SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 PC58

2014 PC58

2014 PC58 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.059 AU it takes 2.95 yr to circle the Sun.

Apollo Observations: 31
Orbital Period · P
2.95 yr
v(q)
37 km/s
v(Q)
11.6 km/s
Diameter · ≈
0.17 km
TJ
3.57
Eccentricity · e
0.5211

Orbit and dynamics

Between its closest point (0.986 AU) and its farthest (3.132 AU), the heliocentric distance changes by 2.146 AU over every revolution.

One full revolution takes 2.95 yr (1,079 days), computed from the semi-major axis of 2.059 AU.

The high eccentricity (0.521) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 14.58° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 37 km/s at perihelion and falls to 11.6 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 = 21.62 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.17 km.

Observation record and orbit quality

Astrometry from 31 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4605 arcseconds.

Condition code U = 4 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
2.059 AU
Eccentricity
0.5211
Perihelion
0.986 AU
Aphelion
3.131945 AU
Inclination
14.58°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
339.03°

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
2073-Dec-27 03:05 0.416811 AU
62354061 km
20.15 km/s
2076-Dec-12 09:19 0.247818 AU
37072987 km
11.98 km/s
2079-Sep-13 01:16 0.176703 AU
26434452 km
10.59 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
21.62

Orbit Quality

RMS
0.46049
Condition
4
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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