| UVS_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | UVS |
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| UVS_DESIGNER_OBSERVATION | | UVS |
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| TRANSIT_ET | Event tool support segment definition | GENERIC |
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| TRAJECTORY_SEGMENT | defined segment for moon coverage tool export functionnality | GENERIC |
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| SWI_RIDER_OBSERVATION | | SWI |
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| SWI_DESIGNER_OBSERVATION | | SWI |
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| SUN_OCC_ET | Event tool support segment definition | GENERIC |
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| SUN_OCC | Solar occultation by Jupiter, as seen from the SC. | Working Group 4 |
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| STELLAR_UVS_OCC_ET | | GENERIC |
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| STELLAR_OCC_ET | Event tool support segment definition | GENERIC |
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| SPICE_ATT_GOTOMARS_NPO | | GENERIC |
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| SPICE_ATT_GOTOMARS_NOA_HOT | | GENERIC |
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| SPICE_ATT_GOTOGANYMEDE_PHASE_SUP_SOL_CONJ | | GENERIC |
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| SPICE_ATT_GOTOGANYMEDE_NPO | | GENERIC |
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| SPICE_ATT_GOTOGANYMEDE_NOA_HOT | | GENERIC |
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| SPICE_ATT_GOTOGANYMEDE_NOA | | GENERIC |
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| SPICE_ATT_GOTOEUROPA_NPO | | GENERIC |
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| SPICE_ATT_GOTOEUROPA_NOA_HOT | | GENERIC |
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| SPICE_ATT_GOTOEUROPA_NOA | | GENERIC |
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| SPICE_ATT_GOTOEARTH_NPO | | GENERIC |
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| SPICE_ATT_GOTOEARTH_NOA_HOT | | GENERIC |
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| SPICE_ATT_GOTOEARTH_NOA | | GENERIC |
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| SPICE_ATT_GOTOCALLISTO_NPO | | GENERIC |
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| SPICE_ATT_GOTOCALLISTO_NOA_HOT | | GENERIC |
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| SPICE_ATT_GOTOCALLISTO_NOA | | GENERIC |
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| SOC_RIDER_OBSERVATION | Placeholder for SOC Rider Observation | SOC |
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| SOC_DESIGNER_OBSERVATION | | SOC |
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| SHADOWEDGE | rings SHADOWEDGE. Imaging of the ring region intersected by the planetary shadow at moderate
elevation and very high phase. Especially for the very faint gossamer rings and the Thebe
extension | Working Group 2 |
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| RPWI_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | RPWI |
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| RINGSPIRAL_MP | RINGSPIRAL_MP (medium phase: JANUS Def) | Working Group 2 |
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| RINGSPIRAL_HP | RINGSPIRAL_HP (high phase, Janus def) | Working Group 2 |
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| RINGPHASE | | Working Group 2 |
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| RINGMOSAIC | RINGMOSAIC (Janus definition). impression of the extent of the whole ring
system | Working Group 2 |
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| RINGMATTER | RINGMATTER. Observations of the main rings and the gossamer rings, imaging the ring ansae from moderately large elevation.
The moderatly large elevation will reveal azimuthal structure in the rings and the presence of clumps at the resolution limit of the imaging. | Working Group 2 |
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| RING_PHASECURV_90 | | Working Group 2 |
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| RING_PHASECURV_80 | | Working Group 2 |
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| RING_PHASECURV_70 | | Working Group 2 |
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| RING_PHASECURV_60 | | Working Group 2 |
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| RING_PHASECURV_50 | | Working Group 2 |
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| RING_PHASECURV_5 | Opportunity 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 deg | Working Group 2 |
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| RING_PHASECURV_40 | | Working Group 2 |
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| RING_PHASECURV_30 | | Working Group 2 |
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| RING_PHASECURV_20 | | Working Group 2 |
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| RING_PHASECURV_170 | | Working Group 2 |
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| RING_PHASECURV_160 | | Working Group 2 |
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| RING_PHASECURV_150 | | Working Group 2 |
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| RING_PHASECURV_140 | | Working Group 2 |
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| RING_PHASECURV_130 | | Working Group 2 |
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| RING_PHASECURV_120 | | Working Group 2 |
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| RING_PHASECURV_110 | | Working Group 2 |
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| RING_PHASECURV_100 | | Working Group 2 |
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| RING_PHASECURV_10 | Opportunity 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 deg | Working Group 2 |
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| RING_LP | Ring low phase | Working Group 2 |
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| RING_HP | Ring high phase | Working Group 2 |
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| RIME_DESIGNER_OBSERVATION | | RIME |
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| RECOVERY | | GENERIC |
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| RADEM_DESIGNER_OBSERVATION | | RADEM |
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| PERIJOVE_TERMINATOR | | Working Group 4 |
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| PERIJOVE_NIGHTSIDE | | Working Group 4 |
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| PERIJOVE_DAYSIDE | | Working Group 4 |
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| NAVCAM_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | NAVCAM |
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| NAVCAM_DESIGNER_OBSERVATION | | NAVCAM |
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| MAJIS_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | MAJIS |
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| JUPITER_TAIL | In situ search for signatures of local magnetic reconnection in the Jovian magnetotail | Working Group 3 |
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| JUPITER_PHASE_MIN | | Working Group 4 |
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| JUPITER_PHASE_MAX | | Working Group 4 |
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| JUPITER_PHASE_165_INC | | Working Group 4 |
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| JUPITER_PHASE_165_DEC | | Working Group 4 |
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| JUPITER_PHASE_150_INC | | Working Group 4 |
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| JUPITER_PHASE_150_DEC | | Working Group 4 |
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| JUPITER_PHASE_135_INC | | Working Group 4 |
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| JUPITER_PHASE_135_DEC | | Working Group 4 |
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| JUPITER_PHASE_120_INC | | Working Group 4 |
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| JUPITER_PHASE_120_DEC | | Working Group 4 |
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| JUPITER_PHASE_090 | | Working Group 4 |
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| JUPITER_PERIJOVE | Jupiter observations | Working Group 4 |
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| JUPITER_PDT | In situ Jupiter particle distribution transition region observation.
Maximize pitch angle coverage for PEP/JEI, JDC,JoEE, JENI (ion mode) | Working Group 3 |
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| JUPITER_NULL | In situ Jupiter magnetic null search | Working Group 3 |
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| JUPITER_MONITORING | | Working Group 4 |
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| JUPITER_INCLINED_AURORA | | Working Group 4 |
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| JUPITER_GM | In situ mapping of global configuration and monitoring dynamics of the Jovian magnetospheric environment.
corotation should be in the FoV of PEP/JDC or PEP/JEI.
Conditions for coverage:
◦ Minimum angle less than about 11.25 deg (half-azimuthal sector size) of a JEI or JDC pixel from corotation
◦ Boresight angle of JDC or JEI less than ˜90 deg
Conditions for ideal coverage:
◦ Minimum angle less than about 11.25 deg (half-azimuthal sector size) of a JEI or JDC pixel from corotation
◦ Boresight angle less than ˜75 deg (JEI) or 70 deg (JDC): corotation away from the FoV edge
JDC is preferred for monitoring corotation, over JEI, when possible. | Working Group 3 |
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| JUPITER_FD_WOL_FB | In the last week before the fly-by a WOL slot shall be combined with the
TCM slot at To– 3 days (i.e. a single 3-hr slot). Another 2-hour WOL slot shall be reserved at To + 12 hours. | GENERIC |
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| JUPITER_FD_WOL | Flight dynamics wheel off-loading slot, outside of Flyby preparation and recuperation | GENERIC |
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| JUPITER_FD_TCM | | GENERIC |
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| JUPITER_FD_NAV_FB | | GENERIC |
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| JUPITER_ENA | Imaging of Jupiter's magnetosphere in energetic neutral atoms (ENAs).Maximize pitch angle coverage with PEP JEI,JDC,JoEE, JENI (ion mode)
a) JENI has a broad FoV and captures Jupiter and the Io/Europa torus and magnetosphere at most times. No special pointing design required for JENI besides requiring an approximate nadir pointing (considerable offsets can still be acceptable)
b) JNA disk-shaped/slit FoV has a slight offset from the XZ spacecraft plane, meaning that during nadir pointing, it images preferentially the northern or southern extension of the Europa/Io torus, whereas Jupiter may be in the edge or outside of the FoV, especially at large distances. Scans (small rotations around Sc-X) or periods with stable, small offset of the SC-xz plane from Nadir can help to better image stronger emissions from the equatorial torus | Working Group 3 |
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| JUPITER_CPS | In situ Jupiter current/plasma sheet observation | Working Group 3 |
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| JUPITER_CP | In situ Jupiter corotation breakdown region and plasma transport observation. Maximize the intervals for which co-rotation is measured to build spatial and temporal coverage of corotation profiles across the magnetosphere and also in the local moon environments.
CP stands for corotation profile | Working Group 3 |
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| JMAG_RIDER_OBSERVATION | Placeholder Segment to accomodate the detailed scenario observation plan generation process. | JMAG |
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| JMAG_DESIGNER_OBSERVATION | | JMAG |
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| JMAG_CALROLL | 5 calibration roll needed by JMAG. 2 as soon as possible after JOI. 3 during phase 5: one at the start of phase 5, the last 2 as late as possible before GOI | WGX |
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| JANUS_RIDER_OBSERVATION | Placeholder for JUICE SOC Observations. | JANUS |
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| JANUS_DESIGNER_OBSERVATION | | JANUS |
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| IO_TOR_DUST | Io torus dust | Working Group 2 |
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| 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 |
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| IO_MAJ_HOTSPOTS | IO_MAJ_HOTSPOTS | Working Group 2 |
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| IO_MAJ_COMPOSITION | IO_MAJ_COMPOSITION | Working Group 2 |
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| IO_ECLIPSE | Io observation while Io is in eclipse. | Working Group 2 |
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| INCLINED_SOUTH | | Working Group 4 |
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| INCLINED_NORTH | | Working Group 4 |
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