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Home Academy Orbital Maneuvers & Station-Keeping Hohmann transfers
LESSON 02 OF 6

Hohmann transfers

Intermediate ~10 min Slide deck Free

The Hohmann transfer is the most fuel-efficient way to move between two circular orbits of different altitudes using two impulsive burns. It's not always the fastest — but it's almost always the cheapest in terms of ΔV.

The Hohmann transfer is the most fuel-efficient way to move between two circular orbits of different altitudes using two impulsive burns. It's not always the fastest — but it's almost always the cheapest in terms of ΔV.

What this lesson covers

The Two-Burn Sequence

A Hohmann transfer works by temporarily placing the satellite into an elliptical transfer orbit that connects the two circular orbits.

A Hohmann Transfer to ISS Altitude (~420 km)

Numbers are approximate and depend on initial orbit and burn timing. The key point: two burns each of a few tens of m/s is enough to make a significant altitude change. Compare this to the ~9,500 m/s needed to reach LEO from the ground.

When Hohmann Isn't Enough

Real missions add complexity to the pure Hohmann geometry. Understanding the deviations is as important as understanding the baseline.

Key facts

💡The Hohmann transfer was mathematically derived by German engineer Walter Hohmann in 1925 — decades before the first satellite flew. His 1925 paper correctly described the optimal transfer trajectory purely from first principles.
💡Starlink satellites using electric propulsion take weeks to spiral from their ~340 km deployment orbit to their ~550 km operational altitude — the same altitude change a chemical thruster could achieve in two burns.
Hohmann is the 'hello world' of maneuvers: simple, efficient, and everywhere.

The eccentricity spike, the period increase mid-transfer, and the return to circular orbit on arrival — recognising this three-phase TLE signature is one of the most useful pattern-recognition skills in practical orbit analysis.

All lessons in Orbital Maneuvers & Station-Keeping
01What a maneuver is~10 min02Hohmann transfers~10 min03Raise/lower orbit~10 min04Inclination changes~10 min05GEO station-keeping~10 min06De-orbit & end-of-life~10 min
← What a maneuver isAll 6 LessonsRaise/lower orbit →
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