SpaceAtlas Space Object Data
NASA JPL SBDB · 2008 EE9

2008 EE9

2008 EE9 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.325 AU it takes 1.53 yr to circle the Sun.

Apollo Observations: 94
Orbital Period · P
1.53 yr
v(q)
46.5 km/s
v(Q)
14.4 km/s
Diameter · ≈
0.12 km
TJ
4.77
Eccentricity · e
0.5276

Orbit and dynamics

The path is an ellipse reaching 0.626 AU from the Sun at perihelion and 2.024 AU at aphelion, a radial span of 1.398 AU.

Applying Kepler's third law to a = 1.325 AU gives an orbital period of 1.53 yr, or about 557 days.

The high eccentricity (0.528) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 9.97° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 46.5 km/s at perihelion and falls to 14.4 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 = 22.32 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

The current orbit solution is based on 94 observations and has a weighted RMS residual of 0.5352 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
1.325 AU
Eccentricity
0.5276
Perihelion
0.626 AU
Aphelion
2.02407 AU
Inclination
9.97°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
27.83°

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-Sep-20 08:09 0.210062 AU
31424839 km
11.64 km/s
2030-Nov-10 13:30 0.362410 AU
54215753 km
15.77 km/s
2033-Dec-20 14:56 0.373003 AU
55800427 km
15.55 km/s
2037-Feb-25 00:03 0.180491 AU
27001129 km
11.45 km/s
2040-Mar-15 01:37 0.199888 AU
29902866 km
22.04 km/s
2050-Aug-14 03:54 0.318930 AU
47711271 km
25.28 km/s
2053-Sep-02 05:53 0.080696 AU
12071956 km
15.36 km/s
2056-Oct-23 21:38 0.324699 AU
48574246 km
14.08 km/s
2059-Dec-10 20:29 0.381077 AU
57008233 km
16.27 km/s
2063-Feb-18 06:02 0.244272 AU
36542613 km
9.59 km/s
2066-Mar-12 09:58 0.129158 AU
19321826 km
19.89 km/s
2069-Mar-28 19:56 0.481398 AU
72016133 km
30.58 km/s
2076-Aug-11 07:32 0.367173 AU
54928239 km
26.72 km/s
2079-Aug-31 17:18 0.071117 AU
10639015 km
16.29 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
22.32

Orbit Quality

RMS
0.53515
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.

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