SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 PC8

2016 PC8

2016 PC8 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.075 AU it takes 1.11 yr to circle the Sun.

Apollo Observations: 25
Orbital Period · P
1.11 yr
v(q)
33.8 km/s
v(Q)
24.4 km/s
Diameter · ≈
0.04 km
TJ
5.73
Eccentricity · e
0.1624

Orbit and dynamics

Between its closest point (0.901 AU) and its farthest (1.25 AU), the heliocentric distance changes by 0.349 AU over every revolution.

One full revolution takes 1.11 yr (407 days), computed from the semi-major axis of 1.075 AU.

An eccentricity of 0.162 makes the orbit moderately elongated.

The orbital plane is tilted 8.81° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.8 km/s at perihelion and falls to 24.4 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

Astrometry from 25 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4776 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
1.075 AU
Eccentricity
0.1624
Perihelion
0.901 AU
Aphelion
1.24958 AU
Inclination
8.81°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
193.51°

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-Jan-31 19:26 0.026922 AU
4027432 km
5.79 km/s
2035-Aug-30 05:36 0.264932 AU
39633305 km
13.04 km/s
2036-Jun-25 01:07 0.245798 AU
36770835 km
5.76 km/s
2037-Feb-14 10:18 0.079521 AU
11896143 km
8.70 km/s
2045-Sep-02 23:13 0.126908 AU
18985233 km
8.44 km/s
2046-May-26 14:25 0.278602 AU
41678231 km
5.26 km/s
2047-Feb-26 02:54 0.261378 AU
39101665 km
13.47 km/s
2055-Aug-27 09:15 0.097234 AU
14546011 km
5.53 km/s
2056-Apr-19 17:45 0.256895 AU
38430891 km
4.13 km/s
2057-Mar-06 02:05 0.431809 AU
64597637 km
17.91 km/s
2065-Aug-03 05:50 0.166127 AU
24852286 km
5.44 km/s
2066-Jan-08 11:20 0.111203 AU
16635668 km
5.25 km/s
2074-Aug-26 09:25 0.387888 AU
58027279 km
15.86 km/s
2075-Jul-12 19:31 0.220795 AU
33030476 km
5.73 km/s
2076-Feb-05 18:52 0.023005 AU
3441439 km
6.37 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
0.47758
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.

Keep exploring

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