SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 JA

2017 JA

2017 JA belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.031 AU it takes 2.89 yr to circle the Sun.

Apollo Observations: 41
Orbital Period · P
2.89 yr
v(q)
42.9 km/s
v(Q)
10.2 km/s
Diameter · ≈
0.01 km
TJ
3.55
Eccentricity · e
0.617

Orbit and dynamics

Between its closest point (0.778 AU) and its farthest (3.284 AU), the heliocentric distance changes by 2.506 AU over every revolution.

One full revolution takes 2.89 yr (1,057 days), computed from the semi-major axis of 2.031 AU.

The high eccentricity (0.617) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.97° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 42.9 km/s at perihelion and falls to 10.2 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 = 29.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 41 individual observations underpins this orbit; the fit leaves an RMS residual of 0.2962 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
2.031 AU
Eccentricity
0.617
Perihelion
0.778 AU
Aphelion
3.284127 AU
Inclination
1.97°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
36.55°

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-Apr-17 17:27 0.074849 AU
11197323 km
22.66 km/s
2069-Oct-02 12:35 0.113349 AU
16956768 km
23.44 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
29.1

Orbit Quality

RMS
0.29623
Condition
6
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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