SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 MT8

2017 MT8

2017 MT8 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.02 AU it takes 1.03 yr to circle the Sun.

Apollo Observations: 99
Orbital Period · P
1.03 yr
v(q)
32.3 km/s
v(Q)
26.9 km/s
Diameter · ≈
0.08 km
TJ
5.97
Eccentricity · e
0.0909

Orbit and dynamics

The path is an ellipse reaching 0.928 AU from the Sun at perihelion and 1.113 AU at aphelion, a radial span of 0.185 AU.

Applying Kepler's third law to a = 1.02 AU gives an orbital period of 1.03 yr, or about 376 days.

With e = 0.091, the orbit is close to circular.

The orbital plane is tilted 10.84° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 32.3 km/s at perihelion and falls to 26.9 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 = 23.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.08 km.

Observation record and orbit quality

The current orbit solution is based on 99 observations and has a weighted RMS residual of 0.4351 arcseconds.

Condition code U = 2 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
1.02 AU
Eccentricity
0.0909
Perihelion
0.928 AU
Aphelion
1.112718 AU
Inclination
10.84°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
59.58°

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
2048-Sep-17 09:51 0.429658 AU
64275991 km
13.77 km/s
2049-Sep-13 21:30 0.271713 AU
40647754 km
8.65 km/s
2050-Aug-16 03:10 0.148535 AU
22220586 km
6.30 km/s
2050-Dec-22 09:33 0.133091 AU
19910204 km
6.80 km/s
2051-Jul-20 08:15 0.093951 AU
14054874 km
5.80 km/s
2052-Jan-25 13:49 0.065873 AU
9854509 km
6.36 km/s
2052-Jun-19 15:15 0.157492 AU
23560460 km
5.93 km/s
2053-Feb-26 16:37 0.208882 AU
31248291 km
8.52 km/s
2054-Mar-30 01:41 0.377458 AU
56466884 km
12.62 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
23.2

Orbit Quality

RMS
0.43512
Condition
2
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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