SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 RV

2017 RV

2017 RV belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.224 AU it takes 1.35 yr to circle the Sun.

Apollo Observations: 85
Orbital Period · P
1.35 yr
v(q)
55.1 km/s
v(Q)
13.2 km/s
Diameter · ≈
0.14 km
TJ
5.02
Eccentricity · e
0.6145

Orbit and dynamics

Between its closest point (0.472 AU) and its farthest (1.976 AU), the heliocentric distance changes by 1.504 AU over every revolution.

One full revolution takes 1.35 yr (495 days), computed from the semi-major axis of 1.224 AU.

The high eccentricity (0.615) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.01° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 55.1 km/s at perihelion and falls to 13.2 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 = 21.96 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.14 km.

Observation record and orbit quality

Astrometry from 85 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6322 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
1.224 AU
Eccentricity
0.6145
Perihelion
0.472 AU
Aphelion
1.976148 AU
Inclination
3.01°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
229.52°

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
2036-Jun-20 10:46 0.434270 AU
64965826 km
15.95 km/s
2036-Aug-21 02:46 0.461824 AU
69087917 km
11.32 km/s
2038-Dec-21 01:54 0.240016 AU
35905847 km
27.19 km/s
2040-Aug-11 12:11 0.142034 AU
21247991 km
15.82 km/s
2043-Jan-04 05:24 0.103120 AU
15426492 km
17.03 km/s
2044-Aug-25 00:42 0.179625 AU
26871489 km
25.29 km/s
2046-Dec-29 12:26 0.426070 AU
63739109 km
11.13 km/s
2047-Feb-20 00:54 0.406545 AU
60818289 km
15.15 km/s
2048-Sep-08 09:28 0.490336 AU
73353232 km
35.01 km/s
2059-May-29 09:34 0.498662 AU
74598835 km
21.39 km/s
2061-Dec-12 01:31 0.434868 AU
65055312 km
33.44 km/s
2063-Aug-10 04:12 0.345885 AU
51743599 km
10.82 km/s
2065-Dec-26 06:09 0.123255 AU
18438701 km
23.46 km/s
2067-Aug-16 23:19 0.029464 AU
4407824 km
19.07 km/s
2070-Jan-07 11:12 0.191789 AU
28691218 km
14.32 km/s
2071-Aug-29 10:01 0.254963 AU
38141905 km
27.61 km/s
2073-Dec-24 10:14 0.474828 AU
71033212 km
11.67 km/s
2074-Feb-28 04:17 0.434952 AU
65067823 km
17.26 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
21.96

Orbit Quality

RMS
0.63223
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.