SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 MM8

2017 MM8

2017 MM8 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.887 AU and a period of 0.84 yr.

Aten Observations: 44
Orbital Period · P
0.84 yr
v(q)
70.8 km/s
v(Q)
14.1 km/s
Diameter · ≈
0.11 km
TJ
6.43
Eccentricity · e
0.6674

Orbit and dynamics

The path is an ellipse reaching 0.295 AU from the Sun at perihelion and 1.48 AU at aphelion, a radial span of 1.185 AU.

Applying Kepler's third law to a = 0.887 AU gives an orbital period of 0.84 yr, or about 305 days.

The high eccentricity (0.667) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 23.35° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 70.8 km/s at perihelion and falls to 14.1 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 = 22.58 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 44 observations and has a weighted RMS residual of 0.6998 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
0.8875 AU
Eccentricity
0.6674
Perihelion
0.295 AU
Aphelion
1.479818 AU
Inclination
23.35°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
160.61°

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-Jul-12 12:30 0.232016 AU
34709167 km
17.55 km/s
2031-May-22 20:54 0.490830 AU
73427096 km
16.58 km/s
2032-Jul-08 09:17 0.294820 AU
44104457 km
17.02 km/s
2036-May-16 11:30 0.470907 AU
70446692 km
16.32 km/s
2037-Jul-04 11:07 0.350222 AU
52392472 km
16.84 km/s
2038-Jun-26 16:35 0.481851 AU
72083858 km
36.12 km/s
2041-May-10 14:36 0.444627 AU
66515210 km
16.14 km/s
2042-Jun-30 03:36 0.396818 AU
59363064 km
16.85 km/s
2043-Jun-30 20:27 0.398562 AU
59624068 km
33.25 km/s
2046-May-04 15:55 0.414101 AU
61948553 km
16.23 km/s
2047-Jun-25 16:24 0.435557 AU
65158437 km
16.95 km/s
2048-Jul-03 22:42 0.313121 AU
46842196 km
30.36 km/s
2051-Apr-29 21:22 0.383589 AU
57384082 km
17.12 km/s
2052-Jun-20 05:07 0.465840 AU
69688728 km
17.02 km/s
2053-Jul-07 17:03 0.230315 AU
34454690 km
27.55 km/s
2056-Apr-27 19:38 0.365294 AU
54647200 km
19.12 km/s
2057-Jun-15 18:58 0.487722 AU
72962100 km
17.06 km/s
2058-Jul-10 23:52 0.156083 AU
23349673 km
24.88 km/s
2061-Apr-29 14:14 0.366589 AU
54840996 km
21.70 km/s
2063-Jul-13 13:30 0.107665 AU
16106424 km
22.44 km/s
2066-May-02 15:40 0.388230 AU
58078439 km
24.42 km/s
2068-Jul-14 01:48 0.116346 AU
17405140 km
20.32 km/s
2071-May-06 09:58 0.427905 AU
64013712 km
27.27 km/s
2073-Jul-14 02:54 0.170189 AU
25459893 km
18.62 km/s
2076-May-09 13:56 0.480987 AU
71954666 km
30.18 km/s
2078-Jul-12 08:40 0.235815 AU
35277435 km
17.53 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
22.58

Orbit Quality

RMS
0.69981
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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