SpaceAtlas Space Object Data
NASA JPL SBDB · 2021 FP2

2021 FP2

2021 FP2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.147 AU it takes 1.23 yr to circle the Sun.

Apollo Observations: 16
Orbital Period · P
1.23 yr
v(q)
37.4 km/s
v(Q)
20.7 km/s
TJ
5.44
Eccentricity · e
0.2884

Orbit and dynamics

Between its closest point (0.816 AU) and its farthest (1.478 AU), the heliocentric distance changes by 0.662 AU over every revolution.

One full revolution takes 1.23 yr (449 days), computed from the semi-major axis of 1.147 AU.

An eccentricity of 0.288 makes the orbit moderately elongated.

Its inclination of 1.43° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37.4 km/s at perihelion and falls to 20.7 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 2021 FP2, so its physical size remains unconstrained.

Observation record and orbit quality

Astrometry from 16 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4455 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
1.147 AU
Eccentricity
0.2884
Perihelion
0.816 AU
Aphelion
1.477795 AU
Inclination
1.43°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
39.2°

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
2026-Dec-30 03:35 0.472731 AU
70719513 km
9.39 km/s
2027-Sep-14 07:15 0.071247 AU
10658348 km
12.37 km/s
2032-Oct-22 12:07 0.315765 AU
47237788 km
7.03 km/s
2037-Mar-13 05:25 0.084689 AU
12669231 km
14.85 km/s
2037-Dec-05 15:17 0.481811 AU
72077841 km
9.50 km/s
2038-Sep-30 13:37 0.356123 AU
53275206 km
22.85 km/s
2048-Nov-11 15:05 0.405833 AU
60711801 km
8.54 km/s
2053-Mar-02 09:43 0.389542 AU
58274708 km
21.88 km/s
2053-Dec-21 17:48 0.490203 AU
73333293 km
9.54 km/s
2054-Sep-19 19:21 0.211604 AU
31655494 km
15.80 km/s
2059-Feb-04 04:09 0.352415 AU
52720522 km
7.31 km/s
2059-Jun-28 12:20 0.191724 AU
28681435 km
7.95 km/s
2059-Oct-10 01:48 0.279407 AU
41798644 km
5.85 km/s
2064-Mar-16 22:21 0.036510 AU
5461847 km
12.41 km/s
2064-Nov-30 01:34 0.469765 AU
70275911 km
9.34 km/s
2070-Jan-09 09:56 0.427904 AU
64013543 km
9.01 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
30.12

Orbit Quality

RMS
0.44552
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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