P[h] | R km | corotation km | release h km | r0/rc | flight min | impact km/s | angle deg
10.00 | 3,390 | 11,203 | 3,960 | 0.66 | 58 | 3.51 | 51
15.00 | 3,390 | 14,680 | 5,135 | 0.58 | 70 | 3.79 | 56
20.00 | 3,390 | 17,783 | 6,100 | 0.53 | 82 | 3.96 | 59
24.62 | 3,390 | 20,426 | 6,875 | 0.50 | 92 | 4.06 | 61
30.37 | 3,390 | 23,494 | 7,735 | 0.47 | 103 | 4.15 | 63
40.00 | 3,390 | 28,230 | 9,000 | 0.44 | 121 | 4.25 | 65
10.00 | 3,593 | 11,203 | 3,860 | 0.67 | 58 | 3.32 | 51
15.00 | 3,593 | 14,680 | 5,025 | 0.59 | 71 | 3.62 | 57
20.00 | 3,593 | 17,783 | 5,980 | 0.54 | 82 | 3.78 | 60
24.62 | 3,593 | 20,426 | 6,745 | 0.51 | 92 | 3.88 | 61
30.37 | 3,593 | 23,494 | 7,600 | 0.48 | 104 | 3.98 | 63
40.00 | 3,593 | 28,230 | 8,850 | 0.44 | 122 | 4.08 | 65
