SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 AT4

2017 AT4

2017 AT4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.376 AU it takes 1.61 yr to circle the Sun.

Apollo Observations: 75
Orbital Period · P
1.61 yr
v(q)
33.3 km/s
v(Q)
19.4 km/s
Diameter · ≈
0.02 km
TJ
4.77
Eccentricity · e
0.2649

Orbit and dynamics

Between its closest point (1.011 AU) and its farthest (1.741 AU), the heliocentric distance changes by 0.73 AU over every revolution.

One full revolution takes 1.61 yr (590 days), computed from the semi-major axis of 1.376 AU.

An eccentricity of 0.265 makes the orbit moderately elongated.

Its inclination of 2.65° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.3 km/s at perihelion and falls to 19.4 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 26.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 75 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4465 arcseconds.

Condition code U = 6 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
1.376 AU
Eccentricity
0.2649
Perihelion
1.011 AU
Aphelion
1.740502 AU
Inclination
2.65°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
298.33°

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
2030-May-01 06:44 0.450741 AU
67429947 km
6.30 km/s
2037-Dec-14 22:10 0.046829 AU
7005526 km
6.88 km/s
2046-Feb-20 08:05 0.164453 AU
24601767 km
10.08 km/s
2058-Nov-29 19:28 0.321969 AU
48165916 km
13.51 km/s
2059-Apr-09 06:46 0.350105 AU
52374948 km
4.06 km/s
2067-Jan-27 21:56 0.045302 AU
6777068 km
4.06 km/s
2074-Sep-25 18:21 0.476750 AU
71320830 km
6.56 km/s
2079-Dec-03 00:41 0.263304 AU
39389667 km
12.20 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
26.6

Orbit Quality

RMS
0.44652
Condition
6
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

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