SpaceAtlas Space Object Data
NASA JPL SBDB · 2011 EE17

2011 EE17

2011 EE17 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.136 AU it takes 1.21 yr to circle the Sun.

Apollo Observations: 79
Orbital Period · P
1.21 yr
v(q)
35.7 km/s
v(Q)
21.9 km/s
Diameter · ≈
0.11 km
TJ
5.44
Eccentricity · e
0.239

Orbit and dynamics

The path is an ellipse reaching 0.864 AU from the Sun at perihelion and 1.408 AU at aphelion, a radial span of 0.544 AU.

Applying Kepler's third law to a = 1.136 AU gives an orbital period of 1.21 yr, or about 442 days.

An eccentricity of 0.239 makes the orbit moderately elongated.

The orbital plane is tilted 18.38° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 35.7 km/s at perihelion and falls to 21.9 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 = 22.56 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

The current orbit solution is based on 79 observations and has a weighted RMS residual of 0.567 arcseconds.

Condition code U = 1 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
1.136 AU
Eccentricity
0.239
Perihelion
0.864 AU
Aphelion
1.407504 AU
Inclination
18.38°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
146.57°

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
2028-Mar-10 14:05 0.285855 AU
42763277 km
18.02 km/s
2029-Sep-25 10:33 0.457625 AU
68459736 km
22.80 km/s
2034-Mar-18 00:36 0.086842 AU
12991317 km
11.29 km/s
2034-Oct-20 23:22 0.473701 AU
70864685 km
8.68 km/s
2040-Feb-28 11:22 0.337468 AU
50484558 km
9.64 km/s
2040-Sep-02 23:50 0.209329 AU
31315113 km
9.49 km/s
2046-Sep-11 21:04 0.115034 AU
17208887 km
14.13 km/s
2051-Mar-10 18:15 0.307951 AU
46068754 km
18.61 km/s
2052-Sep-24 10:09 0.438052 AU
65531715 km
22.28 km/s
2057-Mar-17 20:09 0.083851 AU
12543937 km
11.42 km/s
2057-Oct-22 14:20 0.478901 AU
71642513 km
8.64 km/s
2063-Feb-27 10:15 0.342269 AU
51202718 km
9.66 km/s
2063-Sep-03 12:59 0.202428 AU
30282795 km
9.52 km/s
2069-Sep-12 08:46 0.132025 AU
19750683 km
14.52 km/s
2074-Mar-11 09:51 0.284107 AU
42501824 km
17.96 km/s
2075-Sep-26 10:28 0.464096 AU
69427748 km
22.98 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
22.56

Orbit Quality

RMS
0.567
Condition
1
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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