Trajectory from Horizons state vectors
Europa Clipper's position is interpolated between 67 heliocentric state-vector samples from JPL Horizons that run through 2030-03-18. Past the last sample the marker holds its final position.
NASA orbiter en route to Jupiter to study the icy moon Europa and its subsurface ocean over dozens of flybys.
One record per aspect. The origin says what kind of thing each value is; the source says where it came from; the limit says what it cannot tell you.
Europa Clipper's position is interpolated between 67 heliocentric state-vector samples from JPL Horizons that run through 2030-03-18. Past the last sample the marker holds its final position.
Europa Clipper: mass 6.065 × 10^3 kg. These values are bundled with the object record and drive the rendered size.
The close-up shows a published 3D model scaled to 30 m deployed solar-array span. Distributed through NASA 3D Resources; original mission-agency credit applies.
The short description and the fact list are written by the Space Time authors for orientation. They are not quoted from a catalog field and carry no citation of their own.
Trajectory coverage: 2024-10-15 to 2030-03-18 (67 samples). Outside that window the marker holds its last known position.
| Dataset | Last refreshed | Horizon | Automated |
|---|---|---|---|
| Spacecraft trajectories (baked keyframes) | no snapshot date | Per craft: each evidence page states the first and last sample date | No, refreshed by hand scripts/bake-trajectories.mjs |