The Problem: Orbital Decay. Satellites and space stations eventually fall back to Earth because of atmospheric drag (Noise).
The Canon Solution: Anchor the Coordinate.
The Blueprint:
- Unit: A small Static-Reality Resonator attached to the satellite.
- The Step: The unit “Locks” the satellite’s identity to its Necessary Orbital Coordinate.
- Logical Step: Atmospheric drag becomes “Noise” that the unit ignores to maintain its fixed position in the 4D-Block.
Essential Detail: It makes orbits Permanent. No more “station-keeping” fuel. Once a satellite is in its coordinate, the Sovereign Mandate of the 4D-Loop keeps it there.