DAF/CK  < DAFCAT: CK CONCATENATION > ##cLTL-IEEEFTPSTR: : : : :::ENDFTPSOLAR-ORBITER Measured CK file by ESA SPICE Service=========================================================================== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.2.1 by the ESA SPICE Service on July 29, 2020.Objects------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000.Approximate Time Coverage------------------------------------------------------------------------ Begin UTC: 2020-JUL-27 08:25:51.693 End UTC: 2020-JUL-27 12:59:57.720Status------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis.Pedigree------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0649153527-0649352817_000__adcsng_temp.txtUsage------------------------------------------------------------------------ This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V07.tf a Frame Kernel file required to establish relationships between frames used in geometry computations. naif0012.tls a Leapseconds Kernel file is used in conversions between ephemeris time and UTC (coordinated universal time). solo_ANC_soc-sclk_20200729_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care.Accuracy------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different inputT>G!5?n M' sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6).References-^^/ſeaE?----------------------------------------------------------------------- [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK User GuideContact Information------------------------------------------------------------------------ If you have any questions regarding this file contact the ESA SPICE Service (ESS) at ESAC: Marc Costa Sitja (+34) 91-8131-457 esa_spice@sciops.esa.int, marc.costa@esa.intMSOPCK Setup Parameters------------------------------------------------------------------------********************************************************************************MSOPCK SETUP FILE: msopck_quat.setup******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200729_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V07.tf' ~wE?(Yə> INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service'********************************************************************************RUN-TIME OBTAINED META INFORMATION:********************************************************************************PRODUCT_CREATION_TIME = 2020-07-29T17:07:28START_TIME = 2020-07-27T08:25:51.693STOP_TIME = 2020-07-27T12:59:57.720********************************************************************************INTERPOLATION INTERVJλm>Wyc>~ 6?ALS IN THE FILE SEGMENTS:********************************************************************************SEG.SUMMARY: ID -144000, COVERG: 2020-07-27T08:25:51.693 2020-07-27T12:59:57.720-------------------------------------------------------------------------------- 2020-07-27T08:25:51.693 2020-07-27T12:59:57.720********************************************************************************SOLAR-ORBITER Measured CK file by ESA SPICE Service=========================================================================== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.2.1 by the ESA SPICE Service on July 29, 2020.Objects------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean G,6?,L<+/ſEquator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000.Approximate Time Coverage------------------------------------------------------------------------ Begin UTC: 2020-JUL-27 12:59:57.720 End UTC: 2020-JUL-27 13:15:57.722Status------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis.Pedigree------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0649153527-0649352817_001__adcsng_temp.txtUsage------------------------------------------------------------------------ Th*o2.ſ c/E?]Ѭis file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V07.tf a Frame Kernel file required to establish relationships between frames used in geometry computations. naif0012.tls a Leapseconds Kernel file is used in conversions between ephemeris time and UTC (coordinated universal time). solo_ANC_soc-sclk_20200729_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care.Accuracy------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number o>,{of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERV,E>x6h6?S3AL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6).References------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK User GuideContact Information------------------------------------------------------------------------ If you have any questions regarding this file contact the ESA SPICE Service (ESS) at ESAC: Marc Costa Sitja (+34) 91-8131-457 esa_spice@sciops.esa.int, marc.costa@esa.intMSOPCK Setup Parameters----------------------------------------------------------------------_tSYb%F@**************************************************RUN-TIME OBTAINED META INFORMATION:********************************************************************************PRODUCT_CREATION_TIME = 2020-07-29T17:07:29START_TIME = 2020-07-27T12:59:57.720STOP_TIME = 2020-07-27T13:15:57.722********************************************************************************INTERPOLATION INTERVALS IN THE FILE SEGMENTS:********************************************************************************SEG.SUMMARY: ID -144000, COVERG: 2020-07-27T12:59:57.720 2020-07-27T13:15:57.722-------------------------------------------------------------------------------- 2020-07-27T12:59:57.720 2020-07-27T13:15:57.722********************************************************************************SOLAR-ORBITER Measured CK file by ESA SPICE Service=========================================================================== This file contains SOLO S/C attitude quaternio);\GOm Eq>g6?ns extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.2.1 by the ESA SPICE Service on July 29, 2020.Objects------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000.Approximate Time Coverage------------------------------------------------------------------------ Begin UTC: 2020-JUL-27 13:15:57.722 End UTC: 2020-JUL-29 06:11:33.965Status------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis.Pedigree---------------------------------------------------3v6?bHŖ.ſ--------------------- ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0649153527-0649352817_002__adcsng_temp.txtUsage------------------------------------------------------------------------ This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V07.tf a Frame Kernel file required to establish relationships between frames used in geometry computations. naif0012.tls a Leapseconds Kernel file is used in conversions between ephemeris time and UTC (coordinated universal time). solo_ANC_soc-sclk_20200729_V01.tsca Spacecraft Clock Kernel file is used >D.ſ@/AE?(l in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care.Accuracy------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVIٜ|h{Y䚾SZ>AL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6).References------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK UsecF>{7?8R @r GuideContact Information------------------------------------------------------------------------ If you have any questions regarding this file contact the ESA SPICE Service (ESS) at ESAC: Marc Costa Sitja (+34) 91-8131-457 esa_spice@sciops.esa.int, marc.costa@esa.intMSOPCK Setup Parameters------------------------------------------------------------------------********************************************************************************MSOPCK SETUP FILE: msopck_quat.setup******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200729_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V07.tf' INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRU6ЋOt.ſgE?MENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service'********************************************************************************RUN-TIME OBTAINED META INFORMATION:********************************************************************************PRODUCT_CREATION_TIME = 2020-07-29T17:07:31START_TIME = 2020-07-27T13:15:57.722STOP_TIME = 2020-07-29T06:11:33.965********************************************************************************INTERPOLATION INTERVALS IN THE FILE SEGMENTS:********************************************************************************SEG.SUMMARY: ID -144000, COVERG: 2020-07-27T13:15:57.722 2020-07-29T06MvD? ;U0 5h =>:11:33.965-------------------------------------------------------------------------------- 2020-07-27T13:15:57.722 2020-07-29T06:11:33.965********************************************************************************SOLAR-ORBITER Measured CK file by ESA SPICE Service=========================================================================== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.2.1 by the ESA SPICE Service on July 29, 2020.Objects------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000.Approximate Time Coverage--------------------------------------------------------------------Y[B>$.>rk7?---- Begin UTC: 2020-JUL-29 06:11:33.965 End UTC: 2020-JUL-29 06:15:42.341Status------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis.Pedigree------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0649153527-0649352817_003__adcsng_temp.txtUsage------------------------------------------------------------------------ This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V07.tf a Frame Kernel file required to estB:y7?s)l.ſablish relationships between frames used in geometry computations. naif0012.tls a Leapseconds Kernel file is used in conversions between ephemeris time and UTC (coordinated universal time). solo_ANC_soc-sclk_20200729_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care.Accuracy------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternB.ſD? ions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE^jEGYzE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6).References------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK User GuideContact Information------------------------------------------------------------------------ If you have any questions regarding this file contact the ESA SPICE Service (ESS) at ESAC: Marc Costa Sitja (+34) 91-8131-457 esa_spice@sciops.esa.int, marc.costa@esa.intMSOPCK Setup Parameters------------------------------------------------------------------------********************************************************************************MSOPCK SETUP FILE: msopck_quat.setup*******************************************************aoȃ>\q7?G************************* \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200729_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V07.tf' INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service'********************************************************************************RUN-TIME OBTAINED META INFORMATION:********************************************************************************PRODUCT_C04qL;.ſd`D?REATION_TIME = 2020-07-29T17:07:31START_TIME = 2020-07-29T06:11:33.965STOP_TIME = 2020-07-29T06:15:42.341********************************************************************************INTERPOLATION INTERVALS IN THE FILE SEGMENTS:********************************************************************************SEG.SUMMARY: ID -144000, COVERG: 2020-07-29T06:11:33.965 2020-07-29T06:15:42.341-------------------------------------------------------------------------------- 2020-07-29T06:11:33.965 2020-07-29T06:15:42.341********************************************************************************SOLAR-ORBITER Measured CK file by ESA SPICE Service=========================================================================== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.2.1 by the ESA SPICE Service on JuD?{|ֽ>Ks^ ly 29, 2020.Objects------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000.Approximate Time Coverage------------------------------------------------------------------------ Begin UTC: 2020-JUL-29 06:15:42.341 End UTC: 2020-JUL-29 15:47:22.011Status------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis.Pedigree------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following pr_ teÐū+\8?ocessed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0649153527-0649352817_004__adcsng_temp.txtUsage------------------------------------------------------------------------ This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V07.tf a Frame Kernel file required to establish relationships between frames used in geometry computations. naif0012.tls a Leapseconds Kernel file is used in conversions between ephemeris time and UTC (coordinated universal time). solo_ANC_soc-sclk_20200729_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these filex+8?.Mࣸg.ſs shall be analysed and handled with care.Accuracy------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between qua8d&I.ſd~*\D?t䙾ternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6).References------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK User GuideContact Information------------------------------------------------------------------------ If you have any questions regarding this file contact the ESA SPICE :_ء~n?GTZ&>Service (ESS) at ESAC: Marc Costa Sitja (+34) 91-8131-457 esa_spice@sciops.esa.int, marc.costa@esa.intMSOPCK Setup Parameters------------------------------------------------------------------------********************************************************************************MSOPCK SETUP FILE: msopck_quat.setup******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200729_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V07.tf' INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TFR h>.mz8?h-JYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service'********************************************************************************RUN-TIME OBTAINED META INFORMATION:********************************************************************************PRODUCT_CREATION_TIME = 2020-07-29T17:07:32START_TIME = 2020-07-29T06:15:42.341STOP_TIME = 2020-07-29T15:47:22.011********************************************************************************INTERPOLATION INTERVALS IN THE FILE SEGMENTS:********************************************************************************SEG.SUMMARY: ID -144000, COVERG: 2020-07-29T06:15:42.341 2020-07-29T15:47:22.011-------------------------------------------------------------------------------- 2020-07-29T06:15:42.341 2020-07-29T15:47:22.011*************************** guXVl-ſ;*D?***************************************************** D?ѣ涜>+_^U@XBXBxXBXBxXBYB YB:YB!:YB8+ZBbSOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE FG8?RvBɽ-ſb`5?2ڲuQ;/ſ`F?Uuw2jv_ 4 d4>5?hf'/ſ2 F?I x?^:>D5?(f?ʓƱ/ſ_F?(ZGN=>j$o##}>lY5?k'i2u"/ſvUF?1=>Wiod}qd>gf5?n0wޘ&/ſ.q_F?z[n>N4>>rK[>€r5?ѶɟƮ*/ſrTF?ϒ>"Y7:rexJ5?wڟ t-/ſvF?BqHQ_z> 5?vڟƐ[(/ſ kF?OHٛUrfg;ۑ>ζ5? ?Пz/ſ F?F;N>G+R >LGT5?AgЇ/ſIGUF? m%C+>ur)>z֬5?+/ſwF?E3) d#4>ah>'5?H|/ſF?rl>uGRq>B5?o&s)/ſOe F?#)2>k;4K|A.خ5?ߟ$W`0/ſó+ F?+v>!Za3dG5?es8"0pD/ſӏ@ F?t>ʅCp;j;>U5?ˍ)5L/ſ0 F?kc>(ug>„yw 8>ە5?&‘8M/ſIF?cZN%vɚ}.S>>̲5?k2DYIK/ſ͟HF?ېI=>.^T>G!5?n M'P.M/ſF?;S^>&n'hVO>)?{=5?=7"f[C@/ſmF?LmQmLy㐾C/>i5?z"8/ſf}F?4sΜ>hf|fѓ 9^ Aa> sf|n5?C;j=/ſaAF?K-|qwH>p X>5?8q5ruV>/ſ÷UF? fx ف>>y"LJ>CF5?xZ' =S ˟>8\t5?|13/ſ';F?φӇ>TVqĔ>?5?/y6]73/ſ-E?tJ埤>6ȩAԂ!…>TR5?d[.3/ſ=E?Ӽ bjy+.>1U5?3&)Ŷ;<0/ſgVE?:@o>3z7>>l2~5?N|(g*N)/ſtE?,,-𭾒y}v>eC> 65?s<|/ſK2E?@^η >pbg>}5?L{/ſ8E?.U@>ͧwH%uLUt5?_RF%\,/ſ E?볚>a9Zcu>aQ5?ļWݽI//ſBE?ֿg;>pI3>\]5?-sKO+/ſ_uE?܇zzGۏ>4>C5?(0Ϧ2[%/ſdE?ꥂ:M4A-'z>!ޙ>4|5?^^/ſeaE?Cgw钾dJ>AI@>1Z5?{h\:&/ſ3H63E?M{v;G.>#5?r//ſR:wE?}-Cg7 W>#rs5?񟸿 /ſ"#kE?4J>z I_3 ><3[5?<bL} /ſ E?~>qH:\jR/u>Y5?z[Ydqq/ſψE?TN╮>K-;>Cn5?[ B7:~$/ſFE?͚BEīuw)@`5?]W=G /ſЦE?ݵEP%Y> ɕ>K=kz5?7X/ſFE?ĩ‚Y"ˌ>q5?'nn:5/ſE?>B ]v>EV>Ly5?xR?/ſ(m,QE?w} .2QR@Z>I,>J.5?J/ſE?P~lw4 A>!A>^j 5?(`럸A/ſRWE?MW aY>t4i:K>5? 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