SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 FN5

2026 FN5

2026 FN5 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.662 AU and a period of 0.54 yr.

Aten Observations: 114
Orbital Period · P
0.54 yr
v(q)
69.4 km/s
v(Q)
19.3 km/s
Diameter · ≈
0.02 km
TJ
8.45
Eccentricity · e
0.5654

Orbit and dynamics

Between its closest point (0.288 AU) and its farthest (1.037 AU), the heliocentric distance changes by 0.749 AU over every revolution.

One full revolution takes 0.54 yr (197 days), computed from the semi-major axis of 0.662 AU.

The high eccentricity (0.565) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.24° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 69.4 km/s at perihelion and falls to 19.3 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

No direct size measurement is available; from an absolute magnitude of H = 26.82 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 114 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4727 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
0.6624 AU
Eccentricity
0.5654
Perihelion
0.288 AU
Aphelion
1.036921 AU
Inclination
1.24°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
359.41°

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
2027-Feb-20 00:51 0.144694 AU
21645940 km
16.80 km/s
2033-Mar-19 14:39 0.025977 AU
3886139 km
11.06 km/s
2034-Feb-20 21:47 0.189126 AU
28292839 km
18.69 km/s
2040-Mar-12 16:32 0.041409 AU
6194740 km
10.76 km/s
2047-Mar-06 17:35 0.040288 AU
6026959 km
10.75 km/s
2053-Mar-27 17:24 0.179653 AU
26875778 km
18.45 km/s
2054-Feb-28 03:46 0.025067 AU
3749912 km
11.05 km/s
2060-Mar-28 06:41 0.133783 AU
20013593 km
16.97 km/s
2061-Feb-23 16:38 0.009571 AU
1431730 km
11.67 km/s
2067-Mar-29 07:52 0.063654 AU
9522532 km
15.85 km/s
2068-Feb-22 08:15 0.010057 AU
1504443 km
12.27 km/s
2074-Mar-28 22:40 0.033327 AU
4985623 km
14.00 km/s
2075-Feb-20 00:25 0.040261 AU
6022947 km
13.95 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
26.82

Orbit Quality

RMS
0.4727
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.

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