SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 TK

2022 TK

2022 TK belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.109 AU it takes 1.17 yr to circle the Sun.

Apollo Observations: 29
Orbital Period · P
1.17 yr
v(q)
35.9 km/s
v(Q)
22.2 km/s
Diameter · ≈
0.02 km
TJ
5.59
Eccentricity · e
0.2357

Orbit and dynamics

The path is an ellipse reaching 0.848 AU from the Sun at perihelion and 1.37 AU at aphelion, a radial span of 0.522 AU.

Applying Kepler's third law to a = 1.109 AU gives an orbital period of 1.17 yr, or about 427 days.

An eccentricity of 0.236 makes the orbit moderately elongated.

The orbital plane is tilted 5.04° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 35.9 km/s at perihelion and falls to 22.2 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 = 26.53 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 29 observations and has a weighted RMS residual of 0.3448 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
1.109 AU
Eccentricity
0.2357
Perihelion
0.848 AU
Aphelion
1.370391 AU
Inclination
5.04°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
113.32°

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-Mar-27 14:35 0.305512 AU
45703963 km
17.47 km/s
2029-Jan-16 10:36 0.387124 AU
57912900 km
7.98 km/s
2029-Sep-30 15:28 0.041931 AU
6272808 km
9.99 km/s
2035-Apr-01 15:54 0.191137 AU
28593712 km
14.69 km/s
2036-Jan-08 05:18 0.397456 AU
59458528 km
8.06 km/s
2036-Oct-05 15:19 0.128034 AU
19153582 km
12.95 km/s
2042-Apr-06 04:21 0.078182 AU
11695922 km
11.58 km/s
2042-Dec-29 12:20 0.396736 AU
59350836 km
8.01 km/s
2043-Oct-11 09:29 0.223768 AU
33475220 km
16.01 km/s
2049-Apr-10 08:29 0.034197 AU
5115817 km
8.88 km/s
2049-Dec-21 05:01 0.383789 AU
57413993 km
7.87 km/s
2050-Oct-15 04:45 0.315112 AU
47140010 km
18.44 km/s
2056-Apr-12 10:27 0.034471 AU
5156745 km
7.65 km/s
2056-Dec-16 23:15 0.381505 AU
57072268 km
7.74 km/s
2057-Oct-16 21:33 0.365864 AU
54732441 km
19.62 km/s
2063-Apr-14 23:24 0.034461 AU
5155337 km
6.82 km/s
2064-Oct-18 00:14 0.330813 AU
49488925 km
20.64 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
26.53

Orbit Quality

RMS
0.34481
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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