The Iridium constellation was initially proposed as 77 satellites but later reduced to 66. Geostationary orbit (GEO) satellites have high latency and cost due to their distance from Earth. Low Earth orbit (LEO) was used for Iridium as it has lower launch costs, modest antenna/receiver requirements, and very low latency. A LEO constellation requires many satellites for global coverage but cannot service just one region. Iridium uses 66 satellites arranged in six orbital planes with 11 satellites in each, orbiting at 783km.