macrosatellites

Macrosatellites are large artificial satellites that sit above the small- and micro-satellite classes in terms of payload mass and bus complexity. The term is not part of a formal international standard and is used informally to describe satellites that are significantly larger than typical micro-, nano-, or small-satellite platforms. In practice, estimates of what constitutes a macrosatellite vary, but they are generally described as weighing roughly one tonne or more, often ranging into several tonnes or more, and designed to carry substantial and power‑hungry payloads.

Because there is no single definition, macrosatellites are commonly associated with missions that require substantial propulsion, power generation, and large payload accommodations. They often employ robust spacecraft buses, advanced attitude control, and thermal management systems to support high data rates, heavy sensors, or long mission lifetimes. Depending on mission goals, macrosatellites may operate in low Earth orbit, medium Earth orbit, or geostationary orbit, with the choice driven by communications capacity, imaging performance, or scientific objectives.

Typical applications include high‑capacity communications and broadband services, high‑resolution earth observation, large scientific instruments, and demonstrations of new propulsion or power technologies. The size and cost of macrosatellites tend to make them fewer in number and more reliant on established ground support and launch infrastructure than smaller satellite classes. As launch costs decline and payload demands grow, the use of macrosatellite platforms continues to be discussed in industry and government programs, though the term remains informal and context-dependent.

See also: micro-satellite, mini-satellite, small satellite, mega-constellation, satellite bus.