SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 ST4

2023 ST4

2023 ST4 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.511 AU once every 3.98 yr.

Amor Observations: 49
Orbital Period · P
3.98 yr
v(q)
35.2 km/s
v(Q)
10 km/s
Diameter · ≈
0.08 km
TJ
3.22
Eccentricity · e
0.5564

Orbit and dynamics

Between its closest point (1.114 AU) and its farthest (3.908 AU), the heliocentric distance changes by 2.794 AU over every revolution.

One full revolution takes 3.98 yr (1,453 days), computed from the semi-major axis of 2.511 AU.

The high eccentricity (0.556) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.54° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 35.2 km/s at perihelion and falls to 10 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 23.37 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.08 km.

Observation record and orbit quality

Astrometry from 49 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4873 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
2.511 AU
Eccentricity
0.5564
Perihelion
1.114 AU
Aphelion
3.90812 AU
Inclination
3.54°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
237.5°

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-Oct-12 22:23 0.135609 AU
20286831 km
5.74 km/s
2031-Oct-14 11:20 0.141746 AU
21204959 km
5.46 km/s
2035-Oct-07 00:12 0.154437 AU
23103520 km
7.00 km/s
2039-Sep-28 09:32 0.211133 AU
31585081 km
9.88 km/s
2043-Oct-05 08:12 0.181492 AU
27150840 km
8.23 km/s
2047-Oct-03 05:40 0.176101 AU
26344406 km
8.90 km/s
2051-Sep-30 09:10 0.202560 AU
30302541 km
10.21 km/s
2055-Oct-09 19:23 0.156377 AU
23393624 km
7.46 km/s
2059-Oct-11 21:48 0.123389 AU
18458665 km
6.51 km/s
2063-Oct-12 20:25 0.117264 AU
17542512 km
6.27 km/s
2067-Oct-19 06:10 0.149980 AU
22436616 km
4.50 km/s
2071-Oct-22 19:44 0.155629 AU
23281757 km
4.86 km/s
2075-Oct-25 03:30 0.134894 AU
20179785 km
6.02 km/s
2079-Oct-24 09:12 0.179404 AU
26838440 km
8.26 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
23.37

Orbit Quality

RMS
0.48726
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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