OBJECT = COLUMN NAME = JULIAN_DAY COLUMN_NUMBER = 1 BYTES = 13 DATA_TYPE = ASCII_REAL START_BYTE = 1 FORMAT = "F13.5" DESCRIPTION = "UTC time at *midpoint* of data collection given in Julian day." END_OBJECT = COLUMN OBJECT = COLUMN NAME = UTC_TIME COLUMN_NUMBER = 2 BYTES = 19 DATA_TYPE = CHARACTER START_BYTE = 15 DESCRIPTION = "UTC time at *midpoint* of data collection. Format: YYYY-MM-DDTHH:MM:SS" END_OBJECT = COLUMN OBJECT = COLUMN NAME = MET COLUMN_NUMBER = 3 BYTES = 12 DATA_TYPE = ASCII_INTEGER START_BYTE = 35 DESCRIPTION = "Time tag in seconds at the start of the associated reporting/accumulation period." END_OBJECT = COLUMN OBJECT = COLUMN NAME = ORBIT_NUMBER COLUMN_NUMBER = 4 BYTES = 4 DATA_TYPE = ASCII_INTEGER START_BYTE = 48 DESCRIPTION = "Unique identifier for a given orbit of MESSENGER around Mercury. Orbit number is defined as starting at apoherm and is calculated using the MET value and the appropriate SPICE kernels (see GEOMETRY/geominfo.txt). Orbit numbering does not start until MESSENGER performs the Mercury orbit insertion. Until that time the value for orbit number is 0." END_OBJECT = COLUMN OBJECT = COLUMN NAME = ACTUAL_ACCUM COLUMN_NUMBER = 5 BYTES = 4 DATA_TYPE = ASCII_INTEGER START_BYTE = 53 DESCRIPTION = "Actual accumulation period in seconds for software counters and energy histograms." END_OBJECT = COLUMN OBJECT = COLUMN NAME = SENSOR_TEMP COLUMN_NUMBER = 6 BYTES = 7 DATA_TYPE = ASCII_REAL START_BYTE = 58 FORMAT = "F7.3" DESCRIPTION = "NS sensor temperature in units of degree C." END_OBJECT = COLUMN OBJECT = COLUMN NAME = ALTITUDE COLUMN_NUMBER = 7 BYTES = 10 DATA_TYPE = ASCII_REAL START_BYTE = 66 FORMAT = "F10.3" DESCRIPTION = "Spacecraft altitude above the subsatellite point on the target in units of km." END_OBJECT = COLUMN OBJECT = COLUMN NAME = LATITUDE COLUMN_NUMBER = 8 BYTES = 7 DATA_TYPE = ASCII_REAL START_BYTE = 77 FORMAT = "F7.3" DESCRIPTION = "Target-centric latitude of the spacecraft subsatellite point in degrees." END_OBJECT = COLUMN OBJECT = COLUMN NAME = LONGITUDE COLUMN_NUMBER = 9 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 85 FORMAT = "F8.3" DESCRIPTION = "Target-centric longitude of the spacecraft subsatellite point in degrees." END_OBJECT = COLUMN OBJECT = COLUMN NAME = LOCAL_TIME COLUMN_NUMBER = 10 BYTES = 10 DATA_TYPE = ASCII_REAL START_BYTE = 94 FORMAT = "F10.3" DESCRIPTION = "Local time of the spacecraft subsatellite point in hours from 0 to 24." END_OBJECT = COLUMN OBJECT = COLUMN NAME = VELOCITY_VECTOR COLUMN_NUMBER = 11 BYTES = 26 DATA_TYPE = ASCII_REAL START_BYTE = 105 ITEMS = 3 ITEM_BYTES = 8 ITEM_OFFSET = 9 FORMAT = "F8.3" DESCRIPTION = "Three element spacecraft velocity vector expressed in the nadir-fixed coordinate system with each component in units of km/second." END_OBJECT = COLUMN OBJECT = COLUMN NAME = VEL_NORM COLUMN_NUMBER = 12 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 132 FORMAT = "F8.3" DESCRIPTION = "Magnitude of the spacecraft velocity as expressed in the nadir-fixed coordinate system in units of km/second." END_OBJECT = COLUMN OBJECT = COLUMN NAME = SC_TO_NADIR_ROT COLUMN_NUMBER = 13 BYTES = 80 DATA_TYPE = ASCII_REAL START_BYTE = 141 ITEMS = 9 ITEM_BYTES = 8 ITEM_OFFSET = 9 FORMAT = "F8.3" DESCRIPTION = "Nine element rotation matrix that converts the spacecraft attitude from instrument-fixed coordinates to nadir-fixed coordinates." END_OBJECT = COLUMN OBJECT = COLUMN NAME = VDOT_X COLUMN_NUMBER = 14 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 222 FORMAT = "F8.3" DESCRIPTION = "Velocity normalized dot product of the vector velocity and the spacecraft x-axis unit vector expressed as a unitless number from -1 to 1." END_OBJECT = COLUMN OBJECT = COLUMN NAME = VDOT_Y COLUMN_NUMBER = 15 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 231 FORMAT = "F8.3" DESCRIPTION = "Velocity normalized dot product of the vector velocity and the spacecraft y-axis unit vector expressed as a unitless number from -1 to 1." END_OBJECT = COLUMN OBJECT = COLUMN NAME = VDOT_Z COLUMN_NUMBER = 16 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 240 FORMAT = "F8.3" DESCRIPTION = "Velocity normalized dot product of the vector velocity and the spacecraft z-axis unit vector expressed as a unitless number from -1 to 1." END_OBJECT = COLUMN OBJECT = COLUMN NAME = NADIR_ANGLE COLUMN_NUMBER = 17 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 249 FORMAT = "F8.3" DESCRIPTION = "Spacecraft orientation angle of the spacecraft z-axis and the spacecraft-to-planet center vector in units of degrees." END_OBJECT = COLUMN OBJECT = COLUMN NAME = YAXIS_ANGLE COLUMN_NUMBER = 18 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 258 FORMAT = "F8.3" DESCRIPTION = "Spacecraft orientation angle of the spacecraft y-axis and the spacecraft-to-planet center vector in units of degrees." END_OBJECT = COLUMN OBJECT = COLUMN NAME = XAXIS_ANGLE COLUMN_NUMBER = 19 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 267 FORMAT = "F8.3" DESCRIPTION = "Spacecraft orientation angle of the spacecraft x-axis and the spacecraft-to-planet center vector in units of degrees." END_OBJECT = COLUMN OBJECT = COLUMN NAME = THETA_ANGLE COLUMN_NUMBER = 20 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 276 FORMAT = "F8.3" DESCRIPTION = "Polar angle look direction (in a theta,phi spherical geometry) of the spacecraft in the spacecraft-fixed coordinate system. THETA_ANGLE = 0 degrees is when the spacecraft z-axis points in the same direction as the spacecraft-to-planet center vector (nadir pointing)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = PHI_ANGLE COLUMN_NUMBER = 21 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 285 FORMAT = "F8.3" DESCRIPTION = "Azimuthal angle look direction (in a theta,phi spherical geometry) of the spacecraft in the spacecraft-fixed coordinate system. PHI_ANGLE = 0 degrees is when the spacecraft x-axis points along the direction of travel." END_OBJECT = COLUMN OBJECT = COLUMN NAME = BETA_ANGLE COLUMN_NUMBER = 22 BYTES = 8 DATA_TYPE = ASCII_REAL START_BYTE = 294 FORMAT = "F8.3" DESCRIPTION = "Angle of the normal of the spacecraft orbital plane with respect to Mercury-to-Sun vector in degrees." END_OBJECT = COLUMN OBJECT = COLUMN NAME = SUN_DISTANCE COLUMN_NUMBER = 23 BYTES = 12 DATA_TYPE = ASCII_REAL START_BYTE = 303 FORMAT = "F12.3" DESCRIPTION = "Distance of the spacecraft to the Sun in units of km." END_OBJECT = COLUMN OBJECT = COLUMN NAME = LG1_CPS COLUMN_NUMBER = 24 BYTES = 7 DATA_TYPE = ASCII_REAL START_BYTE = 316 FORMAT = "F7.3" DESCRIPTION = "Net neutron count rate from the LG1 sensor in units of counts per second." END_OBJECT = COLUMN OBJECT = COLUMN NAME = LG1_ERR_CPS COLUMN_NUMBER = 25 BYTES = 7 DATA_TYPE = ASCII_REAL START_BYTE = 324 FORMAT = "F7.3" DESCRIPTION = "Net uncertainty (error) in the the LG1 count rate in units of counts per second." END_OBJECT = COLUMN OBJECT = COLUMN NAME = LG2_CPS COLUMN_NUMBER = 26 BYTES = 7 DATA_TYPE = ASCII_REAL START_BYTE = 332 FORMAT = "F7.3" DESCRIPTION = "Net neutron count rate from the LG2 sensor in units of counts per second." END_OBJECT = COLUMN OBJECT = COLUMN NAME = LG2_ERR_CPS COLUMN_NUMBER = 27 BYTES = 7 DATA_TYPE = ASCII_REAL START_BYTE = 340 FORMAT = "F7.3" DESCRIPTION = "Net uncertainty (error) in the the LG2 count rate in units of counts per second." END_OBJECT = COLUMN OBJECT = COLUMN NAME = BP_CPS COLUMN_NUMBER = 28 BYTES = 7 DATA_TYPE = ASCII_REAL START_BYTE = 348 FORMAT = "F7.3" DESCRIPTION = "Net neutron count rate from the BP sensor in units of counts per second." END_OBJECT = COLUMN OBJECT = COLUMN NAME = BP_ERR_CPS COLUMN_NUMBER = 29 BYTES = 7 DATA_TYPE = ASCII_REAL START_BYTE = 356 FORMAT = "F7.3" DESCRIPTION = "Net uncertainty (error) in the the BP count rate in units of counts per second." END_OBJECT = COLUMN