[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 17th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
295/11:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 220
6
297/11:20:09
352 -2
0 2
0 2
0
N/A -0
1 0
0 228
5
000/00:04:14
704 -0
2 0
0 221
7
301/09:00:02
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 221
5
Coasting Arc #1 (Orbit 1352)
---------------------------------------
Vector Time (GMT): 2013/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2301695
34 A = 6798869
09 meter
Y = -5711008
92 meter E =
0015074
Z = 2864299
65 I = 51
39672
XDOT = 5772
056647 Wp = 72
53082
YDOT = 210
307085 meter/sec RA = 226
24766 deg
ZDOT = 5040
094268 TA = 320
13341
MA = 320
24404
Ha = 228
631 n
mi
Hp = 221
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7551493
91 X = -2251576
72
Y = -18736905
91 feet Y = -5736467
37 meter
Z = 9397308
56 Z = 2853240
49
XDOT = 18937
193725 XDOT = 5744
792165
YDOT = 689
983876 feet/sec YDOT = 274
702063 meter/sec
ZDOT = 16535
742350 ZDOT = 5068
068567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14657693
52 X = 4467664
98
Y = 13932158
55 feet Y = 4246521
93 meter
Z = 9351635
71 Z = 2850378
57
XDOT = -16427
827552 XDOT = -5007
201838
YDOT = 6066
516883 feet/sec YDOT = 1849
074346 meter/sec
ZDOT = 16653
085974 ZDOT = 5075
860605
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 13289
55869815
00016717 00000-0 10270-3 0 9007
2 25544 51
6491 226
9441 0002723 26
6750 333
4540 15
49679053 13539
Satellite: ISS
Catalog Number: 25544
Epoch time: 13289
55869815 = yrday
fracday
Element set: 900
Inclination: 51
6491 deg
RA of node: 226
9441 deg
Eccentricity:
0002723
Arg of perigee: 26
6750 deg
Mean anomaly: 333
4540 deg
Mean motion: 15
49679053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1353
Checksum: 320
Coasting Arc #2 (Orbit 1367)
---------------------------------------
Vector Time (GMT): 2013/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2542852
47 A = 6798226
70 meter
Y = 5503788
86 meter E =
0005779
Z = -3081625
24 I = 51
41773
XDOT = -5899
084831 Wp = 79
58167
YDOT = -1
390642 meter/sec RA = 221
27978 deg
ZDOT = -4877
011818 TA = 135
84340
MA = 135
79725
Ha = 228
627 n
mi
Hp = 221
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8342691
85 X = 2496088
90
Y = 18057050
06 feet Y = 5531962
82 meter
Z = -10110319
03 Z = -3069386
29
XDOT = -19353
952859 XDOT = -5874
939178
YDOT = -4
562473 feet/sec YDOT = -67
223528 meter/sec
ZDOT = -16000
694940 ZDOT = -4905
610941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15323335
62 X = -4670552
70
Y = -12722997
70 feet Y = -3877969
70 meter
Z = -10059663
50 Z = -3066185
43
XDOT = 16477
046119 XDOT = 5022
203657
YDOT = -7116
266386 feet/sec YDOT = -2169
037995 meter/sec
ZDOT = -16120
693090 ZDOT = -4913
587254
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 13290
52599304
00016717 00000-0 10270-3 0 9010
2 25544 51
6499 222
1544 0002794 29
5342 330
5965 15
49714788 13686
Satellite: ISS
Catalog Number: 25544
Epoch time: 13290
52599304 = yrday
fracday
Element set: 901
Inclination: 51
6499 deg
RA of node: 222
1544 deg
Eccentricity:
0002794
Arg of perigee: 29
5342 deg
Mean anomaly: 330
5965 deg
Mean motion: 15
49714788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1368
Checksum: 330
Coasting Arc #3 (Orbit 1383)
---------------------------------------
Vector Time (GMT): 2013/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2770638
67 A = 6797690
46 meter
Y = -5268412
50 meter E =
0014500
Z = 3267166
86 I = 51
43981
XDOT = 6034
586813 Wp = 78
68493
YDOT = -236
080707 meter/sec RA = 216
31368 deg
ZDOT = 4721
740697 TA = 319
29084
MA = 319
39913
Ha = 228
652 n
mi
Hp = 221
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9090021
89 X = -2727391
58
Y = -17284817
91 feet Y = -5299153
38 meter
Z = 10719051
38 Z = 3253812
65
XDOT = 19798
513165 XDOT = 6013
840744
YDOT = -774
543002 feet/sec YDOT = -168
713610 meter/sec
ZDOT = 15491
275252 ZDOT = 4751
006475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15870734
55 X = 4837399
89
Y = 11432286
31 feet Y = 3484560
87 meter
Z = 10663681
59 Z = 3250290
15
XDOT = -16482
801978 XDOT = -5023
958043
YDOT = 8271
397808 feet/sec YDOT = 2521
122052 meter/sec
ZDOT = 15614
108276 ZDOT = 4759
180203
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 13291
55775552
00016717 00000-0 10270-3 0 9026
2 25544 51
6499 217
0459 0002753 33
3674 326
7650 15
49729378 13847
Satellite: ISS
Catalog Number: 25544
Epoch time: 13291
55775552 = yrday
fracday
Element set: 902
Inclination: 51
6499 deg
RA of node: 217
0459 deg
Eccentricity:
0002753
Arg of perigee: 33
3674 deg
Mean anomaly: 326
7650 deg
Mean motion: 15
49729378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1384
Checksum: 337
Coasting Arc #4 (Orbit 1398)
---------------------------------------
Vector Time (GMT): 2013/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2944225
93 A = 6796950
78 meter
Y = 5043848
53 meter E =
0007050
Z = -3485179
06 I = 51
46392
XDOT = -6154
800527 Wp = 70
23395
YDOT = 470
085559 meter/sec RA = 211
34860 deg
ZDOT = -4524
316918 TA = 150
69440
MA = 150
65484
Ha = 228
605 n
mi
Hp = 220
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9659533
88 X = 2904536
16
Y = 16548059
49 feet Y = 5076550
50 meter
Z = -11434314
49 Z = -3470972
79
XDOT = -20192
915116 XDOT = -6137
621223
YDOT = 1542
275456 feet/sec YDOT = 401
354302 meter/sec
ZDOT = -14843
559443 ZDOT = -4554
175445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16237023
18 X = -4949044
67
Y = -10239590
52 feet Y = -3121027
19 meter
Z = -11375336
45 Z = -3467202
55
XDOT = 16406
838717 XDOT = 5000
804441
YDOT = -9406
155238 feet/sec YDOT = -2866
996116 meter/sec
ZDOT = -14968
918811 ZDOT = -4562
526454
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 13292
52501435
00016717 00000-0 10270-3 0 9032
2 25544 51
6507 212
2562 0002790 36
3571 323
7768 15
49774589 13996
Satellite: ISS
Catalog Number: 25544
Epoch time: 13292
52501435 = yrday
fracday
Element set: 903
Inclination: 51
6507 deg
RA of node: 212
2562 deg
Eccentricity:
0002790
Arg of perigee: 36
3571 deg
Mean anomaly: 323
7768 deg
Mean motion: 15
49774589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1399
Checksum: 322
Coasting Arc #5 (Orbit 1414)
---------------------------------------
Vector Time (GMT): 2013/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3100064
92 A = 6796359
36 meter
Y = -4797756
33 meter E =
0013650
Z = 3669765
42 I = 51
48834
XDOT = 6280
917365 Wp = 85
20071
YDOT = -733
798925 meter/sec RA = 206
38513 deg
ZDOT = 4333
690339 TA = 318
49026
MA = 318
59384
Ha = 228
653 n
mi
Hp = 220
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10170816
68 X = -3064012
14
Y = -15740670
39 feet Y = -4832221
38 meter
Z = 12039912
80 Z = 3654793
13
XDOT = 20606
684268 XDOT = 6267
603611
YDOT = -2407
476787 feet/sec YDOT = -663
635830 meter/sec
ZDOT = 14218
144157 ZDOT = 4364
170966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16481581
09 X = 5023585
92
Y = 9003681
56 feet Y = 2744322
14 meter
Z = 11977684
23 Z = 3650798
15
XDOT = -16269
927969 XDOT = -4959
074045
YDOT = 10641
655557 feet/sec YDOT = 3243
576614 meter/sec
ZDOT = 14346
159279 ZDOT = 4372
709348
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 13293
55673875
00016717 00000-0 10270-3 0 9045
2 25544 51
6502 207
1474 0002762 40
1385 319
9969 15
49784780 14154
Satellite: ISS
Catalog Number: 25544
Epoch time: 13293
55673875 = yrday
fracday
Element set: 904
Inclination: 51
6502 deg
RA of node: 207
1474 deg
Eccentricity:
0002762
Arg of perigee: 40
1385 deg
Mean anomaly: 319
9969 deg
Mean motion: 15
49784780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1415
Checksum: 333
Coasting Arc #6 (Orbit 1429)
---------------------------------------
Vector Time (GMT): 2013/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3203925
39 A = 6795561
83 meter
Y = 4573164
49 meter E =
0008721
Z = -3882903
31 I = 51
51472
XDOT = -6384
672770 Wp = 65
68586
YDOT = 995
758629 meter/sec RA = 201
42292 deg
ZDOT = -4099
233275 TA = 161
14662
MA = 161
11430
Ha = 228
561 n
mi
Hp = 220
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10511566
23 X = 3171411
69
Y = 15003820
49 feet Y = 4608810
80 meter
Z = -12739184
10 Z = -3867417
78
XDOT = -20947
089142 XDOT = -6375
419572
YDOT = 3266
924636 feet/sec YDOT = 924
412661 meter/sec
ZDOT = -13448
928066 ZDOT = -4130
227788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16574657
97 X = -5051955
75
Y = -7907303
62 feet Y = -2410146
14 meter
Z = -12674767
38 Z = -3863269
10
XDOT = 16024
408040 XDOT = 4884
239571
YDOT = -11842
792898 feet/sec YDOT = -3609
683275 meter/sec
ZDOT = -13579
147026 ZDOT = -4138
924014
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 13294
52396150
00016717 00000-0 10270-3 0 9052
2 25544 51
6508 202
3576 0002757 42
3271 317
8092 15
49832529 14308
Satellite: ISS
Catalog Number: 25544
Epoch time: 13294
52396150 = yrday
fracday
Element set: 905
Inclination: 51
6508 deg
RA of node: 202
3576 deg
Eccentricity:
0002757
Arg of perigee: 42
3271 deg
Mean anomaly: 317
8092 deg
Mean motion: 15
49832529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1430
Checksum: 304
Coasting Arc #7 (Orbit 1444)
---------------------------------------
Vector Time (GMT): 2013/295/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 927096
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3703817
56 A = 6791677
20 meter
Y = 2947901
25 meter E =
0013468
Z = -4882391
89 I = 51
52990
XDOT = -6184
830215 Wp = 97
11573
YDOT = -3816
645265 meter/sec RA = 196
52163 deg
ZDOT = 2391
489882 TA = 196
39260
MA = 196
43619
Ha = 228
531 n
mi
Hp = 220
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12151632
41 X = -3712788
48
Y = 9671592
03 feet Y = 2906432
44 meter
Z = -16018346
09 Z = -4900407
03
XDOT = -20291
437713 XDOT = -6153
309448
YDOT = -12521
802052 feet/sec YDOT = -3885
631624 meter/sec
ZDOT = 7846
095412 ZDOT = 2361
520578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7376431
62 X = 2248336
36
Y = -13577540
97 feet Y = -4138434
49 meter
Z = -16094344
10 Z = -4905556
08
XDOT = 22608
894883 XDOT = 6891
191160
YDOT = 3146
760655 feet/sec YDOT = 959
132648 meter/sec
ZDOT = 7720
776640 ZDOT = 2353
292720
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 13295
49116767
00016717 00000-0 10270-3 0 9064
2 25544 51
6502 197
5675 0002730 44
9373 315
1998 15
49847915 14456
Satellite: ISS
Catalog Number: 25544
Epoch time: 13295
49116767 = yrday
fracday
Element set: 906
Inclination: 51
6502 deg
RA of node: 197
5675 deg
Eccentricity:
0002730
Arg of perigee: 44
9373 deg
Mean anomaly: 315
1998 deg
Mean motion: 15
49847915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1445
Checksum: 344
Coasting Arc #8 (Orbit 1460)
---------------------------------------
Vector Time (GMT): 2013/296/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 927096
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3758639
10 A = 6792062
11 meter
Y = -3074279
84 meter E =
0010233
Z = 4743836
02 I = 51
56090
XDOT = 6271
950580 Wp = 58
47786
YDOT = 3476
146126 meter/sec RA = 191
56119 deg
ZDOT = -2707
100591 TA = 58
37424
MA = 58
27443
Ha = 228
390 n
mi
Hp = 220
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12331493
11 X = 3769692
28
Y = -10086219
93 feet Y = -3032186
37 meter
Z = 15563766
47 Z = 4762122
48
XDOT = 20577
265683 XDOT = 6245
764028
YDOT = 11404
678891 feet/sec YDOT = 3546
136551 meter/sec
ZDOT = -8881
563620 ZDOT = -2676
695135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7142168
72 X = -2176933
02
Y = 14155533
72 feet Y = 4314606
68 meter
Z = 15640929
40 Z = 4767355
28
XDOT = -22444
639479 XDOT = -6841
126113
YDOT = -1616
994397 feet/sec YDOT = -492
859892 meter/sec
ZDOT = -8754
355406 ZDOT = -2668
327528
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 13296
52283470
00016717 00000-0 10270-3 0 9076
2 25544 51
6496 192
4582 0002718 47
2087 312
9292 15
49895369 14619
Satellite: ISS
Catalog Number: 25544
Epoch time: 13296
52283470 = yrday
fracday
Element set: 907
Inclination: 51
6496 deg
RA of node: 192
4582 deg
Eccentricity:
0002718
Arg of perigee: 47
2087 deg
Mean anomaly: 312
9292 deg
Mean motion: 15
49895369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1461
Checksum: 339
Coasting Arc #9 (Orbit 1475)
---------------------------------------
Vector Time (GMT): 2013/297/11:22:16
704
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -503151
03 A = 6790754
40 meter
Y = 4196009
13 meter E =
0015405
Z = -5328813
11 I = 51
58362
XDOT = -7596
997616 Wp = 84
73362
YDOT = -896
234632 meter/sec RA = 186
65090 deg
ZDOT = 13
015685 TA = 185
38251
MA = 185
39909
Ha = 228
478 n
mi
Hp = 221
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1650757
97 X = -524147
94
Y = 13766434
16 feet Y = 4190264
99 meter
Z = -17482982
65 Z = -5331308
57
XDOT = -24924
532860 XDOT = -7586
474319
YDOT = -2940
402335 feet/sec YDOT = -981
130252 meter/sec
ZDOT = 42
702379 ZDOT = -23
864910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3907463
94 X = -1190995
01
Y = -13288576
45 feet Y = -4050358
10 meter
Z = -17493994
83 Z = -5332169
62
XDOT = 23149
949669 XDOT = 7056
104659
YDOT = -6653
576001 feet/sec YDOT = -2028
009965 meter/sec
ZDOT = -112
037958 ZDOT = -34
149170
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 13297
49000626
00016717 00000-0 10270-3 0 9084
2 25544 51
6502 187
6676 0001543 18
4844 341
6362 15
49538331 14769
Satellite: ISS
Catalog Number: 25544
Epoch time: 13297
49000626 = yrday
fracday
Element set: 908
Inclination: 51
6502 deg
RA of node: 187
6676 deg
Eccentricity:
0001543
Arg of perigee: 18
4844 deg
Mean anomaly: 341
6362 deg
Mean motion: 15
49538331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1476
Checksum: 317
Coasting Arc #10 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2013/298/11:22:16
704
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 382653
44 A = 6790617
24 meter
Y = -4202948
93 meter E =
0003373
Z = 5317464
97 I = 51
61413
XDOT = 7649
486913 Wp = 58
37077
YDOT = 406
665784 meter/sec RA = 181
69676 deg
ZDOT = -227
203422 TA = 33
80756
MA = 33
78606
Ha = 228
361 n
mi
Hp = 221
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1255424
66 X = 403792
08
Y = -13789202
53 feet Y = -4198551
45 meter
Z = 17445751
20 Z = 5319375
41
XDOT = 25096
741840 XDOT = 7645
474664
YDOT = 1334
205329 feet/sec YDOT = 492
184770 meter/sec
ZDOT = -745
418051 ZDOT = -190
052076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4506244
80 X = 1373503
41
Y = 13081028
06 feet Y = 3987097
35 meter
Z = 17454308
78 Z = 5320073
32
XDOT = -22556
514733 XDOT = -6875
225691
YDOT = 8564
987563 feet/sec YDOT = 2610
608209 meter/sec
ZDOT = -589
459158 ZDOT = -179
667151
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 13298
52188881
00016717 00000-0 10270-3 0 9090
2 25544 51
6500 182
5594 0001492 16
8220 343
2979 15
49584233 14925
Satellite: ISS
Catalog Number: 25544
Epoch time: 13298
52188881 = yrday
fracday
Element set: 909
Inclination: 51
6500 deg
RA of node: 182
5594 deg
Eccentricity:
0001492
Arg of perigee: 16
8220 deg
Mean anomaly: 343
2979 deg
Mean motion: 15
49584233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 329
Coasting Arc #11 (Orbit 1506)
---------------------------------------
Vector Time (GMT): 2013/299/11:22:16
704
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -265107
48 A = 6790638
70 meter
Y = 4230410
40 meter E =
0015294
Z = -5318497
54 I = 51
64543
XDOT = -7636
400054 Wp = 87
93511
YDOT = 80
584465 meter/sec RA = 176
74431 deg
ZDOT = 446
394550 TA = 186
32269
MA = 186
34201
Ha = 228
406 n
mi
Hp = 221
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -869775
20 X = -286556
96
Y = 13879299
20 feet Y = 4227325
61 meter
Z = -17449138
92 Z = -5319837
73
XDOT = -25053
805950 XDOT = -7638
902103
YDOT = 264
384727 feet/sec YDOT = -4
824587 meter/sec
ZDOT = 1464
549047 ZDOT = 409
290981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5118552
06 X = -1560134
67
Y = -12921943
70 feet Y = -3938608
44 meter
Z = -17455305
78 Z = -5320377
20
XDOT = 21707
463415 XDOT = 6616
434849
YDOT = -10359
142309 feet/sec YDOT = -3157
466576 meter/sec
ZDOT = 1308
710269 ZDOT = 398
894890
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 13299
48926336
00016717 00000-0 10270-3 0 9103
2 25544 51
6504 177
7702 0001564 20
2905 339
8307 15
49595562 15075
Satellite: ISS
Catalog Number: 25544
Epoch time: 13299
48926336 = yrday
fracday
Element set: 910
Inclination: 51
6504 deg
RA of node: 177
7702 deg
Eccentricity:
0001564
Arg of perigee: 20
2905 deg
Mean anomaly: 339
8307 deg
Mean motion: 15
49595562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1507
Checksum: 322
Coasting Arc #12 (Orbit 1522)
---------------------------------------
Vector Time (GMT): 2013/300/11:22:16
704
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 166588
83 A = 6790586
28 meter
Y = -4249649
84 meter E =
0004176
Z = 5291325
56 I = 51
67651
XDOT = 7613
276905 Wp = 50
32558
YDOT = -553
720708 meter/sec RA = 171
79391 deg
ZDOT = -681
441732 TA = 46
19956
MA = 46
16503
Ha = 228
322 n
mi
Hp = 221
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 546551
28 X = 188392
77
Y = -13942420
72 feet Y = -4247664
71 meter
Z = 17359991
98 Z = 5292188
05
XDOT = 24977
942602 XDOT = 7622
213199
YDOT = -1816
668990 feet/sec YDOT = -468
534276 meter/sec
ZDOT = -2235
701220 ZDOT = -644
434851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5658143
86 X = 1724602
25
Y = 12748750
96 feet Y = 3885819
29 meter
Z = 17364155
39 Z = 5292594
56
XDOT = -20794
081374 XDOT = -6338
036003
YDOT = 12075
332058 feet/sec YDOT = 3680
561211 meter/sec
ZDOT = -2080
191168 ZDOT = -634
042268
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 13300
52110983
00016717 00000-0 10270-3 0 9115
2 25544 51
6505 172
6619 0001531 20
0881 340
0329 15
49636832 15234
Satellite: ISS
Catalog Number: 25544
Epoch time: 13300
52110983 = yrday
fracday
Element set: 911
Inclination: 51
6505 deg
RA of node: 172
6619 deg
Eccentricity:
0001531
Arg of perigee: 20
0881 deg
Mean anomaly: 340
0329 deg
Mean motion: 15
49636832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1523
Checksum: 273
Coasting Arc #13 (Orbit 1536)
---------------------------------------
Vector Time (GMT): 2013/301/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1223786
08 A = 6790405
31 meter
Y = -4032474
94 meter E =
0003156
Z = 5321888
99 I = 51
70230
XDOT = 7422
271178 Wp = 76
68823
YDOT = -1889
704440 meter/sec RA = 167
34369 deg
ZDOT = 275
490728 TA = 10
68990
MA = 10
68319
Ha = 228
342 n
mi
Hp = 221
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4015046
18 X = -1204455
78
Y = -13229904
65 feet Y = -4046051
64 meter
Z = 17460265
71 Z = 5315991
09
XDOT = 24351
283391 XDOT = 7441
512345
YDOT = -6199
817715 feet/sec YDOT = -1806
596277 meter/sec
ZDOT = 903
840971 ZDOT = 311
594855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2018099
26 X = 615116
66
Y = 13708570
03 feet Y = 4178372
14 meter
Z = 17436003
98 Z = 5314494
01
XDOT = -24013
169960 XDOT = -7319
214204
YDOT = 2194
670443 feet/sec YDOT = 668
935551 meter/sec
ZDOT = 1055
743076 ZDOT = 321
790489
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 13301
42396154
00016717 00000-0 10270-3 0 9122
2 25544 51
6493 168
1917 0001514 23
0857 337
0361 15
49664632 15374
Satellite: ISS
Catalog Number: 25544
Epoch time: 13301
42396154 = yrday
fracday
Element set: 912
Inclination: 51
6493 deg
RA of node: 168
1917 deg
Eccentricity:
0001514
Arg of perigee: 23
0857 deg
Mean anomaly: 337
0361 deg
Mean motion: 15
49664632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1537
Checksum: 300
Coasting Arc #14 (Orbit 1551)
---------------------------------------
Vector Time (GMT): 2013/302/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1302273
12 A = 6790372
61 meter
Y = 4005761
91 meter E =
0015714
Z = -5339623
44 I = 51
73276
XDOT = -7285
291604 Wp = 84
71495
YDOT = 2332
647311 meter/sec RA = 162
39640 deg
ZDOT = -25
512165 TA = 185
03376
MA = 185
04957
Ha = 228
378 n
mi
Hp = 221
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4272549
61 X = 1283321
90
Y = 13142263
48 feet Y = 4020218
36 meter
Z = -17518449
59 Z = -5333343
36
XDOT = -23901
875342 XDOT = -7310
710383
YDOT = 7653
042358 feet/sec YDOT = 2251
036416 meter/sec
ZDOT = -83
701330 ZDOT = -60
965971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2521115
23 X = -768435
92
Y = -13620702
80 feet Y = -4151590
21 meter
Z = -17492577
82 Z = -5331737
72
XDOT = 23736
642978 XDOT = 7234
928780
YDOT = -4088
681909 feet/sec YDOT = -1246
230246 meter/sec
ZDOT = -232
942195 ZDOT = -71
000781
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 13302
39128739
00016717 00000-0 10270-3 0 9132
2 25544 51
6501 163
4022 0001630 29
3241 330
8001 15
49669353 15528
Satellite: ISS
Catalog Number: 25544
Epoch time: 13302
39128739 = yrday
fracday
Element set: 913
Inclination: 51
6501 deg
RA of node: 163
4022 deg
Eccentricity:
0001630
Arg of perigee: 29
3241 deg
Mean anomaly: 330
8001 deg
Mean motion: 15
49669353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1552
Checksum: 274
Coasting Arc #15 (Orbit 1567)
---------------------------------------
Vector Time (GMT): 2013/303/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1360876
67 A = 6790218
29 meter
Y = -3980541
58 meter E =
0003608
Z = 5327473
72 I = 51
76157
XDOT = 7144
565265 Wp = 60
87002
YDOT = -2763
498432 meter/sec RA = 157
45118 deg
ZDOT = -237
931015 TA = 31
40598
MA = 31
38444
Ha = 228
302 n
mi
Hp = 221
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4464818
47 X = -1342144
16
Y = -13059519
62 feet Y = -3995654
55 meter
Z = 17478588
32 Z = 5320908
43
XDOT = 23440
174755 XDOT = 7176
092136
YDOT = -9066
595905 feet/sec YDOT = -2683
427099 meter/sec
ZDOT = -780
613565 ZDOT = -203
145867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2955673
93 X = 900889
41
Y = 13516483
13 feet Y = 4119824
06 meter
Z = 17451515
17 Z = 5319221
82
XDOT = -23385
619254 XDOT = -7127
936749
YDOT = 5940
283598 feet/sec YDOT = 1810
598441 meter/sec
ZDOT = -634
113373 ZDOT = -193
277756
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 13303
42308057
00016717 00000-0 10270-3 0 9141
2 25544 51
6498 158
2936 0001559 27
0618 333
0613 15
49721106 15688
Satellite: ISS
Catalog Number: 25544
Epoch time: 13303
42308057 = yrday
fracday
Element set: 914
Inclination: 51
6498 deg
RA of node: 158
2936 deg
Eccentricity:
0001559
Arg of perigee: 27
0618 deg
Mean anomaly: 333
0613 deg
Mean motion: 15
49721106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1568
Checksum: 303
Coasting Arc #16 (Orbit 1582)
---------------------------------------
Vector Time (GMT): 2013/304/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1427778
50 A = 6790269
90 meter
Y = 3982282
09 meter E =
0015567
Z = -5324795
94 I = 51
79020
XDOT = -6945
866386 Wp = 88
59344
YDOT = 3165
252594 meter/sec RA = 152
50736 deg
ZDOT = 506
417872 TA = 186
22977
MA = 186
24915
Ha = 228
306 n
mi
Hp = 221
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4684312
68 X = 1409008
64
Y = 13065229
96 feet Y = 3998142
99 meter
Z = -17469802
96 Z = -5317905
71
XDOT = -22788
275544 XDOT = -6983
204798
YDOT = 10384
686987 feet/sec YDOT = 3087
370768 meter/sec
ZDOT = 1661
475957 ZDOT = 472
583732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3405384
81 X = -1037961
29
Y = -13492187
64 feet Y = -4112418
79 meter
Z = -17441366
39 Z = -5316128
48
XDOT = 22772
373307 XDOT = 6941
019384
YDOT = -7704
143768 feet/sec YDOT = -2348
223021 meter/sec
ZDOT = 1518
906294 ZDOT = 462
962638
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 13304
39037137
00016717 00000-0 10270-3 0 9157
2 25544 51
6502 153
5040 0001652 31
2419 328
8829 15
49727935 15832
Satellite: ISS
Catalog Number: 25544
Epoch time: 13304
39037137 = yrday
fracday
Element set: 915
Inclination: 51
6502 deg
RA of node: 153
5040 deg
Eccentricity:
0001652
Arg of perigee: 31
2419 deg
Mean anomaly: 328
8829 deg
Mean motion: 15
49727935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1583
Checksum: 303
Coasting Arc #17 (Orbit 1598)
---------------------------------------
Vector Time (GMT): 2013/305/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1476735
90 A = 6790227
35 meter
Y = -3990092
69 meter E =
0004581
Z = 5289254
88 I = 51
81709
XDOT = 6746
264441 Wp = 51
62839
YDOT = -3549
858881 meter/sec RA = 147
56514 deg
ZDOT = -791
169308 TA = 45
93682
MA = 45
89912
Ha = 228
252 n
mi
Hp = 221
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4844934
04 X = -1457702
50
Y = -13090855
27 feet Y = -4006499
64 meter
Z = 17353198
43 Z = 5282127
39
XDOT = 22133
413521 XDOT = 6789
301731
YDOT = -11646
518639 feet/sec YDOT = -3474
177285 meter/sec
ZDOT = -2595
699830 ZDOT = -758
290877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3794019
23 X = 1156417
06
Y = 13471073
22 feet Y = 4105983
12 meter
Z = 17323769
15 Z = 5280284
84
XDOT = -22096
927115 XDOT = -6735
143385
YDOT = 9396
901133 feet/sec YDOT = 2864
175465 meter/sec
ZDOT = -2457
081331 ZDOT = -748
918390
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 13305
42212746
00016717 00000-0 10270-3 0 9164
2 25544 51
6498 148
3949 0001611 29
8281 330
2961 15
49777577 15999
Satellite: ISS
Catalog Number: 25544
Epoch time: 13305
42212746 = yrday
fracday
Element set: 916
Inclination: 51
6498 deg
RA of node: 148
3949 deg
Eccentricity:
0001611
Arg of perigee: 29
8281 deg
Mean anomaly: 330
2961 deg
Mean motion: 15
49777577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 337
Coasting Arc #18 (Orbit 1613)
---------------------------------------
Vector Time (GMT): 2013/306/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1544216
54 A = 6790385
77 meter
Y = 4022452
56 meter E =
0015049
Z = -5261388
45 I = 51
84292
XDOT = -6494
467839 Wp = 92
48877
YDOT = 3897
538426 meter/sec RA = 142
62412 deg
ZDOT = 1075
655383 TA = 187
80015
MA = 187
82358
Ha = 228
230 n
mi
Hp = 221
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5066327
22 X = 1524680
97
Y = 13197022
85 feet Y = 4039611
43 meter
Z = -17261773
12 Z = -5253934
25
XDOT = -21307
309183 XDOT = -6542
793681
YDOT = 12787
199560 feet/sec YDOT = 3824
643012 meter/sec
ZDOT = 3529
053093 ZDOT = 1043
987297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4238034
45 X = -1291752
90
Y = -13525172
55 feet Y = -4122472
59 meter
Z = -17230979
84 Z = -5252002
66
XDOT = 21184
676562 XDOT = 6457
089416
YDOT = -10955
417419 feet/sec YDOT = -3339
211229 meter/sec
ZDOT = 3395
458182 ZDOT = 1034
935654
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 13306
38938304
00016717 00000-0 10270-3 0 9176
2 25544 51
6496 143
6047 0001675 32
1046 328
0206 15
49785047 16146
Satellite: ISS
Catalog Number: 25544
Epoch time: 13306
38938304 = yrday
fracday
Element set: 917
Inclination: 51
6496 deg
RA of node: 143
6047 deg
Eccentricity:
0001675
Arg of perigee: 32
1046 deg
Mean anomaly: 328
0206 deg
Mean motion: 15
49785047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1614
Checksum: 306
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