CCSD3ZF0000100000001NJPL3KS0PDSX##mark## /* File information */ PDS_VERSION_ID = "PDS3" FILE_NAME = "L06888.001" RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 202 FILE_RECORDS = 303 LABEL_RECORDS = 151 ^LOSAPDR_HEADER_TABLE = 152 ^LOSAPDR_TIMES_TABLE = 158 ^LOSAPDR_RESULTS_TABLE = 165 SPACECRAFT_NAME = "MAGELLAN" TARGET_NAME = "VENUS" INSTRUMENT_NAME = "RADIO SCIENCE SUBSYSTEM" DATA_SET_ID = "MGN-V-RSS-5-LOSAPDR-L2-V1.13" PRODUCT_ID = "RS-L06888.001" DESCRIPTION = "The LOSAPDR (Line of Sight Acceleration Profile Data Record) is a set of three tables represented in ASCII character format which summarize the analysis of radio tracking data of orbiting planetary spacecraft (specifically, Magellan or Mars Observer). The first table identifies input parameters and conditions; the second table gives times between which spline fits to data points are valid; and the third table gives times, Doppler residuals, spline fit residuals, and inferred values of spacecraft acceleration with respect to the nominal gravity field (MGN120PSAAP) and orbit. The LOSAPDR is produced at the Jet Propulsion Laboratory under the supervision of W.L. Sjogren." SOFTWARE_NAME = "LOSRES.1996.4.1 " START_TIME = 1993-02-15T05:49:20.355 STOP_TIME = 1993-02-15T05:54:04.355 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" PRODUCER_ID = "MGN GRAVSCI TEAM" PRODUCT_CREATION_TIME = 1996-06-12T17:34:40.000 PRODUCT_RELEASE_DATE = 1994-04-15 /* Structure Objects */ OBJECT = LOSAPDR_HEADER_TABLE ROWS = 1 COLUMNS = 42 ROW_BYTES = 1030 ROW_SUFFIX_BYTES = 182 INTERCHANGE_FORMAT = ASCII DESCRIPTION = "The LOSAPDR header includes input data and summary results from initial ODP and LUNRES calculations. It is a single-row table with 42 columns, two of which have three elements each. The data are represented as ASCII characters; entries are delimited by commas. The total of the data plus delimiters is 1030 characters, followed by 180 padding characters and a carriage-return line-feed pair. The row thus has 1212 characters, which is exactly six times the value of RECORD_BYTES." OBJECT = COLUMN NAME = "PLANETARY RADIUS" DATA_TYPE = ASCII_REAL START_BYTE = 1 BYTES = 23 FORMAT = "E23.16" UNIT = "KILOMETER" DESCRIPTION = "The assumed radius of the spherical planet (program mnemonic RADIUS)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "GM" DATA_TYPE = ASCII_REAL START_BYTE = 25 BYTES = 23 FORMAT = "E23.16" UNIT = "KILOMETERS CUBED PER SECOND SQUARED" DESCRIPTION = "The assumed gravitational constant for the planet." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "CALENDAR EPOCH" DATA_TYPE = TIME START_BYTE = 49 BYTES = 23 UNIT = "N/A" DESCRIPTION = "The calendar epoch in ephemeris time of the initial state vector at the spacecraft. The initial state vector is given by SPACECRAFT POSITION and SPACECRAFT VELOCITY below. (program mnemonic CEPOCH)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "JULIAN EPHEMERIS DAYS" DATA_TYPE = ASCII_REAL START_BYTE = 73 BYTES = 23 FORMAT = "E23.16" UNIT = "DAY" DESCRIPTION = "The Julian date corresponding to CEPOCH (ephemeris time at the space- craft) (program mnemonic JED)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "SPACECRAFT POSITION" ITEMS = 3 ITEM_BYTES = 23 ITEM_OFFSET = 24 DATA_TYPE = ASCII_REAL START_BYTE = 97 BYTES = 71 FORMAT = "E23.16" UNIT = "KILOMETER" DESCRIPTION = "The spacecraft position vector at CEPOCH, calculated in program ODP (program mnemonics XS, YS, and ZS)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "SPACECRAFT VELOCITY" ITEMS = 3 ITEM_BYTES = 23 ITEM_OFFSET = 24 DATA_TYPE = ASCII_REAL START_BYTE = 169 BYTES = 71 FORMAT = "E23.16" UNIT = "KILOMETER PER SECOND" DESCRIPTION = "The spacecraft velocity vector at CEPOCH, calculated in program ODP (program mnemonics DXS, DYS, and DZS)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "SPACECRAFT LONGITUDE" POSITIVE_LONGITUDE_DIRECTION = "EAST" DATA_TYPE = ASCII_REAL START_BYTE = 241 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Planetocentric longitude of the spacecraft corresponding to SPACECRAFT POSITION at CEPOCH (program mnemonic LONEP)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "SPACECRAFT HOUR ANGLE" DATA_TYPE = ASCII_REAL START_BYTE = 265 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "The hour angle of the spacecraft corresponding to SPACECRAFT POSITION at CEPOCH (program mnemonic HANG)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "DOBKS" DATA_TYPE = ASCII_INTEGER START_BYTE = 289 BYTES = 2 FORMAT = "I2" UNIT = "N/A" DESCRIPTION = "Flag for constant (-1) or variable (+1) time spacing in spline fits. If DOBKS=+1, the time intervals in BKTIMX will be unequal." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "RECORD SPACING" DATA_TYPE = ASCII_REAL START_BYTE = 292 BYTES = 23 FORMAT = "E23.16" UNIT = "MINUTE" DESCRIPTION = "Time spacing of the output records in the RESULTS_TABLE (program mnemonic DTACC). Large values may mean that spacing defaults to the spacing of the data points (no interpolated data)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "MINBKS" DATA_TYPE = ASCII_INTEGER START_BYTE = 316 BYTES = 10 FORMAT = "I10" UNIT = "N/A" DESCRIPTION = "Minimum number of data points in each spline interval (used only if DOBKS=+1)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "MAXBKS" DATA_TYPE = ASCII_INTEGER START_BYTE = 327 BYTES = 10 FORMAT = "I10" UNIT = "N/A" DESCRIPTION = "Maximum number of data points in each spline interval (used only if DOBKS=+1)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "BAND" DATA_TYPE = ASCII_REAL START_BYTE = 338 BYTES = 23 FORMAT = "E23.16" UNIT = "MILLIMETER PER SECOND" DESCRIPTION = "Conversion factor from Doppler to acceleration. Nominally 0.2955 for X-band data and 1.0833 for S-band data." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "TADD" DATA_TYPE = ASCII_REAL START_BYTE = 362 BYTES = 23 FORMAT = "E23.16" UNIT = "MINUTE" DESCRIPTION = "Time from CEPOCH to first data point (at the spacecraft)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "TFIT" DATA_TYPE = ASCII_REAL START_BYTE = 386 BYTES = 23 FORMAT = "E23.16" UNIT = "MINUTE" DESCRIPTION = "Time from TADD to last data point (at the spacecraft)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "DFIT" DATA_TYPE = ASCII_REAL START_BYTE = 410 BYTES = 23 FORMAT = "E23.16" UNIT = "MINUTE" DESCRIPTION = "Length of each spline interval (used only when DOBKS=-1)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "REJECT" DATA_TYPE = ASCII_REAL START_BYTE = 434 BYTES = 23 FORMAT = "E23.16" UNIT = "HERTZ" DESCRIPTION = "Threshold for rejection of bad data points." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "EARTH LONGITUDE" POSITIVE_LONGITUDE_DIRECTION = "EAST" DATA_TYPE = ASCII_REAL START_BYTE = 458 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Planetocentric longitude of Earth at CEPOCH (program mnemonic LNE)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "EARTH LATITUDE" DATA_TYPE = ASCII_REAL START_BYTE = 482 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Planetocentric north latitude of Earth at CEPOCH (program mnemonic LTE)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "TRANSA" DATA_TYPE = ASCII_REAL START_BYTE = 506 BYTES = 23 FORMAT = "E23.16" UNIT = "SECOND" DESCRIPTION = "One-way downlink light- time for a photon leaving the spacecraft at CEPOCH." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "TRANSB" DATA_TYPE = ASCII_REAL START_BYTE = 530 BYTES = 23 FORMAT = "E23.16" UNIT = "SECOND PER SECOND" DESCRIPTION = "Rate of change of TRANSA" END_OBJECT = COLUMN OBJECT = COLUMN NAME = "DUTSEC" DATA_TYPE = ASCII_REAL START_BYTE = 554 BYTES = 23 FORMAT = "E23.16" UNIT = "SECOND" DESCRIPTION = "Difference between ephemeris time (ET) and universal time (UT)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "REFEP" DATA_TYPE = TIME START_BYTE = 578 BYTES = 23 UNIT = "N/A" DESCRIPTION = "Reference epoch for TRANSA and TRANSB at the spacecraft (same time system, and often the same value, as CEPOCH)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ORBITAL SEMIMAJOR AXIS" DATA_TYPE = ASCII_REAL START_BYTE = 602 BYTES = 23 FORMAT = "E23.16" UNIT = "KILOMETER" DESCRIPTION = "Semi-major axis of spacecraft orbit. Obtained in the orbit solution of program ODP (program mnemonic SMA)" END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ORBITAL ECCENTRICITY" DATA_TYPE = ASCII_REAL START_BYTE = 626 BYTES = 23 FORMAT = "E23.16" UNIT = "DIMENSIONLESS" DESCRIPTION = "Eccentricity of spacecraft orbit. Obtained in the orbit solution of program ODP (program mnemonic ECC)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ORBITAL INCLINATION" DATA_TYPE = ASCII_REAL START_BYTE = 650 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Inclination of spacecraft orbit. Obtained in the orbit solution of program ODP (program mnemonic INC)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ASCENDING NODE LONGITUDE" DATA_TYPE = ASCII_REAL START_BYTE = 674 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Ascending node of spacecraft orbit. Obtained in the orbit solution of program ODP (program mnemonic NODE)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "PERIAPSIS ARGUMENT ANGLE" DATA_TYPE = ASCII_REAL START_BYTE = 698 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Argument of periapsis for spacecraft orbit. Obtained in the orbit solution of program ODP (program mnemonic ARG)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "TRUE ANOMALY ANGLE" DATA_TYPE = ASCII_REAL START_BYTE = 722 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "True anomaly of spacecraft orbit. Obtained in the orbit solution of program ODP (program mnemonic F)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "MEAN ANOMALY ANGLE" DATA_TYPE = ASCII_REAL START_BYTE = 746 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Mean anomaly of spacecraft orbit. Obtained in the orbit solution of program ODP (program mnemonic M)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ECCENTRIC ANOMALY ANGLE" DATA_TYPE = ASCII_REAL START_BYTE = 770 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Eccentric anomaly of spacecraft orbit. Obtained in the orbit solution of program ODP (program mnemonic E)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ORBITAL PERIOD" DATA_TYPE = ASCII_REAL START_BYTE = 794 BYTES = 23 FORMAT = "E23.16" UNIT = "HOUR" DESCRIPTION = "Period of spacecraft orbit. Obtained in the orbit solution of program ODP (program mnemonic P)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "PERIAPSIS LATITUDE" DATA_TYPE = ASCII_REAL START_BYTE = 818 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Planetocentric north latitude at periapsis for spacecraft orbit (program mnemonic LATPER)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "PERIAPSIS LONGITUDE" POSITIVE_LONGITUDE_DIRECTION = "EAST" DATA_TYPE = ASCII_REAL START_BYTE = 842 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Planetocentric longitude of periapsis for spacecraft orbit (program mnemonic LONPER)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "PERIAPSIS RADIUS" DATA_TYPE = ASCII_REAL START_BYTE = 866 BYTES = 23 FORMAT = "E23.16" UNIT = "KILOMETER" DESCRIPTION = "Spacecraft distance from target center of mass at periapsis (program mnemonic RPER)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "PERIAPSIS VELOCITY" DATA_TYPE = ASCII_REAL START_BYTE = 890 BYTES = 23 FORMAT = "E23.16" UNIT = "KILOMETER PER SECOND" DESCRIPTION = "Spacecraft velocity at peripasis (program mnemonic VPER)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "PERIAPSIS ALTITUDE" DATA_TYPE = ASCII_REAL START_BYTE = 914 BYTES = 23 FORMAT = "E23.16" UNIT = "KILOMETER" DESCRIPTION = "Spacecraft altitude over reference surface at periapsis (program mnemonic APER)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "APOAPSIS RADIUS" DATA_TYPE = ASCII_REAL START_BYTE = 938 BYTES = 23 FORMAT = "E23.16" UNIT = "KILOMETER" DESCRIPTION = "Spacecraft distance from target center of mass at apoapsis (program mnemonic RAPO)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "APOAPSIS VELOCITY" DATA_TYPE = ASCII_REAL START_BYTE = 962 BYTES = 23 FORMAT = "E23.16" UNIT = "KILOMETER PER SECOND" DESCRIPTION = "Spacecraft velocity at apoapsis (program mnemonic VAPO)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "APOAPSIS ALTITUDE" DATA_TYPE = ASCII_REAL START_BYTE = 986 BYTES = 23 FORMAT = "E23.16" UNIT = "KILOMETER" DESCRIPTION = "Spacecraft altitude over reference surface at apoapsis (program mnemonic AAPO)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "NBKS" DATA_TYPE = ASCII_INTEGER START_BYTE = 1010 BYTES = 10 FORMAT = "I10" UNIT = "N/A" DESCRIPTION = "Number of times in the Times Table defining spline intervals." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "NPOINT" DATA_TYPE = ASCII_INTEGER START_BYTE = 1021 BYTES = 10 FORMAT = "I10" UNIT = "N/A" DESCRIPTION = "Number of data points used to make this file." END_OBJECT = COLUMN END_OBJECT = LOSAPDR_HEADER_TABLE OBJECT = LOSAPDR_TIMES_TABLE ROWS = 7 COLUMNS = 1 ROW_BYTES = 23 ROW_SUFFIX_BYTES = 179 INTERCHANGE_FORMAT = ASCII DESCRIPTION = "The LOSAPDR times table contains exact times bounding each spline interval. Each row contains one 23-digit number, 177 spaces, and a carriage-return line-feed pair." OBJECT = COLUMN NAME = "SPLINE BREAK TIMES" DATA_TYPE = ASCII_REAL START_BYTE = 1 BYTES = 23 FORMAT = "E23.16" UNIT = "MINUTE" DESCRIPTION = "The exact times of spline interval boundaries measured from midnight at the spacecraft (program mnemonic BKTIMX)." END_OBJECT = COLUMN END_OBJECT = LOSAPDR_TIMES_TABLE OBJECT = LOSAPDR_RESULTS_TABLE ROWS = 139 COLUMNS = 11 ROW_BYTES = 202 INTERCHANGE_FORMAT = ASCII DESCRIPTION = "The LOSAPDR Results Table contains the results from spline fits to Doppler tracking residuals. Each row in the table contains times, Doppler residuals, spacecraft position information, residuals to spline fits, and inferred spacecraft acceleration with respect to the nominal orbit. Each row has length 202 bytes; the first 200 are column data delimited by commas; the last two are a carriage- return line-feed pair." OBJECT = COLUMN NAME = "HH" DATA_TYPE = ASCII_INTEGER START_BYTE = 1 BYTES = 2 FORMAT = "I2.2" UNIT = "HOUR" DESCRIPTION = "The hour of a Doppler residual data point at the spacecraft." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "MM" DATA_TYPE = ASCII_INTEGER START_BYTE = 4 BYTES = 2 FORMAT = "I2.2" UNIT = "MINUTE" DESCRIPTION = "The minute of a Doppler residual data point at the spacecraft." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "SS" DATA_TYPE = ASCII_INTEGER START_BYTE = 7 BYTES = 2 FORMAT = "I2.2" UNIT = "SECOND" DESCRIPTION = "The whole seconds of a Doppler residual data point at the spacecraft. Note that there are generally fractional seconds; for full time accuracy use OFFSET TIME." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "OFFSET TIME" DATA_TYPE = ASCII_REAL START_BYTE = 10 BYTES = 23 FORMAT = "E23.16" UNIT = "MINUTE" DESCRIPTION = "Offset from CEPOCH to the time of the Doppler residual data point or inter- polation (program mnemonic DMIN)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "DOPPLER RESIDUAL" DATA_TYPE = ASCII_REAL START_BYTE = 34 BYTES = 23 FORMAT = "E23.16" UNIT = "HERTZ" DESCRIPTION = "Doppler residual from input data (program mnemonic DATA_RESID)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "SPACECRAFT ALTITUDE" DATA_TYPE = ASCII_REAL START_BYTE = 58 BYTES = 23 FORMAT = "E23.16" UNIT = "KILOMETER" DESCRIPTION = "Spacecraft altitude over reference surface (program mnemonic SC_ALT)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "SPACECRAFT LATITUDE" DATA_TYPE = ASCII_REAL START_BYTE = 82 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Spacecraft planetocentric north latitude (program mnemonic SC_LAT)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "SPACECRAFT LONGITUDE" POSITIVE_LONGITUDE_DIRECTION = "EAST" DATA_TYPE = ASCII_REAL START_BYTE = 106 BYTES = 23 FORMAT = "E23.16" UNIT = "DEGREE" DESCRIPTION = "Spacecraft planetocentric longitude (program mnemonic SC_LON)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "FIT RESIDUAL" DATA_TYPE = ASCII_REAL START_BYTE = 130 BYTES = 23 FORMAT = "E23.16" UNIT = "HERTZ" DESCRIPTION = "Doppler residual from fitted spline at HHMMSS (program mnemonic FIT_RESID)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "ACCELERATION" DATA_TYPE = ASCII_REAL START_BYTE = 154 BYTES = 23 FORMAT = "E23.16" UNIT = "MILLIMETER PER SECOND PER SECOND" DESCRIPTION = "Acceleration from fitted Doppler residual (program mnemonic ACCEL)." END_OBJECT = COLUMN OBJECT = COLUMN NAME = "HARMONIC ACCELERATION" DATA_TYPE = ASCII_REAL START_BYTE = 178 BYTES = 23 FORMAT = "E23.16" UNIT = "MILLIMETER PER SECOND PER SECOND" DESCRIPTION = "The acceleration in the line-of-sight direction due to the spherical harmonic gravity field (MGN120PSAAP). This acceleration is to be added to the acceleration from the Doppler residual to obtain the total line-of-sight acceleration." END_OBJECT = COLUMN END_OBJECT = LOSAPDR_RESULTS_TABLE END CCSD$$MARKER##mark##NJPL3IF0003000000001 .6051000000000000E+04, .3248585897263532E+06,1993-02-15T05:49:20.355, .2449033742596705E+07, -.2080845748620478E+04, -.6886579399086082E+02, .7086391905433646E+04, -.5933153404791374E+01, -.2257066147861750E+01, -.4046315214789210E+01, -.1781044824038557E+03, .2802739214662445E+03, 1, .1000000000000000E+21, 4, 1000, .2955000000000000E+00, .0000000000000000E+00, .4733333334326744E+01, .8333333333333333E+00, .5640157924421883E+02, -.9243686536512446E+02, -.4454350040616453E+01, .2458297771588861E+03, .0000000000000000E+00, .5918513166904449E+02,1993-02-15T05:49:20.355, .1037958716119950E+05, .4009393020305332E+00, .8537652954847835E+02, -.6185327805828926E+02, .1691411596286085E+03, -.6341754591764390E+02, -.2804098289618698E+02, -.4399826469142826E+02, .3238174962841605E+01, .1082307798304168E+02, -.1630130627332784E+03, .6218002729423089E+04, .8555223953575811E+01, .1670027294230895E+03, 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