SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 VA4

2020 VA4

2020 VA4 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.982 AU and a period of 0.97 yr.

Aten Observations: 69
Orbital Period · P
0.97 yr
v(q)
34.7 km/s
v(Q)
26 km/s
Diameter · ≈
0.01 km
TJ
6.16
Eccentricity · e
0.1432

Orbit and dynamics

The path is an ellipse reaching 0.842 AU from the Sun at perihelion and 1.123 AU at aphelion, a radial span of 0.281 AU.

Applying Kepler's third law to a = 0.982 AU gives an orbital period of 0.97 yr, or about 356 days.

An eccentricity of 0.143 makes the orbit moderately elongated.

Its inclination of 0.37° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.7 km/s at perihelion and falls to 26 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 = 27.43 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 69 observations and has a weighted RMS residual of 0.4743 arcseconds.

Condition code U = 2 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

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
0.9823 AU
Eccentricity
0.1432
Perihelion
0.842 AU
Aphelion
1.122965 AU
Inclination
0.37°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
353.26°

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-19 01:50 0.355853 AU
53234862 km
15.50 km/s
2055-Nov-14 18:56 0.384761 AU
57559470 km
16.46 km/s
2056-Nov-07 11:54 0.221159 AU
33084922 km
11.45 km/s
2057-Nov-01 20:21 0.057822 AU
8649998 km
6.50 km/s
2058-Nov-21 16:56 0.088940 AU
13305290 km
3.13 km/s
2059-Aug-11 06:09 0.164814 AU
24655829 km
5.04 km/s
2060-Jan-10 00:53 0.139576 AU
20880325 km
4.26 km/s
2060-Jul-02 06:17 0.171165 AU
25605888 km
5.27 km/s
2061-Feb-21 06:30 0.113358 AU
16958188 km
3.65 km/s
2061-May-17 00:41 0.127459 AU
19067612 km
3.56 km/s
2062-Mar-31 11:23 0.015316 AU
2291200 km
5.24 km/s
2063-Mar-25 04:08 0.215223 AU
32196948 km
11.25 km/s
2064-Mar-16 12:01 0.414455 AU
62001523 km
17.33 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
27.43

Orbit Quality

RMS
0.47425
Condition
2
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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