(67) Asia
Orbital Elements
The following orbital elements are taken from MPC 26379:(67) Asia Epoch 2003 Dec. 27.0 TT = JDT 2453000.5 Goffin M 254.54781 (2000.0) P Q n 0.26148206 Peri. 106.21029 +0.62646027 +0.77839735 a 2.4220036 Node 202.72999 -0.74922481 +0.58699819 e 0.1844078 Incl. 6.02554 -0.21496446 +0.22255494 P 3.77 H 8.28 G 0.15 U 0 From 412 observations at 63 oppositions, 1861-1994, mean residual 1".00.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 2004 03 26 14 26.31 -13 56.0 1.544 2.441 146.8 12.9 11.9 2004 03 31 14 23.82 -13 29.3 1.501 2.431 152.5 10.9 11.8 2004 04 05 14 20.73 -12 58.7 1.463 2.421 158.3 8.8 11.6 2004 04 10 14 17.10 -12 24.8 1.431 2.411 164.2 6.5 11.5 2004 04 15 14 13.04 -11 48.1 1.406 2.401 170.2 4.1 11.3 2004 04 20 14 08.67 -11 09.5 1.387 2.390 176.0 1.7 11.1 2004 04 25 14 04.14 -10 29.8 1.375 2.380 176.8 1.4 11.0 2004 04 30 13 59.61 -09 50.2 1.369 2.370 171.1 3.8 11.2 2004 05 05 13 55.23 -09 11.8 1.370 2.359 165.0 6.3 11.3 2004 05 10 13 51.15 -08 35.5 1.378 2.349 159.1 8.8 11.4 2004 05 15 13 47.48 -08 02.4 1.391 2.339 153.2 11.2 11.5 2004 05 20 13 44.35 -07 33.1 1.410 2.328 147.5 13.5 11.6 2004 05 25 13 41.83 -07 08.3 1.434 2.318 142.0 15.6 11.7 2004 05 30 13 39.99 -06 48.6 1.463 2.307 136.7 17.5 11.8 2004 06 04 13 38.87 -06 33.9 1.495 2.297 131.5 19.3 11.9
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