SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 RX13

2024 RX13

2024 RX13 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.177 AU it takes 1.28 yr to circle the Sun.

Apollo Observations: 22
Orbital Period · P
1.28 yr
v(q)
33 km/s
v(Q)
22.9 km/s
TJ
5.36
Eccentricity · e
0.1811

Orbit and dynamics

The path is an ellipse reaching 0.964 AU from the Sun at perihelion and 1.39 AU at aphelion, a radial span of 0.426 AU.

Applying Kepler's third law to a = 1.177 AU gives an orbital period of 1.28 yr, or about 466 days.

An eccentricity of 0.181 makes the orbit moderately elongated.

Its inclination of 2.75° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33 km/s at perihelion and falls to 22.9 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

Neither a measured diameter nor a reliable absolute magnitude is available for 2024 RX13, so its physical size remains unconstrained.

Observation record and orbit quality

The current orbit solution is based on 22 observations and has a weighted RMS residual of 0.3065 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
1.177 AU
Eccentricity
0.1811
Perihelion
0.964 AU
Aphelion
1.390155 AU
Inclination
2.75°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
161.98°

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
2029-Feb-01 06:02 0.403265 AU
60327542 km
7.39 km/s
2033-May-19 11:47 0.181376 AU
27133429 km
10.17 km/s
2033-Nov-29 21:08 0.310975 AU
46521210 km
5.53 km/s
2038-Mar-13 18:26 0.321575 AU
48107002 km
5.96 km/s
2038-Oct-02 02:51 0.218947 AU
32753949 km
11.78 km/s
2043-Jan-11 18:26 0.400541 AU
59920134 km
7.35 km/s
2052-Feb-17 07:45 0.378401 AU
56607940 km
7.07 km/s
2052-Oct-13 01:53 0.439205 AU
65704134 km
18.94 km/s
2056-May-10 10:42 0.309497 AU
46300084 km
15.21 km/s
2056-Dec-19 04:27 0.354312 AU
53004270 km
6.60 km/s
2061-Sep-21 02:05 0.005061 AU
757183 km
6.83 km/s
2066-Jan-22 17:04 0.407092 AU
60900167 km
7.47 km/s
2070-Jun-01 03:26 0.054931 AU
8217491 km
5.61 km/s
2070-Nov-05 17:28 0.237184 AU
35482280 km
3.77 km/s
2075-Feb-25 14:18 0.357702 AU
53511451 km
6.78 km/s
2075-Oct-10 07:55 0.341425 AU
51076473 km
16.45 km/s
2079-May-07 13:54 0.362015 AU
54156677 km
17.71 km/s
2079-Dec-28 23:34 0.369254 AU
55239586 km
6.96 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
31.06

Orbit Quality

RMS
0.30652
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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