SpaceAtlas Space Object Data
NASA JPL SBDB · 2003 ME1

2003 ME1

2003 ME1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.04 AU it takes 1.06 yr to circle the Sun.

Apollo Observations: 69
Orbital Period · P
1.06 yr
v(q)
39.9 km/s
v(Q)
21.4 km/s
Diameter · ≈
0.07 km
TJ
5.8
Eccentricity · e
0.3029

Orbit and dynamics

Between its closest point (0.725 AU) and its farthest (1.355 AU), the heliocentric distance changes by 0.63 AU over every revolution.

One full revolution takes 1.06 yr (387 days), computed from the semi-major axis of 1.04 AU.

An eccentricity of 0.303 makes the orbit moderately elongated.

A steep inclination of 21.05° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.9 km/s at perihelion and falls to 21.4 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 = 23.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.07 km.

Observation record and orbit quality

Astrometry from 69 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4318 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
1.04 AU
Eccentricity
0.3029
Perihelion
0.725 AU
Aphelion
1.355016 AU
Inclination
21.05°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
300.4°

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
2033-Nov-21 10:50 0.331145 AU
49538655 km
22.76 km/s
2034-Dec-14 00:34 0.084884 AU
12698497 km
14.18 km/s
2036-Feb-05 08:25 0.347900 AU
52045146 km
11.95 km/s
2037-Jun-16 05:07 0.200719 AU
30027065 km
10.72 km/s
2038-Jun-24 13:16 0.085125 AU
12734565 km
16.53 km/s
2039-Jul-10 08:30 0.448745 AU
67131296 km
25.91 km/s
2050-Nov-15 13:22 0.432302 AU
64671428 km
25.99 km/s
2051-Dec-06 08:33 0.097931 AU
14650308 km
16.51 km/s
2053-Jan-10 14:38 0.227174 AU
33984821 km
12.11 km/s
2054-Jun-26 17:36 0.308384 AU
46133570 km
10.54 km/s
2055-Jun-20 11:14 0.003935 AU
588655 km
14.02 km/s
2056-Jul-05 13:40 0.359581 AU
53792603 km
23.35 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
23.6

Orbit Quality

RMS
0.4318
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.

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