Motion · module · mission design

Keplerian propagator — elements to ground track

2D polar plot in the orbit plane. Elements shown live; true anomaly sweeps per Kepler's 2nd law (equal areas in equal times).

LIVE
semi-major axis · a
6778 km
eccentricity · e
0.0067
inclination · i
51.6°
true anomaly · ν
period · T
92.7 min
altitude · h
418 km

Equal-area sweep visible: the swept sector stays the same area per unit time even as angular speed changes. This is the real law, computed numerically.