SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 VL6

2023 VL6

2023 VL6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.122 AU it takes 1.19 yr to circle the Sun.

Apollo Observations: 54
Orbital Period · P
1.19 yr
v(q)
31.1 km/s
v(Q)
25.4 km/s
Diameter · ≈
0.02 km
TJ
5.55
Eccentricity · e
0.1002

Orbit and dynamics

Between its closest point (1.01 AU) and its farthest (1.234 AU), the heliocentric distance changes by 0.224 AU over every revolution.

One full revolution takes 1.19 yr (434 days), computed from the semi-major axis of 1.122 AU.

An eccentricity of 0.1 makes the orbit moderately elongated.

The orbital plane is tilted 9.3° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 31.1 km/s at perihelion and falls to 25.4 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 26.64 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 54 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4655 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
1.122 AU
Eccentricity
0.1002
Perihelion
1.01 AU
Aphelion
1.234424 AU
Inclination
9.3°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
47.55°

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
2029-Oct-25 09:47 0.335241 AU
50151322 km
11.88 km/s
2030-Apr-14 15:38 0.217513 AU
32539498 km
5.53 km/s
2036-Jun-02 02:07 0.227079 AU
33970473 km
5.78 km/s
2036-Dec-03 08:51 0.440026 AU
65826938 km
14.85 km/s
2042-Nov-20 06:04 0.083790 AU
12534820 km
6.04 km/s
2048-Nov-03 05:06 0.157083 AU
23499293 km
8.22 km/s
2055-May-12 03:01 0.221459 AU
33129803 km
5.97 km/s
2061-Jun-30 07:51 0.233542 AU
34937377 km
4.85 km/s
2061-Nov-27 16:43 0.271053 AU
40548964 km
10.18 km/s
2067-Nov-13 11:51 0.025098 AU
3754631 km
5.18 km/s
2073-Oct-18 11:16 0.449548 AU
67251480 km
14.95 km/s
2074-May-01 14:50 0.215253 AU
32201458 km
5.87 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
26.64

Orbit Quality

RMS
0.46554
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

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