SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 FW32

2014 FW32

2014 FW32 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.931 AU and a period of 0.90 yr.

Aten Observations: 22
Orbital Period · P
0.90 yr
v(q)
36.3 km/s
v(Q)
26.3 km/s
Diameter · ≈
0.01 km
TJ
6.42
Eccentricity · e
0.16

Orbit and dynamics

The path is an ellipse reaching 0.782 AU from the Sun at perihelion and 1.08 AU at aphelion, a radial span of 0.298 AU.

Applying Kepler's third law to a = 0.931 AU gives an orbital period of 0.90 yr, or about 328 days.

An eccentricity of 0.16 makes the orbit moderately elongated.

Its inclination of 1.31° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 36.3 km/s at perihelion and falls to 26.3 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 = 26.98 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 22 observations and has a weighted RMS residual of 0.5418 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
0.931 AU
Eccentricity
0.16
Perihelion
0.782 AU
Aphelion
1.07996 AU
Inclination
1.31°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
346.12°

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
2031-Mar-12 00:09 0.326422 AU
48832106 km
15.58 km/s
2032-Jun-15 04:15 0.018510 AU
2769130 km
3.47 km/s
2040-Mar-09 16:15 0.354335 AU
53007715 km
15.34 km/s
2040-Dec-05 12:54 0.183572 AU
27462000 km
5.20 km/s
2041-Jun-14 02:38 0.033195 AU
4965943 km
3.35 km/s
2049-Mar-13 00:53 0.415454 AU
62150965 km
18.00 km/s
2051-Jun-05 04:59 0.403416 AU
60350188 km
18.08 km/s
2060-Jun-07 07:09 0.277250 AU
41475944 km
15.40 km/s
2068-Sep-06 09:17 0.175578 AU
26266070 km
4.96 km/s
2069-Jun-06 03:00 0.340159 AU
50887096 km
15.36 km/s
2076-Mar-12 16:16 0.460872 AU
68945497 km
18.66 km/s
2076-Dec-30 20:25 0.145182 AU
21718844 km
3.60 km/s
2077-Apr-29 17:19 0.073855 AU
11048523 km
3.29 km/s
2078-May-31 20:34 0.494569 AU
73986459 km
19.09 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
26.98

Orbit Quality

RMS
0.54184
Condition
7
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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