Talk:Geosynchronous orbit derivation
Appearance
The error (for those interested) is calculated as cuberoot(1+.5/667 x 1+0.5/598). (There is a lot less error in omega so it is swamped by the previous). Mat-C 20:23, 1 May 2004 (UTC)
The error (for those interested) is calculated as cuberoot(1+.5/667 x 1+0.5/598). (There is a lot less error in omega so it is swamped by the previous). Mat-C 20:23, 1 May 2004 (UTC)[reply]