Hi,
YAOGAN 8 traveling faster could be due to possible initial orbit corrections and maneuvering that includes minor correction of injection velocity (delta V). The drag do influence even at geo-transfer and geo-synchronous orbits.
73 de Mani, VU2WMY Secretary & Station-In-Charge Upagrah Amateur Radio Club VU2URC ISRO Satellite Centre Airport Road, Bangalore-560 017. Phone:(O)91-80-2508 2054/2192/2537 Mobile: 91-80-98803 41456 E-mail ID: wmy@isac.gov.in vu2wmy_mani@yahoo.com isrohams@yahoo.com
Quoting Alexandru Csete alexc@phys.au.dk:
The influence of the drag force also depends on the mass since F=m*a, so the same drag force will cause less deceleration on a heavier satellite. You have to put this together with F=pressure*surface_area to take both the size and the mass of the satellite into account.
By the way, is there any significant atmospheric drag at 1200 km altitude?
73 Alex OZ9AEC
On Wed, 16 Dec 2009 18:56:20 +0000 Nigel Gunn G8IFF/W8IFF nigel@ngunn.net wrote:
OK, I'll revise my earlier question and suggest a reply.
The physically larger satellite will have more atmospheric drag which will spiral it into a lower orbit. The lower orbit, the higher the velocity and thereforeit crosses your horizon earlier.
Nigel Gunn G8IFF/W8IFF wrote:
Is this correct that the higher mass satellite travels faster than the lower mass of XW?
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