SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 FL127

2017 FL127

2017 FL127 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.519 AU it takes 4.00 yr to circle the Sun.

Apollo Observations: 80
Orbital Period · P
4.00 yr
v(q)
37.9 km/s
v(Q)
9.3 km/s
Diameter · ≈
0.1 km
TJ
3.09
Eccentricity · e
0.6068

Orbit and dynamics

Between its closest point (0.99 AU) and its farthest (4.048 AU), the heliocentric distance changes by 3.058 AU over every revolution.

One full revolution takes 4.00 yr (1,460 days), computed from the semi-major axis of 2.519 AU.

The high eccentricity (0.607) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 22.46° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 37.9 km/s at perihelion and falls to 9.3 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 = 22.8 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

Astrometry from 80 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5232 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
2.519 AU
Eccentricity
0.6068
Perihelion
0.99 AU
Aphelion
4.047529 AU
Inclination
22.46°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
120.5°

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
2029-Feb-25 07:03 0.056057 AU
8386044 km
16.03 km/s
2033-Feb-24 00:27 0.043182 AU
6459927 km
15.81 km/s
2037-Feb-23 22:11 0.042462 AU
6352282 km
15.81 km/s
2041-Feb-28 14:27 0.092938 AU
13903295 km
16.72 km/s
2045-Mar-03 23:12 0.135618 AU
20288132 km
17.57 km/s
2049-Mar-07 00:43 0.179463 AU
26847228 km
18.45 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
22.8

Orbit Quality

RMS
0.52319
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.