SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 OD4

2022 OD4

2022 OD4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.472 AU it takes 1.79 yr to circle the Sun.

Apollo Observations: 45
Orbital Period · P
1.79 yr
v(q)
47.7 km/s
v(Q)
12.6 km/s
Diameter · ≈
0.24 km
TJ
4.37
Eccentricity · e
0.5809

Orbit and dynamics

The path is an ellipse reaching 0.617 AU from the Sun at perihelion and 2.327 AU at aphelion, a radial span of 1.71 AU.

Applying Kepler's third law to a = 1.472 AU gives an orbital period of 1.79 yr, or about 652 days.

The high eccentricity (0.581) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 14.25° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 47.7 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 = 20.84 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.24 km.

Observation record and orbit quality

The current orbit solution is based on 45 observations and has a weighted RMS residual of 0.6018 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
1.472 AU
Eccentricity
0.5809
Perihelion
0.617 AU
Aphelion
2.327085 AU
Inclination
14.25°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
335.9°

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-Apr-03 09:20 0.322064 AU
48180093 km
25.06 km/s
2031-Oct-27 11:15 0.337456 AU
50482650 km
11.91 km/s
2039-Feb-23 18:07 0.246465 AU
36870693 km
15.45 km/s
2040-Sep-10 04:17 0.262684 AU
39296906 km
22.81 km/s
2047-Dec-25 20:31 0.382801 AU
57266280 km
19.09 km/s
2055-Mar-28 15:55 0.249509 AU
37326004 km
22.13 km/s
2056-Sep-26 03:15 0.246496 AU
36875333 km
13.22 km/s
2064-Jan-24 08:30 0.333214 AU
49848078 km
17.74 km/s
2065-Aug-30 07:03 0.460856 AU
68943151 km
29.91 km/s
2071-Apr-09 14:20 0.406830 AU
60860947 km
27.98 km/s
2072-Nov-12 01:07 0.365653 AU
54700973 km
14.61 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
20.84

Orbit Quality

RMS
0.60182
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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