SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 VP2

2024 VP2

2024 VP2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.415 AU it takes 3.75 yr to circle the Sun.

Apollo Observations: 99
Orbital Period · P
3.75 yr
v(q)
41.3 km/s
v(Q)
8.9 km/s
Diameter · ≈
0.49 km
TJ
3.05
Eccentricity · e
0.6459

Orbit and dynamics

Between its closest point (0.855 AU) and its farthest (3.975 AU), the heliocentric distance changes by 3.12 AU over every revolution.

One full revolution takes 3.75 yr (1,371 days), computed from the semi-major axis of 2.415 AU.

The high eccentricity (0.646) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 30.82° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 41.3 km/s at perihelion and falls to 8.9 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 = 19.31 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.49 km.

Observation record and orbit quality

Astrometry from 99 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4748 arcseconds.

Condition code U = 4 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
2.415 AU
Eccentricity
0.6459
Perihelion
0.855 AU
Aphelion
3.974849 AU
Inclination
30.82°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
137.79°

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
2054-Dec-23 02:51 0.048869 AU
7310768 km
21.44 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
19.31

Orbit Quality

RMS
0.47482
Condition
4
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

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