OE2PV | ||
| 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. | |
| Filename: | oe2pv.zip | |
| ID: | 9172 | |
| Current version: | 1.0 | |
| Author: | David Sims: https://jenab6.livejournal.com | |
| Downloaded file size: | 3,611 bytes | |
| Size on calculator: | 16 KB | |
| Platforms: | Prime | |
| User rating: | Not yet rated (you must be logged in to vote) | |
| Primary category: | Science | |
| Languages: | ENG | |
| File date: | 2020-05-14 11:52:54 | |
| Creation date: | 2020-05-14 | |
| Source code: | Not included | |
| Download count: | 317 | |
| Version history: | 2020-06-06: Added to site | |
| Archive contents: |
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| Screenshot: |  | |
| User comments: | No comments at this time. | |
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