SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 VV5

2016 VV5

2016 VV5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.435 AU it takes 1.72 yr to circle the Sun.

Apollo Observations: 66
Orbital Period · P
1.72 yr
v(q)
42.6 km/s
v(Q)
14.5 km/s
Diameter · ≈
0.12 km
TJ
4.53
Eccentricity · e
0.4927

Orbit and dynamics

The path is an ellipse reaching 0.728 AU from the Sun at perihelion and 2.142 AU at aphelion, a radial span of 1.414 AU.

Applying Kepler's third law to a = 1.435 AU gives an orbital period of 1.72 yr, or about 628 days.

The high eccentricity (0.493) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 10.34° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 42.6 km/s at perihelion and falls to 14.5 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 = 22.29 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 66 observations and has a weighted RMS residual of 0.57 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
1.435 AU
Eccentricity
0.4927
Perihelion
0.728 AU
Aphelion
2.142025 AU
Inclination
10.34°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
250.67°

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-Oct-24 13:51 0.087945 AU
13156387 km
17.61 km/s
2035-Jul-08 05:50 0.311962 AU
46668843 km
12.47 km/s
2040-Nov-06 20:04 0.337179 AU
50441288 km
24.99 km/s
2042-Apr-18 21:15 0.360807 AU
53975941 km
25.24 km/s
2047-Aug-23 06:04 0.294460 AU
44050547 km
12.99 km/s
2054-May-04 09:11 0.095276 AU
14253027 km
15.84 km/s
2059-Oct-18 12:03 0.043719 AU
6540344 km
14.62 km/s
2066-Jul-01 21:30 0.303493 AU
45401843 km
11.98 km/s
2071-Nov-09 06:32 0.367221 AU
54935436 km
25.88 km/s
2073-Apr-21 01:36 0.314839 AU
47099311 km
23.84 km/s
2078-Sep-13 18:53 0.240270 AU
35943916 km
11.72 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
22.29

Orbit Quality

RMS
0.56996
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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