SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 VG64

2015 VG64

2015 VG64 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.425 AU it takes 1.70 yr to circle the Sun.

Apollo Observations: 140
Orbital Period · P
1.70 yr
v(q)
47.6 km/s
v(Q)
13.1 km/s
Diameter · ≈
0.16 km
TJ
4.51
Eccentricity · e
0.5681

Orbit and dynamics

The path is an ellipse reaching 0.615 AU from the Sun at perihelion and 2.235 AU at aphelion, a radial span of 1.62 AU.

Applying Kepler's third law to a = 1.425 AU gives an orbital period of 1.70 yr, or about 621 days.

The high eccentricity (0.568) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.29° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 47.6 km/s at perihelion and falls to 13.1 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 = 21.76 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.16 km.

Observation record and orbit quality

The current orbit solution is based on 140 observations and has a weighted RMS residual of 0.4587 arcseconds.

Condition code U = 1 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
1.425 AU
Eccentricity
0.5681
Perihelion
0.615 AU
Aphelion
2.234543 AU
Inclination
4.29°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
121.56°

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
2027-Jul-31 22:11 0.394276 AU
58982805 km
18.04 km/s
2032-Oct-22 08:46 0.073268 AU
10960753 km
17.95 km/s
2034-Mar-26 10:15 0.358028 AU
53560155 km
28.26 km/s
2039-May-17 16:31 0.286384 AU
42842463 km
12.09 km/s
2044-Aug-09 14:50 0.382575 AU
57232439 km
17.36 km/s
2049-Oct-27 10:11 0.122008 AU
18252176 km
20.64 km/s
2051-Mar-31 03:49 0.268755 AU
40205163 km
25.47 km/s
2056-Jun-04 08:43 0.340472 AU
50933824 km
14.59 km/s
2061-Aug-24 09:36 0.353988 AU
52955898 km
15.69 km/s
2066-Nov-02 20:07 0.234522 AU
35083998 km
24.41 km/s
2068-Apr-05 11:54 0.151627 AU
22683027 km
21.69 km/s
2073-Jun-22 02:58 0.379138 AU
56718266 km
16.90 km/s
2078-Sep-12 00:44 0.302105 AU
45194244 km
13.11 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
21.76

Orbit Quality

RMS
0.45866
Condition
1
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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