SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 JE

2018 JE

2018 JE belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.154 AU it takes 1.24 yr to circle the Sun.

Apollo Observations: 123
Orbital Period · P
1.24 yr
v(q)
38.3 km/s
v(Q)
20.1 km/s
Diameter · ≈
0.23 km
TJ
5.31
Eccentricity · e
0.3118

Orbit and dynamics

The path is an ellipse reaching 0.794 AU from the Sun at perihelion and 1.514 AU at aphelion, a radial span of 0.72 AU.

Applying Kepler's third law to a = 1.154 AU gives an orbital period of 1.24 yr, or about 453 days.

An eccentricity of 0.312 makes the orbit moderately elongated.

A steep inclination of 26.26° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 38.3 km/s at perihelion and falls to 20.1 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

No direct size measurement is available; from an absolute magnitude of H = 20.96 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.23 km.

Observation record and orbit quality

The current orbit solution is based on 123 observations and has a weighted RMS residual of 0.3921 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
1.154 AU
Eccentricity
0.3118
Perihelion
0.794 AU
Aphelion
1.513817 AU
Inclination
26.26°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
258.54°

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
2027-Nov-25 21:34 0.250599 AU
37489148 km
14.56 km/s
2028-May-09 17:02 0.379845 AU
56824000 km
13.27 km/s
2032-Nov-05 02:38 0.062491 AU
9348487 km
16.79 km/s
2037-Oct-20 13:44 0.303461 AU
45397048 km
22.19 km/s
2044-May-01 00:31 0.256516 AU
38374229 km
19.38 km/s
2049-Apr-28 11:10 0.154965 AU
23182412 km
14.65 km/s
2053-Dec-01 17:16 0.305050 AU
45634871 km
14.61 km/s
2054-May-07 09:58 0.340649 AU
50960381 km
13.30 km/s
2058-Nov-07 20:22 0.059139 AU
8847047 km
16.29 km/s
2063-Oct-22 21:42 0.272592 AU
40779118 km
21.49 km/s
2070-May-02 11:59 0.286180 AU
42811937 km
20.16 km/s
2075-Apr-28 19:00 0.144188 AU
21570281 km
15.23 km/s
2079-Dec-12 20:32 0.370533 AU
55431015 km
14.76 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
20.96

Orbit Quality

RMS
0.39212
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.