CelesTrak has a TLE for 1 object from the launch (2021-126) of TURKSAT 5B atop a Falcon 9 rocket from Cape Canaveral on Dec 19 at 0358 UTC
Two Falcon 9 launches completed in ~15 hours
At 10:58 PM ET last night, Türksat 5B lifts off into the night sky.📷: Me for @SuperclusterHQ @elonmusk
Last night SpaceX launched Türksat 5B. Check out these remote camera shots from Space Explored photographers @baserunner0723 and @derekiswise.
Watching the landing on the broadcast, I noticed the displayed stage 1 velocity was still 263 kph when the altitude reach 0.0 km, and was still 183 kph when the altitude flipped from 0.0 km to -0.0 km, which presumable meant effectively 0 m. Since the video had cut out (as usual) I found this telemetry disconcerting. Fortunately, a few seconds later we got confirmation of a safe landing so clearly the broadcast telemetry was inaccurate (maybe just out of synch). I haven't watched every landing, but it always seemed like the displayed telemetry converged nicely to 0 velocity and altitude at the same time in the past. Was this landing unique or have we seen misleading telemetry in the broadcast previously? Any idea why the two data streams would be so far out of synch?
https://twitter.com/TSKelso/status/1472737958050484227QuoteCelesTrak has a TLE for 1 object from the launch (2021-126) of TURKSAT 5B atop a Falcon 9 rocket from Cape Canaveral on Dec 19 at 0358 UTC198 x 68,931km, 27.12 degrees
Quote from: gongora on 12/20/2021 12:27 amhttps://twitter.com/TSKelso/status/1472737958050484227QuoteCelesTrak has a TLE for 1 object from the launch (2021-126) of TURKSAT 5B atop a Falcon 9 rocket from Cape Canaveral on Dec 19 at 0358 UTC198 x 68,931km, 27.12 degreesWith the listed orbital parameters, the delta-v to get to GEO is around 1,611 m/s.https://gtocalc.github.io/
Super-sync transfer.First maneuver:Perigee changed to 35786kmInclination changed to 1.4563 degreesCurrent Orbit: 35786.0000 km x 68931.0000 km x 1.4563 degrees;Apogee Speed: 1949.2716 m/s; Perigee Speed: 3481.8429 m/s; delta v to this orbit: 1187.6282Second maneuver:Apogee changed to 35786kmInclination changed to 0 degreesCurrent Orbit: 35786.0000 km x 35786.0000 km x 0.0000 degrees;Apogee Speed: 3074.9218 m/s; Perigee Speed: 3074.9218 m/s; delta v to this orbit: 1602.9613Total delta v to GEO: 1602.9613 m/s