Design, Analysis, Optimization, Manufacturing, and Testing of a 2U Cubesat

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left" colspan="2">ISS orbit</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Semimajor axis (km)</td><td class="align_center">6780</td></tr><tr><td class="align_left">Eccentricity (degrees)</td><td class="align_center">0</td></tr><tr><td class="align_left">Ascending node longitude (degrees)</td><td class="align_center">−94.354</td></tr><tr><td class="align_left">Inclination (degrees)</td><td class="align_center">51.64</td></tr><tr><td class="align_left">Mean anomaly (degrees)</td><td class="align_center">254.215</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

tab4

Table 4

Table 4: Design, Analysis, Optimization, Manufacturing, and Testing of a 2U Cubesat 