SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 PC2

2022 PC2

2022 PC2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.054 AU it takes 1.08 yr to circle the Sun.

Apollo Observations: 56
Orbital Period · P
1.08 yr
v(q)
32.4 km/s
v(Q)
26 km/s
Diameter · ≈
0.01 km
TJ
5.83
Eccentricity · e
0.1095

Orbit and dynamics

Between its closest point (0.938 AU) and its farthest (1.169 AU), the heliocentric distance changes by 0.231 AU over every revolution.

One full revolution takes 1.08 yr (395 days), computed from the semi-major axis of 1.054 AU.

An eccentricity of 0.11 makes the orbit moderately elongated.

Its inclination of 3.01° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.4 km/s at perihelion and falls to 26 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 = 27.05 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 56 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4466 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
1.054 AU
Eccentricity
0.1095
Perihelion
0.938 AU
Aphelion
1.169413 AU
Inclination
3.01°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
264.14°

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
2034-Feb-19 17:34 0.382417 AU
57208780 km
15.15 km/s
2035-Jan-30 15:27 0.112231 AU
16789463 km
2.88 km/s
2035-May-17 18:09 0.088188 AU
13192807 km
3.00 km/s
2035-Sep-24 18:54 0.137434 AU
20559838 km
2.86 km/s
2036-Aug-23 11:28 0.340841 AU
50989119 km
13.74 km/s
2048-Mar-05 13:45 0.031957 AU
4780657 km
4.18 km/s
2048-Nov-05 00:22 0.180988 AU
27075402 km
3.98 km/s
2049-Aug-17 16:37 0.176077 AU
26340729 km
8.98 km/s
2061-Feb-19 15:30 0.351371 AU
52564314 km
14.76 km/s
2062-Sep-29 01:35 0.133235 AU
19931738 km
2.99 km/s
2063-Aug-23 21:43 0.298504 AU
44655546 km
13.01 km/s
2075-Feb-25 20:36 0.202925 AU
30357197 km
10.11 km/s
2075-Dec-19 00:48 0.169340 AU
25332976 km
3.99 km/s
2076-Aug-03 07:53 0.001574 AU
235430 km
3.55 km/s
2077-Aug-25 08:02 0.279246 AU
41774536 km
15.11 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
27.05

Orbit Quality

RMS
0.44661
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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