SpaceAtlas Space Object Data
NASA JPL SBDB · 2004 XJ50

2004 XJ50

2004 XJ50 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.24 AU once every 3.35 yr.

Amor Observations: 95
Orbital Period · P
3.35 yr
v(q)
35 km/s
v(Q)
11.3 km/s
Diameter · ≈
0.49 km
TJ
3.36
Eccentricity · e
0.5117

Orbit and dynamics

Between its closest point (1.094 AU) and its farthest (3.386 AU), the heliocentric distance changes by 2.292 AU over every revolution.

One full revolution takes 3.35 yr (1,225 days), computed from the semi-major axis of 2.24 AU.

The high eccentricity (0.512) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 23.35° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 35 km/s at perihelion and falls to 11.3 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 19.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.49 km.

Observation record and orbit quality

Astrometry from 95 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4686 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
2.24 AU
Eccentricity
0.5117
Perihelion
1.094 AU
Aphelion
3.386208 AU
Inclination
23.35°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
161.57°

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
2051-Aug-27 04:38 0.478915 AU
71644666 km
14.79 km/s
2051-Dec-08 03:13 0.405495 AU
60661160 km
11.95 km/s
2061-Aug-23 00:23 0.482247 AU
72143104 km
9.81 km/s
2061-Dec-07 10:24 0.359462 AU
53774699 km
16.52 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
19.3

Orbit Quality

RMS
0.46861
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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