Eclipse intervals for satellites in circular orbit under the effects of Earth’s oblateness and solar radiation pressure
Ismail, M., Bakry, A., Selim, H., Shehata, M. (2015). Eclipse intervals for satellites in circular orbit under the effects of Earth’s oblateness and solar radiation pressure. EKB Journal Management System, 4(1), 117-122. doi: 10.1016/j.nrjag.2015.06.001
M.N. Ismail; A. Bakry; H.H. Selim; M.H. Shehata. "Eclipse intervals for satellites in circular orbit under the effects of Earth’s oblateness and solar radiation pressure". EKB Journal Management System, 4, 1, 2015, 117-122. doi: 10.1016/j.nrjag.2015.06.001
Ismail, M., Bakry, A., Selim, H., Shehata, M. (2015). 'Eclipse intervals for satellites in circular orbit under the effects of Earth’s oblateness and solar radiation pressure', EKB Journal Management System, 4(1), pp. 117-122. doi: 10.1016/j.nrjag.2015.06.001
Ismail, M., Bakry, A., Selim, H., Shehata, M. Eclipse intervals for satellites in circular orbit under the effects of Earth’s oblateness and solar radiation pressure. EKB Journal Management System, 2015; 4(1): 117-122. doi: 10.1016/j.nrjag.2015.06.001

Eclipse intervals for satellites in circular orbit under the effects of Earth’s oblateness and solar radiation pressure

NRIAG Journal of Astronomy and Geophysics
Volume 4, Issue 1, June 2015, Pages 117-122    PDF (1.16 M)
DOI: 10.1016/j.nrjag.2015.06.001
Authors
M.N. Ismail; A. Bakry; H.H. Selim; M.H. Shehata
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
Perturbation theory; Circular orbital motion; Earth’s gravity; Radiation pressure effects
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