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Title: Design of Mega LEO Constellations for Continuous Coverage over Pakistan: Satellite Communication
Authors: Jahanzeb Qureshi, Hamna Butt, Tayyaba Fayyaz, Nadeem Faisal
Journal: International Journal of Innovations in Science & Technology
Publisher: 50SEA JOURNALS (SMC-PRIVATE) LIMITED
Country: Pakistan
Year: 2023
Volume: 5
Issue: 1
Language: English
Keywords: SatelliteLatency RateConstellationCoverageInclinationAntenna
Satellite communication was effectively done in Geostationary Earth Orbit (GEO) in the past years. Recently the trend has shifted from GEO to Low Earth Orbit (LEO). The objective of our study is to propose a satellite constellation for Pakistan in LEO that will provide continuous coverage over Pakistan. As LEO is much closer to the earth as compared to other orbits such as GEO and High Earth Orbit (HEO) etc. one can achieve benefits like low latency rate, less fuel consumption, and signal transmission loss. In ongoing research, an attempt has been made to design the satellite constellation in LEO using the software, System Tool Kit (STK) which has 2D and 3D environment modeling. In the designed constellation, the satellites pass over Pakistan and access the target area. To get uninterrupted continuous coverage, the number of satellites per plane and the number of orbits is increased. The orbital inclinations were also adjusted to achieve the objective. One of the important tasks for continuous coverage is the concept of satellite handshaking which means that soon a satellite gets away from the line of sight of the ground station antenna; another satellite comes within the line of sight of that antenna. LEO satellites are more favorable for communication purposes as they provide reliable communication as well as higher bandwidth.
To propose a satellite constellation in Low Earth Orbit (LEO) for Pakistan that provides continuous coverage, aiming for low latency, reduced fuel consumption, and minimal signal transmission loss.
The study utilized System Tool Kit (STK) software for designing and visualizing a satellite constellation. Pakistan was selected as the target region. The methodology involved defining orbital parameters (inclination and altitude), creating a constellation of satellites (initially 20, then 6 for demonstration), and analyzing satellite access and coverage using STK's tools like figure of merit and grid inspector. The concept of "satellite handshaking" was central to achieving continuous coverage.
graph TD;
A[Define Target Area: Pakistan] --> B[Select Orbital Parameters: Inclination, Altitude];
B --> C[Design Satellite Constellation using STK];
C --> D[Simulate Satellite Access and Coverage];
D --> E[Implement Satellite Handshaking];
E --> F[Analyze Results: Coverage Percentage];
F --> G[Propose Constellation Specifications];
LEO constellations offer cost-effectiveness and improved performance compared to GEO, making them suitable for developing countries. The lifetime of LEO satellites (5-8 years) necessitates replacement strategies. The study highlights that LEO constellations can support 5G and beyond, providing services like voice, SMS, and broadband with low latency. Regulatory compliance with the ITU's tiered management approach is important for deploying such constellations.
A proposed LEO constellation design for Pakistan can achieve 100% coverage per day. The study demonstrated that by adjusting orbital inclination and altitude, and implementing satellite handshaking, continuous communication can be maintained. The proposed constellation specifications include circular orbits at altitudes of 1000 km and 1800 km with inclinations of 40° and 37° respectively for 24-hour coverage.
LEO constellations of small satellites are a growing trend for global coverage, especially in areas lacking terrestrial infrastructure. The designed constellation for Pakistan aims to provide continuous, timely, and instant information with low communication latency, cost-effectiveness, and reduced fuel consumption, supporting services like voice, SMS, and broadband.
* LEO Satellite Lifetime: The text states LEO satellites have a lifetime of around 5-8 years. This is generally consistent with industry estimates, though it can vary based on satellite design and mission.
* Constellation Size: The text mentions SpaceX's Starlink constellation is proposed to hold 4,425 satellites. While the initial proposal was for this number, Starlink's plans have evolved and are much larger.
* Coverage Achievement: The study claims 100% coverage is achieved per day for the targeted area (Pakistan) with the proposed constellation. This is a simulation outcome based on the STK software.
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