SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 DQ35

2017 DQ35

2017 DQ35 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.52 AU it takes 1.87 yr to circle the Sun.

Apollo Observations: 43
Orbital Period · P
1.87 yr
v(q)
41.1 km/s
v(Q)
14.2 km/s
Diameter · ≈
0.1 km
TJ
4.35
Eccentricity · e
0.4869

Orbit and dynamics

The path is an ellipse reaching 0.78 AU from the Sun at perihelion and 2.26 AU at aphelion, a radial span of 1.48 AU.

Applying Kepler's third law to a = 1.52 AU gives an orbital period of 1.87 yr, or about 684 days.

The high eccentricity (0.487) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 11.97° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 41.1 km/s at perihelion and falls to 14.2 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 = 22.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

The current orbit solution is based on 43 observations and has a weighted RMS residual of 0.5128 arcseconds.

Condition code U = 1 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
1.52 AU
Eccentricity
0.4869
Perihelion
0.78 AU
Aphelion
2.260088 AU
Inclination
11.97°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
24.67°

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
2032-Jan-28 07:13 0.167672 AU
25083410 km
10.85 km/s
2033-Sep-02 11:44 0.116735 AU
17463311 km
17.16 km/s
2047-Jan-20 22:02 0.211464 AU
31634600 km
9.01 km/s
2048-Aug-29 12:40 0.180568 AU
27012537 km
18.95 km/s
2061-Dec-16 15:17 0.260922 AU
39033321 km
10.11 km/s
2063-Aug-24 23:15 0.279509 AU
41813954 km
21.69 km/s
2075-Feb-24 11:24 0.460669 AU
68915057 km
26.57 km/s
2076-Nov-20 11:29 0.269270 AU
40282161 km
11.37 km/s
2078-Aug-19 11:58 0.379949 AU
56839526 km
24.54 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
22.7

Orbit Quality

RMS
0.51275
Condition
1
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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