SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 XP23

2016 XP23

2016 XP23 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.461 AU it takes 3.86 yr to circle the Sun.

Apollo Observations: 46
Orbital Period · P
3.86 yr
v(q)
40.9 km/s
v(Q)
8.8 km/s
Diameter · ≈
0.41 km
TJ
2.94
Eccentricity · e
0.645

Orbit and dynamics

Between its closest point (0.874 AU) and its farthest (4.048 AU), the heliocentric distance changes by 3.174 AU over every revolution.

One full revolution takes 3.86 yr (1,410 days), computed from the semi-major axis of 2.461 AU.

The high eccentricity (0.645) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 37.96° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 40.9 km/s at perihelion and falls to 8.8 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 = 19.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.41 km.

Observation record and orbit quality

Astrometry from 46 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6695 arcseconds.

Condition code U = 0 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
2.461 AU
Eccentricity
0.645
Perihelion
0.874 AU
Aphelion
4.048345 AU
Inclination
37.96°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
178.44°

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
2047-Oct-13 10:06 0.304882 AU
45609706 km
22.77 km/s
2074-Nov-22 06:03 0.412346 AU
61686039 km
32.20 km/s
2078-Oct-14 06:52 0.296208 AU
44312161 km
22.44 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
19.7

Orbit Quality

RMS
0.66951
Condition
0
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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