Abstract

According to altitude, the orbits of satellites constellations can be divided into geostationary Earth orbit (GEO), medium Earth orbit (MEO), and low Earth orbit (LEO) constellations. We propose to use a Walker star constellation with polar orbits, at any altitude, to emulate the geostationary orbit with zenith paths at any latitude. Any transmitter/receiver will be linked to a satellite as if the site were at the equator and the satellite at the local zenith. This constellation design can have most of the advantages of the current GEO, MEO, and LEO constellations, without having most of their drawbacks. Doppler phenomena are largely minimized because the connected satellite is always seen almost at the local zenith. The extra free-space loss, due to the fixed pointing of all antennas, is at most 6 dBs when the satellite enters or leaves the service area. The connections among satellites are easy because the positions in the orbital plane and in adjacent planes are constant, although with variable distances. No steering antennas are required. The tropospheric propagation fading and scintillations are minimized. Our aim is to put forth the theoretical ideas about this design, to which we refer to as the geostationary surface (GeoSurf) constellation.

Highlights

  • According to altitude, the orbits of satellites constellations can be divided into geostationary Earth orbit (GEO), medium Earth orbit (MEO), and low Earth orbit (LEO) constellations

  • We propose to use a Walker star constellation with polar orbits, at any altitude, to emulate the geostationary orbit with zenith paths at any latitude

  • Our aim is to put forth the theoretical ideas about this design, to which we refer to as the geostationary surface (GeoSurf) constellation

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Summary

Satellite Constellations

According to the altitude above the Earth surface, satellite orbits can be divided into geostationary Earth orbits (GEO), medium Earth orbits (MEO), and low Earth orbits (LEO) [1,2,3,4]. Because of the advantages of the fixed position, i.e., does not require steering antennas or steering arrays, wide coverage, and constant propagation delay (constant latency), GEO satellites are mostly used to implement communication and broadcasting systems. It is necessary to study a system architecture that must integrate with terrestrial networks to offer continuous coverage worldwide For this purpose satellite constellation design and coverage schemes are fundamental. The design of a satellite constellation is one of the critical factors that determine the performance of MEO and, especially, LEO satellite communication systems.

Geocentric Spherical Surfaces Emulating the Geostationary Orbit
Discussion and Conclusions
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