SpaceAtlas Space Object Data
NASA JPL SBDB · 2008 EM

2008 EM

2008 EM belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.148 AU it takes 1.23 yr to circle the Sun.

Apollo Observations: 29
Orbital Period · P
1.23 yr
v(q)
32.2 km/s
v(Q)
24 km/s
Diameter · ≈
0.04 km
TJ
5.37
Eccentricity · e
0.1445

Orbit and dynamics

Between its closest point (0.982 AU) and its farthest (1.314 AU), the heliocentric distance changes by 0.332 AU over every revolution.

One full revolution takes 1.23 yr (449 days), computed from the semi-major axis of 1.148 AU.

An eccentricity of 0.144 makes the orbit moderately elongated.

A steep inclination of 25.82° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 32.2 km/s at perihelion and falls to 24 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 = 24.68 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 29 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5627 arcseconds.

Condition code U = 0 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
1.148 AU
Eccentricity
0.1445
Perihelion
0.982 AU
Aphelion
1.313886 AU
Inclination
25.82°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
239.42°

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
2029-Mar-01 10:44 0.469657 AU
70259695 km
21.83 km/s
2029-Sep-25 15:41 0.466377 AU
69769050 km
12.96 km/s
2035-Feb-28 03:22 0.430213 AU
64358913 km
13.90 km/s
2035-Sep-03 05:58 0.373460 AU
55868835 km
18.61 km/s
2040-Mar-09 06:52 0.098140 AU
14681593 km
14.26 km/s
2040-Sep-04 00:11 0.173567 AU
25965293 km
13.05 km/s
2051-Mar-04 00:28 0.371290 AU
55544191 km
13.68 km/s
2051-Sep-02 13:21 0.314620 AU
47066526 km
17.36 km/s
2056-Mar-08 14:37 0.142033 AU
21247814 km
15.13 km/s
2056-Sep-06 01:54 0.217134 AU
32482731 km
12.90 km/s
2067-Mar-07 11:02 0.291423 AU
43596212 km
13.36 km/s
2067-Sep-02 00:45 0.241278 AU
36094682 km
15.89 km/s
2072-Mar-07 05:59 0.222657 AU
33308979 km
16.56 km/s
2072-Sep-09 13:55 0.283086 AU
42349094 km
12.91 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
24.68

Orbit Quality

RMS
0.56267
Condition
0
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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