SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 FN1

2017 FN1

2017 FN1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.466 AU it takes 1.78 yr to circle the Sun.

Apollo Observations: 18
Orbital Period · P
1.78 yr
v(q)
47.6 km/s
v(Q)
12.7 km/s
TJ
4.42
Eccentricity · e
0.5776

Orbit and dynamics

The path is an ellipse reaching 0.619 AU from the Sun at perihelion and 2.313 AU at aphelion, a radial span of 1.694 AU.

Applying Kepler's third law to a = 1.466 AU gives an orbital period of 1.78 yr, or about 648 days.

The high eccentricity (0.578) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.25° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 47.6 km/s at perihelion and falls to 12.7 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

Neither a measured diameter nor a reliable absolute magnitude is available for 2017 FN1, so its physical size remains unconstrained.

Observation record and orbit quality

The current orbit solution is based on 18 observations and has a weighted RMS residual of 0.4006 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.466 AU
Eccentricity
0.5776
Perihelion
0.619 AU
Aphelion
2.312762 AU
Inclination
2.25°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
40.11°

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
2033-Mar-15 10:44 0.000151 AU
22619 km
21.15 km/s
2038-Oct-19 05:18 0.320147 AU
47893326 km
30.98 km/s
2047-Aug-15 15:45 0.285765 AU
42749866 km
13.30 km/s
2049-Mar-07 18:23 0.241144 AU
36074571 km
26.05 km/s
2054-Oct-10 17:25 0.217670 AU
32562985 km
25.40 km/s
2056-Apr-30 01:10 0.269231 AU
40276365 km
12.90 km/s
2065-Feb-26 02:00 0.352885 AU
52790848 km
32.54 km/s
2070-Sep-30 23:31 0.003571 AU
534258 km
19.37 km/s
2079-Jul-01 22:42 0.394920 AU
59079211 km
18.11 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
30.6

Orbit Quality

RMS
0.40058
Condition
7
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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