Orbital Elements
Component A
Perturbed ephemeris below is based on elements from NK 1458.
Epoch (TT/JD) T (TT/JD) Peri. Node Incl.
2455360.50000 2455340.9918528 149.37029 246.08554 12.80247
e q a Epoch (TT)
0.7489014 0.7577860 3.01788 2010/06/13.00
Component D
The following orbital elements are taken from MPC 59599:
Epoch 2010 June 13.0 TT = JDT 2455360.5
T 2010 May 29.7100 TT MPC
q 0.757825 (2000.0) P Q
n 0.1877247 Peri. 149.3310 +0.8033730 -0.5599588
a 3.020799 Node 246.0850 +0.4914425 +0.8155824
e 0.749131 Incl. 12.8032 +0.3362679 +0.1458477
P 5.25
From 117 observations 1994-1999, mean residual 1".0. Nongravitational
parameters A1 = +2.19, A2 = +0.5808.
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