SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 MT200

2015 MT200

2015 MT200 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.865 AU and a period of 0.81 yr.

Aten Observations: 19
Orbital Period · P
0.81 yr
v(q)
52.7 km/s
v(Q)
19.4 km/s
Diameter · ≈
0.1 km
TJ
6.74
Eccentricity · e
0.4619

Orbit and dynamics

Between its closest point (0.466 AU) and its farthest (1.265 AU), the heliocentric distance changes by 0.799 AU over every revolution.

One full revolution takes 0.81 yr (294 days), computed from the semi-major axis of 0.865 AU.

The high eccentricity (0.462) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.25° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 52.7 km/s at perihelion and falls to 19.4 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 = 22.81 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

Astrometry from 19 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4668 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
0.8654 AU
Eccentricity
0.4619
Perihelion
0.466 AU
Aphelion
1.265128 AU
Inclination
2.25°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
96.8°

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-Jan-31 16:40 0.440537 AU
65903443 km
15.14 km/s
2027-Jun-09 22:35 0.249965 AU
37394263 km
9.96 km/s
2027-Oct-03 21:53 0.423855 AU
63407851 km
12.97 km/s
2031-Feb-23 06:23 0.374801 AU
56069398 km
9.49 km/s
2031-May-23 08:32 0.236224 AU
35338644 km
9.82 km/s
2031-Oct-22 12:16 0.471401 AU
70520544 km
17.23 km/s
2035-May-04 14:05 0.174467 AU
26099883 km
9.41 km/s
2035-Nov-07 00:44 0.499503 AU
74724627 km
20.09 km/s
2036-Jul-09 17:33 0.395089 AU
59104430 km
24.96 km/s
2039-Apr-21 13:15 0.064953 AU
9716895 km
11.07 km/s
2040-Jul-15 12:10 0.257032 AU
38451494 km
20.54 km/s
2043-Apr-22 03:30 0.085102 AU
12731125 km
14.93 km/s
2044-Jul-20 08:09 0.124280 AU
18592046 km
16.38 km/s
2047-Apr-26 13:22 0.215767 AU
32278322 km
19.18 km/s
2048-Jul-22 20:01 0.019480 AU
2914201 km
12.36 km/s
2051-May-02 12:09 0.361417 AU
54067192 km
23.85 km/s
2052-Jul-14 14:26 0.144592 AU
21630609 km
9.49 km/s
2056-Jan-16 17:34 0.476784 AU
71325908 km
18.43 km/s
2056-Jun-25 04:15 0.224543 AU
33591171 km
9.67 km/s
2060-Feb-03 13:09 0.433542 AU
64856991 km
14.52 km/s
2060-Jun-06 21:05 0.250669 AU
37499561 km
9.96 km/s
2060-Oct-05 23:55 0.431647 AU
64573442 km
13.66 km/s
2064-Feb-27 09:53 0.364164 AU
54478100 km
8.48 km/s
2064-May-20 15:06 0.231114 AU
34574217 km
9.76 km/s
2064-Oct-23 05:35 0.474600 AU
70999121 km
17.55 km/s
2068-May-03 19:33 0.173735 AU
25990456 km
9.41 km/s
2068-Nov-06 01:55 0.499181 AU
74676410 km
20.06 km/s
2069-Jul-09 17:33 0.399613 AU
59781237 km
25.11 km/s
2072-Apr-21 14:05 0.079706 AU
11923830 km
10.63 km/s
2073-Jul-14 16:51 0.282131 AU
42206228 km
21.33 km/s
2076-Apr-20 12:35 0.046533 AU
6961189 km
13.47 km/s
2077-Jul-18 15:03 0.180015 AU
26929807 km
18.11 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
22.81

Orbit Quality

RMS
0.46676
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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