SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 SC17

2015 SC17

2015 SC17 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.326 AU it takes 1.53 yr to circle the Sun.

Apollo Observations: 74
Orbital Period · P
1.53 yr
v(q)
38.5 km/s
v(Q)
17.4 km/s
Diameter · ≈
0.09 km
TJ
4.86
Eccentricity · e
0.3772

Orbit and dynamics

Between its closest point (0.826 AU) and its farthest (1.826 AU), the heliocentric distance changes by 1 AU over every revolution.

One full revolution takes 1.53 yr (558 days), computed from the semi-major axis of 1.326 AU.

An eccentricity of 0.377 makes the orbit moderately elongated.

Its inclination of 4.74° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.5 km/s at perihelion and falls to 17.4 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 = 22.95 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.09 km.

Observation record and orbit quality

Astrometry from 74 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5954 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
1.326 AU
Eccentricity
0.3772
Perihelion
0.826 AU
Aphelion
1.826167 AU
Inclination
4.74°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
308.37°

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
2041-Oct-15 05:48 0.280210 AU
41918783 km
17.61 km/s
2044-Nov-10 14:36 0.100830 AU
15083882 km
7.70 km/s
2045-Apr-28 05:52 0.485802 AU
72674932 km
7.20 km/s
2047-Sep-29 05:51 0.409883 AU
61317599 km
6.33 km/s
2048-Feb-06 02:01 0.136704 AU
20450574 km
7.93 km/s
2051-Mar-26 03:17 0.163661 AU
24483358 km
14.38 km/s
2054-Apr-12 22:14 0.496491 AU
74273980 km
24.30 km/s
2070-Oct-21 06:19 0.184132 AU
27545686 km
14.55 km/s
2073-Dec-13 05:31 0.154159 AU
23061803 km
7.84 km/s
2074-Apr-15 21:07 0.414913 AU
62070049 km
5.62 km/s
2076-Sep-16 22:54 0.484369 AU
72460568 km
7.75 km/s
2077-Mar-06 21:18 0.058080 AU
8688574 km
8.49 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
22.95

Orbit Quality

RMS
0.59536
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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