SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 SP142

2014 SP142

2014 SP142 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.16 AU it takes 1.25 yr to circle the Sun.

Apollo Observations: 65
Orbital Period · P
1.25 yr
v(q)
43.3 km/s
v(Q)
17.7 km/s
Diameter · ≈
0.15 km
TJ
5.34
Eccentricity · e
0.42

Orbit and dynamics

The path is an ellipse reaching 0.673 AU from the Sun at perihelion and 1.647 AU at aphelion, a radial span of 0.974 AU.

Applying Kepler's third law to a = 1.16 AU gives an orbital period of 1.25 yr, or about 456 days.

The high eccentricity (0.42) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 5.57° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 43.3 km/s at perihelion and falls to 17.7 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 = 21.84 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.15 km.

Observation record and orbit quality

The current orbit solution is based on 65 observations and has a weighted RMS residual of 0.4911 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
1.16 AU
Eccentricity
0.42
Perihelion
0.673 AU
Aphelion
1.6472 AU
Inclination
5.57°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
237.13°

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
2029-Jul-04 14:20 0.212847 AU
31841508 km
7.76 km/s
2034-Jul-02 11:13 0.218098 AU
32627064 km
7.87 km/s
2039-Jun-29 03:27 0.226751 AU
33921464 km
8.07 km/s
2044-Jun-09 00:48 0.274532 AU
41069361 km
9.97 km/s
2044-Jul-31 12:14 0.309218 AU
46258369 km
6.43 km/s
2049-May-22 22:00 0.311847 AU
46651655 km
11.81 km/s
2049-Aug-18 00:09 0.385942 AU
57736138 km
8.11 km/s
2054-May-09 19:45 0.331361 AU
49570875 km
12.90 km/s
2054-Aug-27 15:01 0.441616 AU
66064845 km
9.06 km/s
2059-Apr-27 07:36 0.340460 AU
50932158 km
13.52 km/s
2059-Sep-04 15:07 0.489043 AU
73159798 km
9.80 km/s
2063-Dec-06 01:56 0.490725 AU
73411415 km
10.00 km/s
2064-Apr-13 15:17 0.339535 AU
50793760 km
13.57 km/s
2068-Dec-13 07:28 0.441016 AU
65975017 km
9.23 km/s
2069-Mar-31 14:31 0.327971 AU
49063784 km
13.08 km/s
2073-Dec-23 06:02 0.382361 AU
57200328 km
8.23 km/s
2074-Mar-18 01:07 0.305391 AU
45685851 km
12.01 km/s
2079-Jan-07 08:07 0.313282 AU
46866392 km
6.63 km/s
2079-Mar-03 07:30 0.270712 AU
40497984 km
10.41 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
21.84

Orbit Quality

RMS
0.49109
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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