SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 VX8

2018 VX8

2018 VX8 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.186 AU it takes 1.29 yr to circle the Sun.

Apollo Observations: 93
Orbital Period · P
1.29 yr
v(q)
34.6 km/s
v(Q)
21.6 km/s
Diameter · ≈
0.11 km
TJ
5.21
Eccentricity · e
0.2314

Orbit and dynamics

The path is an ellipse reaching 0.912 AU from the Sun at perihelion and 1.46 AU at aphelion, a radial span of 0.548 AU.

Applying Kepler's third law to a = 1.186 AU gives an orbital period of 1.29 yr, or about 472 days.

An eccentricity of 0.231 makes the orbit moderately elongated.

A steep inclination of 27.8° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 34.6 km/s at perihelion and falls to 21.6 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 = 22.49 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

The current orbit solution is based on 93 observations and has a weighted RMS residual of 0.4763 arcseconds.

Condition code U = 2 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
1.186 AU
Eccentricity
0.2314
Perihelion
0.912 AU
Aphelion
1.46044 AU
Inclination
27.8°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
213.41°

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-Nov-10 00:01 0.410240 AU
61371050 km
14.20 km/s
2028-May-23 07:10 0.243866 AU
36481795 km
19.28 km/s
2031-Nov-29 03:45 0.350978 AU
52505515 km
18.57 km/s
2040-Nov-26 11:05 0.234591 AU
35094370 km
15.32 km/s
2041-May-01 11:11 0.256918 AU
38434426 km
14.70 km/s
2049-Nov-19 16:21 0.286835 AU
42909856 km
14.29 km/s
2050-May-12 20:21 0.005254 AU
785930 km
15.62 km/s
2058-Nov-10 03:58 0.392302 AU
58687511 km
14.22 km/s
2059-May-24 06:21 0.219258 AU
32800456 km
19.31 km/s
2062-Nov-29 04:59 0.335679 AU
50216823 km
18.72 km/s
2068-Jun-03 22:48 0.440595 AU
65912076 km
24.59 km/s
2071-Nov-27 18:42 0.237083 AU
35467142 km
15.50 km/s
2072-Apr-30 12:16 0.211368 AU
31620157 km
14.80 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
22.49

Orbit Quality

RMS
0.47628
Condition
2
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.