#00213
Place accelerators on satellites in sun-synchronous orbit, drawing near-continuous solar power, rejecting heat through radiators, and linking satellites by free-space optical fabric. One GPU has flown; independent analyses put costs at least an order of magnitude above equivalent
Parent issue
#00204 Data-centers siting concentrates noise, water, air and cost burdens on host communities while the benefits are dispersed
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Description
Fly accelerators on satellites in sun-synchronous or dawn-dusk orbit, drawing near-continuous solar power without atmospheric losses, rejecting heat through radiators, and linking satellites by free-space optical fabric. The community argument is absolute: no host community, no municipal water, no grid interconnection queue, no noise.
Starcloud-1 launched on 2 November 2025 on a Falcon 9 into a 325 km orbit: a 60 kg satellite on an Astro Digital bus carrying a single Nvidia H100, the first data-centre-class GPU in orbit, with a design life of about 11 months and controlled deorbit (Gunter's Space Page, Data Center Frontier). Company-sourced reporting says it ran Gemma inference and trained a nanoGPT-scale model.
That demonstrates one GPU surviving and operating in low Earth orbit. It does not demonstrate multi-kilowatt thermal rejection, inter-satellite fabric, multi-year radiation survival, or any economics.
Elsewhere: Google's Project Suncatcher plans 81 satellites at about 650 km using Trillium TPUs with two Planet Labs prototypes by early 2027, and nothing has flown (Google). China launched the first 12 satellites of a computing constellation in May 2025 at up to 744 TOPS each with 100 Gbps laser links, holding ITU approval for 2,800 (China-in-Space). Starcloud raised $170 million at a $1.1 billion valuation in March 2026 and describes a long-term 5 GW deployment with a 4 square kilometre solar array (DCD).
In vacuum the only heat path is radiation, so a data centre in orbit is mostly a radiator. Published estimates per megawatt: about 1,600 m² (World Economic Forum), about 1,200 m² (EE Times), and 700 to 1,800 m² (RCR Wireless). Scaling ISS-era thermal hardware implies roughly 100 tonnes of radiator per megawatt against about 10 tonnes of compute. A gigawatt implies 0.7 to 2 km² of radiator, and coating degradation from UV and atomic oxygen increases required area over the mission.
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