SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 FY2

2016 FY2

2016 FY2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.872 AU and a period of 0.81 yr.

Aten Observations: 134
Orbital Period · P
0.81 yr
v(q)
38.2 km/s
v(Q)
26.6 km/s
Diameter · ≈
0.03 km
TJ
6.77
Eccentricity · e
0.1788

Orbit and dynamics

The path is an ellipse reaching 0.716 AU from the Sun at perihelion and 1.028 AU at aphelion, a radial span of 0.312 AU.

Applying Kepler's third law to a = 0.872 AU gives an orbital period of 0.81 yr, or about 297 days.

An eccentricity of 0.179 makes the orbit moderately elongated.

Its inclination of 1.9° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.2 km/s at perihelion and falls to 26.6 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 = 25.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 134 observations and has a weighted RMS residual of 0.5327 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
0.8719 AU
Eccentricity
0.1788
Perihelion
0.716 AU
Aphelion
1.027796 AU
Inclination
1.9°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
41.96°

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-Dec-06 16:37 0.187664 AU
28074174 km
3.62 km/s
2029-Apr-16 04:17 0.036300 AU
5430436 km
4.87 km/s
2033-Feb-04 13:32 0.155618 AU
23280096 km
9.11 km/s
2033-Jul-16 21:21 0.244339 AU
36552663 km
6.17 km/s
2037-Sep-12 09:30 0.291717 AU
43640268 km
8.70 km/s
2038-Apr-07 17:31 0.481183 AU
71983900 km
19.29 km/s
2041-Nov-08 22:15 0.241151 AU
36075686 km
6.26 km/s
2042-Apr-18 17:55 0.145716 AU
21798851 km
8.57 km/s
2046-Feb-04 17:23 0.045041 AU
6737966 km
5.46 km/s
2046-Jun-20 12:37 0.198615 AU
29712446 km
3.83 km/s
2050-Feb-14 07:29 0.416910 AU
62368827 km
17.25 km/s
2050-Aug-30 13:31 0.288054 AU
43092194 km
8.50 km/s
2054-Oct-27 22:46 0.258367 AU
38651181 km
7.11 km/s
2055-Apr-17 11:14 0.210696 AU
31519709 km
10.61 km/s
2059-Feb-11 00:25 0.004636 AU
693502 km
4.13 km/s
2063-Feb-15 07:34 0.381510 AU
57073142 km
18.07 km/s
2068-Apr-17 18:27 0.038587 AU
5772585 km
5.95 km/s
2072-Feb-09 21:58 0.066107 AU
9889435 km
13.89 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
25.5

Orbit Quality

RMS
0.53269
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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