SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 QL1

2023 QL1

2023 QL1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.053 AU it takes 1.08 yr to circle the Sun.

Apollo Observations: 56
Orbital Period · P
1.08 yr
v(q)
58.3 km/s
v(Q)
14.5 km/s
Diameter · ≈
0.21 km
TJ
5.58
Eccentricity · e
0.6027

Orbit and dynamics

Between its closest point (0.418 AU) and its farthest (1.688 AU), the heliocentric distance changes by 1.27 AU over every revolution.

One full revolution takes 1.08 yr (395 days), computed from the semi-major axis of 1.053 AU.

The high eccentricity (0.603) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 27.36° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 58.3 km/s at perihelion and falls to 14.5 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 = 21.16 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.21 km.

Observation record and orbit quality

Astrometry from 56 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3525 arcseconds.

Condition code U = 3 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
1.053 AU
Eccentricity
0.6027
Perihelion
0.418 AU
Aphelion
1.687643 AU
Inclination
27.36°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
145.99°

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
2028-Mar-31 01:31 0.392568 AU
58727263 km
22.91 km/s
2029-May-08 11:57 0.493797 AU
73871044 km
30.21 km/s
2036-Aug-28 02:50 0.109073 AU
16317162 km
25.21 km/s
2037-Sep-03 21:55 0.350952 AU
52501672 km
16.11 km/s
2041-Mar-12 01:37 0.438254 AU
65561860 km
24.27 km/s
2042-Apr-25 17:46 0.408358 AU
61089460 km
25.90 km/s
2049-Aug-20 03:38 0.307330 AU
45975847 km
30.81 km/s
2050-Sep-05 14:27 0.156562 AU
23421268 km
18.86 km/s
2054-Feb-20 04:16 0.499171 AU
74674902 km
27.07 km/s
2055-Apr-08 15:21 0.383944 AU
57437190 km
23.14 km/s
2062-Aug-11 22:11 0.492486 AU
73674833 km
36.39 km/s
2063-Aug-31 15:06 0.038886 AU
5817191 km
23.33 km/s
2064-Aug-31 23:48 0.410481 AU
61407124 km
15.83 km/s
2068-Mar-18 05:22 0.421644 AU
63077061 km
23.65 km/s
2069-Apr-30 00:09 0.430661 AU
64425940 km
27.13 km/s
2076-Aug-21 22:06 0.264874 AU
39624658 km
29.56 km/s
2077-Sep-05 22:44 0.197820 AU
29593484 km
18.07 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
21.16

Orbit Quality

RMS
0.35254
Condition
3
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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