> Hi,
>
> This may again be a FAQ, but..
>
> I'm getting very strange elevations from stations to inertial objects. I
> follow kind of the examples with:
> (note python-code, so view it as pseudo-code.. :)
>
> ae = 6378137.0 # // equatorial radius in meter (WGS84)
>
> f = 1.0 / 298.257223563 #; // flattening (WGS84)
>
> ITRF2005 = FramesFactory.getITRF2005() #; // terrestrial frame at an
> arbitrary date
>
> earth = OneAxisEllipsoid(ae, f, ITRF2005)
>
> # Station
>
> longitude = radians( 21.063)
>
> latitude = radians(67.878)
>
> altitude = 341.0
>
> station1 = GeodeticPoint(latitude, longitude, altitude)
>
> sta1Frame = TopocentricFrame(earth, station1, "Station")
>
>
> Then I setup the propagation (inertial position verified with STK),
> propagate and:
>
>
> el_tmp =
> sta1Frame.getElevation(pv.getPosition(),inertialFrame, extrapDate)*180.0/pi
>
>
> The result seems to be much too low with no passes above horizon and a
> mean about -42 degrees. Somehow my frames must be mixed up. Any comments
> appriciated.
I don't see any obvious error here. Topocentric frames are really basic