In orbdir.ks the function expects no parameters. However in etaAN and etaDN, the function is called with refNorm. How do you use those functions for time to AN/DN for equatorial orbit or any other orbit (like that of a target orbitable)?
In orbdir.ks the function expects no parameters.
However in etaAN and etaDN, the function is called with refNorm.
How do you use those functions for time to AN/DN for equatorial orbit or any other orbit (like that of a target orbitable)?