The last orbit state vector we received in that observation is: 2021-02-07 23:23:03.744100 18791639.655712113 211029173.8782428 96492674.05965108 -21.108400067542537 4.768376820024702 1.8445381918644286
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According to that state vector, the periapsis altitude is now 386 km, with passage at 11:59:52 UTC. The MOI burn will start several minutes before this, and probably lower the periapsis slightly.pic.twitter.com/A5jvUKhvGL
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This shows in yellow the period in which the 3kN engine will be burning, and the spacecraft returning to a slightly lower periapsis some 11 days later (this is just a prediction based on some papers describing the orbit planning).pic.twitter.com/i9s4e833Fe
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Where can we get the TLE data and the transmission schedule?
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The spacecraft transmits constantly and TLEs can only be used for Earth-orbiting satellites. You can head over to https://ssd.jpl.nasa.gov/horizons.cgi to compute ephemerides for your location.
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