SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 RW13

2024 RW13

2024 RW13 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.073 AU it takes 1.11 yr to circle the Sun.

Apollo Observations: 26
Orbital Period · P
1.11 yr
v(q)
54.7 km/s
v(Q)
15.1 km/s
Diameter · ≈
0.01 km
TJ
5.52
Eccentricity · e
0.5676

Orbit and dynamics

Between its closest point (0.464 AU) and its farthest (1.682 AU), the heliocentric distance changes by 1.218 AU over every revolution.

One full revolution takes 1.11 yr (406 days), computed from the semi-major axis of 1.073 AU.

The high eccentricity (0.568) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 27.1° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 54.7 km/s at perihelion and falls to 15.1 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 = 27.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 26 individual observations underpins this orbit; the fit leaves an RMS residual of 0.7027 arcseconds.

Condition code U = 8 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
1.073 AU
Eccentricity
0.5676
Perihelion
0.464 AU
Aphelion
1.682035 AU
Inclination
27.1°
Orbital Period
— yr
Epoch
2460565.5
Mean Anomaly
52.95°

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
2034-Sep-12 03:44 0.002371 AU
354682 km
23.12 km/s
2044-Sep-14 14:15 0.002893 AU
432754 km
25.12 km/s
2051-Feb-22 19:36 0.334610 AU
50056944 km
22.04 km/s
2053-Sep-11 09:47 0.421884 AU
63112937 km
15.26 km/s
2054-Sep-18 12:11 0.170478 AU
25503084 km
27.43 km/s
2060-Jan-09 18:13 0.445550 AU
66653276 km
31.71 km/s
2061-Mar-04 05:50 0.386265 AU
57784371 km
22.50 km/s
2063-Sep-07 06:42 0.299208 AU
44760926 km
15.55 km/s
2064-Sep-22 00:31 0.203276 AU
30409614 km
30.14 km/s
2070-Jan-14 23:26 0.331490 AU
49590160 km
29.24 km/s
2073-Sep-05 01:26 0.108139 AU
16177352 km
16.47 km/s
2074-Sep-26 06:48 0.182371 AU
27282355 km
32.66 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
27.1

Orbit Quality

RMS
0.70272
Condition
8
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.