SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 TO17

2023 TO17

2023 TO17 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.187 AU it takes 1.29 yr to circle the Sun.

Apollo Observations: 24
Orbital Period · P
1.29 yr
v(q)
45 km/s
v(Q)
16.6 km/s
Diameter · ≈
0 km
TJ
5.23
Eccentricity · e
0.4603

Orbit and dynamics

The path is an ellipse reaching 0.64 AU from the Sun at perihelion and 1.733 AU at aphelion, a radial span of 1.093 AU.

Applying Kepler's third law to a = 1.187 AU gives an orbital period of 1.29 yr, or about 472 days.

The high eccentricity (0.46) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.63° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 45 km/s at perihelion and falls to 16.6 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 = 29.67 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0 km.

Observation record and orbit quality

The current orbit solution is based on 24 observations and has a weighted RMS residual of 0.5383 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.187 AU
Eccentricity
0.4603
Perihelion
0.64 AU
Aphelion
1.733376 AU
Inclination
3.63°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
63.24°

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-Jun-30 18:16 0.377694 AU
56502152 km
15.62 km/s
2031-Mar-22 22:46 0.048086 AU
7193520 km
17.06 km/s
2032-Oct-27 20:19 0.267200 AU
39972486 km
23.82 km/s
2036-Aug-05 18:04 0.336851 AU
50392193 km
13.87 km/s
2036-Nov-04 14:36 0.410094 AU
61349214 km
9.32 km/s
2045-Oct-02 02:54 0.118282 AU
17694737 km
9.14 km/s
2049-Mar-03 22:32 0.394933 AU
59081110 km
9.38 km/s
2053-Mar-12 08:57 0.218159 AU
32636173 km
23.85 km/s
2054-Oct-18 04:41 0.000605 AU
90528 km
16.93 km/s
2058-Jul-09 00:42 0.377612 AU
56489882 km
15.65 km/s
2062-Mar-25 17:10 0.016170 AU
2418944 km
15.32 km/s
2063-Oct-30 23:26 0.297179 AU
44457372 km
25.20 km/s
2067-Aug-08 19:32 0.343887 AU
51444803 km
13.64 km/s
2067-Nov-04 14:51 0.426003 AU
63729164 km
9.21 km/s
2071-Apr-08 05:07 0.152455 AU
22806953 km
9.32 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
29.67

Orbit Quality

RMS
0.53832
Condition
6
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.