{"id":1163,"date":"2025-02-14T17:38:23","date_gmt":"2026-06-15T08:58:41","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/?p=1163"},"modified":"2026-06-15T09:29:58","modified_gmt":"2026-06-15T09:29:58","slug":"what-do-you-mean-by-hohmann-transfer-orbit","status":"publish","type":"post","link":"https:\/\/starpath.global\/blog\/what-do-you-mean-by-hohmann-transfer-orbit\/","title":{"rendered":"What do you mean by Hohmann Transfer Orbit?"},"content":{"rendered":"

Hohmann Transfer Orbit is an elliptical orbit that is used to transfer a spacecraft between two orbits of different altitudes around a central body. It is a maneuver that was invented by German scientist Wolfman Hohmann, in 1925. This orbit is considered the most fuel-efficient way of transferring a satellite or a spacecraft from one lower circular orbit to another higher circular orbit. <\/p>\n

When a satellite or a spacecraft is traveling from earth to any other destination such as the Moon or Mars, the spacecraft or the satellite moving directly from Point A to Point B consumes more fuel to escape from the earth\u2019s gravitational pull and is more expensive to achieve. <\/p>\n

<\/p>\n

\n

Also Read: What are the Best Practices for optimizing Satellite Orbit Control?<\/h4>\n<\/div>\n

To reduce this menace, the spacecraft is first launched in a circular orbit from earth. Once it\u2019s in orbit, the spacecraft accelerates itself by firing its rocket motors for a brief period to create a new elliptical orbit known as the \u2018Hohmann Transfer Orbit<\/strong>\u2019 where the satellite or the spacecraft steers away from the earth to reach the orbit at a higher altitude. Once it reaches the apogee (farthest point from the earth) of the Hohmann transfer orbit from the earth, the satellite or the spacecraft decelerates to then stabilize itself in the higher orbit from earth.<\/p>\n

India\u2019s Mars Orbiter Mission (MOM) used the Hohmann Transfer orbit to place the spacecraft in mars orbit. Instead of a direct exit from the earth, a slow exit with the Hohmann transfer orbit made the MOM more economical and a considerable amount of fuel was also conserved.<\/p>\n