SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 JF2

2022 JF2

2022 JF2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.08 AU it takes 1.12 yr to circle the Sun.

Apollo Observations: 34
Orbital Period · P
1.12 yr
v(q)
37.9 km/s
v(Q)
21.7 km/s
Diameter · ≈
0.01 km
TJ
5.7
Eccentricity · e
0.2723

Orbit and dynamics

The path is an ellipse reaching 0.786 AU from the Sun at perihelion and 1.374 AU at aphelion, a radial span of 0.588 AU.

Applying Kepler's third law to a = 1.08 AU gives an orbital period of 1.12 yr, or about 410 days.

An eccentricity of 0.272 makes the orbit moderately elongated.

Its inclination of 0.78° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37.9 km/s at perihelion and falls to 21.7 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 = 27.61 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 34 observations and has a weighted RMS residual of 0.4886 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
1.08 AU
Eccentricity
0.2723
Perihelion
0.786 AU
Aphelion
1.374084 AU
Inclination
0.78°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
291.57°

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
2029-Nov-02 22:38 0.086252 AU
12903049 km
11.95 km/s
2030-Aug-23 14:01 0.342581 AU
51249425 km
7.58 km/s
2038-Oct-25 15:09 0.235230 AU
35189919 km
17.32 km/s
2039-Sep-11 23:58 0.288907 AU
43219869 km
6.96 km/s
2041-May-29 19:28 0.346833 AU
51885449 km
20.37 km/s
2049-Jul-15 03:35 0.315339 AU
47174005 km
7.18 km/s
2050-May-21 04:28 0.162943 AU
24375996 km
14.83 km/s
2058-Aug-01 09:49 0.353809 AU
52929027 km
7.64 km/s
2059-May-13 13:40 0.037768 AU
5649980 km
10.21 km/s
2066-Nov-10 11:49 0.009854 AU
1474112 km
7.93 km/s
2067-Aug-12 08:44 0.348391 AU
52118597 km
7.68 km/s
2068-May-07 03:25 0.009854 AU
1474080 km
6.74 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
27.61

Orbit Quality

RMS
0.48865
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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