sign in sign up
<<
Home , Areocentric orbit, Geocentric orbit, Heliocentric orbit, Plane of reference

International Journal of Research p-ISSN: 2348-6848 e-ISSN: 2348-795X Available at http://internationaljournalofresearch.org/ Volume 02 Issue 04 April 2015

Orbital Inclination of

Tamanna Kundra1 & Abhinav Sharma Electronics and Computer Science Engineering, Maharishi Dayanand University, Gurgaon,Haryana, India [email protected]; [email protected]

ABSTRACT Equations are derived which govern the rate of the primary's or the ), normally change of the inclination of a satellite to the stated in degrees. equator of an . It is shown that if the motion of the satellite’s ascending node on the equator In the , the inclination of the orbit of plane has a period which is short as compared to a planet is defined as the between the plane with the planet precession period then the of the orbit of the planet and satellite’s orbit will maintain a constant the ecliptic. Therefore 's inclination is, by inclination to plane’s equator. This criterion is definition, zero. Inclination could instead be satisfied by many satellite orbit in the soldar measured with respect to another plane, such as system. These include all satellite whose orbit the 's equator or even 's orbital plane, planes lie in the planet’s equator planes. but the ecliptic is more practical for Earth-bound observers. Most planetary in the Solar 1. INTRODUCTION System have relatively small inclinations, both in relation to each other and to the Sun's equator. On The inclination is one of the six orbital the other hand, the dwarf parameters describing the shape and orientation of Pluto and Eris have inclinations to a celestial orbit. It is the angular of the the ecliptic of 17 degrees and 44 degrees orbital plane from the (usually respectively, and the large Pallas is inclined at 34 degrees.

Available online:http://internationaljournalofresearch.org/ P a g e | 1113 International Journal of Research p-ISSN: 2348-6848 e-ISSN: 2348-795X Available at http://internationaljournalofresearch.org/ Volume 02 Issue 04 April 2015

2. operators may decide to omit these expensive maneuver’s to correct inclination and only control . A satellite is in an inclined orbit when its . This prolongs the life-time of the plane is tipped some number of degrees from the satellite as it consumes less fuel over time, but the horizontal defined by the equator. In the case of an satellite can then only be used by ground antennas inclined , although the capable of following the north-south movement, satellite remains geosynchronous (that is, Satellite Tracking earth stations. Before the fuel completing one orbit around the earth every 24 comes to an end, satellites can be moved to hours), it is no longer geostationary. From a fixed a to keep the geostationary altitude observation point on Earth, it would appear to free for subsequent missions.Satellites are allowed out a small as the gravitational effects of to drift into an inclined orbit to save satellite other stellar bodies (Sun and ) exhibit station-keeping propellant. East-West station- influence over the satellite, as the effect keeping maneuvers must be performed to keep the accumulates over time the trace becomes satellite in its assigned orbital position. North- an with lobes oriented north-southward. South station-keeping is performed to keep the The satellite traces the same analemma once satellite in the earth's equatorial plane. Natural each sidereal day.A is not tend to cause the satellite's orbital plane to stable. It takes regular maneuvers to actively tilt, or become inclined to the earth's equatorial counteract the above gravitational forces. The plane. By suspending North-South station-keeping majority of the fuel of the satellite, maneuvers (while continuing East-West station- typically hydrazine, is spent for this purpose. keeping), a significant savings of propellant can be Otherwise, the satellite experiences a change in the realized. Typically, for a geostationary satellite, 90 inclination over time. At the end of the satellite's percent of the total propellant usage is due to lifetime, when fuel approaches depletion, satellite North-South station-keeping maneuvers.

Available online:http://internationaljournalofresearch.org/ P a g e | 1114 International Journal of Research p-ISSN: 2348-6848 e-ISSN: 2348-795X Available at http://internationaljournalofresearch.org/ Volume 02 Issue 04 April 2015

3. TYPES OF SATELLITE ORBITS orbit (MEO): Geocentric orbits ranging in altitude from 2,000 km (1,240 miles) to just below geosynchronous orbit at 35,786 kilometers (22,236 mi). Also 3.1 CENTERIC CLASSIFCATIONS known as an intermediate .  Galactocentric orbit: An orbit about the These are commonly at 20,200 center of a galaxy. The Sun follows this kilometers (12,600 mi), or 20,650 type of orbit about the galactic center of kilometers (12,830 mi), with an orbital the Milky Way. period of 12 hours.  : An orbit around  Both Geosynchronous orbit (GSO) the Sun. In the Solar System, and Geostationary orbit (GEO) are all planets, , and are in orbits around Earth matching such orbits, as are many artificial Earth's sidereal rotation period. All satellites and pieces of space geosynchronous and geostationary orbits have a semi-major axis of 42,164 km debris. by contrast are not in [3] a heliocentric orbit but rather orbit their (26,199 mi). All geostationary orbits parent object. are also geosynchronous, but not all geosynchronous orbits are  : An orbit around the geostationary. A geostationary orbit planet Earth, such as that of the Moon or stays exactly above the equator, whereas of artificial satellites. a geosynchronous orbit may swing north  : An orbit around the and south to cover more of the Earth's planet , such as that of its surface. Both complete one full orbit of moons or artificial satellites. Earth per sidereal day (relative to the  (also selenocentric orbit): stars, not the Sun). An orbit around the Earth's moon.  : Geocentric  Hermocentric orbit: An orbit around the orbits above the altitude planet Mercury. of geosynchronous  Aphrodiocentric orbit (also orbit 35,786 km (22,240 miles). cytheriocentric orbit): An orbit around the planet Venus. 4. CONCLUSION  Jovicentric orbit (also zeocentric orbit): In the paper we have talked about the An orbit around the planet Jupiter. various orbits which are being used for  Cronocentric orbit (also saturnocentric putting the satellite’s in their respective orbit): An orbit around the orbits for performing their desired functions planet . .The orbit chosen depends ipon the function  Uranocentric orbit: An orbit around the to be performed. The orbits aren’t only planet Uranus. meant for artificial satellites but some  Neptunocentric orbit: An orbit around planets do follow some of the orbit’s rules. the planet Neptune. 5. REFERENCES 3.2 ALTITUDE CLASSIFICATIONS [1.] http://en.wikipedia.org/wiki/Satellite FOR GEOMETRIC ORBITS [2.] http://articles.adsabs.harvard.edu/cgi-  (LEO): Geocentric bin/nph- orbits with altitudes up to 2,000 km (0– iarticle_query?bibcode=1965AJ.....70....5G&db 1,240 miles). Medium Earth

Available online:http://internationaljournalofresearch.org/ P a g e | 1115 International Journal of Research p-ISSN: 2348-6848 e-ISSN: 2348-795X Available at http://internationaljournalofresearch.org/ Volume 02 Issue 04 April 2015

_key=AST&page_ind=0&data_type=GIF&typ e=SCREEN_VIEW&classic=YES

[3.] http://muller.lbl.gov/papers/lbl- 35665.html

[4.] http://en.wikipedia.org/wiki/Orbital_incl ination

[5.] http://en.wikipedia.org/wiki/List_of_orb its

[6.] http://en.wikipedia.org/wiki/Inclined_or bit

Available online:http://internationaljournalofresearch.org/ P a g e | 1116