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C/2004 R2 (ASAS)
Orbital Elements
The following orbital elements are taken from MPEC 2004-R48:
C/2004 R2 (ASAS)
T 2004 Oct. 7.931 TT MPC
q 0.11376 (2000.0) P Q
Peri. 5.228 -0.993248 +0.109860
Node 182.395 -0.108282 -0.762686
e 1.0 Incl. 63.109 +0.041628 +0.637370
From 24 observations 2004 Sept. 1-9.
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 m1 m2
2004 09 02 06 38.81 -19 03.6 0.991 1.096 66.4 57.6 11.9
2004 09 07 07 19.19 -20 50.6 0.917 0.983 61.2 63.9 11.2
2004 09 12 08 06.60 -22 07.7 0.866 0.865 54.4 71.1 10.6
2004 09 17 08 59.71 -22 25.9 0.844 0.739 46.1 78.5 9.8
2004 09 22 09 55.33 -21 20.5 0.856 0.603 36.8 85.0 9.0
2004 10 22 15 44.09 +05 02.6 0.903 0.550 33.2 82.7 8.7
2004 10 27 16 39.62 +05 29.3 0.907 0.689 42.2 75.6 9.7
2004 11 01 17 29.97 +05 21.1 0.951 0.818 49.8 67.7 10.5
2004 11 06 18 13.41 +04 54.9 1.026 0.940 55.5 60.4 11.3
2004 11 11 18 49.88 +04 23.1 1.123 1.054 59.4 54.0 12.0
2004 11 16 19 20.24 +03 52.8 1.237 1.164 61.9 48.5 12.6
2004 11 21 19 45.65 +03 27.4 1.361 1.269 63.1 44.0 13.2
2004 11 26 20 07.17 +03 07.7 1.493 1.370 63.3 40.0 13.7
