This package provides an interface to representation of the position and geometry of space objects such as stars, planets or asteroids.
The position of celestial bodies is represented by the CelestialBody interface. This interface provides the methods needed to either consider the body as an external one for its gravity or lighting influence on spacecraft (typically in perturbing force computations) or as an internal one with its own frame.
The CelestialBodyFactory class is a factory providing several predefined instances implementing the CelestialBody interface for the main solar system bodies. The Sun, the Moon, the eight planets and the Pluto dwarf planet are the supported bodies. In addition to these real bodies, two points are supported for convenience as if they were real bodies: the solar system barycenter and the Earth-Moon barycenter. By default, the CelestialBodyFactory retrieve positions and velocities from binary ephemerides files compatible with the the JPL DE formats like DE 405, DE 406, DE 423 ... as well as the IMCCE Inpop ephemerides which share a similar format. This default handling can be overridden by defining a user specific loader for JPL ephemerides.
As an example, computing the position of the Sun and the Moon, in the EME2000 frame, is done as follows:
CelestialBody sun = CelestialBodyFactory.getSun();
CelestialBody moon = CelestialBodyFactory.getMoon();
Vector3D sunInEME2000 =
sun.getPVCoordinates(date, FramesFactory.getEME2000()).getPosition();
Vector3D moonInEME2000 =
moon.getPVCoordinates(date, FramesFactory.getEME2000()).getPosition();Since the supported bodies implement the CelestialBody interface, they all provide their own body-centered inertially-oriented frame and their own body-centered body-oriented frame, hence adding a few more frames to the ones provided by the frames package. The body-oriented frames use the IAU pole and prime meridian definition. Since the frames tree is rooted at an Earth-centered frame, the solar system bodies frames tree does not seem to be in canonical form. This of course is only a side effect of the arbitrary choice of GCRF as the root frame and has no effect at all on computations. The solar system bodies frames tree is shown below:
The shape of celestial bodies is represented by the BodyShape interface.
Only one implementation is provided by Orekit for now: the OneAxisEllipsoid class, which represents the natural flattened shape of big space rotating bodies like planets or the Sun.
For asteroids, it is expected that users will provide their own shape models, for example based on tessellation. They should implement the BodyShape interface in order to be used by Orekit.
When using OneAxisEllipsoid body representation, points are generally described in associated body frame, by so-called geodetic coordinates (longitude, latitude, altitude). The GeodeticPoint class allows handling of such coordinates. It is a simple container that does not provide processing methods except basic computation of canonical topocentric directions (Zenith/Nadir, East/West, North/South).