SpaceAtlas Space Object Data
NASA JPL SBDB · 2000 QV7

2000 QV7

2000 QV7 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.409 AU it takes 1.67 yr to circle the Sun.

Apollo Observations: 182
Orbital Period · P
1.67 yr
v(q)
44.8 km/s
v(Q)
14 km/s
Diameter · ≈
0.17 km
TJ
4.57
Eccentricity · e
0.5229

Orbit and dynamics

The path is an ellipse reaching 0.672 AU from the Sun at perihelion and 2.146 AU at aphelion, a radial span of 1.474 AU.

Applying Kepler's third law to a = 1.409 AU gives an orbital period of 1.67 yr, or about 611 days.

The high eccentricity (0.523) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 9.12° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44.8 km/s at perihelion and falls to 14 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 = 21.55 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.17 km.

Observation record and orbit quality

The current orbit solution is based on 182 observations and has a weighted RMS residual of 0.5319 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
1.409 AU
Eccentricity
0.5229
Perihelion
0.672 AU
Aphelion
2.145766 AU
Inclination
9.12°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
191.12°

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-01 16:41 0.328813 AU
49189660 km
26.13 km/s
2032-Feb-06 16:56 0.229683 AU
34360071 km
23.16 km/s
2037-Feb-10 07:50 0.141312 AU
21139995 km
20.53 km/s
2042-Feb-14 10:22 0.067084 AU
10035550 km
18.33 km/s
2047-Feb-17 20:48 0.017571 AU
2628533 km
16.67 km/s
2052-Feb-19 19:21 0.025490 AU
3813311 km
15.87 km/s
2057-Feb-23 15:12 0.089003 AU
13314689 km
13.95 km/s
2062-Mar-04 02:23 0.170921 AU
25569433 km
11.81 km/s
2067-Mar-21 17:36 0.249296 AU
37294083 km
11.40 km/s
2072-Apr-09 02:56 0.307107 AU
45942579 km
13.19 km/s
2077-Apr-25 03:41 0.341788 AU
51130703 km
14.59 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
21.55

Orbit Quality

RMS
0.53185
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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