SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 RT

2022 RT

2022 RT belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.36 AU it takes 1.59 yr to circle the Sun.

Apollo Observations: 96
Orbital Period · P
1.59 yr
v(q)
39.4 km/s
v(Q)
16.6 km/s
Diameter · ≈
0.04 km
TJ
4.72
Eccentricity · e
0.4079

Orbit and dynamics

Between its closest point (0.805 AU) and its farthest (1.915 AU), the heliocentric distance changes by 1.11 AU over every revolution.

One full revolution takes 1.59 yr (579 days), computed from the semi-major axis of 1.36 AU.

The high eccentricity (0.408) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 17.37° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.4 km/s at perihelion and falls to 16.6 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 = 24.55 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 96 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3338 arcseconds.

Condition code U = 5 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
1.36 AU
Eccentricity
0.4079
Perihelion
0.805 AU
Aphelion
1.914744 AU
Inclination
17.37°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
169.11°

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
2030-Mar-14 21:46 0.370008 AU
55352432 km
10.08 km/s
2030-Jun-14 13:12 0.338071 AU
50574693 km
10.61 km/s
2038-Mar-19 11:40 0.174893 AU
26163598 km
16.70 km/s
2041-Sep-09 16:09 0.175781 AU
26296520 km
19.18 km/s
2049-Aug-02 02:28 0.239933 AU
35893521 km
10.66 km/s
2057-Mar-23 20:21 0.166844 AU
24959453 km
12.55 km/s
2060-Sep-18 05:50 0.348933 AU
52199667 km
23.95 km/s
2065-Mar-09 16:51 0.377061 AU
56407496 km
23.83 km/s
2068-Aug-25 11:21 0.061290 AU
9168902 km
13.01 km/s
2076-Mar-21 23:36 0.268154 AU
40115202 km
10.30 km/s
2079-Sep-25 12:46 0.488729 AU
73112874 km
27.75 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
24.55

Orbit Quality

RMS
0.33377
Condition
5
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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