node Use the figure above to determine the Cartesian coordinates (X, Y, Z) of the satellite f: the distance from the center of the Earth to the satellite is 26560.000 km and the orbit is circular in shape. Determine (X, Y, Z) of the satellite for the following cases: Position 1 Position 2 Position 3 Position 4 Ω Ω i 210.0 90.0 20.0 19.0 142.0 f i Ω f 0.0 14.0 25.0 45.0 6.0 9.0 | 81.0 180.0 | 0.0 | 30.0 61.0 Satellite orbit
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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![Satellite
orbit
Perigee
Line of
apsides
Vernal
equinox
Equator
Equator
Nodal line
Ascending
Node
Use the figure above to determine the Cartesian coordinates (X, Y, Z) of the satellite
f: the distance from the center of the Earth to the satellite is 26560.000 km and the orbit is circular in shape.
Determine (X, Y, Z) of the satellite for the following cases:
Position 1
Position 2
Position 3
Position 4
Ω
Ω
i
210.0 90.0 20.0 19.0 142.0
f
i
Ω
f
0.0
14.0
25.0
45.0 6.0 9.0 | 81.0 180.0 | 0.0 | 30.0
61.0
Satellite orbit](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fff2b8187-30bf-40eb-aaad-9c0e4c191499%2Ffce272d4-a61f-4d5b-a01d-78670a29f15c%2Fb75ncjo.png&w=3840&q=75)
Transcribed Image Text:Satellite
orbit
Perigee
Line of
apsides
Vernal
equinox
Equator
Equator
Nodal line
Ascending
Node
Use the figure above to determine the Cartesian coordinates (X, Y, Z) of the satellite
f: the distance from the center of the Earth to the satellite is 26560.000 km and the orbit is circular in shape.
Determine (X, Y, Z) of the satellite for the following cases:
Position 1
Position 2
Position 3
Position 4
Ω
Ω
i
210.0 90.0 20.0 19.0 142.0
f
i
Ω
f
0.0
14.0
25.0
45.0 6.0 9.0 | 81.0 180.0 | 0.0 | 30.0
61.0
Satellite orbit
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