SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 FC5

2022 FC5

2022 FC5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.981 AU it takes 2.79 yr to circle the Sun.

Apollo Observations: 52
Orbital Period · P
2.79 yr
v(q)
50.4 km/s
v(Q)
8.9 km/s
Diameter · ≈
0.04 km
TJ
3.5
Eccentricity · e
0.7007

Orbit and dynamics

The path is an ellipse reaching 0.593 AU from the Sun at perihelion and 3.369 AU at aphelion, a radial span of 2.776 AU.

Applying Kepler's third law to a = 1.981 AU gives an orbital period of 2.79 yr, or about 1,018 days.

The high eccentricity (0.701) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 5.12° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 50.4 km/s at perihelion and falls to 8.9 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 = 24.83 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

The current orbit solution is based on 52 observations and has a weighted RMS residual of 0.6301 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
1.981 AU
Eccentricity
0.7007
Perihelion
0.593 AU
Aphelion
3.369087 AU
Inclination
5.12°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
199.02°

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
2036-Feb-04 20:35 0.352690 AU
52761675 km
17.42 km/s
2038-Sep-17 04:13 0.341420 AU
51075741 km
30.62 km/s
2047-Apr-21 23:53 0.398749 AU
59651967 km
32.40 km/s
2049-Dec-04 16:40 0.370168 AU
55376331 km
18.21 km/s
2061-Mar-21 02:32 0.147400 AU
22050775 km
16.25 km/s
2063-Oct-01 20:42 0.063825 AU
9548085 km
22.33 km/s
2075-Jan-14 14:55 0.389393 AU
58252387 km
19.74 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
24.83

Orbit Quality

RMS
0.63007
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.

Keep exploring

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