SpaceAtlas Space Object Data
NASA JPL SBDB · 2003 MK4

2003 MK4

2003 MK4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.081 AU it takes 1.12 yr to circle the Sun.

Apollo Observations: 276
Orbital Period · P
1.12 yr
v(q)
34.4 km/s
v(Q)
23.8 km/s
Diameter · ≈
0.24 km
TJ
5.64
Eccentricity · e
0.1813

Orbit and dynamics

The path is an ellipse reaching 0.885 AU from the Sun at perihelion and 1.277 AU at aphelion, a radial span of 0.392 AU.

Applying Kepler's third law to a = 1.081 AU gives an orbital period of 1.12 yr, or about 411 days.

An eccentricity of 0.181 makes the orbit moderately elongated.

A steep inclination of 22.32° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 34.4 km/s at perihelion and falls to 23.8 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 = 20.86 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.24 km.

Observation record and orbit quality

The current orbit solution is based on 276 observations and has a weighted RMS residual of 0.4375 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
1.081 AU
Eccentricity
0.1813
Perihelion
0.885 AU
Aphelion
1.276985 AU
Inclination
22.32°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
64.92°

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
2030-Jul-05 16:08 0.335349 AU
50167447 km
18.11 km/s
2031-Jun-20 23:30 0.367754 AU
55015180 km
11.22 km/s
2032-Jan-04 18:20 0.025197 AU
3769355 km
13.18 km/s
2039-Jul-06 08:01 0.332688 AU
49769463 km
18.02 km/s
2040-Jun-18 13:38 0.378354 AU
56600943 km
11.18 km/s
2041-Jan-04 20:31 0.045518 AU
6809429 km
13.47 km/s
2048-Jul-07 11:18 0.270616 AU
40483541 km
16.56 km/s
2049-Jun-09 17:57 0.427393 AU
63937080 km
10.94 km/s
2050-Jan-08 09:46 0.125042 AU
18706001 km
14.76 km/s
2057-Jul-09 10:18 0.192045 AU
28729477 km
14.79 km/s
2058-May-25 09:54 0.478312 AU
71554527 km
10.00 km/s
2059-Jan-12 13:46 0.218362 AU
32666538 km
16.60 km/s
2066-Jul-10 16:36 0.123507 AU
18476387 km
13.32 km/s
2066-Dec-23 12:05 0.487478 AU
72925705 km
14.83 km/s
2068-Jan-16 18:39 0.308862 AU
46205160 km
18.62 km/s
2075-Jul-11 01:08 0.091115 AU
13630626 km
12.32 km/s
2075-Dec-20 23:54 0.408953 AU
61178442 km
13.74 km/s
2077-Jan-19 10:20 0.386651 AU
57842139 km
20.50 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
20.86

Orbit Quality

RMS
0.43748
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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