SpaceAtlas Space Object Data
NASA JPL SBDB · 2005 SH26

2005 SH26

2005 SH26 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.098 AU it takes 1.15 yr to circle the Sun.

Apollo Observations: 100
Orbital Period · P
1.15 yr
v(q)
39.2 km/s
v(Q)
20.6 km/s
Diameter · ≈
0.26 km
TJ
5.55
Eccentricity · e
0.3114

Orbit and dynamics

Between its closest point (0.756 AU) and its farthest (1.44 AU), the heliocentric distance changes by 0.684 AU over every revolution.

One full revolution takes 1.15 yr (420 days), computed from the semi-major axis of 1.098 AU.

An eccentricity of 0.311 makes the orbit moderately elongated.

A steep inclination of 22.41° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.2 km/s at perihelion and falls to 20.6 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 = 20.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.26 km.

Observation record and orbit quality

Astrometry from 100 individual observations underpins this orbit; the fit leaves an RMS residual of 0.7215 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
1.098 AU
Eccentricity
0.3114
Perihelion
0.756 AU
Aphelion
1.439917 AU
Inclination
22.41°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
111.29°

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-Feb-10 00:12 0.432379 AU
64682974 km
22.70 km/s
2028-May-19 15:00 0.360078 AU
53866830 km
14.74 km/s
2028-Sep-27 14:15 0.323076 AU
48331494 km
12.63 km/s
2035-Mar-07 16:51 0.218791 AU
32730659 km
16.79 km/s
2036-Sep-12 19:13 0.238462 AU
35673382 km
13.67 km/s
2043-Apr-10 13:02 0.231214 AU
34589157 km
15.37 km/s
2043-Oct-15 15:52 0.435094 AU
65089072 km
12.91 km/s
2044-Sep-11 17:20 0.360125 AU
53873910 km
19.24 km/s
2050-Feb-10 15:43 0.422685 AU
63232744 km
22.44 km/s
2051-May-22 12:49 0.365021 AU
54606335 km
14.61 km/s
2051-Sep-27 19:14 0.317968 AU
47567399 km
12.62 km/s
2058-Mar-08 20:48 0.212936 AU
31854717 km
16.63 km/s
2059-Sep-13 05:16 0.238291 AU
35647848 km
13.84 km/s
2066-Apr-13 03:20 0.240463 AU
35972739 km
15.39 km/s
2066-Oct-14 05:58 0.427866 AU
64007859 km
12.91 km/s
2067-Sep-13 00:34 0.375977 AU
56245353 km
19.83 km/s
2073-Feb-12 10:50 0.400703 AU
59944379 km
21.82 km/s
2074-May-26 18:55 0.374840 AU
56075301 km
14.27 km/s
2074-Sep-26 02:30 0.307414 AU
45988426 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
20.7

Orbit Quality

RMS
0.72153
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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