OBJECT = COLUMN NAME = "UTC_TIME" COLUMN_NUMBER = 1 DATA_TYPE = TIME START_BYTE = 1 BYTES = 23 FORMAT = "A23" DESCRIPTION = "UTC time." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ACS_MODE" COLUMN_NUMBER = 2 DATA_TYPE = CHARACTER START_BYTE = 26 BYTES = 7 FORMAT = "A7" DESCRIPTION = "Attitude Control Subsystem (ACS) mode." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ATT_QU_I2B_1" COLUMN_NUMBER = 3 DATA_TYPE = ASCII_REAL START_BYTE = 35 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current Spacecraft Attitude Quaternion Based on the Current AD State Running. 1st Element. This quaternion rotates a vector in Earth-Mean-Equator J2000 frame into the spacecraft frame. It follows the convention identified as ``the second system'' in the dictionary definition of the standard PDS keyword QUATERNION_DESC." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ATT_QU_I2B_2" COLUMN_NUMBER = 4 DATA_TYPE = ASCII_REAL START_BYTE = 48 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current Spacecraft Attitude Quaternion Based on the Current AD State Running. 2nd Element. This quaternion rotates a vector in Earth-Mean-Equator J2000 frame into the spacecraft frame. It follows the convention identified as ``the second system'' in the dictionary definition of the standard PDS keyword QUATERNION_DESC." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ATT_QU_I2B_3" COLUMN_NUMBER = 5 DATA_TYPE = ASCII_REAL START_BYTE = 61 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current Spacecraft Attitude Quaternion Based on the Current AD State Running. 3rd Element. This quaternion rotates a vector in Earth-Mean-Equator J2000 frame into the spacecraft frame. It follows the convention identified as ``the second system'' in the dictionary definition of the standard PDS keyword QUATERNION_DESC." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ATT_QU_I2B_4" COLUMN_NUMBER = 6 DATA_TYPE = ASCII_REAL START_BYTE = 74 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current Spacecraft Attitude Quaternion Based on the Current AD State Running. Scalar Component. This quaternion rotates a vector in Earth-Mean-Equator J2000 frame into the spacecraft frame. It follows the convention identified as ``the second system'' in the dictionary definition of the standard PDS keyword QUATERNION_DESC." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ATT_RAT_BF_X" COLUMN_NUMBER = 7 DATA_TYPE = ASCII_REAL START_BYTE = 87 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current Spacecraft Angular Rates in the Spacecraft Body Frame Based on the Current AD State Running. Radians/sec. X-Axis Component." UNIT = "RADIAN PER SECOND" END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ATT_RAT_BF_Y" COLUMN_NUMBER = 8 DATA_TYPE = ASCII_REAL START_BYTE = 100 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current Spacecraft Angular Rates in the Spacecraft Body Frame Based on the Current AD State Running. Radians/sec. Y-Axis Component." UNIT = "RADIAN PER SECOND" END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ATT_RAT_BF_Z" COLUMN_NUMBER = 9 DATA_TYPE = ASCII_REAL START_BYTE = 113 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current Spacecraft Angular Rates in the Spacecraft Body Frame Based on the Current AD State Running. Radians/sec. Z-Axis Component." UNIT = "RADIAN PER SECOND" END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ATT_ERR_BF_X" COLUMN_NUMBER = 10 DATA_TYPE = ASCII_REAL START_BYTE = 126 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current S/C Angular Attitude Error in the Spacecraft Body Frame, Phased as Current Attitude Subtracted from Reference Attitude. Radians. X-Axis Component." UNIT = "RADIAN" END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ATT_ERR_BF_Y" COLUMN_NUMBER = 11 DATA_TYPE = ASCII_REAL START_BYTE = 139 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current S/C Angular Attitude Error in the Spacecraft Body Frame, Phased as Current Attitude Subtracted from Reference Attitude. Radians. Y-Axis Component." UNIT = "RADIAN" END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ATT_ERR_BF_Z" COLUMN_NUMBER = 12 DATA_TYPE = ASCII_REAL START_BYTE = 152 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current S/C Angular Attitude Error in the Spacecraft Body Frame, Phased as Current Attitude Subtracted from Reference Attitude. Radians. Z-Axis Component." UNIT = "RADIAN" END_OBJECT = COLUMN OBJECT = COLUMN NAME = "RAT_ERR_BF_X" COLUMN_NUMBER = 13 DATA_TYPE = ASCII_REAL START_BYTE = 165 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current Spacecraft Angular Rate Error in the Spacecraft Body Frame, Phased as Current Rate Subtracted from Reference Rate. Radians/sec. X-Axis Component." UNIT = "RADIAN PER SECOND" END_OBJECT = COLUMN OBJECT = COLUMN NAME = "RAT_ERR_BF_Y" COLUMN_NUMBER = 14 DATA_TYPE = ASCII_REAL START_BYTE = 178 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current Spacecraft Angular Rate Error in the Spacecraft Body Frame, Phased as Current Rate Subtracted from Reference Rate. Radians/sec. Y-Axis Component." UNIT = "RADIAN PER SECOND" END_OBJECT = COLUMN OBJECT = COLUMN NAME = "RAT_ERR_BF_Z" COLUMN_NUMBER = 15 DATA_TYPE = ASCII_REAL START_BYTE = 191 BYTES = 12 FORMAT = "F12.9" DESCRIPTION = "Current Spacecraft Angular Rate Error in the Spacecraft Body Frame, Phased as Current Rate Subtracted from Reference Rate. Radians/sec. Z-Axis Component." UNIT = "RADIAN PER SECOND" END_OBJECT = COLUMN