SpaceAtlas Space Object Data
NASA JPL SBDB · 5590

5590

5590 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.986 AU and a period of 0.98 yr.

Aten Observations: 67
Orbital Period · P
0.98 yr
v(q)
40 km/s
v(Q)
22.5 km/s
Diameter · ≈
0.37 km
TJ
6.09
Eccentricity · e
0.2801

Orbit and dynamics

The path is an ellipse reaching 0.71 AU from the Sun at perihelion and 1.263 AU at aphelion, a radial span of 0.553 AU.

Applying Kepler's third law to a = 0.986 AU gives an orbital period of 0.98 yr, or about 358 days.

An eccentricity of 0.28 makes the orbit moderately elongated.

The orbital plane is tilted 14.18° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 40 km/s at perihelion and falls to 22.5 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 = 19.91 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.37 km.

Observation record and orbit quality

The current orbit solution is based on 67 observations and has a weighted RMS residual of 0.6565 arcseconds.

Condition code U = 2 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
0.9864 AU
Eccentricity
0.2801
Perihelion
0.71 AU
Aphelion
1.262691 AU
Inclination
14.18°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
269.55°

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
2031-Oct-12 20:27 0.394680 AU
59043330 km
20.85 km/s
2032-Oct-08 07:13 0.281228 AU
42071184 km
17.25 km/s
2033-Oct-06 01:26 0.179946 AU
26919547 km
13.85 km/s
2034-Oct-06 21:39 0.122422 AU
18314009 km
10.99 km/s
2035-Oct-14 00:13 0.150358 AU
22493260 km
9.45 km/s
2036-Aug-04 17:50 0.320635 AU
47966349 km
6.51 km/s
2036-Oct-25 09:38 0.211426 AU
31628927 km
9.31 km/s
2037-Jul-04 19:30 0.343108 AU
51328195 km
10.67 km/s
2037-Nov-07 20:14 0.264724 AU
39602190 km
9.52 km/s
2038-Jun-15 03:30 0.339498 AU
50788216 km
12.28 km/s
2038-Nov-21 08:06 0.303519 AU
45405841 km
9.59 km/s
2039-May-28 11:15 0.322193 AU
48199322 km
12.88 km/s
2039-Dec-05 11:13 0.327045 AU
48925298 km
9.35 km/s
2040-May-10 06:54 0.295642 AU
44227347 km
12.78 km/s
2040-Dec-20 20:36 0.333753 AU
49928680 km
8.65 km/s
2041-Apr-22 19:10 0.263168 AU
39369433 km
12.14 km/s
2042-Jan-17 10:22 0.316831 AU
47397196 km
6.55 km/s
2042-Apr-04 09:22 0.229927 AU
34396650 km
11.23 km/s
2043-Mar-15 20:09 0.207395 AU
31025797 km
10.75 km/s
2044-Feb-27 03:07 0.221317 AU
33108519 km
12.20 km/s
2045-Feb-15 09:49 0.285486 AU
42708041 km
15.30 km/s
2046-Feb-07 14:51 0.380223 AU
56880571 km
18.92 km/s
2047-Feb-01 01:40 0.486155 AU
72727766 km
22.63 km/s
2077-Oct-15 10:58 0.277095 AU
41452880 km
23.21 km/s
2078-Oct-11 18:02 0.169438 AU
25347502 km
19.80 km/s
2079-Oct-08 16:03 0.123673 AU
18501180 km
16.45 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
19.91

Orbit Quality

RMS
0.65649
Condition
2
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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