MITM11 | Synergies between space missions and ground-based observations

MITM11

Synergies between space missions and ground-based observations
Conveners: Abbie Donaldson, Colin Snodgrass | Co-conveners: Richard P. Binzel, Zuri Gray, Matthew M. Knight, Cecilia Tubiana
Orals FRI-OB2
| Fri, 12 Sep, 09:30–10:30 (EEST)
 
Room Neptune (rooms 22+23)
Posters THU-POS
| Attendance Thu, 11 Sep, 18:00–19:30 (EEST) | Display Thu, 11 Sep, 08:30–19:30
 
Finlandia Hall foyer, F94–98
Fri, 09:30
Thu, 18:00
Space missions to study bodies throughout the Solar System up-close have led to significant advances in understanding how our planetary system formed and evolved. A host of current and upcoming missions will further revolutionise our knowledge of the Solar System’s structure and history e.g. the characterisation of numerous Jupiter Trojans by the Lucy flybys, the Hera mission to assess the Didymos-Dimorphos system following the DART impact, and the first ever up-close study of a long period comet by Comet Interceptor. In addition to these small-body missions, there are missions flying or in development to visit all the major planets from Mercury to Jupiter, and discussions about future missions to the ice giants. Each of these missions are greatly enhanced by the support of ground-based facilities to provide necessary context through remote sensing and target characterisation. This session invites contributions from researchers undertaking telescopic observations related to mission targets, including pre-encounter characterisation, parallel ground and space observations, or follow up studies.

Session assets

Orals: Fri, 12 Sep, 09:30–10:30 | Room Neptune (rooms 22+23)

Chairpersons: Abbie Donaldson, Zuri Gray, Colin Snodgrass
09:30–09:42
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EPSC-DPS2025-866
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On-site presentation
Matthew M. Knight, Peter Scheirich, Petr Pravec, Joanna Thomas-Osip, Colin O. Chandler, Max Frissell, Harrison Agrusa, Steven R. Chesley, Tony L. Farnham, Julia de Leon, Petr Fatka, Rosita Kokotanekova, Michael Kueppers, Tim A. Lister, Nicholas A. Moskovitz, William J. Oldroyd, Cyrielle Opitom, Agata Rozek, Colin Snodgrass, and Cristina Thomas and the additional authors

On 2022 September 26, NASA's DART mission intentionally impacted Dimorphos, the moon of near-Earth asteroid (65803) Didymos, changing the binary system’s orbital period. The system was studied intensively from the ground over the ensuing months until February 2023 when its brightness and low solar elongation precluded further observations. These observations revealed a clear period change of 33 minutes due to the DART impact (Thomas et al. 2023). However, there is uncertainty on whether there was a single impulsive change in the orbital period resulting in a constant post-impact value, or if there is (or was) an evolution in the period with time as the system settled into a new configuration. Careful analysis of the full post-DART lightcurve dataset (through February 2023) showed that there was insufficient data to distinguish between constant or changing post-impact orbital periods (Naidu et al. 2024, Scheirich et al. 2024). 

In order to understand the final outcome of the DART mission, it is therefore critical to monitor the evolution of the Didymos system prior to the European Space Agency’s Hera mission arrival in late 2026. Observations from Hera will be too far removed from the time of impact to reveal whether or not the orbit period was changing over months as the asteroid system reached a new equilibrium. Our team obtained data during 2024 June to August on Magellan (6.5-m, PI: Thomas), SOAR  (4.1-m, Program ID 2024A-120042), NTT (3.6-m, PI: Snodgrass), and Faulkes Telescope South (2-m, PI: Lister), but poor weather at all sites plus Didymos’s positioning in front of the galactic plane throughout the visibility window prevented our analyses from attaining the needed sensitivity. The next visibility window occurred from late January through early March 2025, and our team was awarded time on Faulkes Telescope North (FTN, 2-m, PI: Lister), Lowell Discovery Telescope (LDT, 4.3-m, PI: Moskovitz), Palomar (5.1-m, PI: Chesley), Gemini-N (8.1-m, Program ID GN-2025A-Q-142), and Gran Telescopio Canarias (GTC, 10.4-m, PI: de Leon). 

Here we report on Gemini-N observations obtained on 2025 February 24, 26, and 28 when Didymos was at an apparent V magnitude about 20.3. The GTC observing run was weathered out. Observations acquired with FTN, LDT, and Palomar were successfully acquired, but are still being analyzed. Our Gemini observations were timed to optimize coverage of the Didymos binary orbit within the run and to provide complementary observations with neighboring runs scheduled on Palomar and GTC. We observed Didymos for 3.7 hr at the start of each night using the SDSS-i filter. We tracked at the sidereal rate and limited individual exposure times to 20 sec to keep the asteroid’s trailing from significantly exceeding the stellar point spread function. Images were processed using the Gemini DRAGONS pipeline (Labrie et al. 2023) and photometry was measured using Photometry Pipeline (Mommert 2017). After manually removing frames that were contaminated by nearby stars or other image artifacts, lightcurve deconvolution was performed using the binary asteroid lightcurve decomposition method as earlier Didymos datasets (Pravec et al. 2022, 2024). 

Our preliminary analysis finds that mutual events occurred about 70 min earlier than the nominal prediction (see Figure 1), a difference of 1.6-sigma. This yields a binary orbital period of 11.3667 +/- 0.0002 hr (3-sigma), assuming that the period has been constant since 2022/2023. With the much longer time baseline, these observations reduce the uncertainty in the binary period by about a factor of 6 compared to the previously published 3-sigma measurement of 11.3675 +/- 0.0012 hr (Scheirich et al. 2024). As expected, the data quality was insufficient to constrain Dimorphos’ rotation (which needed rms residuals of 0.004-0.007 mag, while residuals of 0.017 mag were obtained). Deep stacking of all images collected on a night did not reveal evidence of a tail or any remaining large fragments, though we have not yet quantified these non-detections. 

We will provide updated results on the full 2025 dataset. If ongoing analyses of the FTN, LDT, and/or Palomar datasets yield sufficiently small rms residuals, the lightcurve deconvolution will be re-run on the larger dataset, though the solution is not expected to change appreciably. The question of whether or not the orbital period has changed or if the apparently shorter period is just a statistical fluke is unlikely to be resolved from these data since they were all acquired relatively close to the Gemini observations. We plan to propose for similar observations during Didymos’s next apparition in 2026 July to attempt to resolve this question.

Acknowledgements: The work at Ondřejov has been supported by the "Praemium Academiae" award by the Academy of Sciences of the Czech Republic, grant AP2401.

References 

  • Labrie et al., RNAAS 7, id.214 (2023)
  • Mommert, M. Astronomy & Computing 18, 47 (2017)
  • Naidu et al., PSJ 5, 74 (2024)
  • Pravec et al., PSJ 3, 175 (2022)
  • Pravec et al., Icarus 418, id.116138 (2024)
  • Scheirich et al., PSJ 5, 17 (2024)
  • Thomas et al., Nature 616, 448 (2023)

Figure 1: Decomposition of Didymos system lightcurve from 2025 February 24-28 (a) into signals from mutual events (b), and primary rotation (c). The top panel (a) shows the combined lightcurve over 11.37 hr. The full lightcurve can be decomposed into a contribution from the 2.260-hr rotation of Didymos (bottom panel c) and a contribution due to mutual events. The mutual events are indicated by horizontal lines underneath the lightcurve in panel (b). The blue lines are the observed mutual events (PE = primary eclipse, PO = primary occultation, SE = secondary eclipse, SO = secondary occultation), while the red lines are the nominal predictions of these same events from Scheirich et al. (2024), which occurred ~70 minutes later than observed.

 

How to cite: Knight, M. M., Scheirich, P., Pravec, P., Thomas-Osip, J., Chandler, C. O., Frissell, M., Agrusa, H., Chesley, S. R., Farnham, T. L., de Leon, J., Fatka, P., Kokotanekova, R., Kueppers, M., Lister, T. A., Moskovitz, N. A., Oldroyd, W. J., Opitom, C., Rozek, A., Snodgrass, C., and Thomas, C. and the additional authors: Ground-based observations of (65803) Didymos 2.5 years after the DART impact: searching for ongoing evolution, EPSC-DPS Joint Meeting 2025, Helsinki, Finland, 7–13 Sep 2025, EPSC-DPS2025-866, https://doi.org/10.5194/epsc-dps2025-866, 2025.

09:42–09:54
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EPSC-DPS2025-1138
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Virtual presentation
Ground Based Follow-up Observations to Expand the Science Return of Near-Earth Object Surveyor
(withdrawn)
Tyler Linder, Jana Pittichová, Joe Masiero, Steve Chesley, Garrett Levine, Amy Mainzer, and the NEO Surveyor Team
09:54–10:06
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EPSC-DPS2025-1454
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On-site presentation
Toni Santana-Ros, Przemysław Bartczak, Karri Muinonen, Agata Rożek, Thomas Müller, Masatoshi Hirabayashi, Davide Farnocchia, Marco Micheli, Richard Cannon, Marina Brozović, Olivier Hainaut, Dagmara Oszkiewicz, Anne Virkki, Lance Benner, Adriano Campo Bagatin, Paula Benavidez, Antonio Cabrera-Lavers, Clara Martínez-Vázquez, and Kathy Vivas

Summary

Asteroid 1998 KY26 is a decametre-sized, rapidly rotating body that has been selected as a target for the extended Hayabusa2# mission. Understanding its physical properties is crucial for optimizing mission planning, as it presents both challenges and opportunities for asteroid exploration. This study[1] provides a detailed characterization of 1998 KY26 using a combination of new optical photometric data and radar observations, extending previous analyses of the asteroid’s size, spin state, shape, and surface composition[2]. Our results offer new insights into the asteroid's structure and dynamics and highlight the importance of integrating diverse observational techniques to refine the models for small asteroid behavior and non-gravitational forces.

Observational Data and Methodology

Our new observations were gathered during the 2024 apparition with the GTC, Gemini South, VLT and Blanco telescopes. For our study, we incorporated the photometric and radar data collected in 1998. Optical data covered a wide range of phase angles to allow for accurate determination of the asteroid's albedo and surface properties. Additionally, the 2024 close approach offered an opportunity to examine potential non-gravitational forces, such as outgassing, which could influence the asteroid's trajectory.

Lightcurve inversion techniques were applied to the optical data to refine the asteroid's spin period and shape. The combination of radar data and lightcurve inversion models allowed us to generate a three-dimensional model of 1998 KY26 and derive its size, surface properties, and taxonomic classification.

Results

Spin Period One of the primary results of this study is a revised spin period for 1998 KY26 of 5.35 minutes, significantly shorter than the previously reported value of 10.7 minutes (Figure 1). The reduced spin period is consistent with the asteroid's small size and relatively high rotational stress, which is expected for bodies of this scale.

Figure 1: Lightcurve analysis of 1998 KY26 showing the revised spin period of 5.35 minutes, with a comparison to the previous model from Ostro et al. 1999[2].

 

Size and Shape

Using the revised spin period and lightcurve data, we derived convex and non-convex shape models which indicates that 1998 KY26 is an irregular, slightly elongated body.

We used the new models to fit the 1998 radar data (Figure 2), leading to an updated diameter estimate of 11±2 meters (see Figure 2), which is significantly smaller than the previously reported value of approximately 30 meters. The asteroid’s small size presents unique challenges for spacecraft exploration, particularly in terms of navigation and surface operations.

Figure 2: Rebinned Doppler-only (cw) observations of 1998 KY26 collected on 8 June 1998, compared with synthetic echoes generated using models derived with lightcurve-inversion methods.

Surface Albedo and Composition

From the combination of optical photometric data at multiple phase angles and radar observations, we derived a geometric albedo of 0.52±0.08. This high albedo is consistent with that observed in enstatite-rich, Xe-type asteroids, which are known for their bright surfaces.

Impact on Mission Planning

The new spin period, size, and surface properties of 1998 KY26 have significant implications for the extended Hayabusa2# mission. The smaller size of the asteroid will necessitate adjustments to the mission's approach and landing strategies. Additionally, the revised spin period and irregular shape mean that precise navigation will be critical to ensure safe operations near the asteroid.

Conclusion

This study provides a comprehensive physical characterization of asteroid 1998 KY26 using a variety of observational techniques. Our results indicate that 1998 KY26 is a small, rapidly rotating body with an irregular shape and a high albedo, consistent with an enstatite-rich composition. We revised its spin period to 5.35 minutes and determined its diameter to be 11±2 meters, which is significantly smaller than previous estimates. We also found no evidence of non-gravitational forces acting on the asteroid, such as outgassing, during the 2024 close approach. These findings provide critical insights into the physical properties of 1998 KY26 and will inform mission planning for the Hayabusa2# spacecraft. Further studies, particularly with regard to non-gravitational forces and surface properties, will be essential for refining our understanding of small, fast-rotating asteroids.

References

[1] Toni Santana-Ros, Przemyslaw Bartczak, Karri Muinonen et al., "Hayabusa2# mission target 1998 KY26 preview: a small optically bright rapid rotator", 21 January 2025, PREPRINT (Version 1) available at Research Square [https://doi.org/10.21203/rs.3.rs-5821856/v1]

[2] Ostro, S. J., “Radar and Optical Observations of Asteroid 1998 KY26”, Science, vol. 285, pp. 557–559, 1999. doi:10.1126/science.285.5427.557.

How to cite: Santana-Ros, T., Bartczak, P., Muinonen, K., Rożek, A., Müller, T., Hirabayashi, M., Farnocchia, D., Micheli, M., Cannon, R., Brozović, M., Hainaut, O., Oszkiewicz, D., Virkki, A., Benner, L., Campo Bagatin, A., Benavidez, P., Cabrera-Lavers, A., Martínez-Vázquez, C., and Vivas, K.: Hayabusa2# mission target 1998 KY26 preview: a small optically bright rapid rotator, EPSC-DPS Joint Meeting 2025, Helsinki, Finland, 7–13 Sep 2025, EPSC-DPS2025-1454, https://doi.org/10.5194/epsc-dps2025-1454, 2025.

10:06–10:18
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EPSC-DPS2025-1683
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ECP
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On-site presentation
Helen Usher, Colin Snodgrass, Andrew Norton, Simon Green, Paul Roche, Sally Jordan, Tony Angel, Richard Miles, and Ben Wooding

Amateur astronomers make useful contributions to many areas of astronomy.  For comets, they can add temporal coverage and multi-scale observations which aid the study of fast-changing, and large-scale features. 

The Halley, Deep Impact and Rosetta comet Missions all included amateur campaigns as part of their wider ground-based observing campaigns.  Amateur observations can particularly add value when the viewing geometry is unfavourable for larger telescopes eg at small solar elongation, and (due to the worldwide spread of amateurs) when observing windows are small.

We will present the results of an analysis of the effectiveness of these campaigns, particularly the Rosetta Amateur Observing Campaign, and lessons and recommendations for action for future campaigns (Usher et al 2022). 

The analysis of the Rosetta professional and amateur campaign data shows that around the critical period of the perihelion of comet 67P there were 15 days when the only observations available were from amateur observers.

The lessons for future campaigns include the need for: clarity of objectives; recognising the wider impact campaigns can have on increasing science capital; clear, consistent, timely and tailored guidance; easy upload procedures with in-built quality control; and, regular communication, feedback and recognition.

We have been working with the Pro-Am comet community to implement these recommendations and we will report progress and outstanding work (Usher et al 2022).

Astronomy is recognised as an effective point of engagement for students of all ages, inspiring curiosity and providing a stimulus to learn and exciting context for developing skills (Salimpour et al. 2021).  Linking student learning with space missions can add an extra dimension.

We will present our experience of working with educators, supported by professional and amateur astronomers, to use observing campaigns to engage, educate, inspire and raise the aspirations of students.  This will include a case study of observations and activities linked to the DART Mission (Usher et al .  2023, Lister et al 2024).

Salimpour, S., Bartlett, S., Fitzgerald, M.T. et al. The Gateway Science: a Review of Astronomy in the OECD School Curricula, Including China and South Africa. Res Sci Educ 51, 975–996 (2021)

Usher, H., Snodgrass, C., Biver, N., Kargl, G., Tautvaišienė, G., James, N., Walter, F., and Černý, J.: Strengthening Pro-Am Comet Community Cooperation: Report on Europlanet Pro-Am Workshop (10-12 June 2022)  , Europlanet Science Congress 2022, Granada, Spain, 18–23 Sep 2022, EPSC2022-1135, https://doi.org/10.5194/epsc2022-1135, 2022

Usher, H., Snodgrass, C., Green, S.F., Norton, A., Roche, P.,   Seeing the Bigger Picture: Rosetta Mission Amateur Observing Campaign and Lessons for the Future 2020 Planet. Sci. J. 1 84 DOI 10.3847/PSJ/abca46

Usher, H., Stoddard-Jones, I.C. , Roche, P.D., Snodgrass, C., Wooding, B., and Lister, T.,  Using Killer Asteroids to Engage Children in Astronomy and Science (Planetary Defence Conference, April 2023)

Lister, T., Constantinescu, C., Ryan William, Ryan, E., Gomez,E., Phillips, L., Rożek, A., Usher, H., Murphy, B. P., Chatelain J., Greenstreet, S., 2024 Planet. Sci. J. 5 127

How to cite: Usher, H., Snodgrass, C., Norton, A., Green, S., Roche, P., Jordan, S., Angel, T., Miles, R., and Wooding, B.: Pro-Am-Schools Observing Campaigns in Support of Space Missions and the  Broader Study of Small Bodies, EPSC-DPS Joint Meeting 2025, Helsinki, Finland, 7–13 Sep 2025, EPSC-DPS2025-1683, https://doi.org/10.5194/epsc-dps2025-1683, 2025.

10:18–10:30
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EPSC-DPS2025-1789
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ECP
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Virtual presentation
Anastasia Kokori

Ground based telescopes have been proven efficient enough for successful follow-up observations of exoplanets for more than 20 years now. In the field of exoplanets we have entered the era of characterisation, where the confirmation of exoplanets is not enough. The ExoClock project - www.exoclock.space – aims to monitor regularly transiting exoplanets for the Ariel space mission by integrating observations coming both from space and ground-based telescopes. The goal of the project is the delivery of a homogenous catalogue with the exoplanet parameters to increase the mission efficiency, supporting the ultimale goal of exoplanet characterisation with large telescopes. The project is part of the ephemerides working group of ESA's Ariel space mission and counts already 6 years in operation. In this effort we are actively collaborating with both professional and amateur astronomers coming from various countries around the world using snall, medium or larger scale telescopes. This presentation will highlight the capabilities of ground telescopes and how they can become valuable for exoplanet studies and space missions in this new era of characterisation. More specifically, I will talk in detail about the organisation of the project and the main tools used to achieve an efficient international collaboration. I will also present the status of the project and the results of the publications we have produced so far which include the update of 620 exoplanet ephemerides. Our research includes a collective analysis of observations acquired by both space telescopes (TESS, Kepler) and ground telescopes belonging to profeesional and amateur astronomers. This data is used to update the ephemerides of exoplanets that are candidates for the Ariel space mission. The ExoClock network currently consists of more than 2000 participants, a fact that highlights the significant aspect of collaborations in large scale research programs. The talk will end with lessons learned and how the integrated and collaborative approach of the project advances exoplanet observations and techniques.

 

How to cite: Kokori, A.: Integrating data from ground-based and space telescopes to support future space missions in the new exoplanet era: The case of the ExoClock project , EPSC-DPS Joint Meeting 2025, Helsinki, Finland, 7–13 Sep 2025, EPSC-DPS2025-1789, https://doi.org/10.5194/epsc-dps2025-1789, 2025.

Posters: Thu, 11 Sep, 18:00–19:30 | Finlandia Hall foyer

Display time: Thu, 11 Sep, 08:30–19:30
F94
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EPSC-DPS2025-377
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Virtual presentation
Multi-interferometric Investigation of Outer Planets Magneto-bremsstrahlung Radiation in Support of Planetary Exploration
(withdrawn)
Daniel Santos-Costa, Bryan Butler, Imke de Pater, Quentin Nénon, Nicolas André, Hajime Kita, Anil Bhardwaj, Corentin K. Louis, Julien Girard, Laurent Lamy, Oleg Smirnov, and Nickolay Ivchenko
F95
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EPSC-DPS2025-670
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On-site presentation
Elena Mazzotta Epifani, Livio Agostini, Pasquale Palumbo, Cecilia Tubiana, Federico Tosi, Alice Lucchetti, Maurizio Pajola, Ivano Bertini, and Elisabetta Dotto

The ESA JUICE mission. ESA’s Jupiter Icy Moons Explorer (JUICE) [1] has been successfully launched from Europe's Spaceport in French Guiana on April 14th, 2023. A suite of remote sensing, geophysical and in situ instruments are accommodated onboard, with the aim to i) explore Jupiter’s complex environment in depth, ii) study the wider Jupiter system as an archetype for gas giants across the Universe, and iii) characterize in detail the three large ocean-bearing moons (Ganymede, Callisto and Europa), as both planetary objects and possible astrobiological habitats. Before reaching the Jovian system in July 2031, JUICE will cruise ~8 years inside the inner Solar System (see Figure 1), performing 4 planetary fly-bys (the first one ever attempted with both the Moon and Earth, then with Venus and two more with Earth). JUICE instrument operations during such fly-bys are heavily constrained for technical reasons and to give full priority to navigation and mission safety. Nevertheless, such events are good opportunities to perform calibration checks and experience typical fly-by operations that will be undertaken with Galilean satellites. In addition to these planned fly-bys, the JUICE spacecraft will be routinely operated in specific time windows to perform instruments and probe “checkout operations” (see Figure 2). In particular, some of these “checkout windows” without attitude constraints (i.e., above 1.4 AU Sun distance) can be exploited to optimize observation of small bodies of our Solar System, in view of similar observations to be performed on minor targets in the Jupiter system. These data will therefore increase the scientific output of the whole mission at no resources expense, by properly choosing the pointing towards targets of planetary interest. These observations, if properly planned, could significantly contribute to explore the Cosmic Vision’s main theme “How does the Solar System work?”

 

The JANUS instrument onboard JUICE. The JANUS (Jovis, Amorum ac Natorum Undique Scrutator) instrument [2] onboard JUICE is the multispectral camera enabling imaging in the 340-1080 nm wavelength range. JANUS allows  imaging of many different targets: from the icy satellites, to Io, to small inner and irregular moons, the rings and Jupiter itself. While in the Jupiter system, the JUICE trajectory will allow icy Galilean satellites observations down to closest approaches of a few hundred km, resulting in spatial sampling  up to a few m/pixel. All the other targets will be observed from distances above a few 105 km, i.e. spatial sampling above several km/pixel. 13 filters from the near ultraviolet to the near infrared will guarantee good spectral coverage with bandwidths from several tens of nm down to 10 nm.

 

Science during checkout windows and coordination with ground-based campaigns. We propose to exploit the checkout windows during the JUICE cruise phase to perform cometary science with JANUS, adding no cost science to the plans of testing instrument’s capability to detect faint sources (representative for exospheres and rings in Jupiter system) and to characterize unresolved objects (representative for Jupiter small moons). Among small bodies orbiting our Solar System, comets are thought to provide the most direct information on how planets form in all protoplanetary disks [3]. The observation of comets provides key information to investigate the processes of formation and evolution of pebbles forming planetesimals at different heliocentric distance of the primordial Solar Nebula, the pebbles themselves probably originating from different regions of the solar protoplanetary disk [4]. JANUS checkout pointing campaigns of comets of several dynamical groups could allow these targets to be observed at phase angles (i.e., angle Sun-Target-Observer) hardly available from Earth. In particular, optical imagery of cometary coma as a function of phase angle has a key importance in investigating the intimate nature of cometary dust [5]: size, size distribution, shape, and composition of dust particles can be investigated by means of observations taken in different broadband filters as those potentially provided by JANUS, and by means of comparison with data obtained e.g. with ground-based telescopes, with different observing geometries.

 

Here we present the results of a “test” we performed for the Checkout #4, foreseen for the week of 23 February 2026, where the Pointing Campaign #1 will be executed and the spacecraft pointing will not undergo strict thermal constraints as during cruising in the inner Solar System. To this aim, we designed a specific tool, J-SCOUT (Search for Cruise-phase Observation Utility Tool) [6] to query the JPL Horizon database [7] and take an “instant picture” of the small bodies complex within the Solar System at the checkout date(s), considering the latest Consolidated Report on Mission Analysis (CreMA 5.0b23) as the baseline mission profile. We designed the possibility to limit the query to the “active bodies” (as defined in the JPL Horizon Database), resulting in investigations of comets pertaining to 6 different dynamical categories. This allowed us to derive a list of potential “campaign cometary targets” for Checkout#4, which will be used as a “testbed” for such an operational plan, aimed at nominal instrument functional and performance verification activities during cruise. The Checkout #4 outcomes will be used to prepare for next checkout(s), for which J-SCOUT will be used to obtain a new list of “JUICE targets” that will be proposed for a campaign of quasi-contemporary, possibly multi-telescope ground-based observations, hence enhancing the synergy among space missions and ground-based telescopes.

 

References. [1] Grasset et al., 2013, PSS 78, 1. [2] Palumbo P. et al., 2025, SSR 221, 3, id. 32. [3] Blum J. et al., 2017, MNRAS 469: S755-S773. [4] Fulle M., 2021, MNRAS: 505, 2, 3107-2112. [5] Bertini et al., 2017, MNRAS 469, S404; [6] Agostini et al., 2022, PSS 216, 105476. [7] https://ssd.jpl.nasa.gov/horizons/

Figure 1 – Trajectory of JUICE spacecraft through the inner Solar System, before reaching Jupiter system in July 2031. The yellow stars show the Earth gravity assists and the Venus fly-by. The grey circular band show the extension of the asteroid Main Belt extension.

Figure 2 – JUICE mission profile (heliocentric and geocentric distance) with periodic payload checkout (including the pointing campaigns)

How to cite: Mazzotta Epifani, E., Agostini, L., Palumbo, P., Tubiana, C., Tosi, F., Lucchetti, A., Pajola, M., Bertini, I., and Dotto, E.: Exploit each Occasion: Making Science at Performance Checks with the JANUS Instrument onboard ESA/JUICE S/C during its Cruise towards Jupiter, EPSC-DPS Joint Meeting 2025, Helsinki, Finland, 7–13 Sep 2025, EPSC-DPS2025-670, https://doi.org/10.5194/epsc-dps2025-670, 2025.

F97
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EPSC-DPS2025-951
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Virtual presentation
Boncho Bonev, Geronimo Villanueva, Neil Dello Russo, Michael Disanti, Sara Faggi, Ronald Vervack, Erika Gibb, Hideyo Kawakita, Hitomi Kobayashi, Lori Feaga, Manuela Lippi, Tilak Hewagama, Mohammad Saki, Nathan Roth, Younas Khan, Yinsi Shou, and Michael Combi

Comet research has been a high priority in solar system exploration. The last two decades have witnessed three spacecraft missions to short-period comets (Stardust / NExT, Deep Impact / EPOXI, and Rosetta) as well as tremendously increased capabilities of astronomical remote sensing facilities. The primary motivation for  these extensive studies has been the need to understand comets as remnants from the protosolar nebula. These objects retain the volatiles (ices) from the cold regions in the protosolar disk, where they formed. Deciphering this cosmogonic heritage requires a strong synergy between mission findings and remote-sensing observations. Missions explore specific comets at unprecedented levels of detail that cannot be gained by other means. Whereas missions are necessarily restricted to only a few targets, remote sensing observations study comets as a population. This includes objects with a wide range of dynamical histories, nucleus sizes and shapes, gas production rates, and inner coma parent volatile compositions. 

This presentation is focused on the close and continually evolving synergy between missions and remote sensing near-infrared (near-IR) spectroscopic measurements of cometary volatiles. The near-IR samples a suite of molecules, such as CH4, C2H2, C2H4, C2H6, NH3, HCN, CO, OCS, H2CO, CH3OH, and CO2 (from space only). It also provides the easiest way to simultaneously measure H2O (the most abundant coma gas in most active comets) from the ground through its non-resonant fluorescence lines. In whole or in part these species are considered parent volatiles – those originally stored as ices in cometary nuclei. Abundances of isotopologues (e.g., HDO, CH3D) can be constrained in exceptionally bright comets.

Previous missions to short-period comets, especially Deep Impact / EPOXI and Rosetta, demonstrated the importance of ground-based near-IR observations of parent volatiles for pre-encounter characterization, parallel spacecraft and Earth-based measurements, or follow-up astronomical studies [1-11]. Extending this synergy, the Comet Interceptor mission (targeting a long-period comet [12]) can be supported by the modern near-IR spectrographs now operating at the NASA Infrared Telescope Facility, W. M. Keck Observatory, European Southern Observatory, and Gemini. These ground-based facilities offer high spectral resolving power, allowing emission lines from different molecules to be distinguished and establishing volatile abundances with unprecedented sensitivity. Examples of particular avenues for integration with mission results include:

1.    Detailed compositional measurements with emphasis on relative coma abundances among species (for example, C2H2/C2H6, CO/H2CO/CH3OH, NH3/H2O, etc.).

2.    Spatially resolved measurements of volatile column densities and gas rotational temperatures. These are diagnostic of the physical conditions in the inner collisional coma (to which near-IR observations are most sensitive), and to the role of various dynamic and thermodynamic processes that shape the coma environment. 

3.    Spatial studies also provide insights into heterogeneous outgassing and the sources of volatile release – directly from the nucleus versus release from icy grains ejected into the coma. Physical coma models [13] have been developed to evaluate the contributions of both nucleus and extended sources. Previously validated against EPOXI, Rosetta, and ground-based data, these models can be applied to the vastly different spatial scales and observing geometries of spacecraft measurements versus simultaneously or contemporaneously obtained ground-based data, thereby enabling unified interpretation of both.

4.    As done for the EPOXI target 103P/Hartley 2 [6], a near-IR spectral survey would provide a complete inventory of all emission lines detected in the L-band. Through comparison with molecular fluorescence models and available laboratory spectra, emission lines can be identified by measured frequency, intensity, and quantum assignment, and included in a database available to both mission and ground-based researchers.

In addition to providing direct mission support, telescopic near-IR measurements serve as a “bridge” between detailed findings on specific mission targets and taxonomic studies of a larger number of comets using established and uniformly implemented remote sensing techniques.

References

[1] Mumma et al. 2005, Science, 310, 270
[2] DiSanti et al. 2007, Icarus, 187, 240
[3] Dello Russo et al. 2014, Icarus, 238, 125
[4] Mumma et al. 2011, ApJ Letters, 734, L7
[5] Dello Russo et al. 2011, ApJ Letters, L8
[6] Dello Russo et al. 2013, Icarus, 222, 707
[7] Kawakita et al. 2013, Icarus, 222, 723
[8] Bonev et al. 2013, Icarus, 222, 740
[9] Feaga et al. 2023, LPI Contributions 2851, 2476
[10] Bonev et al. 2023, Astron. Journal, 166, 233
[11] Shou et al. 2024, AAS/DPS Meeting, 56, abstract 401.04
[12] Jones et al. 2024, Space Science Reviews, 220, 9
[13] Tenishev et al. 2024, Frontiers in Astron. and Space Sci., 11, 1484360

How to cite: Bonev, B., Villanueva, G., Dello Russo, N., Disanti, M., Faggi, S., Vervack, R., Gibb, E., Kawakita, H., Kobayashi, H., Feaga, L., Lippi, M., Hewagama, T., Saki, M., Roth, N., Khan, Y., Shou, Y., and Combi, M.: From Deep Impact to the Comet Interceptor: Integrating ground-based near-infrared spectroscopic measurements of volatiles with spacecraft cometary missions, EPSC-DPS Joint Meeting 2025, Helsinki, Finland, 7–13 Sep 2025, EPSC-DPS2025-951, https://doi.org/10.5194/epsc-dps2025-951, 2025.

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EPSC-DPS2025-1129
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On-site presentation
The Near-Earth Object Surveyor: NASA’s Next Planetary Defense Mission
(withdrawn)
Amy Mainzer, Bonnie Buratti, Jana Chesley, Serina Diniega, Josh Emery, Garrett Levine, Tyler Linder, and Joseph Masiero and the Near Earth Object Surveyor Team