linear error≈Rtan(Δθ)≈RΔθ
Here linear error is the error in position, R is the distance from the observer to the target and θ is the angle error. You would need incredibly good optics and resolution to minimise angular error and thus linear error.
This contrasts greatly with actual GNSS – the whole point of GPS and the others is that you don't need to determine those angles. The only thing you need to determine is the signal delay (i.e. distance) from a few satellites. That's a lot more convenient.
There are other reasons we don’t currently experience major problems with collisions in space, and why airplanes sometimes do, but it is not this.
I've also seen reports that, as the satellites become overburdened, speeds are pretty variable. Again, not saying it's a net negative, but I just don't think there are "huge advantages" to Starlink.
I’m thinking buying a camper van, and just travel through the world. Except I need internet, everywhere.
There are no such options. Starlink is the best, but there are two main problems with it:
- In the countries where it would be the most useful, it’s not allowed to be used (Garmin has the same problem with their Fenix 8 Pro, their availability maps are a joke) - You need to go back to your “home” country every other month (there is a non legal, thus risky, option to circumvent this for now)
So, that huge advantage is not here yet at all.
- data throughput orders of magnitude higher,
- the ability to use smaller and more portable antennas (e.g. ~100 Mbps with something the size of a textbook, currently ~2 Mbps and soon ~10s Mbps with your normal mobile phone),
- order of magnitude lower latency compared to GSO satellites.
Other constellations like Iridium dedicate large portions to use by government(s?), too, but simply do not have the throughput or total bandwidth that Starlink does. Your speeds there, on the expensive business plans that offer it, are measured in the low Kbps.
Conversations about the net benefit of all this, damage to having an unobstructed night sky, risks and benefits to control by a single company, competitors coming in and increasing the number of satellites yet further, potential higher-orbit constellations that won’t de-orbit for centuries, etc. can get very complex quite fast, however.
I wonder if there are other satellites not included in this dataset, or if I should search way further from the location on the map
the anti collision manuevers are hard as well.
orbits are simpler at lower lattitudes where you run a trajectory, close to parallel to the equator.
There are two clearly demarcations both north and south
In order to cover those northern/southern extremes, more expensive high inclination orbits are required (in the US these are launched from California). They are more expensive because you’re no longer getting the rotational velocity of the earth for free in your orbital velocity.
So for a LEO constellation you want to minimize the launches to high inclinations and keep the bulk in those juicy easterly ones.
click on a dot and it will show up on a list to top left, click on an item in that list and you get a flyout menu to the top left with a bunch of data regarding the satellite.