SpaceAtlas Space Object Data
NASA JPL SBDB · 2000 EM26

2000 EM26

2000 EM26 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.817 AU and a period of 0.74 yr.

Aten Observations: 93
Orbital Period · P
0.74 yr
v(q)
54.6 km/s
v(Q)
19.9 km/s
Diameter · ≈
0.11 km
TJ
7.07
Eccentricity · e
0.4668

Orbit and dynamics

The path is an ellipse reaching 0.436 AU from the Sun at perihelion and 1.199 AU at aphelion, a radial span of 0.763 AU.

Applying Kepler's third law to a = 0.817 AU gives an orbital period of 0.74 yr, or about 270 days.

The high eccentricity (0.467) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.84° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 54.6 km/s at perihelion and falls to 19.9 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 = 22.51 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

The current orbit solution is based on 93 observations and has a weighted RMS residual of 0.7025 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
0.8172 AU
Eccentricity
0.4668
Perihelion
0.436 AU
Aphelion
1.198669 AU
Inclination
3.84°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
327.39°

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
2028-Feb-23 07:55 0.232146 AU
34728508 km
20.04 km/s
2031-Feb-18 14:25 0.031050 AU
4644960 km
11.94 km/s
2034-Mar-18 14:24 0.192021 AU
28725900 km
10.04 km/s
2034-Jul-21 11:22 0.455773 AU
68182651 km
13.32 km/s
2036-Nov-22 14:54 0.489530 AU
73232659 km
17.58 km/s
2037-Apr-22 13:59 0.160579 AU
24022340 km
9.83 km/s
2040-May-07 09:05 0.090509 AU
13539906 km
14.73 km/s
2042-Mar-02 14:53 0.423484 AU
63352260 km
26.40 km/s
2043-Apr-29 20:31 0.335370 AU
50170595 km
23.24 km/s
2045-Feb-20 03:26 0.156635 AU
23432237 km
17.57 km/s
2048-Feb-23 13:47 0.097566 AU
14595598 km
10.32 km/s
2050-Dec-18 08:43 0.412583 AU
61721561 km
10.60 km/s
2051-Mar-29 06:22 0.202309 AU
30264949 km
10.07 km/s
2051-Jul-09 04:15 0.417330 AU
62431703 km
9.89 km/s
2054-May-02 09:41 0.116252 AU
17391092 km
10.23 km/s
2057-May-06 01:07 0.154615 AU
23130000 km
17.11 km/s
2059-Feb-27 19:21 0.349398 AU
52269233 km
23.92 km/s
2060-Apr-26 07:20 0.405699 AU
60691722 km
25.63 km/s
2062-Feb-18 15:27 0.085552 AU
12798430 km
15.26 km/s
2065-Mar-02 09:48 0.142890 AU
21376072 km
9.90 km/s
2065-Aug-05 14:52 0.498451 AU
74567174 km
17.19 km/s
2067-Dec-09 12:27 0.441828 AU
66096558 km
13.26 km/s
2068-Apr-05 03:42 0.199576 AU
29856147 km
10.05 km/s
2071-May-06 16:40 0.083930 AU
12555822 km
11.04 km/s
2074-May-05 02:08 0.195662 AU
29270689 km
18.51 km/s
2076-Feb-26 11:30 0.309205 AU
46256433 km
22.58 km/s
2077-Apr-25 03:25 0.441741 AU
66083556 km
26.84 km/s
2079-Feb-18 10:31 0.052902 AU
7914047 km
14.17 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
22.51

Orbit Quality

RMS
0.7025
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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