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Mission record

Rosetta

ESA, DLR, CNES · Launched

Explore trajectory

Completed · Success

ESA's Rosetta was the first mission to rendezvous with a comet, the first to follow one around the Sun, and the first to deploy a lander to a comet's surface. Launched 2 March 2004 on an Ariane 5 G+ from Kourou, it used three Earth gravity assists and one Mars gravity assist, flew past asteroids Steins and Lutetia, hibernated for 31 months, and arrived at Comet 67P/Churyumov-Gerasimenko on 6 August 2014. It released the Philae lander on 12 November 2014 and ended with a controlled descent onto the comet on 30 September 2016.

Destinations
Launch vehicle
Ariane 5 G+
Launch site
Kourou, French Guiana
Countries
Austria, Finland, France, Germany, Hungary, Ireland, Italy, United Kingdom, United States
Mission types
Orbiter, Lander, Flyby

Chronology

Mission timeline

  1. Launch

    Launch on Ariane 5 G+ from Kourou

    Rosetta launched on 2 March 2004 at 07:17 UT on an Ariane 5 G+ from Europe's spaceport at Kourou, French Guiana.

    Earth
  2. Gravity assist

    First Earth gravity assist

    First of three Earth gravity assists used to shape the trajectory toward Comet 67P/Churyumov-Gerasimenko.

    Earth
  3. Gravity assist

    Mars gravity assist

    The only Mars gravity assist of the mission, one of four gravity-assist manoeuvres (three Earth, one Mars) en route to the comet.

    Mars
  4. Gravity assist

    Second Earth gravity assist

    Earth
  5. Flyby

    Flyby of asteroid (2867) Steins

    2867 Steins
  6. Gravity assist

    Third Earth gravity assist

    Earth
  7. Flyby

    Flyby of asteroid (21) Lutetia

    21 Lutetia
  8. Milestone

    Enters deep space hibernation

    Rosetta was placed in deep space hibernation for the coldest, most distant leg of its cruise.

  9. Milestone

    Exits deep space hibernation

    Rosetta woke from 31 months of hibernation and resumed operations ahead of the comet rendezvous manoeuvres of May-August 2014.

  10. Milestone

    Rendezvous with Comet 67P/Churyumov-Gerasimenko

    Rosetta became the first spacecraft in history to rendezvous with a comet, arriving 100 km from the nucleus after ten years, five months and four days of travel covering 6.4 billion kilometres and five loops around the Sun.

    67P/Churyumov-Gerasimenko
  11. Deployment

    Philae released from Rosetta

    Deployment of the Philae lander was confirmed at 09:03 GMT (10:03 CET) on 12 November 2014 at a distance of 22.5 km from the centre of the comet, beginning a roughly seven-hour descent.

    67P/Churyumov-Gerasimenko
  12. Landing

    Philae lands on Comet 67P/Churyumov-Gerasimenko

    The first soft landing on a comet. The signal confirming successful touchdown arrived on Earth at 16:03 GMT (17:03 CET) on 12 November 2014, at a landing site named Agilkia on the head of the double-lobed nucleus. The anchoring harpoons did not fire and Philae made contact with the surface three times, rebounding from Agilkia before coming to rest at a site later named Abydos on the comet's smaller lobe.

    67P/Churyumov-Gerasimenko
  13. Loss of contact

    Philae falls silent as its primary battery is exhausted

    Philae completed 80% of its planned first science sequence before falling into hibernation in the early hours of 15 November 2014 when the primary battery was exhausted.

    67P/Churyumov-Gerasimenko
  14. Milestone

    Philae wakes from hibernation and contacts Earth

    Signals from Philae were received at ESA's European Space Operations Centre in Darmstadt at 22:28 CEST on 13 June 2015. Philae 'spoke' with its team for 85 seconds, via Rosetta, in the first contact since going into hibernation in November 2014.

    67P/Churyumov-Gerasimenko
  15. Milestone

    Comet 67P reaches perihelion with Rosetta escorting it

    Closest approach to the Sun for Comet 67P/Churyumov-Gerasimenko, observed by Rosetta from close quarters.

    67P/Churyumov-Gerasimenko
  16. Milestone

    Philae located in Rosetta imagery

    Rosetta's OSIRIS narrow-angle camera imaged Philae wedged into a dark crack on the comet at Abydos on the smaller lobe, less than a month before the end of the mission.

    67P/Churyumov-Gerasimenko
  17. Mission end

    Controlled descent onto the comet ends the mission

    Rosetta carried out its final manoeuvre the previous night at 20:50 GMT (22:50 CEST), setting it on a collision course with the comet from an altitude of about 19 km, targeting a region on the small lobe close to a region of active pits in the Ma'at region. Confirmation of the end of the mission arrived at ESA's control centre in Darmstadt at 11:19 GMT (13:19 CEST) with the loss of Rosetta's signal upon impact.

    67P/Churyumov-Gerasimenko

Mission architecture

Vehicles

  • Rosetta orbiter · Orbiter · Ended mission with a controlled descent onto the comet on 30 September 2016; launch mass 2900 kg including 1670 kg propellant and 165 kg science payload

    Destinations: 67P/Churyumov-Gerasimenko, Earth, Mars, 2867 Steins, 21 Lutetia

    • Philae · Lander · Landed 12 November 2014 at Agilkia, bounced and came to rest at Abydos; hibernated 15 November 2014, briefly re-contacted 13 June 2015, imaged in place 2 September 2016. Mass 100 kg

      Destinations: 67P/Churyumov-Gerasimenko

Trajectory record

Precise trajectory

Sun-centred J2000 states sampled offline from NASA/JPL NAIF SPICE kernels with geometric (NONE) aberration correction, using the Rosetta orbiter's reconstructed cruise ephemeris ORHR_______________00122.BSP - the ESA/ESOC solution the archive describes as spanning the cruise phase from launch to the comet rendezvous manoeuvre, and as superseding all earlier versions - with the Martian system ephemeris MAR097_030101_170101_V0001.BSP furnished for Mars's own body centre, which DE440s does not carry (it holds the Mars system barycentre alone), and DE440s furnished last so planetary positions match the committed body ephemerides. Sampling is weekly across the cruise and tightens to 60 s within six hours of the Mars closest approach. The record covers only the cruise phase, from the kernel's first tracked state about two hours after launch to 2014-08-04, some seventy-five minutes before that kernel's coverage ends and two days before the arrival at Comet 67P/Churyumov-Gerasimenko this record's events describe. The comet phase is deliberately not included: it lives in separate orbit-determination files whose own archive documentation warns that they and their companion comet ephemerides carry one-second discontinuities within which the relative orbit between spacecraft and comet is significantly wrong, and a rendezvous has no closest approach for this pipeline's encounter model to find. The single committed encounter is the 25 February 2007 Mars gravity assist, the mission's only planetary swing-by that was not of Earth. Its published figure is a pericentre radius rather than an altitude, and the source distinguishes the two itself: Budnik and Morley's ESA/ESOC navigation paper gives the nominal pericentre altitude as 250 km above the surface of Mars in its introduction, and its table of swing-by parameters as determined after the swing-by gives a Pericentre Radius of 3648.084 km. The two readings are 3,396 km apart - Mars's own equatorial radius, read from the same pck00011.tpc this dataset furnishes - so which one is meant is not a rounding question: the computed centre distance of 3,649.087 km sits 1.003 km from the radius reading and 3,395 km from the altitude reading. The paper's own printed osculating elements agree, since its semi-major axis of -551.986 km and eccentricity of 7.609013 give a conic pericentre of 3648.083 km about the focus, which is Mars's centre of mass. The epoch comes from a second source rather than that one, because the paper prints the pericentre passage in TDB (01:59:04.46) and this catalogue records UTC; ESA's own Rosetta status report for May 2007 gives 1:57:59 UTC, and converting the paper's TDB instant through the furnished leapseconds kernel lands on 01:57:59.275 UTC, so two independently published epochs agree to 0.3 s. The computed closest approach falls at 01:57:59.305 UTC. The remaining 1.003 km of distance difference is accounted for rather than unexplained. The same archive also ships ORMR_______________00052.BSP, the dedicated Mars-flyby solution ESOC delivered four days after the swing-by, and that file reproduces the published 3648.084 km to 0.0004 km, which most likely makes it the orbit determination the published table was computed from - an inference from the kernel's own creation date and that agreement, since the paper names no kernel, so it is not recorded as a published fact. The archive states that it is superseded by the cruise kernel used here, so this dataset follows the archive's own latest solution and records the difference between the 2007 short-arc and the 2011 long-arc reconstruction, rather than selecting the kernel that flatters the published number. Mars's system barycentre and its body centre are the same point to 0.00004 km at this encounter, Phobos and Deimos being negligible against Mars, so the barycentre offset the viewer draws against is zero to the precision recorded.

Provenance

Sources

Each source is listed once and labeled with the mission, event, trajectory, or destination/body context it supports.

Data verified through September 4, 2026