SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 FR1

2012 FR1

2012 FR1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.179 AU it takes 3.22 yr to circle the Sun.

Apollo Observations: 161
Orbital Period · P
3.22 yr
v(q)
49 km/s
v(Q)
8.3 km/s
Diameter · ≈
0.53 km
TJ
3.28
Eccentricity · e
0.7099

Orbit and dynamics

Between its closest point (0.632 AU) and its farthest (3.726 AU), the heliocentric distance changes by 3.094 AU over every revolution.

One full revolution takes 3.22 yr (1,175 days), computed from the semi-major axis of 2.179 AU.

The high eccentricity (0.71) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 13.29° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 49 km/s at perihelion and falls to 8.3 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 = 19.12 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.53 km.

Observation record and orbit quality

Astrometry from 161 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4283 arcseconds.

Condition code U = 0 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
2.179 AU
Eccentricity
0.7099
Perihelion
0.632 AU
Aphelion
3.725872 AU
Inclination
13.29°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
180.72°

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
2028-Feb-29 19:08 0.096356 AU
14414630 km
18.46 km/s
2040-Oct-25 04:57 0.297854 AU
44558283 km
14.74 km/s
2044-Mar-26 20:27 0.395684 AU
59193429 km
32.50 km/s
2056-Dec-29 15:52 0.384242 AU
57481765 km
18.03 km/s
2069-Sep-13 22:24 0.126421 AU
18912359 km
24.41 km/s
2073-Mar-04 09:57 0.044701 AU
6687200 km
19.98 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
19.12

Orbit Quality

RMS
0.42828
Condition
0
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

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