SpaceAtlas Space Object Data
NASA JPL SBDB · 2002 RZ125

2002 RZ125

2002 RZ125 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.414 AU it takes 1.68 yr to circle the Sun.

Apollo Observations: 45
Orbital Period · P
1.68 yr
v(q)
45.5 km/s
v(Q)
13.8 km/s
Diameter · ≈
0.3 km
TJ
4.45
Eccentricity · e
0.5346

Orbit and dynamics

Between its closest point (0.658 AU) and its farthest (2.17 AU), the heliocentric distance changes by 1.512 AU over every revolution.

One full revolution takes 1.68 yr (614 days), computed from the semi-major axis of 1.414 AU.

The high eccentricity (0.535) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 28.95° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 45.5 km/s at perihelion and falls to 13.8 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 = 20.35 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.3 km.

Observation record and orbit quality

Astrometry from 45 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5616 arcseconds.

Condition code U = 2 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
1.414 AU
Eccentricity
0.5346
Perihelion
0.658 AU
Aphelion
2.169924 AU
Inclination
28.95°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
93.43°

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-May-06 09:42 0.489493 AU
73227061 km
19.94 km/s
2034-Aug-25 05:26 0.391788 AU
58610651 km
16.05 km/s
2039-Aug-25 05:53 0.234332 AU
35055507 km
19.65 km/s
2044-Sep-01 01:19 0.312845 AU
46801018 km
26.02 km/s
2046-Jan-29 06:27 0.494395 AU
73960463 km
33.46 km/s
2051-Feb-14 06:13 0.263037 AU
39349728 km
26.65 km/s
2056-Mar-04 15:49 0.180831 AU
27051976 km
21.61 km/s
2061-Mar-31 23:11 0.340256 AU
50901618 km
20.08 km/s
2066-May-06 13:24 0.489234 AU
73188380 km
19.94 km/s
2071-Aug-25 17:22 0.394557 AU
59024933 km
16.01 km/s
2076-Aug-24 09:02 0.236804 AU
35425357 km
19.29 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
20.35

Orbit Quality

RMS
0.56159
Condition
2
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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