SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 ES11

2013 ES11

2013 ES11 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.203 AU it takes 1.32 yr to circle the Sun.

Apollo Observations: 136
Orbital Period · P
1.32 yr
v(q)
38.7 km/s
v(Q)
19.1 km/s
Diameter · ≈
0.06 km
TJ
5.23
Eccentricity · e
0.3395

Orbit and dynamics

The path is an ellipse reaching 0.794 AU from the Sun at perihelion and 1.611 AU at aphelion, a radial span of 0.817 AU.

Applying Kepler's third law to a = 1.203 AU gives an orbital period of 1.32 yr, or about 482 days.

An eccentricity of 0.34 makes the orbit moderately elongated.

Its inclination of 0.37° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.7 km/s at perihelion and falls to 19.1 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 = 23.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

The current orbit solution is based on 136 observations and has a weighted RMS residual of 0.3075 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.203 AU
Eccentricity
0.3395
Perihelion
0.794 AU
Aphelion
1.611419 AU
Inclination
0.37°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
323.18°

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-Sep-09 19:57 0.006581 AU
984450 km
12.19 km/s
2034-Jan-27 17:25 0.460171 AU
68840561 km
9.17 km/s
2038-Feb-21 12:58 0.323503 AU
48395302 km
6.60 km/s
2038-Oct-15 17:04 0.381780 AU
57113549 km
7.53 km/s
2042-Apr-03 20:43 0.076152 AU
11392190 km
7.43 km/s
2046-Mar-14 16:45 0.155224 AU
23221242 km
15.32 km/s
2050-Mar-01 13:12 0.401662 AU
60087784 km
23.86 km/s
2055-Sep-27 04:23 0.305166 AU
45652113 km
22.36 km/s
2059-Sep-12 20:48 0.006699 AU
1002088 km
13.52 km/s
2075-Mar-12 01:53 0.213829 AU
31988433 km
17.23 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
23.7

Orbit Quality

RMS
0.30755
Condition
7
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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