SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 VU76

2012 VU76

2012 VU76 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.019 AU it takes 1.03 yr to circle the Sun.

Apollo Observations: 47
Orbital Period · P
1.03 yr
v(q)
33.6 km/s
v(Q)
25.9 km/s
Diameter · ≈
0.03 km
TJ
5.98
Eccentricity · e
0.1286

Orbit and dynamics

Between its closest point (0.888 AU) and its farthest (1.15 AU), the heliocentric distance changes by 0.262 AU over every revolution.

One full revolution takes 1.03 yr (376 days), computed from the semi-major axis of 1.019 AU.

An eccentricity of 0.129 makes the orbit moderately elongated.

The orbital plane is tilted 6.76° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.6 km/s at perihelion and falls to 25.9 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 = 25.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 47 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3447 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
1.019 AU
Eccentricity
0.1286
Perihelion
0.888 AU
Aphelion
1.150043 AU
Inclination
6.76°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
358.27°

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
2046-Oct-26 13:09 0.498480 AU
74571607 km
18.82 km/s
2047-Nov-03 19:04 0.325185 AU
48646984 km
13.71 km/s
2048-Nov-10 23:11 0.149803 AU
22410219 km
8.71 km/s
2049-Nov-17 10:42 0.023334 AU
3490779 km
4.52 km/s
2050-Sep-13 23:52 0.177124 AU
26497307 km
3.59 km/s
2051-Mar-06 16:52 0.142603 AU
21333167 km
3.44 km/s
2051-Jun-21 12:59 0.154617 AU
23130378 km
3.42 km/s
2052-May-14 05:27 0.030046 AU
4494847 km
5.58 km/s
2053-May-25 01:24 0.246863 AU
36930241 km
11.29 km/s
2054-Jun-04 12:27 0.461812 AU
69086151 km
17.43 km/s
2077-Nov-04 05:24 0.328186 AU
49095901 km
13.83 km/s
2078-Nov-14 03:38 0.107637 AU
16102275 km
7.58 km/s
2079-Nov-09 09:25 0.106270 AU
15897808 km
3.60 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
25.7

Orbit Quality

RMS
0.34466
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.

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