SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 PA40

2016 PA40

2016 PA40 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.012 AU it takes 1.02 yr to circle the Sun.

Apollo Observations: 96
Orbital Period · P
1.02 yr
v(q)
39.7 km/s
v(Q)
22.1 km/s
Diameter · ≈
0.04 km
TJ
5.97
Eccentricity · e
0.2853

Orbit and dynamics

Between its closest point (0.723 AU) and its farthest (1.301 AU), the heliocentric distance changes by 0.578 AU over every revolution.

One full revolution takes 1.02 yr (372 days), computed from the semi-major axis of 1.012 AU.

An eccentricity of 0.285 makes the orbit moderately elongated.

The orbital plane is tilted 10.47° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.7 km/s at perihelion and falls to 22.1 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 = 24.49 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 96 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5421 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.012 AU
Eccentricity
0.2853
Perihelion
0.723 AU
Aphelion
1.300724 AU
Inclination
10.47°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
139.92°

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-27 00:17 0.134619 AU
20138766 km
12.10 km/s
2028-Apr-02 06:59 0.217693 AU
32566400 km
15.11 km/s
2029-Apr-08 16:41 0.315494 AU
47197211 km
18.21 km/s
2030-Apr-14 18:38 0.417438 AU
62447880 km
21.39 km/s
2069-Aug-14 14:45 0.394245 AU
58978258 km
21.42 km/s
2070-Aug-19 10:34 0.288466 AU
43153928 km
18.29 km/s
2071-Aug-24 02:57 0.182958 AU
27370144 km
15.22 km/s
2072-Aug-27 07:32 0.080449 AU
12034942 km
12.20 km/s
2073-Aug-30 02:52 0.034677 AU
5187541 km
9.48 km/s
2074-Aug-28 01:03 0.087280 AU
13056926 km
7.36 km/s
2075-Aug-13 10:48 0.173518 AU
25957852 km
7.00 km/s
2076-Jul-25 23:23 0.242874 AU
36333431 km
7.42 km/s
2077-Jul-10 05:04 0.291941 AU
43673822 km
7.66 km/s
2078-Jun-25 06:26 0.323800 AU
48439765 km
7.66 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
24.49

Orbit Quality

RMS
0.54206
Condition
6
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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