SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 VN2

2017 VN2

2017 VN2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.894 AU and a period of 0.85 yr.

Aten Observations: 66
Orbital Period · P
0.85 yr
v(q)
38.8 km/s
v(Q)
25.6 km/s
Diameter · ≈
0.01 km
TJ
6.63
Eccentricity · e
0.2055

Orbit and dynamics

The path is an ellipse reaching 0.711 AU from the Sun at perihelion and 1.078 AU at aphelion, a radial span of 0.367 AU.

Applying Kepler's third law to a = 0.894 AU gives an orbital period of 0.85 yr, or about 309 days.

An eccentricity of 0.205 makes the orbit moderately elongated.

Its inclination of 1.39° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.8 km/s at perihelion and falls to 25.6 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 = 27.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 66 observations and has a weighted RMS residual of 0.5089 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
0.8943 AU
Eccentricity
0.2055
Perihelion
0.711 AU
Aphelion
1.078079 AU
Inclination
1.39°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
287.19°

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-May-27 13:56 0.238165 AU
35628953 km
6.46 km/s
2028-Nov-20 04:26 0.005429 AU
812166 km
5.53 km/s
2038-Aug-19 23:46 0.027679 AU
4140704 km
7.21 km/s
2043-Aug-24 20:44 0.033725 AU
5045256 km
12.91 km/s
2044-Nov-08 06:16 0.188659 AU
28222992 km
19.09 km/s
2048-Aug-31 04:41 0.247403 AU
37010907 km
18.47 km/s
2049-Nov-15 20:23 0.104127 AU
15577232 km
13.52 km/s
2054-May-17 20:51 0.258356 AU
38649452 km
7.50 km/s
2054-Nov-21 12:29 0.065861 AU
9852594 km
8.08 km/s
2069-Aug-20 00:24 0.066722 AU
9981519 km
9.01 km/s
2074-Aug-27 07:10 0.277691 AU
41541938 km
15.53 km/s
2075-Apr-05 02:15 0.292586 AU
43770183 km
9.16 km/s
2075-Nov-12 17:02 0.269633 AU
40336454 km
16.30 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
27.4

Orbit Quality

RMS
0.50885
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.

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