[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 13th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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
256/23:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
3
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
261/05:32:00
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
269/21:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
3
270/16:51:48
829 -0
9 1
4 1
4
N/A -0
9 0
0 220
7
000/00:03:37
658 -0
6 0
0 215
8
Coasting Arc #1 (Orbit 3548)
---------------------------------------
Vector Time (GMT): 2017/256/13:53:07
209
Vector Time (MET): N/A
Weight (LBS) : 924173
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4878624
46 A = 6789250
83 meter
Y = -4710642
22 meter E =
0009718
Z = -154432
91 I = 51
40799
XDOT = 3419
237363 Wp = 26
51585
YDOT = 3349
805940 meter/sec RA = 317
04491 deg
ZDOT = 5991
565274 TA = 331
81504
MA = 331
86760
Ha = 219
531 n
mi
Hp = 216
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16005985
75 X = 4931687
68
Y = -15454862
94 feet Y = -4655789
43 meter
Z = -506669
64 Z = -130604
89
XDOT = 11217
970350 XDOT = 3352
420658
YDOT = 10990
176968 feet/sec YDOT = 3387
668881 meter/sec
ZDOT = 19657
366386 ZDOT = 6008
012458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9701450
06 X = -2957001
98
Y = 20025548
76 feet Y = 6103787
26 meter
Z = -400431
99 Z = -122051
67
XDOT = -12737
529170 XDOT = -3882
398891
YDOT = -5789
051940 feet/sec YDOT = -1764
503031 meter/sec
ZDOT = 19729
585012 ZDOT = 6013
577512
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
57879341
00016717 00000-0 10270-3 0 9002
2 25544 51
6411 317
6917 0003931 272
9702 87
1001 15
54152897 35494
Satellite: ISS
Catalog Number: 25544
Epoch time: 17256
57879341 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 317
6917 deg
Eccentricity:
0003931
Arg of perigee: 272
9702 deg
Mean anomaly: 87
1001 deg
Mean motion: 15
54152897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3549
Checksum: 320
Coasting Arc #2 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2017/256/23:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 924173
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5079949
95 A = 6780528
74 meter
Y = 914
30 meter E =
0005079
Z = 4489074
07 I = 51
37153
XDOT = -2812
741082 Wp = 125
45401
YDOT = 6388
190167 meter/sec RA = 315
08735 deg
ZDOT = 3176
234888 TA = 292
50153
MA = 292
55529
Ha = 219
318 n
mi
Hp = 216
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16666502
46 X = 5057756
43
Y = 2999
67 feet Y = 57597
89 meter
Z = 14727933
29 Z = 4513697
00
XDOT = -9228
153155 XDOT = -2899
395078
YDOT = 20958
629157 feet/sec YDOT = 6356
251820 meter/sec
ZDOT = 10420
718135 ZDOT = 3162
360676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15867126
76 X = 4836300
24
Y = 4773380
82 feet Y = 1454926
47 meter
Z = 14836895
09 Z = 4522285
62
XDOT = -14587
685306 XDOT = -4446
326481
YDOT = 16239
613671 feet/sec YDOT = 4949
834247 meter/sec
ZDOT = 10358
249746 ZDOT = 3157
194523
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
02889364
00016717 00000-0 10270-3 0 9010
2 25544 51
6430 315
4493 0004075 275
9918 84
0770 15
54171015 35562
Satellite: ISS
Catalog Number: 25544
Epoch time: 17257
02889364 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 315
4493 deg
Eccentricity:
0004075
Arg of perigee: 275
9918 deg
Mean anomaly: 84
0770 deg
Mean motion: 15
54171015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 316
Coasting Arc #3 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2017/257/23:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 924173
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4155152
37 A = 6777711
48 meter
Y = -1470514
74 meter E =
0010189
Z = -5157794
97 I = 51
33956
XDOT = 3965
412586 Wp = 71
02477
YDOT = -6411
065703 meter/sec RA = 310
07153 deg
ZDOT = -1365
698879 TA = 185
77273
MA = 185
78448
Ha = 219
432 n
mi
Hp = 215
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13632389
65 X = -4113345
90
Y = -4824523
41 feet Y = -1516747
00 meter
Z = -16921899
51 Z = -5177877
73
XDOT = 13009
883813 XDOT = 4043
441984
YDOT = -21033
680128 feet/sec YDOT = -6366
285541 meter/sec
ZDOT = -4480
639368 ZDOT = -1346
246333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11704571
21 X = -3567553
31
Y = -8313470
44 feet Y = -2533945
79 meter
Z = -17010525
52 Z = -5184808
18
XDOT = 17650
621595 XDOT = 5379
909462
YDOT = -15853
780134 feet/sec YDOT = -4832
232185 meter/sec
ZDOT = -4393
493349 ZDOT = -1339
136773
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
99338870
00016717 00000-0 10270-3 0 9028
2 25544 51
6425 310
6411 0004146 280
9775 79
0912 15
54209756 35712
Satellite: ISS
Catalog Number: 25544
Epoch time: 17257
99338870 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 310
6411 deg
Eccentricity:
0004146
Arg of perigee: 280
9775 deg
Mean anomaly: 79
0912 deg
Mean motion: 15
54209756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 324
Coasting Arc #4 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2017/258/23:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 924173
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3068501
27 A = 6777221
73 meter
Y = 2967041
19 meter E =
0002618
Z = 5265625
89 I = 51
31714
XDOT = -4767
408838 Wp = 326
69053
YDOT = 5976
785561 meter/sec RA = 305
04983 deg
ZDOT = -587
582061 TA = 128
95468
MA = 128
93135
Ha = 219
347 n
mi
Hp = 216
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10067261
38 X = 3009517
30
Y = 9734387
12 feet Y = 3001025
83 meter
Z = 17275675
50 Z = 5280388
16
XDOT = -15641
105113 XDOT = -4831
034352
YDOT = 19608
876511 feet/sec YDOT = 5923
117353 meter/sec
ZDOT = -1927
762666 ZDOT = -610
895455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7145471
53 X = 2177939
72
Y = 11950137
64 feet Y = 3642401
95 meter
Z = 17340514
86 Z = 5285388
93
XDOT = -19236
012125 XDOT = -5863
136496
YDOT = 14459
968223 feet/sec YDOT = 4407
398314 meter/sec
ZDOT = -2031
908196 ZDOT = -619
325618
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
02218116
00016717 00000-0 10270-3 0 9035
2 25544 51
6420 305
5126 0004198 283
5006 76
5679 15
54215637 35870
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
02218116 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 305
5126 deg
Eccentricity:
0004198
Arg of perigee: 283
5006 deg
Mean anomaly: 76
5679 deg
Mean motion: 15
54215637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 309
Coasting Arc #5 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2017/259/23:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 924173
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1937693
84 A = 6779191
58 meter
Y = -4362947
50 meter E =
0007325
Z = -4820201
36 I = 51
30550
XDOT = 5207
267676 Wp = 107
61238
YDOT = -5046
614205 meter/sec RA = 300
02822 deg
ZDOT = 2475
530859 TA = 186
83515
MA = 186
84515
Ha = 219
498 n
mi
Hp = 215
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6357263
25 X = -1865348
18
Y = -14314132
22 feet Y = -4384212
03 meter
Z = -15814308
92 Z = -4829437
90
XDOT = 17084
211534 XDOT = 5251
288416
YDOT = -16557
133219 feet/sec YDOT = -4988
136633 meter/sec
ZDOT = 8121
820405 ZDOT = 2500
933329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2665818
57 X = -812541
50
Y = -15392546
91 feet Y = -4691648
30 meter
Z = -15854477
44 Z = -4832444
72
XDOT = 19359
860020 XDOT = 5900
885334
YDOT = -11831
920260 feet/sec YDOT = -3606
369295 meter/sec
ZDOT = 8235
044424 ZDOT = 2510
041541
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
98667185
00016717 00000-0 10270-3 0 9045
2 25544 51
6418 300
7041 0004282 287
9485 72
1201 15
54212870 36020
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
98667185 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 300
7041 deg
Eccentricity:
0004282
Arg of perigee: 287
9485 deg
Mean anomaly: 72
1201 deg
Mean motion: 15
54212870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 309
Coasting Arc #6 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2017/260/08:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 334605
01 A = 6784934
19 meter
Y = -5996552
32 meter E =
0002037
Z = -3154625
28 I = 51
31812
XDOT = 5544
002431 Wp = 9
26082
YDOT = -2218
253614 meter/sec RA = 298
06225 deg
ZDOT = 4807
075284 TA = 314
17741
MA = 314
19415
Ha = 219
484 n
mi
Hp = 216
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1097785
47 X = 416958
70
Y = -19673728
08 feet Y = -5992350
38 meter
Z = -10349820
49 Z = -3152799
29
XDOT = 18188
984353 XDOT = 5545
045245
YDOT = -7277
734954 feet/sec YDOT = -2156
250503 meter/sec
ZDOT = 15771
244369 ZDOT = 4834
008878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16344731
96 X = -4981874
30
Y = 11013516
17 feet Y = 3356919
73 meter
Z = -10340778
13 Z = -3151869
17
XDOT = -15955
570441 XDOT = -4863
257871
YDOT = -8766
338949 feet/sec YDOT = -2671
980112 meter/sec
ZDOT = 15890
784143 ZDOT = 4843
511007
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
37246678
00016717 00000-0 10270-3 0 9051
2 25544 51
6418 298
7780 0004208 283
8836 76
1849 15
54190696 36088
Satellite: ISS
Catalog Number: 25544
Epoch time: 17260
37246678 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 298
7780 deg
Eccentricity:
0004208
Arg of perigee: 283
8836 deg
Mean anomaly: 76
1849 deg
Mean motion: 15
54190696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 353
Coasting Arc #7 (Orbit 3621)
---------------------------------------
Vector Time (GMT): 2017/261/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1674692
28 A = 6781029
48 meter
Y = 4901601
81 meter E =
0006719
Z = 4374257
75 I = 51
29043
XDOT = -5019
613833 Wp = 51
06248
YDOT = 4722
517128 meter/sec RA = 293
73005 deg
ZDOT = -3362
435563 TA = 73
16283
MA = 73
08914
Ha = 219
622 n
mi
Hp = 215
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5494397
25 X = 1598508
93
Y = 16081370
77 feet Y = 4919903
89 meter
Z = 14351239
33 Z = 4382207
24
XDOT = -16468
549320 XDOT = -5055
716241
YDOT = 15493
822599 feet/sec YDOT = 4666
182139 meter/sec
ZDOT = -11031
612741 ZDOT = -3386
907367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16798766
31 X = 5120263
97
Y = -2368913
56 feet Y = -722044
85 meter
Z = 14385640
63 Z = 4384743
26
XDOT = 12061
531992 XDOT = 3676
354951
YDOT = 17726
969342 feet/sec YDOT = 5403
180255 meter/sec
ZDOT = -11140
648120 ZDOT = -3395
669547
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
27265467
00016717 00000-0 10270-3 0 9069
2 25544 51
6399 294
2877 0003838 286
4076 73
6654 15
54178031 36228
Satellite: ISS
Catalog Number: 25544
Epoch time: 17261
27265467 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 294
2877 deg
Eccentricity:
0003838
Arg of perigee: 286
4076 deg
Mean anomaly: 73
6654 deg
Mean motion: 15
54178031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3622
Checksum: 341
Coasting Arc #8 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2017/262/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -677118
51 A = 6784835
76 meter
Y = -5951973
72 meter E =
0002426
Z = -3183794
81 I = 51
29075
XDOT = 5107
268819 Wp = 17
54779
YDOT = -3136
063277 meter/sec RA = 288
71999 deg
ZDOT = 4779
771584 TA = 305
47945
MA = 305
50208
Ha = 219
670 n
mi
Hp = 215
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2221517
42 X = -595046
36
Y = -19527472
83 feet Y = -5959087
24 meter
Z = -10445521
02 Z = -3186883
92
XDOT = 16756
131297 XDOT = 5118
739810
YDOT = -10288
921511 feet/sec YDOT = -3078
885554 meter/sec
ZDOT = 15681
665302 ZDOT = 4804
609304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19614914
91 X = -5978626
06
Y = -1116280
35 feet Y = -340242
25 meter
Z = -10458263
51 Z = -3187678
72
XDOT = -7464
056217 XDOT = -2275
044335
YDOT = -16698
412983 feet/sec YDOT = -5089
676277 meter/sec
ZDOT = 15792
058085 ZDOT = 4813
419304
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
23713588
00016717 00000-0 10270-3 0 9079
2 25544 51
6396 289
4797 0004006 291
2219 68
8505 15
54191378 36379
Satellite: ISS
Catalog Number: 25544
Epoch time: 17262
23713588 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 289
4797 deg
Eccentricity:
0004006
Arg of perigee: 291
2219 deg
Mean anomaly: 68
8505 deg
Mean motion: 15
54191378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 342
Coasting Arc #9 (Orbit 3652)
---------------------------------------
Vector Time (GMT): 2017/263/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -261048
06 A = 6787977
54 meter
Y = 6579064
47 meter E =
0009974
Z = 1630519
94 I = 51
29206
XDOT = -4992
558311 Wp = 117
76372
YDOT = 1218
024186 meter/sec RA = 283
71875 deg
ZDOT = -5691
774625 TA = 44
29500
MA = 44
21522
Ha = 219
727 n
mi
Hp = 215
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -856456
89 X = -342517
78
Y = 21584857
18 feet Y = 6575689
95 meter
Z = 5349474
88 Z = 1629053
05
XDOT = -16379
784485 XDOT = -4978
159642
YDOT = 3996
142343 feet/sec YDOT = 1162
273705 meter/sec
ZDOT = -18673
801262 ZDOT = -5715
992145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21211938
57 X = 6465398
88
Y = 4095536
71 feet Y = 1248319
59 meter
Z = 5341975
35 Z = 1628234
09
XDOT = 1828
136854 XDOT = 557
216113
YDOT = 15123
731895 feet/sec YDOT = 4609
713482 meter/sec
ZDOT = -18781
145358 ZDOT = -5724
493105
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
26591320
00016717 00000-0 10270-3 0 9082
2 25544 51
6398 284
3503 0003960 293
4649 66
6087 15
54207164 36539
Satellite: ISS
Catalog Number: 25544
Epoch time: 17263
26591320 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 284
3503 deg
Eccentricity:
0003960
Arg of perigee: 293
4649 deg
Mean anomaly: 66
6087 deg
Mean motion: 15
54207164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3653
Checksum: 325
Coasting Arc #10 (Orbit 3668)
---------------------------------------
Vector Time (GMT): 2017/264/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1092683
68 A = 6789068
38 meter
Y = -6692788
75 meter E =
0011844
Z = 81122
34 I = 51
29002
XDOT = 4722
427649 Wp = 27
60813
YDOT = 847
672965 meter/sec RA = 278
72315 deg
ZDOT = 5984
700117 TA = 333
27020
MA = 333
33120
Ha = 219
865 n
mi
Hp = 215
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3584920
21 X = 1167048
96
Y = -21957968
35 feet Y = -6680153
80 meter
Z = 266149
42 Z = 86611
86
XDOT = 15493
529031 XDOT = 4683
526867
YDOT = 2781
079282 feet/sec YDOT = 900
265715 meter/sec
ZDOT = 19634
842902 ZDOT = 6007
545719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21293722
62 X = -6490326
66
Y = -6447270
38 feet Y = -1965128
01 meter
Z = 291451
28 Z = 88834
35
XDOT = 4314
267980 XDOT = 1314
988880
YDOT = -13310
566051 feet/sec YDOT = -4057
060532 meter/sec
ZDOT = 19735
799284 ZDOT = 6015
471622
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
29468595
00016717 00000-0 10270-3 0 9094
2 25544 51
6407 279
2209 0003939 301
0178 59
0588 15
54218175 36698
Satellite: ISS
Catalog Number: 25544
Epoch time: 17264
29468595 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 279
2209 deg
Eccentricity:
0003939
Arg of perigee: 301
0178 deg
Mean anomaly: 59
0588 deg
Mean motion: 15
54218175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3669
Checksum: 346
Coasting Arc #11 (Orbit 3683)
---------------------------------------
Vector Time (GMT): 2017/265/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1859450
27 A = 6787634
38 meter
Y = 6271051
46 meter E =
0003780
Z = -1805955
57 I = 51
28074
XDOT = -4328
170239 Wp = 160
40785
YDOT = -2900
549557 meter/sec RA = 273
72739 deg
ZDOT = -5622
503026 TA = 39
53683
MA = 39
50927
Ha = 219
936 n
mi
Hp = 215
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6100558
62 X = -1920664
11
Y = 20574315
83 feet Y = 6249915
31 meter
Z = -5925051
09 Z = -1815137
82
XDOT = -14200
033591 XDOT = -4268
102230
YDOT = -9516
238704 feet/sec YDOT = -2948
615012 meter/sec
ZDOT = -18446
532238 ZDOT = -5643
381831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19741994
09 X = 6017359
80
Y = 8383237
73 feet Y = 2555210
86 meter
Z = -5966616
47 Z = -1818624
70
XDOT = -10459
670650 XDOT = -3188
107614
YDOT = 11453
503144 feet/sec YDOT = 3491
027758 meter/sec
ZDOT = -18538
479832 ZDOT = -5650
528653
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 17265
25915699
00016717 00000-0 10270-3 0 9105
2 25544 51
6401 274
4126 0003929 303
1553 56
9223 15
54228122 36848
Satellite: ISS
Catalog Number: 25544
Epoch time: 17265
25915699 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 274
4126 deg
Eccentricity:
0003929
Arg of perigee: 303
1553 deg
Mean anomaly: 56
9223 deg
Mean motion: 15
54228122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3684
Checksum: 307
Coasting Arc #12 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2017/266/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2541896
86 A = 6784242
29 meter
Y = -5337659
35 meter E =
0009787
Z = 3316744
56 I = 51
26944
XDOT = 3842
740701 Wp = 74
38835
YDOT = 4730
415368 meter/sec RA = 268
72410 deg
ZDOT = 4658
764997 TA = 324
45574
MA = 324
52089
Ha = 219
903 n
mi
Hp = 215
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8339556
62 X = 2585283
76
Y = -17512005
73 feet Y = -5308991
12 meter
Z = 10881707
88 Z = 3329198
49
XDOT = 12607
416997 XDOT = 3766
928072
YDOT = 15519
735460 feet/sec YDOT = 4772
964196 meter/sec
ZDOT = 15284
662064 ZDOT = 4677
247334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16619662
00 X = -5065672
98
Y = -9939105
99 feet Y = -3029439
50 meter
Z = 10937601
34 Z = 3333780
89
XDOT = 15943
771548 XDOT = 4859
661568
YDOT = -9718
937279 feet/sec YDOT = -2962
332083 meter/sec
ZDOT = 15365
740669 ZDOT = 4683
477756
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 17266
28792195
00016717 00000-0 10270-3 0 9114
2 25544 51
6409 269
2833 0003922 306
9225 53
1568 15
54256376 37005
Satellite: ISS
Catalog Number: 25544
Epoch time: 17266
28792195 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 269
2833 deg
Eccentricity:
0003922
Arg of perigee: 306
9225 deg
Mean anomaly: 53
1568 deg
Mean motion: 15
54256376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 323
Coasting Arc #13 (Orbit 3714)
---------------------------------------
Vector Time (GMT): 2017/267/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3180539
28 A = 6780453
37 meter
Y = 3978997
93 meter E =
0008424
Z = -4483494
29 I = 51
25847
XDOT = -3242
948487 Wp = 44
65605
YDOT = -6172
055752 meter/sec RA = 263
71063 deg
ZDOT = -3174
808224 TA = 193
23853
MA = 193
26065
Ha = 220
141 n
mi
Hp = 215
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10434840
16 X = -3203018
20
Y = 13054455
15 feet Y = 3943304
80 meter
Z = -14709626
94 Z = -4498999
60
XDOT = -10639
594775 XDOT = -3158
268029
YDOT = -20249
526744 feet/sec YDOT = -6207
847480 meter/sec
ZDOT = -10416
037479 ZDOT = -3190
355321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12178028
85 X = 3711863
19
Y = 11356056
37 feet Y = 3461325
98 meter
Z = -14778816
26 Z = -4504583
20
XDOT = -20208
033857 XDOT = -6159
408720
YDOT = 8017
391998 feet/sec YDOT = 2443
701081 meter/sec
ZDOT = -10483
926373 ZDOT = -3195
500758
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 17267
25238650
00016717 00000-0 10270-3 0 9124
2 25544 51
6412 264
4751 0004056 310
8604 49
2197 15
54226585 37158
Satellite: ISS
Catalog Number: 25544
Epoch time: 17267
25238650 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 264
4751 deg
Eccentricity:
0004056
Arg of perigee: 310
8604 deg
Mean anomaly: 49
2197 deg
Mean motion: 15
54226585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3715
Checksum: 306
Coasting Arc #14 (Orbit 3730)
---------------------------------------
Vector Time (GMT): 2017/268/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3751130
80 A = 6777545
70 meter
Y = -2312073
58 meter E =
0000882
Z = 5148850
25 I = 51
25403
XDOT = 2529
231398 Wp = 61
33099
YDOT = 7113
203790 meter/sec RA = 258
68734 deg
ZDOT = 1351
759188 TA = 15
60971
MA = 15
60699
Ha = 220
068 n
mi
Hp = 215
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12306859
58 X = 3751695
31
Y = -7585543
23 feet Y = -2270122
23 meter
Z = 16892553
30 Z = 5167073
91
XDOT = 8298
003274 XDOT = 2442
935411
YDOT = 23337
282776 feet/sec YDOT = 7141
004998 meter/sec
ZDOT = 4434
905473 ZDOT = 1363
835301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6795702
28 X = -2071330
06
Y = -12652092
55 feet Y = -3856357
81 meter
Z = 16973526
46 Z = 5173530
86
XDOT = 22892
319452 XDOT = 6977
578969
YDOT = -6276
998316 feet/sec YDOT = -1913
229087 meter/sec
ZDOT = 4487
311165 ZDOT = 1367
732443
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 17268
28114284
00016717 00000-0 10270-3 0 9135
2 25544 51
6414 259
3460 0004083 316
2384 43
8445 15
54272619 37318
Satellite: ISS
Catalog Number: 25544
Epoch time: 17268
28114284 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 259
3460 deg
Eccentricity:
0004083
Arg of perigee: 316
2384 deg
Mean anomaly: 43
8445 deg
Mean motion: 15
54272619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3731
Checksum: 307
Coasting Arc #15 (Orbit 3745)
---------------------------------------
Vector Time (GMT): 2017/269/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4250183
30 A = 6777128
20 meter
Y = 514805
96 meter E =
0012160
Z = -5263864
12 I = 51
25891
XDOT = -1666
221677 Wp = 80
79928
YDOT = -7450
988781 meter/sec RA = 253
66033 deg
ZDOT = 619
783715 TA = 195
13671
MA = 195
17313
Ha = 220
335 n
mi
Hp = 215
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13944170
95 X = -4230054
53
Y = 1688995
94 feet Y = 467389
62 meter
Z = -17269895
42 Z = -5284461
60
XDOT = -5466
606551 XDOT = -1585
789543
YDOT = -24445
501251 feet/sec YDOT = -7469
171834 meter/sec
ZDOT = 2033
411139 ZDOT = 611
885603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1046487
65 X = 318969
43
Y = 13893825
79 feet Y = 4234838
10 meter
Z = -17361116
52 Z = -5291668
32
XDOT = -23659
342756 XDOT = -7211
367672
YDOT = 4267
751684 feet/sec YDOT = 1300
810713 meter/sec
ZDOT = 1999
528207 ZDOT = 609
456198
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 17269
24560060
00016717 00000-0 10270-3 0 9140
2 25544 51
6405 254
5383 0004129 320
3556 39
7295 15
54248336 37469
Satellite: ISS
Catalog Number: 25544
Epoch time: 17269
24560060 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 254
5383 deg
Eccentricity:
0004129
Arg of perigee: 320
3556 deg
Mean anomaly: 39
7295 deg
Mean motion: 15
54248336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3746
Checksum: 313
Coasting Arc #16 (Orbit 3756)
---------------------------------------
Vector Time (GMT): 2017/269/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4309112
04 A = 6777330
85 meter
Y = -382327
99 meter E =
0005463
Z = 5217387
50 I = 51
26434
XDOT = 1827
743208 Wp = 5
21842
YDOT = 7385
212860 meter/sec RA = 250
27203 deg
ZDOT = -962
944257 TA = 94
07634
MA = 94
01390
Ha = 220
410 n
mi
Hp = 215
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14137506
71 X = 4287723
27
Y = -1254356
93 feet Y = -334259
75 meter
Z = 17117413
07 Z = 5238268
15
XDOT = 5996
532836 XDOT = 1749
701516
YDOT = 24229
700985 feet/sec YDOT = 7405
215499 meter/sec
ZDOT = -3159
265936 ZDOT = -954
255669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12900331
92 X = 3932021
17
Y = 5643587
31 feet Y = 1720165
41 meter
Z = 17209872
05 Z = 5245569
00
XDOT = -5960
135895 XDOT = -1816
649421
YDOT = 23197
924172 feet/sec YDOT = 7070
727288 meter/sec
ZDOT = -3121
865706 ZDOT = -951
544667
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 17269
95286634
00016717 00000-0 10270-3 0 9151
2 25544 51
6387 251
0122 0004395 325
2303 34
8562 15
54238236 37573
Satellite: ISS
Catalog Number: 25544
Epoch time: 17269
95286634 = yrday
fracday
Element set: 915
Inclination: 51
6387 deg
RA of node: 251
0122 deg
Eccentricity:
0004395
Arg of perigee: 325
2303 deg
Mean anomaly: 34
8562 deg
Mean motion: 15
54238236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3757
Checksum: 318
Coasting Arc #17 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/270/16:53:37
658
Vector Time (MET): N/A
Weight (LBS) : 904716
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2396937
96 A = 6779782
81 meter
Y = 4140413
29 meter E =
0010484
Z = -4813502
25 I = 51
28246
XDOT = -4625
704974 Wp = 49
36052
YDOT = -5575
121654 meter/sec RA = 246
30515 deg
ZDOT = -2488
984223 TA = 196
01174
MA = 196
04490
Ha = 220
654 n
mi
Hp = 215
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7863969
68 X = -2419677
14
Y = 13584033
10 feet Y = 4113481
60 meter
Z = -15792330
23 Z = -4825201
48
XDOT = -15176
197422 XDOT = -4550
928299
YDOT = -18291
081541 feet/sec YDOT = -5626
431521 meter/sec
ZDOT = -8165
958736 ZDOT = -2511
272663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11889759
52 X = -3623998
70
Y = -10165878
83 feet Y = -3098559
87 meter
Z = -15844689
80 Z = -4829461
45
XDOT = 20058
139989 XDOT = 6113
721069
YDOT = -10563
464854 feet/sec YDOT = -3219
744088 meter/sec
ZDOT = -8263
814249 ZDOT = -2518
810583
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 17270
72442880
00016717 00000-0 10270-3 0 9166
2 25544 51
6415 247
1674 0004505 316
9808 43
0992 15
54017485 37696
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
72442880 = yrday
fracday
Element set: 916
Inclination: 51
6415 deg
RA of node: 247
1674 deg
Eccentricity:
0004505
Arg of perigee: 316
9808 deg
Mean anomaly: 43
0992 deg
Mean motion: 15
54017485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 326
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