- #1
Ed
- 12
- 0
Hi folks,
If I have the elements of a spacecraft 's (eliptical) orbit (a,e,i,etc) and the lat/long of a ground station, how can I calculate the times at which the spacecraft will be visibile from the groundstation (preferably in terms of time since perifocal passage)? I've been googling for hours on this one with no luck so far...
If I have the elements of a spacecraft 's (eliptical) orbit (a,e,i,etc) and the lat/long of a ground station, how can I calculate the times at which the spacecraft will be visibile from the groundstation (preferably in terms of time since perifocal passage)? I've been googling for hours on this one with no luck so far...