SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 PO

2024 PO

2024 PO belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.176 AU it takes 1.28 yr to circle the Sun.

Apollo Observations: 42
Orbital Period · P
1.28 yr
v(q)
31.6 km/s
v(Q)
23.9 km/s
Diameter · ≈
0.01 km
TJ
5.3
Eccentricity · e
0.1398

Orbit and dynamics

Between its closest point (1.012 AU) and its farthest (1.34 AU), the heliocentric distance changes by 0.328 AU over every revolution.

One full revolution takes 1.28 yr (466 days), computed from the semi-major axis of 1.176 AU.

An eccentricity of 0.14 makes the orbit moderately elongated.

A steep inclination of 21.24° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 31.6 km/s at perihelion and falls to 23.9 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 26.96 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 42 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4265 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
1.176 AU
Eccentricity
0.1398
Perihelion
1.012 AU
Aphelion
1.340405 AU
Inclination
21.24°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
179.63°

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
2029-Jan-29 08:35 0.344128 AU
51480880 km
11.67 km/s
2033-Jul-09 10:07 0.379486 AU
56770325 km
15.62 km/s
2033-Dec-11 14:21 0.470474 AU
70381848 km
9.15 km/s
2038-Feb-24 14:19 0.327762 AU
49032454 km
11.30 km/s
2038-Aug-14 12:37 0.124596 AU
18639360 km
13.70 km/s
2043-Jan-17 07:38 0.377802 AU
56518387 km
11.56 km/s
2047-Jul-23 08:43 0.095199 AU
14241530 km
12.22 km/s
2052-Feb-12 00:39 0.323413 AU
48381887 km
11.55 km/s
2052-Aug-24 05:21 0.265865 AU
39772800 km
17.90 km/s
2061-Aug-03 03:40 0.006318 AU
945101 km
11.41 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
26.96

Orbit Quality

RMS
0.42651
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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