Preliminary Orbit Determination of Artificial Satellites: A Vectorial Sixth-Order Approach

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="960582.fig.002a" src="https://static.hindawi.com/articles/aaa/volume-2013/960582/figures/960582.fig.002a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Newton</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="960582.fig.002b" src="https://static.hindawi.com/articles/aaa/volume-2013/960582/figures/960582.fig.002b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Traub</td></tr></table></td></tr><tr class="fig-image" id="c"><td><img alt="960582.fig.002c" src="https://static.hindawi.com/articles/aaa/volume-2013/960582/figures/960582.fig.002c.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(c) </b>Jarratt</td></tr></table></td></tr></table>

<table>Dynamical planes from classical methods and Reference Orbit I.</table>

Abstract and Applied Analysis

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Figure 2

Figure 2: Preliminary Orbit Determination of Artificial Satellites: A Vectorial Sixth-Order Approach 