SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 VM1

2022 VM1

2022 VM1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.09 AU it takes 1.14 yr to circle the Sun.

Apollo Observations: 50
Orbital Period · P
1.14 yr
v(q)
30.8 km/s
v(Q)
26.4 km/s
Diameter · ≈
0.02 km
TJ
5.59
Eccentricity · e
0.0771

Orbit and dynamics

Between its closest point (1.006 AU) and its farthest (1.174 AU), the heliocentric distance changes by 0.168 AU over every revolution.

One full revolution takes 1.14 yr (416 days), computed from the semi-major axis of 1.09 AU.

With e = 0.077, the orbit is close to circular.

A steep inclination of 26.33° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 30.8 km/s at perihelion and falls to 26.4 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 26.39 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 50 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4063 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
1.09 AU
Eccentricity
0.0771
Perihelion
1.006 AU
Aphelion
1.174039 AU
Inclination
26.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
52.94°

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
2030-Nov-03 02:54 0.162362 AU
24288990 km
15.38 km/s
2031-May-02 10:30 0.218683 AU
32714449 km
13.61 km/s
2038-Oct-25 20:36 0.332196 AU
49695787 km
19.55 km/s
2039-May-10 04:09 0.163731 AU
24493841 km
13.09 km/s
2039-Nov-22 16:40 0.225170 AU
33684997 km
17.81 km/s
2047-May-17 10:05 0.199534 AU
29849853 km
13.84 km/s
2047-Nov-15 02:04 0.064535 AU
9654314 km
14.45 km/s
2055-May-24 10:37 0.258273 AU
38637117 km
15.61 km/s
2055-Nov-07 16:48 0.035138 AU
5256501 km
14.18 km/s
2063-Oct-30 11:55 0.103720 AU
15516289 km
17.14 km/s
2064-Nov-25 23:40 0.260449 AU
38962613 km
20.32 km/s
2072-May-13 00:38 0.173793 AU
25999034 km
13.30 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
26.39

Orbit Quality

RMS
0.40632
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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