Package org.jscience.astronomy.solarsystem.artificialsatellites

Interface Summary
Propagator Instances of classes which implement this interface propagate orbital state from an epoch at which the orbital state is known to a desired delta since the epoch.
 

Class Summary
AbstractPropagator An abstract class providing implementations of methods common across all implementations of the Propagator interface.
DRIVER DRIVER 3 NOV 80

WGS-72 PHYSICAL AND GEOPOTENTIAL CONSTANTS CK2= .5*J2*AE**2 CK4=-.375*J4*AE**4

ElementSet  
OrbitalState Represents orbital state of the spacecraft at a point in time.
PropagatorFactory Instances of this factory construct instances of AbstractPropagator based on
SDP4 Implementation of NORAD's SDP4 deep space propagator.
SDP8 Implementation of NORAD's SDP8 deep space propagator.
SGP Implementation of NORAD's SGP near-Earth propagator.
SGP4 Implementation of NORAD's SGP4 near-Earth propagator.
SGP8 Implementation of NORAD's SGP8 near-Earth propagator.
 

Exception Summary
NoSuchPropagatorException