SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 FG2

2022 FG2

2022 FG2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.138 AU it takes 1.21 yr to circle the Sun.

Apollo Observations: 78
Orbital Period · P
1.21 yr
v(q)
34.4 km/s
v(Q)
22.7 km/s
Diameter · ≈
0.07 km
TJ
5.44
Eccentricity · e
0.2048

Orbit and dynamics

Between its closest point (0.905 AU) and its farthest (1.371 AU), the heliocentric distance changes by 0.466 AU over every revolution.

One full revolution takes 1.21 yr (443 days), computed from the semi-major axis of 1.138 AU.

An eccentricity of 0.205 makes the orbit moderately elongated.

The orbital plane is tilted 17.79° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 34.4 km/s at perihelion and falls to 22.7 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

No direct size measurement is available; from an absolute magnitude of H = 23.43 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.07 km.

Observation record and orbit quality

Astrometry from 78 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3582 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.138 AU
Eccentricity
0.2048
Perihelion
0.905 AU
Aphelion
1.371062 AU
Inclination
17.79°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
94.83°

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-24 03:43 0.456715 AU
68323658 km
7.77 km/s
2028-Oct-02 14:06 0.145413 AU
21753483 km
12.61 km/s
2033-Apr-01 23:07 0.341603 AU
51103053 km
19.21 km/s
2039-Apr-19 01:33 0.065058 AU
9732611 km
9.84 km/s
2039-Oct-21 19:25 0.268067 AU
40102236 km
9.46 km/s
2045-Feb-13 12:37 0.466364 AU
69767093 km
7.49 km/s
2045-Oct-03 06:44 0.155801 AU
23307559 km
13.54 km/s
2050-Apr-04 14:59 0.258499 AU
38670879 km
17.69 km/s
2050-Dec-04 07:26 0.473713 AU
70866457 km
8.85 km/s
2056-Apr-19 21:43 0.126793 AU
18967956 km
9.29 km/s
2056-Oct-14 12:59 0.209827 AU
31389600 km
9.44 km/s
2062-Oct-04 23:01 0.213575 AU
31950353 km
15.44 km/s
2067-Apr-08 13:14 0.166611 AU
24924602 km
15.46 km/s
2067-Nov-23 16:13 0.437274 AU
65415285 km
9.17 km/s
2073-Apr-19 12:46 0.227271 AU
33999221 km
9.21 km/s
2073-Oct-08 08:19 0.154825 AU
23161419 km
9.63 km/s
2079-Oct-07 09:43 0.302624 AU
45271882 km
17.60 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
23.43

Orbit Quality

RMS
0.35823
Condition
6
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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