SpaceAtlas Space Object Data
NASA JPL SBDB · 2003 XJ7

2003 XJ7

2003 XJ7 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.243 AU it takes 1.39 yr to circle the Sun.

Apollo Observations: 35
Orbital Period · P
1.39 yr
v(q)
44.3 km/s
v(Q)
16.1 km/s
Diameter · ≈
0.02 km
TJ
5.01
Eccentricity · e
0.4657

Orbit and dynamics

The path is an ellipse reaching 0.664 AU from the Sun at perihelion and 1.822 AU at aphelion, a radial span of 1.158 AU.

Applying Kepler's third law to a = 1.243 AU gives an orbital period of 1.39 yr, or about 506 days.

The high eccentricity (0.466) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 18.17° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44.3 km/s at perihelion and falls to 16.1 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 = 26.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 35 observations and has a weighted RMS residual of 0.4002 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
1.243 AU
Eccentricity
0.4657
Perihelion
0.664 AU
Aphelion
1.821865 AU
Inclination
18.17°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
48.14°

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-Nov-18 13:27 0.269919 AU
40379310 km
27.26 km/s
2037-Jun-25 15:24 0.216704 AU
32418506 km
25.01 km/s
2039-Dec-13 04:03 0.018553 AU
2775464 km
13.64 km/s
2044-Jun-01 18:09 0.043026 AU
6436661 km
13.85 km/s
2046-Nov-21 21:00 0.226961 AU
33952845 km
25.54 km/s
2055-Jun-28 18:30 0.302118 AU
45196230 km
26.50 km/s
2057-Dec-15 15:24 0.115319 AU
17251508 km
12.46 km/s
2062-Jun-05 11:53 0.038465 AU
5754335 km
14.93 km/s
2064-Nov-23 11:20 0.230469 AU
34477664 km
24.24 km/s
2069-Mar-21 22:57 0.404241 AU
60473538 km
14.08 km/s
2073-Jun-29 21:28 0.391765 AU
58607213 km
27.39 km/s
2075-Dec-18 00:11 0.212133 AU
31734719 km
11.83 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
26.4

Orbit Quality

RMS
0.40018
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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