“ Cross-seam inter-satellite link hand-offs would have to happen very rapidly and cope with large Doppler shifts; therefore, Iridium supports inter-satellite links only between satellites orbiting in the same direction.”
https://en.m.wikipedia.org/wiki/Iridium_satellite_constellat...
https://info.cobaltiron.com/blog/petabyte-how-much-informati...
Maybe the future of usb in 10 years :)
Probably close to none. The lifetime of the satellites is about 5 years give or take. According to this page [1], a total of 355 satellites have deorbited over the past roughly 5 years. That's an average of about 71 per year or about one every 5 days.
Since planned disposals are done over uninhabited areas (e.g. the pacific ocean), the likelihood of spotting one is very low.
Hope that helps answer your question, even it wasn't necessarily meant seriously :)
[1] https://starlinkinsider.com/starlink-launch-statistics/There's an animation on linked article that explains this pretty well: https://upload.wikimedia.org/wikipedia/commons/thumb/9/90/Ir...
I don’t know how you would know that. People are very bad at seeing distances at these scales.
If they were indeed satelites they could be starlink satelites. They are put into orbit as a bunch together and then they spread along their orbital path as they take up their position.
This article has a picture, maybe you can check if it is similar to what you have seen? https://earthsky.org/space/spacex-starlink-satellites-explai...
If you could recall more details then maybe we can figure out more exactly what this might have been. (Such as where you were, which direction you were looking at, when did this happen, how fast did they cross the sky and how far the dots were from each other. Were the line spread in the direction they were moving or sideways?)
https://satellitemap.space is pretty amazing but a Starlink satellite looks massive on there, really at the scales we are talking they wouldn't even be a pixel. Do we know how many of the satellites are actually interlinked by lasers?
https://www.timeanddate.com/astronomy/different-types-twilig...
It's been awhile, but I'm pretty sure I've seen these much later than that. I'm talking about lying in a sleeping bag, looking up at the amazing starfields of pitch-black wilderness nights (tip: never use a tent except in extremis - look what you're missing!).
https://en.wikipedia.org/wiki/Shannon%E2%80%93Hartley_theore...
I don't think that breaks net neutrality either, which the FCC seems to be reimplementing
Edit: see https://openconnect.netflix.com/en/
https://en.wikipedia.org/wiki/Defense_Production_Act_of_1950
300+ minutes a day for TV + vMOD (streaming services). Since no one actually watches TV anymore, at least not through traditional TV, I summed them.
not for awhile. apple vision / oculus will stream (4k/8k) 3d movies.
Assuming the lenses are about 2 inches across (from photos) and they are 1310nm IR lasers:
https://www.wolframalpha.com/input?i=single+slit+diffraction...
So we have a minimum beam width of 0.0014 degrees.
And the speed of light round trip distance is say 3.3 milliseconds.
So the question is, does the angle between the satellites change faster than 0.0014/0.0033 = 0.42 degrees/second?
Well the worst case is one satellite heading north at 7.4 Km/s and another heading south at 7.4 km/s. Lets assume the satellites are 550 km apart (the distance between planes at the equator), and use the small angle approximation... Comes out as 1.4 degrees per second.
So yes, these satellites do need the ability to aim transmit and receive in different directions! (although they might be able to just defocus the beam a little when angles are changing fast to trade off throughput for design complexity)
Apparently it only happens above/below 68 degrees latitude, so the next satellite with a working inter-orbital-plane connection is at most one hop ahead or behind.
https://spaceflight101.com/spacecraft/iridium-next/ has some more photos and diagrams; seems like they're really mechanically steered even on the NEXT constellation.
Even back to 1950, for per household data, it was above 4 hours.
[1] https://www.nielsen.com/insights/2009/average-tv-viewing-for...
https://en.wikipedia.org/wiki/Category:United_States_Navy_sh...
But that's mostly been "optimized away" in more-recent times, in the name of Capitalism and Campaign Donations.
The flashing of satellites will generally be gentler than the short burst strobing of an aircraft.
https://www.sda.mil/wp-content/uploads/2023/06/SDA_OCT_Stand...
SpaceX says otherwise, see [1]
SpaceX spokesman James Gleeson, when asked about the 10 satellites, said SpaceX is “performing a controlled de-orbit of several first iteration Starlink satellites,” using onboard propulsion.
There's a difference between unscheduled deorbiting (as happened to about 40 satellites after a solar storm in February 2022) and a scheduled deorbiting manoeuvre trigged by ground control. Starlink satellites use electric on-board propulsion (Krypton powered Hall thrusters) that doesn't run out as quickly as chemical or cold gas gas thrusters. There's also not much precision needed to avoid major population centres - Earth is pretty big after all.[1] https://spacenews.com/spacex-launches-fourth-batch-of-starli...
Men spent 3 hours a day watching TV, and women 2.5 hours. But TV time is lower (around 2 hrs/day) from ages 20-44, then increases again after 45 and peaks at 75 years old at nearly 5 hours a day.
Households without kids watch more TV, which surprised me.
I'm not sure that's saying household time. For example, when they survey a household it wasn't clear to me if they survey everyone in the household or just one person. If it's one person then it sounds like they collect how that one person (age 15+) spent their own time and if there were kids in their household.
So then it'd be accurate to say that individuals in households without kids watch more TV as a singular activity (the survey doesn't allow simultaneous activities).
In comparison Nielsen used TV viewing diaries and automated data collection meters. You could have the TV on in the background while doing chores and it would still count.
It's interesting that the 2009 ATUS survey [3] had a 2.82 hour/person average because that's fairly different from the Nielsen data (4 hours 49 minutes/person).
I wonder if this difference is people underreporting in ATUS or Nielsen overreporting or a factor of differences in limitations in ATUS (no simultaneous activities allowed, 15+ age limitation) or Nielsen.
[1] https://www.bls.gov/opub/hom/atus/data.htm
[2] https://www.bls.gov/tus/questionnaires/tuquestionnaire.pdf
[3] https://www.bls.gov/news.release/archives/atus_06222010.pdf
This generally involves landing at a precise location of the Earth. It goes by a nickname, Point Nemo. A patch of ocean in the south pacific farthest away from any land. It's also far from standard shipping lanes. If you can't achieve this type of targeting it, definitionally, is not a controlled re-entry.
> It simply means aiming for a certain latitude by adjusting the orbit accordingly
You cannot aim a satellite for a "certain latitude" as orbits cannot follow lines of latitude. That's not how orbital dynamics work. I'm not quite sure what you meant to convey here.
> This also means that the target is not "all over the world" as you put it - it's a very narrow, well defined stripe/trace (remember the scale we're talking about here!) and that's exactly what a controlled de-orbit is about.
No it's all over the world, definitionally, because low earth orbits cross the entire planet as the Earth rotates. The possible locations the satellite can re-enter span a large portion of the globe from the negative to the positive latitude equivalent to the spacecraft's inclination.
I think you have a major misunderstanding yourself. If there's some term I'm using that you don't understand please let me know so I can help you.
So actually this Iridium-type "seam" disappears, meaning that every satellite should always have co-orbiting "neighbors" on both sides. Cool!
[0] https://en.wikipedia.org/wiki/Right_ascension_of_the_ascendi...