SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 VR5

2023 VR5

2023 VR5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.01 AU it takes 1.02 yr to circle the Sun.

Apollo Observations: 23
Orbital Period · P
1.02 yr
v(q)
32.8 km/s
v(Q)
26.7 km/s
Diameter · ≈
0.01 km
TJ
6.03
Eccentricity · e
0.1022

Orbit and dynamics

The path is an ellipse reaching 0.907 AU from the Sun at perihelion and 1.113 AU at aphelion, a radial span of 0.206 AU.

Applying Kepler's third law to a = 1.01 AU gives an orbital period of 1.02 yr, or about 371 days.

An eccentricity of 0.102 makes the orbit moderately elongated.

Its inclination of 1.23° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.8 km/s at perihelion and falls to 26.7 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 = 27.69 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 23 observations and has a weighted RMS residual of 0.4905 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
1.01 AU
Eccentricity
0.1022
Perihelion
0.907 AU
Aphelion
1.113222 AU
Inclination
1.23°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
105.11°

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-May-24 02:12 0.082061 AU
12276204 km
5.10 km/s
2028-May-28 20:21 0.191334 AU
28623186 km
8.36 km/s
2029-Jun-03 15:31 0.302463 AU
45247846 km
11.66 km/s
2030-Jun-09 09:23 0.414400 AU
61993407 km
15.03 km/s
2073-Oct-31 12:27 0.381384 AU
57054303 km
16.77 km/s
2074-Nov-06 04:16 0.262891 AU
39327992 km
13.27 km/s
2075-Nov-12 04:07 0.144872 AU
21672503 km
9.76 km/s
2076-Nov-16 14:59 0.031195 AU
4666773 km
6.33 km/s
2077-Nov-21 12:03 0.008871 AU
1327059 km
3.13 km/s
2078-Nov-21 13:13 0.008862 AU
1325770 km
2.20 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
27.69

Orbit Quality

RMS
0.49048
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.

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