SpaceAtlas Space Object Data
NASA JPL SBDB · 2021 LL2

2021 LL2

2021 LL2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.727 AU it takes 2.27 yr to circle the Sun.

Apollo Observations: 66
Orbital Period · P
2.27 yr
v(q)
55.5 km/s
v(Q)
9.3 km/s
Diameter · ≈
0.17 km
TJ
3.82
Eccentricity · e
0.714

Orbit and dynamics

The path is an ellipse reaching 0.494 AU from the Sun at perihelion and 2.96 AU at aphelion, a radial span of 2.466 AU.

Applying Kepler's third law to a = 1.727 AU gives an orbital period of 2.27 yr, or about 829 days.

The high eccentricity (0.714) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.11° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 55.5 km/s at perihelion and falls to 9.3 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 = 21.58 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.17 km.

Observation record and orbit quality

The current orbit solution is based on 66 observations and has a weighted RMS residual of 0.7132 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
1.727 AU
Eccentricity
0.714
Perihelion
0.494 AU
Aphelion
2.960078 AU
Inclination
3.11°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
45.02°

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-Aug-01 21:56 0.331714 AU
49623709 km
13.85 km/s
2033-Feb-01 07:53 0.132728 AU
19855878 km
26.29 km/s
2039-Oct-05 19:57 0.499652 AU
74746873 km
25.15 km/s
2046-Jun-18 01:29 0.325419 AU
48682004 km
32.21 km/s
2048-Nov-23 23:08 0.445119 AU
66588804 km
21.06 km/s
2055-Jul-13 01:14 0.163931 AU
24523717 km
18.04 km/s
2058-Jan-23 23:16 0.079511 AU
11894676 km
20.85 km/s
2064-Sep-16 03:45 0.475048 AU
71066136 km
22.49 km/s
2067-Feb-16 21:31 0.433880 AU
64907571 km
35.87 km/s
2073-Nov-02 22:39 0.490374 AU
73358866 km
24.75 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
21.58

Orbit Quality

RMS
0.71316
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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