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Just to simply simulate a last-minute landing burn below 2 km altitude.

Thanks for the update. Speaking of the "1-3-1" engine sequence, could there be a way to implement that engine sequence as an optional choice for the landing burn?

In the 2022 scenario folder, what's supposed to be the Globalstar mission is actually a duplicate of the Nilesat 301 scenario.

Kyle, is there a March 2022 update available, or will that update be combined with April's by the end of this month?

Where's the download page for this addon?

There was this F9 scenario I created while OneWeb was launching atop Soyuz: A 5,991.2-kg payload, which simulates 36 OneWeb satellites (147.7 kilograms each) attached to a 674-kilogram dispenser. Launch site was out of Vandenberg going toward a 200 by 1,000 km parking orbit inclined -87.9...

I presume so.

Following the Starlink 4-12 launch, Elon posted this tweet regarding the total mass of the 53 Starlink v1.5 satellites. Not sure if this means each Starlink v1.5 sat is 306.6 each, since it's 16,250 kg divided by 53.

Where did you get the payload masses for NROL-108 and NROL-87? Are both 5,000 kg each?

49 Starlink satellites on this mission (Starlink Group 4-5); launch time is 21:49:10 UTC (4:49:10 PM EST). Also, I'm assuming the targeted orbit will be 210 by 340 kilometers inclined -53.2 degrees.

Could this mean that future Cargo and Crew Dragons will go southeast?

What would the initial launch inclination be before the dogleg?

https://www.google.com/maps/d/u/0/viewer?hl=en&mid=1x4aQQOdlKvWRN7007gVEm_yoTxnRYmLn&ll=32.21307141834425%2C-119.18678279384298&z=7 Here is the Launch Hazard Area map for the upcoming Starlink 4-4 mission from Vandenberg this week. Apogee: 341 km Perigee: 211 km Inclination: -53.22 degrees...

Why dogleg after fairing sep? I thought it was after Stage 1 sep.

https://www.spacex.com/launches/index.html The Starlink v1.0 P1 mission will launch 51 Starlink sats; total payload mass is 13.26 tons.

I saw on Gunter's Space Page's "Orbital Launches of 2021" that the website's author guessed 40 Starlink sats per polar mission. This adds up to a total mass of 10.4 tons compared to 15.6 tons (60 Starlink sats). Orbital Launches of 2021

For the first polar Starlink mission (Starlink v1.0 P1), the ASDS and FRV positions have been posted on the General SpaceX Map: Starlink v1.0 P1 Recovery Locations OCISLY Position: Lng.-117.849722 Lat.29.375556 FRV Position: Lng.-117.657826 Lat.28.985422 Don't really know what the initial...

Per ULA's PDF about Atlas V/Starliner, the total mass is 13,250 kilograms. Is there any way to change the total mass to that number on a config file?

Where is the 2020 update package in this thread? Is it in the first page with the description?

It doglegs after fairing sep per the new SAOCOM 1B addon BrianJ made.