A Walker constellation is a symmetric satellite pattern: identical circular orbits at one inclination, planes spaced evenly around the equator, satellites spaced evenly within each plane, with a fixed phase offset between planes. Written i: t/p/f — Galileo's design is 56°: 24/3/1.
Understanding Walker Constellation
Reading i: t/p/f
Take 56°: 24/3/1. Inclination 56°; 24 satellites; 3 planes of 8, their ascending nodes 120° apart; and f = 1, meaning when a satellite crosses the equator, its counterpart one plane east sits 1 × 360°/24 = 15° further along its orbit. The phasing term is the subtle one — it staggers the planes like bricks in a wall so coverage gaps never align. Different f values change nothing about each plane individually yet dramatically change worst-case coverage and, for dense constellations, self-conjunction geometry: a poorly phased pattern brings satellites of adjacent planes repeatedly close at the orbit crossings, while a well-chosen f keeps the whole lattice comfortably separated.
From elegant maths to operational lattice
A paper Walker is perfectly symmetric; a real one is a maintained approximation. Earth's oblateness precesses all planes together (the design survives because symmetry is preserved), but drag differences, failures and launch insertion errors constantly nudge satellites off their slots, so operators fly continuous station-keeping to hold the pattern, keep spares parked below the operational altitude, and rebalance planes after losses. Filling a Walker is also a logistics puzzle: each launch delivers a batch to one plane, then phasing manoeuvres spread the batch around it — and reaching a different plane is expensive, since plane changes cost far more than altitude changes. The pattern's elegance on paper conceals years of choreography in practice.