SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 VH64

2015 VH64

2015 VH64 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.607 AU it takes 4.21 yr to circle the Sun.

Apollo Observations: 84
Orbital Period · P
4.21 yr
v(q)
39.2 km/s
v(Q)
8.7 km/s
Diameter · ≈
0.17 km
TJ
2.99
Eccentricity · e
0.6369

Orbit and dynamics

Between its closest point (0.946 AU) and its farthest (4.267 AU), the heliocentric distance changes by 3.321 AU over every revolution.

One full revolution takes 4.21 yr (1,537 days), computed from the semi-major axis of 2.607 AU.

The high eccentricity (0.637) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 23.8° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.2 km/s at perihelion and falls to 8.7 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 = 21.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.17 km.

Observation record and orbit quality

Astrometry from 84 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4707 arcseconds.

Condition code U = 5 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
2.607 AU
Eccentricity
0.6369
Perihelion
0.946 AU
Aphelion
4.267398 AU
Inclination
23.8°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
170.05°

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
2036-Dec-04 21:01 0.301037 AU
45034477 km
13.21 km/s
2037-Mar-17 00:18 0.386346 AU
57796533 km
12.22 km/s
2057-Dec-01 01:05 0.224116 AU
33527289 km
14.67 km/s
2058-Mar-17 12:49 0.423011 AU
63281608 km
10.73 km/s
2078-Nov-12 06:07 0.332665 AU
49766027 km
25.12 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
21.6

Orbit Quality

RMS
0.47066
Condition
5
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.