Avherald has got hold of the preliminary report.
https://avherald.com/h?article=4f24b2d7&opt=0
The Commander stated that during cockpit preparation, she noticed that the altitude selector was set to 0000 feet and she selected it to 4,000 feet, which was also verified by the flight data recorder. The selection of 4,000 feet on the altitude selector was in accordance with the planned standard instrument departure (SID) of SENPA 2F1.
At 23:10:29 UTC, the Aircraft lifted off, and at 23:10:40 the landing gears were selected to ‘up’ position (retracted).
The Commander stated that after lift-off, and during climb, she followed the flight director command. However, the Aircraft rate of climb reached to a maximum of approximately 800 feet per minute. The flight crew were not able to adhere to published climb gradient of the SID due to the shallow climb.
At 23:11:01, the takeoff/go-around (TOGA) switch was selected and the flight mode annunciations (FMA) were changed to TOGA/TOGA. The flight directors indicated climb attitude on the Commander’s primary flight display (PFD). A flap 15 over-speed occurred as the airspeed increased towards 250 knots. The flight crew continued to their destination and landed uneventfully.