TPU Core Temperature
48.2 °C
Thermal Margin: +31.8°C
In-Orbit AI Throughput
20.4 PFLOPS
100% Full Yield (FP8)
Solar Yield / Load
10.4 kW
+1.9 kW Net Surplus
Orbit Period / Eclipse
95.6 min
0 min shadow (Sunlit)
PROPAGATING ORBIT
Alt: 550 km | V: 7.59 km/s | Inc: 97.6° (SSO)
t = 00:00
ORBITAL CYCLE HARMONICS (1 REVOLUTION PROFILE)
TPU Core Temp (°C)
Solar Gen (kW)
Inference FLOPS
Throttle Line (80°C)

Why Project Suncatcher Uses Dawn-Dusk SSO

Standard LEO orbits spend ~35 minutes of every 90-minute pass inside Earth's cold eclipse shadow (umbra), draining massive battery mass and triggering extreme thermal cycling. At high beta angles (β ≥ 68° in Sun-Synchronous Orbit), the satellite skims Earth's terminator line in perpetual sunlight, unlocking continuous solar power and uninterrupted inference pipelines.

Stefan-Boltzmann Radiative Cooling in Vacuum

With no atmosphere for convection, heat can only escape via thermal radiation: Q = ε · σ · A · (T_rad&sup4; - T_space&sup4;). When an 8.5 kW AI payload runs hot, deployable loop heat pipes transfer silicon die heat to edge-oriented optical solar reflectors. If radiator equilibrium exceeds 80°C, dynamic frequency scaling throttles FLOPS to prevent latchup.

Enjoy this tool? Build your own with Super