Trajectory from Horizons state vectors
Solar Orbiter's position is interpolated between 1,959 heliocentric state-vector samples from JPL Horizons that run through 2030-11-01. Past the last sample the marker holds its final position.
ESA/NASA Sun observatory in an inclined heliocentric orbit, imaging the poles and sampling the solar wind up close.
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.
Solar Orbiter's position is interpolated between 1,959 heliocentric state-vector samples from JPL Horizons that run through 2030-11-01. Past the last sample the marker holds its final position.
Solar Orbiter: mass 1.800 × 10^3 kg. These values are bundled with the object record and drive the rendered size.
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: 2020-02-11 to 2030-11-01 (1,959 samples). Outside that window the marker holds its last known position.
Nothing on this page is a reconstruction or a schematic; every record above is observed, catalogued or computed.
| 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 |