Artificial satellites in retrograde orbit
Israel has successfully launched five Shavit satellites in retrograde orbit. One or more of these are spy satellites. They were launched in retrograde orbit so that launch debris would land in the Mediterranean Sea, and not on Israel's Arab neighbors.
The USA launched two Future Imagery Architecture (FIA) radar satellites into 122 degree inclined retrograde orbits in 2010 and 2012. The use of a retrograde orbit suggest these satellites employ SAR techniques.
Earth-observing satellites may also be launched into a sun-synchronous orbit, which is slightly retrograde. This is typically done in order to keep a constant surface illumination angle, which is useful for observations in the visible or infrared spectrums. SEASAT and ERS-1 are examples of satellites launched into sun-synchronous orbits for this reason.
Space warfare and accidents
Arthur C. Clarke wrote an article called, "War and Peace in the Space Age," in which he suggested that an artificial satellite in retrograde orbit could use "a bucket of nails" to destroy an SDI (anti-warhead) satellite. This premise was ridiculed on account of the vastness of space and the low probability of an encounter.
Nevertheless, a satellite in retrograde orbit could pose a major hazard to other satellites, especially if it was placed in the Clarke belt, where geostationary satellites orbit. This risk highlights the fragility of communication satellites and the importance of international cooperation in preventing space collisions due to negligence or malice.
- http://www.wseas.us/e-library/conferences/2009/istanbul/TELE-INFO/TELE-INFO-08.pdf "Most satellites are launched in a prograde orbit because the Earth's rotational velocity provides part of the orbital velocity with a consequent saving "
- www.ioccg.org/training/turkey/DrLynch_lectures2.pdf "Most Earth observing satellites are launched so as to have retrograde orbits."
- www.sac.gov.in/Satcom_Overview.doc "Orbits of almost all communication satellites are prograde orbits, as it takes less propellant to achieve the final velocity of the satellite in prograde orbit by taking advantage of the earth's rotational"