SpaceAtlas Space Object Data
NASA JPL SBDB · 2021 LO3

2021 LO3

2021 LO3 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.789 AU and a period of 0.70 yr.

Aten Observations: 25
Orbital Period · P
0.70 yr
v(q)
57.2 km/s
v(Q)
19.7 km/s
Diameter · ≈
0.06 km
TJ
7.28
Eccentricity · e
0.4884

Orbit and dynamics

Between its closest point (0.404 AU) and its farthest (1.174 AU), the heliocentric distance changes by 0.77 AU over every revolution.

One full revolution takes 0.70 yr (256 days), computed from the semi-major axis of 0.789 AU.

The high eccentricity (0.488) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.96° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 57.2 km/s at perihelion and falls to 19.7 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 = 23.91 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

Astrometry from 25 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5251 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
0.7887 AU
Eccentricity
0.4884
Perihelion
0.404 AU
Aphelion
1.173901 AU
Inclination
3.96°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
235.25°

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
2028-Jun-06 15:58 0.173922 AU
26018341 km
9.68 km/s
2030-May-07 02:59 0.176112 AU
26345992 km
20.38 km/s
2033-Jul-07 05:55 0.153332 AU
22938120 km
19.78 km/s
2037-May-07 23:52 0.153088 AU
22901641 km
21.27 km/s
2040-Jul-08 04:21 0.093263 AU
13951920 km
18.78 km/s
2044-May-09 06:04 0.161499 AU
24159873 km
22.45 km/s
2047-Jul-09 21:29 0.071738 AU
10731851 km
17.82 km/s
2051-May-10 18:26 0.174110 AU
26046461 km
23.05 km/s
2054-Jul-10 02:31 0.070124 AU
10490447 km
17.36 km/s
2058-May-10 23:31 0.201672 AU
30169728 km
23.37 km/s
2061-Jul-10 04:47 0.073986 AU
11068166 km
17.07 km/s
2065-May-11 04:34 0.234366 AU
35060656 km
23.72 km/s
2068-Jul-10 04:40 0.069400 AU
10382040 km
16.80 km/s
2072-May-11 00:17 0.171854 AU
25708953 km
23.72 km/s
2075-Jul-10 19:08 0.069613 AU
10414011 km
16.99 km/s
2079-May-11 10:26 0.129006 AU
19298952 km
23.43 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
23.91

Orbit Quality

RMS
0.52512
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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