Telstar 19V is, I believe, the most massive payload to reach geotransfer orbit. It is an SSL-1300 model built by SSL/MAXAR (Palo Alto)
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Quite a bit - I estimate that would be 13000 km apogee or so. Subsync makes sense, with part of the enormous payload mass being extra prop for orbit raising. But we'll see soon enough
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Is the apogee around 13000 km or 18000 km? Since I saw that someone posted here showing a 17863 km apogee: https://www.reddit.com/r/spacex/wiki/launches/gto_performance … Which one correct? Thanks.
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