Description:Accepts as input the elements for a heliocentric elliptical or hyperbolic orbit, and a time of interest. The user inputs data by adjusting the values within the code. OE2PV outputs heliocentric state vectors for the object and for Earth, and it further outputs the geocentric distance, right ascension, and declination for the object.
Current version:1.0
Author:David Sims: https://jenab6.livejournal.com
Downloaded file size:3,611 bytes
Size on calculator:16 KB
User rating:Not yet rated (you must be logged in to vote)
Primary category:Science
File date:2020/05/14 11:52:54
Creation date:2020/05/14
Source code:Not included
Download count:253
Version history:2020/06/06: Added to site
Archive contents:
  Length      Date    Time    Name
---------  ---------- -----   ----
    15878  2020-05-14 11:48   OE2PV.hpprgm
     1845  2020-05-14 12:03   Readme for OE2PV.txt
---------                     -------
    17723                     2 files
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Copyright 1997-2023 Eric Rechlin.