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Re: PCsat Keplerian Elements
- Subject: [amsat-bb] Re: PCsat Keplerian Elements
- From: Bob Bruninga <bruninga@xxxxxxxx>
- Date: Wed, 1 May 2002 23:27:18 -0400 (EDT)
- In-Reply-To: <LYR27951-77413-2002.05.01-20.53.42--bruninga#usna.edu@lists.tapr.org>
On Wed, 1 May 2002, Donald B. McGehee wrote:
> How often should Kep elements be updated for PCsat?
PCsat is in a very stable 800km orbit which should last over 100 years.
So the drag is very small. I'd think elements should last a few months at
a time because PCsat requires no antenna pointing and so a few degrees
error in angles wont make any difference to someone listening on an OMNI.
The higher altitude means that PCsat has a lot bigger coverage area than
ISS. Compare the footprints of ISS and PCsat and you will see a
difference. But although ISS and PCsat have identical transponders, and
ISS sees a smaller area, it seems taht the activity on ISS is at least 3
times that on PCsat... I donno why...
bob
PCsat WEB page http://www.ew.usna.edu/~bruninga/pcsat.html
ISS-APRS FAQ: http://www.ew.usna.edu/~bruninga/iss-faq.html
CUBESAT Designs http://www.ew.usna.edu/~bruninga/cubesat.html
APRS LIVE pages http://www.ew.usna.edu/~bruninga/aprs.html
APRS SATELLITES http://www.ew.usna.edu/~bruninga/astars.html
MIM/Mic-E/Mic-Lite http://www.toad.net/~wclement/bruninga/mic-lite.html
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