SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 PF68

2014 PF68

2014 PF68 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.857 AU once every 4.83 yr.

Amor Observations: 276
Orbital Period · P
4.83 yr
v(q)
34.5 km/s
v(Q)
9 km/s
Diameter · ≈
0.87 km
TJ
2.93
Eccentricity · e
0.5863

Orbit and dynamics

Between its closest point (1.182 AU) and its farthest (4.532 AU), the heliocentric distance changes by 3.35 AU over every revolution.

One full revolution takes 4.83 yr (1,764 days), computed from the semi-major axis of 2.857 AU.

The high eccentricity (0.586) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 22.59° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 34.5 km/s at perihelion and falls to 9 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

The measured diameter is 3.33 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.01 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

Astrometry from 276 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3529 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

Semi-Major Axis
2.857 AU
Eccentricity
0.5863
Perihelion
1.182 AU
Aphelion
4.532059 AU
Inclination
22.59°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
136.56°

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
2048-Sep-09 17:07 0.195406 AU
29232394 km
13.22 km/s

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

Physical Parameters

Diameter
3.33 km
Albedo
0.01
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
18.05

Orbit Quality

RMS
0.3529
Condition
0
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

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