Orbital Elements
Epoch 1976 mar. 3.0 TT = JDT 0000000 T 0000 XXX 0.00000 TT q 0,196626 (2000.0) P Q z +0.0002325 Peri. 358.427 -0.00000000 -0.00000000 +/-0.0000002 Node 118.924 -0.00000000 -0.00000000 e 0.999971 Incl. 43.0664 +0.00000000 -0.00000000
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