SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 TM22

2023 TM22

2023 TM22 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.962 AU and a period of 0.94 yr.

Aten Observations: 22
Orbital Period · P
0.94 yr
v(q)
46.7 km/s
v(Q)
19.7 km/s
Diameter · ≈
0.06 km
TJ
6.12
Eccentricity · e
0.4071

Orbit and dynamics

The path is an ellipse reaching 0.571 AU from the Sun at perihelion and 1.354 AU at aphelion, a radial span of 0.783 AU.

Applying Kepler's third law to a = 0.962 AU gives an orbital period of 0.94 yr, or about 345 days.

The high eccentricity (0.407) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 24.38° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 46.7 km/s at perihelion and falls to 19.7 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 = 24.05 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

The current orbit solution is based on 22 observations and has a weighted RMS residual of 0.528 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
0.9624 AU
Eccentricity
0.4071
Perihelion
0.571 AU
Aphelion
1.354193 AU
Inclination
24.38°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
205.72°

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
2040-Oct-22 18:34 0.011443 AU
1711786 km
16.08 km/s
2041-Oct-12 05:30 0.109525 AU
16384727 km
24.10 km/s
2053-Jun-02 10:41 0.304840 AU
45603357 km
20.37 km/s
2054-May-01 20:56 0.294607 AU
44072593 km
17.83 km/s
2055-Mar-26 10:11 0.405854 AU
60714819 km
19.30 km/s
2056-Oct-09 09:00 0.376783 AU
56365866 km
12.91 km/s
2057-Oct-23 20:08 0.075600 AU
11309560 km
15.13 km/s
2058-Oct-14 14:10 0.221067 AU
33071107 km
22.70 km/s
2074-Oct-24 04:06 0.041465 AU
6203043 km
13.94 km/s
2075-Oct-17 20:57 0.015675 AU
2344957 km
20.59 km/s
2076-Oct-04 00:28 0.260177 AU
38921964 km
29.50 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
24.05

Orbit Quality

RMS
0.52797
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.

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