SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 RF1

2024 RF1

2024 RF1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.133 AU it takes 1.21 yr to circle the Sun.

Apollo Observations: 26
Orbital Period · P
1.21 yr
v(q)
47.6 km/s
v(Q)
16.5 km/s
Diameter · ≈
0.1 km
TJ
5.38
Eccentricity · e
0.4863

Orbit and dynamics

The path is an ellipse reaching 0.582 AU from the Sun at perihelion and 1.684 AU at aphelion, a radial span of 1.102 AU.

Applying Kepler's third law to a = 1.133 AU gives an orbital period of 1.21 yr, or about 440 days.

The high eccentricity (0.486) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 15.8° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 47.6 km/s at perihelion and falls to 16.5 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 = 22.86 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

The current orbit solution is based on 26 observations and has a weighted RMS residual of 0.7792 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
1.133 AU
Eccentricity
0.4863
Perihelion
0.582 AU
Aphelion
1.683978 AU
Inclination
15.8°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
89.21°

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
2030-Sep-11 18:47 0.352365 AU
52712999 km
11.32 km/s
2030-Nov-20 02:17 0.374578 AU
56036042 km
13.13 km/s
2032-Apr-25 03:22 0.271614 AU
40632900 km
16.14 km/s
2036-Aug-29 20:55 0.442006 AU
66123102 km
12.19 km/s
2036-Dec-15 06:20 0.405832 AU
60711615 km
17.71 km/s
2038-May-07 02:17 0.324769 AU
48584688 km
21.24 km/s
2043-Jan-05 02:07 0.410335 AU
61385174 km
19.66 km/s
2044-May-16 01:05 0.430863 AU
64456154 km
26.40 km/s
2047-Sep-09 09:38 0.386779 AU
57861305 km
26.55 km/s
2049-Jan-24 14:34 0.393527 AU
58870848 km
19.84 km/s
2053-Sep-16 08:01 0.251987 AU
37696689 km
21.29 km/s
2059-Sep-23 01:07 0.218620 AU
32705021 km
16.17 km/s
2065-Sep-23 08:03 0.222881 AU
33342521 km
11.98 km/s
2077-Aug-30 10:15 0.390700 AU
58447817 km
12.18 km/s
2079-May-07 15:46 0.276328 AU
41338019 km
21.25 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
22.86

Orbit Quality

RMS
0.77919
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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