Yesterday we tracked Tianwen-1 with one of the 6.1 metre dishes at Allen Telescope Array. Even at 188 million km distance the signal is strong enough to decode most of the frames. The spacecraft will arrive to Mars orbit on Wednesday at 12:00 UTC.
The last orbit state vector we received in that observation is:
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.
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).
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Today at 15:45 UTC @HopeMarsMission will be performing its Mars orbit insertion burn. Here are some technical details about this manoeuvre. Thread...
The spacecraft would arrive to periapsis with a velocity of 5.1 km/s, a C3 of 7.23 km^2/s^2, and an altitude of 1162 km. The inclination of the hyperbolic orbit is 20 degrees. Some media state a target capture orbit of 1000 km x 49380 km (altitude).
This orbit has a semi-major axis of 28580 km, and a C3 of -1.5 km^2/s^2. The required C3 delta of 8.7 km^2/s^2 can be supplied by an (impulse) delta v of 943 m/s. This is what such a capture orbit would look like seen from over Mars north pole.