Transformation of the small body's coordinates
Osculating elements must obey the following order:
1) first element (see below)
2) eccentricity
3) inclination (deg.)
4) ascending node (deg.)
5) argument of perihelion (deg.)
6) sixth element (see below)
For a transformation of the date (epoch) press
here
Source parameters
Results of transformation
Start epoch (JD):
Final epoch (JD):
2.63175247682656786E-02 -1.15069612611999668E+00 -5.26832094716382978E-01 7.54329011174517878E-03 -8.93364562089686035E-03 -7.50017430598116142E-03
Gaussian gravitational constant:
^2
Mass of the body:
of the Sun's mass
equator 2000.0
ecliptic 2000.0
equator 2000.0
ecliptic 2000.0
rectangular coordinates and velocities
osculating elements
rectangular coordinates and velocities
osculating elements
Output format:
fixed
exponential
number of decimal places
For the osculating elements:
First element:
semi-major axis (AU)
perihelion distance (AU)
mean motion (deg./day)
Sixth element:
mean anomaly (deg.)
perihelion time (JD)
First element:
semi-major axis (AU)
perihelion distance (AU)
mean motion (deg./day)
Sixth element:
mean anomaly (deg.)
perihelion time (JD)