Even with a feathered solar panel, drag at 440 km altitude is significantly higher than at the operational altitude.
I would like to show some graphs by Hugo, a member of the german forum raumfahrer.net. I asked for his consent to show them here.Link to the threadhttps://www.raumfahrer.net/forum/smf/index.php?topic=13231.msg456752#msg456752
It's one plane. Some satellites had problems. A couple may have been chosen in advance for deorbit testing.
https://twitter.com/planet4589/status/1162605103142113280Quote No change in Starlink satellite orbital heights for last week or so. Object AV [44] still in low 312 x 348 km orbit (and reported by Jay Respler to be 2nd magnitude)
No change in Starlink satellite orbital heights for last week or so. Object AV [44] still in low 312 x 348 km orbit (and reported by Jay Respler to be 2nd magnitude)
I was going to say, the middle portion That are stuck around 430km are waiting for something. A test or plane change. I really don't know. I hope we get an update on them during the next launch
Quote from: intelati on 08/18/2019 02:37 amI was going to say, the middle portion That are stuck around 430km are waiting for something. A test or plane change. I really don't know. I hope we get an update on them during the next launchThose are the ones that failed early.
A summary of visual brightness observations of individual Starlink satellites reported on Seesat-L (http://satobs.org) in July-August. Blue: operational sats. Red: non-op sats in lower orbits. Green: debris. Vertical bars: sats with no brightness estimates.Thanks to observers Jay Respler, Brad Young, @cgBassa, Bram Dorreman, and Ron Lee for their data.I have provided as-observed magnitudes rather than deriving so-called 'standard mag' needed for future predictions - I wanted to show what people are typically seeing in actuality.Note that almost all the individual satellites have been observed at least once. Range from mag 4 to 7 seems typical. This should be representative of the operational constellation modulo any design changes to reduce albedo.For comparison here are the current apogees (upward pointing triangles) and perigees (downward) for each satellite in the same colour scheme (blue operational, red not, green debris)Trivial correction to last plot (44249 is non-operational)
5 months in and 5 satellites deorbiting - already a near disaster. 2400 planned deorbits per year will be impossible to manage. Will there be any regulation / safety standards inquiry...or will the @fcc wait until an actual collision?https://twitter.com/greg_wyler/status/1168988584818425857
5 months in and 5 satellites deorbiting - already a near disaster. 2400 planned deorbits per year will be impossible to manage. Will there be any regulation / safety standards inquiry...or will the @fcc wait until an actual collision?
I probably don't need to say this but just in case: At least 3 SpaceX satellites are being deorbited intentionally as proof of concept. If there are 2 more, they may be defective but that ratio of bad sats can't be extrapolated to an entire constellation because this was only V0.9 and because SpaceX was testing a number of configurations. These are not the final form of Starlink sats. I even read one headline saying that the ESA had dodged a constellation of SpaceX sats. Clearly this has some political motivation aimed at people who are not familiar with what happened. ESA maneuvered because they were coming close to 1 (one) SpaceX sat. It is irrelevant that this sat was launched as part of a constellation because ESA was not near any of the other sats in the constellation. They were only near the one in the lowest orbit. None of the others ever come near the ESA sat.