SpaceAtlas Space Object Data
NASA JPL SBDB · 622577

Miorita

Miorita belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.287 AU it takes 1.46 yr to circle the Sun.

Apollo Observations: 95
Orbital Period · P
1.46 yr
v(q)
42.6 km/s
v(Q)
16.2 km/s
Diameter · ≈
0.41 km
TJ
4.85
Eccentricity · e
0.4496

Orbit and dynamics

Between its closest point (0.708 AU) and its farthest (1.866 AU), the heliocentric distance changes by 1.158 AU over every revolution.

One full revolution takes 1.46 yr (533 days), computed from the semi-major axis of 1.287 AU.

The high eccentricity (0.45) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 25.31° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 42.6 km/s at perihelion and falls to 16.2 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 = 19.71 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.41 km.

Observation record and orbit quality

Astrometry from 95 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4852 arcseconds.

Condition code U = 1 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
1.287 AU
Eccentricity
0.4496
Perihelion
0.708 AU
Aphelion
1.865635 AU
Inclination
25.31°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
192.92°

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
2027-Feb-10 15:05 0.395792 AU
59209715 km
17.73 km/s
2027-Jun-03 02:35 0.440811 AU
65944411 km
13.93 km/s
2029-Dec-14 08:47 0.197698 AU
29575129 km
18.83 km/s
2032-Nov-04 18:21 0.468688 AU
70114665 km
27.29 km/s
2043-May-23 16:27 0.311432 AU
46589635 km
15.77 km/s
2046-Jan-21 14:27 0.329423 AU
49280931 km
18.38 km/s
2048-Nov-30 00:01 0.227618 AU
34051118 km
20.43 km/s
2059-May-29 05:25 0.419674 AU
62782367 km
23.14 km/s
2062-May-26 15:29 0.351349 AU
52561038 km
14.24 km/s
2065-Jan-03 17:19 0.257529 AU
38525724 km
18.32 km/s
2067-Nov-18 23:22 0.315903 AU
47258473 km
22.99 km/s
2078-May-25 09:45 0.344325 AU
51510255 km
19.79 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
19.71

Orbit Quality

RMS
0.48515
Condition
1
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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