SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 SF4

2022 SF4

2022 SF4 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.781 AU and a period of 0.69 yr.

Aten Observations: 21
Orbital Period · P
0.69 yr
v(q)
53.3 km/s
v(Q)
21.3 km/s
Diameter · ≈
0.01 km
TJ
7.34
Eccentricity · e
0.4292

Orbit and dynamics

The path is an ellipse reaching 0.446 AU from the Sun at perihelion and 1.117 AU at aphelion, a radial span of 0.671 AU.

Applying Kepler's third law to a = 0.781 AU gives an orbital period of 0.69 yr, or about 252 days.

The high eccentricity (0.429) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 13.91° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 53.3 km/s at perihelion and falls to 21.3 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 = 26.96 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 21 observations and has a weighted RMS residual of 0.4614 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
0.7813 AU
Eccentricity
0.4292
Perihelion
0.446 AU
Aphelion
1.116634 AU
Inclination
13.91°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
258.07°

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-16 18:47 0.218947 AU
32754037 km
12.64 km/s
2031-Sep-25 18:00 0.095921 AU
14349585 km
10.42 km/s
2032-Jan-27 19:45 0.417182 AU
62409594 km
13.23 km/s
2033-Sep-20 07:37 0.240741 AU
36014275 km
20.10 km/s
2038-Nov-16 15:27 0.279963 AU
41881837 km
17.22 km/s
2040-Oct-14 06:50 0.168841 AU
25258268 km
10.19 km/s
2042-Sep-16 20:38 0.086081 AU
12877569 km
15.69 km/s
2043-Feb-27 15:32 0.491017 AU
73455143 km
20.41 km/s
2047-Nov-12 12:34 0.377670 AU
56498691 km
21.92 km/s
2049-Jul-04 08:29 0.448777 AU
67136095 km
10.61 km/s
2049-Nov-04 09:26 0.200041 AU
29925709 km
10.37 km/s
2051-Sep-17 07:10 0.008642 AU
1292849 km
12.25 km/s
2052-Feb-12 23:20 0.456592 AU
68305219 km
17.25 km/s
2053-Sep-24 11:27 0.280362 AU
41941498 km
23.80 km/s
2058-Nov-17 17:18 0.209003 AU
31266378 km
14.41 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
26.96

Orbit Quality

RMS
0.46139
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.