SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 FS1

2024 FS1

2024 FS1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.065 AU it takes 1.10 yr to circle the Sun.

Apollo Observations: 33
Orbital Period · P
1.10 yr
v(q)
39.1 km/s
v(Q)
21.3 km/s
Diameter · ≈
0.07 km
TJ
5.71
Eccentricity · e
0.2955

Orbit and dynamics

The path is an ellipse reaching 0.75 AU from the Sun at perihelion and 1.38 AU at aphelion, a radial span of 0.63 AU.

Applying Kepler's third law to a = 1.065 AU gives an orbital period of 1.10 yr, or about 401 days.

An eccentricity of 0.295 makes the orbit moderately elongated.

The orbital plane is tilted 18.3° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.1 km/s at perihelion and falls to 21.3 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 = 23.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.07 km.

Observation record and orbit quality

The current orbit solution is based on 33 observations and has a weighted RMS residual of 0.4341 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
1.065 AU
Eccentricity
0.2955
Perihelion
0.75 AU
Aphelion
1.379708 AU
Inclination
18.3°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
287.85°

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
2035-Mar-26 16:03 0.109711 AU
16412564 km
13.35 km/s
2036-Feb-15 10:09 0.399864 AU
59818852 km
10.83 km/s
2037-Oct-18 22:37 0.192966 AU
28867266 km
18.09 km/s
2046-Mar-26 06:41 0.111361 AU
16659356 km
14.06 km/s
2048-Oct-16 11:02 0.139480 AU
20865946 km
17.26 km/s
2057-Mar-25 11:03 0.113851 AU
17031932 km
15.09 km/s
2068-Mar-24 05:28 0.116978 AU
17499642 km
16.37 km/s
2079-Mar-23 10:41 0.124134 AU
18570213 km
17.99 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
23.6

Orbit Quality

RMS
0.4341
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.