SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 JR25

2014 JR25

2014 JR25 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.511 AU it takes 3.98 yr to circle the Sun.

Apollo Observations: 106
Orbital Period · P
3.98 yr
v(q)
41.9 km/s
v(Q)
8.4 km/s
Diameter · ≈
0.08 km
TJ
3.09
Eccentricity · e
0.6653

Orbit and dynamics

Between its closest point (0.84 AU) and its farthest (4.182 AU), the heliocentric distance changes by 3.342 AU over every revolution.

One full revolution takes 3.98 yr (1,453 days), computed from the semi-major axis of 2.511 AU.

The high eccentricity (0.665) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 10.29° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 41.9 km/s at perihelion and falls to 8.4 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 = 23.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.08 km.

Observation record and orbit quality

Astrometry from 106 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4283 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
2.511 AU
Eccentricity
0.6653
Perihelion
0.84 AU
Aphelion
4.181568 AU
Inclination
10.29°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
22.58°

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
2030-Feb-11 16:25 0.199187 AU
29797963 km
11.98 km/s
2034-Jan-17 00:23 0.169232 AU
25316673 km
14.78 km/s
2038-Jan-04 23:19 0.236163 AU
35329511 km
19.60 km/s
2041-Dec-28 17:25 0.338169 AU
50589401 km
23.45 km/s
2045-Dec-19 22:24 0.489971 AU
73298654 km
28.49 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
23.3

Orbit Quality

RMS
0.42827
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.