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Sun-synchronous orbit

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maximum for a Sun-synchronous orbit, and doing more than 16 would require an orbit inside the Earth's atmosphere or surface. The resulting valid orbits are shown in the following table. (The table has been calculated assuming the periods given. The orbital period that should be used is actually slightly longer. For instance, a retrograde equatorial orbit that passes over the same spot after 24 hours has a true period about
2901: 607: 2791: 2865: 2889: 2841: 2877: 2853: 1106: 893:{\displaystyle {\begin{aligned}\rho &\approx -{\frac {3J_{2}R_{\text{E}}^{2}{\sqrt {\mu }}\cos i}{2a^{7/2}}}\\&=-(360^{\circ }{\text{ per year}})\times \left({\frac {a}{12\,352{\text{ km}}}}\right)^{-7/2}\cos i\\&=-(360^{\circ }{\text{ per year}})\times \left({\frac {T}{3.795{\text{ h}}}}\right)^{-7/3}\cos i,\end{aligned}}} 132:
between day and night. Riding the terminator is useful for active radar satellites, as the satellites' solar panels can always see the Sun, without being shadowed by the Earth. It is also useful for some satellites with passive instruments that need to limit the Sun's influence on the measurements,
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wavelengths, such as weather and spy satellites, and for other remote-sensing satellites, such as those carrying ocean and atmospheric remote-sensing instruments that require sunlight. For example, a satellite in Sun-synchronous orbit might ascend across the equator twelve times a day, each time at
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evolve, due to higher-order perturbations in the Earth's gravitational field, the pressure of sunlight, and other causes. Earth observation satellites, in particular, prefer orbits with constant altitude when passing over the same spot. Careful selection of eccentricity and location of perigee
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If one wants a satellite to fly over some given spot on Earth every day at the same hour, the satellite must complete a whole number of orbits per day. Assuming a circular orbit, this comes down to between 7 and 16 orbits per day, as doing less than 7 orbits would require an altitude above the
913: 181:, which perturbs inclined orbits, causes the orbital plane of the spacecraft to precess with the desired rate. The plane of the orbit is not fixed in space relative to the distant stars, but rotates slowly about the Earth's axis. 308: 36:
Diagram showing the orientation of a Sun-synchronous orbit (green) at four points in the year. A non-Sun-synchronous orbit (magenta) is also shown for reference. Dates are shown in white: day/month.
1101:{\displaystyle \cos i\approx -{\frac {2\rho }{3J_{2}R_{\text{E}}^{2}{\sqrt {\mu }}}}a^{7/2}=-\left({\frac {a}{12\,352{\text{ km}}}}\right)^{7/2}=-\left({\frac {T}{3.795{\text{ h}}}}\right)^{7/3}.} 562: 612: 1733: 1682: 225: 1640:
reveals specific combinations where the rate of change of perturbations are minimized, and hence the orbit is relatively stable – a
1971: 1792: 2668: 2816: 133:
as it is possible to always point the instruments towards the night side of the Earth. The dawn/dusk orbit has been used for solar-observing
1753: 2728: 1154:, which means that only lower orbits can be Sun-synchronous. The period can be in the range from 88 minutes for a very low orbit ( 1838: 116:
of 10:30. The LST zones show how the local time beneath the satellite varies at different latitudes and different points on its orbit.
1645: 128:, where the local mean solar time of passage for equatorial latitudes is around sunrise or sunset, so that the satellite rides the 2723: 2603: 2022: 580: 184:
Typical Sun-synchronous orbits around Earth are about 600–800 km (370–500 mi) in altitude, with periods in the 96–100-
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Low, Samuel Y. W. (January 2022). "Designing a Reference Trajectory for Frozen Repeat Near-Equatorial Low Earth Orbits".
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compared to the direction of Earth's rotation: 0° represents an equatorial orbit, and 90° represents a polar orbit.
2807: 2633: 2460: 2771: 2756: 2281: 1958: 77: 1226:≈ 1.0027 times longer than the time between overpasses. For non-equatorial orbits the factor is closer to 1.) 56:
around a planet, in which the satellite passes over any given point of the planet's surface at the same local
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over the Earth surface. Even if an orbit remains Sun-synchronous, however, other orbital parameters such as
2628: 2230: 2150: 2138: 124:, where the local mean solar time of passage for equatorial latitudes is around noon or midnight, and the 100: 2921: 2751: 2693: 2663: 2451: 2296: 2266: 2210: 2089: 1978: 1712: 1669: 1653: 1632: 134: 88:
on the planet underneath it is nearly the same. This consistent lighting is a useful characteristic for
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through one complete revolution each year, so it always maintains the same relationship with the Sun.
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of the spacecraft over Earth's surface, this formula gives a Sun-synchronous inclination of 98.7°.
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Rosengren, M. (November 1992). "ERS-1 - An Earth Observer that exactly follows its Chosen Path".
1612:. The Sun will not be in exactly the same position in the sky during the course of the year (see 337: 142: 129: 85: 1830: 1734:"Stabilization of heliosynchronous orbits of an Earth's artificial satellite by solar pressure" 2678: 2576: 2506: 2261: 2215: 2133: 1834: 1182:= 180°). A period longer than 3.8 hours may be possible by using an eccentric orbit with 189: 81: 73: 2845: 2658: 2590: 2354: 2316: 2190: 2160: 2113: 1927:
Rosengren, Mats (1989). "Improved technique for Passive Eccentricity Control (AAS 89-155)".
1901: 1822: 1775: 1613: 216: 178: 166: 162: 158: 2698: 2291: 2195: 2185: 2084: 2008: 1605: 572: 196: 173:. This precession is achieved by tuning the inclination to the altitude of the orbit (see 57: 1936: 1897: 1870: 1749: 207:
that is almost spherical will need an outside push to maintain a Sun-synchronous orbit.
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When one says that a Sun-synchronous orbit goes over a spot on the Earth at the same
414: 363: 2900: 2857: 2713: 2623: 2497: 2480: 2338: 2235: 2103: 1641: 113: 303:{\displaystyle \Delta \Omega =-3\pi {\frac {J_{2}R_{\text{E}}^{2}}{p^{2}}}\cos i,} 2718: 2553: 2323: 2303: 2220: 1707: 53: 2286: 1665: 341: 109: 61: 2703: 2055: 89: 1687: 1661: 1617: 105: 93: 165:(rotate) approximately one degree eastward each day with respect to the 2608: 2000: 1649: 146: 1905: 430: 185: 219:
per orbit for an Earth orbiting satellite is approximately given by
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Sandwell, David T., The Gravity Field of the Earth - Part 1 (2002)
1657: 204: 138: 99: 31: 84:, because every time that the satellite is overhead, the surface 1240: 200: 2004: 1644:, where the motion of position of the periapsis is stable. The 1732:
Tscherbakova, N. N.; Beletskii, V. V.; Sazonov, V. V. (1999).
170: 1829:(1st ed.). Cambridge University Press. 2007. p.  1672:, are all operated in such Sun-synchronous frozen orbits. 376:
An orbit will be Sun-synchronous when the precession rate
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for a circular or almost circular orbit, it follows that
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range, and inclinations of around 98°. This is slightly
60:. More technically, it is an orbit arranged so that it 149:, affording them a nearly continuous view of the Sun. 2805: 916: 610: 557:{\displaystyle T=2\pi {\sqrt {\frac {a^{3}}{\mu }}},} 519: 228: 2677: 2589: 2533: 2469: 2422: 2362: 2353: 2249: 2159: 2048: 2039: 1977:. Space Flight Mechanics Conference. Archived from 120:Special cases of the Sun-synchronous orbit are the 1100: 892: 556: 507:is the period of the spacecraft around the earth. 404:equals the mean motion of the Earth about the Sun 302: 169:to keep pace with the Earth's movement around the 157:A Sun-synchronous orbit is achieved by having the 195:Sun-synchronous orbits are possible around other 1623:Sun-synchronous orbits are mostly selected for 372:is the inclination of the orbit to the equator. 2016: 1627:, with an altitude typically between 600 and 104:Sun-synchronous orbit from a top view of the 92:that image the Earth's surface in visible or 8: 1972:"The A-B-Cs of Sun Synchronous Orbit Design" 1996:List of satellites in Sun-synchronous orbit 1961:, from U.S. Centennial of Flight Commission 1178:, but this orbit would be equatorial, with 2790: 2359: 2045: 2023: 2009: 2001: 1683:Orbital perturbation analysis (spacecraft) 1146:equals −1 when the semi-major axis equals 1139:Note that according to this approximation 1085: 1081: 1069: 1060: 1039: 1035: 1023: 1019: 1010: 989: 985: 971: 965: 960: 950: 932: 915: 864: 857: 845: 836: 820: 814: 775: 768: 756: 752: 743: 727: 721: 688: 684: 659: 653: 648: 638: 628: 611: 609: 539: 532: 518: 510:As the orbital period of a spacecraft is 280: 269: 264: 254: 247: 227: 1825:Our Changing Planet: The View from Space 1230: 203:. A satellite orbiting a planet such as 2812: 1724: 2669:Transposition, docking, and extraction 1959:Sun-Synchronous Orbit dictionary entry 1929:Advances in the Astronautical Sciences 1886:AIAA Journal of Spacecraft and Rockets 174: 72:A Sun-synchronous orbit is useful for 338:coefficient for the second zonal term 97:approximately 15:00 mean local time. 7: 1852: 1850: 1970:Boain, Ronald J. (February 2004). 503:is the earth orbital period while 232: 229: 25: 2729:Kepler's laws of planetary motion 1865:(72). European Space Agency: 76. 2899: 2887: 2875: 2863: 2851: 2839: 2827: 2815: 2789: 2724:Interplanetary Transport Network 2604:Collision avoidance (spacecraft) 581:standard gravitational parameter 356:is the mean radius of the Earth, 112:(LST) zones for reference and a 2689:Astronomical coordinate systems 2443:Longitude of the ascending node 2762:Retrograde and prograde motion 825: 807: 732: 714: 1: 2709:Equatorial coordinate system 1625:Earth observation satellites 2938: 2461:Longitude of the periapsis 1931:. Vol. 69. AAS/NASA. 1604:each time, this refers to 1166:= 96°) to 3.8 hours ( 2785: 2772:Specific angular momentum 1238: 1119:, i.e., for an altitude 27:Type of geocentric orbit 2767:Specific orbital energy 1776:"SATELLITES AND ORBITS" 2179:Geostationary transfer 1102: 894: 558: 304: 117: 50:heliosynchronous orbit 37: 18:Heliosynchronous orbit 2752:Orbital state vectors 2694:Characteristic energy 2664:Trans-lunar injection 2452:Argument of periapsis 2129:Prograde / Retrograde 2090:Hyperbolic trajectory 1713:World Geodetic System 1670:Canadian Space Agency 1654:European Space Agency 1633:argument of periapsis 1103: 895: 559: 305: 135:scientific satellites 103: 42:Sun-synchronous orbit 35: 2599:Bi-elliptic transfer 2119:Parabolic trajectory 1693:Geosynchronous orbit 1637:orbital eccentricity 1111:As an example, with 914: 608: 517: 413:, which is 360° per 226: 177:) such that Earth's 2639:Low-energy transfer 1984:on 25 October 2007. 1937:1989ommd.proc...49R 1898:2022JSpRo..59...84L 1871:1992ESABu..72...76R 1750:1999KosIs..37..417S 1698:Geostationary orbit 1610:apparent solar time 970: 658: 274: 122:noon/midnight orbit 2634:Inclination change 2282:Distant retrograde 1797:marine.rutgers.edu 1098: 956: 907:is 360° per year, 890: 888: 644: 575:of the orbit, and 554: 435:), so we must set 300: 260: 153:Orbital precession 118: 86:illumination angle 82:weather satellites 38: 2803: 2802: 2777:Two-line elements 2585: 2584: 2507:Eccentric anomaly 2349: 2348: 2216:Orbit of the Moon 2075:Highly elliptical 1803:on 22 August 2019 1793:"Types of Orbits" 1656:, as well as the 1596: 1595: 1075: 1072: 1029: 1026: 979: 976: 963: 851: 848: 823: 762: 759: 730: 699: 664: 651: 549: 548: 364:semi-latus rectum 286: 267: 211:Technical details 199:planets, such as 175:Technical details 48:), also called a 16:(Redirected from 2929: 2904: 2903: 2892: 2891: 2890: 2880: 2879: 2878: 2868: 2867: 2866: 2856: 2855: 2844: 2843: 2842: 2832: 2831: 2820: 2819: 2811: 2793: 2792: 2734:Lagrangian point 2629:Hohmann transfer 2574: 2560: 2551: 2542: 2522: 2513: 2504: 2495: 2491: 2487: 2478: 2458: 2449: 2440: 2431: 2411: 2407: 2398: 2389: 2380: 2360: 2329:Heliosynchronous 2278:Lagrange points 2231:Transatmospheric 2046: 2025: 2018: 2011: 2002: 1985: 1983: 1976: 1941: 1940: 1924: 1918: 1917: 1906:10.2514/1.A34934 1881: 1875: 1874: 1854: 1845: 1844: 1828: 1819: 1813: 1812: 1810: 1808: 1799:. Archived from 1789: 1783: 1782: 1780: 1772: 1766: 1765: 1763: 1761: 1752:. Archived from 1729: 1630: 1614:Equation of time 1580: 1578: 1577: 1574: 1571: 1567: 1524: 1522: 1521: 1518: 1515: 1511: 1487: 1485: 1484: 1481: 1478: 1474: 1450: 1448: 1447: 1444: 1441: 1437: 1394: 1392: 1391: 1388: 1385: 1381: 1357: 1355: 1354: 1351: 1348: 1344: 1320: 1318: 1317: 1314: 1311: 1307: 1283: 1281: 1280: 1277: 1274: 1270: 1231: 1225: 1223: 1222: 1219: 1216: 1205: 1203: 1197: 1193: 1191: 1185: 1181: 1177: 1175: 1169: 1165: 1161: 1157: 1153: 1151: 1145: 1135: 1131: 1118: 1114: 1107: 1105: 1104: 1099: 1094: 1093: 1089: 1080: 1076: 1074: 1073: 1070: 1061: 1048: 1047: 1043: 1034: 1030: 1028: 1027: 1024: 1011: 998: 997: 993: 980: 978: 977: 972: 969: 964: 961: 955: 954: 941: 933: 906: 899: 897: 896: 891: 889: 873: 872: 868: 856: 852: 850: 849: 846: 837: 824: 821: 819: 818: 797: 784: 783: 779: 767: 763: 761: 760: 757: 744: 731: 728: 726: 725: 704: 700: 698: 697: 696: 692: 675: 665: 660: 657: 652: 649: 643: 642: 629: 600: 590: 588: 578: 570: 563: 561: 560: 555: 550: 544: 543: 534: 533: 506: 502: 495: 494: 492: 491: 486: 483: 469: 467: 466: 458: 455: 434: 428: 425: 422: 412: 403: 402: 400: 399: 393: 390: 371: 361: 355: 335: 334: 332: 329: 309: 307: 306: 301: 287: 285: 284: 275: 273: 268: 265: 259: 258: 248: 179:equatorial bulge 167:celestial sphere 110:local solar time 21: 2937: 2936: 2932: 2931: 2930: 2928: 2927: 2926: 2912: 2911: 2910: 2898: 2888: 2886: 2876: 2874: 2864: 2862: 2850: 2840: 2838: 2826: 2814: 2806: 2804: 2799: 2781: 2699:Escape velocity 2680: 2673: 2654:Rocket equation 2581: 2573: 2567: 2558: 2549: 2540: 2529: 2520: 2511: 2502: 2493: 2489: 2485: 2476: 2465: 2456: 2447: 2438: 2429: 2418: 2409: 2405: 2401:Semi-minor axis 2396: 2392:Semi-major axis 2387: 2378: 2372: 2345: 2267:Areosynchronous 2251: 2245: 2226:Sun-synchronous 2211:Near-equatorial 2155: 2035: 2029: 1992: 1981: 1974: 1969: 1949: 1947:Further reading 1944: 1926: 1925: 1921: 1883: 1882: 1878: 1856: 1855: 1848: 1841: 1821: 1820: 1816: 1806: 1804: 1791: 1790: 1786: 1778: 1774: 1773: 1769: 1759: 1757: 1756:on 3 March 2016 1738:Cosmic Research 1731: 1730: 1726: 1722: 1717: 1678: 1628: 1606:mean solar time 1575: 1572: 1569: 1568: 1565: 1563: 1519: 1516: 1513: 1512: 1509: 1507: 1482: 1479: 1476: 1475: 1472: 1470: 1445: 1442: 1439: 1438: 1435: 1433: 1389: 1386: 1383: 1382: 1379: 1377: 1352: 1349: 1346: 1345: 1342: 1340: 1315: 1312: 1309: 1308: 1305: 1303: 1278: 1275: 1272: 1271: 1268: 1266: 1257: 1252: 1247: 1235: 1220: 1217: 1214: 1213: 1211: 1201: 1199: 1195: 1189: 1187: 1183: 1179: 1173: 1171: 1167: 1163: 1159: 1155: 1149: 1147: 1140: 1133: 1130: 1120: 1116: 1112: 1065: 1056: 1055: 1015: 1006: 1005: 981: 946: 942: 934: 912: 911: 904: 887: 886: 841: 832: 831: 810: 795: 794: 748: 739: 738: 717: 702: 701: 680: 676: 634: 630: 618: 606: 605: 592: 591:for Earth); as 586: 584: 583:of the planet ( 576: 573:semi-major axis 568: 535: 515: 514: 504: 501: 497: 487: 484: 478: 477: 475: 465: 459: 456: 454: 447: 446: 444: 442: 436: 426: 423: 420: 418: 411: 405: 394: 391: 385: 384: 382: 377: 369: 359: 353: 347: 340:related to the 330: 327: 325: 323: 317: 276: 250: 249: 224: 223: 213: 155: 126:dawn/dusk orbit 114:descending node 70: 58:mean solar time 28: 23: 22: 15: 12: 11: 5: 2935: 2933: 2925: 2924: 2914: 2913: 2909: 2908: 2896: 2884: 2872: 2860: 2848: 2836: 2824: 2801: 2800: 2798: 2797: 2795:List of orbits 2786: 2783: 2782: 2780: 2779: 2774: 2769: 2764: 2759: 2754: 2749: 2747:Orbit equation 2744: 2736: 2731: 2726: 2721: 2716: 2711: 2706: 2701: 2696: 2691: 2685: 2683: 2675: 2674: 2672: 2671: 2666: 2661: 2656: 2651: 2646: 2641: 2636: 2631: 2626: 2621: 2619:Gravity assist 2616: 2614:Delta-v budget 2611: 2606: 2601: 2595: 2593: 2587: 2586: 2583: 2582: 2580: 2579: 2571: 2565: 2556: 2547: 2545:Orbital period 2537: 2535: 2531: 2530: 2528: 2527: 2525:True longitude 2518: 2516:Mean longitude 2509: 2500: 2483: 2473: 2471: 2467: 2466: 2464: 2463: 2454: 2445: 2436: 2426: 2424: 2420: 2419: 2417: 2416: 2403: 2394: 2385: 2375: 2373: 2371: 2370: 2367: 2363: 2357: 2351: 2350: 2347: 2346: 2344: 2343: 2342: 2341: 2333: 2332: 2331: 2326: 2321: 2320: 2319: 2306: 2301: 2300: 2299: 2294: 2289: 2284: 2276: 2275: 2274: 2272:Areostationary 2269: 2264: 2255: 2253: 2247: 2246: 2244: 2243: 2241:Very low Earth 2238: 2233: 2228: 2223: 2218: 2213: 2208: 2203: 2198: 2193: 2188: 2183: 2182: 2181: 2176: 2169:Geosynchronous 2165: 2163: 2157: 2156: 2154: 2153: 2151:Transfer orbit 2148: 2147: 2146: 2141: 2131: 2126: 2121: 2116: 2111: 2109:Lagrange point 2106: 2101: 2092: 2087: 2082: 2077: 2068: 2063: 2058: 2052: 2050: 2043: 2037: 2036: 2031:Gravitational 2030: 2028: 2027: 2020: 2013: 2005: 1999: 1998: 1991: 1990:External links 1988: 1987: 1986: 1967: 1962: 1956: 1948: 1945: 1943: 1942: 1919: 1876: 1846: 1840:978-0521828703 1839: 1814: 1784: 1767: 1744:(4): 393–403. 1723: 1721: 1718: 1716: 1715: 1710: 1705: 1703:List of orbits 1700: 1695: 1690: 1685: 1679: 1677: 1674: 1660:spacecraft of 1598: 1597: 1594: 1593: 1590: 1587: 1584: 1581: 1561: 1557: 1556: 1553: 1550: 1547: 1545: 1542: 1538: 1537: 1534: 1531: 1528: 1525: 1505: 1501: 1500: 1497: 1494: 1491: 1488: 1468: 1464: 1463: 1460: 1457: 1454: 1451: 1431: 1427: 1426: 1423: 1420: 1417: 1415: 1412: 1408: 1407: 1404: 1401: 1398: 1395: 1375: 1371: 1370: 1367: 1364: 1361: 1358: 1338: 1334: 1333: 1330: 1327: 1324: 1321: 1301: 1297: 1296: 1293: 1290: 1287: 1284: 1264: 1260: 1259: 1254: 1249: 1244: 1237: 1128: 1109: 1108: 1097: 1092: 1088: 1084: 1079: 1068: 1064: 1059: 1054: 1051: 1046: 1042: 1038: 1033: 1022: 1018: 1014: 1009: 1004: 1001: 996: 992: 988: 984: 975: 968: 959: 953: 949: 945: 940: 937: 931: 928: 925: 922: 919: 901: 900: 885: 882: 879: 876: 871: 867: 863: 860: 855: 844: 840: 835: 830: 827: 822: per year 817: 813: 809: 806: 803: 800: 798: 796: 793: 790: 787: 782: 778: 774: 771: 766: 755: 751: 747: 742: 737: 734: 729: per year 724: 720: 716: 713: 710: 707: 705: 703: 695: 691: 687: 683: 679: 674: 671: 668: 663: 656: 647: 641: 637: 633: 627: 624: 621: 619: 617: 614: 613: 589:.440 km/s 565: 564: 553: 547: 542: 538: 531: 528: 525: 522: 499: 463: 452: 440: 409: 374: 373: 367: 357: 351: 345: 321: 311: 310: 299: 296: 293: 290: 283: 279: 272: 263: 257: 253: 246: 243: 240: 237: 234: 231: 212: 209: 161:orbital plane 154: 151: 106:ecliptic plane 78:reconnaissance 69: 66: 52:, is a nearly 26: 24: 14: 13: 10: 9: 6: 4: 3: 2: 2934: 2923: 2920: 2919: 2917: 2907: 2902: 2897: 2895: 2885: 2883: 2873: 2871: 2861: 2859: 2854: 2849: 2847: 2837: 2835: 2830: 2825: 2823: 2818: 2813: 2809: 2796: 2788: 2787: 2784: 2778: 2775: 2773: 2770: 2768: 2765: 2763: 2760: 2758: 2755: 2753: 2750: 2748: 2745: 2743: 2742:-body problem 2741: 2737: 2735: 2732: 2730: 2727: 2725: 2722: 2720: 2717: 2715: 2712: 2710: 2707: 2705: 2702: 2700: 2697: 2695: 2692: 2690: 2687: 2686: 2684: 2682: 2676: 2670: 2667: 2665: 2662: 2660: 2657: 2655: 2652: 2650: 2647: 2645: 2644:Oberth effect 2642: 2640: 2637: 2635: 2632: 2630: 2627: 2625: 2622: 2620: 2617: 2615: 2612: 2610: 2607: 2605: 2602: 2600: 2597: 2596: 2594: 2592: 2588: 2578: 2570: 2566: 2564: 2563:Orbital speed 2557: 2555: 2548: 2546: 2539: 2538: 2536: 2532: 2526: 2519: 2517: 2510: 2508: 2501: 2499: 2484: 2482: 2475: 2474: 2472: 2468: 2462: 2455: 2453: 2446: 2444: 2437: 2435: 2428: 2427: 2425: 2421: 2415: 2404: 2402: 2395: 2393: 2386: 2384: 2377: 2376: 2374: 2368: 2365: 2364: 2361: 2358: 2356: 2352: 2340: 2337: 2336: 2334: 2330: 2327: 2325: 2322: 2318: 2317:Earth's orbit 2315: 2314: 2313: 2310: 2309: 2307: 2305: 2302: 2298: 2295: 2293: 2290: 2288: 2285: 2283: 2280: 2279: 2277: 2273: 2270: 2268: 2265: 2263: 2260: 2259: 2257: 2256: 2254: 2248: 2242: 2239: 2237: 2234: 2232: 2229: 2227: 2224: 2222: 2219: 2217: 2214: 2212: 2209: 2207: 2204: 2202: 2199: 2197: 2194: 2192: 2189: 2187: 2184: 2180: 2177: 2175: 2174:Geostationary 2172: 2171: 2170: 2167: 2166: 2164: 2162: 2158: 2152: 2149: 2145: 2142: 2140: 2137: 2136: 2135: 2132: 2130: 2127: 2125: 2122: 2120: 2117: 2115: 2112: 2110: 2107: 2105: 2102: 2100: 2096: 2093: 2091: 2088: 2086: 2083: 2081: 2078: 2076: 2072: 2069: 2067: 2064: 2062: 2059: 2057: 2054: 2053: 2051: 2047: 2044: 2042: 2038: 2034: 2026: 2021: 2019: 2014: 2012: 2007: 2006: 2003: 1997: 1994: 1993: 1989: 1980: 1973: 1968: 1966: 1963: 1960: 1957: 1954: 1951: 1950: 1946: 1938: 1934: 1930: 1923: 1920: 1915: 1911: 1907: 1903: 1899: 1895: 1891: 1887: 1880: 1877: 1872: 1868: 1864: 1860: 1853: 1851: 1847: 1842: 1836: 1832: 1827: 1826: 1818: 1815: 1802: 1798: 1794: 1788: 1785: 1777: 1771: 1768: 1755: 1751: 1747: 1743: 1739: 1735: 1728: 1725: 1719: 1714: 1711: 1709: 1706: 1704: 1701: 1699: 1696: 1694: 1691: 1689: 1686: 1684: 1681: 1680: 1675: 1673: 1671: 1667: 1663: 1659: 1655: 1651: 1647: 1643: 1638: 1634: 1626: 1621: 1619: 1615: 1611: 1607: 1603: 1591: 1588: 1585: 1582: 1562: 1559: 1558: 1554: 1551: 1548: 1546: 1543: 1540: 1539: 1535: 1532: 1529: 1526: 1506: 1503: 1502: 1498: 1495: 1492: 1489: 1469: 1466: 1465: 1461: 1458: 1455: 1452: 1432: 1429: 1428: 1424: 1421: 1418: 1416: 1413: 1410: 1409: 1405: 1402: 1399: 1396: 1376: 1373: 1372: 1368: 1365: 1362: 1359: 1339: 1336: 1335: 1331: 1328: 1325: 1322: 1302: 1299: 1298: 1294: 1291: 1288: 1285: 1265: 1262: 1261: 1255: 1250: 1245: 1242: 1233: 1232: 1229: 1228: 1227: 1207: 1144: 1137: 1127: 1123: 1095: 1090: 1086: 1082: 1077: 1066: 1062: 1057: 1052: 1049: 1044: 1040: 1036: 1031: 1020: 1016: 1012: 1007: 1002: 999: 994: 990: 986: 982: 973: 966: 957: 951: 947: 943: 938: 935: 929: 926: 923: 920: 917: 910: 909: 908: 883: 880: 877: 874: 869: 865: 861: 858: 853: 842: 838: 833: 828: 815: 811: 804: 801: 799: 791: 788: 785: 780: 776: 772: 769: 764: 753: 749: 745: 740: 735: 722: 718: 711: 708: 706: 693: 689: 685: 681: 677: 672: 669: 666: 661: 654: 645: 639: 635: 631: 625: 622: 620: 615: 604: 603: 602: 599: 595: 582: 574: 551: 545: 540: 536: 529: 526: 523: 520: 513: 512: 511: 508: 490: 482: 473: 462: 451: 439: 432: 416: 415:sidereal year 408: 398: 389: 380: 368: 366:of the orbit, 365: 358: 350: 346: 344:of the Earth, 343: 339: 320: 316: 315: 314: 297: 294: 291: 288: 281: 277: 270: 261: 255: 251: 244: 241: 238: 235: 222: 221: 220: 218: 210: 208: 206: 202: 198: 193: 191: 187: 182: 180: 176: 172: 168: 164: 160: 152: 150: 148: 144: 140: 136: 131: 127: 123: 115: 111: 107: 102: 98: 95: 91: 87: 83: 79: 75: 67: 65: 63: 59: 55: 51: 47: 43: 34: 30: 19: 2922:Earth orbits 2894:Solar System 2757:Perturbation 2739: 2714:Ground track 2624:Gravity turn 2575:   2568: 2561:   2552:   2543:   2523:   2514:   2505:   2498:True anomaly 2496:   2481:Mean anomaly 2479:   2459:   2450:   2441:   2432:   2412:   2399:   2390:   2383:Eccentricity 2381:   2339:Lunar cycler 2328: 2312:Heliocentric 2252:other points 2225: 2201:Medium Earth 2099:Non-inclined 1979:the original 1965:NASA Q&A 1928: 1922: 1892:(1): 84–93. 1889: 1885: 1879: 1862: 1859:ESA Bulletin 1858: 1824: 1817: 1805:. Retrieved 1801:the original 1796: 1787: 1770: 1758:. Retrieved 1754:the original 1741: 1737: 1727: 1646:ERS-1, ERS-2 1642:frozen orbit 1629:1000 km 1622: 1601: 1599: 1208: 1160:6554 km 1142: 1138: 1125: 1121: 1117:7200 km 1110: 902: 597: 593: 566: 509: 488: 480: 471: 460: 449: 437: 406: 396: 387: 378: 375: 348: 318: 312: 215:The angular 214: 194: 183: 156: 125: 121: 119: 71: 68:Applications 49: 45: 41: 39: 29: 2882:Outer space 2870:Spaceflight 2834:Mathematics 2719:Hill sphere 2554:Mean motion 2434:Inclination 2423:Orientation 2324:Mars cycler 2262:Areocentric 2134:Synchronous 1708:Polar orbit 1134:800 km 54:polar orbit 2659:Rendezvous 2355:Parameters 2191:High Earth 2161:Geocentric 2114:Osculating 2071:Elliptical 1720:References 1666:RADARSAT-2 1602:local time 342:oblateness 217:precession 190:retrograde 159:osculating 130:terminator 90:satellites 2846:Astronomy 2704:Ephemeris 2681:mechanics 2591:Maneuvers 2534:Variation 2297:Libration 2292:Lissajous 2196:Low Earth 2186:Graveyard 2085:Horseshoe 1914:236275629 1608:, not to 1253:latitude 1246:Altitude 1053:− 1003:− 974:μ 939:ρ 930:− 927:≈ 921:⁡ 878:⁡ 859:− 829:× 816:∘ 805:− 789:⁡ 770:− 736:× 723:∘ 712:− 670:⁡ 662:μ 626:− 623:≈ 616:ρ 546:μ 530:π 354:≈ 6378 km 292:⁡ 245:π 239:− 233:Ω 230:Δ 62:precesses 2916:Category 2470:Position 2095:Inclined 2066:Circular 1688:Analemma 1676:See also 1662:EUMETSAT 1635:and the 1618:Analemma 1564:⁠3 1508:⁠2 1471:⁠2 1434:⁠2 1378:⁠1 1341:⁠1 1304:⁠1 1267:⁠1 1251:Maximal 1239:Period ( 1236:per day 1204: km 1192: km 1176: km 1152: km 1025: km 903:or when 758: km 496:, where 429:10  137:such as 94:infrared 2906:Science 2822:Physics 2808:Portals 2679:Orbital 2649:Phasing 2609:Delta-v 2414:Apsides 2408:,  2206:Molniya 2124:Parking 2061:Capture 2049:General 1933:Bibcode 1894:Bibcode 1867:Bibcode 1807:24 June 1746:Bibcode 1668:of the 1650:Envisat 1592:142.1° 1579:⁠ 1555:125.3° 1536:116.0° 1523:⁠ 1499:110.1° 1486:⁠ 1462:106.0° 1449:⁠ 1425:103.0° 1406:100.7° 1393:⁠ 1356:⁠ 1319:⁠ 1282:⁠ 1256:Inclin- 1234:Orbits 1224:⁠ 1212:⁠ 1071: h 847: h 579:is the 571:is the 493:⁠ 476:⁠ 468:⁠ 445:⁠ 401:⁠ 383:⁠ 362:is the 336:is the 163:precess 147:PROBA-2 74:imaging 2335:Other 2236:Tundra 2104:Kepler 2080:Escape 2033:orbits 1955:(p. 8) 1912:  1837:  1760:19 May 1583:≈ 3:26 1527:= 2:40 1490:= 2:24 1453:≈ 2:11 1397:≈ 1:51 1369:99.0° 1360:≈ 1:43 1332:97.7° 1323:= 1:36 1295:96.6° 1286:= 1:30 1258:ation 567:where 313:where 197:oblate 186:minute 143:Hinode 80:, and 2858:Stars 2577:Epoch 2366:Shape 2304:Lunar 2258:Mars 2250:About 2221:Polar 2041:Types 1982:(PDF) 1975:(PDF) 1910:S2CID 1779:(PDF) 1658:MetOp 1589:37.9° 1552:54.7° 1533:64.0° 1496:69.9° 1459:74.0° 1422:77.0° 1403:79.3° 1366:81.0° 1329:82.3° 1292:83.4° 1248:(km) 1198:> 1186:< 1067:3.795 843:3.795 419:1.990 326:1.082 205:Venus 139:TRACE 108:with 2369:Size 2308:Sun 2287:Halo 2139:semi 1835:ISBN 1809:2017 1762:2015 1664:and 1648:and 1616:and 1586:5165 1549:4182 1530:3385 1493:2722 1456:2162 1419:1681 1400:1262 1194:but 1141:cos 201:Mars 145:and 2144:sub 2056:Box 1902:doi 1831:339 1652:of 1620:). 1363:894 1326:567 1289:274 1221:364 1215:365 1202:352 1190:352 1174:352 1150:352 1021:352 918:cos 875:cos 812:360 786:cos 754:352 719:360 667:cos 587:600 585:398 431:rad 421:968 289:cos 171:Sun 46:SSO 2918:: 2492:, 2488:, 2097:/ 2073:/ 1908:. 1900:. 1890:59 1888:. 1863:72 1861:. 1849:^ 1833:. 1795:. 1742:37 1740:. 1736:. 1467:10 1446:11 1430:11 1411:12 1390:13 1384:11 1374:13 1337:14 1300:15 1263:16 1243:) 1206:. 1200:12 1188:12 1172:12 1170:= 1162:, 1158:= 1148:12 1132:≈ 1124:− 1115:= 1017:12 750:12 596:≈ 474:= 470:= 443:= 433:/s 424:71 381:= 333:10 328:63 324:= 141:, 76:, 40:A 2810:: 2740:n 2572:0 2569:t 2559:v 2550:n 2541:T 2521:l 2512:L 2503:E 2494:f 2490:θ 2486:ν 2477:M 2457:ϖ 2448:ω 2439:Ω 2430:i 2410:q 2406:Q 2397:b 2388:a 2379:e 2024:e 2017:t 2010:v 1939:. 1935:: 1916:. 1904:: 1896:: 1873:. 1869:: 1843:. 1811:. 1781:. 1764:. 1748:: 1576:7 1573:/ 1570:3 1566:+ 1560:7 1544:3 1541:8 1520:3 1517:/ 1514:2 1510:+ 1504:9 1483:5 1480:/ 1477:2 1473:+ 1443:/ 1440:2 1436:+ 1414:2 1387:/ 1380:+ 1353:7 1350:/ 1347:5 1343:+ 1316:5 1313:/ 1310:3 1306:+ 1279:2 1276:/ 1273:1 1269:+ 1241:h 1218:/ 1196:a 1184:p 1180:i 1168:a 1164:i 1156:a 1143:i 1129:E 1126:R 1122:a 1113:a 1096:. 1091:3 1087:/ 1083:7 1078:) 1063:T 1058:( 1050:= 1045:2 1041:/ 1037:7 1032:) 1013:a 1008:( 1000:= 995:2 991:/ 987:7 983:a 967:2 962:E 958:R 952:2 948:J 944:3 936:2 924:i 905:ρ 884:, 881:i 870:3 866:/ 862:7 854:) 839:T 834:( 826:) 808:( 802:= 792:i 781:2 777:/ 773:7 765:) 746:a 741:( 733:) 715:( 709:= 694:2 690:/ 686:7 682:a 678:2 673:i 655:2 650:E 646:R 640:2 636:J 632:3 598:a 594:p 577:μ 569:a 552:, 541:3 537:a 527:2 524:= 521:T 505:T 500:E 498:T 489:T 485:/ 481:Ω 479:Δ 472:ρ 464:E 461:T 457:/ 453:E 450:Ω 448:Δ 441:E 438:n 427:× 417:( 410:E 407:n 397:t 395:d 392:/ 388:Ω 386:d 379:ρ 370:i 360:p 352:E 349:R 331:× 322:2 319:J 298:, 295:i 282:2 278:p 271:2 266:E 262:R 256:2 252:J 242:3 236:= 44:( 20:)

Index

Heliosynchronous orbit

polar orbit
mean solar time
precesses
imaging
reconnaissance
weather satellites
illumination angle
satellites
infrared

ecliptic plane
local solar time
descending node
terminator
scientific satellites
TRACE
Hinode
PROBA-2
osculating
precess
celestial sphere
Sun
Technical details
equatorial bulge
minute
retrograde
oblate
Mars

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