<page_title> Chandrayaan-1 </page_title> <section_title> Lunar orbit insertion </section_title> <table> <cell> 504 km <col_header> Resulting periselene </col_header> <row_header> 8 November </row_header> </cell> <cell> 7,502 km <col_header> Resulting aposelene </col_header> <row_header> 8 November </row_header> </cell> <cell> 200 km <col_header> Resulting periselene </col_header> <row_header> 9 November </row_header> </cell> <cell> 7,502 km <col_header> Resulting aposelene </col_header> <row_header> 9 November </row_header> </cell> </table>
Lunar orbit insertion reduced the periselene to 200 km while aposelene remained unchanged at 7,502 km.