SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 FM2

2017 FM2

2017 FM2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.952 AU and a period of 0.93 yr.

Aten Observations: 39
Orbital Period · P
0.93 yr
v(q)
32.5 km/s
v(Q)
28.7 km/s
Diameter · ≈
0.03 km
TJ
6.32
Eccentricity · e
0.0632

Orbit and dynamics

Between its closest point (0.891 AU) and its farthest (1.012 AU), the heliocentric distance changes by 0.121 AU over every revolution.

One full revolution takes 0.93 yr (339 days), computed from the semi-major axis of 0.952 AU.

With e = 0.063, the orbit is close to circular.

The orbital plane is tilted 6.02° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 32.5 km/s at perihelion and falls to 28.7 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

No direct size measurement is available; from an absolute magnitude of H = 25.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 39 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3282 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
0.9515 AU
Eccentricity
0.0632
Perihelion
0.891 AU
Aphelion
1.011635 AU
Inclination
6.02°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
145.72°

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-15 10:14 0.379603 AU
56787873 km
13.31 km/s
2030-Mar-13 22:26 0.039117 AU
5851758 km
3.45 km/s
2031-Apr-15 00:45 0.460791 AU
68933369 km
15.40 km/s
2042-Feb-15 02:46 0.103050 AU
15416037 km
5.20 km/s
2042-Aug-14 18:07 0.112516 AU
16832228 km
4.10 km/s
2043-Apr-17 01:13 0.297261 AU
44469575 km
10.35 km/s
2054-Feb-15 01:57 0.317150 AU
47444959 km
11.57 km/s
2054-Oct-21 09:32 0.123612 AU
18492109 km
3.71 km/s
2055-Mar-31 01:07 0.096964 AU
14505618 km
4.45 km/s
2066-Feb-19 12:03 0.446846 AU
66847219 km
15.33 km/s
2067-Mar-03 06:51 0.012225 AU
1828779 km
3.37 km/s
2068-Apr-10 00:47 0.429968 AU
64322371 km
14.75 km/s
2078-Feb-15 20:18 0.281913 AU
42173569 km
14.60 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
25.6

Orbit Quality

RMS
0.32817
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.

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