@spiceErrorCheck<EOL>def conics(elts, et):
elts = stypes.toDoubleVector(elts)<EOL>et = ctypes.c_double(et)<EOL>state = stypes.emptyDoubleVector(<NUM_LIT:6>)<EOL>libspice.conics_c(elts, et, state)<EOL>return stypes.cVectorToPython(state)<EOL>
Determine the state (position, velocity) of an orbiting body
from a set of elliptic, hyperbolic, or parabolic orbital
elements.

http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/conics_c.html

:param elts: Conic elements.
:type elts: 8-Element Array of floats
:param et: Input time.
:type et: float
:return: State of orbiting body at et.
:rtype: 6-Element Array of floats