Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1780602 | NRIAG Journal of Astronomy and Geophysics | 2015 | 6 Pages |
Abstract
In this work, the circumstances of eclipse for a circular satellites’ orbit are studied. The time of passage of the ingress and egress points is calculated. Finally, the eclipse intervals of satellites’ orbit are calculated. An application was done taken into account the effects of solar radiation pressure and Earth’s oblateness on the orbital elements of circular orbit satellite.
Keywords
Related Topics
Physical Sciences and Engineering
Physics and Astronomy
Astronomy and Astrophysics
Authors
M.N. Ismail, A. Bakry, H.H. Selim, M.H. Shehata,