SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 VS7

2019 VS7

2019 VS7 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.492 AU it takes 3.93 yr to circle the Sun.

Apollo Observations: 51
Orbital Period · P
3.93 yr
v(q)
41.1 km/s
v(Q)
8.7 km/s
Diameter · ≈
0.69 km
TJ
2.99
Eccentricity · e
0.6521

Orbit and dynamics

The path is an ellipse reaching 0.867 AU from the Sun at perihelion and 4.117 AU at aphelion, a radial span of 3.25 AU.

Applying Kepler's third law to a = 2.492 AU gives an orbital period of 3.93 yr, or about 1,437 days.

The high eccentricity (0.652) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 30.26° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 41.1 km/s at perihelion and falls to 8.7 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 = 18.55 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.69 km.

Observation record and orbit quality

The current orbit solution is based on 51 observations and has a weighted RMS residual of 0.6403 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
2.492 AU
Eccentricity
0.6521
Perihelion
0.867 AU
Aphelion
4.117033 AU
Inclination
30.26°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
192.47°

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-Jun-02 04:21 0.321529 AU
48100029 km
22.65 km/s
2032-Jan-16 04:26 0.371844 AU
55627093 km
16.49 km/s
2032-May-24 06:44 0.443474 AU
66342815 km
15.61 km/s
2036-Jan-04 04:19 0.225535 AU
33739572 km
23.49 km/s
2079-Jun-06 20:21 0.335756 AU
50228405 km
25.42 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
18.55

Orbit Quality

RMS
0.64031
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.

Keep exploring

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