[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 6th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 ET - UTC (sec) : 68 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
255/21:17:02
000 0
0 0
0 0
0
N/A 0
0 0
0 219
2
000/00:00:00
000 0
0 0
0 216
1
256/02:57:42
000 0
0 0
0 0
0
N/A 0
0 0
0 219
4
000/00:00:00
000 0
0 0
0 216
2
256/23:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
4
000/00:00:00
000 0
0 0
0 216
1
260/08:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 216
1
261/05:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 215
9
Coasting Arc #1 (Orbit 3438)
---------------------------------------
Vector Time (GMT): 2017/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5404197
75 A = 6786228
24 meter
Y = -2979739
23 meter E =
0000354
Z = -2823142
49 I = 51
60598
XDOT = 4566
450749 Wp = 84
10410
YDOT = 3459
263001 meter/sec RA = 352
38298 deg
ZDOT = 5090
765159 TA = 243
83766
MA = 243
84130
Ha = 220
138 n
mi
Hp = 216
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17730307
58 X = 5450829
67
Y = -9776047
36 feet Y = -2919045
39 meter
Z = -9262278
52 Z = -2796777
20
XDOT = 14981
793797 XDOT = 4502
700726
YDOT = 11349
288061 feet/sec YDOT = 3509
972291 meter/sec
ZDOT = 16701
985429 ZDOT = 5112
792148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19722943
21 X = -6011553
09
Y = 4806092
84 feet Y = 1464897
10 meter
Z = -9145036
63 Z = -2787407
16
XDOT = -11052
173224 XDOT = -3368
702399
YDOT = -13393
956232 feet/sec YDOT = -4082
477859 meter/sec
ZDOT = 16798
904165 ZDOT = 5120
305989
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 17249
50565021
00016717 00000-0 10270-3 0 9004
2 25544 51
6430 352
9495 0004420 237
5851 122
4874 15
54061704 34399
Satellite: ISS
Catalog Number: 25544
Epoch time: 17249
50565021 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 352
9495 deg
Eccentricity:
0004420
Arg of perigee: 237
5851 deg
Mean anomaly: 122
4874 deg
Mean motion: 15
54061704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3439
Checksum: 297
Coasting Arc #2 (Orbit 3454)
---------------------------------------
Vector Time (GMT): 2017/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6219429
80 A = 6788848
06 meter
Y = 2399931
45 meter E =
0012328
Z = 1243399
72 I = 51
58264
XDOT = -2766
301012 Wp = 139
70285
YDOT = -4129
841072 meter/sec RA = 347
40620 deg
ZDOT = -5842
556099 TA = 26
76335
MA = 26
69978
Ha = 220
072 n
mi
Hp = 216
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20404953
43 X = -6251844
04
Y = 7873790
84 feet Y = 2330200
45 meter
Z = 4079395
39 Z = 1213108
77
XDOT = -9075
790722 XDOT = -2691
534280
YDOT = -13549
347349 feet/sec YDOT = -4160
358387 meter/sec
ZDOT = -19168
491140 ZDOT = -5855
811784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21734437
31 X = 6624656
49
Y = -2655609
52 feet Y = -809429
78 meter
Z = 3944888
61 Z = 1202402
05
XDOT = 5182
667963 XDOT = 1579
677195
YDOT = 13739
078413 feet/sec YDOT = 4187
671100 meter/sec
ZDOT = -19226
459036 ZDOT = -5860
224714
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 17250
53450818
00016717 00000-0 10270-3 0 9017
2 25544 51
6429 347
8215 0004374 239
3866 120
6855 15
54084090 34554
Satellite: ISS
Catalog Number: 25544
Epoch time: 17250
53450818 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 347
8215 deg
Eccentricity:
0004374
Arg of perigee: 239
3866 deg
Mean anomaly: 120
6855 deg
Mean motion: 15
54084090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3455
Checksum: 315
Coasting Arc #3 (Orbit 3470)
---------------------------------------
Vector Time (GMT): 2017/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6552595
56 A = 6789296
54 meter
Y = -1700116
20 meter E =
0008956
Z = 449725
84 I = 51
55307
XDOT = 811
180853 Wp = 42
48841
YDOT = 4725
943927 meter/sec RA = 342
43156 deg
ZDOT = 5983
391079 TA = 322
36682
MA = 322
42945
Ha = 219
858 n
mi
Hp = 216
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21498016
92 X = 6568935
16
Y = -5577809
06 feet Y = -1626749
20 meter
Z = 1475478
49 Z = 481596
21
XDOT = 2661
354506 XDOT = 729
209415
YDOT = 15505
065376 feet/sec YDOT = 4734
557490 meter/sec
ZDOT = 19630
548158 ZDOT = 5987
131882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22193108
65 X = -6764459
52
Y = 552695
43 feet Y = 168461
57 meter
Z = 1616842
13 Z = 492813
48
XDOT = 1094
977957 XDOT = 333
749281
YDOT = -14058
357406 feet/sec YDOT = -4284
987337 meter/sec
ZDOT = 19646
294307 ZDOT = 5988
190505
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 17251
56335620
00016717 00000-0 10270-3 0 9025
2 25544 51
6432 342
6933 0004221 246
3541 113
7169 15
54104561 34712
Satellite: ISS
Catalog Number: 25544
Epoch time: 17251
56335620 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 342
6933 deg
Eccentricity:
0004221
Arg of perigee: 246
3541 deg
Mean anomaly: 113
7169 deg
Mean motion: 15
54104561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3471
Checksum: 281
Coasting Arc #4 (Orbit 3485)
---------------------------------------
Vector Time (GMT): 2017/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6390868
07 A = 6787387
33 meter
Y = 830390
15 meter E =
0006213
Z = -2117622
37 I = 51
51467
XDOT = 1144
364826 Wp = 177
76475
YDOT = -5213
583251 meter/sec RA = 337
45350 deg
ZDOT = -5504
673315 TA = 25
73850
MA = 25
70759
Ha = 219
681 n
mi
Hp = 216
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20967414
93 X = -6389392
32
Y = 2724377
12 feet Y = 758931
12 meter
Z = -6947579
96 Z = -2148663
87
XDOT = 3754
477776 XDOT = 1229
318570
YDOT = -17104
931927 feet/sec YDOT = -5200
311799 meter/sec
ZDOT = -18059
951822 ZDOT = -5498
907395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21026388
88 X = 6408843
33
Y = 1736586
32 feet Y = 529311
51 meter
Z = -7085112
97 Z = -2159542
43
XDOT = -7256
799664 XDOT = -2211
872538
YDOT = 14376
258622 feet/sec YDOT = 4381
883628 meter/sec
ZDOT = -18033
538636 ZDOT = -5496
622576
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 17252
52789462
00016717 00000-0 10270-3 0 9030
2 25544 51
6418 337
8863 0004295 248
7023 111
3672 15
54115596 34865
Satellite: ISS
Catalog Number: 25544
Epoch time: 17252
52789462 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 337
8863 deg
Eccentricity:
0004295
Arg of perigee: 248
7023 deg
Mean anomaly: 111
3672 deg
Mean motion: 15
54115596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3486
Checksum: 329
Coasting Arc #5 (Orbit 3501)
---------------------------------------
Vector Time (GMT): 2017/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5775389
77 A = 6783805
63 meter
Y = 175862
81 meter E =
0008098
Z = 3549333
85 I = 51
47379
XDOT = -2912
827686 Wp = 102
97568
YDOT = 5519
503406 meter/sec RA = 332
46420 deg
ZDOT = 4455
830953 TA = 299
01804
MA = 299
09916
Ha = 219
506 n
mi
Hp = 216
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18948129
16 X = 5755752
94
Y = 576977
73 feet Y = 240337
71 meter
Z = 11644796
10 Z = 3577341
39
XDOT = -9556
521280 XDOT = -2995
976149
YDOT = 18108
606974 feet/sec YDOT = 5486
465708 meter/sec
ZDOT = 14618
867955 ZDOT = 4441
478741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18403150
18 X = -5609280
17
Y = -4217473
55 feet Y = -1285485
94 meter
Z = 11768719
50 Z = 3587105
70
XDOT = 12665
430286 XDOT = 3860
423151
YDOT = -14558
689715 feet/sec YDOT = -4437
488625 meter/sec
ZDOT = 14554
406439 ZDOT = 4436
183083
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 17253
55672565
00016717 00000-0 10270-3 0 9040
2 25544 51
6422 332
7572 0004305 253
8567 106
2112 15
54151947 35024
Satellite: ISS
Catalog Number: 25544
Epoch time: 17253
55672565 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 332
7572 deg
Eccentricity:
0004305
Arg of perigee: 253
8567 deg
Mean anomaly: 106
2112 deg
Mean motion: 15
54151947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3502
Checksum: 298
Coasting Arc #6 (Orbit 3516)
---------------------------------------
Vector Time (GMT): 2017/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4781766
50 A = 6780130
76 meter
Y = -1325425
84 meter E =
0006349
Z = -4626706
11 I = 51
43199
XDOT = 4377
513183 Wp = 64
27425
YDOT = -5564
546474 meter/sec RA = 327
46325 deg
ZDOT = -2930
573265 TA = 176
44313
MA = 176
43861
Ha = 219
501 n
mi
Hp = 216
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15688210
29 X = -4744115
39
Y = -4348509
97 feet Y = -1378688
66 meter
Z = -15179481
99 Z = -4649843
07
XDOT = 14361
919892 XDOT = 4453
647473
YDOT = -18256
386070 feet/sec YDOT = -5515
168678 meter/sec
ZDOT = -9614
741684 ZDOT = -2909
123138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14575659
06 X = 4442660
88
Y = 7033316
27 feet Y = 2143754
80 meter
Z = -15281648
46 Z = -4657846
45
XDOT = -16908
215870 XDOT = -5153
624197
YDOT = 14361
143301 feet/sec YDOT = 4377
276478 meter/sec
ZDOT = -9518
867223 ZDOT = -2901
350730
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 17254
52124933
00016717 00000-0 10270-3 0 9050
2 25544 51
6414 327
9495 0004242 258
9254 101
1421 15
54131377 35172
Satellite: ISS
Catalog Number: 25544
Epoch time: 17254
52124933 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 327
9495 deg
Eccentricity:
0004242
Arg of perigee: 258
9254 deg
Mean anomaly: 101
1421 deg
Mean motion: 15
54131377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3517
Checksum: 296
Coasting Arc #7 (Orbit 3532)
---------------------------------------
Vector Time (GMT): 2017/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3525923
74 A = 6777592
27 meter
Y = 2532314
74 meter E =
0002753
Z = 5206217
79 I = 51
39687
XDOT = -5436
950732 Wp = 202
17153
YDOT = 5292
570394 meter/sec RA = 322
45122 deg
ZDOT = 1105
561278 TA = 237
18327
MA = 237
20978
Ha = 219
283 n
mi
Hp = 216
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11567991
27 X = 3472055
26
Y = 8308119
22 feet Y = 2571443
14 meter
Z = 17080767
02 Z = 5223214
74
XDOT = -17837
764868 XDOT = -5501
099882
YDOT = 17364
076095 feet/sec YDOT = 5231
412093 meter/sec
ZDOT = 3627
169546 ZDOT = 1078
993963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9982959
72 X = -3042806
12
Y = -10031117
82 feet Y = -3057484
71 meter
Z = 17155554
77 Z = 5229013
09
XDOT = 19671
731436 XDOT = 5995
943742
YDOT = -13563
682132 feet/sec YDOT = -4134
210314 meter/sec
ZDOT = 3508
703376 ZDOT = 1069
452789
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 17255
55006659
00016717 00000-0 10270-3 0 9069
2 25544 51
6414 322
8209 0004235 263
4044 96
6626 15
54175095 35337
Satellite: ISS
Catalog Number: 25544
Epoch time: 17255
55006659 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 322
8209 deg
Eccentricity:
0004235
Arg of perigee: 263
4044 deg
Mean anomaly: 96
6626 deg
Mean motion: 15
54175095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3533
Checksum: 310
Coasting Arc #8 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2017/255/21:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3127069
65 A = 6777239
00 meter
Y = 2884704
73 meter E =
0001902
Z = 5276985
68 I = 51
38495
XDOT = -5636
520230 Wp = 239
00141
YDOT = 5173
271018 meter/sec RA = 320
51368 deg
ZDOT = 511
292138 TA = 206
09823
MA = 206
10782
Ha = 219
248 n
mi
Hp = 216
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10259414
85 X = 3068946
56
Y = 9464254
35 feet Y = 2919349
06 meter
Z = 17312945
15 Z = 5292034
76
XDOT = -18492
520439 XDOT = -5696
433822
YDOT = 16972
673944 feet/sec YDOT = 5109
904639 meter/sec
ZDOT = 1677
467644 ZDOT = 483
765725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -618997
82 X = -188670
53
Y = 13861858
07 feet Y = 4225094
34 meter
Z = 17379053
65 Z = 5297135
55
XDOT = -23909
938202 XDOT = -7287
749164
YDOT = -3020
348417 feet/sec YDOT = -920
602197 meter/sec
ZDOT = 1554
780361 ZDOT = 473
897054
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 17255
93587274
00016717 00000-0 10270-3 0 9079
2 25544 51
6405 320
8996 0004192 269
8732 90
1940 15
54191676 35391
Satellite: ISS
Catalog Number: 25544
Epoch time: 17255
93587274 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 320
8996 deg
Eccentricity:
0004192
Arg of perigee: 269
8732 deg
Mean anomaly: 90
1940 deg
Mean motion: 15
54191676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 344
Coasting Arc #9 (Orbit 3541)
---------------------------------------
Vector Time (GMT): 2017/256/02:57:42
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3039437
70 A = 6786222
51 meter
Y = -5439424
84 meter E =
0002850
Z = -2683951
76 I = 51
40737
XDOT = 5630
507313 Wp = 355
06690
YDOT = 597
393626 meter/sec RA = 319
30199 deg
ZDOT = 5167
928838 TA = 334
52583
MA = 334
53987
Ha = 219
396 n
mi
Hp = 216
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9971908
47 X = 3113074
28
Y = -17845882
03 feet Y = -5405024
19 meter
Z = -8805616
01 Z = -2669007
91
XDOT = 18472
793023 XDOT = 5598
305256
YDOT = 1959
952841 feet/sec YDOT = 660
178015 meter/sec
ZDOT = 16955
147105 ZDOT = 5195
201966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2325300
75 X = -708751
67
Y = -20339217
38 feet Y = -6199393
46 meter
Z = -8738566
82 Z = -2663515
17
XDOT = 14547
148750 XDOT = 4433
970939
YDOT = -8996
185042 feet/sec YDOT = -2742
037201 meter/sec
ZDOT = 17075
736905 ZDOT = 5204
684609
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 17256
12877425
00016717 00000-0 10270-3 0 9082
2 25544 51
6393 319
9361 0004267 269
6657 90
4007 15
54161623 35429
Satellite: ISS
Catalog Number: 25544
Epoch time: 17256
12877425 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 319
9361 deg
Eccentricity:
0004267
Arg of perigee: 269
6657 deg
Mean anomaly: 90
4007 deg
Mean motion: 15
54161623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3542
Checksum: 325
Coasting Arc #10 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2017/256/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2146908
53 A = 6785114
88 meter
Y = -5637067
57 meter E =
0001565
Z = -3105095
81 I = 51
38705
XDOT = 5917
142938 Wp = 7
83602
YDOT = -419
723560 meter/sec RA = 315
12497 deg
ZDOT = 4854
985325 TA = 316
30869
MA = 316
32108
Ha = 219
419 n
mi
Hp = 216
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7043663
15 X = 2224867
20
Y = -18494316
19 feet Y = -5612623
64 meter
Z = -10187322
20 Z = -3094477
16
XDOT = 19413
198614 XDOT = 5897
813463
YDOT = -1377
045800 feet/sec YDOT = -353
661880 meter/sec
ZDOT = 15928
429545 ZDOT = 4883
682069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13708140
74 X = 4178241
30
Y = -14307836
20 feet Y = -4361028
48 meter
Z = -10139386
37 Z = -3090484
97
XDOT = 17295
382894 XDOT = 5271
632706
YDOT = 5196
818302 feet/sec YDOT = 1583
990218 meter/sec
ZDOT = 16055
489321 ZDOT = 4893
713145
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 17256
96468228
00016717 00000-0 10270-3 0 9092
2 25544 51
6428 315
7707 0004131 274
3211 85
7470 15
54184547 35550
Satellite: ISS
Catalog Number: 25544
Epoch time: 17256
96468228 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 315
7707 deg
Eccentricity:
0004131
Arg of perigee: 274
3211 deg
Mean anomaly: 85
7470 deg
Mean motion: 15
54184547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 326
Coasting Arc #11 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2017/257/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3235277
90 A = 6788272
05 meter
Y = 5756906
25 meter E =
0010256
Z = 1548163
02 I = 51
37452
XDOT = -4946
923711 Wp = 125
35469
YDOT = -1233
796320 meter/sec RA = 310
13165 deg
ZDOT = -5728
890248 TA = 37
65785
MA = 37
58609
Ha = 219
539 n
mi
Hp = 216
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10614428
82 X = -3306932
90
Y = 18887487
70 feet Y = 5720326
60 meter
Z = 5079275
00 Z = 1532272
75
XDOT = -16230
064668 XDOT = -4904
931353
YDOT = -4047
888190 feet/sec YDOT = -1288
881704 meter/sec
ZDOT = -18795
571680 ZDOT = -5752
818736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16890763
73 X = -5148304
78
Y = 13595011
95 feet Y = 4143759
64 meter
Z = 5008001
22 Z = 1526438
77
XDOT = -12466
346266 XDOT = -3799
742342
YDOT = -8500
033069 feet/sec YDOT = -2590
810079 meter/sec
ZDOT = -18901
254946 ZDOT = -5761
102508
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 17257
99348527
00016717 00000-0 10270-3 0 9107
2 25544 51
6424 310
6425 0003983 277
5628 82
5072 15
54152782 35715
Satellite: ISS
Catalog Number: 25544
Epoch time: 17257
99348527 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 310
6425 deg
Eccentricity:
0003983
Arg of perigee: 277
5628 deg
Mean anomaly: 82
5072 deg
Mean motion: 15
54152782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 326
Coasting Arc #12 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2017/258/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4005457
87 A = 6789122
79 meter
Y = -5471334
95 meter E =
0010674
Z = 157698
83 I = 51
35715
XDOT = 3781
174916 Wp = 28
09758
YDOT = 2945
213174 meter/sec RA = 305
14171 deg
ZDOT = 5987
695653 TA = 333
60825
MA = 333
66258
Ha = 219
471 n
mi
Hp = 216
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13141265
98 X = 4065576
08
Y = -17950574
00 feet Y = -5426207
04 meter
Z = 517384
63 Z = 177302
38
XDOT = 12405
429515 XDOT = 3718
874623
YDOT = 9662
772880 feet/sec YDOT = 2987
148915 meter/sec
ZDOT = 19644
670776 ZDOT = 6005
911797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18650146
22 X = 5684564
57
Y = -12123928
77 feet Y = -3695373
49 meter
Z = 605030
79 Z = 184413
39
XDOT = 7166
404989 XDOT = 2184
320241
YDOT = 12030
261290 feet/sec YDOT = 3666
823641 meter/sec
ZDOT = 19724
797454 ZDOT = 6012
118264
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 17259
02228070
00016717 00000-0 10270-3 0 9114
2 25544 51
6420 305
5135 0004179 283
2730 76
7957 15
54195378 35870
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
02228070 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 305
5135 deg
Eccentricity:
0004179
Arg of perigee: 283
2730 deg
Mean anomaly: 76
7957 deg
Mean motion: 15
54195378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 318
Coasting Arc #13 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2017/259/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4480940
08 A = 6787691
07 meter
Y = 4740554
74 meter E =
0004398
Z = -1866656
71 I = 51
33440
XDOT = -2520
248885 Wp = 175
40846
YDOT = -4586
168403 meter/sec RA = 300
15069 deg
ZDOT = -5602
338666 TA = 25
22256
MA = 25
20109
Ha = 219
523 n
mi
Hp = 216
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14701246
99 X = -4524549
96
Y = 15553001
12 feet Y = 4690201
81 meter
Z = -6124201
82 Z = -1888529
91
XDOT = -8268
533087 XDOT = -2441
564605
YDOT = -15046
484261 feet/sec YDOT = -4613
912088 meter/sec
ZDOT = -18380
376200 ZDOT = -5614
389647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19060240
92 X = -5809561
43
Y = 9670847
07 feet Y = 2947674
19 meter
Z = -6221759
21 Z = -1896392
21
XDOT = -1867
112903 XDOT = -569
096013
YDOT = -15527
924450 feet/sec YDOT = -4732
911372 meter/sec
ZDOT = -18432
962607 ZDOT = -5618
367002
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 17259
98677334
00016717 00000-0 10270-3 0 9121
2 25544 51
6422 300
7060 0004266 284
8868 75
1812 15
54166698 36026
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
98677334 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 300
7060 deg
Eccentricity:
0004266
Arg of perigee: 284
8868 deg
Mean anomaly: 75
1812 deg
Mean motion: 15
54166698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 331
Coasting Arc #14 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2017/260/08:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 286456
50 A = 6784818
58 meter
Y = -5976976
01 meter E =
0001809
Z = -3196348
12 I = 51
31775
XDOT = 5547
472029 Wp = 12
35307
YDOT = -2284
689501 meter/sec RA = 298
06394 deg
ZDOT = 4771
631136 TA = 310
52119
MA = 310
53694
Ha = 219
469 n
mi
Hp = 216
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 939817
93 X = 368797
53
Y = -19609501
35 feet Y = -5973312
57 meter
Z = -10486706
42 Z = -3194756
04
XDOT = 18200
367549 XDOT = 5549
429658
YDOT = -7495
700462 feet/sec YDOT = -2222
642478 meter/sec
ZDOT = 15654
957794 ZDOT = 4798
583812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16198374
31 X = -4937264
49
Y = 11099381
95 feet Y = 3383091
62 meter
Z = -10478702
33 Z = -3193908
47
XDOT = -16129
926225 XDOT = -4916
401513
YDOT = -8654
381703 feet/sec YDOT = -2637
855543 meter/sec
ZDOT = 15774
592674 ZDOT = 4808
095847
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 17260
37256764
00016717 00000-0 10270-3 0 9137
2 25544 51
6417 298
7790 0004192 282
8018 77
2666 15
54191620 36088
Satellite: ISS
Catalog Number: 25544
Epoch time: 17260
37256764 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 298
7790 deg
Eccentricity:
0004192
Arg of perigee: 282
8018 deg
Mean anomaly: 77
2666 deg
Mean motion: 15
54191620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 329
Coasting Arc #15 (Orbit 3620)
---------------------------------------
Vector Time (GMT): 2017/261/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2685407
05 A = 6789091
83 meter
Y = -6227886
39 meter E =
0010668
Z = -79974
59 I = 51
31806
XDOT = 4428
509993 Wp = 26
39987
YDOT = 1836
735919 meter/sec RA = 293
86619 deg
ZDOT = 5986
493373 TA = 332
73467
MA = 332
79063
Ha = 219
590 n
mi
Hp = 215
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8810390
59 X = 2755237
82
Y = -20432698
12 feet Y = -6197465
89 meter
Z = -262383
82 Z = -66759
48
XDOT = 14529
232260 XDOT = 4378
562711
YDOT = 6026
036479 feet/sec YDOT = 1885
979944 meter/sec
ZDOT = 19640
726290 ZDOT = 6007
884048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16566236
65 X = -5049388
93
Y = -14856163
92 feet Y = -4528158
76 meter
Z = -202920
99 Z = -61850
32
XDOT = 9213
551217 XDOT = 2808
290411
YDOT = -10525
271050 feet/sec YDOT = -3208
102616 meter/sec
ZDOT = 19735
089817 ZDOT = 6015
255376
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 17261
20845522
00016717 00000-0 10270-3 0 9147
2 25544 51
6399 294
6092 0003853 286
0122 74
0606 15
54209480 36210
Satellite: ISS
Catalog Number: 25544
Epoch time: 17261
20845522 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 294
6092 deg
Eccentricity:
0003853
Arg of perigee: 286
0122 deg
Mean anomaly: 74
0606 deg
Mean motion: 15
54209480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3621
Checksum: 301
Coasting Arc #16 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2017/262/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3335632
34 A = 6787853
22 meter
Y = 5673673
39 meter E =
0004913
Z = -1649021
07 I = 51
30063
XDOT = -3538
740289 Wp = 166
80331
YDOT = -3730
742792 meter/sec RA = 288
87251 deg
ZDOT = -5686
020216 TA = 31
34115
MA = 31
31187
Ha = 219
629 n
mi
Hp = 215
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10943675
65 X = -3390818
84
Y = 18614414
00 feet Y = 5636063
29 meter
Z = -5410174
13 Z = -1665359
26
XDOT = -11610
040317 XDOT = -3469
139307
YDOT = -12239
969789 feet/sec YDOT = -3769
926973 meter/sec
ZDOT = -18654
921967 ZDOT = -5703
040731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14452683
67 X = 4405177
98
Y = 16018214
84 feet Y = 4882351
88 meter
Z = -5483352
76 Z = -1671325
92
XDOT = -13970
140999 XDOT = -4258
098976
YDOT = 6202
173598 feet/sec YDOT = 1890
422513 meter/sec
ZDOT = -18729
655170 ZDOT = -5708
798896
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 17262
23723360
00016717 00000-0 10270-3 0 9157
2 25544 51
6386 289
4802 0003898 290
0815 69
9918 15
54227913 36377
Satellite: ISS
Catalog Number: 25544
Epoch time: 17262
23723360 = yrday
fracday
Element set: 915
Inclination: 51
6386 deg
RA of node: 289
4802 deg
Eccentricity:
0003898
Arg of perigee: 290
0815 deg
Mean anomaly: 69
9918 deg
Mean motion: 15
54227913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 338
Coasting Arc #17 (Orbit 3652)
---------------------------------------
Vector Time (GMT): 2017/263/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3775703
19 A = 6784584
83 meter
Y = -4644717
71 meter E =
0009376
Z = 3183422
54 I = 51
28159
XDOT = 2610
772678 Wp = 76
01308
YDOT = 5403
334442 meter/sec RA = 283
87104 deg
ZDOT = 4777
496549 TA = 320
98715
MA = 321
05474
Ha = 219
517 n
mi
Hp = 215
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12387477
66 X = 3811897
52
Y = -15238575
17 feet Y = -4602292
40 meter
Z = 10444299
68 Z = 3201852
31
XDOT = 8565
527159 XDOT = 2526
950356
YDOT = 17727
475204 feet/sec YDOT = 5432
061871 meter/sec
ZDOT = 15674
201276 ZDOT = 4789
974537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11087607
95 X = -3379502
90
Y = -16155607
54 feet Y = -4924229
18 meter
Z = 10526560
07 Z = 3208495
51
XDOT = 18228
634473 XDOT = 5556
087787
YDOT = -2241
570138 feet/sec YDOT = -683
230578 meter/sec
ZDOT = 15728
584844 ZDOT = 4794
072660
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 17263
26600496
00016717 00000-0 10270-3 0 9166
2 25544 51
6398 284
3507 0003965 292
0088 68
0644 15
54258571 36533
Satellite: ISS
Catalog Number: 25544
Epoch time: 17263
26600496 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 284
3507 deg
Eccentricity:
0003965
Arg of perigee: 292
0088 deg
Mean anomaly: 68
0644 deg
Mean motion: 15
54258571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3653
Checksum: 333
Coasting Arc #18 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2017/264/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4063369
38 A = 6780783
13 meter
Y = 3203680
04 meter E =
0007104
Z = -4389602
15 I = 51
26201
XDOT = -1667
583072 Wp = 44
91643
YDOT = -6691
498875 meter/sec RA = 278
85903 deg
ZDOT = -3338
409565 TA = 191
11588
MA = 191
13159
Ha = 219
808 n
mi
Hp = 215
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13331264
36 X = -4077569
13
Y = 10510761
28 feet Y = 3158160
65 meter
Z = -14401581
87 Z = -4409375
79
XDOT = -5471
073070 XDOT = -1576
416569
YDOT = -21953
736468 feet/sec YDOT = -6709
637658 meter/sec
ZDOT = -10952
787286 ZDOT = -3346
287827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6563076
06 X = 2000425
58
Y = 15575075
84 feet Y = 4747283
12 meter
Z = -14489558
92 Z = -4416417
56
XDOT = -21462
073050 XDOT = -6541
639866
YDOT = -1182
078065 feet/sec YDOT = -360
297394 meter/sec
ZDOT = -10986
633571 ZDOT = -3348
725912
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 17264
23047472
00016717 00000-0 10270-3 0 9174
2 25544 51
6401 279
5424 0003937 297
8406 62
2347 15
54226925 36688
Satellite: ISS
Catalog Number: 25544
Epoch time: 17264
23047472 = yrday
fracday
Element set: 917
Inclination: 51
6401 deg
RA of node: 279
5424 deg
Eccentricity:
0003937
Arg of perigee: 297
8406 deg
Mean anomaly: 62
2347 deg
Mean motion: 15
54226925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 326
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