SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 FQ64

2017 FQ64

2017 FQ64 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.012 AU it takes 2.85 yr to circle the Sun.

Apollo Observations: 104
Orbital Period · P
2.85 yr
v(q)
37.4 km/s
v(Q)
11.8 km/s
Diameter · ≈
0.23 km
TJ
3.65
Eccentricity · e
0.5209

Orbit and dynamics

The path is an ellipse reaching 0.964 AU from the Sun at perihelion and 3.06 AU at aphelion, a radial span of 2.096 AU.

Applying Kepler's third law to a = 2.012 AU gives an orbital period of 2.85 yr, or about 1,042 days.

The high eccentricity (0.521) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.41° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37.4 km/s at perihelion and falls to 11.8 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 = 20.94 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.23 km.

Observation record and orbit quality

The current orbit solution is based on 104 observations and has a weighted RMS residual of 0.6229 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
2.012 AU
Eccentricity
0.5209
Perihelion
0.964 AU
Aphelion
3.060051 AU
Inclination
4.41°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
45.77°

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
2037-Jul-14 00:14 0.064342 AU
9625479 km
8.75 km/s
2057-Jun-04 13:09 0.037353 AU
5587977 km
8.67 km/s
2077-Jul-16 00:57 0.060344 AU
9027328 km
8.69 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
20.94

Orbit Quality

RMS
0.6229
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.

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