SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 VR2

2024 VR2

2024 VR2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.959 AU and a period of 0.94 yr.

Aten Observations: 95
Orbital Period · P
0.94 yr
v(q)
37.6 km/s
v(Q)
24.6 km/s
Diameter · ≈
0.03 km
TJ
6.25
Eccentricity · e
0.2087

Orbit and dynamics

Between its closest point (0.759 AU) and its farthest (1.159 AU), the heliocentric distance changes by 0.4 AU over every revolution.

One full revolution takes 0.94 yr (343 days), computed from the semi-major axis of 0.959 AU.

An eccentricity of 0.209 makes the orbit moderately elongated.

The orbital plane is tilted 9.98° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 37.6 km/s at perihelion and falls to 24.6 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 = 25.48 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 95 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4028 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
0.9591 AU
Eccentricity
0.2087
Perihelion
0.759 AU
Aphelion
1.159264 AU
Inclination
9.98°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
338.68°

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-Mar-27 20:43 0.153376 AU
22944700 km
10.68 km/s
2039-Nov-10 14:00 0.121289 AU
18144625 km
11.55 km/s
2042-Apr-11 23:49 0.119114 AU
17819243 km
7.65 km/s
2055-Nov-11 07:10 0.066921 AU
10011312 km
6.85 km/s
2057-May-14 14:42 0.193546 AU
28954005 km
7.83 km/s
2070-Nov-08 19:29 0.047044 AU
7037750 km
9.42 km/s
2073-Apr-02 08:03 0.120449 AU
18018900 km
9.07 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
25.48

Orbit Quality

RMS
0.40276
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.