SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 VF6

2019 VF6

2019 VF6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.23 AU it takes 1.36 yr to circle the Sun.

Apollo Observations: 97
Orbital Period · P
1.36 yr
v(q)
43 km/s
v(Q)
16.8 km/s
Diameter · ≈
0.21 km
TJ
5.08
Eccentricity · e
0.4392

Orbit and dynamics

The path is an ellipse reaching 0.69 AU from the Sun at perihelion and 1.77 AU at aphelion, a radial span of 1.08 AU.

Applying Kepler's third law to a = 1.23 AU gives an orbital period of 1.36 yr, or about 498 days.

The high eccentricity (0.439) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 14.91° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 43 km/s at perihelion and falls to 16.8 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 = 21.16 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.21 km.

Observation record and orbit quality

The current orbit solution is based on 97 observations and has a weighted RMS residual of 0.4986 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
1.23 AU
Eccentricity
0.4392
Perihelion
0.69 AU
Aphelion
1.770216 AU
Inclination
14.91°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
210.54°

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-Jul-11 19:45 0.120464 AU
18021222 km
18.30 km/s
2030-Dec-15 20:54 0.403928 AU
60426723 km
26.68 km/s
2035-Jan-14 07:44 0.185686 AU
27778249 km
10.81 km/s
2039-May-07 09:34 0.341843 AU
51139045 km
11.89 km/s
2043-Jul-15 16:12 0.182741 AU
27337737 km
20.00 km/s
2045-Dec-18 16:37 0.338510 AU
50640370 km
24.74 km/s
2050-Jan-25 19:53 0.256222 AU
38330194 km
9.66 km/s
2054-May-25 15:06 0.298735 AU
44690056 km
10.57 km/s
2058-Jul-19 14:53 0.268292 AU
40135855 km
22.37 km/s
2060-Dec-22 16:30 0.248601 AU
37190217 km
22.14 km/s
2065-Feb-23 11:47 0.325000 AU
48619321 km
11.32 km/s
2069-Jun-18 22:05 0.221098 AU
33075862 km
10.19 km/s
2073-Jul-23 14:18 0.355227 AU
53141145 km
24.81 km/s
2075-Dec-27 12:26 0.159979 AU
23932488 km
19.63 km/s
2079-Dec-24 19:48 0.431583 AU
64563871 km
9.14 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
21.16

Orbit Quality

RMS
0.49859
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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