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Updated on July 31, 2010 |
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Orbital ElementsComponent C Epoch 2001 Jan. 11.0 TT = JDT 2451920.5 T 2001 Jan. 27.71491 TT Muraoka q 0.9373554 (2000.0) P Q n 0.18400239 Peri. 198.77573 -0.02869243 +0.98217944 a 3.0614023 Node 69.92228 -0.88992362 +0.05952112 e 0.6938150 Incl. 11.40605 -0.45520621 -0.17827165 P 5.36 From 226 observations 1994 Dec. 28-2000 Dec. 1, mean residual 0".83. Nongravitational parameters A1 = +0.65 +/- 0.08, A2 = -0.0681 +/- 0.0295. Component B Perturbed ephemeris below is based on elements from NK 934. Epoch (TT/JD) T (TT/JD) Peri. Node Incl. 2451920.50000 2451937.4861394 198.77742 69.91831 11.40594 e q a Epoch (TT) 0.6938423 0.9374028 3.06183 2001/01/11.00 Component E Perturbed ephemeris below is based on elements from NK 934. Epoch (TT/JD) T (TT/JD) Peri. Node Incl. 2451920.50000 2451937.9538056 198.77119 69.91932 11.40649 e q a Epoch (TT) 0.6938782 0.9374405 3.06231 2001/01/11.00
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Finding Charts
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Magnitudes GraphComponent C: m1 = 7.5 + 5 log d + 18.0 log r Component B: m1 = 12.5 + 5 log d + 18.0 log r Component E: m1 = 17 + 5 log d + 190 log r(t + 60)
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The orbital elements of component C are calculated by Kenji Muraoka.
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