SpaceAtlas Space Object Data
NASA JPL SBDB · 2008 JE

2008 JE

2008 JE is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.984 AU and a period of 0.98 yr.

Aten Observations: 31
Orbital Period · P
0.98 yr
v(q)
33 km/s
v(Q)
27.4 km/s
Diameter · ≈
0.02 km
TJ
6.15
Eccentricity · e
0.0931

Orbit and dynamics

The path is an ellipse reaching 0.892 AU from the Sun at perihelion and 1.076 AU at aphelion, a radial span of 0.184 AU.

Applying Kepler's third law to a = 0.984 AU gives an orbital period of 0.98 yr, or about 356 days.

With e = 0.093, the orbit is close to circular.

The orbital plane is tilted 6.96° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33 km/s at perihelion and falls to 27.4 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 = 25.8 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 31 observations and has a weighted RMS residual of 0.5946 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
0.9839 AU
Eccentricity
0.0931
Perihelion
0.892 AU
Aphelion
1.075501 AU
Inclination
6.96°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
72.1°

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
2043-Dec-30 17:58 0.362180 AU
54181293 km
14.09 km/s
2044-Dec-20 14:41 0.217283 AU
32505073 km
9.67 km/s
2045-Dec-05 23:45 0.091330 AU
13662738 km
5.82 km/s
2046-Nov-03 17:25 0.082101 AU
12282075 km
4.50 km/s
2047-Feb-21 09:13 0.138390 AU
20702807 km
3.12 km/s
2047-Sep-17 23:07 0.141716 AU
21200412 km
4.39 km/s
2048-Apr-23 06:58 0.070109 AU
10488145 km
3.94 km/s
2049-May-12 15:46 0.060818 AU
9098242 km
5.57 km/s
2050-May-12 22:10 0.198474 AU
29691340 km
9.35 km/s
2051-May-09 06:52 0.345287 AU
51654191 km
13.56 km/s
2052-May-03 11:54 0.492506 AU
73677818 km
17.87 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
25.8

Orbit Quality

RMS
0.59461
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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