Graveyard orbit

 ( Derelict ) 

A graveyard orbit, also called a junk orbit or disposal orbit, is an orbit that lies away from common operational orbits. One significant graveyard orbit is a supersynchronous orbit well beyond geosynchronous orbit. Some satellites are moved into such orbits at the end of their operational life to reduce the probability of colliding with operational spacecraft and generating space debris.

---

Overview A graveyard orbit is used when the change in velocity required to perform a de-orbit Orbital maneuver is too large. De-orbiting a geostationary satellite requires a delta-v of about , whereas re-orbiting it to a graveyard orbit only requires about .

For satellites in geostationary orbit and geosynchronous orbits, the graveyard orbit is a few hundred beyond the operational orbit. The transfer to a graveyard orbit beyond geostationary orbit requires the same amount of fuel as a satellite needs for about three months of stationkeeping. It also requires a reliable attitude control during the transfer maneuver. While most satellite operators plan to perform such a maneuver at the end of their satellites' operational lives, through 2005 only about one-third succeeded. Given the economic value of the positions at geosynchronous altitude, unless premature spacecraft failure precludes it, satellites are moved to a graveyard orbit prior to decommissioning.

According to the Inter-Agency Space Debris Coordination Committee (IADC) the minimum recommended perigee altitude $\backslash Delta\{H\}$ beyond the geostationary orbit is

$\backslash Delta\{H\}\; =\; 235\backslash mbox\{\; km\}\; +\; C\_\backslash mathrm\{R\}\; \backslash frac\{A\; \backslash left\}\{m\; \backslash left\}\; \backslash cdot\; 1000\backslash mbox\{\; km\}$

where

$C\_\backslash mathrm\{R\}$ is the satellite's solar radiation pressure coefficient, whose value is between 1 (for absorbtion) and 2 (for specular reflection),

$A$ is its aspect area,

$m$ is its mass.

This formula includes for the GEO-protected zone to also permit orbit maneuvers in GEO without interference with the graveyard orbit. Another of tolerance must be allowed for the effects of gravitational perturbations (primarily solar and lunar). The remaining part of the equation considers the effects of the solar radiation pressure, which depends on the physical parameters of the satellite.

In order to obtain a license to provide telecommunications services in the United States, the Federal Communications Commission (FCC) requires all geostationary satellites launched after March 18, 2002, to commit to moving to a graveyard orbit at the end of their operational lives. U.S. government regulations require a boost, $\backslash Delta\{H\}$, of about . In 2023 Dish Network received the first-ever fine by the FCC for failing to de-orbit its EchoStar VII satellite according to the terms of its license.

A spacecraft moved to a graveyard orbit will typically be passivated.

Uncontrolled objects in a near geostationary Earth orbit (GEO) exhibit a 53-year cycle of orbital inclination due to the interaction of the Earth's tilt with the lunar orbit. The orbital inclination varies ± 7.4°, at up to 0.8°pa.

---

Disposal orbit While the standard geosynchronous satellite graveyard orbit results in an expected orbital lifetime of millions of years, the increasing number of satellites, the launch of microsatellites, and the FCC approval of large megaconstellations of thousands of satellites for launch by 2022 necessitated new approaches for deorbiting to assure earlier removal of the objects once they have reached end-of-life. Contrary to GEO graveyard orbits requiring three months' worth of fuel (delta-V of 11 m/s) to reach, large satellite networks in LEO require orbits that passively decay into the Earth's atmosphere. For example, both OneWeb and SpaceX have committed to the FCC regulatory authorities that decommissioned satellites will decay to a lower orbita disposal orbitwhere the satellite orbital altitude would decay due to atmospheric drag and then naturally reenter the atmosphere and burn up within one year of end-of-life.

---

See also

• List of orbits
• SNAP-10A – nuclear reactor satellite, remaining in a sub-synchronous Earth orbit for an expected 4,000 years
• Spacecraft cemetery, in the Pacific Ocean

---

Notes

Post Comment