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G_RS_1G1 Working Group 2
G_RS_5G5 Working Group 2
RING_PHASECURV_170 Working Group 2
RING_PHASECURV_160 Working Group 2
RING_PHASECURV_150 Working Group 2
RING_PHASECURV_140 Working Group 2
RING_PHASECURV_130 Working Group 2
RING_PHASECURV_120 Working Group 2
RING_PHASECURV_110 Working Group 2
RING_PHASECURV_100 Working Group 2
RING_PHASECURV_90 Working Group 2
RING_PHASECURV_80 Working Group 2
RING_PHASECURV_70 Working Group 2
RING_PHASECURV_60 Working Group 2
RING_PHASECURV_50 Working Group 2
RING_PHASECURV_40 Working Group 2
RING_PHASECURV_30 Working Group 2
RING_PHASECURV_20 Working Group 2
EUROPA_DISTANT Working Group 2
J_SAT_INN_AST_A Working Group 2
J_SAT_IRR_AST_E Working Group 2
J_SAT_INN_CHAR_A Working Group 2
J_SAT_INN_AST_T Working Group 2
J_SAT_IRR_CHAR_E Working Group 2
G_RS_26G11 Working Group 2
G_RS_25G10 Working Group 2
G_RS_24G9 Working Group 2
G_RS_23G8 Working Group 2
G_RS_22G7 Working Group 2
C_RS_21C13 Working Group 2
C_RS_20C12 Working Group 2
C_RS_19C11 Working Group 2
G_RS_18G6 Working Group 2
G_RS_17G5 Working Group 2
C_RS_16C10 Working Group 2
C_RS_15C9 Working Group 2
C_RS_14C8 Working Group 2
C_RS_13C7 Working Group 2
C_RS_12C6 Working Group 2
C_RS_11C5 Working Group 2
C_RS_10C4 Working Group 2
C_RS_9C3 Working Group 2
C_RS_8C2 Working Group 2
E_RS_7E2 Working Group 2
E_RS_6E1 Working Group 2
C_RS_5C1 Working Group 2
G_RS_4G4 Working Group 2
G_RS_2G2 Working Group 2
IO_RS Working Group 2
J_RING Working Group 2
FB_RS Working Group 2
G_distant Working Group 2
E_RS Working Group 2
E_distant Working Group 2
C_RS Working Group 2
C_distant Working Group 2
ASTRO_IRR2_SINOPE Working Group 2
ASTRO_IRR_ELARA Working Group 2
CALLISTO_DISTANT Working Group 2
CALLISTO_FLYBY_WG2 Working Group 2
CHARACTERIZATION_IRR2_CARME Working Group 2
EUROPA_FLYBY_WG2 Working Group 2
GANYMEDE_DISTANT Working Group 2
GANYMEDE_FLYBY_WG2 Working Group 2
IO_MONITORING- JANUS minimum distance = 7.00e+05 km - MAJIS minimum distance = 8.00e+05 km - SWI minimum distance = 6.00e+05 km (able to resolve target when angular size is > 1 mrad) Working Group 2
ASTRO_INNERAstrometry inner moonsWorking Group 2
ASTRO_IRR2_ANANKEAstrometry irregular moon AnankeWorking Group 2
ASTRO_IRR2_CARMEAstrometry irregular moon CarmeWorking Group 2
ASTRO_IRR1_CARPOAstrometry irregular moon CARPOWorking Group 2
ASTRO_IRR1_CHALDENEAstrometry irregular moon CHALDENEWorking Group 2
ASTRO_IRR1_HIMALIAAstrometry irregular moon HIMALIAWorking Group 2
ASTRO_IRR1_KALLICHOREAstrometry irregular moon KALLICHOREWorking Group 2
ASTRO_IRR1_LEDAAstrometry irregular moon LEDAWorking Group 2
ASTRO_IRR1_LYSITHEAAstrometry irregular moon LYSITHEAWorking Group 2
ASTRO_IRR1_TAYGETEAstrometry irregular moon TAYGETEWorking Group 2
ASTRO_IRR1_THEMISTOAstrometry irregular moon THEMISTOWorking Group 2
ASTRO_IRR2_PASIPHAEastrometry measurement with inertial pointing to moon PasiphaeWorking Group 2
CALLISTO_FB_RSCallisto Flyby remote sensingWorking Group 2
C_RS_OBSCallisto Remote sensing GENERIC containing obs database linkWorking Group 2
CHARACTERIZATION_IRR2_ANANKECharacterization irregular moon ANANKEWorking Group 2
CHARACTERIZATION_IRR_ELARACharacterization irregular moon ElaraWorking Group 2
CHARACTERIZATION_IRR2_PASIPHAEcharacterization irregular moon PasiphaeWorking Group 2
CHARACTERIZATION_IRR2_SINOPECharacterization irregular moon SinopeWorking Group 2
CHAR_IRR1Characterization irregular moons group 1 (see list below)Working Group 2
EUROPA_FB_RSEuropa Flyby remote sensingWorking Group 2
E_RS_OBSEuropa remote sensing generic segment containing obs database linkWorking Group 2
G_RS_OBSG_RS GENERICWorking Group 2
GANYMEDE_FB_RSGanymede flyby remote sensingWorking Group 2
G_RS_3G3HAA as per 3GM UM IS considering NIMWorking Group 2
IO_ECLIPSEIo observation while Io is in eclipse.Working Group 2
IO_TOR_DUSTIo torus dustWorking Group 2
J_SATjupiter satellite GENERICWorking Group 2
RING_PHASECURV_10Opportunity implementation in geopipeline SC distance to Jupiter larger than 8e5 km SC elevation above the rings lower than 0.5 deg Only one Ansae tested for phase conditions - value must be between 10 deg and 20 degWorking Group 2
RING_PHASECURV_5Opportunity implementation in geopipeline SC distance to Jupiter larger than 8e5 km SC elevation above the rings lower than 0.5 deg Only one Ansae tested for phase conditions - value must be between 5 deg and 10 degWorking Group 2
RING_HPRing high phaseWorking Group 2
RING_LPRing low phaseWorking Group 2
G_RS_9G6test 3_2Working Group 2
G_RS_26G12test 3_2Working Group 2
G_RS_24G10test 3_2Working Group 2
G_RS_21G9test 3_2Working Group 2

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