SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 FS5

2026 FS5

2026 FS5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.051 AU it takes 1.08 yr to circle the Sun.

Apollo Observations: 23
Orbital Period · P
1.08 yr
v(q)
40.9 km/s
v(Q)
20.6 km/s
TJ
5.8
Eccentricity · e
0.3302

Orbit and dynamics

Between its closest point (0.704 AU) and its farthest (1.398 AU), the heliocentric distance changes by 0.694 AU over every revolution.

One full revolution takes 1.08 yr (394 days), computed from the semi-major axis of 1.051 AU.

An eccentricity of 0.33 makes the orbit moderately elongated.

The orbital plane is tilted 5.41° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 40.9 km/s at perihelion and falls to 20.6 km/s at aphelion.

Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.

Size and surface

Neither a measured diameter nor a reliable absolute magnitude is available for 2026 FS5, so its physical size remains unconstrained.

Observation record and orbit quality

Astrometry from 23 individual observations underpins this orbit; the fit leaves an RMS residual of 0.39 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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

Semi-Major Axis
1.051 AU
Eccentricity
0.3302
Perihelion
0.704 AU
Aphelion
1.39804 AU
Inclination
5.41°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
134.07°

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 distanceVelocity
2037-Oct-05 13:33 0.180995 AU
27076504 km
6.63 km/s
2040-Mar-25 06:48 0.058449 AU
8743885 km
12.19 km/s
2050-Aug-26 08:54 0.147796 AU
22109982 km
14.52 km/s
2064-Aug-30 20:09 0.065289 AU
9767039 km
11.59 km/s
2067-Feb-21 18:36 0.192242 AU
28759017 km
5.85 km/s
2067-Mar-29 03:03 0.191398 AU
28632738 km
5.64 km/s
2078-Aug-30 06:15 0.076288 AU
11412460 km
12.22 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
— km
Albedo
—
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
31.32

Orbit Quality

RMS
0.39002
Condition
6
Orbit ID
—
Data source: NASA JPL Small-Body Database · NASA CNEOS. 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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.