SpaceAtlas Space Object Data
NASA JPL SBDB · 2002 LX64

2002 LX64

2002 LX64 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.357 AU it takes 1.58 yr to circle the Sun.

Apollo Observations: 106
Orbital Period · P
1.58 yr
v(q)
48.9 km/s
v(Q)
13.4 km/s
Diameter · ≈
0.2 km
TJ
4.67
Eccentricity · e
0.5707

Orbit and dynamics

The path is an ellipse reaching 0.583 AU from the Sun at perihelion and 2.131 AU at aphelion, a radial span of 1.548 AU.

Applying Kepler's third law to a = 1.357 AU gives an orbital period of 1.58 yr, or about 577 days.

The high eccentricity (0.571) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.85° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 48.9 km/s at perihelion and falls to 13.4 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 = 21.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.2 km.

Observation record and orbit quality

The current orbit solution is based on 106 observations and has a weighted RMS residual of 0.4979 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
1.357 AU
Eccentricity
0.5707
Perihelion
0.583 AU
Aphelion
2.13144 AU
Inclination
4.85°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
104.23°

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-Feb-16 02:41 0.404957 AU
60580734 km
18.67 km/s
2032-Jun-13 17:45 0.132881 AU
19878713 km
21.15 km/s
2036-Nov-26 07:47 0.093098 AU
13927260 km
15.29 km/s
2040-Apr-07 05:52 0.366098 AU
54767510 km
15.23 km/s
2040-Jun-07 21:41 0.454531 AU
67996837 km
8.07 km/s
2044-Oct-28 23:42 0.498885 AU
74632061 km
32.52 km/s
2048-Jan-31 08:43 0.380245 AU
56883785 km
17.20 km/s
2051-Jun-08 07:17 0.041107 AU
6149573 km
17.39 km/s
2055-Nov-20 09:00 0.079193 AU
11847078 km
18.99 km/s
2059-Mar-23 03:10 0.396258 AU
59279284 km
17.47 km/s
2062-Jun-28 17:14 0.424989 AU
63577468 km
29.98 km/s
2067-Jan-12 13:35 0.333521 AU
49893970 km
14.42 km/s
2070-May-31 08:46 0.147224 AU
22024454 km
13.32 km/s
2074-Nov-12 15:00 0.214652 AU
32111505 km
23.66 km/s
2078-Mar-04 15:12 0.410733 AU
61444746 km
18.84 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
21.2

Orbit Quality

RMS
0.49792
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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