SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 VD2

2019 VD2

2019 VD2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.972 AU it takes 2.77 yr to circle the Sun.

Apollo Observations: 57
Orbital Period · P
2.77 yr
v(q)
54.3 km/s
v(Q)
8.3 km/s
Diameter · ≈
0.19 km
TJ
3.34
Eccentricity · e
0.7354

Orbit and dynamics

Between its closest point (0.522 AU) and its farthest (3.422 AU), the heliocentric distance changes by 2.9 AU over every revolution.

One full revolution takes 2.77 yr (1,011 days), computed from the semi-major axis of 1.972 AU.

The high eccentricity (0.735) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 33.47° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 54.3 km/s at perihelion and falls to 8.3 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 = 21.31 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.19 km.

Observation record and orbit quality

Astrometry from 57 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5244 arcseconds.

Condition code U = 2 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
1.972 AU
Eccentricity
0.7354
Perihelion
0.522 AU
Aphelion
3.422209 AU
Inclination
33.47°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
155.18°

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
2036-Mar-22 13:04 0.496520 AU
74278297 km
41.69 km/s
2044-Oct-12 10:47 0.392688 AU
58745319 km
19.98 km/s
2047-Apr-17 05:36 0.150653 AU
22537433 km
29.49 km/s
2055-Nov-01 03:31 0.079747 AU
11929968 km
30.43 km/s
2058-May-23 07:46 0.439353 AU
65726260 km
22.77 km/s
2072-Mar-23 12:17 0.473216 AU
70792120 km
41.03 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
21.31

Orbit Quality

RMS
0.52437
Condition
2
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.