SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 FT2

2026 FT2

2026 FT2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.905 AU and a period of 0.86 yr.

Aten Observations: 25
Orbital Period · P
0.86 yr
v(q)
40.9 km/s
v(Q)
24 km/s
Diameter · ≈
0.02 km
TJ
6.56
Eccentricity · e
0.2607

Orbit and dynamics

Between its closest point (0.669 AU) and its farthest (1.141 AU), the heliocentric distance changes by 0.472 AU over every revolution.

One full revolution takes 0.86 yr (314 days), computed from the semi-major axis of 0.905 AU.

An eccentricity of 0.261 makes the orbit moderately elongated.

Its inclination of 2.84° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 40.9 km/s at perihelion and falls to 24 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 = 26.69 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 25 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5937 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
0.9049 AU
Eccentricity
0.2607
Perihelion
0.669 AU
Aphelion
1.140807 AU
Inclination
2.84°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
348.98°

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
2032-Feb-29 06:50 0.125784 AU
18817087 km
5.84 km/s
2038-Jan-18 13:57 0.157437 AU
23552308 km
6.22 km/s
2043-Dec-06 09:04 0.053040 AU
7934658 km
6.64 km/s
2049-Dec-07 18:39 0.150814 AU
22561465 km
12.67 km/s
2051-Mar-24 06:00 0.082732 AU
12376518 km
10.70 km/s
2057-Mar-15 04:23 0.083394 AU
12475513 km
5.77 km/s
2063-Jan-26 21:02 0.162097 AU
24249351 km
6.33 km/s
2068-Dec-07 18:45 0.073066 AU
10930566 km
6.07 km/s
2074-Dec-07 11:56 0.138493 AU
20718290 km
12.14 km/s
2076-Mar-23 03:42 0.096991 AU
14509711 km
11.19 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
26.69

Orbit Quality

RMS
0.59365
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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