SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 VF1

2022 VF1

2022 VF1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.038 AU it takes 2.91 yr to circle the Sun.

Apollo Observations: 246
Orbital Period · P
2.91 yr
v(q)
44.9 km/s
v(Q)
9.7 km/s
Diameter · ≈
0.12 km
TJ
3.51
Eccentricity · e
0.6448

Orbit and dynamics

The path is an ellipse reaching 0.724 AU from the Sun at perihelion and 3.352 AU at aphelion, a radial span of 2.628 AU.

Applying Kepler's third law to a = 2.038 AU gives an orbital period of 2.91 yr, or about 1,063 days.

The high eccentricity (0.645) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 5.53° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44.9 km/s at perihelion and falls to 9.7 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 = 22.29 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

The current orbit solution is based on 246 observations and has a weighted RMS residual of 0.4874 arcseconds.

Condition code U = 1 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
2.038 AU
Eccentricity
0.6448
Perihelion
0.724 AU
Aphelion
3.352102 AU
Inclination
5.53°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
100.85°

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-May-29 05:03 0.013829 AU
2068765 km
18.10 km/s
2051-Oct-20 17:54 0.134820 AU
20168742 km
14.23 km/s
2077-Oct-14 01:24 0.177007 AU
26479920 km
13.28 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
22.29

Orbit Quality

RMS
0.48738
Condition
1
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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