SpaceAtlas Space Object Data
NASA JPL SBDB · 2001 JV1

2001 JV1

2001 JV1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.705 AU it takes 2.23 yr to circle the Sun.

Apollo Observations: 211
Orbital Period · P
2.23 yr
v(q)
36.4 km/s
v(Q)
14.3 km/s
Diameter · ≈
0.18 km
TJ
4.08
Eccentricity · e
0.436

Orbit and dynamics

The path is an ellipse reaching 0.961 AU from the Sun at perihelion and 2.448 AU at aphelion, a radial span of 1.487 AU.

Applying Kepler's third law to a = 1.705 AU gives an orbital period of 2.23 yr, or about 813 days.

The high eccentricity (0.436) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 6.62° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 36.4 km/s at perihelion and falls to 14.3 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 = 21.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.18 km.

Observation record and orbit quality

The current orbit solution is based on 211 observations and has a weighted RMS residual of 0.4943 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
1.705 AU
Eccentricity
0.436
Perihelion
0.961 AU
Aphelion
2.44838 AU
Inclination
6.62°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
71.14°

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
2030-May-08 05:47 0.416239 AU
62268445 km
20.68 km/s
2041-Sep-02 20:23 0.169012 AU
25283858 km
12.22 km/s
2050-May-25 02:17 0.157267 AU
23526874 km
13.14 km/s
2061-Sep-20 22:55 0.401862 AU
60117769 km
19.83 km/s
2070-Jun-26 17:16 0.041172 AU
6159241 km
8.12 km/s
2079-May-06 22:17 0.452814 AU
67739975 km
21.76 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
21.5

Orbit Quality

RMS
0.49426
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

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