In celestial mechanics, a horseshoe orbit is a type of co-orbital motion of a small orbiting body relative to a larger orbiting body. The orbital period of the smaller body is very nearly the same as for the larger body, and its path appears to have a horseshoe shape as viewed from the larger object in a rotating reference frame.
The loop is not closed but will drift forward or backward slightly each time, so that the point it circles will appear to move smoothly along the larger body's orbit over a long period of time. When the object approaches the larger body closely at either end of its trajectory, its apparent direction changes. Over an entire cycle the center traces the outline of a horseshoe, with the larger body between the 'horns'.
Asteroids in horseshoe orbits with respect to Earth include 54509 YORP, 2002 AA29, 2010 SO16, 2015 SO2 and possibly 2001 GO2. A broader definition includes 3753 Cruithne, which can be said to be in a compound and/or transition orbit, or (85770) 1998 UP1 and 2003 YN107. By 2016, 12 horseshoe librators of Earth have been discovered.
The following explanation relates to an asteroid which is in such an orbit around the Sun, and is also affected by the Earth.
The asteroid is in almost the same solar orbit as Earth. Both take approximately one year to orbit the Sun.
It is also necessary to grasp two rules of orbit dynamics:
The horseshoe orbit arises because the gravitational attraction of the Earth changes the shape of the elliptical orbit of the asteroid. The shape changes are very small but result in significant changes relative to the Earth.
The horseshoe becomes apparent only when mapping the movement of the asteroid relative to both the Sun and the Earth. The asteroid always orbits the Sun in the same direction. However, it goes through a cycle of catching up with the Earth and falling behind, so that its movement relative to both the Sun and the Earth traces a shape like the outline of a horseshoe.
Starting at point A, on the inner ring between L5 and Earth, the satellite is orbiting faster than the Earth and is on its way toward passing between the Earth and the Sun. But Earth's gravity exerts an outward accelerating force, pulling the satellite into a higher orbit which (per Kepler's third law) decreases its angular speed.
When the satellite gets to point B, it is traveling at the same speed as Earth. Earth's gravity is still accelerating the satellite along the orbital path, and continues to pull the satellite into a higher orbit. Eventually, at Point C, the satellite reaches a high and slow enough orbit such that it starts to lag behind Earth. It then spends the next century or more appearing to drift 'backwards' around the orbit when viewed relative to the Earth. Its orbit around the Sun still takes only slightly more than one Earth year. Given enough time, the Earth and the satellite will be on opposite sides of the Sun.
Eventually the satellite comes around to point D where Earth's gravity is now reducing the satellite's orbital velocity. This causes it to fall into a lower orbit, which actually increases the angular speed of the satellite around the Sun. This continues until point E where the satellite's orbit is now lower and faster than Earth's orbit, and it begins moving out ahead of Earth. Over the next few centuries it completes its journey back to point A.
On the longer term, asteroids can transfer between horseshoe orbits and quasi-satellite orbits. Quasi-satellites aren't gravitationally bound to their planet, but appear to circle it in a retrograde direction as they circle the Sun with the same orbital period as the planet. By 2016, orbital calculations showed that four of Earth's horseshoe librators and all five of its then known quasi-satellites repeatedly transfer between horseshoe and quasi-satellite orbits.
A somewhat different, but equivalent, view of the situation may be noted by considering conservation of energy. It is a theorem of classical mechanics that a body moving in a time-independent potential field will have its total energy, E = T + V, conserved, where E is total energy, T is kinetic energy (always non-negative) and V is potential energy, which is negative. It is apparent then, since V = -GM/R near a gravitating body of mass M and orbital radius R, that seen from a stationary frame, V will be increasing for the region behind M, and decreasing for the region in front of it. However, orbits with lower total energy have shorter periods, and so a body moving slowly on the forward side of a planet will lose energy, fall into a shorter-period orbit, and thus slowly move away, or be "repelled" from it. Bodies moving slowly on the trailing side of the planet will gain energy, rise to a higher, slower, orbit, and thereby fall behind, similarly repelled. Thus a small body can move back and forth between a leading and a trailing position, never approaching too close to the planet that dominates the region.
Figure 1 above shows shorter orbits around the Lagrangian points L4 and L5 (e.g. the lines close to the blue triangles). These are called tadpole orbits and can be explained in a similar way, except that the asteroid's distance from the Earth does not oscillate as far as the L3 point on the other side of the Sun. As it moves closer to or farther from the Earth, the changing pull of Earth's gravitational field causes it to accelerate or decelerate, causing a change in its orbit known as libration.
An example of a body in a tadpole orbit is Polydeuces, a small moon of Saturn which librates around the trailing L5 point relative to a larger moon, Dione. In relation to the orbit of Earth, the 300-metre-diameter (980-foot) asteroid 2010 TK7 is in a tadpole orbit around the leading L4 point. 2020 VT1 follows a temporary horseshoe orbit with respect to Mars.
|Discoverer||Year of Discovery||Type||Current Type|
|Moon||0.055||1737400||?||?||Natural satellite||Natural satellite|
|1913 Great Meteor Procession||?||?||?||9 February 1913||Possible Temporary satellite||Destroyed|
|3753 Cruithne||0.515||5000||Duncan Waldron||10 October 1986||Quasi-satellite||Horseshoe orbit|
|1991 VG||0.053||5–12||Spacewatch||6 November 1991||Temporary satellite||Apollo asteroid|
|(85770) 1998 UP1||0.345||210–470||Lincoln Lab's ETS||18 October 1998||Horseshoe orbit||Horseshoe orbit|
|54509 YORP||0.230||124||Lincoln Lab's ETS||3 August 2000||Horseshoe orbit||Horseshoe orbit|
|2001 GO2||0.168||35–85||Lincoln Lab's ETS||13 April 2001||Possible Horseshoe orbit||Possible Horseshoe orbit|
|2002 AA29||0.013||20–100||LINEAR||9 January 2002||Quasi-satellite||Horseshoe orbit|
|2003 YN107||0.014||10–30||LINEAR||20 December 2003||Quasi-satellite||Horseshoe orbit|
|(164207) 2004 GU9||0.136||160–360||LINEAR||13 April 2004||Quasi-satellite||Quasi-satellite|
|(277810) 2006 FV35||0.377||140–320||Spacewatch||29 March 2006||Quasi-satellite||Quasi-satellite|
|2006 JY26||0.083||6–13||Catalina Sky Survey||6 May 2006||Horseshoe orbit||Horseshoe orbit|
|2006 RH120||0.024||2–3||Catalina Sky Survey||14 September 2006||Temporary satellite||Apollo asteroid|
|(419624) 2010 SO16||0.075||357||WISE||17 September 2010||Horseshoe orbit||Horseshoe orbit|
|2010 TK7||0.191||150–500||WISE||1 October 2010||Earth trojan||Earth trojan|
|2013 BS45||0.083||20–40||Spacewatch||20 January 2010||Horseshoe orbit||Horseshoe orbit|
|2013 LX28||0.452||130–300||Pan-STARRS||12 June 2013||Quasi-satellite temporary||Quasi-satellite temporary|
|2014 OL339||0.461||70–160||EURONEAR||29 July 2014||Quasi-satellite temporary||Quasi-satellite temporary|
|2015 SO2||0.108||50–110||Črni Vrh Observatory||21 September 2015||Quasi-satellite||Horseshoe orbit temporary|
|2015 XX169||0.184||9–22||Mount Lemmon Survey||9 December 2015||Horseshoe orbit temporary||Horseshoe orbit temporary|
|2015 YA||0.279||9–22||Catalina Sky Survey||16 December 2015||Horseshoe orbit temporary||Horseshoe orbit temporary|
|2015 YQ1||0.404||7–16||Mount Lemmon Survey||19 December 2015||Horseshoe orbit temporary||Horseshoe orbit temporary|
|469219 Kamoʻoalewa||0.104||40-100||Pan-STARRS||27 April 2016||Quasi-satellite stable||Quasi-satellite stable|
|DN16082203||?||?||?||22 August 2016||Possible Temporary satellite||Destroyed|
|2020 CD3||0.017||1–6||Mount Lemmon Survey||15 February 2020||Temporary satellite||Temporary satellite|
|2020 PN1||0.127||10–50||ATLAS-HKO||12 August 2020||Horseshoe orbit temporary||Horseshoe orbit temporary|
|2020 PP1||0.074||10–20||Pan-STARRS||12 August 2020||Quasi-satellite stable||Quasi-satellite stable|
|2020 VT1||0.167||70–150||Pan-STARRS||10 November 2020||Horseshoe orbit temporary||Horseshoe orbit temporary|
|2020 XL5||0.387||250–550||Pan-STARRS||12 December 2020||Earth trojan (suspected)||Earth trojan|