function atv_elements()
{
/*
1 AAAAAU 00  0  0 BBBBB.BBBBBBBB  .CCCCCCCC  00000-0  00000-0 0  DDDZ
2 AAAAA EEE.EEEE FFF.FFFF GGGGGGG HHH.HHHH III.IIII JJ.JJJJJJJJKKKKKZ

KEY: A-CATALOGNUM B-EPOCHTIME C-DECAY D-ELSETNUM E-INCLINATION F-RAAN
G-ECCENTRICITY H-ARGPERIGEE I-MNANOM J-MNMOTION K-ORBITNUM Z-CHECKSUM
*/

var tle1 = "1 32686U 08008A   08099.82951447  .00034699  00000-0  21012-3 0  2708";
var tle2 = "2 32686  51.6422  13.9162 0000814  11.6347  87.2278 15.77226090537580";

atv_status = "orbit"; /* atv_status = "ground" */

SAT = "ATV";
YE = parseFloat("20" + tle1.substring(18,20));
TE = parseFloat(tle1.substring(20,32));
INC = parseFloat(tle2.substring(8,16));
RA = parseFloat(tle2.substring(17,25));
EC = parseFloat("0." + tle2.substring(26,33));
WP = parseFloat(tle2.substring(34,42));
MA = parseFloat(tle2.substring(43,51));
MM = parseFloat(tle2.substring(52,63));
M2 = parseFloat("0" + tle1.substring(34,43));
RV = parseFloat(tle2.substring(63,68));
}