SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 PW59

2014 PW59

2014 PW59 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.407 AU it takes 3.73 yr to circle the Sun.

Apollo Observations: 98
Orbital Period · P
3.73 yr
v(q)
45.7 km/s
v(Q)
8.1 km/s
Diameter · ≈
0.23 km
TJ
3.13
Eccentricity · e
0.7001

Orbit and dynamics

Between its closest point (0.722 AU) and its farthest (4.092 AU), the heliocentric distance changes by 3.37 AU over every revolution.

One full revolution takes 3.73 yr (1,364 days), computed from the semi-major axis of 2.407 AU.

The high eccentricity (0.7) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.38° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 45.7 km/s at perihelion and falls to 8.1 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

The measured diameter is 0.41 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.045 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

Astrometry from 98 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4239 arcseconds.

Condition code U = 1 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
2.407 AU
Eccentricity
0.7001
Perihelion
0.722 AU
Aphelion
4.092141 AU
Inclination
2.38°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
64.12°

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
2029-Aug-16 21:10 0.357598 AU
53495914 km
29.01 km/s
2033-Feb-15 02:33 0.244776 AU
36617991 km
25.75 km/s
2044-Jun-11 01:44 0.268541 AU
40173101 km
15.29 km/s
2059-Feb-19 21:32 0.141663 AU
21192495 km
22.97 km/s
2070-Jul-10 20:11 0.159714 AU
23892872 km
14.42 km/s

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

Physical Parameters

Diameter
0.412 km
Albedo
0.045
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
20.9

Orbit Quality

RMS
0.42389
Condition
1
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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