Key Facts

  • Categorized as a Apollo-class Asteroid
  • Comparable in size to a school bus or smaller
  • Will pass within 9,651,493 km of Earth in 2021
  • Classified as a Near Earth Asteroid (NEA)
  • Not a Potentially Hazardous Object
  • See orbit simulation

Overview

2016 RP40 is a very small asteroid whose orbit crosses the orbit of Earth. NASA JPL has classified 2016 RP40 as a "Near Earth Asteroid" due to its orbit's proximity to Earth, but it is not considered potentially hazardous because computer simulations have not indicated any imminent likelihood of future collision.

2016 RP40 orbits the sun every 456 days (1.25 years), coming as close as 0.78 AU and reaching as far as 1.53 AU from the sun. Based on its brightness and the way it reflects light, 2016 RP40 is probably between 0.019 to 0.085 kilometers in diameter, making it a small to average asteroid, very roughly comparable in size to a school bus or smaller.

Close Approaches

2016 RP40's orbit is 0.01 AU from Earth's orbit at its closest point. This means that its orbit is relatively close to Earth's orbit.

2016 RP40 has 20 close approaches predicted in the coming decades:

Date Distance from Earth (km) Velocity (km/s)
Sept. 4, 2021 9,651,493 8.903
Aug. 31, 2026 16,186,923 7.730
Aug. 18, 2031 25,018,881 6.648
April 18, 2066 28,035,498 7.140
March 30, 2071 20,366,673 7.081
March 23, 2076 12,608,069 8.352
March 19, 2081 5,428,725 9.657
March 20, 2086 6,722,568 9.413
March 24, 2091 13,224,112 8.231
April 1, 2096 21,804,370 6.920
April 25, 2101 29,717,672 7.446
Aug. 10, 2131 27,645,999 6.940
Aug. 30, 2136 17,938,049 7.436
Sept. 5, 2141 8,481,206 9.123
Sept. 8, 2146 3,191,488 10.234
Sept. 8, 2151 4,809,460 9.829
Sept. 4, 2156 10,655,389 8.702
Aug. 29, 2161 19,458,749 7.199
Aug. 6, 2166 28,888,935 7.095
April 5, 2196 23,447,426 6.778

Images and Observations

2016 RP40's orbit is determined by observations dating back to Sept. 13, 2016. It was last officially observed on Oct. 6, 2021. The IAU Minor Planet Center records 60 observations used to determine its orbit.

Accessibility and Exploration

2016 RP40 can be reached with a journey of 378 days. This trajectory would require a delta-v of 11.686 km/s. To put this into perspective, the delta-v to launch a rocket to Low-Earth Orbit is 9.7 km/s. There are 9 potential trajectories and launch windows to this asteroid.

See more at the NHATS Mission Trajectories table for 2016 RP40.

Similar Objects

These objects have orbits that share similar characteristics to the orbit of 2016 RP40:

References

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Orbital Elements

  • Epoch: 2460200.5 JD
  • Semi-major axis: 1.159 AU
  • Eccentricity: 0.324
  • Inclination: 7.4°
  • Longitude of Ascending Node: 352.58°
  • Argument of Periapsis: 267.32°
  • Mean Anomaly: 272.95°

Physical Characteristics

  • Diameter: ~0.052 km
  • Magnitude: 24.81

Derived Characteristics

  • Orbit Period: 456 days (1.25 years)
  • Avg. Orbit Speed: 27.65 km/s
  • Aphelion Distance: 1.53 AU
  • Perihelion Distance: 0.78 AU

Map Comparison

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Orbit Simulation

Sky Map

The position of 2016 RP40 is indicated by a ◯ pink circle. Note that the object may not be in your current field of view. Use the controls below to adjust position, location, and time.

Size Rendering

The below comparison is an artistic rendering that uses available data on the diameter of 2016 RP40 to create an approximate landscape rendering with New York City in the background. This approximation is built for full-resolution desktop browsers. Shape, color, and texture of asteroid are imagined.