Below are a couple of online sites. The first one purports to do the conversion in either direction, from state vector to TLE or vice versa. "The applet below allows conversions between orbit elements and state vectors.": http://alpha.fesg.tu-muenchen.de/dieter/java/TLOrbit.html "Transform from orbital elements to state vector" http://www.geocities.com/SiliconValley/2902/ele2vec.htm The above is one of several orbital calculators on the following site: http://www.geocities.com/SiliconValley/2902/orbit.htm Ed Cannon - ecannon@mail.utexas.edu - Austin, Texas, USA ----------------------------------------------------------------- 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 May 09 2000 - 23:26:26 PDT