Multi-Layer Remote Sensing Telemetry and Spatial Field Trajectories Across Concentric Cislunar Interfaces

This paper presents a multi-layer remote sensing telemetry and spatial field trajectory architecture designed for operations across concentric cislunar interfaces, including Distant Retrograde Orbits (DRO), Near-Rectilinear Halo Orbits (NRHO), and Earth-Moon Lagrange point regimes. The framework integrates high-rate mechanical Reflector Links with low-latency electronically steered Phased Array Links and models free-space optical inter-satellite links using Gaussian beam propagation with explicit sub-microradian structural jitter. Orbital dynamics are modeled within the Circular Restricted Three-Body Problem (CR3BP) framework, augmented with J₂ gravitational perturbations to better represent real cislunar conditions. A novel Relative Planarity Factor is introduced to maintain short-arc filter stability and multi-target observability during tracking handoffs across these regimes. A decentralized SatNetOps protocol stack with LLM-GLM parallel routing achieves sustained end-to-end availability above 99.99% while enabling autonomous, self-healing topology management with minimal ground-in-the-loop dependence. This work provides a practical systems-engineering foundation for persistent multi-agent coordination and situational awareness for the Genesis Mission across the Earth-Moon system.