Orbit and dynamics
The path is an ellipse reaching 1.338 AU from the Sun at perihelion and 5.242 AU at aphelion, a radial span of 3.904 AU.
Applying Kepler's third law to a = 3.29 AU gives an orbital period of 5.97 yr, or about 2,180 days.
The high eccentricity (0.593) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.
The orbital plane is tilted 5.37° relative to the ecliptic.
By the vis-viva equation its orbital speed rises to 32.5 km/s at perihelion and falls to 8.3 km/s at aphelion.
Its Tisserand parameter with respect to Jupiter is T_J = 2.86, a standard discriminator between asteroidal and cometary dynamics.
Size and surface
Neither a measured diameter nor a reliable absolute magnitude is available for LONEOS, so its physical size remains unconstrained.
Observation record and orbit quality
The current orbit solution is based on 197 observations and has a weighted RMS residual of 0.5976 arcseconds.
Condition code U = 0 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.
About these computed values
Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.
Orbital Parameters
Orbit diagram
The Sun sits at the focus (orange). Earth's orbit is the grey circle at 1 AU. The red dot marks the object's position at the catalog epoch.
3D orbit (interactive)
Drag to rotate; scroll or pinch to zoom. The Sun is at the focus (orange), Earth's orbit is the grey ring at 1 AU, and the red dot marks the object's current position.
Close approaches
Predicted close approaches to Earth, from NASA's Center for Near-Earth Object Studies (CNEOS).
| Date (UTC) | Miss distance | Velocity |
|---|---|---|
| 2035-Aug-29 14:16 | 0.254410 AU 38059248 km |
6.99 km/s |
| 2074-Aug-03 02:05 | 0.465353 AU 69615772 km |
15.72 km/s |
Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.
Physical Parameters
Orbit Quality
Related Objects
Same object type
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