SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 VL1

2017 VL1

2017 VL1 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.951 AU and a period of 0.93 yr.

Aten Observations: 24
Orbital Period · P
0.93 yr
v(q)
42.3 km/s
v(Q)
22.1 km/s
Diameter · ≈
0.02 km
TJ
6.28
Eccentricity · e
0.3136

Orbit and dynamics

The path is an ellipse reaching 0.652 AU from the Sun at perihelion and 1.249 AU at aphelion, a radial span of 0.597 AU.

Applying Kepler's third law to a = 0.951 AU gives an orbital period of 0.93 yr, or about 338 days.

An eccentricity of 0.314 makes the orbit moderately elongated.

Its inclination of 4.34° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 42.3 km/s at perihelion and falls to 22.1 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 = 26.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 24 observations and has a weighted RMS residual of 0.4137 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
0.9505 AU
Eccentricity
0.3136
Perihelion
0.652 AU
Aphelion
1.248577 AU
Inclination
4.34°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
171.29°

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-Nov-19 09:09 0.385771 AU
57710505 km
22.16 km/s
2030-Nov-05 15:13 0.028805 AU
4309099 km
8.73 km/s
2031-Aug-10 04:31 0.340072 AU
50874111 km
11.64 km/s
2032-Jan-04 21:22 0.273408 AU
40901258 km
8.29 km/s
2032-Jun-12 10:04 0.346377 AU
51817201 km
12.17 km/s
2033-Mar-14 04:12 0.081323 AU
12165800 km
7.39 km/s
2034-Feb-28 05:27 0.318170 AU
47597564 km
20.92 km/s
2042-Nov-17 16:13 0.221000 AU
33061166 km
20.84 km/s
2043-Nov-06 21:57 0.010660 AU
1594721 km
7.71 km/s
2046-Mar-14 21:34 0.061775 AU
9241373 km
8.08 km/s
2047-Feb-27 18:55 0.242130 AU
36222148 km
21.52 km/s
2055-Nov-18 00:12 0.186709 AU
27931270 km
20.92 km/s
2056-Nov-05 23:54 0.010326 AU
1544695 km
7.78 km/s
2059-Mar-15 01:25 0.061549 AU
9207564 km
8.02 km/s
2060-Feb-28 01:02 0.233264 AU
34895798 km
21.47 km/s
2068-Nov-16 19:54 0.233538 AU
34936794 km
20.56 km/s
2069-Nov-07 01:55 0.012582 AU
1882239 km
7.47 km/s
2072-Mar-14 04:21 0.062259 AU
9313742 km
8.60 km/s
2073-Feb-26 06:48 0.329657 AU
49316004 km
22.16 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
26.5

Orbit Quality

RMS
0.41374
Condition
7
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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