SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 RT5

2024 RT5

2024 RT5 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.833 AU and a period of 0.76 yr.

Aten Observations: 13
Orbital Period · P
0.76 yr
v(q)
57.2 km/s
v(Q)
18.6 km/s
Diameter · ≈
0.06 km
TJ
6.92
Eccentricity · e
0.5086

Orbit and dynamics

The path is an ellipse reaching 0.409 AU from the Sun at perihelion and 1.256 AU at aphelion, a radial span of 0.847 AU.

Applying Kepler's third law to a = 0.833 AU gives an orbital period of 0.76 yr, or about 277 days.

The high eccentricity (0.509) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 14.84° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 57.2 km/s at perihelion and falls to 18.6 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 = 23.92 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

The current orbit solution is based on 13 observations and has a weighted RMS residual of 0.7627 arcseconds.

Condition code U = 7 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
0.8325 AU
Eccentricity
0.5086
Perihelion
0.409 AU
Aphelion
1.25591 AU
Inclination
14.84°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
267.08°

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-Aug-11 18:40 0.077278 AU
11560638 km
13.39 km/s
2030-Aug-11 01:32 0.081197 AU
12146922 km
18.54 km/s
2031-Oct-18 17:16 0.350333 AU
52409142 km
24.23 km/s
2033-Aug-17 18:40 0.248654 AU
37198062 km
25.16 km/s
2034-Oct-25 22:55 0.232125 AU
34725389 km
17.08 km/s
2049-Aug-09 18:58 0.057078 AU
8538688 km
16.84 km/s
2052-Aug-15 10:46 0.057737 AU
8637311 km
23.31 km/s
2053-Oct-24 06:26 0.226660 AU
33907861 km
18.99 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
23.92

Orbit Quality

RMS
0.76265
Condition
7
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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