SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 DO1

2024 DO1

2024 DO1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.468 AU it takes 1.78 yr to circle the Sun.

Apollo Observations: 32
Orbital Period · P
1.78 yr
v(q)
40.4 km/s
v(Q)
14.9 km/s
Diameter · ≈
0.11 km
TJ
4.48
Eccentricity · e
0.4601

Orbit and dynamics

Between its closest point (0.792 AU) and its farthest (2.143 AU), the heliocentric distance changes by 1.351 AU over every revolution.

One full revolution takes 1.78 yr (650 days), computed from the semi-major axis of 1.468 AU.

The high eccentricity (0.46) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 7.37° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 40.4 km/s at perihelion and falls to 14.9 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 = 22.62 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

Astrometry from 32 individual observations underpins this orbit; the fit leaves an RMS residual of 0.7521 arcseconds.

Condition code U = 6 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
1.468 AU
Eccentricity
0.4601
Perihelion
0.792 AU
Aphelion
2.143427 AU
Inclination
7.37°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
67.43°

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
2031-Jul-09 15:34 0.176023 AU
26332616 km
10.13 km/s
2038-Sep-07 19:11 0.469926 AU
70299978 km
27.26 km/s
2040-Mar-11 02:15 0.110156 AU
16479076 km
15.23 km/s
2047-Jul-14 20:29 0.148320 AU
22188329 km
10.00 km/s
2054-Sep-08 04:22 0.461587 AU
69052431 km
27.40 km/s
2056-Mar-11 08:27 0.104437 AU
15623532 km
15.18 km/s
2063-Jul-11 05:56 0.157759 AU
23600476 km
10.10 km/s
2070-Sep-06 07:53 0.424681 AU
63531421 km
26.22 km/s
2072-Mar-08 22:29 0.131494 AU
19671194 km
16.52 km/s
2079-Jun-27 20:00 0.201958 AU
30212422 km
10.63 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
22.62

Orbit Quality

RMS
0.75209
Condition
6
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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