Turksat-5A with stage2 as two cataloged objects with initial orbital parameters:
2021-001A - TBA - TO BE ASSIGNED - 2021-01-08 05:47 UTC - 286.17/55031.12km/17.66°
2021-001B - TBA - TO BE ASSIGNED - 2021-01-08 05:52 UTC - 285.5/55277.64km/17.66°
This is an interesting compromise. F9 could give this payload any apogee they want (the NASA LSP web calculator, which is known to be pretty conservative, shows F9 can put 3300 kg to Earth escape). And in theory a really high apogee is even better - you go super high where the plane change costs almost nothing, then back down into geosync. This gives about 1275 m/s total, rather than the 1540 m/s or so here.
But a super high apogee can cause problems. Minor perturbations by the moon, etc., can lower the perigee and cause accidental re-entry if you can't raise the perigee quickly enough (this has happened). Also geo-sync satellites may not be designed for deep space operation - Earth sensors, communication, and so on is all designed for geosync. And super high orbits take a lot of patience - a single orbit can take weeks.
So it looks like they picked the greatest apogee they were comfortable with, then spend the rest of the delta-V on inclination reduction.
PS: The satellite that had problems with a very high apogee (120,000 km) was Superbird 6. A discussion of how this might have happened is on
this non-NSF forum.
SoaceX photos by Ben Cooper
To be clear, that tweet means it's the first attempt to catch a fairing this year. There wasn't any news on whether it was successful.
Yes, it was posted before the launch. Mostly to show that only one catch attempt was going to be made. Thanks for clarifying.
Elizabeth S, Christine S, Hawk and another pilot boat outbound. Finn Falgout continues to make slow progress toward port entrance.
B1060.4 and its entourage now entering port channel. Should be visible on Fleetcam shortly.