SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 VM2

2022 VM2

2022 VM2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.32 AU it takes 1.52 yr to circle the Sun.

Apollo Observations: 81
Orbital Period · P
1.52 yr
v(q)
33.1 km/s
v(Q)
20.3 km/s
Diameter · ≈
0.03 km
TJ
4.92
Eccentricity · e
0.2393

Orbit and dynamics

Between its closest point (1.004 AU) and its farthest (1.636 AU), the heliocentric distance changes by 0.632 AU over every revolution.

One full revolution takes 1.52 yr (554 days), computed from the semi-major axis of 1.32 AU.

An eccentricity of 0.239 makes the orbit moderately elongated.

Its inclination of 4.12° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.1 km/s at perihelion and falls to 20.3 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 25.75 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 81 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3803 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
1.32 AU
Eccentricity
0.2393
Perihelion
1.004 AU
Aphelion
1.635876 AU
Inclination
4.12°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
120.02°

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-Aug-10 00:37 0.392151 AU
58664881 km
5.07 km/s
2029-Jan-10 07:29 0.411124 AU
61503275 km
15.59 km/s
2031-Jul-20 22:27 0.478506 AU
71583545 km
6.80 km/s
2058-Mar-18 17:50 0.440108 AU
65839260 km
6.71 km/s
2060-Oct-02 19:42 0.304893 AU
45611355 km
13.48 km/s
2061-Feb-24 18:57 0.341108 AU
51029029 km
4.78 km/s
2063-Oct-19 18:24 0.092823 AU
13886144 km
7.14 km/s
2066-Dec-03 08:55 0.022973 AU
3436756 km
4.12 km/s
2069-Aug-28 01:21 0.330054 AU
49375378 km
3.50 km/s
2070-Jan-03 14:16 0.289486 AU
43306439 km
11.74 km/s
2072-Jul-28 02:57 0.441799 AU
66092136 km
6.23 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
25.75

Orbit Quality

RMS
0.38032
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.

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