Research Article

Minimizing satellite residence time in the GEO region through elevated eccentricity method

Volume: 8 Number: 3 July 28, 2024
EN

Minimizing satellite residence time in the GEO region through elevated eccentricity method

Abstract

This research focuses on a critical aspect of the space environment, addressing the escalating issue of space debris and congestion in the geostationary orbit. The geostationary orbit is facing many satellites, leading to hazardous congestion levels and jeopardizing the limited resources available. Although organizations have established regulations for retiring satellites to graveyard orbits, a complete removal is not always achievable for numerous reasons. In response to this challenge, our study proposes a practical and cost-effective solution to mitigate debris accumulation in the region. In addition to the above, our research focuses on protecting the geostationary space environment, especially in unforeseen events involving inclined-operated satellites. We explore the implementation of an elevated eccentricity method, increasing the eccentricity of aging satellites and assessing its impact on their time in the geostationary and geostationary-protected regions. Our analysis encompasses short-term, medium-term, and long-term periods, enabling us to evaluate the effectiveness of this approach over different time frames. The study reveals a significant reduction in the time satellites spend in these regions as their eccentricity increases. Moderate eccentricity levels can reduce satellite residence time in these regions from 100.00% to 3.81%. This compelling evidence demonstrates the feasibility and effectiveness of adopting elevated eccentricity as a viable strategy to mitigate space debris in the regions. This proposed approach offers satellite operators a reliable and cost-effective solution, ensuring safe operations and protecting critical regions for aging GEO satellites. Accordingly, we contribute to space environment protection, securing the sustainability of the geostationary orbit.

Keywords

References

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Details

Primary Language

English

Subjects

Environmental Engineering (Other)

Journal Section

Research Article

Early Pub Date

July 5, 2024

Publication Date

July 28, 2024

Submission Date

November 23, 2023

Acceptance Date

March 1, 2024

Published in Issue

Year 2024 Volume: 8 Number: 3

APA
Öz, İ. (2024). Minimizing satellite residence time in the GEO region through elevated eccentricity method. Turkish Journal of Engineering, 8(3), 416-426. https://doi.org/10.31127/tuje.1395250
AMA
1.Öz İ. Minimizing satellite residence time in the GEO region through elevated eccentricity method. TUJE. 2024;8(3):416-426. doi:10.31127/tuje.1395250
Chicago
Öz, İbrahim. 2024. “Minimizing Satellite Residence Time in the GEO Region through Elevated Eccentricity Method”. Turkish Journal of Engineering 8 (3): 416-26. https://doi.org/10.31127/tuje.1395250.
EndNote
Öz İ (July 1, 2024) Minimizing satellite residence time in the GEO region through elevated eccentricity method. Turkish Journal of Engineering 8 3 416–426.
IEEE
[1]İ. Öz, “Minimizing satellite residence time in the GEO region through elevated eccentricity method”, TUJE, vol. 8, no. 3, pp. 416–426, July 2024, doi: 10.31127/tuje.1395250.
ISNAD
Öz, İbrahim. “Minimizing Satellite Residence Time in the GEO Region through Elevated Eccentricity Method”. Turkish Journal of Engineering 8/3 (July 1, 2024): 416-426. https://doi.org/10.31127/tuje.1395250.
JAMA
1.Öz İ. Minimizing satellite residence time in the GEO region through elevated eccentricity method. TUJE. 2024;8:416–426.
MLA
Öz, İbrahim. “Minimizing Satellite Residence Time in the GEO Region through Elevated Eccentricity Method”. Turkish Journal of Engineering, vol. 8, no. 3, July 2024, pp. 416-2, doi:10.31127/tuje.1395250.
Vancouver
1.İbrahim Öz. Minimizing satellite residence time in the GEO region through elevated eccentricity method. TUJE. 2024 Jul. 1;8(3):416-2. doi:10.31127/tuje.1395250

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