@spiceErrorCheck<EOL>def sce2s(sc, et, lenout=_default_len_out):
sc = ctypes.c_int(sc)<EOL>et = ctypes.c_double(et)<EOL>sclkch = stypes.stringToCharP("<STR_LIT:U+0020>" * lenout)<EOL>lenout = ctypes.c_int(lenout)<EOL>libspice.sce2s_c(sc, et, lenout, sclkch)<EOL>return stypes.toPythonString(sclkch)<EOL>
Convert an epoch specified as ephemeris seconds past J2000 (ET) to a
character string representation of a spacecraft clock value (SCLK).

http://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/cspice/sce2s_c.html

:param sc: NAIF spacecraft clock ID code.
:type sc: int
:param et: Ephemeris time, specified as seconds past J2000.
:type et: float
:param lenout: Maximum length of output string.
:type lenout: int
:return: An SCLK string.
:rtype: str