SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 TO1

2022 TO1

2022 TO1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.509 AU it takes 1.85 yr to circle the Sun.

Apollo Observations: 65
Orbital Period · P
1.85 yr
v(q)
46.7 km/s
v(Q)
12.6 km/s
Diameter · ≈
0.37 km
TJ
4.29
Eccentricity · e
0.5758

Orbit and dynamics

Between its closest point (0.64 AU) and its farthest (2.378 AU), the heliocentric distance changes by 1.738 AU over every revolution.

One full revolution takes 1.85 yr (677 days), computed from the semi-major axis of 1.509 AU.

The high eccentricity (0.576) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 18.13° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 46.7 km/s at perihelion and falls to 12.6 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 = 19.92 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.37 km.

Observation record and orbit quality

Astrometry from 65 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4695 arcseconds.

Condition code U = 0 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

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
1.509 AU
Eccentricity
0.5758
Perihelion
0.64 AU
Aphelion
2.377882 AU
Inclination
18.13°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
41.33°

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
2033-Oct-09 22:06 0.437090 AU
65387807 km
26.75 km/s
2035-Jul-05 11:43 0.377955 AU
56541278 km
20.67 km/s
2037-Mar-23 09:55 0.325776 AU
48735405 km
21.08 km/s
2046-Oct-03 04:39 0.360078 AU
53866955 km
22.90 km/s
2048-Jun-20 12:58 0.375920 AU
56236855 km
20.94 km/s
2050-Mar-15 13:00 0.388725 AU
58152370 km
24.82 km/s
2059-Sep-25 12:52 0.317650 AU
47519746 km
19.25 km/s
2061-Jun-08 01:20 0.369035 AU
55206885 km
20.56 km/s
2063-Mar-09 06:06 0.469816 AU
70283455 km
28.34 km/s
2072-Sep-15 07:32 0.315208 AU
47154510 km
16.47 km/s
2074-May-27 14:42 0.358469 AU
53626247 km
19.73 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
19.92

Orbit Quality

RMS
0.46953
Condition
0
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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