SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 AE65

2016 AE65

2016 AE65 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.845 AU and a period of 0.78 yr.

Aten Observations: 14
Orbital Period · P
0.78 yr
v(q)
44.1 km/s
v(Q)
23.8 km/s
Diameter · ≈
0.04 km
TJ
6.93
Eccentricity · e
0.2996

Orbit and dynamics

The path is an ellipse reaching 0.592 AU from the Sun at perihelion and 1.098 AU at aphelion, a radial span of 0.506 AU.

Applying Kepler's third law to a = 0.845 AU gives an orbital period of 0.78 yr, or about 284 days.

An eccentricity of 0.3 makes the orbit moderately elongated.

Its inclination of 3.34° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 44.1 km/s at perihelion and falls to 23.8 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 = 24.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

The current orbit solution is based on 14 observations and has a weighted RMS residual of 0.5099 arcseconds.

Condition code U = 8 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
0.8446 AU
Eccentricity
0.2996
Perihelion
0.592 AU
Aphelion
1.097642 AU
Inclination
3.34°
Orbital Period
— yr
Epoch
2457396.5
Mean Anomaly
130.93°

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-Mar-07 07:14 0.248839 AU
37225855 km
19.32 km/s
2033-Jan-01 04:15 0.299679 AU
44831381 km
22.45 km/s
2034-Mar-02 13:21 0.336606 AU
50355513 km
22.95 km/s
2039-Dec-28 10:47 0.185833 AU
27800186 km
18.73 km/s
2046-Dec-24 12:50 0.045533 AU
6811680 km
15.46 km/s
2051-Mar-15 06:28 0.054506 AU
8153943 km
9.97 km/s
2053-Dec-21 06:43 0.009764 AU
1460738 km
11.76 km/s
2058-Mar-13 01:43 0.076522 AU
11447562 km
13.65 km/s
2060-Dec-21 05:50 0.010656 AU
1594184 km
8.42 km/s
2065-Mar-12 05:47 0.092129 AU
13782270 km
14.91 km/s
2067-Dec-21 16:06 0.010595 AU
1585062 km
8.68 km/s
2071-Sep-06 07:59 0.385930 AU
57734330 km
13.14 km/s
2072-Mar-14 10:27 0.119443 AU
17868449 km
12.70 km/s
2074-Dec-21 20:18 0.007516 AU
1124396 km
12.07 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
24.7

Orbit Quality

RMS
0.50992
Condition
8
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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