Orbits that drift¶
Gravity and orbits · level 8, lesson 4 of 6
A question to start¶
NASA's Mars Reconnaissance Orbiter photographs the surface every day at about 3 pm local time, so shadows always fall the same way and pictures taken years apart can be compared. But a plain orbit stays fixed in space while Mars goes round the Sun, so the local time under it should drift through the whole day over a Mars year. How does MRO stay at 3 pm?
The idea¶
Mars is not a perfect ball. It spins, and it bulges at the equator: its equatorial radius is 3,396 km and its polar radius 3,376 km, and the huge volcanic Tharsis region adds more. In the gravity field this shows up as the \(J_2\) term, the main correction to \(GM/r\). For Mars \(J_2 = 1.96 \times 10^{-3}\), nearly twice the Earth's \(1.08 \times 10^{-3}\).
The extra mass at the equator tugs on a tilted orbit, trying to pull it into the equator's plane. Like a spinning top pushed sideways, the orbit does not flatten; it precesses: the line where the orbit crosses the equator (the node) swings slowly round. The rate is
where \(n = \sqrt{GM/a^3}\) is the mean motion and \(i\) the inclination. For a prograde orbit (\(i < 90°\)) the node drifts west; for a retrograde one (\(i > 90°\)) east; for a polar orbit (\(i = 90°\)) not at all.
Sun-synchronous. Choose \(i\) so the node drifts east by exactly 360° per Mars year, keeping pace with the Sun:
Then the orbit always crosses the equator at the same local time. For a circular orbit 300 km above Mars, the sum gives \(i = 92.6°\): nearly polar, a little retrograde. MRO's orbit is just like this.
| Mars, 300 km | Earth, 700 km | |
|---|---|---|
| \(J_2\) | \(1.96 \times 10^{-3}\) | \(1.08 \times 10^{-3}\) |
| Required drift | 0.524° per day | 0.986° per day |
| Sun-synchronous inclination | 92.6° | 98.2° |
Mars's larger \(J_2\) and slower year mean its sun-synchronous orbits are closer to polar than Earth's.
Worked examples¶
1. The Mars sum. \(a = 3{,}689.5\) km. \(n = \sqrt{42828/3689.5^3} = 9.23\times10^{-4}\) rad/s. \((R/a)^2 = (3396.2/3689.5)^2 = 0.847\). So \(\tfrac32 n J_2 (R/a)^2 = 1.5 \times 9.23\times10^{-4} \times 1.96\times10^{-3} \times 0.847 = 2.30\times10^{-6}\) rad/s. The required rate is \(2\pi/(686.98 \times 86400) = 1.059\times10^{-7}\) rad/s. So \(\cos i = -1.059\times10^{-7}/2.30\times10^{-6} = -0.046\) and \(i = 92.6°\).
2. An equatorial orbit's drift. At \(i = 0\) the node is not defined, but the same term makes the periapsis of an elliptical equatorial orbit swing round. For a polar orbit, \(\cos i = 0\): no nodal drift, so the local time under it cycles once per Mars year.
3. A low inclined orbit. At \(i = 45°\), 300 km up: \(\dot\Omega = -2.30\times10^{-6} \times 0.707 = -1.63\times10^{-6}\) rad/s \(= -8.0°\) per day. The node goes round in 45 days.
Try it¶
- Why does \(\cos i\) have to be negative for a sun-synchronous orbit?
- Find \(\dot\Omega\) for a circular orbit 300 km up at \(i = 60°\).
- Would a sun-synchronous orbit 1,000 km above Mars need more or less inclination than one at 300 km? Why?
- What would happen to MRO's afternoon pictures if its orbit were exactly polar?
- Why does a satellite designer want \(J_2\) known precisely?
Answers
- The node must drift eastwards, with the Sun, and the formula gives eastward drift only for \(\cos i < 0\).
- \(-2.30\times10^{-6} \times 0.5 = -1.15 \times 10^{-6}\) rad/s \(\approx -5.7°\) per day.
- More: farther out \(n\) and \((R/a)^2\) are smaller, so \(|\cos i|\) must be larger, meaning \(i\) farther from 90°.
- The local time under it would drift through all hours over a Mars year, so shadows would change from picture to picture.
- Its drift sets where the orbit will be months later; an error in \(J_2\) becomes an error in the local time.
Common mistake¶
Thinking the orbit's plane is fixed. For a point mass it is. Round a real, flattened planet it turns, and mission designers use that turning on purpose.
Where it leads¶
- Back: Lagrange points · Next: The fate of Phobos
- Level 8 page · Gravity and orbits topic page
- MRO: NASA, Mars Reconnaissance Orbiter. \(J_2\) from NASA's Mars fact sheet.