/**************************************************************************/
/* This structure describes the format of the */
/* ephemeris data records of the Pioneer Venus Orbiter (PVO) */
/* Supplementary Experimental Data Record (SEDR). The following is */
/* an overview in tabular form of each ephemeris data record: */
/**************************************************************************/
/* BIT 1 1 1 1 1 1 1 1 1 1 2 2 2 2 2 2 2 2 2 2 3 3 */
/* 0 1 2 3 4 5 6 7 8 9 0 1 2 3 4 5 6 7 8 9 0 1 2 3 4 5 6 7 8 9 0 1 */
/* WORD ________________________________________________________________________________*/
/* 0 | S/C YEAR | S/C DOY | NAME VAR */
/* |_______________________________________________________________|_______________*/
/* 1 | S/C UT in binary | SCUT 1 */
/* |_______________________________________________________________|_______________*/
/* 2-3 |DP Julian Date, Days (elapsed days from | JULDAT */
/* |Noon, 1 Jan. 4713 B.C. | 2 */
/* |_______________________________________________________________|_______________*/
/* 4-5 |Gregorian Calendar Date (2 integer words which | */
/* |represent the vigestimal date) based on number 20 | VIGDAT 3 */
/* |_______________________________________________________________|_______________*/
/* 6-7 |ET - UTC, set (Universal Time Co-ordinated) | ETMUTC 4 */
/* |_______________________________________________________________|_______________*/
/* 8-9 |Range rate of probe. km/sec + | RANGRF 5 */
/* |___________________________________________________|___________|_______________*/
/* 10-11 |Magnitude of velocity vector, km/sec (speed of S/C)| Geocentric| MAGVEL 6 */
/* |___________________________________________________|___________|_______________*/
/* 12-13 |Earth.probe range, km (radius to S/C) + | REARPR 7 */
/* |_______________________________________________________________|_______________*/
/* 14-15 |Range to probe, km + | MRANGE 8 */
/* |___________________________________________________|___________|_______________*/
/* 16-17 |Probe inertia velocity, km/sec | | MMAGVF 9 */
/* |___________________________________________________|___________|_______________*/
/* 16-19 |Probe inertial path angle, deg | HELIO- | HINFTP 10 */
/* |___________________________________________________| CENTRIC |_______________*/
/* 20-21 |Celestial latitude of probe, deg | | CELLTF 11 */
/* |___________________________________________________|___________|_______________*/
/* 22-23 |Celestial longitude of probe, deg | | CELLNF 12 */
/* |___________________________________________________|___________|_______________*/
/* 24-25 |Celestial latitude of Earth, deg | | CELLTE 13 */
/* |___________________________________________________|___________|_______________*/
/* 26-27 |Celestial longitude of Earth, deg | | CELLNE 14 */
/* |___________________________________________________|___________________________*/
/* 28-29 |X component of S/C in Sun-Earth line, km | HELIO- | XSCSEL 15 */
/* |___________________________________________________| CENTRIC _|_______________*/
/* 30-31 |Y component of S/C in Sun.Earth line, km | | YSCSEL 16 */
/* |___________________________________________________|___________|_______________*/
/* 32-33 |Z component of S/C in Sun.Earth line, km | | ZSCSEL 17 */
/* |___________________________________________________|___________|_______________*/
/* 34-35 |Sun-probe distance in Sun-Earth X-Y plane, km | | */
/* |(projection of Sun-S/C vector onto the X-Y plane | | SPSE 18 */
/* |___________________________________________________|___________|_______________*/
/* 36-37 | Longitude of S/C in Sun-Earth line system, deg + | LNPSEL 19 */
/* |_______________________________________________________________|_______________*/
/* 38-39 |X component of geocentric r of S/C, km + | XPGSFF 20 */
/* |____________________________________________|__________________|_______________*/
/* 40-41 |Y component of geocentric r of S/C, km | | YPGSFF 21 */
/* |____________________________________________|__________________|_______________*/
/* 42-43 |Z component of geocentric r of S/C, km | | ZPGSFF 22 */
/* |____________________________________________|__________________|_______________*/
/* 44-45 |X component of geocentric r of S/C, km/sec | | DXPGSF 23 */
/* |____________________________________________|__________________|_______________*/
/* 46-47 |Y component of geocentric r of S/C, km/sec | | DYPGSF 24 */
/* |____________________________________________|__________________|_______________*/
/* 46-49 |Z component of geocentric r of S/C, km/sec | | DZPGSF 25 */
/* |____________________________________________|__________________|_______________*/
/* 50-51 |X component of heliocentric r of S/C, km | | XPHSFF 26 */
/* |____________________________________________|__________________|_______________*/
/* 52-53 |Y component of heliocentric r of S/C, km | Space-fixed | YPHSFF 27 */
/* |____________________________________________| Coordinates ____|_______________*/
/* 54-55 |Z component of heliocentric r of S/C, km | FERP | ZPHSFF 28 */
/* |____________________________________________|_ Earth Mean ____|_______________*/
/* 56-57 |X component of heliocentric r of S/C, km/sec| Equinox & | DXPHSF 29 */
/* |____________________________________________| Ecliptic of ____|_______________*/
/* 56-55 |Y component of heliocentric r of S/C, km/sec| 1950.0 | DYPHSF 30 */
/* |____________________________________________|__________________|_______________*/
/* 60-61 |Z component of heliocentric r of S/C, km/sec| | DZPHSF 31 */
/* |____________________________________________|__________________|_______________*/
/* 62-63 |X component of body 1 - S/C r, km | + | XP1SFF 32 */
/* |____________________________________________|_|________________|_______________*/
/* 64-65 |Y component of body 1 - S/C r, km | | | YP1SFF 33 */
/* |____________________________________________|_|________________|_______________*/
/* 66-67 |Z component of body 1 - S/C r, km | | | ZP1SFF 34 */
/* |____________________________________________|_|_ Body ___|_______________*/
/* 68-69 |X component of body 1 - S/C r, km/sec | | 1 = Venus | DXP1SF 35 */
/* |____________________________________________|_|________________|_______________*/
/* 70-71 |Y component of body 1 - S/C r, km/sec | | | DYP1SF 36 */
/* |____________________________________________|_|________________|_______________*/
/* 72-73 |Z component of body 1 - S/C r, km/sec | | | DZP1SF 37 */
/* |____________________________________________|_|________________|_______________*/
/* 74-75 |Body 1 - S/C range, km | | | B1MAGR 38 */
/* |____________________________________________|_|________________|_______________*/
/* 76-77 |Body l - S/C velocity magnitude, km/sec + + | B1MAGV 39 */
/* |_______________________________________________________________|_______________*/
/* 78-79 |Latitude of probe, deg + | EALATP 40 */
/* |____________________________________________|__________________|_______________*/
/* 80-81 |Longitude of probe, deg | | EALOMP 41 */
/* |____________________________________________|_ Body Fixed Earth|_______________*/
/* 82-83 |Velocity magnitude of probe relative to body| (see EN/1) | EAVELP 42 */
/* |km/sec. | | */
/* |____________________________________________|__________________|_______________*/
/* 84-85 |Body fixed path angle of probe. deg | | EAPTHP 43 */
/* |____________________________________________|__________________|_______________*/
/* 86-87 |Body fixed azimuth angle of probe. deg + | EAAZIP 44 */
/* |_______________________________________________________________________________*/
/* 88-89 | Latitude of probe. deg + | B1LATP 45 */
/* |____________________________________________|__________________|_______________*/
/* 90-91 | Longitude of probe. deg | | B1LOMP 46 */
/* |____________________________________________| Body Fixed _|_______________*/
/* 92-93 | Velocity magnitude of probe relative to | Body 1 = Venus | B1VELP 47 */
/* | body km/sec | (see EN/2) | */
/* |____________________________________________|__________________|_______________*/
/* 94-95 | Body fixed path angle of probe. deg | | B1PTHP 48 */
/* |____________________________________________|__________________|_______________*/
/* 96-97 | Body fixed azimuth angle of probe. deg + | B1AZIP 49 */
/* |_______________________________________________________________|_______________*/
/* 98-100 | Earth-probe-body 1 angle, deg + | EPB1AN 50 */
/* |____________________________________________|__________________|_______________*/
/*100-101 | Earth-probe-sun angle, deg | | EPSUAN 51 */
/* |____________________________________________|_ Angle Group __|_______________*/
/*102-103 | Sun-Earth-probe angle, deg | All angles in | SEPANG 52 */
/* |____________________________________________|_ degrees __|_______________*/
/*104-105 | Earth-Sun-probe angle, deg | | ESPANG 53 */
/* |____________________________________________|__________________|_______________*/
/*106-107 | Sun-probe-body 1 angle, deg | | SPB1AN 54 */
/* |____________________________________________|__________________|_______________*/
/*108-109 | Body 1-Earth-probe angle, deg + | B1EPAN 55 */
/* |_______________________________________________________________|_______________*/
/*110-111 | Flag for periapsis (See EN/3) | PERIAP 56 */
/* |_______________________________________________________________|_______________*/
/*112-113 | X-coordinate of XROLL + + | XROLLX 57 */
/* |______________________________|_____________|__________________|_______________*/
/*114-115 | Y-coordinate of XROLL | | | XROLLY 58 */
/* |______________________________|_____________|__________________|_______________*/
/*116-117 | Z-coordinate of XROLL | | | XROLLZ 59 */
/* |______________________________|_____________|__________________|_______________*/
/*118-119 | X-coordinate of YROLL | | | YROLLX 60 */
/* |______________________________| Attitude | Spacecraft - ____|_______________*/
/*120-121 | Y-coordinate of YROLL | Data | Centered | YROLLY 61 */
/* |______________________________|_____________| Non-Rotating ____|_______________*/
/*122-123 | Z-coordinate of YROLL | | Coordinates | YROLLZ 62 */
/* |______________________________|_____________|__________________|_______________*/
/*124-125 | X-coordinate of ATT | | | ATTX 63 */
/* |______________________________|_____________|__________________|_______________*/
/*126-127 | Y-coordinate of ATT | | | ATTY 64 */
/* |______________________________|_____________|__________________|_______________*/
/*128-129 | Z-coordinate of ATT + | | ATTZ 65 */
/* |____________________________________________|__________________|_______________*/
/*130-131 | NADROL | | NADROL 66 */
/* |____________________________________________|__________________|_______________*/
/*132-133 | NADLOK | | NADLOK 67 */
/* |____________________________________________|__________________|_______________*/
/*134-135 | RAMROL | | RAMROL 68 */
/* |____________________________________________|__________________|_______________*/
/*136-137 | RAMLOK + | RAMLOK 69 */
/* ________________________________________________________________|_______________*/
/*138-153 | SPARES | 70-77 */
/* |_______________________________________________________________|_______________*/
/*154-155 |Celestial latitude of probe, deg + | DECPI 78 */
/* |____________________________________________|__________________|_______________*/
/*156-157 |Celestial longitude of probe, deg | | RAP1 79 */
/* |____________________________________________|__________________|_______________*/
/*158-159 |Flight-path angle of probe, deg | | PTHP1 80 */
/* |____________________________________________|__________________|_______________*/
/*160-161 |Azimuth angle of probe, deg | | AZP1 81 */
/* |____________________________________________|__________________|_______________*/
/*162-163 |Range rate of probe. km/sec | | DR1 82 */
/* |____________________________________________|__________________|_______________*/
/*164-165 |X-component of Earth position, km | (EC) | XE1 83 */
/* |____________________________________________|__________________|_______________*/
/*166-167 |Y-component of Earth position, km | (EC) | YE1 84 */
/* |____________________________________________|__________________|_______________*/
/*168-169 |Z-component of Earth position, km | (EC) | ZE1 85 */
/* |____________________________________________|__________________|_______________*/
/*170-171 |X-component of Earth velocity, km/sec | (EC) | DXE1 86 */
/* |____________________________________________|__________________|_______________*/
/*172-173 |Y-component of Earth velocity, km/sec | (EC) | DYE1 87 */
/* |____________________________________________|__________________|_______________*/
/*174-175 |Z-component of Earth velocity, km/sec | (EC) | DZE1 88 */
/* |____________________________________________|__________________|_______________*/
/*176-177 |Venus-to-Earth range, km | Venus Centered | RE1 89 */
/* |____________________________________________|_ Earth Mean _|_______________*/
/*178-179 |Celestial latitude of Earth direction, deg | Equinox & | DECE1 90 */
/* |____________________________________________|_ Ecliptic of _|_______________*/
/*180-181 |Celestial longitude of Earth direction, deg | 1950.0 | RAE1 91 */
/* |____________________________________________|__________________|_______________*/
/*182-183 |X-component of Sun position. km | (EC) | XS1 92 */
/* |____________________________________________|__________________|_______________*/
/*184-185 |Y-component of Sun position, km | (EC) | YS1 93 */
/* |____________________________________________|__________________|_______________*/
/*186-187 |Z-component of Sun position, km | (EC) | ZS1 94 */
/* |____________________________________________|__________________|_______________*/
/*188-189 |X-component of Sun velocity, km/sec | | DXS1 95 */
/* |____________________________________________|__________________|_______________*/
/*190-191 |Y-component of Sun velocity, km/sec | | DYS1 96 */
/* |____________________________________________|__________________|_______________*/
/*192-193 |Z-component of Sun velocity, km./sec | | DZS1 97 */
/* |____________________________________________|__________________|_______________*/
/*194-195 |Venus-to-Sun range, km | | RS1 98 */
/* |____________________________________________|__________________|_______________*/
/*196-197 |Celestial latitude of Sun direction, deg | | DESC1 99 */
/* |____________________________________________|__________________|_______________*/
/*198-199 |Celestial longitude of Sun direction. deg + | RAS1 100 */
/* |_______________________________________________________________|_______________*/
/*200-201 |Orbit semimajor axis, km + + | SMA 101 */
/* |_________________________________________|_____|_______________|_______________*/
/*202-203 |Orbit eccentricity | | | ECC 102 */
/* |_________________________________________|_____|_______________|_______________*/
/*204-205 |Time from periapsis, secs | | | TFP 103 */
/* |_________________________________________|_____|_______________|_______________*/
/*206-207 |Radius of closest approach, km | | | RCA 104 */
/* |_________________________________________|_____|_______________|_______________*/
/*208-209 |orbit period, day | | | PER 105 */
/* |_________________________________________|Conic|_______________|_______________*/
/*210-211 |Spacecraft true anomaly, deg |Group| | TA 106 */
/* |_________________________________________|_____|_______________|_______________*/
/*212-213 |Orbit inclination, deg | | Venus Centered| INCL 107 */
/* |_________________________________________|_____| Earth Mean |_______________*/
/*214-215 |Longitude of ascending node, deg | | Equinox & | LANL 108 */
/* |_________________________________________|_____| Ecliptic of |_______________*/
/*216-217 |Argument of periapsis, deg | | 1950.0 | APF1 109 */
/* |_________________________________________|_____|_______________|_______________*/
/*218-219 |X-component of unit vector to periapsis | | | PX1 110 */
/* |_________________________________________|_____|_______________|_______________*/
/*220-221 |Y-component of unit vector to periapsis | | | PY1 111 */
/* |_________________________________________|_____|_______________|_______________*/
/*222-223 |Z-component of unit vector to periapsis | | | PZ1 112 */
/* |_________________________________________|_____|_______________|_______________*/
/*224-225 |X-component of unit normal to orbit plane| | | WX1 113 */
/* |_________________________________________|_____|_______________|_______________*/
/*228-227 |Y.component of unit normal to orbit plane| | | WY1 114 */
/* |_________________________________________|_____|_______________|_______________*/
/*228-229 |Z-component of unit normal to orbit plane+ | | WZ1 115 */
/* |_______________________________________________|_______________|_______________*/
/*230-231 |Sun-Venus-probe angle, deg + | | S200P 116 */
/* |_________________________________________|Angle|_______________|_______________*/
/*232-233 |Sun-Earth-Venus angle, deg +Group| | SE200 117 */
/* |_______________________________________________|_______________|_______________*/
/*234-235 |X-component of probe position, km | | XP1 118 */
/* |_______________________________________________|_______________|_______________*/
/*236-237 |Y-component of probe position, km | | YP1 119 */
/* |_______________________________________________|_______________|_______________*/
/*238-239 |Z-component of probe position, km | | ZP1 120 */
/* |_______________________________________________|_______________|_______________*/
/*240-241 |X-component of probe velocity, km/sec | | DXP1 121 */
/* |_______________________________________________|_______________|_______________*/
/*242-243 |Y-component of probe velocity. km/sec | | DYP1 122 */
/* |_______________________________________________|_______________|_______________*/
/*244-245 |Z-component of probe velocity, km/sec + | DZP1 123 */
/* |_______________________________________________________________|_______________*/
/*248-249 |Y-component of Earth position, km + | YE1 125 */
/* |_______________________________________________|_______________|_______________*/
/*250-251 |Z-component of Earth position, km | | ZE1 126 */
/* |_______________________________________________|_______________|_______________*/
/*252-253 |X-component of Sun position, km | | XS1 127 */
/* |_______________________________________________|_______________|_______________*/
/*254-255 |Y-component of Sun position, km | | YS1 128 */
/* |_______________________________________________| Venus Centered|_______________*/
/*256-257 |Z-component of Sun position, km | Earth Mean | ZS1 129 */
/* |_______________________________________________| Equinox & |_______________*/
/*258-259 |X-component of probe position, km | Ecliptic of | XP2 130 */
/* |_______________________________________________| 1950.0 |_______________*/
/*260-261 |Y-component of probe position, km | | YP2 131 */
/* |_______________________________________________|_______________|_______________*/
/*262-263 |Z-component of probe position, km | | ZP2 132 */
/* |_______________________________________________|_______________|_______________*/
/*264-265 |X-component of probe velocity, km/sec | | DXP2 133 */
/* |_______________________________________________|_______________|_______________*/
/*266-267 |Y-component of probe velocity, km/sec | | DYP2 134 */
/* |_______________________________________________|_______________|_______________*/
/*268-269 |Z-component of probe velocity. km/sec+ + | DZP2 135 */
/* |_______________________________________________________________|_______________*/
/*270-271 |Celestial latitude of Earth-to-probe direction, deg (see EN/4) | DECP3 136 */
/* |_______________________________________________________________|_______________*/
/*272-273 |Celestial longitude of Earth-to-probe direction, deg | RAP3 137 */
/* |_______________________________________________________________|_______________*/
/*274-279 | (SPARES - Double Precision Zeros) | 138-140 */
/* |_______________________________________________________________________________*/
/* */
/* Note: The term "probe" refers to the Multiprobe or Orbiter spacecraft */
/* and not to the separated Large or Small Probes. */
/* */
/* EN/1 -- Earth true equator of date and Greenwich Meridian */
/* EN/2 -- Venus true equator of date and Prime Meridian */
/* EN/3 -- PERIAP = 0. for no closest approach, */
/* = 1 for periapsis to PCB, */
/* = 2 for apoapsis to PCB */
/* EN/4 Earth-centered, Earth mean Equinox & Ecliptic of 1950.0 */
/*
/**************************************************************************/
OBJECT = COLUMN
NAME = "YEAR OF EPHEMERIS DATA"
DATA_TYPE = "MSB INTEGER"
START_BYTE = 1
BYTES = 2
DESCRIPTION = "This object contains the four digit year in
spacecraft universal time for the PVO ephemeris data record."
END_OBJECT = COLUMN
/* Changed NOTE to DESCRIPTION throughout file. */
OBJECT = COLUMN
NAME = "DAY OF YEAR OF EPHEMERIS DATA"
DATA_TYPE = "MSB INTEGER"
START_BYTE = 3
BYTES = 2
DESCRIPTION = "This object contains the three digit day of year
in spacecraft universal time, ranging from 1 to 366, for the PVO
ephemeris data record."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "MILLISECONDS OF DAY OF EPHEMERIS DATA"
DATA_TYPE = "MSB INTEGER"
START_BYTE = 5
BYTES = 4
DESCRIPTION = "This object contains the milliseconds of the day
in spacecraft universal time, where midnight is 0.00, for the PVO
ephemeris data record."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "JULIAN DATE"
DATA_TYPE = "IBM REAL"
START_BYTE = 9
BYTES = 8
DESCRIPTION = "This object contains the Julian date, in days,
which is the elapsed days from Noon, 1 January 4713 B.C."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "GREGORIAN CALENDAR DATE"
DATA_TYPE = "IBM REAL"
START_BYTE = 17
BYTES = 8
DESCRIPTION = "This object contains the Gregorian Calendar
date as two integer words which represent the vigestimal date based
on number 20."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "ET UTC"
DATA_TYPE = "IBM REAL"
START_BYTE = 25
BYTES = 8
DESCRIPTION = "This object contains the ET-UTC, Universal Time
Co-ordinated, measured in seconds."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "RANGE RATE OF PVO GEOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 33
BYTES = 8
DESCRIPTION = "This object contains the rate by which PVO is
moving through its orbital range as seen from the Earth, measured in
kilometers per second."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VELOCITY OF PVO GEOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 41
BYTES = 8
DESCRIPTION = "This object contains the magnitude of the
velocity vector of PVO, i.e. speed of the spacecraft, as seen from
the Earth, measured in kilometers per second."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "EARTH PVO RANGE GEOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 49
BYTES = 8
DESCRIPTION = "This object contains the distance from the
Earth to the spacecraft, measured in kilometers."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SUN PVO RANGE HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 57
BYTES = 8
DESCRIPTION = "This object contains the distance from the Sun
to the PVO spacecraft, measured in kilometers."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "PVO INERTIAL VELOCITY HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 65
BYTES = 8
DESCRIPTION = "This object contains the inertial velocity of
the PVO spacecraft, measured in kilometers per second."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "PVO INERTIAL PATH ANGLE HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 73
BYTES = 8
DESCRIPTION = "This object contains the inertial path angle of
the PVO spacecraft, measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LATITUDE OF PVO HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 81
BYTES = 8
DESCRIPTION = "This object contains the celestial latitude of
the PVO spacecraft, measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LONGITUDE OF PVO HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 89
BYTES = 8
DESCRIPTION = "This object contains the celestial longitude of
the PVO spacecraft, measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LATITUDE OF EARTH HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 97
BYTES = 8
DESCRIPTION = "This object contains the celestial latitude of
the Earth, measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LONGITUDE OF EARTH HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 105
BYTES = 8
DESCRIPTION = "This object contains the celestial longitude of
the Earth, measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X OF PVO IN ECLIPTIC PLANE"
DATA_TYPE = "IBM REAL"
START_BYTE = 113
BYTES = 8
DESCRIPTION = "This object contains the X component of the PVO
spacecraft in the Sun-Earth line along the ecliptic plane of date,
measured in kilometers."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y OF PVO IN ECLIPTIC PLANE"
DATA_TYPE = "IBM REAL"
START_BYTE = 121
BYTES = 8
DESCRIPTION = "This object contains the Y component of the PVO
spacecraft in the Sun-Earth line along the ecliptic plane of date,
measured in kilometers."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z OF PVO IN ECLIPTIC PLANE"
DATA_TYPE = "IBM REAL"
START_BYTE = 129
BYTES = 8
DESCRIPTION = "This object contains the Z component of the PVO
spacecraft in the Sun-Earth line along the ecliptic plane of date,
measured in kilometers."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SUN PVO RANGE ON ECLIPTIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 137
BYTES = 8
DESCRIPTION = "This object contains the Sun-PVO distance in
the Sun-Earth X-Y plane, i.e., the projection of the Sun-PVO vector
onto the X-Y plane, measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "LONGITUDE OF PVO TO ECLIPTIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 145
BYTES = 8
DESCRIPTION = "This object contains the longitude of the PVO
spacecraft in the Sun-Earth line system, measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF PVO POSITION GEOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 153
BYTES = 8
DESCRIPTION = "This object contains the X component of geocentric
position of the PVO spacecraft, measured in kilometers, using space-fixed
FERP coordinates and the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF PVO POSITION GEOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 161
BYTES = 8
DESCRIPTION = "This object contains the Y component of geocentric
position of the PVO spacecraft, measured in kilometers, using space-fixed
FERP coordinates and the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF PVO POSITION GEOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 169
BYTES = 8
DESCRIPTION = "This object contains the Z component of geocentric
position of the PVO spacecraft, measured in kilometers, using space-fixed
FERP coordinates and the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF PVO VELOCITY GEOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 177
BYTES = 8
DESCRIPTION = "This object contains the X component of geocentric
velocity of the PVO spacecraft, measured in kilometers per second, using
space-fixed FERP coordinates and the Earth mean equinox and ecliptic of
1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF PVO VELOCITY GEOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 185
BYTES = 8
DESCRIPTION = "This object contains the Y component of geocentric
velocity of the PVO spacecraft, measured in kilometers per second, using
space-fixed FERP coordinates and the Earth mean equinox and ecliptic of
1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF PVO VELOCITY GEOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 193
BYTES = 8
DESCRIPTION = "This object contains the Z component of geocentric
velocity of the PVO spacecraft, measured in kilometers per second, using
space-fixed FERP coordinates and the Earth mean equinox and ecliptic of
1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF PVO POSITION HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 201
BYTES = 8
DESCRIPTION = "This object contains the X component of heliocentric
position of the PVO spacecraft, measured in kilometers, using space-fixed
FERP coordinates and the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF PVO POSITION HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 209
BYTES = 8
DESCRIPTION = "This object contains the Y component of heliocentric
position of the PVO spacecraft, measured in kilometers, using space-fixed
FERP coordinates and the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF PVO POSITION HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 217
BYTES = 8
DESCRIPTION = "This object contains the Z component of heliocentric
position of the PVO spacecraft, measured in kilometers, using space-fixed
FERP coordinates and the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF PVO VELOCITY HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 225
BYTES = 8
DESCRIPTION = "This object contains the X component of heliocentric
velocity of the PVO spacecraft, measured in kilometers per second, using
space-fixed FERP coordinates and the Earth mean equinox and ecliptic of
1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF PVO VELOCITY HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 233
BYTES = 8
DESCRIPTION = "This object contains the Y component of heliocentric
velocity of the PVO spacecraft, measured in kilometers per second, using
space-fixed FERP coordinates and the Earth mean equinox and ecliptic of
1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF PVO VELOCITY HELIOCENTRIC"
DATA_TYPE = "IBM REAL"
START_BYTE = 241
BYTES = 8
DESCRIPTION = "This object contains the Z component of heliocentric
velocity of the PVO spacecraft, measured in kilometers per second, using
space-fixed FERP coordinates and the Earth mean equinox and ecliptic of
1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF PVO POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 249
BYTES = 8
DESCRIPTION = "This object contains the X component of the Venus
centered position of the PVO spacecraft, measured in kilometers, using
space-fixed FERP coordinates and the Earth mean equinox and ecliptic of
1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF PVO POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 257
BYTES = 8
DESCRIPTION = "This object contains the Y component of the Venus
centered position of the PVO spacecraft, measured in kilometers, using
space-fixed FERP coordinates and the Earth mean equinox and ecliptic of
1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF PVO POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 265
BYTES = 8
DESCRIPTION = "This object contains the Z component of the Venus
centered position of the PVO spacecraft, measured in kilometers, using
space-fixed FERP coordinates and the Earth mean equinox and ecliptic of
1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF PVO VELOCITY VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 273
BYTES = 8
DESCRIPTION = "This object contains the X component of the Venus
centered velocity of the PVO spacecraft, measured in kilometers per second,
using space-fixed FERP coordinates and the Earth mean equinox and ecliptic
of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF PVO VELOCITY VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 281
BYTES = 8
DESCRIPTION = "This object contains the Y component of the Venus
centered velocity of the PVO spacecraft, measured in kilometers per second,
using space-fixed FERP coordinates and the Earth mean equinox and ecliptic
of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF PVO VELOCITY VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 289
BYTES = 8
DESCRIPTION = "This object contains the Z component of the Venus
centered velocity of the PVO spacecraft, measured in kilometers per second,
using space-fixed FERP coordinates and the Earth mean equinox and ecliptic
of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VENUS PVO RANGE"
DATA_TYPE = "IBM REAL"
START_BYTE = 297
BYTES = 8
DESCRIPTION = "This object contains the distance from Venus to
the spacecraft, measured in kilometers, using space-fixed FERP coordinates
and the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VELOCITY OF PVO VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 305
BYTES = 8
DESCRIPTION = "This object contains the magnitude of the
velocity vector of PVO, i.e. speed of the spacecraft, as seen from
Venus, measured in kilometers per second, using space-fixed FERP
coordinates and the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "EARTH FIXED LATITUDE OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 313
BYTES = 8
DESCRIPTION = "This object contains the latitude of the PVO
spacecraft, measured in degrees, using a Body Fixed Earth of Earth true
equator of date and Greenwich Meridian."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "EARTH FIXED LONGITUDE OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 321
BYTES = 8
DESCRIPTION = "This object contains the longitude of the PVO
spacecraft, measured in degrees, using a Body Fixed Earth of Earth true
equator of date and Greenwich Meridian."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VELOCITY OF PVO RELATIVE TO FIXED EARTH"
DATA_TYPE = "IBM REAL"
START_BYTE = 329
BYTES = 8
DESCRIPTION = "This object contains the velocity of the PVO
spacecraft relative to Earth, measured in kilometers per second, using
a Body Fixed Earth of Earth true equator of date and Greenwich Meridian."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "EARTH FIXED PATH ANGLE OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 337
BYTES = 8
DESCRIPTION = "This object contains the path angle of the PVO
spacecraft, measured in degrees, using a Body Fixed Earth of Earth true
equator of date and Greenwich Meridian."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "EARTH FIXED AZIMUTH ANGLE OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 345
BYTES = 8
DESCRIPTION = "This object contains the azimuth angle of the PVO
spacecraft, measured in degrees, using a Body Fixed Earth of Earth true
equator of date and Greenwich Meridian."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VENUS FIXED LATITUDE OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 353
BYTES = 8
DESCRIPTION = "This object contains the latitude of the PVO
spacecraft, measured in degrees, using a Body Fixed Venus of Venus true
equator of date and Prime Meridian."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VENUS FIXED LONGITUDE OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 361
BYTES = 8
DESCRIPTION = "This object contains the longitude of the PVO
spacecraft, measured in degrees, using a Body Fixed Venus of Venus true
equator of date and Prime Meridian."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VELOCITY OF PVO RELATIVE TO FIXED VENUS"
DATA_TYPE = "IBM REAL"
START_BYTE = 369
BYTES = 8
DESCRIPTION = "This object contains the velocity of the PVO
spacecraft relative to Venus, measured in kilometers per second, using
a Body Fixed Venus of Venus true equator of date and Prime Meridian."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VENUS FIXED PATH ANGLE OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 377
BYTES = 8
DESCRIPTION = "This object contains the path angle of the PVO
spacecraft, measured in degrees, using a Body Fixed Venus of Venus true
equator of date and Prime Meridian."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VENUS FIXED AZIMUTH ANGLE OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 385
BYTES = 8
DESCRIPTION = "This object contains the azimuth angle of the PVO
spacecraft, measured in degrees, using a Body Fixed Venus of Venus true
equator of date and Prime Meridian."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "EARTH PVO VENUS ANGLE"
DATA_TYPE = "IBM REAL"
START_BYTE = 393
BYTES = 8
DESCRIPTION = "This object contains the Earth-PVO-Venus angle,
measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "EARTH PVO SUN ANGLE"
DATA_TYPE = "IBM REAL"
START_BYTE = 401
BYTES = 8
DESCRIPTION = "This object contains the Earth-PVO-Sun angle,
measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SUN EARTH PVO ANGLE"
DATA_TYPE = "IBM REAL"
START_BYTE = 409
BYTES = 8
DESCRIPTION = "This object contains the Sun-Earth-PVO angle,
measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "EARTH SUN PVO ANGLE"
DATA_TYPE = "IBM REAL"
START_BYTE = 417
BYTES = 8
DESCRIPTION = "This object contains the Earth-Sun-PVO angle,
measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SUN PVO VENUS ANGLE"
DATA_TYPE = "IBM REAL"
START_BYTE = 425
BYTES = 8
DESCRIPTION = "This object contains the Sun-PVO-Venus angle,
measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VENUS EARTH PVO ANGLE"
DATA_TYPE = "IBM REAL"
START_BYTE = 433
BYTES = 8
DESCRIPTION = "This object contains the Venus-Earth-PVO angle,
measured in degrees."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "FLAG FOR PERIAPSIS"
DATA_TYPE = "IBM REAL"
START_BYTE = 441
BYTES = 8
DESCRIPTION = "This object contains a non-zero value to identify
the present record as a periapsis or apoapsis event, typically at a
non-standard record time. The possible values are: 0=no closest
approach, 1=periapsis to PCB and 2=apoapsis to PCB."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COORDINATE OF X AXIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 449
BYTES = 8
DESCRIPTION = "This object contains the X coordinate of the
position of the X-axis of the PVO spacecraft, in spacecraft centered
non-rotating coordinates, using the Earth mean equinox and ecliptic
of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COORDINATE OF X AXIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 457
BYTES = 8
DESCRIPTION = "This object contains the Y coordinate of the
position of the X-axis of the PVO spacecraft, in spacecraft centered
non-rotating coordinates, using the Earth mean equinox and ecliptic
of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COORDINATE OF X AXIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 465
BYTES = 8
DESCRIPTION = "This object contains the Z coordinate of the
position of the X-axis of the PVO spacecraft, in spacecraft centered
non-rotating coordinates, using the Earth mean equinox and ecliptic
of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COORDINATE OF Y AXIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 473
BYTES = 8
DESCRIPTION = "This object contains the X coordinate of the
position of the Y-axis of the PVO spacecraft, in spacecraft centered
non-rotating coordinates, using the Earth mean equinox and ecliptic
of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COORDINATE OF Y AXIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 481
BYTES = 8
DESCRIPTION = "This object contains the Y coordinate of the
position of the Y-axis of the PVO spacecraft, in spacecraft centered
non-rotating coordinates, using the Earth mean equinox and ecliptic
of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COORDINATE OF Y AXIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 489
BYTES = 8
DESCRIPTION = "This object contains the Z coordinate of the
position of the Y-axis of the PVO spacecraft, in spacecraft centered
non-rotating coordinates, using the Earth mean equinox and ecliptic
of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COORDINATE OF Z AXIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 497
BYTES = 8
DESCRIPTION = "This object contains the X coordinate of the
position of the Z-axis (spin axis) of the PVO spacecraft, in spacecraft
centered non-rotating coordinates, using the Earth mean equinox and
ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COORDINATE OF Z AXIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 505
BYTES = 8
DESCRIPTION = "This object contains the Y coordinate of the
position of the Z-axis (spin axis) of the PVO spacecraft, in spacecraft
centered non-rotating coordinates, using the Earth mean equinox and
ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COORDINATE OF Z AXIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 513
BYTES = 8
DESCRIPTION = "This object contains the Z coordinate of the
position of the Z-axis (spin axis) of the PVO spacecraft, in spacecraft
centered non-rotating coordinates, using the Earth mean equinox and
ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "NADROL COMPONENT OF NADIR DATA"
DATA_TYPE = "IBM REAL"
START_BYTE = 521
BYTES = 8
DESCRIPTION = "This object contains the NADROL component of
the NADIR data."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "NADLOK COMPONENT OF NADIR DATA"
DATA_TYPE = "IBM REAL"
START_BYTE = 529
BYTES = 8
DESCRIPTION = "This object contains the NADLOK component of
the NADIR data."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "RAMROL COMPONENT OF RAM DATA"
DATA_TYPE = "IBM REAL"
START_BYTE = 537
BYTES = 8
DESCRIPTION = "This object contains the RAMROL component of
the RAM data."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "RAMLOK COMPONENT OF RAM DATA"
DATA_TYPE = "IBM REAL"
START_BYTE = 545
BYTES = 8
DESCRIPTION = "This object contains the RAMLOK component of
the RAM data."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE1"
DATA_TYPE = "IBM REAL"
START_BYTE = 553
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE2"
DATA_TYPE = "IBM REAL"
START_BYTE = 561
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE3"
DATA_TYPE = "IBM REAL"
START_BYTE = 569
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE4"
DATA_TYPE = "IBM REAL"
START_BYTE = 577
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE5"
DATA_TYPE = "IBM REAL"
START_BYTE = 585
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE6"
DATA_TYPE = "IBM REAL"
START_BYTE = 593
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE7"
DATA_TYPE = "IBM REAL"
START_BYTE = 601
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE8"
DATA_TYPE = "IBM REAL"
START_BYTE = 609
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LATITUDE OF PVO VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 617
BYTES = 8
DESCRIPTION = "This object contains the celestial latitude of
the PVO spacecraft, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LONGITUDE OF PVO VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 625
BYTES = 8
DESCRIPTION = "This object contains the celestial longitude of
the PVO spacecraft, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "FLIGHT PATH ANGLE OF PVO VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 633
BYTES = 8
DESCRIPTION = "This object contains the flight-path angle of
the PVO spacecraft, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "AZIMUTH ANGLE OF PVO VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 641
BYTES = 8
DESCRIPTION = "This object contains the azimuth angle of the
PVO spacecraft, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "RANGE RATE OF PVO VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 649
BYTES = 8
DESCRIPTION = "This object contains the range rate of the
PVO spacecraft, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF EARTH POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 657
BYTES = 8
DESCRIPTION = "This object contains the X component of the
Earth's position, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF EARTH POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 665
BYTES = 8
DESCRIPTION = "This object contains the Y component of the
Earth's position, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF EARTH POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 673
BYTES = 8
DESCRIPTION = "This object contains the Z component of the
Earth's position, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF EARTH VELOCITY VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 681
BYTES = 8
DESCRIPTION = "This object contains the X component of the
Earth's velocity, measured in kilometers per second, in venus-centered
coordinates, using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF EARTH VELOCITY VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 689
BYTES = 8
DESCRIPTION = "This object contains the Y component of the
Earth's velocity, measured in kilometers per second, in venus-centered
coordinates, using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF EARTH VELOCITY VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 697
BYTES = 8
DESCRIPTION = "This object contains the Z component of the
Earth's velocity, measured in kilometers per second, in venus-centered
coordinates, using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VENUS TO EARTH RANGE VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 705
BYTES = 8
DESCRIPTION = "This object contains the Venus-to-Earth range,
measured in kilometers , in venus-centered coordinates, using the Earth
mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LATITUDE OF EARTH DIR VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 713
BYTES = 8
DESCRIPTION = "This object contains the celestial latitude of the
Earth direction, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LONGITUDE OF EARTH DIR VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 721
BYTES = 8
DESCRIPTION = "This object contains the celestial longitude of the
Earth direction, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF SUN POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 729
BYTES = 8
DESCRIPTION = "This object contains the X component of the
Sun's position, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF SUN POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 737
BYTES = 8
DESCRIPTION = "This object contains the Y component of the
Sun's position, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF SUN POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 745
BYTES = 8
DESCRIPTION = "This object contains the Z component of the
Sun's position, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF SUN VELOCITY VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 753
BYTES = 8
DESCRIPTION = "This object contains the X component of the
Sun's velocity, measured in kilometers per second, in venus-centered
coordinates, using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF SUN VELOCITY VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 761
BYTES = 8
DESCRIPTION = "This object contains the Y component of the
Sun's velocity, measured in kilometers per second, in venus-centered
coordinates, using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF SUN VELOCITY VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 769
BYTES = 8
DESCRIPTION = "This object contains the Z component of the
Sun's velocity, measured in kilometers per second, in venus-centered
coordinates, using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "VENUS TO SUN RANGE VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 777
BYTES = 8
DESCRIPTION = "This object contains the Venus-to-Sun range,
measured in kilometers , in venus-centered coordinates, using the Earth
mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LATITUDE OF SUN DIR VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 785
BYTES = 8
DESCRIPTION = "This object contains the celestial latitude of
the Sun direction, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LONGITUDE OF SUN DIR VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 793
BYTES = 8
DESCRIPTION = "This object contains the celestial longitude of
the Sun direction, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "ORBIT SEMIMAJOR AXIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 801
BYTES = 8
DESCRIPTION = "This object contains the orbit semimajor axis of
the PVO spacecraft, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "ORBIT ECCENTRICITY OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 809
BYTES = 8
DESCRIPTION = "This object contains the orbit eccentricity of
the PVO spacecraft, in venus-centered coordinates, using the Earth mean
equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "TIME FROM PERIAPSIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 817
BYTES = 8
DESCRIPTION = "This object contains the time from periapsis of
the PVO spacecraft, measured in seconds, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "RADIUS OF CLOSEST APPROACH OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 825
BYTES = 8
DESCRIPTION = "This object contains the radius of closest approach of
the PVO spacecraft, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "ORBIT PERIOD OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 833
BYTES = 8
DESCRIPTION = "This object contains the orbit period of the
PVO spacecraft, measured in days, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPACECRAFT TRUE ANOMALY OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 841
BYTES = 8
DESCRIPTION = "This object contains the spacecraft true anomaly of
the PVO spacecraft, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "ORBIT INCLINATION OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 849
BYTES = 8
DESCRIPTION = "This object contains the orbit inclination of the
PVO spacecraft, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "LONGITUDE OF ASCENDING NODE OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 857
BYTES = 8
DESCRIPTION = "This object contains the longitude of the ascending
node of the PVO spacecraft, measured in degrees, in venus-centered
coordinates, using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "ARGUMENT OF PERIAPSIS OF PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 865
BYTES = 8
DESCRIPTION = "This object contains the argument of periapsis of
the PVO spacecraft, measured in degrees, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF UNIT VECTOR TO PERIAPSIS PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 873
BYTES = 8
DESCRIPTION = "This object contains the X component of the unit
vector to periapsis of the PVO spacecraft, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF UNIT VECTOR TO PERIAPSIS PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 881
BYTES = 8
DESCRIPTION = "This object contains the Y component of the unit
vector to periapsis of the PVO spacecraft, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF UNIT VECTOR TO PERIAPSIS PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 889
BYTES = 8
DESCRIPTION = "This object contains the Z component of the unit
vector to periapsis of the PVO spacecraft, in venus-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF UNIT NORMAL TO ORBITAL PLANE PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 897
BYTES = 8
DESCRIPTION = "This object contains the X component of the unit
normal to the orbit plane of the PVO spacecraft, in venus-centered
coordinates, using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF UNIT NORMAL TO ORBITAL PLANE PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 905
BYTES = 8
DESCRIPTION = "This object contains the Y component of the unit
normal to the orbit plane of the PVO spacecraft, in venus-centered
coordinates, using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF UNIT NORMAL TO ORBITAL PLANE PVO"
DATA_TYPE = "IBM REAL"
START_BYTE = 913
BYTES = 8
DESCRIPTION = "This object contains the Z component of the unit
normal to the orbit plane of the PVO spacecraft, in venus-centered
coordinates, using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SUN VENUS PVO ANGLE"
DATA_TYPE = "IBM REAL"
START_BYTE = 921
BYTES = 8
DESCRIPTION = "This object contains the Sun-Venus-PVO angle,
measured in degrees, in venus-centered coordinates, using the Earth
mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SUN EARTH VENUS ANGLE"
DATA_TYPE = "IBM REAL"
START_BYTE = 929
BYTES = 8
DESCRIPTION = "This object contains the Sun_Earth-Venus angle,
measured in degrees, in venus-centered coordinates, using the Earth
mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT PVO POSITION VENUS CENTERED EARTH EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 937
BYTES = 8
DESCRIPTION = "This object contains the X component of the position
of the PVO spacecraft, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT PVO POSITION VENUS CENTERED EARTH EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 945
BYTES = 8
DESCRIPTION = "This object contains the Y component of the position
of the PVO spacecraft, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT PVO POSITION VENUS CENTERED EARTH EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 953
BYTES = 8
DESCRIPTION = "This object contains the Z component of the position
of the PVO spacecraft, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT PVO VELOCITY VENUS CENTERED EARTH EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 961
BYTES = 8
DESCRIPTION = "This object contains the X component of the velocity
of the PVO spacecraft, measured in kilometers per second, in venus-centered
coordinates, using the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT PVO VELOCITY VENUS CENTERED EARTH EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 969
BYTES = 8
DESCRIPTION = "This object contains the Y component of the velocity
of the PVO spacecraft, measured in kilometers per second, in venus-centered
coordinates, using the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT PVO VELOCITY VENUS CENTERED EARTH EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 977
BYTES = 8
DESCRIPTION = "This object contains the Z component of the velocity
of the PVO spacecraft, measured in kilometers per second, in venus-centered
coordinates, using the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT EARTH POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 985
BYTES = 8
DESCRIPTION = "This object contains the X component of the position
of the Earth, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF EARTH POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 993
BYTES = 8
DESCRIPTION = "This object contains the Y component of the position
of the Earth, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF EARTH POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 1001
BYTES = 8
DESCRIPTION = "This object contains the Z component of the position
of the Earth, measured in kilometers, in venus-centered coordinates,
using the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT OF SUN POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 1009
BYTES = 8
DESCRIPTION = "This object contains the X component of the position
of the Sun, measured in kilometers, in venus-centered coordinates, using
the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT OF SUN POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 1017
BYTES = 8
DESCRIPTION = "This object contains the Y component of the position
of the Sun, measured in kilometers, in venus-centered coordinates, using
the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT OF SUN POSITION VENUS CENTERED"
DATA_TYPE = "IBM REAL"
START_BYTE = 1025
BYTES = 8
DESCRIPTION = "This object contains the Z component of the position
of the Sun, measured in kilometers, in venus-centered coordinates, using
the Earth mean equinox and Earth equator of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT PVO POSITION VENUS CENTERED VENUS EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 1033
BYTES = 8
DESCRIPTION = "This object contains the X component of the position
of the PVO spacecraft, measured in kilometers, in venus-centered coordinates,
using the Venus mean equinox and Venus orbit of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT PVO POSITION VENUS CENTERED VENUS EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 1041
BYTES = 8
DESCRIPTION = "This object contains the Y component of the position
of the PVO spacecraft, measured in kilometers, in venus-centered coordinates,
using the Venus mean equinox and Venus orbit of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT PVO POSITION VENUS CENTERED VENUS EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 1049
BYTES = 8
DESCRIPTION = "This object contains the Z component of the position
of the PVO spacecraft, measured in kilometers, in venus-centered coordinates,
using the Venus mean equinox and Venus orbit of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "X COMPONENT PVO VELOCITY VENUS CENTERED VENUS EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 1057
BYTES = 8
DESCRIPTION = "This object contains the X component of the velocity
of the PVO spacecraft, measured in kilometers per second, in venus-centered
coordinates, using the Venus mean equinox and Venus orbit of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Y COMPONENT PVO VELOCITY VENUS CENTERED VENUS EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 1065
BYTES = 8
DESCRIPTION = "This object contains the Y component of the velocity
of the PVO spacecraft, measured in kilometers per second, in venus-centered
coordinates, using the Venus mean equinox and Venus orbit of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "Z COMPONENT PVO VELOCITY VENUS CENTERED VENUS EQUINOX"
DATA_TYPE = "IBM REAL"
START_BYTE = 1073
BYTES = 8
DESCRIPTION = "This object contains the Z component of the velocity
of the PVO spacecraft, measured in kilometers per second, in venus-centered
coordinates, using the Venus mean equinox and Venus orbit of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LATITUDE OF EARTH TO PVO DIRECTION"
DATA_TYPE = "IBM REAL"
START_BYTE = 1081
BYTES = 8
DESCRIPTION = "This object contains the celestial latitude of the
Earth-to-PVO direction, measured in degrees, in Earth-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "CELESTIAL LONGITUDE OF EARTH TO PVO DIRECTION"
DATA_TYPE = "IBM REAL"
START_BYTE = 1089
BYTES = 8
DESCRIPTION = "This object contains the celestial longitude of the
Earth-to-PVO direction, measured in degrees, in Earth-centered coordinates,
using the Earth mean equinox and ecliptic of 1950.0."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE9"
DATA_TYPE = "IBM REAL"
START_BYTE = 1097
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE10"
DATA_TYPE = "IBM REAL"
START_BYTE = 1105
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE11"
DATA_TYPE = "IBM REAL"
START_BYTE = 1113
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE12"
DATA_TYPE = "IBM REAL"
START_BYTE = 1121
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
OBJECT = COLUMN
NAME = "SPARE13"
DATA_TYPE = "IBM REAL"
START_BYTE = 1129
BYTES = 8
DESCRIPTION = "This object contains a spare (empty) value."
END_OBJECT = COLUMN
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