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22671

Perturbation effect on ground tracks of Molniya satellite orbits

Article

Last updated: 03 Jan 2025

Subjects

-

Tags

Astronomy

Abstract

The main concern in the present research work is to define the basic requirements study of many
perturbations forces that affect ground tracks of Molniya satellite orbits.
In this we are going to design a mathematical model to calculate the footprint of any satellite taking
into account the effect of disturbing forces (oblatness and solar radiation pressure) in order to get the
most accurate sub-satellite point, matlab language is used to design program to calculate the
mathematical models of footprint satellites with numerical application of some different Molniya
satellites orbit.

DOI

10.21608/absb.2014.22671

Keywords

Artificial Satellites, Kozai's method, oblateness, solar radiation pressure, ground Track, Longitude, Latitude

Authors

First Name

Awad

Last Name

M.E.

MiddleName

-

Affiliation

Faculty of Science - Cairo University, Egypt

Email

-

City

-

Orcid

-

First Name

Hassan

Last Name

I.A.

MiddleName

-

Affiliation

Faculty of Science - Cairo University, Egypt

Email

-

City

-

Orcid

-

First Name

Dewdar

Last Name

H.R.

MiddleName

-

Affiliation

Faculty of Science - Cairo University, Egypt

Email

-

City

-

Orcid

-

First Name

Tealib

Last Name

S.K.

MiddleName

-

Affiliation

Faculty of Science - Cairo University, Egypt.

Email

-

City

-

Orcid

-

Volume

25

Article Issue

Issue 2-B

Related Issue

4289

Issue Date

2014-12-01

Receive Date

2014-07-23

Publish Date

2014-12-01

Page Start

13

Page End

20

Print ISSN

1110-2535

Online ISSN

2636-3305

Link

https://absb.journals.ekb.eg/article_22671.html

Detail API

https://absb.journals.ekb.eg/service?article_code=22671

Order

5

Type

Original Article

Type Code

520

Publication Type

Journal

Publication Title

Al-Azhar Bulletin of Science

Publication Link

https://absb.journals.ekb.eg/

MainTitle

Perturbation effect on ground tracks of Molniya satellite orbits

Details

Type

Article

Created At

22 Jan 2023