SpaceAtlas Space Object Data
NASA JPL SBDB · 2011 EN40

2011 EN40

2011 EN40 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.288 AU it takes 1.46 yr to circle the Sun.

Apollo Observations: 67
Orbital Period · P
1.46 yr
v(q)
67.8 km/s
v(Q)
10.2 km/s
Diameter · ≈
0.27 km
TJ
4.69
Eccentricity · e
0.7391

Orbit and dynamics

Between its closest point (0.336 AU) and its farthest (2.24 AU), the heliocentric distance changes by 1.904 AU over every revolution.

One full revolution takes 1.46 yr (534 days), computed from the semi-major axis of 1.288 AU.

The high eccentricity (0.739) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 13.41° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 67.8 km/s at perihelion and falls to 10.2 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 = 20.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.27 km.

Observation record and orbit quality

Astrometry from 67 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3743 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
1.288 AU
Eccentricity
0.7391
Perihelion
0.336 AU
Aphelion
2.239961 AU
Inclination
13.41°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
96.26°

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-Apr-05 06:24 0.379377 AU
56754048 km
16.82 km/s
2033-Mar-23 21:54 0.188029 AU
28128716 km
29.06 km/s
2034-Dec-09 06:58 0.218261 AU
32651341 km
25.57 km/s
2049-Apr-05 07:43 0.357444 AU
53472894 km
17.24 km/s
2050-Dec-28 21:10 0.486383 AU
72761845 km
39.42 km/s
2052-Mar-22 22:50 0.202322 AU
30266922 km
29.72 km/s
2053-Dec-08 06:40 0.219070 AU
32772414 km
24.90 km/s
2068-Apr-05 05:49 0.344015 AU
51463894 km
17.52 km/s
2069-Dec-28 01:16 0.473356 AU
70813099 km
38.91 km/s
2071-Mar-23 03:48 0.214168 AU
32039105 km
30.23 km/s
2072-Dec-07 11:24 0.221202 AU
33091346 km
24.38 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
20.6

Orbit Quality

RMS
0.37433
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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