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UT clock confusion...


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I decided to try messing around with time- based orbits to simplify astronavigation and ran into a weird problem.

According to my math, an orbit at 147,319m of should have a period of 36 minutes on the dot. I orbited a ship at exactly this altitude and timed my passage over KSC. It actually takes precisely 40 minutes according to the UTC clock. :confused:

This has to be confusion on my part about sidereal vs. solar time, but I'm having a hard time wrapping my head around it. Why am I missing 4 minutes per orbit?? *scratches head*...

Anyone run into this problem or have any ideas?

Best,

-Slashy

Edited by GoSlash27
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Your passage over KSC appears to be delayed (compared to your orbital period) because Kerbin is rotating underneath you.

After your 36-minute orbit, you return to the exact same point with regard to the fixed stars. However, Kerbin has rotated 36 x 360° / 6 x 60 = 36°. To catch up to KSC you have to orbit that additional 36°, plus the amount Kerbin rotates while you're completing that additional orbit.

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Your passage over KSC appears to be delayed (compared to your orbital period) because Kerbin is rotating underneath you.

After your 36-minute orbit, you return to the exact same point with regard to the fixed stars. However, Kerbin has rotated 36 x 360° / 6 x 60 = 36°. To catch up to KSC you have to orbit that additional 36°, plus the amount Kerbin rotates while you're completing that additional orbit.

I think this might be it.

If I want to orbit 10 times a day WRT the ground, I have to select an orbit that cycles 11 times a day to make up for Kerbin's 1 orbit. That would explain why the discrepancy is 4 minutes per orbit exactly...

I'll try that. If it works, I'll switch it to "answered".

Thanks!

-Slashy

Edited by GoSlash27
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Having had time now to jot down some notes about this, I think the easy way to think about it is in terms of rotational velocities.

Your 36-minute orbit has a rotational velocity of 10°/minute (I'm using minutes because it makes the calculations easy in this case)

Kerbin has a rotational velocity of 1°/minute.

So your relative rotational velocity is 10-1 = 9°/minute.

Therefore to complete a 360° orbit relative to a fixed point on the ground requires 360/9 = 40 minutes.

This is, of course, the simplified case not accounting for orbital inclination.

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