SpaceObject.update¶
SpaceObject.update
-
SpaceObject.
update
(**kwargs)[source]¶ If a pyorb.Orbit is present, updates the orbital elements and Cartesian state vector of the space object.
Can update any of the related state parameters, all others will automatically update.
Cannot update Keplerian and Cartesian elements simultaneously.
- Parameters
a (float) – Semi-major axis in km
e (float) – Eccentricity
i (float) – Inclination in degrees
aop/omega (float) – Argument of perigee in degrees
raan/Omega (float) – Right ascension of the ascending node in degrees
mu0/anom (float) – Mean anomaly in degrees
x (float) – X position in km
y (float) – Y position in km
z (float) – Z position in km
vx (float) – X-direction velocity in km/s
vy (float) – Y-direction velocity in km/s
vz (float) – Z-direction velocity in km/s