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LTP04 has been confirmed to run from 2021-06-28T00:00:00Z until 2021-09-27T00:00:00Z.

In March 2021, it was decided to change the typical duration of an LTP from 6 to 3 months, in order to allow Flight Dynamics to produce stable LTP input and to add flexibility by planning LTP closer to the execution dates.
This page was originally called "LTP04 July 2021-Dec 2021" and included the mission-level planning for the full 6 months period done at SWT#27 (Oct 2020).
We now greyed out all information regarding the period Oct-Dec 2021 and copied that to the new page LTP05 Oct 2021-Dec 2021.

Orbital context

Plots are in GSE (geocentric solar ecliptic) coordinates, so Earth is at [0,0], the Sun is at [1,0]. The plot is the projection of the orbit on the ecliptic plane.

Animated Version: Orbit_GSE_2021H2.mp4

New definition for the grey shading representing downlink rates:

  • white = maximum downlink rate at which you can empty the SSMM in ~10 days
  • light-grey = SSMM fill state decreases with everyone operating at EID-A rates
  • mid-grey = SSMM fill state increases within RSW (10 instruments operating) and decreases outside RSW (IS-only breakeven rate < downlink rate < inside-RSW breakeven rate )
  • dark-grey = SSMM fill state increases with just IS operating (downlink rate < IS-only breakeven rate)

RS checkout window placement

Period

Window/GAM

EXT Start/
GAM restriction Start

Start

End

Heliocentric
Distance
Range [AU]

Heliographic
Latitude
Range [deg]

SC-Sun-Earth
Angle Range
[deg]

Conjunction

Safe Mode Comms Blackout

Largest Comms Roll

GAM Restrictions

LTP 04RSCW4 (cold)n/a2021-09-12T00:00:002021-09-20T00:00:000.5870.5890.5950.751.131.47

50.88

44.66
38.61nono0 (TBC)no

GAMs and conjunctions

  • Venus GAM 2 on 2021-08-09, GAM restriction period runs from 2021-07-12 to 2021-08-23
  • Earth GAM 1 on 2021-11-27, GAM restriction period expected to run from 2021-10-30 to 2021-12-04 (now in LTP05)

Science and calibration planning

IS science + 4th opportunity for RS payload to characterise and calibrate the instruments.

  • IS science modes, incl. regular and coordinated bursts
  • MAG calibration roll to be scheduled in window 2021-10-01T00:00:00.000Z - 2021-10-04T00:00:00.000Z (heliocentric distance ~0.64 AU) - now in LTP05
  • RSCW4: 8-day window of RS instrument specific characterisation and calibration campaigns (cold checkout)

Coordinated campaigns (updated based on change of RSCW timing agreed SWT 27)

RSCW4:

  • PHI+EUI coordinated Offpointing Mosaic for Flatfielding with FDT and FSI (campaign details in TN-0019). (star)
    This campaign is scheduled on 2021-09-13 (06:00-06:55) 
  • EUI/HRI flatfielding campaign, involving smaller offpoints (Sect 3 in TN-0019). 
    This campaign is scheduled on 2021-09-13 (07:00-07:55) 
  • Limb Pointing RS-Alignment campaign (TN-0035) (star), tailored for high-resolution telescopes SPICE, PHI/HRT and EUI/HRI, involving limb pointings to N,S,E,W + disc centre. The whole campaign takes about 9 hours, based on SPICE durations of full scans. 
    This campaign is tentatively scheduled on 2021-09-14 (01:00-09:50)
    Metis is also participating.
  • S/C offpoints for SoloHI and Metis specific straylight calibration  (TN-0036(star)
    Scheduled on 2021-09-19 (9:30-15:05)

    • SPICE and EUI also participate in this offpointing campaign
  • Limb pointing for SPICE's "out of field response" campaign involving a single "East" (wrt spacecraft) limb pointing (TN-0046(star) 
    The campaign takes 3 hours in total and is scheduled on 2021-09-19 (16:30-19:40)
  • RS+IS SOOP to try out first coordinated science campaign, incl. VSTP cycle.
    L_SMALL_HRES_HCAD_SlowWindConnection SOOP scheduled from 16 to 19 Sep 2021.
  • At SWT24, the RSWG proposed to test out the SPROUT SOOP, i.e. out-of-window RS synoptics during the last day of RSCW4. SPROUT already tested in LTP2
  • EUI proposes to synchronize its observations with STEREO observations during RSCW 4 (almost the same LOS). Other instruments may be interested too, to be discussed during SOWG.

Note that there is an opportunity to "upgrade" RSCW4 → the original timeline from MLP has been upgraded with factor 5 in TM during SOWG #17 - Apr 2021

Extra, special campaigns:

These address the opportunities identified during SWT 27 (listed in the table below). The activities taking place in the last 3 months - now LTP5 - have been greyed out and moved to LTP05 Oct 2021-Dec 2021

  • Remote sensing checkout window 4 has been moved to 12-20 September. (Affected instruments: ALL)
  • High rate observations have been added for the in situ instruments for the following periods (affected instruments: EPD, MAG, RPW, SWA):
    • 2021-08-02 - 2021-08-23 (VGAM, combined science with Bepi Colombo, Parker Solar Probe)
    • 2021-09-06 - 2021-09-27 (Perihelion; Radial Alignment with PSP, STA)
    • 2021-12-04 - 2022-01-01 (start nominal mission phase, plentiful downlink)
  • Remote sensing synoptic programme (based on L_FULL_LRES_MCAD_Coronal-Synoptic SOOP definition with additional SPICE observations included) added during the following periods (affected instruments: EUI, Metis, PHI, SoloHI, SPICE, STIX):
    • 2021-08-30 - 2021-09-12 (close distance, prior to RSCW)
    • 2021-09-20 - 2021-10-11  (post RSCW, support BC Mercury Flyby; 180 degree field ambiguity resolution)
    • 2021-12-04 - 2022-01-01 (start nominal mission phase, assumed default synoptic programme)
  • Mercury moving through FSI FOV (2.63 Rsun) on 4 Oct, i.e. during the RS synoptics above. FSI may want to adjust the observations to take advantage of this opportunity.
  • Metis star calibration opportunities:
    • 2021-08-22 - 2021-08-26, τ Tauri
    • 2021-08-28 - 2021-08-30, HD36819
    • 2021-12-17 - 2021-12-26, θ Ophiuchi
  • Limb-pointing campaign (star) (following same format as alignment, TN-0035) for coordinated observations at quadrature between EUI/HRI, SPICE and Earth assets. Scheduled on 2021-08-17.
  • S/C roll campaign (star) requested by Metis to for determination of vignetting function. This involves a full revolution around S/C+X, split into 18 rolls of 20º, with a dwell time at each position of 30 minutes. In total this campaign will last about 14 hours, scheduled on 2021-08-31 to not interfere with RSCW4 and the high-priority scientific opportunities listed in the table below.
  • Cross- and inter-calibration opportunity with Earth-based assets, aligned with crossing the Earth-Sun line on 5 Nov 2021 (note this is during the NAV window, detailed timing TBC by flight dynamics). Data volumes currently placeholders (affected instruments: PHI, SPICE, Metis, EUI, SoloHI)
  • Both EUI and PHI plan to run a test annealing campaign at the end of Cruise phase, i.e. after RSCW4 (decision made by RSWG at SOWG#14). Moved to LTP5.
    • EUI input: This annealing campaign is meant to assess the detector degradation and in case of strong degradation, to foresee an annealing campaign preceded and followed by an onboard calibration to assess its efficiency. Ideally, this campaign would have a TM of 1900 MiB. If this is not feasible, we can limit the TM by taking subframes.
  • RS Instruments with internal memories can transfer extra TM to the SSMM after the RSCW4, to take advantage of good downlink performance close to Earth. Mainly applicable to LTP5

(star) Note that the coordinated offpointing campaigns and rolls need to be requested to MOC (flight dynamics) before LTP planning and timing/details cannot be changed anymore at time of Long Term Planning.

MLP: Changes from SWT27 (Oct 2020)

Since launch, comms performance has been found to be much better than baselined, so there is significant scope for extra activities. These were handled directly by the SOWG for LTP2 and LTP3, however for LTP4 the priorities for how to use the additional telemetry will be set by the SWT in line with the expected procedure for the nominal mission phase. The new level of available telemetry is summarised in the below plot. The decision taken by the SWT in order to use this Telemetry are reflected in the information above. This section is left here for context.

Note there will be some carry-over of data from LTP3, and the SSMM will need to be empty close to the EGAM to allow for repartitioning.

First priority will be given to completing any necessary calibration and characterisation campaigns, followed by addressing the science priorities decided by the SWT.

Table of Opportunities

This is a work in progress. Not all the opportunities described here may be addressed in the final operational plan. Those that have already been scheduled are included in the information above

Start DateEnd DateHeliocentric DistanceDescriptionInvolved InstrumentsConstraintsS/C manoeuvre required?
2021-07-012021-08-02
Cone geometry with BepiColombo

no
2021-08-032021-08-17
Support joint Bepi-SO Venus flybys (SO: 9 August, Bepi: 10 August)in-situ (TBC)VGAMno
2021-08-092021-08-09 +/- some weeks0.72 AU

Unique opportunity for science with PSP (best on 7-9 Aug for PSP perihelion), SOLO, BEPI, STEREO-A. SOLO & Bepi Venus flyby within a few days of each other.

PSP encounter will give radial and Parker alignments, also quadrature with SOLO & STEREO-A within a few days. RS observations in NAV window will be very important if this is possible. SOC will discuss with MOC.

All?

VGAM

(-20º roll)

no (in NAV window)
TBD

After Venus encounter?

or End RSCW4 / before EGAM?


MAG calibration rollsMAGTBC with flight dynamicsRolls
2021-08-12

2021-08-15


PSP spiral alignments for Solar Orbiter (for a 400 km/s wind)

In Situ


–20º rollno
2021-08-22

2021-08-25 


UV star calibration τ Tauri (context plot, times)

Too faint for SPICE and EUI.

Metis 

–20º rollno
2021-08-282021-08-30 

UV star calibration HD 36819 (context plot, times)

Too faint and too far from disk for SPICE and EUI.

Metis–20º rollno
2021-09-01

2021-09-30

(Full month of September)


Proposal to plan RS synoptics throughout the month to support linkage with IS data and alignments with other spacecraft.
–20º, 0º, +20ºno
2021-09-12

2021-09-12

~08:00


Solar Orbiter perihelion. Ideal opportunity for high cadence sequences of EUI, PHI, SPICE, ....

Ideal would be to adjust pointing reactively so we can link RS observations with IS measurements. This is the "dress rehearsal" in RSCW4.

All RS instruments

no roll (TBC by FD)

Off-point

2021-09-12


2021-09-20 


RSCW4 (8 days)


All

Nominal attitude required 
no SRP roll (TBC by FD)

Several campaigns involving Off-points
2021-09-172021-09-29
PSP-SO radial alignment  (also with STEREO-A for Sep 17-23)In Situ
no
2021-09-192021-09-26


Solar Orbiter at ideal angle to Earth to resolve 180º ambiguities in magnetic field

(S/C-Sun-Earth angle: 30º – 40º)

PHI + ...+20º rollno
2021-09-242021-10-080.6 AUBepiColombo Mercury flyby (1 Oct). Solar Orbiter is downstream of Mercury at the time.RS+20º rollno
2021-10-30

2021-10-30 (before NAV)

or closer to 27 Nov (better alignment but in NAV)

SOC will discuss proposed dates with MOC

New date 5 Nov

~0.75 AU

(up to 1 AU depending on date)

Cross- and inter-cal opportunity with Earth-based assets (~1 day needed, mainly driven by PHI heating and switching telescopes).
Last chance for RS Ops before Nav window (TBD if concept changes).

To be decided whether we want to plan a secured campaign right before NAV window, or better centred on the Earth-Sun line with risk of last-minute replanning due to a TCM being planned by flight dynamics. 

New date 5 Nov, close to crossing Earth-Sun line (~2 deg latitude angle remaining)

PHI, SPICE, EUI, Metis,

SoloHI

+20º roll

no

2021-12-172021-12-26

UV star calibration θ Ophiuchi (context plot, times)

Too far from disk for SPICE and EUI.

Metis
no
2021-12-04± a few days
Emptying of SSMM for re-partitioning.

no
2021-12-04

First month of NMP: Start of RS synoptic programme together with nominal IS science.All
no


Orbit plots courtesy of V. Andretta.

SOOP Kitchen plan

High-level (=MLP) plan of whole cruise:

Starting point for LTP04 planning in SOWG#17: https://solarorbiter.esac.esa.int/soopkitchen/#/planning/plan/LTP04_Jun2021-Sep2021/908 (bookmarked version used for pre-SOWG#17 simulation)

What’s changed since the end of the SOWG?

Following the intensive planning exercise, a few items have been tidied up and several simluations run so that we could arrive at a valid long-term plan in SOOP Kitchen:

  • Heat-Shield Door manoeuvres have now been agreed and placed
  • All resulting ATT_DIST and EMC_PREF_NOISY events have been generated
  • EMC_MAND_QUIET and IS_COORD BURST events have been placed. Note that on some days there is very little time free of EMC disturbances or thruster firings, so these have been placed as best we could, but the conditions may be less than ideal for usual use of these events
  • Roll manoeuvres for the CALIB_ROLL_RS campaign have been updated to take into account the fact that the S/C roll angle is –20º before and afterwards (S/C is tilted for calibration of solar radiation pressure on the solar arrays).
  • POINT_CENTRE no longer overlaps with the WOL at the beginning of the PTR window. In addition, note that the VSTP_UPDATEs represent the time of SLEWs to the to-be-updated pointings
  • HSDs are closed for Metis around the MAINT-ANY windows
  • FSI occulter-calibration campaign on 7th September moved to 9th September to de-conflict with SPICE HSD opening.
  • EUI event-detection campaign takes place on 8th July
  • L_FULL_LRES_MCAD_Coronal-Synoptic LF5_111 has been tidied up, such that observations don’t belong to two versions of the same, simultaneous SOOP (there had been a parallel LF5_112 which was redundant).

Released plan version

Final plan LTP04 (V2): https://solarorbiter.esac.esa.int/soopkitchen/#/planning/plan/LTP04_Jun2021-Sep2021 : Baseline 8 / version 2584.

Planning products V2 distributed on  via GFTS.



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