STEREO SEP Suite Pointing Data

STEREO atttitude and orbit data are distributed as SPICE kernels.
Since most SEP investigators would rather not deal with SPICE kernels,
Caltech provides text files containing transformation matrices for
converting vectors from the Spacecraft coordinate system to the
following coordinate systems: GEI, GSE, GSM, HCI, HEE, HEEQ, RTN.

Important Note: these data produced at Caltech for the benefit of SEP instrument suite
investigators. The data are not currently officially "blessed" by the larger STEREO
team. 

The format of each record in these files is as follows:

YYYY DoY Second Flag M_00 M_01 M_02 M_10 M_11 M_12 M_20 M_21 M_22 
	Where YYYY is the 4-digit year
	DoY is the day-of-year (counting from 1)
	Second is the second-of-day
	Flag is	0 if the data are predictive, 1 if the data are definitive
	M_ij are the transformation matrix elements from the S/C coordinate system 
	to the new coordinate system, where i is the row index, j is the column index.

The time cadence of records within these files is variable. A new record is appended only 
	At the beginning of each day, or 
	If the direction of the S/C X-axis changes by more than TOL degrees, or
	If the direction of the S/C Y-axis changes by more than TOL degrees

Currently, TOL is set at 0.25 degrees.

Further information about the Spacecraft coordinate system, converting from an SEP 
instrument coordinate system to the S/C coordinate system, and descriptions of the 
geocentric and heliocentric coordinate systems listed above, may be found in
SEP_Attitude_Orbit.pdf (http://www.srl.caltech.edu/STEREO2/Pointing/SEP_Attitude_Orbit.pdf).

The daily updating of these data goes 40 days into the future, and 15 days
into the past.  This is usually sufficient to ensure that all the data in the
files eventually get promoted form "predicted" to definitive".  On occasion, I
take a manual look at the data to make sure that this is all working as
expected.  Occasionally, the MOC has been very slow in delivering definitive
data.

SEP_Attitude_orbit.pdf

Coordinate system descriptions