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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
/
2012
/
Article
/
Fig 3
/
Research Article
Semianalytic Integration of High-Altitude Orbits under Lunisolar Effects
Figure 3
The same as Figure
2
but now
𝑁
=
1
8
0
instead of
𝑁
=
0
deg.
(a)
(b)