Table 2
Orbital elements: Semimajor axis (a), eccentricity (e), inclination (i), the argument of perihelion (Ω), ascending node (ω), time of perihelion passage (T0) obtained for this study (TS) compared with the nominal ones taken from NASA JPL Web-interface service (JPL) at time of reference tref

Asteroid tref(JD) Data Orbital elements
a (AU) e i (°) Ω (°) ω (°) T 0 (JD)
(1864) Daedalus 2458789.80310 TS 1.4639 0.6098 22.7320 7.2799 325.2213 2458603.39671
JPL 1.4610 0.6144 22.2092 6.6280 325.6275 2458604.12044
2003 GW 2458354.55596 TS 1.8647 0.4848 48.3890 183.4034 91.8637 2458254.98649
JPL 1.8207 0.4762 49.4358 183.2111 90.6109 2458253.92435
(4690) Strasbourg 2458188.03505 TS 1.9536 0.0862 17.1201 298.1088 115.1864 2458016.23371
JPL 1.9374 0.1089 16.9095 295.7938 105.4774 2457993.92200
2019 JA8 2458627.44160 TS 2.6154 0.5296 10.1768 74.7833 202.4851 2458580.45560
JPL 2.4197 0.4965 9.5019 79.2309 197.7623 2458673.81805
(1738) Oosterhoff 2458032.92310 TS 2.1628 0.1945 5.5060 37.9928 294.1069 2458019.14392
JPL 2.1835 0.2025 4.8774 44.1111 284.4315 2458011.86828
(2717) Tellervo 2458184.20493 TS 2.2555 0.2810 2.7606 162.0936 159.6214 2457782.89620
JPL 2.2146 0.2185 3.2854 164.8653 163.5006 2458627.03995
(1568) Aisleen 2457434.87988 TS 2.3667 0.2735 24.9534 144.2715 227.5491 2457182.98599
JPL 2.3517 0.2541 24.8966 146.2405 228.7325 2457187.56159
(2235) Vittore 2458675.39060 TS 3.2352 0.2160 18.0316 206.3595 269.6413 2457857.97201
JPL 3.2043 0.2149 18.7807 205.0291 274.4220 2459510.61840