SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 FR2

2017 FR2

2017 FR2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.499 AU it takes 1.84 yr to circle the Sun.

Apollo Observations: 59
Orbital Period · P
1.84 yr
v(q)
35 km/s
v(Q)
16.9 km/s
Diameter · ≈
0.09 km
TJ
4.47
Eccentricity · e
0.3473

Orbit and dynamics

Between its closest point (0.978 AU) and its farthest (2.02 AU), the heliocentric distance changes by 1.042 AU over every revolution.

One full revolution takes 1.84 yr (670 days), computed from the semi-major axis of 1.499 AU.

An eccentricity of 0.347 makes the orbit moderately elongated.

The orbital plane is tilted 6.26° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 35 km/s at perihelion and falls to 16.9 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 = 23 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.09 km.

Observation record and orbit quality

Astrometry from 59 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4594 arcseconds.

Condition code U = 5 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
1.499 AU
Eccentricity
0.3473
Perihelion
0.978 AU
Aphelion
2.019603 AU
Inclination
6.26°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
328.95°

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
2028-Jul-02 21:01 0.035944 AU
5377097 km
6.72 km/s
2039-Jun-30 13:03 0.041695 AU
6237465 km
6.52 km/s
2050-May-26 10:53 0.095165 AU
14236432 km
6.19 km/s
2061-Apr-21 12:47 0.136648 AU
20442310 km
8.81 km/s
2072-Apr-06 16:00 0.270667 AU
40491264 km
14.16 km/s
2072-Aug-28 12:50 0.481694 AU
72060419 km
5.02 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
23.0

Orbit Quality

RMS
0.45944
Condition
5
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.