(111) Ate
Orbital Elements
The following orbital elements are taken from MPO 4876(111) Ate Epoch 2002 May 6.0 TT = JDT 2452400.5 Goffin M 44.69538 (2000.0) P Q n 0.23590789 Peri. 165.65578 -0.36832822 -0.92709224 a 2.5940265 Node 305.91112 +0.84429606 -0.30224727 e 0.1017242 Incl. 4.92468 +0.38922805 -0.22169023 P 4.18 H 8.02 G 0.15 U 0 From 405 observations at 52 oppositions, 1870-2000, mean residual 0".55.An explanation of the orbital elements is available.
These orbital elements are also available in forms suitable for loading into a number of popular planetarium-type software programs.
Ephemeris
The following ephemeris is at intervals of five days. A daily ephemeris covering the same time interval is also available.
Date TT R. A. (2000) Decl. Delta r Elong. Phase V 2001 12 22 10 01.55 +11 54.3 1.664 2.338 121.9 20.9 12.0 2001 12 27 10 01.96 +11 40.3 1.614 2.340 126.8 19.7 11.9 2002 01 06 10 00.47 +11 22.7 1.524 2.343 137.2 16.6 11.7 2002 01 11 09 58.57 +11 19.3 1.486 2.345 142.7 14.7 11.6 2002 01 16 09 55.93 +11 19.3 1.452 2.347 148.4 12.7 11.4 2002 01 21 09 52.60 +11 22.6 1.424 2.350 154.3 10.5 11.3 2002 01 26 09 48.69 +11 28.7 1.401 2.352 160.3 8.1 11.2 2002 01 31 09 44.30 +11 37.2 1.385 2.354 166.4 5.7 11.0 2002 02 05 09 39.58 +11 47.4 1.376 2.357 172.4 3.2 10.9 2002 02 10 09 34.66 +11 58.8 1.373 2.360 177.5 1.1 10.7 2002 02 15 09 29.74 +12 10.6 1.378 2.362 174.2 2.4 10.9 2002 02 20 09 24.99 +12 22.2 1.389 2.365 168.2 4.9 11.0 2002 02 25 09 20.57 +12 33.0 1.406 2.368 162.2 7.3 11.2 2002 03 02 09 16.63 +12 42.3 1.430 2.371 156.3 9.7 11.3 2002 03 07 09 13.26 +12 49.9 1.460 2.375 150.5 11.9 11.4 2002 03 12 09 10.57 +12 55.5 1.496 2.378 144.8 13.9 11.6 2002 03 17 09 08.60 +12 58.8 1.536 2.382 139.4 15.8 11.7 2002 03 22 09 07.40 +12 59.6 1.581 2.385 134.1 17.4 11.8 2002 03 27 09 06.96 +12 57.9 1.630 2.389 129.1 18.9 11.9
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