NASA/JPL HORIZONS EPHEMERIS

Lucy

NASA · Jupiter Trojan asteroids · Launched 2021-10-16

Real-time solar-system position sceneGlowing Sun · stars & galaxies · compressed scale · drag / pinch to explore
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TRACKER GUIDE & MISSION EXPLAINER

Lucy Spacecraft Tracker: Journey to the Jupiter Trojan Asteroids

Lucy is NASA's first mission to the Jupiter Trojan asteroids, primitive objects that share Jupiter's orbit around the Sun in two broad swarms. The tracker above uses JPL Horizons ephemerides to follow Lucy's complex solar orbit and changing distance from Earth and Sun.

The spacecraft launched on October 16, 2021. Its long trajectory uses Earth gravity assists and multiple flybys to reach a record number of asteroid targets rather than travelling to one final planet.

Lucy Spacecraft Tracker interface showing the main tracker view
The main Lucy Spacecraft Tracker interface on SpaceTracker.live. The position and values shown are a time-specific snapshot and will change as the tracker updates.

Why Trojan asteroids are important

Trojan asteroids occupy regions around the Sun-Jupiter L4 and L5 Lagrange points, leading and trailing Jupiter in its orbit. Their diversity may preserve clues about how the giant planets moved and mixed material during the early Solar System.

Lucy's planned encounters include main-belt asteroids and multiple Trojans. It flew past the main-belt asteroid Donaldjohanson in April 2025 while preparing for the Trojan phase beginning in 2027.

Understanding the tracker path

Horizons supplies a trajectory vector at defined times. The page interpolates cached points to create readable continuous values. Lucy's looping route can look surprising because gravity assists return the spacecraft near Earth and reshape its heliocentric orbit.

The scene cannot show asteroid encounter distances or target sizes at scale. A target may be millions of times smaller than the orbital path represented on screen.

Lucy Spacecraft Tracker data and feature panel
The mission visualization and ephemeris panel connect the spacecraft's route with its distance, light-time and velocity data. The visual scale is compressed for clarity.

Educational uses

  • Follow how an Earth flyby changes heliocentric speed and direction.
  • Compare L4 and L5 Trojan populations with the main asteroid belt.
  • Examine why a multi-target flyby mission needs precise timing.
  • Calculate how light time affects commanding during distant encounters.
  • Use official NASA pages to match tracker position with mission milestones.

Limits

The page does not show camera pointing, flyby sequences or instrument status. NASA's mission team provides official encounter information. The displayed distances and vectors are ephemeris-derived and the scene is compressed.

Why the itinerary takes many years

Lucy's targets are spread across different regions of the Solar System and cannot be visited on a simple outward cruise. The spacecraft repeatedly uses orbital geometry to meet objects that are themselves moving rapidly around the Sun. Each encounter must occur at the correct place and time, much like meeting several moving trains without stopping at every station. This makes the mission a useful example of trajectory design, long-term navigation and the scientific value of visiting a diverse sample instead of one representative asteroid.

Frequently asked questions

Why is the mission named Lucy?

It is named after the famous fossil that transformed understanding of human evolution, reflecting hopes that Trojan asteroids will transform knowledge of planetary origins.

Are Trojan asteroids moons of Jupiter?

No. They orbit the Sun near stable regions associated with Jupiter's orbit.

Will Lucy orbit an asteroid?

The mission is designed around a series of flybys rather than entering orbit around each target.

Why does the route return near Earth?

Earth gravity assists alter Lucy's solar orbit and provide energy for later encounters.

Sources and further reading

Educational-use note: SpaceTracker.live is an independent educational website and is not an official mission-control service. Positions, paths, distances and pass predictions are computed from third-party orbital elements or ephemerides. They may be delayed or approximate and must not be used for navigation, collision avoidance or safety-critical decisions.

Last reviewed: August 21, 2026