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Table A.1

Orbital elements and physical properties for the sample of 20 observed asteroids collected at epoch 61200 mjd.

Asteroid a [au] e i [°] Ω [°] ω [°] H [mag] albedo d [km] m [kg] MOID [au] MMOID [rad]
4179 Toutatis 2.54 0.62 0.45 125.37 277.86 15.30 0.254 2.64 2.12 × 1013 4.10 × 10−4 (6.19, 2.74)
69230 Hermes 1.66 0.62 6.07 34.03 92.93 17.57 0.265 0.82 6.35 × 1011 1.45 × 10−4 (0.40, 2.07)*
2002 PZ39 1.47 0.55 1.67 328.72 260.19 19.10 1.79 × 1011 9.89 × 10−5 (0.51, 3.83)*
2013 FA8 1.93 0.67 3.12 165.42 281.06 20.93 1.43 × 1010 2.28 × 10−5 (0.30, 5.50)
1997 BR 1.34 0.31 17.25 116.63 133.86 17.80 0.51 0.56 2.02 × 1011 1.31 × 10−4 (0.42, 5.56)**
2007 UY1 0.95 0.18 1.02 337.45 274.12 23.08 7.28 × 108 7.64 × 10−6 (4.60, 0.68)*
2003 QQ47 1.09 0.19 62.10 0.98 104.97 17.37 1.96 × 1012 4.38 × 10−4 (0.96, 1.46)*
1999 MN 0.67 0.67 2.03 81.38 9.21 20.57 2.35 × 1010 6.29 × 10−5 (1.90, 0.57)
2003 YK118 1.70 0.49 7.83 326.73 233.28 18.81 0.07 0.90 8.40 × 1011 3.44 × 10−4 (5.97, 5.05)
2011 BO24 1.38 0.28 20.37 91.46 178.67 18.78 2.78 × 1011 2.42 × 10−4 (0.01, 5.14)**
2003 AC23 2.17 0.58 2.06 43.73 126.41 21.90 3.72 × 109 3.97 × 10−5 (0.16, 6.17)
2020 FR1 1.41 0.61 13.11 26.37 255.89 21.20 9.86 × 109 8.58 × 10−5 (0.54, 2.92)
2018 DA1 1.21 0.73 25.49 139.90 233.94 18.85 2.52 × 1011 3.37 × 10−4 (0.62, 4.95)
2016 CU193 1.47 0.36 49.89 322.37 323.12 19.94 5.59 × 1010 1.73 × 10−4 (0.29, 1.83)
2014 UC192 1.41 0.36 11.66 34.92 304.61 23.72 3.03 × 108 1.78 × 10−5 (0.44, 3.06)
2005 TU50 1.43 0.60 12.42 22.18 259.71 21.45 6.92 × 109 1.14 × 10−4 (0.53, 2.84)
2006 BC10 2.02 0.66 0.91 20.25 235.24 19.50 1.03 × 1011 7.24 × 10−4 (6.01, 5.62)
2024 QP2 2.54 0.62 1.64 205.32 202.15 21.57 5.83 × 109 1.78 × 10−4 (6.20, 4.98)*
2015 DU180 1.93 0.92 4.86 51.74 315.41 21.03 0.28 0.39 6.83 × 1010 1.08 × 10−3 (6.05, 0.17)
2014 WK7 1.56 0.36 23.91 233.74 180.93 22.17 2.59 × 109 1.68 × 10−4 (6.27, 1.32)**

Notes. The mass was computed using Eq. 2 either using the values of observed properties or assuming the intermediate values. MMOID indicates the mean anomalies needed for the asteroid and spacecraft 2 (* for spacecraft 1, ** for spacecraft 3) to be in a close approach configuration at the MOID, respectively.

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