[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 6th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
256/03:28:22
700 1
2 1
3 1
3
N/A 0
4 -0
1 228
0
000/00:02:45
399 -0
1 0
0 219
9
Coasting Arc #1 (Orbit 732)
---------------------------------------
Vector Time (GMT): 2013/249/13:59:55
052
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4439398
87 A = 6797156
88 meter
Y = 4395950
42 meter E =
0008331
Z = -2674415
38 I = 51
97871
XDOT = -2024
973027 Wp = 47
92704
YDOT = 5216
833605 meter/sec RA = 64
27262 deg
ZDOT = 5229
432183 TA = 282
10328
MA = 282
19662
Ha = 227
847 n
mi
Hp = 219
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14564956
93 X = 4402903
98
Y = 14422409
52 feet Y = 4445390
21 meter
Z = -8774328
67 Z = -2652938
45
XDOT = -6643
612294 XDOT = -2108
561375
YDOT = 17115
595818 feet/sec YDOT = 5193
722353 meter/sec
ZDOT = 17156
929733 ZDOT = 5219
391404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17851164
02 X = -5441034
79
Y = -10150994
17 feet Y = -3094023
02 meter
Z = -8684812
65 Z = -2647130
90
XDOT = 1354
090861 XDOT = 412
726894
YDOT = -16978
442682 feet/sec YDOT = -5175
029329 meter/sec
ZDOT = 17114
049075 ZDOT = 5216
362158
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13249
58861251
00016717 00000-0 10270-3 0 9002
2 25544 51
6463 64
9654 0003404 39
4714 320
6684 15
50424180 7332
Satellite: ISS
Catalog Number: 25544
Epoch time: 13249
58861251 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 64
9654 deg
Eccentricity:
0003404
Arg of perigee: 39
4714 deg
Mean anomaly: 320
6684 deg
Mean motion: 15
50424180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 733
Checksum: 298
Coasting Arc #2 (Orbit 748)
---------------------------------------
Vector Time (GMT): 2013/250/13:59:55
052
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4645210
96 A = 6798086
65 meter
Y = -4431003
67 meter E =
0015498
Z = 2219600
04 I = 51
96719
XDOT = 2067
300059 Wp = 97
27431
YDOT = -4932
279927 meter/sec RA = 59
33904 deg
ZDOT = -5489
001192 TA = 58
21494
MA = 58
06408
Ha = 227
849 n
mi
Hp = 219
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15240193
45 X = -4606099
49
Y = -14537413
62 feet Y = -4482730
41 meter
Z = 7282152
37 Z = 2197129
57
XDOT = 6782
480509 XDOT = 2148
964336
YDOT = -16182
020758 feet/sec YDOT = -4908
706123 meter/sec
ZDOT = -18008
534093 ZDOT = -5478
759474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18695060
17 X = 5698254
34
Y = 9769856
59 feet Y = 2977852
29 meter
Z = 7188481
17 Z = 2191049
06
XDOT = -1462
585196 XDOT = -445
795968
YDOT = 16092
415590 feet/sec YDOT = 4904
968272 meter/sec
ZDOT = -17964
844960 ZDOT = -5475
684744
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13250
61990120
00016717 00000-0 10270-3 0 9017
2 25544 51
6459 59
8523 0003386 42
2571 317
8840 15
50427312 7496
Satellite: ISS
Catalog Number: 25544
Epoch time: 13250
61990120 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 59
8523 deg
Eccentricity:
0003386
Arg of perigee: 42
2571 deg
Mean anomaly: 317
8840 deg
Mean motion: 15
50427312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 749
Checksum: 297
Coasting Arc #3 (Orbit 763)
---------------------------------------
Vector Time (GMT): 2013/251/13:59:55
052
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4864869
39 A = 6798736
29 meter
Y = 4394680
66 meter E =
0010948
Z = -1786495
18 I = 51
95484
XDOT = -2135
529539 Wp = 40
23122
YDOT = 4665
514095 meter/sec RA = 54
40579 deg
ZDOT = 5689
109681 TA = 300
26626
MA = 300
37456
Ha = 227
886 n
mi
Hp = 219
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15960857
59 X = 4824043
88
Y = 14418243
63 feet Y = 4448854
25 meter
Z = -5861204
67 Z = -1762961
66
XDOT = -7006
330510 XDOT = -2215
177879
YDOT = 15306
804774 feet/sec YDOT = 4641
188548 meter/sec
ZDOT = 18665
058009 ZDOT = 5678
541448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19506502
31 X = -5945581
90
Y = -9125335
55 feet Y = -2781402
28 meter
Z = -5763077
59 Z = -1756586
05
XDOT = 1682
263537 XDOT = 512
753926
YDOT = -15297
435411 feet/sec YDOT = -4662
658313 meter/sec
ZDOT = 18620
030743 ZDOT = 5675
385370
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13251
58672514
00016717 00000-0 10270-3 0 9029
2 25544 51
6476 55
0600 0003474 45
0166 315
1266 15
50449986 7649
Satellite: ISS
Catalog Number: 25544
Epoch time: 13251
58672514 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 55
0600 deg
Eccentricity:
0003474
Arg of perigee: 45
0166 deg
Mean anomaly: 315
1266 deg
Mean motion: 15
50449986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 764
Checksum: 302
Coasting Arc #4 (Orbit 779)
---------------------------------------
Vector Time (GMT): 2013/252/13:59:55
052
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5051219
36 A = 6799339
67 meter
Y = -4357141
87 meter E =
0015087
Z = 1287286
80 I = 51
93823
XDOT = 2279
647630 Wp = 108
25250
YDOT = -4387
579522 meter/sec RA = 49
47163 deg
ZDOT = -5854
080364 TA = 57
82238
MA = 57
67613
Ha = 227
851 n
mi
Hp = 219
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16572241
99 X = -5008374
75
Y = -14295084
88 feet Y = -4413388
13 meter
Z = 4223381
90 Z = 1262852
78
XDOT = 7479
158891 XDOT = 2356
978784
YDOT = -14394
945937 feet/sec YDOT = -4361
655242 meter/sec
ZDOT = -19206
300408 ZDOT = -5842
817715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20194644
36 X = 6155327
60
Y = 8486185
51 feet Y = 2586589
34 meter
Z = 4121481
03 Z = 1256227
42
XDOT = -2174
843191 XDOT = -662
892205
YDOT = 14564
392821 feet/sec YDOT = 4439
226932 meter/sec
ZDOT = -19158
392914 ZDOT = -5839
478160
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13252
61799452
00016717 00000-0 10270-3 0 9036
2 25544 51
6475 49
9473 0003445 48
1531 311
9911 15
50463562 7801
Satellite: ISS
Catalog Number: 25544
Epoch time: 13252
61799452 = yrday
fracday
Element set: 903
Inclination: 51
6475 deg
RA of node: 49
9473 deg
Eccentricity:
0003445
Arg of perigee: 48
1531 deg
Mean anomaly: 311
9911 deg
Mean motion: 15
50463562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 780
Checksum: 311
Coasting Arc #5 (Orbit 794)
---------------------------------------
Vector Time (GMT): 2013/253/13:59:55
052
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5235771
73 A = 6799704
49 meter
Y = 4250923
37 meter E =
0013825
Z = -819559
08 I = 51
92020
XDOT = -2444
918812 Wp = 42
11462
YDOT = 4147
616682 meter/sec RA = 44
53688 deg
ZDOT = 5961
738106 TA = 309
06986
MA = 309
19278
Ha = 227
917 n
mi
Hp = 219
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17177728
78 X = 5191829
06
Y = 13946598
98 feet Y = 4309227
33 meter
Z = -2688842
11 Z = -794231
08
XDOT = -8021
387179 XDOT = -2520
077357
YDOT = 13607
666280 feet/sec YDOT = 4119
856286 meter/sec
ZDOT = 19559
508223 ZDOT = 5949
677948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20788344
41 X = -6336287
38
Y = -7614706
82 feet Y = -2320962
64 meter
Z = -2583183
66 Z = -787354
38
XDOT = 2732
469861 XDOT = 832
856813
YDOT = -13998
703649 feet/sec YDOT = -4266
804872 meter/sec
ZDOT = 19508
282969 ZDOT = 5946
124649
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13253
58480024
00016717 00000-0 10270-3 0 9046
2 25544 51
6488 45
1551 0003572 50
1250 310
0214 15
50475635 7958
Satellite: ISS
Catalog Number: 25544
Epoch time: 13253
58480024 = yrday
fracday
Element set: 904
Inclination: 51
6488 deg
RA of node: 45
1551 deg
Eccentricity:
0003572
Arg of perigee: 50
1250 deg
Mean anomaly: 310
0214 deg
Mean motion: 15
50475635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 795
Checksum: 278
Coasting Arc #6 (Orbit 810)
---------------------------------------
Vector Time (GMT): 2013/254/13:59:55
052
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5373488
21 A = 6799871
97 meter
Y = -4149133
28 meter E =
0013704
Z = 291203
07 I = 51
89834
XDOT = 2680
445653 Wp = 117
03769
YDOT = -3908
753399 meter/sec RA = 39
60099 deg
ZDOT = -6019
687721 TA = 59
84052
MA = 59
70482
Ha = 227
855 n
mi
Hp = 219
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17629554
51 X = -5328106
92
Y = -13612642
00 feet Y = -4208969
28 meter
Z = 955390
64 Z = 265209
51
XDOT = 8794
113036 XDOT = 2753
197133
YDOT = -12823
994091 feet/sec YDOT = -3878
372552 meter/sec
ZDOT = -19749
631629 ZDOT = -6006
489339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21217227
78 X = 6467011
03
Y = 6791902
37 feet Y = 2070171
84 meter
Z = 846931
72 Z = 258144
79
XDOT = -3519
653446 XDOT = -1072
790370
YDOT = 13548
487770 feet/sec YDOT = 4129
579072 meter/sec
ZDOT = -19693
659746 ZDOT = -6002
627491
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13254
61604978
00016717 00000-0 10270-3 0 9058
2 25544 51
6488 40
0428 0003526 53
7875 306
3601 15
50498716 8118
Satellite: ISS
Catalog Number: 25544
Epoch time: 13254
61604978 = yrday
fracday
Element set: 905
Inclination: 51
6488 deg
RA of node: 40
0428 deg
Eccentricity:
0003526
Arg of perigee: 53
7875 deg
Mean anomaly: 306
3601 deg
Mean motion: 15
50498716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 811
Checksum: 310
Coasting Arc #7 (Orbit 826)
---------------------------------------
Vector Time (GMT): 2013/255/13:59:55
052
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5495591
66 A = 6799861
02 meter
Y = 3987023
77 meter E =
0016154
Z = 195881
61 I = 51
87484
XDOT = -2928
001211 Wp = 49
15234
YDOT = 3724
425173 meter/sec RA = 34
66328 deg
ZDOT = 6025
258981 TA = 312
94855
MA = 313
08393
Ha = 227
934 n
mi
Hp = 219
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18030156
37 X = 5449647
90
Y = 13080786
64 feet Y = 4048222
09 meter
Z = 642656
20 Z = 222466
94
XDOT = -9606
303187 XDOT = -2998
700062
YDOT = 12219
242694 feet/sec YDOT = 3691
287414 meter/sec
ZDOT = 19767
910044 ZDOT = 6010
863076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21506198
47 X = -6555089
29
Y = -5789819
75 feet Y = -1764737
06 meter
Z = 753617
44 Z = 229702
60
XDOT = 4307
051061 XDOT = 1312
789163
YDOT = -13319
055796 feet/sec YDOT = -4059
648207 meter/sec
ZDOT = 19706
936007 ZDOT = 6006
674095
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13255
64728914
00016717 00000-0 10270-3 0 9060
2 25544 51
6495 34
9306 0003679 55
7803 304
3696 15
50505946 8278
Satellite: ISS
Catalog Number: 25544
Epoch time: 13255
64728914 = yrday
fracday
Element set: 906
Inclination: 51
6495 deg
RA of node: 34
9306 deg
Eccentricity:
0003679
Arg of perigee: 55
7803 deg
Mean anomaly: 304
3696 deg
Mean motion: 15
50505946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 827
Checksum: 332
Coasting Arc #8 (Orbit 834)
---------------------------------------
Vector Time (GMT): 2013/256/03:29:45
399
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1547960
53 A = 6788648
93 meter
Y = -3955140
22 meter E =
0017138
Z = -5310717
02 I = 51
82116
XDOT = 6737
094854 Wp = 77
63716
YDOT = 3557
961993 meter/sec RA = 31
88942 deg
ZDOT = -684
357595 TA = 185
81793
MA = 185
83786
Ha = 227
951 n
mi
Hp = 219
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5078610
68 X = 1617870
74
Y = -12976181
83 feet Y = -3937439
32 meter
Z = -17423612
28 Z = -5303027
17
XDOT = 22103
329573 XDOT = 6700
132648
YDOT = 11673
103653 feet/sec YDOT = 3633
093764 meter/sec
ZDOT = -2245
267701 ZDOT = -651
719373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5264433
35 X = -1604599
29
Y = -12946182
71 feet Y = -3945996
49 meter
Z = -17390742
96 Z = -5300698
45
XDOT = 23084
648321 XDOT = 7036
200808
YDOT = -6546
779951 feet/sec YDOT = -1995
458529 meter/sec
ZDOT = -2108
843030 ZDOT = -642
775356
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13256
16290536
00016717 00000-0 10270-3 0 9073
2 25544 51
6496 32
3775 0003164 43
8139 316
3263 15
50305521 8359
Satellite: ISS
Catalog Number: 25544
Epoch time: 13256
16290536 = yrday
fracday
Element set: 907
Inclination: 51
6496 deg
RA of node: 32
3775 deg
Eccentricity:
0003164
Arg of perigee: 43
8139 deg
Mean anomaly: 316
3263 deg
Mean motion: 15
50305521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 835
Checksum: 296
Coasting Arc #9 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2013/257/03:29:45
399
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1714245
08 A = 6788409
64 meter
Y = 3834059
76 meter E =
0004973
Z = 5329261
95 I = 51
79387
XDOT = -6897
552652 Wp = 67
38497
YDOT = -3340
866737 meter/sec RA = 26
94127 deg
ZDOT = 186
552950 TA = 20
85056
MA = 20
83029
Ha = 227
961 n
mi
Hp = 219
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5624163
65 X = -1782878
96
Y = 12578936
22 feet Y = 3814506
53 meter
Z = 17484455
21 Z = 5320767
41
XDOT = -22629
765917 XDOT = -6860
587924
YDOT = -10960
848874 feet/sec YDOT = -3417
792858 meter/sec
ZDOT = 612
050361 ZDOT = 153
135395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4819241
54 X = 1468904
82
Y = 12957676
00 feet Y = 3949499
65 meter
Z = 17448225
43 Z = 5318219
11
XDOT = -22824
080239 XDOT = -6956
779657
YDOT = 7860
405008 feet/sec YDOT = 2395
851446 meter/sec
ZDOT = 472
324786 ZDOT = 143
964595
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13257
19428183
00016717 00000-0 10270-3 0 9089
2 25544 51
6493 27
2658 0003077 45
3764 314
7638 15
50337117 8515
Satellite: ISS
Catalog Number: 25544
Epoch time: 13257
19428183 = yrday
fracday
Element set: 908
Inclination: 51
6493 deg
RA of node: 27
2658 deg
Eccentricity:
0003077
Arg of perigee: 45
3764 deg
Mean anomaly: 314
7638 deg
Mean motion: 15
50337117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 318
Coasting Arc #10 (Orbit 865)
---------------------------------------
Vector Time (GMT): 2013/258/03:29:45
399
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1902278
09 A = 6788462
25 meter
Y = -3764116
11 meter E =
0017189
Z = -5334130
35 I = 51
76664
XDOT = 6990
589815 Wp = 84
85016
YDOT = 3090
399720 meter/sec RA = 21
99091 deg
ZDOT = 314
596699 TA = 188
13702
MA = 188
16493
Ha = 227
950 n
mi
Hp = 219
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6241069
83 X = 1970139
44
Y = -12349462
29 feet Y = -3742464
58 meter
Z = -17500427
65 Z = -5324724
22
XDOT = 22935
005956 XDOT = 6953
984518
YDOT = 10139
106693 feet/sec YDOT = 3168
368286 meter/sec
ZDOT = 1032
141401 ZDOT = 348
466945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4447173
77 X = -1355498
56
Y = -13156093
95 feet Y = -4009977
44 meter
Z = -17460383
07 Z = -5321924
76
XDOT = 22280
331127 XDOT = 6791
044928
YDOT = -9078
916967 feet/sec YDOT = -2767
253891 meter/sec
ZDOT = 1173
802328 ZDOT = 357
774949
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13258
16118937
00016717 00000-0 10270-3 0 9091
2 25544 51
6499 22
4733 0003185 48
0356 312
1065 15
50336616 8664
Satellite: ISS
Catalog Number: 25544
Epoch time: 13258
16118937 = yrday
fracday
Element set: 909
Inclination: 51
6499 deg
RA of node: 22
4733 deg
Eccentricity:
0003185
Arg of perigee: 48
0356 deg
Mean anomaly: 312
1065 deg
Mean motion: 15
50336616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 866
Checksum: 309
Coasting Arc #11 (Orbit 881)
---------------------------------------
Vector Time (GMT): 2013/259/03:29:45
399
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2113836
42 A = 6788550
45 meter
Y = 3704953
62 meter E =
0006461
Z = 5276955
05 I = 51
73858
XDOT = -7069
076579 Wp = 54
38256
YDOT = -2848
778900 meter/sec RA = 17
03862 deg
ZDOT = -827
207115 TA = 43
54158
MA = 43
49059
Ha = 227
965 n
mi
Hp = 219
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6935158
85 X = -2180742
71
Y = 12155359
64 feet Y = 3680941
77 meter
Z = 17312844
64 Z = 5266523
45
XDOT = -23192
508461 XDOT = -7032
677206
YDOT = -9346
387466 feet/sec YDOT = -2927
626364 meter/sec
ZDOT = -2713
934104 ZDOT = -861
459054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4057436
74 X = 1236706
72
Y = 13450636
94 feet Y = 4099754
14 meter
Z = 17268507
72 Z = 5263441
15
XDOT = -21684
120653 XDOT = -6609
319975
YDOT = 10227
853918 feet/sec YDOT = 3117
449874 meter/sec
ZDOT = -2857
229644 ZDOT = -870
883595
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13259
19254513
00016717 00000-0 10270-3 0 9108
2 25544 51
6500 17
3614 0003129 49
6742 310
4682 15
50373100 8825
Satellite: ISS
Catalog Number: 25544
Epoch time: 13259
19254513 = yrday
fracday
Element set: 910
Inclination: 51
6500 deg
RA of node: 17
3614 deg
Eccentricity:
0003129
Arg of perigee: 49
6742 deg
Mean anomaly: 310
4682 deg
Mean motion: 15
50373100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 882
Checksum: 277
Coasting Arc #12 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2013/260/03:29:45
399
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2328433
94 A = 6788951
35 meter
Y = -3703985
47 meter E =
0016165
Z = -5205287
26 I = 51
71031
XDOT = 7076
190427 Wp = 91
53107
YDOT = 2586
892090 meter/sec RA = 12
08432 deg
ZDOT = 1327
693703 TA = 191
22519
MA = 191
26130
Ha = 227
939 n
mi
Hp = 219
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7639218
98 X = 2394965
35
Y = -12152183
30 feet Y = -3677576
06 meter
Z = -17077714
11 Z = -5193813
99
XDOT = 23215
847857 XDOT = 7040
287785
YDOT = 8487
178774 feet/sec YDOT = 2665
821961 meter/sec
ZDOT = 4355
950468 ZDOT = 1361
981419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3814401
76 X = -1162629
66
Y = -13897651
38 feet Y = -4236004
14 meter
Z = -17029009
66 Z = -5190442
15
XDOT = 20838
985311 XDOT = 6351
722723
YDOT = -11220
069191 feet/sec YDOT = -3419
877089 meter/sec
ZDOT = 4499
429670 ZDOT = 1371
426163
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13260
15943317
00016717 00000-0 10270-3 0 9114
2 25544 51
6502 12
5687 0003187 52
1019 308
0420 15
50367047 8976
Satellite: ISS
Catalog Number: 25544
Epoch time: 13260
15943317 = yrday
fracday
Element set: 911
Inclination: 51
6502 deg
RA of node: 12
5687 deg
Eccentricity:
0003187
Arg of perigee: 52
1019 deg
Mean anomaly: 308
0420 deg
Mean motion: 15
50367047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 284
Coasting Arc #13 (Orbit 912)
---------------------------------------
Vector Time (GMT): 2013/261/03:29:45
399
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2560960
38 A = 6789375
29 meter
Y = 3715735
79 meter E =
0008769
Z = 5067747
40 I = 51
68223
XDOT = -7062
002280 Wp = 54
54892
YDOT = -2348
346778 meter/sec RA = 7
12853 deg
ZDOT = -1839
696472 TA = 53
30134
MA = 53
22081
Ha = 227
954 n
mi
Hp = 219
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8402100
99 X = -2626937
86
Y = 12190734
22 feet Y = 3686729
28 meter
Z = 16626467
86 Z = 5055145
80
XDOT = -23169
298819 XDOT = -7026
280976
YDOT = -7704
549796 feet/sec YDOT = -2427
119091 meter/sec
ZDOT = -6035
749580 ZDOT = -1873
915809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3581662
76 X = 1091690
81
Y = 14427579
69 feet Y = 4397526
29 meter
Z = 16573031
46 Z = 5051459
99
XDOT = -19972
679684 XDOT = -6087
672768
YDOT = 12083
324561 feet/sec YDOT = 3682
997326 meter/sec
ZDOT = -6178
969239 ZDOT = -1883
349824
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13261
19076814
00016717 00000-0 10270-3 0 9129
2 25544 51
6506 7
4570 0003156 53
7727 306
3715 15
50408030 9138
Satellite: ISS
Catalog Number: 25544
Epoch time: 13261
19076814 = yrday
fracday
Element set: 912
Inclination: 51
6506 deg
RA of node: 7
4570 deg
Eccentricity:
0003156
Arg of perigee: 53
7727 deg
Mean anomaly: 306
3715 deg
Mean motion: 15
50408030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 913
Checksum: 281
Coasting Arc #14 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2013/262/03:29:45
399
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2776342
42 A = 6790094
43 meter
Y = -3787410
28 meter E =
0014182
Z = -4917169
97 I = 51
65339
XDOT = 6979
525158 Wp = 96
69071
YDOT = 2104
375532 meter/sec RA = 2
17060 deg
ZDOT = 2324
075318 TA = 196
07318
MA = 196
11822
Ha = 227
929 n
mi
Hp = 219
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9108734
97 X = 2842374
01
Y = -12425886
74 feet Y = -3755994
94 meter
Z = -16132447
39 Z = -4903521
82
XDOT = 22898
704586 XDOT = 6944
185100
YDOT = 6904
119201 feet/sec YDOT = 2182
227749 meter/sec
ZDOT = 7624
919021 ZDOT = 2357
895086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3555102
13 X = -1083595
13
Y = -15053093
13 feet Y = -4588182
78 meter
Z = -16074613
81 Z = -4899542
29
XDOT = 18919
169948 XDOT = 5766
563000
YDOT = -12747
061793 feet/sec YDOT = -3885
304435 meter/sec
ZDOT = 7766
488537 ZDOT = 2367
225706
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13262
15763675
00016717 00000-0 10270-3 0 9135
2 25544 51
6502 2
6643 0003178 56
7410 303
4045 15
50396724 9284
Satellite: ISS
Catalog Number: 25544
Epoch time: 13262
15763675 = yrday
fracday
Element set: 913
Inclination: 51
6502 deg
RA of node: 2
6643 deg
Eccentricity:
0003178
Arg of perigee: 56
7410 deg
Mean anomaly: 303
4045 deg
Mean motion: 15
50396724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 293
Coasting Arc #15 (Orbit 943)
---------------------------------------
Vector Time (GMT): 2013/263/03:29:45
399
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3002802
86 A = 6790820
42 meter
Y = 3870120
05 meter E =
0011216
Z = 4697114
78 I = 51
62570
XDOT = -6871
875183 Wp = 61
87575
YDOT = -1899
312641 meter/sec RA = 357
21159 deg
ZDOT = -2817
877484 TA = 56
13781
MA = 56
03114
Ha = 227
931 n
mi
Hp = 219
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9851715
42 X = -3068673
64
Y = 12697244
25 feet Y = 3836173
15 meter
Z = 15410481
56 Z = 4682366
82
XDOT = -22545
522254 XDOT = -6836
437361
YDOT = -6231
340685 feet/sec YDOT = -1975
960571 meter/sec
ZDOT = -9245
004869 ZDOT = -2851
174246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3557181
20 X = 1084228
83
Y = 15733525
36 feet Y = 4795578
53 meter
Z = 15348025
66 Z = 4678078
22
XDOT = -17891
983729 XDOT = -5453
476641
YDOT = 13232
779867 feet/sec YDOT = 4033
351303 meter/sec
ZDOT = -9384
399996 ZDOT = -2860
365119
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13263
18895084
00016717 00000-0 10270-3 0 9140
2 25544 51
6504 357
5526 0003154 58
1389 302
0068 15
50440268 9444
Satellite: ISS
Catalog Number: 25544
Epoch time: 13263
18895084 = yrday
fracday
Element set: 914
Inclination: 51
6504 deg
RA of node: 357
5526 deg
Eccentricity:
0003154
Arg of perigee: 58
1389 deg
Mean anomaly: 302
0068 deg
Mean motion: 15
50440268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 944
Checksum: 308
Coasting Arc #16 (Orbit 958)
---------------------------------------
Vector Time (GMT): 2013/264/03:29:45
399
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3192656
40 A = 6791782
29 meter
Y = -4008750
20 meter E =
0011556
Z = -4467890
75 I = 51
59684
XDOT = 6706
267763 Wp = 98
29134
YDOT = 1703
071441 meter/sec RA = 352
25011 deg
ZDOT = 3269
728982 TA = 204
71991
MA = 204
77533
Ha = 227
922 n
mi
Hp = 219
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10474594
50 X = 3258949
84
Y = -13152067
58 feet Y = -3972677
81 meter
Z = -14658434
22 Z = -4452219
42
XDOT = 22002
190823 XDOT = 6670
841617
YDOT = 5587
504728 feet/sec YDOT = 1777
867549 meter/sec
ZDOT = 10727
457291 ZDOT = 3302
221428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3802358
93 X = -1158959
00
Y = -16437054
41 feet Y = -5010014
18 meter
Z = -14592087
38 Z = -4447668
23
XDOT = 16758
217612 XDOT = 5107
904728
YDOT = -13504
300555 feet/sec YDOT = -4116
110809 meter/sec
ZDOT = 10863
497483 ZDOT = 3311
194033
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13264
15580000
00016717 00000-0 10270-3 0 9158
2 25544 51
6492 352
7595 0003169 62
4148 297
7324 15
50425477 9596
Satellite: ISS
Catalog Number: 25544
Epoch time: 13264
15580000 = yrday
fracday
Element set: 915
Inclination: 51
6492 deg
RA of node: 352
7595 deg
Eccentricity:
0003169
Arg of perigee: 62
4148 deg
Mean anomaly: 297
7324 deg
Mean motion: 15
50425477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 959
Checksum: 318
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