Intuition The ONE core idea
Every orbit — LEO, GEO, Molniya, all of them — is the same thing: an object falling around Earth on an ellipse, held by gravity alone. The "types" are just different sizes (a ), different stretches (e ), and different tilts (i ) of that one ellipse, chosen for what the mission needs to see or do.
Before you can read the parent note Orbit types , you must own every symbol it throws at you. This page builds each one from nothing — plain words, then a picture, then why the topic can't live without it . Read top to bottom; each block uses only symbols defined above it. Each figure is called out by number in the text — look for "Figure 1 ", "Figure 2 ", and so on.
Common mistake The units trap that ruins every calculation
Why it feels right: distances look natural in kilometres. The fix: μ carries units of metres (m 3 / s 2 ), so before you plug into any formula, convert every length to metres (SI). On this page R ⊕ , h , r are quoted in km for readability, but a 6791 km radius must enter formulas as 6.791 × 1 0 6 m. Mixing km and m is the single most common orbital-mechanics blunder.
Picture a satellite as a dot going around a big ball (Earth). Three lengths describe "how high up" it is. See Figure 1 .
Definition The three heights
R ⊕ — the radius of the Earth itself, ground to centre. The little cross-in-a-circle ⊕ is the astronomer's symbol for Earth. Value: R ⊕ ≈ 6371 km.
h — the altitude : how far the satellite floats above the ground .
r — the orbital radius : distance from Earth's centre to the satellite.
Figure 1 — the three lengths R ⊕ (cyan), h (amber) and r (white) sharing Earth's centre as origin.
WHY three symbols and not one? Because gravity is measured from the centre of the Earth, not the surface. So all the physics formulas want r — but engineers quote h because that's what you see. The bridge is simple:
h where the formula wants r
Why it feels right: h is "the height", so surely that's the distance. The fix: every gravity formula measures from Earth's centre . Always add R ⊕ first. Forgetting this makes a 420 km ISS look 15× too close to Earth's centre.
Not every orbit is a perfect circle. Most are ellipses — a circle that's been squashed. One number, e , measures how squashed. See Figure 2 .
e
e is a number that says how stretched an orbit is . For orbits that stay bound to Earth (the only kind this topic cares about) it runs from 0 up to just below 1 :
e = 0 → a perfect circle .
0 < e < 1 → a closed ellipse ; the bigger e , the more egg-shaped (a long, thin "cigar" as e → 1 ).
e = 1 → a parabola (escapes, never returns); e > 1 → a hyperbola (a fly-by). These are unbound and never orbit — so every orbit type here has 0 ≤ e < 1 .
Figure 2 — as e grows from 0 (cyan circle) to 0.7 (amber), the ellipse stretches while Earth stays at one focus.
Intuition What Figure 2 shows
As e grows, the orbit stretches. Earth sits not at the centre but at one focus — pushed off to one side. So one end of the orbit sits close to Earth and the other end sits far . That asymmetry is the whole trick behind Molniya orbits.
WHY the topic needs e : it is the single knob that separates a GEO (needs e = 0 , must hang still) from a Molniya (wants big e , so it can loiter far away over the north). No e , no orbit types.
An ellipse has a "long way across" and a "short way across". Half the long way is the master size number. See Figure 3 .
Definition Semi-major axis and the two extremes
a — the semi-major axis : half the length of the longest line through the ellipse. This is the size of the orbit.
r p — perigee radius : distance from Earth's centre to the closest point (peri = near).
r a — apogee radius : distance to the farthest point (apo = away).
Figure 3 — perigee r p and apogee r a from Earth at the focus; the full span is 2 a = r p + r a , with r p = a ( 1 − e ) , r a = a ( 1 + e ) .
a is the star of the show
Two orbits with the same a take the same time to go round — even if one is a circle and one is a stretched cigar (as long as a matches). That is why a Molniya and a 12-hour circular MEO share the same a = 26 560 km. The parent note leans on this in Worked Example 3. For a circle e = 0 , so r p = r a = a = r — the ellipse formulas quietly reduce to the circle ones.
An orbit lives in a flat plane slicing through Earth's centre. i measures how tilted that plane is compared to the equator. See Figure 4 .
Figure 4 — three inclinations: equatorial (i = 0 ∘ , cyan), the Molniya critical angle (i = 6 3 ∘ , white), and retrograde SSO-like (i = 9 8 ∘ , amber).
Intuition Why every quadrant of
i matters
i = 0 ∘ is forced for GEO — only an equatorial orbit can hang over one spot.
i ≈ 63. 4 ∘ is the magic Molniya angle.
i ≈ 9 8 ∘ (just past polar, retrograde) is what makes Sun-synchronous orbits work.
The whole "types" story is a story about choosing i . Notice cos i : it is positive below 9 0 ∘ , zero at 9 0 ∘ , and negative above. The parent note needs a negative cos i to make an SSO precess the right way — that is exactly why SSO must be retrograde.
Gravity's pull depends on two things: how strong gravity is in general, and how heavy the puller is.
Definition Gravity constants
G — the universal gravitational constant , the same everywhere in the cosmos: G ≈ 6.674 × 1 0 − 11 m 3 kg − 1 s − 2 . (Those units are what make the final force come out in newtons — and they are why lengths must be in metres and mass in kilograms.)
M — the mass of the pulling body (here, Earth's mass, in kilograms).
μ (Greek "mu") — the ==shorthand μ = GM ==, called the standard gravitational parameter . For Earth μ ≈ 3.986 × 1 0 14 m 3 / s 2 . Notice the kg in G has cancelled against the mass — that is why μ has no kilograms left.
G and M into μ ?
We can never weigh the Earth directly, but we can measure how satellites move, and that measurement gives GM as one combined number to superb precision. So astrodynamics never splits them — it always uses μ . Fewer symbols, more accuracy. Every orbit formula in the parent note carries a μ .
μ as a mass
Why it feels right: it looks like it stands for "the planet". The fix: μ has units of m 3 / s 2 , not kilograms — it is G times mass, a rate-of-pull, not a weight.
To stay in orbit, a satellite must move. A few symbols describe that motion.
Definition Speed, period, and satellite mass
v — the orbital speed (metres per second): how fast the satellite travels.
T — the period : the time for one full lap (seconds).
m — the mass of the satellite itself (kilograms) — the little object doing the orbiting, not Earth's mass M . It appears in the force balance and, beautifully, cancels out.
Intuition Why anything can circle at all — centripetal force
To move in a circle, something must constantly pull you toward the centre , otherwise you fly off straight. That inward pull is called the centripetal ("centre-seeking") requirement, of size m v 2 / r for a satellite of mass m at speed v and radius r . For a satellite, gravity provides exactly this pull — nothing else is out there. Set gravity's pull equal to the centripetal need and the whole of orbital speed falls out. That single balance is the seed of every formula the parent note derives.
The parent note insists GEO uses 86 164 s, not 86 400 s. Here is why there are two days at all.
Definition Solar day vs sidereal day
Solar day (86 400 s) — Sun overhead to Sun overhead again. This is the clock day.
Sidereal day (86 164 s) — one full spin of Earth relative to the distant stars .
Intuition Why the star-day is shorter
While Earth spins once, it also creeps a little along its year-long path around the Sun. So after one true spin (measured against the fixed stars), Earth must turn a tiny bit extra to bring the Sun back overhead. That extra bit is about 4 minutes. A satellite doesn't care about the Sun — it must match Earth's true spin against the stars, so GEO uses the sidereal day.
Earth is not a perfect ball; it bulges at the equator. That bulge has a name in the maths.
J 2 term
J 2 is a number describing Earth's equatorial bulge , about 1.083 × 1 0 − 3 . It measures how much Earth's gravity differs from a perfect sphere's.
Intuition Why one small number matters so much
The bulge tugs sideways on a tilted orbit and slowly rotates the orbit plane and rotates the ellipse within its plane . Left alone this is a nuisance; but SSO and Molniya orbits deliberately harness these two rotations. So J 2 is the villain-turned-hero of the parent note — you can't understand SSO or the 63. 4 ∘ magic without it. The full machinery lives in J2 Perturbation and Nodal Precession .
circular speed v and period T
Orbit types LEO MEO GEO HEO SSO Molniya
The deeper machinery each foundation opens: the balance in §6 is fully worked in the Two-Body Problem and the Vis-Viva Equation ; the timing law T 2 ∝ a 3 is Kepler's Laws of Planetary Motion ; low-orbit consequences appear in Atmospheric Drag and Orbital Decay and Satellite Ground Tracks ; and changing a (raising or lowering an orbit) costs energy studied in Hohmann Transfer and Delta-v Budgets .
Cover the right side and test yourself.
Convert altitude 420 km to orbital radius r (in SI) r = 6371 + 420 = 6791 km = 6.791 × 1 0 6 m.
What does eccentricity e = 0 mean geometrically? A perfect circle.
What is the range of e for a bound orbit, and what is e = 1 ? 0 ≤ e < 1 for orbits; e = 1 is a parabola (escape).
Write r p and r a in terms of a and e r p = a ( 1 − e ) , r a = a ( 1 + e ) .
Write a in terms of apogee and perigee radii a = ( r p + r a ) /2 .
What is inclination i the angle between? The orbit plane and Earth's equator.
Is cos i positive or negative for a retrograde (i > 9 0 ∘ ) orbit? Negative.
What does μ stand for, its units, and G 's units? μ = GM , units m 3 / s 2 ; G is m 3 kg − 1 s − 2 .
Which force supplies the centripetal pull for a satellite? Gravity, GM m / r 2 .
What is m in the force balance, and why does the orbit not depend on it? The satellite's own mass; it cancels from both sides.
Which day (sidereal or solar) does GEO use, and its length? Sidereal, 86 164 s.
What does J 2 physically represent? Earth's equatorial bulge (non-spherical gravity).
Recall Self-test: can you state the core idea in one breath?
Every orbit is one ellipse under gravity; the types just vary its size a , stretch e , and tilt i .
Ready? ::: If you answered all checklist items, open the parent note.