SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 GT

2022 GT

2022 GT belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.453 AU it takes 1.75 yr to circle the Sun.

Apollo Observations: 52
Orbital Period · P
1.75 yr
v(q)
33.7 km/s
v(Q)
18.1 km/s
Diameter · ≈
0.02 km
TJ
4.59
Eccentricity · e
0.3003

Orbit and dynamics

Between its closest point (1.016 AU) and its farthest (1.889 AU), the heliocentric distance changes by 0.873 AU over every revolution.

One full revolution takes 1.75 yr (640 days), computed from the semi-major axis of 1.453 AU.

An eccentricity of 0.3 makes the orbit moderately elongated.

Its inclination of 0.53° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.7 km/s at perihelion and falls to 18.1 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 26.69 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 52 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5323 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
1.453 AU
Eccentricity
0.3003
Perihelion
1.016 AU
Aphelion
1.889336 AU
Inclination
0.53°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
128.57°

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-Mar-15 18:35 0.204430 AU
30582323 km
11.31 km/s
2036-Jul-07 00:00 0.331366 AU
49571675 km
1.91 km/s
2043-Mar-02 22:58 0.445119 AU
66588901 km
18.84 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
26.69

Orbit Quality

RMS
0.53228
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.

Keep exploring

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