Solar Synchronous Orbits. Predicting the Mean Local Time of the Ascending Node

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Andrey Nazarenko
Andrey Nazarenko

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Solar Synchronous Orbits. Predicting the Mean Local Time of the Ascending Node

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Abstract

Based on the orbital data of the Meteor M1 spacecraft, the possible causes of the deviations of the mean local time of the ascending node (MLTAN) from the initial value are considered. It has been established that the main cause of deviations is the change in inclination. This occurs as a result of solar gravitational disturbances and leads to a change in the MLTAN under the law, which at intervals of up to 7 years is close to parabola. In general, these variations are long-period with the period of 28 years. The simplified system of differential equations describing the evolution of inclination and MLTAN has been proposed. The results of the integration of this system of equations are well consistent with the real data on the evolution of the parameters of the orbit of the Meteor M1 spacecraft.

References

8 Cites in Article
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Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

Data Availability

Not applicable for this article.

How to Cite This Article

Andrey Nazarenko. 2020. \u201cSolar Synchronous Orbits. Predicting the Mean Local Time of the Ascending Node\u201d. Global Journal of Research in Engineering - I: Numerical Methods GJRE-I Volume 20 (GJRE Volume 20 Issue I1): .

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Journal Specifications

Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

Keywords
Classification
GJRE-I Classification: FOR Code: 230116
Version of record

v1.2

Issue date

July 3, 2020

Language
ru
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Based on the orbital data of the Meteor M1 spacecraft, the possible causes of the deviations of the mean local time of the ascending node (MLTAN) from the initial value are considered. It has been established that the main cause of deviations is the change in inclination. This occurs as a result of solar gravitational disturbances and leads to a change in the MLTAN under the law, which at intervals of up to 7 years is close to parabola. In general, these variations are long-period with the period of 28 years. The simplified system of differential equations describing the evolution of inclination and MLTAN has been proposed. The results of the integration of this system of equations are well consistent with the real data on the evolution of the parameters of the orbit of the Meteor M1 spacecraft.

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Solar Synchronous Orbits. Predicting the Mean Local Time of the Ascending Node

Andrey Nazarenko
Andrey Nazarenko

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