SpaceAtlas Space Object Data
NASA JPL SBDB · 2002 VR14

2002 VR14

2002 VR14 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.628 AU it takes 2.08 yr to circle the Sun.

Apollo Observations: 35
Orbital Period · P
2.08 yr
v(q)
40.4 km/s
v(Q)
13.5 km/s
Diameter · ≈
0.12 km
TJ
4.16
Eccentricity · e
0.4994

Orbit and dynamics

The path is an ellipse reaching 0.815 AU from the Sun at perihelion and 2.441 AU at aphelion, a radial span of 1.626 AU.

Applying Kepler's third law to a = 1.628 AU gives an orbital period of 2.08 yr, or about 759 days.

The high eccentricity (0.499) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 5.53° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 40.4 km/s at perihelion and falls to 13.5 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 = 22.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

The current orbit solution is based on 35 observations and has a weighted RMS residual of 0.5192 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.628 AU
Eccentricity
0.4994
Perihelion
0.815 AU
Aphelion
2.441023 AU
Inclination
5.53°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
99.01°

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-Oct-27 23:28 0.295750 AU
44243571 km
24.35 km/s
2034-Apr-21 04:07 0.336845 AU
50391252 km
24.92 km/s
2054-Oct-30 14:24 0.280491 AU
41960912 km
22.84 km/s
2059-Mar-25 11:00 0.091340 AU
13664281 km
11.93 km/s
2061-Apr-23 14:08 0.422802 AU
63250246 km
26.32 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
22.4

Orbit Quality

RMS
0.51919
Condition
6
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.

Keep exploring

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