395 future LOS -pointing satellite developments, as well as how they translate to other spacecraft units with a  potent ially deleterious IV signature,  e.g., rotating or dithering components, etc. From a global viewpoint, it  can seem difficult to see how a few -ounce miniscule part’s ( i.e., RWA bearing raceway/retainer) barely  measurable imperfections can amplify into a formidable challenge for a ~12- ton spacecraft’s primary LOS  jitter allocations under unfavorable conditions. Although not common for most satellites to engage all of  these approach details, attainment and prudent management of lower -level IV data is essential for finepointing space platform’s success. This paper’s predominant value is in exposing both applicability guidance plus revealin g insights/means to pursue in- depth key details to attain fine- pointing requirements.  

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