SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 VH4

2020 VH4

2020 VH4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.092 AU it takes 1.14 yr to circle the Sun.

Apollo Observations: 32
Orbital Period · P
1.14 yr
v(q)
44 km/s
v(Q)
18.5 km/s
Diameter · ≈
0.08 km
TJ
5.59
Eccentricity · e
0.4088

Orbit and dynamics

Between its closest point (0.646 AU) and its farthest (1.538 AU), the heliocentric distance changes by 0.892 AU over every revolution.

One full revolution takes 1.14 yr (417 days), computed from the semi-major axis of 1.092 AU.

The high eccentricity (0.409) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 11.44° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44 km/s at perihelion and falls to 18.5 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 = 23.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.08 km.

Observation record and orbit quality

Astrometry from 32 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4401 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
1.092 AU
Eccentricity
0.4088
Perihelion
0.646 AU
Aphelion
1.53841 AU
Inclination
11.44°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
245.54°

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
2028-Nov-30 10:38 0.113758 AU
17018008 km
10.45 km/s
2030-Apr-25 00:11 0.296237 AU
44316437 km
10.56 km/s
2030-Jun-19 15:33 0.328050 AU
49075613 km
7.24 km/s
2036-Nov-26 15:33 0.044208 AU
6613367 km
12.16 km/s
2038-Apr-13 19:04 0.321441 AU
48086846 km
11.65 km/s
2038-Jul-04 06:44 0.369487 AU
55274459 km
8.25 km/s
2039-Jul-07 00:21 0.443790 AU
66390051 km
26.83 km/s
2044-Nov-24 13:39 0.033480 AU
5008534 km
13.27 km/s
2046-Apr-07 14:28 0.330568 AU
49452289 km
12.20 km/s
2046-Jul-09 17:55 0.384507 AU
57521442 km
8.62 km/s
2047-Jul-05 09:37 0.387497 AU
57968728 km
25.86 km/s
2052-Nov-23 05:23 0.033222 AU
4969992 km
14.04 km/s
2055-Jul-03 17:29 0.268140 AU
40113133 km
24.79 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
23.2

Orbit Quality

RMS
0.44007
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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