SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 VF5

2023 VF5

2023 VF5 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.799 AU and a period of 0.71 yr.

Aten Observations: 41
Orbital Period · P
0.71 yr
v(q)
51.1 km/s
v(Q)
21.7 km/s
Diameter · ≈
0.05 km
TJ
7.23
Eccentricity · e
0.4031

Orbit and dynamics

Between its closest point (0.477 AU) and its farthest (1.121 AU), the heliocentric distance changes by 0.644 AU over every revolution.

One full revolution takes 0.71 yr (261 days), computed from the semi-major axis of 0.799 AU.

The high eccentricity (0.403) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.12° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 51.1 km/s at perihelion and falls to 21.7 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 = 24.34 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

Astrometry from 41 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5604 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
0.7991 AU
Eccentricity
0.4031
Perihelion
0.477 AU
Aphelion
1.121217 AU
Inclination
2.12°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
76.98°

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
2028-Jul-10 09:04 0.383137 AU
57316468 km
9.77 km/s
2028-Nov-16 23:14 0.082397 AU
12326474 km
8.24 km/s
2030-Sep-29 08:16 0.409898 AU
61319884 km
24.83 km/s
2033-Jul-12 22:46 0.363526 AU
54382660 km
9.22 km/s
2033-Nov-14 21:43 0.079307 AU
11864218 km
8.19 km/s
2035-Sep-30 01:32 0.398376 AU
59596239 km
25.24 km/s
2040-Sep-30 01:05 0.400470 AU
59909531 km
25.84 km/s
2045-Sep-30 19:31 0.412462 AU
61703402 km
26.24 km/s
2058-Oct-28 02:09 0.130351 AU
19500244 km
8.20 km/s
2063-Oct-20 23:20 0.129948 AU
19439922 km
8.22 km/s
2068-Oct-12 20:40 0.123991 AU
18548788 km
8.15 km/s
2069-Jan-22 23:53 0.337300 AU
50459289 km
7.08 km/s
2073-Oct-07 10:54 0.102998 AU
15408258 km
8.15 km/s
2074-Jan-29 21:58 0.342681 AU
51264333 km
8.77 km/s
2076-Nov-15 07:18 0.423325 AU
63328546 km
26.07 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
24.34

Orbit Quality

RMS
0.56042
Condition
7
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.