SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 FP4

2025 FP4

2025 FP4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.001 AU it takes 1.00 yr to circle the Sun.

Apollo Observations: 65
Orbital Period · P
1.00 yr
v(q)
39.2 km/s
v(Q)
22.6 km/s
Diameter · ≈
0.06 km
TJ
6.03
Eccentricity · e
0.2682

Orbit and dynamics

The path is an ellipse reaching 0.733 AU from the Sun at perihelion and 1.269 AU at aphelion, a radial span of 0.536 AU.

Applying Kepler's third law to a = 1.001 AU gives an orbital period of 1.00 yr, or about 366 days.

An eccentricity of 0.268 makes the orbit moderately elongated.

The orbital plane is tilted 10.98° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.2 km/s at perihelion and falls to 22.6 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 = 23.69 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 65 observations and has a weighted RMS residual of 0.5285 arcseconds.

Condition code U = 1 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

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
1.001 AU
Eccentricity
0.2682
Perihelion
0.733 AU
Aphelion
1.269468 AU
Inclination
10.98°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
219.29°

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
2031-Feb-21 03:02 0.198395 AU
29679414 km
7.51 km/s
2032-Feb-19 21:01 0.192197 AU
28752237 km
7.47 km/s
2033-Feb-17 22:23 0.186644 AU
27921530 km
7.45 km/s
2034-Feb-17 03:51 0.181612 AU
27168709 km
7.45 km/s
2035-Feb-16 08:12 0.177125 AU
26497594 km
7.44 km/s
2036-Feb-15 17:41 0.172702 AU
25835791 km
7.42 km/s
2037-Feb-14 06:00 0.168706 AU
25238015 km
7.43 km/s
2038-Feb-13 20:56 0.165773 AU
24799241 km
7.43 km/s
2039-Feb-13 23:52 0.164848 AU
24660917 km
7.42 km/s
2040-Feb-14 04:39 0.164503 AU
24609296 km
7.44 km/s
2041-Feb-13 11:33 0.165110 AU
24700071 km
7.42 km/s
2042-Feb-14 02:20 0.166458 AU
24901690 km
7.43 km/s
2043-Feb-14 15:54 0.168487 AU
25205349 km
7.44 km/s
2044-Feb-15 09:26 0.170974 AU
25577413 km
7.42 km/s
2045-Feb-15 08:13 0.174064 AU
26039531 km
7.45 km/s
2046-Feb-16 08:55 0.178121 AU
26646577 km
7.44 km/s
2047-Feb-17 21:56 0.183734 AU
27486283 km
7.46 km/s
2048-Feb-19 09:28 0.189562 AU
28358144 km
7.49 km/s
2049-Feb-20 02:19 0.195984 AU
29318768 km
7.50 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
23.69

Orbit Quality

RMS
0.52848
Condition
1
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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