SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 JC4

2023 JC4

2023 JC4 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.871 AU and a period of 0.81 yr.

Aten Observations: 56
Orbital Period · P
0.81 yr
v(q)
39.7 km/s
v(Q)
25.7 km/s
Diameter · ≈
0.03 km
TJ
6.77
Eccentricity · e
0.2141

Orbit and dynamics

The path is an ellipse reaching 0.684 AU from the Sun at perihelion and 1.057 AU at aphelion, a radial span of 0.373 AU.

Applying Kepler's third law to a = 0.871 AU gives an orbital period of 0.81 yr, or about 297 days.

An eccentricity of 0.214 makes the orbit moderately elongated.

Its inclination of 2.38° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 39.7 km/s at perihelion and falls to 25.7 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 = 25.42 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 56 observations and has a weighted RMS residual of 0.4006 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
0.8709 AU
Eccentricity
0.2141
Perihelion
0.684 AU
Aphelion
1.05736 AU
Inclination
2.38°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
118.39°

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
2027-Mar-23 03:09 0.209737 AU
31376201 km
11.61 km/s
2027-Sep-22 17:36 0.285875 AU
42766265 km
8.36 km/s
2031-Nov-20 04:55 0.298619 AU
44672786 km
9.33 km/s
2032-Jun-02 12:15 0.291707 AU
43638742 km
14.22 km/s
2036-May-10 03:50 0.050871 AU
7610140 km
4.01 km/s
2040-Mar-23 08:54 0.230694 AU
34511342 km
12.76 km/s
2040-Sep-27 18:51 0.290056 AU
43391830 km
8.73 km/s
2044-Nov-29 02:34 0.288504 AU
43159511 km
8.85 km/s
2045-Jun-04 22:15 0.223154 AU
33383349 km
12.13 km/s
2049-Apr-07 10:52 0.036074 AU
5396558 km
4.08 km/s
2053-Mar-25 05:53 0.295068 AU
44141602 km
14.35 km/s
2053-Oct-04 20:03 0.299076 AU
44741064 km
9.15 km/s
2057-Nov-28 06:13 0.289060 AU
43242774 km
8.90 km/s
2058-Jun-04 04:54 0.219948 AU
32903691 km
12.43 km/s
2066-Mar-23 13:53 0.207723 AU
31074915 km
13.33 km/s
2071-Jun-02 15:20 0.173666 AU
25980002 km
13.75 km/s
2079-Mar-21 03:10 0.010698 AU
1600334 km
10.82 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
25.42

Orbit Quality

RMS
0.40064
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.

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