Orbit
Altitude, inclination, epoch and eclipse geometry.
02 / SPACE ENVIRONMENT
Conditions beyond the spacecraft.
Operational context from trusted public sources, presented with source times and clear data classifications.
LIVE ENVIRONMENT SOURCE CONNECTION PLANNED
PLANETARY K-INDEX3QUIET
SOLAR WIND412KM/S
ACTIVE REGIONS08VISIBLE DISK
RADIO BLACKOUTR0NONE
DEMONSTRATION VALUES · LIVE NOAA CONNECTION SCHEDULED FOR PRODUCT PHASE
03 / THE POWER PROBLEM
A mission is an energy sequence, not a static spreadsheet.
Solar generation, system loads and payload activities change throughout every orbit. A positive average power budget can still hide a critical period of battery depletion.
See what SolaGuard models04 / SOLAGUARD SIM
Test the power margin.
Adjust a simplified mission profile and see how the battery responds across a representative low Earth orbit.
MISSION INPUTSDEMO MODEL
ORBIT 001 RESULTREVIEW REQUIRED
SUNLIGHT · 58 MINECLIPSE · 31 MIN
MINIMUM SOC64%
ORBIT ENERGY-3.5 Wh
CLASSIFICATIONMODELLED
05 / MODEL
One connected system.
Power is calculated across orbit geometry, solar input, storage, spacecraft loads and timed activities.
Solar
Illumination, panel area, orientation and efficiency.
Battery
Capacity, charge rate, depth of discharge and margin.
Mission loads
Bus demand, payload modes and communication windows.
06 / OPEN DATA
Transparent by design.
Every live value will retain its source, observation time, fetch time and freshness state.
01CELESTRAK
Orbital elements
2–4 HR02NOAA SWPC
Space weather
15–30 MIN03NASA DONKI
Solar events
15–60 MIN04SATNOGS
Satellite metadata
DAILYPRELIMINARY MISSION MODELLING