SpaceAtlas Space Object Data
NASA JPL SBDB · 2001 VE2

2001 VE2

2001 VE2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.106 AU it takes 1.16 yr to circle the Sun.

Apollo Observations: 70
Orbital Period · P
1.16 yr
v(q)
34 km/s
v(Q)
23.6 km/s
Diameter · ≈
0.04 km
TJ
5.61
Eccentricity · e
0.1811

Orbit and dynamics

The path is an ellipse reaching 0.906 AU from the Sun at perihelion and 1.306 AU at aphelion, a radial span of 0.4 AU.

Applying Kepler's third law to a = 1.106 AU gives an orbital period of 1.16 yr, or about 425 days.

An eccentricity of 0.181 makes the orbit moderately elongated.

Its inclination of 4.39° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34 km/s at perihelion and falls to 23.6 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 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

The current orbit solution is based on 70 observations and has a weighted RMS residual of 0.5755 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
1.106 AU
Eccentricity
0.1811
Perihelion
0.906 AU
Aphelion
1.306297 AU
Inclination
4.39°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
352.99°

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
2031-Apr-14 01:32 0.105853 AU
15835393 km
9.98 km/s
2038-Apr-07 07:20 0.044746 AU
6693980 km
6.26 km/s
2044-Sep-19 13:10 0.222423 AU
33274041 km
4.44 km/s
2045-Apr-03 10:34 0.044722 AU
6690346 km
4.55 km/s
2051-Oct-01 01:42 0.197135 AU
29491001 km
3.98 km/s
2052-Mar-28 17:52 0.059528 AU
8905279 km
3.24 km/s
2058-Oct-21 04:10 0.152422 AU
22801988 km
3.07 km/s
2059-Apr-21 18:28 0.124976 AU
18696077 km
3.00 km/s
2065-Dec-19 01:11 0.080524 AU
12046192 km
3.56 km/s
2066-May-13 03:45 0.183221 AU
27409421 km
3.91 km/s
2072-Nov-24 14:27 0.040706 AU
6089491 km
3.90 km/s
2073-May-21 23:57 0.206769 AU
30932197 km
4.33 km/s
2079-Dec-03 02:56 0.057043 AU
8533576 km
3.53 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
25.0

Orbit Quality

RMS
0.57545
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.

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