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Mission record

Tianwen-2

China National Space Administration · Launched

Explore trajectory

Active · Active

China's active Tianwen-2 mission launched on 29 May 2025 from Xichang on a Long March 3B Y110. It has begun scientific exploration of asteroid 2016 HO3; the mission plans to return an asteroid sample to Earth before continuing to main-belt comet 311P.

Destinations
Launch vehicle
Long March-3B Y110 rocket
Launch site
Xichang Satellite Launch Center in southwest China's Sichuan Province
Countries
Peoples Republic of China
Mission types
Sample return

Chronology

Mission timeline

  1. Launch

    Launched on Long March 3B Y110 from Xichang Satellite Launch Center

    Launch began at 01:31 on May 29, 2025 Beijing time, which is 2025-05-28T17:31Z; the catalog launch date uses the local date and this event stores the UTC epoch.

    Earth
  2. Milestone

    First acquired asteroid 2016 HO3

    2016 HO3
  3. Milestone

    Performed approach control about 30,000 km from asteroid 2016 HO3

    CNSA reports a capture-control action and coplanar flight at about 30,000 km from the asteroid. The day is published without a UTC clock or direction to the asteroid.

    2016 HO3
  4. Milestone

    Approached to about 2,000 km from asteroid 2016 HO3

    CNSA reports an approximate asteroid range on this day without a UTC clock or relative direction.

    2016 HO3
  5. Milestone

    Captured an image of asteroid 2016 HO3 from about 20 km during science operations

    2016 HO3

Mission architecture

Vehicles

  • Tianwen-2 · Spacecraft

    Destinations: 2016 HO3, Earth, 311P

    • Tianwen-2 Reentry Capsule · Return capsule · Planned to separate from the main spacecraft for Earth reentry

      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?
  • CNSA reports approximately 43 million km from Earth and 45 million km from asteroid 2016 HO3 as current in its 1 October 2025 release; it does not give observation clocks, relative directions or formal range errors.
  • CNSA gives approximate spacecraft-to-asteroid ranges on June 7, June 19 and July 2, 2026, each at day precision without a relative direction or state velocity.
  • The June 7 capture-control action and earlier deep-space corrections lack maneuver clocks and vectors.
  • A time-tagged, frame-qualified spacecraft state or sufficient optical/radiometric observations are needed to reconstruct the transfer and close approach; the published asteroid ephemeris alone is not the spacecraft state.
  • The reentry capsule remains planned to separate later and has no independently observed trajectory.

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