Satellite Orbit and Ephemeris Determination using Inter Satellite Links

Satellite Orbit and Ephemeris Determination using Inter Satellite Links Satellite Orbit and Ephemeris Determination using Inter Satellite Links

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Simulations and ResultsInter Satellite Links6.1.1.5 Pure LEO ConstellationThe next constellation is a pure 1250 km LEO constellation, with a total of 81 S/V at 9 orbitplanes with 1 pattern unit phase difference between adjacent planes. All orbit planes have a55° inclination. The following picture shows the ground tracks of the satellites, as well as thelocations of the DORIS network.Figure 6-9 Ground Tracks of LEO ConstellationThe next picture shows the earth coverage of such a constellation. Due to the low orbitaltitude navigation service can be provided only up to ~ 65 ° North / South.Page 100R. Wolf

Inter Satellite LinksSimulations and ResultsFigure 6-10 Visibility of LEO ConstellationIt is clear that building a navigation constellation using satellites at low Earth orbits wouldrequire a large number of space crafts. This constellation here with 81 space vehicles can beregarded as the minimum.6.1.1.6 GEO / LEOTo overcome the bad global coverage of a pure LEO constellation, the next constellationintroduces some high altitude satellites in addition to the LEOs. The LEO part is a 72 / 8 / 2Walker constellation with an orbit altitude of 1250 km and 55° inclination. In addition, thereare 9 GEOs, evenly spaced by 40 °, starting at 10°E. The following picture shows groundtracks and S/V positions, as well as the station locations of the DORIS network.R. Wolf Page 101

<strong>Inter</strong> <strong>Satellite</strong> <strong>Links</strong>Simulations <strong>and</strong> ResultsFigure 6-10 Visibility of LEO ConstellationIt is clear that building a navigation constellation <strong>using</strong> satellites at low Earth orbits wouldrequire a large number of space crafts. This constellation here with 81 space vehicles can beregarded as the minimum.6.1.1.6 GEO / LEOTo overcome the bad global coverage of a pure LEO constellation, the next constellationintroduces some high altitude satellites in addition to the LEOs. The LEO part is a 72 / 8 / 2Walker constellation with an orbit altitude of 1250 km <strong>and</strong> 55° inclination. In addition, thereare 9 GEOs, evenly spaced by 40 °, starting at 10°E. The following picture shows groundtracks <strong>and</strong> S/V positions, as well as the station locations of the DORIS network.R. Wolf Page 101

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