The next generation of airborne GNSS equipment will process dual-frequency L1/L5 signals broadcast by up to four core constellations (GPS, Galileo, GLONASS and BeiDou), with integrity provided by Aircraft, Satellite or Ground Based Augmentation Systems. The current GPS/SBAS standard RTCA/DO-229E [1] requires that airborne receivers implement a minimum of 6 channels for GPS tracking and 2 channels for SBAS tracking. For future standards addressing dual-Frequency L1/L5 multi-constellation equipment, there is a will to improve the availability figures of SBAS enabled CAT I approach, and target new operations enabled by narrower integrity bounds, by increasing the minimum number of tracking channels and possibly defining performance of the satellite selection algorithm. On the other hand, airborne receivers have finite resources, and the "all-in-view" expectation for two or more constellations reaching 30 to 32 satellites (SV) each may not be realistic. It is therefore necessary to define the minimum requirements for satellite selection in future Dual-Frequency Multi-Constellation (DFMC) standards, including the minimum number of channels to implement, or alternatively the minimal performance of the SV selection strategy. Previous studies have already assessed a promising solution to optimize the satellite selection process under SBAS coverage: the "Downdate" method [2] [3]. The objective of this paper is to assess the performance of different selection algorithms under DFMC SBAS augmentation by taking into account not only the number of tracking channels, but also the dynamic of the reallocation process. We also consider the impact of the prediction mechanism recommended in the current GPS/SBAS standard for LPV approach.