SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 FO4

2023 FO4

2023 FO4 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.917 AU and a period of 0.88 yr.

Aten Observations: 30
Orbital Period · P
0.88 yr
v(q)
37.8 km/s
v(Q)
25.6 km/s
Diameter · ≈
0.02 km
TJ
6.49
Eccentricity · e
0.1932

Orbit and dynamics

The path is an ellipse reaching 0.74 AU from the Sun at perihelion and 1.095 AU at aphelion, a radial span of 0.355 AU.

Applying Kepler's third law to a = 0.917 AU gives an orbital period of 0.88 yr, or about 321 days.

An eccentricity of 0.193 makes the orbit moderately elongated.

Its inclination of 3.76° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37.8 km/s at perihelion and falls to 25.6 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 = 26.26 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 30 observations and has a weighted RMS residual of 0.5309 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
0.9175 AU
Eccentricity
0.1932
Perihelion
0.74 AU
Aphelion
1.094761 AU
Inclination
3.76°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
13.11°

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-Feb-26 23:05 0.106701 AU
15962209 km
9.04 km/s
2030-Oct-06 23:20 0.252110 AU
37715080 km
7.97 km/s
2031-Jun-07 02:48 0.249619 AU
37342411 km
13.03 km/s
2037-Mar-06 10:36 0.307925 AU
46064994 km
15.67 km/s
2037-Nov-13 01:30 0.242777 AU
36318872 km
7.61 km/s
2038-Jun-12 20:26 0.068469 AU
10242758 km
6.59 km/s
2052-Feb-29 06:41 0.023213 AU
3472683 km
5.14 km/s
2052-Sep-11 12:11 0.229493 AU
34331735 km
7.02 km/s
2053-May-31 22:05 0.353124 AU
52826571 km
17.14 km/s
2059-Mar-01 03:56 0.031434 AU
4702445 km
11.14 km/s
2060-Jun-08 16:09 0.075158 AU
11243460 km
11.03 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
26.26

Orbit Quality

RMS
0.53088
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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