Eclipses intervals for satellites in elliptical orbit under effects of solar radiation pressure and earth’s oblatness

M. N., Ismail and A., Bakry and H. H., Se lim and M. H., Shehata (2015) Eclipses intervals for satellites in elliptical orbit under effects of solar radiation pressure and earth’s oblatness. Al-Azhar Bulletin of Science, 26 (1). pp. 17-22. ISSN 1110-2535

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Abstract

The eclipse of a satellite in elliptical orbit is studied. The geocentric angle in the orbital plane between the perigee and conjunction point is determined. Eclipse times and duration of eclipse for elliptical orbits are obtained. The effects of the direct solar radiation pressure on the orbital elements are calculated taken into account the eclipses intervals. An application on the MOLNIYA 1-87 artificial satellite is done.

Item Type: Article
Subjects: Digital Open Archives > Medical Science
Depositing User: Unnamed user with email support@digiopenarchives.com
Date Deposited: 26 Jun 2024 09:52
Last Modified: 26 Jun 2024 09:52
URI: http://geographical.openuniversityarchive.com/id/eprint/1720

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