SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 JV

2015 JV

2015 JV belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.45 AU it takes 3.83 yr to circle the Sun.

Apollo Observations: 234
Orbital Period · P
3.83 yr
v(q)
43 km/s
v(Q)
8.4 km/s
Diameter · ≈
0.19 km
TJ
3.13
Eccentricity · e
0.6723

Orbit and dynamics

Between its closest point (0.803 AU) and its farthest (4.097 AU), the heliocentric distance changes by 3.294 AU over every revolution.

One full revolution takes 3.83 yr (1,401 days), computed from the semi-major axis of 2.45 AU.

The high eccentricity (0.672) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 7.23° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 43 km/s at perihelion and falls to 8.4 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 = 21.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.19 km.

Observation record and orbit quality

Astrometry from 234 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4666 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
2.45 AU
Eccentricity
0.6723
Perihelion
0.803 AU
Aphelion
4.097135 AU
Inclination
7.23°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
330.05°

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
2038-May-18 06:55 0.208147 AU
31138302 km
21.43 km/s
2041-Dec-25 04:29 0.128355 AU
19201691 km
19.66 km/s
2061-May-07 00:33 0.092039 AU
13768843 km
16.61 km/s
2064-Dec-15 16:52 0.290037 AU
43388904 km
24.53 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
21.4

Orbit Quality

RMS
0.46657
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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