Ground track and station geometry
A CubeSat inside an orbital environment
F3 environmentSimulated truth
CubeSTEM MissionLab Twin
Orbit workbench · M3-A environment + Orbit v2 J2 · Practice only
Mission time
— s
Latitude / longitude
—
Altitude
— km
Illumination
—
Orbital reference vectors
Sun direction ECI
—
Simulated
Nadir direction ECI
—
Derived
Magnetic direction ECI
—
Simulated