It is not quite that simple - (most) satellites do not follow a great circle. Extreme cases are near-geosynchronous, or highly elliptic orbits. My program takes at least three predictions points, and does a least-squares fit to the points - in alt/az mode, then converts the pole location back to H.A/dec, or R.A/dec a given time before the pass. A typical LEO track has a "declination" of about -5, ie pole is 95 degrees "above" culmination. > The mathematics for equatorial mount pointing are this simple that not even > a piece of paper is needed: To provide a minimal rotation about the ----------------------------------------------------------------- Unsubscribe from SeeSat-L by sending a message with 'unsubscribe' in the SUBJECT to SeeSat-L-request@lists.satellite.eu.org http://www2.satellite.eu.org/seesat/seesatindex.html
This archive was generated by hypermail 2b29 : Tue Apr 03 2001 - 13:54:30 PDT