Mission Atlas
← Mission directory

Mission record

Zond 6

U.S.S.R · Launched

Explore trajectory

Partial success · Partial success

Soviet uncrewed circumlunar spacecraft that photographed the Moon and completed a guided skip reentry. The return capsule depressurized and its parachute was jettisoned at excessive altitude; it was destroyed on impact, although some photographic film was recovered.

Destinations
Launch vehicle
Proton Booster Plus Upper Stage and Escape Stages
Launch site
Tyuratam (Baikonur Cosmodrome), U.S.S.R
Countries
Soviet Union
Mission types
Flyby

Chronology

Mission timeline

  1. Milestone

    Translunar injection

  2. Launch

    Zond 6 launched on a lunar flyby mission from a parent satellite in Earth parking orbit

    Earth
  3. Milestone

    Midcourse correction

  4. Flyby

    Zond 6 flew around the Moon at a minimum distance of 2420 km

    Moon
  5. Milestone

    Inbound midcourse correction

  6. Impact

    Return capsule destroyed after premature parachute jettison

    NASA’s later history documents depressurization and parachute release at about5.3km altitude, correcting the contemporary account of a successful landing.

    Earth
  7. Milestone

    Final midcourse correction

Mission architecture

Vehicles

  • Zond 6 · Spacecraft

    Destinations: Moon

    • Zond 6 return capsule · Return capsule

      Destinations: Earth

Trajectory record

Trajectory dataset not yet available

Known dates and encounters do not uniquely determine a flight path. This mission’s sourced timeline is available above; no verified trajectory is currently published here.

What is needed to reconstruct this path?
  • A frame-qualified position and vector velocity at an epoch, or equivalent complete orbital elements.
  • Approach/departure directions and burn vectors between the reported encounters; body names and encounter distances alone are insufficient.
  • Independent descent/return states and a source-defined body-fixed landing location; a landing date alone does not define either.
  • Separate state histories and release epochs for the listed vehicles; a parent mission trajectory cannot be assigned to every component.
  • Finer event-time constraints where required by an orbital reconstruction; the stored day/month/year precision is retained.

Provenance

Sources

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

Data verified through October 12, 2026