private formula
Accounts for argument of periapsis and true anomaly of satellite at point of instantaneous change in velocity
Formula has warnings so can not be used - press "edit" below in order to fix.
| Δvi | delta-v (m*s-1) |
| vi | instantaneous velocity (m*s-1) |
| Δi | change in inclination (deg) |
| e | eccentricity (dimensionless) |
| ω | argument of periapsis (deg) |
| f | true anomaly (deg) |
| n | mean motion (°*s-1) |
| a | semi-major axis (m) |