SpaceAtlas Space Object Data
NASA JPL SBDB · 2004 VZ14

2004 VZ14

2004 VZ14 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.529 AU it takes 1.89 yr to circle the Sun.

Apollo Observations: 127
Orbital Period · P
1.89 yr
v(q)
43.2 km/s
v(Q)
13.4 km/s
Diameter · ≈
0.03 km
TJ
4.32
Eccentricity · e
0.5255

Orbit and dynamics

Between its closest point (0.725 AU) and its farthest (2.332 AU), the heliocentric distance changes by 1.607 AU over every revolution.

One full revolution takes 1.89 yr (691 days), computed from the semi-major axis of 1.529 AU.

The high eccentricity (0.525) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.61° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 43.2 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 = 25.04 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 127 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4853 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
1.529 AU
Eccentricity
0.5255
Perihelion
0.725 AU
Aphelion
2.332489 AU
Inclination
4.61°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
161.37°

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
2027-May-05 12:04 0.326259 AU
48807652 km
24.79 km/s
2040-Nov-04 08:13 0.043887 AU
6565404 km
16.55 km/s
2042-Jul-27 19:48 0.286889 AU
42918024 km
13.33 km/s
2044-May-08 18:08 0.250530 AU
37478714 km
22.52 km/s
2057-Nov-14 03:04 0.217632 AU
32557314 km
21.73 km/s
2059-Aug-23 10:15 0.291127 AU
43552023 km
13.67 km/s
2061-May-18 00:35 0.086519 AU
12943123 km
17.61 km/s
2074-Nov-19 16:29 0.320150 AU
47893801 km
24.83 km/s
2076-Sep-05 03:47 0.275577 AU
41225750 km
13.03 km/s
2078-May-22 07:30 0.034781 AU
5203178 km
15.71 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
25.04

Orbit Quality

RMS
0.48527
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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