US Government issues first-ever space debris penalty to Dish Network
theguardian.com
theguardian.com
If you read the consent decree[1] you can see that the monetary fee is not the only thing DISH agreed to.
In section 18 you can see they agreed to implement a compliance plan. Basically they improve on their fuel tracking, and end of mission planning. This makes it more likely that this thing won't happen again, and also makes it easier to argue if it still happens that it happened wilfully.
> Wouldn't they have also implemented a compliance program if they were fined 10% of revenue, you know to avoid future fines?
They would have spent up to 10% of revenue on lawyers and lobbying to get out of the fine entirely and thereby have no fear of another one.
But 10% of their revenue is $1.7B. It would cost them almost a decade's worth of profit, so that's how much they'd spend to prevent it, which is plenty enough to influence legislation. "Percent of revenue" fines are dumb and create crazy incentives.
This. There are other compliance conditions, and failure to comply means no more launch licenses.
There are some places where this doesn't seem to operate very well, particularly in the financial world, but in general, this is often the idea behind these penalties. Especially for the first time a law is getting enforced; it isn't really very just to ignore a law for years/decades and then one day out of the blue slam someone with multi-million dollar judgments. There are even some Common Law doctrines that the targets could use to argue against such penalties holding up in court, though, as always, trying to counter a written law with common law general doctrines is tricky. But I'd say there's at least a good chance you could get a sudden, huge initial penalty argued way down in a lawsuit.
And OK, let's say they keep getting fined. Seems like a badge of honor these days. Move fast and break things, right? The government just doesn't like, get us, man. We're the good guys here and they're trying to slow us down with red tape and bureaucracy.
If you have several choices and one is getting sanctioned for shitty practices, maybe you’ll look elsewhere.
Saying you’re a rocket engineer sounds pretty neat, but the shine wears off a bit if people recognise your employer for negative reasons.
Which is what Tesla is experiencing at the moment in their facility Grünheide [1]... a toxic mixture of low wages, bad employment conditions, and reports about unsafe practices.
[1] https://t3n.de/news/tesla-gruenheide-personalmangel-und-ange...
I agree with the sentiment that the reputation hit is imaginary, and really only serves to prevent stiffer fines.
Actually, they shouldn't be charged a fine, instead, they should have to go and get it back.
Curious. Willing to bet some of these regulators kids end up at Dish over the next few years.
In reference to your previous question, along with the obvious brute fact of the fines not escalating for the same infraction over time, I would take a first stab at an answer being that the stronger the "revolving door" the less likely the fines are to be serious.
Note that just a one way industry -> regulator won't necessarily produce this effect, because in that situation a regulator can still want to flex by producing meaningful fines. But the more the cycle is industry -> regulator -> and back to industry, the more the regulator is going to be thinking in terms of what will come around when they're in the industry again.
Now, most probably nothing is out there waiting to get run over by a derelict Dish bird, but if there was...
2002 - Dish Network launches EchoStar-7 with a 10 year license from the FCC
2004 - FCC passes new Orbital Debris Mitigation rules, grandfathering existing satellites[1]
2012 - Dish Network applies for a license extension, which includes provisions according to the new rules
2020 - FCC updates debris mitigation rules[2]
2022 - Dish Network notices unexpected fuel loss, and begins moving satellite to graveyard orbit, but only makes it 122km instead of the required 300km.
2022 - FCC updates debris mitigation rules again[3]
I had remembered recent press releases about new debris mitigation rules and my first reaction when reading this story was surprise that the FCC was applying the new rules to a satellite launched over 20 years ago, but it appears that is not the case. Dish Network is being fined according to rules that were in place when they requested their license extensions, not the more recent rules.
[1] https://www.fcc.gov/document/mitigration-orbital-debris
[2] https://www.fcc.gov/document/fcc-updates-orbital-debris-miti...
[3] https://www.fcc.gov/document/fcc-adopts-new-5-year-rule-deor...
It almost seems like we need some ion drive cleanup tugs in orbit. Mayb they could reclaim reaction mass gradually from the solar wind.
Additionally to prevent a company from just going bankrupt they should be required to pay in advance a fee to a fund (ala FDIC) that will deal with issues that have to be dealt with. In this case it may be "ok" but what if this satellite was not out of the active geostationary zone and posed a risk to others important satellites?
Seems like a plan with a bad risk/reward ratio. Right now the satellite isn't where it's supposed to be, but neither is it directly in the way of other geostationary satellites. But if you send up another satellite to deliberately interface with this one and move both up, you risk something going wrong and either getting stuck with two satellites in that position, or worse, both crashing into each other and making a huge mess. It's probably better to wait until the technology for grappling satellites in space is mature. This is presently an active area of research and development (OSAM), so a bit of patience should pay off.
I suppose that in orbit, space has won out over tabs. :-)
(sorry I couldn't help myself)
Maybe read the first line of the parent comment more carefully?
> Not enough, they should be require to fix their mistake by sending out another Satellite to either retrieve it or push it out where it was INDENTED TO BE[emphasis mine].
the error wasn't the typo in `indented`. it was that a single newline ("CR") is like an html space in HN formatting. it doesn't start a new paragraph. GP notes that he only used a single "CR" and thus his own commentary ran together with his intended (also indented, in this case) quote.
Plus, retrieving it is almost guaranteed to be unrealistic. It's out near geostationary orbit. The only options are to have an MEV move it into normal geostationary orbit or dump it into a graveyard orbit.
"Too much! I get sending a message with a small initial fine like 150k plus requiring a compliance plan, but this high amount is a step too far. Prepayment is just the epitome of regulatory capture IMO. Even for selfish reasons a satellite company will strive to keep their satellites minimally functional and safe from any systemic dangers in orbit. But I guess Uncle Sam always has to get his cut."
Space libertarianism here we go!
The orbit it is in is perfectly between geostationary and the disposal orbit. That means any other satellite who is travelling from one orbit to the other can stop off on-route for no fuel or time cost.
'grabbing' a satellite is fairly easy too. Even a fridge magnet would be enough to grab this satellite - since even tiny forces over many hours are enough in space.
I therefore suspect that it would be possible to complete this disposal with a satellite already on orbit - ie. not specially designed for the purpose, and using very little additional fuel - perhaps some operational satellites even have enough extra in reserve.
Damage is unlikely - collision speeds would be measured in millimeters per second, and forces in millinewtons.
For position accuracy, it would probably require a camera onboard - but most satellites already have a star tracker that includes a capable camera.
The main risk is that the satellites touch at the 'wrong angle' or blocking an attitude control thruster. That would immobilize both of them.
> collision speeds would be measured in millimeters per second, and forces in millinewtons.
What satellite ending their end of life, and already in orbit do you suggest are capable of such delicate manoeuvring? This is a very delicate task you are describing, and most satellites are simply not designed for it.
> The main risk is that the satellites touch at the 'wrong angle' or blocking an attitude control thruster.
If someone tries this, the most likely outcome is that the satelites wizz by each other without ever touching. If you somehow manage to aim the "pushing" satellite accurately enough at the "stranded" satellite they would most likely collide at anything from a few hundred meter/s to a few of km/s depending on the orbital arrangements.
As a result I think you're misunderstanding what the orbital dynamics would be.
I do understand what geostationary orbit is.
The commenter I was responding to said "any other satellite who is travelling from one orbit to the other can stop off on-route for no fuel or time cost". If they wanted to only talk about geo sats they should have said that.
But sure, let's think about using a geo sat to fly this intercept. Let's just pick Echostar-8 as a concrete example. It is at 6.4 degree inclination while Echostart-7 is at 1.5 degree. So you will at best have a glancing blow between these two.
https://www.satnow.com/products/thrusters/space-electric-thr...
It has a thrust of ~20 milli Newtons.
Power that up for 10 seconds on a satellite weighing 500 kg, and you will move an extra 0.4 millimeters per second.
So how exactly is precise maneuvering hard?
For example, the satellite bus used by EchoStar-7, which is the satellite in question here (https://en.m.wikipedia.org/wiki/Lockheed_Martin_A2100) uses Hydrazine and NTO for primary propulsion, with hydrazine monoprop for atittude control, and the monoprop thrusters and ion thrusters for station keeping.
While the new version of that bus has the option for all-electric propulsion, it really isn't clear how popular that option has actually been. There aren't really many details about it.
Define "typical" because it's not being used on any geostationary satellites.
> Power that up for 10 seconds on a satellite weighing 500 kg
500kg? Hilarious. These satellites are the size of a bus and their weights are measured in tons.
> satellites already have a star tracker that includes a capable camera
Which is focused at infinity. Neither the hardware nor the software is capable of tracking a big object nearby and providing feedback to align itself how you're proposing, without significant changes.
Edit: just to give an idea of how difficult docking in space is in general, take a look at the International Docking System Standard (used on the ISS): https://www.internationaldockingstandard.com/
Table 3.3.1.1-2 tells you the conditions for docking; velocities of 50-100mm/s are expected. And look at how much hardware is needed to dampen the energy. It has 6 DoF actuators, hydraulic components, etc. etc. And that's for the ISS - all spacecraft going there are specifically designed to be able to accurately approach and dock with the ISS. There's just no way you can get that level of precision with a satellite bus designed for communications and station keeping.
For instance, if the satellite is dead or has lost propulsion, it will likely have started to spin and will have no way to stop that. Reaction wheels can only do so much and can get saturated, requiring other attitude control systems to be used to desaturate them first. Approaching it with an unspecialized satellite will then definitely generate smaller debris, which is far more problematic.
This also amplifies the risk you mention about ending up immobilized for other reasons. You'd have two pieces of junk literally on top of each other, it would take very little for them to damage each other and start producing much smaller debris.
Further, you can't just repurpose a star tracking camera to look at a satellite instead, they're dealing with completely different kinds of requirements, and it isn't even a given that you would have the processing capability on the tracker to handle the kind of computer vision needed. Nor is it likely that the tracking camera feed can be transmitted down to Earth for manual control.
The only cases we have of a satellite contacting another satellite when it wasn't initially designed with that in mind, involved dedicated extension vehicles designed and launched to dock to the engine nozzle of satellites which were still fully functional and without the extension would've still been able to move themselves into a graveyard orbit.
Just asking this tech focused community, but shouldn't the correct action be for a UN level entity charge an automatic de-orbiting fee.
Even thinking it as a bottle deposit return if the launching company succeeds in its de-orbit burnup for ongoing constellations.
Like, “we’re warning you!”
But it’s only notable as an action because they haven’t done any prior enforcement. Not because now, suddenly, they are signaling that they’re going to address the problem.
[0] https://en.wikipedia.org/wiki/Strategic_Defense_Initiative
In at least 1 case, they also issued fines to a US company that tried to use an international launch to circumvent US rules
Although of course since this is geostationary orbit, the point of putting it over a geographical area is to do business over that area down on Earth.
So, if it was a German company, but was doing business in the US, the US could use access to their market as leverage for a fine.
Geostationary satellites have antennae which are meant to optimize communications with ground stations in certain countries, but they can’t fly over the USA especially.
So if you're a non-US company operating services in the US, you'll have to have a US subsidiary anyway and that subsidiary would be required to get the license. If you're a non-US company not doing business in the US then that's outside of regulatory jurisdiction.
Incidents like this one are pretty uncommon, and as space debris goes, this is pretty benign in the sense that it's a large intact satellite and can thus be tracked fairly easily and precisely. Once the technology matures, a cleanup vehicle could even be sent to move it into graveyard orbit.
The kind of space debris that tends to be problematic is stuff that is too small to track, since then you're stuck relying either on pure luck or giving the area a wide berth to not have it hit something else.
We'll see. Starlink/Kuiper use a low enough orbit that non-functional satellites will de-orbit on their own in a reasonable timeframe. But OneWeb, which is up at 1000km+ already has had a satellite failure. And although they've vowed to remove it somehow, it's not obvious how they'll do so.
Edit: correction, oneweb doesn't specifically use the astroscale grappling fixture, instead it seems they use either their own design, or ones designed by Altius. Apparently these designs are such that they can be grappled either mechanically or magnetically, so presumably the difference is not significant enough to meaningfully limit which MEV can handle the job.
In higher orbits, particularly GEO (like the satellite in question), it's much more of a problem. Laser brooms might one day be used to deorbit small pieces of debris, but dead satellites beyond LEO will need to be grabbed and tugged/thrown into safer orbits.
Most things of significant mass are in stable orbits or they wouldn't be there for very long. Regional sats like the one from Dish are in GSO way away, so they don't really matter. The problem is that Dish didn't have a disposal plan for this satellite. It's mostly when operators create clouds of junk, especially fragments from unnecessary collisions that cross other orbits, that pose a threat to lives and property. It's good to require operators to have a deorbit or parking orbit plan.
The biggest threat is LEO-crossing MMOD, which is why crewed craft have hundreds of Whipple shielding configurations to choose from for a given application.
This isn't a problem in need of solving in such a deliberate, costly, and arbitrary manner. Instead, the solutions are holistic: don't create debris that poses a risk to LEO, have a decommissioning plan for GSO objects, and protect what needs protecting by defensive spacecraft design.
Edit: The Kosmos 2251/Iridium 33 collision was reckless operation by the Russians leaving space junk in LEO.
The issue with the Dish satellite is that it's close to geostationary orbit, which is a limited resource and where the atmospheric drag is low enough that they are essentially up there forever.
- DISH