SIMPLE = T / FITS STANDARD BITPIX = 16 / FITS BITS/PIXEL NAXIS = 1 / NUMBER OF AXES NAXIS1 = 965 / BLOCKED = T / Tape may be blocked EXTEND = T / There maybe standard extensions BSCALE = 1.0E0 / REAL = TAPE*BSCALE + BZERO BZERO = 0.0E0 / OPSIZE = 256 / PSIZE of original image ORIGIN = 'STScI-STSDAS' / FITSDATE= '21/09/90' / Date FITS file was created IRAFNAME= 'x0c90101t_cvt.shh' / NAME OF IRAF IMAGE FILE IRAF-MAX= 6.528100E4 / DATA MAX IRAF-MIN= 0.000000E0 / DATA MIN IRAF-B/P= 16 / DATA BITS/PIXEL IRAFTYPE= 'USHORT ' / SDASMGNU= 1 / Number of groups in original image FILLCNT = 0 ERRCNT = 0 PKTTIME = '23-AUG-1990 00:36:28.93' / GROUP PARAMETERS: OSS / FOC DATA DESCRIPTOR KEYWORDS INSTRUME= 'FOC ' / instrument in use ROOTNAME= 'X0C90101T ' / rootname of the observation set FILETYPE= 'SHP ' / shp, udl, sci CTYPE1 = 'UNITLESS ' / unitless, line, pixel, channel, sample, time NSEGPGRP= 0 / not computed - used only by OSS DEFAULTS= F / default values used in reformatting these data / STATISTICAL KEYWORDS DATE = '23/08/90 ' / date this file was written (dd/mm/yy) DCFOBSN = 13 / DCF observation number in SHP PKTFMT = 170 / packet format code TIMECODE= 82981683 / packet time code / TIME CONVERSION KEYWORDS CLKDRFTR= 0.1413348447722E-16 / spacecraft clock drift rate CLKRATE = 0.1250000005429E+00 / spacecraft clock rate SPCLINCN= 23541596 / spacecraft clock at UTCO UTCO1 = 356619520 / bytes 5-8 of UTCO UTCO2 = 9664005 / bytes 1-4 of UTCO / PODPS SUPPORT SCHEDULE: PROGRAMMATIC DATA PROGRMID= '0C9 ' / program id (base 36) PR_INV_L= 'MACCHETTO ' / last name of principal investigator PR_INV_F= 'F. DUCCIO ' / first name of principal investigator PR_INV_M= ' ' / middle initial of principal investigator AFFILIAT= 'TES ' / observer organization or affiliation ACCPDATE= '1990223 ' / proposal acceptance date (yyyyddd) OBSET_ID= '01 ' / observation set id CALIBRAT= 'Y ' / calibrate data flag OBSERVTN= '01 ' / observation number (base 36) EXPACKET= 514 / expected number of source packets PRODTYPE= 'F ' / output product medium type OPFORMAT= 'A ' / output product format specification CALIBTYP= ' ' / calibration type : E, I or Blank CDBSDATA= 'FALSE ' / cdbs notification flag: 'CAL' or 'FALSE' / PODPS SUPPORT SCHEDULE: FLAGS AND INDICATORS OPTCRLY = 'F96 ' / optical relay: F48, F96 SMMMODE = 'NOTUSED ' / spectro. mirror mechanism: INBEAM, NOTUSED SHTMODE = 'NOTUSED ' / shutter mode: INBEAM, NOTUSED LEDMODE = 'NOTUSED ' / led calibration status: ACTIVE, NOTUSED PXFORMT = 'ZOOM ' / format of the image: NORMAL, ZOOM OPTELT1 = 0 / filter element, wheel 1 f48: (0-7), f96: (0-11)OPTELT2 = 11 / filter element, wheel 2 f48: (0-7), f96: (0-11)OPTELT3 = 0 / filter element, wheel 3 f48: (0), f96: (0-11)OPTELT4 = 0 / filter element, wheel 4 f48: (0), f96: (0-11)CAMMODE = 'NOTUSED ' / coronographic apodizer mask: INBEAM, NOTUSED SAMPOFF = 0.0000000E+00 / sample offset (0.0-1023.75) LINEOFF = 0.0000000E+00 / line offset (0.0-1023.75) SAMPPLN = 512 / samples per line (64, 128, 256, or 512) LINEPFM = 1024 / lines per frame (64, 128, 256, 512, or 1024) RTAMATCH= 'NO RTA FI AVAILABL' / above f&i match RTA (TRUE,FALSE,NO RTA F&I AVL) / PODPS SUPPORT SCHEDULE: DATA GROUP II DATA INSTRUID= 'FOC ' / instrument in use WRD11_14= 13 / word 11/14 (0-255) PSTRTIME= '1990.235:00:26:19 ' / predicted obs. start time (yydddhhmmss) PSTPTIME= '1990.235:02:01:34 ' / predicted obs. stop time (yydddhhmmss) APEROBJ = 'X96ZLRG ' / si object aperture id APERSKY = ' ' / si sky aperture id TRGTNAME= '2995_1 ' / target name APERTYPE= 'SICS ' / aperture shape RTASCNV1= 0.3558864746094E+03 / right ascension of v1 axis of st DECLNV1 = -0.1519909477230E+02 / declination of v1 axis of st PSANGLV3= 0.8207261E+02 / position angle of v3 axis of st APEROFFX= 0.0000000E+00 / x component of offset of object in aperture APEROFFY= 0.0000000E+00 / y component of offset of object in aperture ANGLESEP= 0.0000000E+00 / ang. separation of target from ref. object DGESTAR = '0583600600F3 ' / FGS ID(F1,F2,F3) concat. w/ dom. gd. star id SGESTAR = '0640400568F2 ' / FGS ID(F1,F2,F3) concat. w/ subdom. gd. star idRTASNTRG= 0.3559559020996E+03 / right ascension of target DECLNTRG= -0.1528432750700E+02 / declination of target PANGAPER= 0.1388243E+03 / position angle of aperture used with target REFOBJPA= 0.0000000E+00 / pos. angle of target from ref. object (degrees)SAAAVOID= '03 ' / SAA model for SAA Avoidance (range 02-99) TARAQMOD= '01 ' / target acquisition mode (values 00, 01, 02, 03)POSTNSTX= 0.6006815917969E+04 / position of space telescope x axis POSTNSTY= -0.3032073486328E+04 / position of space telescope y axis POSTNSTZ= 0.1894986083984E+04 / position of space telescope z axis VELOCSTX= 0.3853793621100E+01 / velocity of space telescope along the x axis VELOCSTY= 0.5782227993000E+01 / velocity of space telescope along the y axis VELOCSTZ= -0.2964079856900E+01 / velocity of space telescope along the z axis RTASCSUN= 0.1518739776611E+03 / right ascension of the sun DECLNSUN= 0.1155156326290E+02 / declination of the sun RTASMOON= 0.1785349578857E+03 / right ascension of the moon DECLMOON= -0.3919294118900E+01 / declination of the moon VELABBRA= 0.0000000E+00 / aberration in position of the target ANNPARRA= 0.0000000E+00 / par. shift in position, non-solar sys target V2APERCE= 0.0000000E+00 / V2 offset of target from aper. center (arc-sec)V3APERCE= 0.0000000E+00 / V3 offset of target from aper. center (arc-sec)EQRADTRG= 0.0000000E+00 / equatorial radius of target FLATNTRG= 0.0000000E+00 / flattening of target NPDECTRG= 0.0000000E+00 / north pole declination of target NPASNTRG= 0.0000000E+00 / north pole right ascension of target ROTRTTRG= 0.0000000E+00 / rotation rate of target LONGPMER= 0.0000000E+00 / longitude of prime meridian EPLONGPM= 0.0000000E+00 / epoch of longitude of prime meridian SURFLATD= 0.0000000E+00 / surface feature latitude SURFLONG= 0.0000000E+00 / surface feature longitude SURFALTD= 0.0000000E+00 / surface feature altitude MTFLAG = ' ' / moving target flag; T if it is a moving target S0INVMAG= 0.0000000000000E+00 / S0 inverse magnitude S0XDIR = 0.0000000000000E+00 / S0 X direction S0YDIR = 0.0000000000000E+00 / S0 Y direction S0ZDIR = 0.0000000000000E+00 / S0 Z direction START48 = 0.0000000000000E+00 / command start time; seconds from 1980 END48 = 0.0000000000000E+00 / command end time; seconds from 1980 ACOEF1X = 0.0000000000000E+00 / coefficient A(1,X) of the #48 command ACOEF1Y = 0.0000000000000E+00 / coefficient A(1,Y) of the #48 command ACOEF1Z = 0.0000000000000E+00 / coefficient A(1,Z) of the #48 command ACOEF2X = 0.0000000000000E+00 / coefficient A(2,X) of the #48 command ACOEF2Y = 0.0000000000000E+00 / coefficient A(2,Y) of the #48 command ACOEF2Z = 0.0000000000000E+00 / coefficient A(2,Z) of the #48 command ACOEF3X = 0.0000000000000E+00 / coefficient A(3,X) of the #48 command ACOEF3Y = 0.0000000000000E+00 / coefficient A(3,Y) of the #48 command ACOEF3Z = 0.0000000000000E+00 / coefficient A(3,Z) of the #48 command ACOEF4X = 0.0000000000000E+00 / coefficient A(4,X) of the #48 command ACOEF4Y = 0.0000000000000E+00 / coefficient A(4,Y) of the #48 command ACOEF4Z = 0.0000000000000E+00 / coefficient A(4,Z) of the #48 command ACOEF5X = 0.0000000000000E+00 / coefficient A(5,X) of the #48 command ACOEF5Y = 0.0000000000000E+00 / coefficient A(5,Y) of the #48 command ACOEF5Z = 0.0000000000000E+00 / coefficient A(5,Z) of the #48 command REFOBJRA= 0.3559559020996E+03 / right ascension of reference object REFOBDEC= -0.1528432750700E+02 / declination of reference object / ONBOARD EPHEMERIS MODEL PARAMETERS EPCHTIME= 0.1778976000000E+09 / epoch time of parameters (secs since 1/1/85) SDMEANAN= 0.9894276032735E-14 / 2nd derivative coef for mean anomly (revs/sec/sCIRVELOC= 0.7554099427995E+04 / circular orbit linear velocity (meters/second) COSINCLI= 0.8791913062337E+00 / cosine of inclination ECCENTRY= 0.1078639887528E-02 / eccentricity ECCENTX2= 0.2157279775056E-02 / eccentricity times 2 ECBDX4D3= 0.1673278247488E-08 / eccentricity cubed times 4/3 ESQDX5D2= 0.2908660017415E-05 / eccentricity squared times 5/2 ECBDX3 = 0.3764876056849E-08 / eccentricity cubed times 3 FDMEANAN= 0.1719878476939E-03 / 1st derivative coef for mean anomly (revs/sec) RCASCNRD= -0.1285545004612E-05 / rt chge right ascension ascend node (rads/sec) RCASCNRV= -0.2046008420511E-06 / rt chge right ascension ascend node (revs/sec) ARGPERIG= 0.2583110710441E+00 / argument of perigee (revolutions/second) MEANANOM= 0.6272118167978E+01 / mean anomaly (radians) RCARGPER= 0.1934880917612E-06 / rate change of argument of perigee (revs/sec) RASCASCN= 0.5306096355224E+00 / right ascension of ascending node (revolutions)SINEINCL= 0.4764689360735E+00 / sine of inclination SEMILREC= 0.6990183965534E+07 / semi-latus rectum (meters) TIMEFFEC= 0.1778988000000E+09 / time parameters took effect (secs since 1/1/85)OBSSTRTT= 0.1780719790000E+09 / predicted obs. start time (secs since 1/0/85) / DMF EXPOSURE DATA PROPOSID= '02995 ' / PEP proposal identifier PEP_EXPO= '0.5000000 ' / PEP exposure identifier including sequence TARGNAM1= 'R-AQR ' / proposer's target name (first 18 char) TARGNAMC= ' ' / target name continuation (last 12 char) PLAN_EXP= 0.6000000000000E+03 / proposed time per exposure PLAN_SN = 0.0000000000000E+00 / proposed signal-to-noise ratio PRIORITY= 1 / proposer's priority for exposure RA = 0.3559559E+03 / right ascension of the target (degrees) DEC = -0.1528433E+02 / declination of the target (degrees) EXPOSURE= 0.8967500E+03 / exposure duration (seconds)--calculated EXPSTRT = 0.8294753E-05 / exposure start time (seconds) EXPEND = 0.8295470E-05 / exposure end time (seconds) SUNANGLE= 0.1563696E+03 / angle between sun and V1 axis (degrees) MOONANGL= 0.1607025E+03 / angle between moon and V1 axis (degrees) END 7   (     ~  L ref}~tyzzu[uwQx|{{Xb' K=}t<ͫ-ϻ4 0C901010AN060909J020W067050209F5404vAg7\& S?'[$t@QUUUUUUu|XTENSION= 'TABLE ' / FITS STANDARD BITPIX = 8 / 8-bits per 'pixels' NAXIS = 2 / Simple 2-D matrix NAXIS1 = 49 / No of characters per row NAXIS2 = 1 / The number of rows PCOUNT = 0 / No 'random' parameters GCOUNT = 1 / Only one group TFIELDS = 3 / Number of fields per row EXTNAME = 'x0c90101t_cvt.shh.tab' / Name of table TTYPE1 = 'FILLCNT ' / TBCOL1 = 1 / TFORM1 = 'I11 ' / %11d TUNIT1 = ' ' / TTYPE2 = 'ERRCNT ' / TBCOL2 = 13 / TFORM2 = 'I11 ' / %11d TUNIT2 = ' ' / TTYPE3 = 'PKTTIME ' / TBCOL3 = 25 / TFORM3 = 'A24 ' / %-24s TUNIT3 = 'CH*24 ' / FILLCNT = ' number of segments containing fill' / ERRCNT = ' number of segments containing errors' / PKTTIME = ' time from the packet ancillary data' / END 0 023-AUG-1990 00:36:28.93