[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: November 17th 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) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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


323/23:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 213 5

328/13:44:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 213 6

333/15:51:39 863 0 6 1 3 1 3
N/A -1 1 -0 0 221 5
000/00:03:19 725 0 2 -0 0 214 7

Coasting Arc #1 (Orbit 527)
---------------------------------------

Vector Time (GMT): 2017/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6410889
27                 A    =         6788179
43  meter
 Y    =       -1602934
80  meter          E    =           
0011997
 Z    =       -1536334
71                 I    =           51
68471
 XDOT =       2475
098446                 Wp   =          133
69874
 YDOT =      -4411
637114  meter/sec      RA   =            3
45220  deg
 ZDOT =      -5761
521105                 TA   =           63
07615
                                          MA   =           62
95362
                                          Ha   =            222
336  n
mi
                                          Hp   =            213
216

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21033101
29                 X    =        -6385025
42
 Y    =       -5258972
44  feet           Y    =        -1674481
16  meter
 Z    =       -5040468
21                 Z    =        -1567414
70
 XDOT =       8120
401726                 XDOT =        2552
233898
 YDOT =     -14473
875047  feet/sec       YDOT =       -4383
527699  meter/sec
 ZDOT =     -18902
628296                 ZDOT =       -5749
310118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16623142
98                 X    =         5066733
98
 Y    =      -13867698
83  feet           Y    =        -4226874
60  meter
 Z    =       -5178079
54                 Z    =        -1578278
64
 XDOT =       5826
395436                 XDOT =        1775
885329
 YDOT =      13978
463448  feet/sec       YDOT =        4260
635659  meter/sec
 ZDOT =     -18847
661775                 ZDOT =       -5744
767309


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   17319
52912091  
00016717  00000-0  10270-3 0  9007
2 25544  51
6416   3
8651 0004186 118
6018 241
5556 15
54159345  5287


Satellite: ISS
Catalog Number: 25544
Epoch time:      17319
52912091   =   yrday
fracday
Element set:     900
Inclination:       51
6416  deg
RA of node:         3
8651  deg
Eccentricity:     
0004186     
Arg of perigee:   118
6018  deg
Mean anomaly:     241
5556  deg
Mean motion:   15
54159345  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             528
Checksum:              298


Coasting Arc #2 (Orbit 543)
---------------------------------------

Vector Time (GMT): 2017/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5604196
65                 A    =         6785218
87  meter
 Y    =        2275029
12  meter          E    =           
0016641
 Z    =        3061671
03                 I    =           51
64133
 XDOT =      -4322
390025                 Wp   =           92
61505
 YDOT =       4004
178773  meter/sec      RA   =          358
47823  deg
 ZDOT =       4912
683171                 TA   =          302
55164
                                          MA   =          302
71226
                                          Ha   =            222
354  n
mi
                                          Hp   =            213
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18386471
96                 X    =         5563467
68
 Y    =        7464006
29  feet           Y    =         2337471
36  meter
 Z    =       10044852
45                 Z    =         3088796
23
 XDOT =     -14181
069636                 XDOT =       -4390
708588
 YDOT =      13137
069464  feet/sec       YDOT =        3955
460892  meter/sec
 ZDOT =      16117
726939                 ZDOT =        4891
519839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16644782
72                 X    =        -5073329
77
 Y    =       10691170
36  feet           Y    =         3258668
72  meter
 Z    =       10164786
60                 Z    =         3098226
95
 XDOT =      -1748
824848                 XDOT =        -533
041814
 YDOT =     -18030
285824  feet/sec       YDOT =       -5495
631119  meter/sec
 ZDOT =      16023
117147                 ZDOT =        4883
846106


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   17320
55793759  
00016717  00000-0  10270-3 0  9011
2 25544  51
6410 358
7368 0004235 119
9366 240
2207 15
54143010  5442


Satellite: ISS
Catalog Number: 25544
Epoch time:      17320
55793759   =   yrday
fracday
Element set:     901
Inclination:       51
6410  deg
RA of node:       358
7368  deg
Eccentricity:     
0004235     
Arg of perigee:   119
9366  deg
Mean anomaly:     240
2207  deg
Mean motion:   15
54143010  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             544
Checksum:              297


Coasting Arc #3 (Orbit 558)
---------------------------------------

Vector Time (GMT): 2017/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4342816
90                 A    =         6781275
21  meter
 Y    =       -2941851
52  meter          E    =           
0011541
 Z    =       -4308211
40                 I    =           51
59608
 XDOT =       5844
086206                 Wp   =           86
57394
 YDOT =      -3477
964641  meter/sec      RA   =          353
49188  deg
 ZDOT =      -3523
596447                 TA   =          147
51388
                                          MA   =          147
44280
                                          Ha   =            222
308  n
mi
                                          Hp   =            213
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14248086
95                 X    =        -4288669
83
 Y    =       -9651743
85  feet           Y    =        -2990113
06  meter
 Z    =      -14134551
84                 Z    =        -4329176
54
 XDOT =      19173
511174                 XDOT =        5899
659748
 YDOT =     -11410
645146  feet/sec       YDOT =       -3412
301304  meter/sec
 ZDOT =     -11560
355798                 ZDOT =       -3495
071990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15932530
32                 X    =         4856235
24
 Y    =       -6300461
14  feet           Y    =        -1920380
56  meter
 Z    =      -14227029
34                 Z    =        -4336398
54
 XDOT =      -1814
111986                 XDOT =        -552
941333
 YDOT =      21174
592124  feet/sec       YDOT =        6454
015679  meter/sec
 ZDOT =     -11433
188415                 ZDOT =       -3484
835829


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   17321
52244829  
00016717  00000-0  10270-3 0  9029
2 25544  51
6414 353
9287 0004208 125
2607 234
8940 15
54160771  5593


Satellite: ISS
Catalog Number: 25544
Epoch time:      17321
52244829   =   yrday
fracday
Element set:     902
Inclination:       51
6414  deg
RA of node:       353
9287  deg
Eccentricity:     
0004208     
Arg of perigee:   125
2607  deg
Mean anomaly:     234
8940  deg
Mean motion:   15
54160771  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             559
Checksum:              306


Coasting Arc #4 (Orbit 574)
---------------------------------------

Vector Time (GMT): 2017/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2782046
10                 A    =         6778203
87  meter
 Y    =        3536617
02  meter          E    =           
0009492
 Z    =        5063962
56                 I    =           51
55235
 XDOT =      -6894
950232                 Wp   =          125
34495
 YDOT =       2852
422561  meter/sec      RA   =          348
49322  deg
 ZDOT =       1788
109681                 TA   =          307
30078
                                          MA   =          307
38726
                                          Ha   =            222
207  n
mi
                                          Hp   =            213
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9127447
84                 X    =         2717693
04
 Y    =       11603074
20  feet           Y    =         3567367
78  meter
 Z    =       16614050
39                 Z    =         5077321
03
 XDOT =     -22621
227795                 XDOT =       -6935
020322
 YDOT =       9358
341734  feet/sec       YDOT =        2775
094417  meter/sec
 ZDOT =       5866
501577                 ZDOT =        1754
518026

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14647078
57                 X    =        -4464429
55
 Y    =        1205584
44  feet           Y    =          367462
14  meter
 Z    =       16672671
08                 Z    =         5081830
14
 XDOT =       4641
566018                 XDOT =        1414
749322
 YDOT =     -23021
226962  feet/sec       YDOT =       -7016
869978  meter/sec
 ZDOT =       5716
973852                 ZDOT =        1742
533630


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   17322
55125456  
00016717  00000-0  10270-3 0  9038
2 25544  51
6403 348
7998 0004214 127
2774 232
8764 15
54180145  5753


Satellite: ISS
Catalog Number: 25544
Epoch time:      17322
55125456   =   yrday
fracday
Element set:     903
Inclination:       51
6403  deg
RA of node:       348
7998  deg
Eccentricity:     
0004214     
Arg of perigee:   127
2774  deg
Mean anomaly:     232
8764  deg
Mean motion:   15
54180145  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             575
Checksum:              315


Coasting Arc #5 (Orbit 589)
---------------------------------------

Vector Time (GMT): 2017/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1029401
28                 A    =         6777263
88  meter
 Y    =       -4099856
09  meter          E    =           
0018155
 Z    =       -5313020
90                 I    =           51
51865
 XDOT =       7372
261721                 Wp   =           99
32523
 YDOT =      -2056
360806  meter/sec      RA   =          343
48607  deg
 ZDOT =        156
014210                 TA   =          172
18077
                                          MA   =          172
15243
                                          Ha   =            222
216  n
mi
                                          Hp   =            213
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3377300
77                 X    =         -957670
39
 Y    =      -13450971
43  feet           Y    =        -4110966
24  meter
 Z    =      -17431170
92                 Z    =        -5317847
50
 XDOT =      24187
210370                 XDOT =        7393
950713
 YDOT =      -6746
590570  feet/sec       YDOT =       -1973
797877  meter/sec
 ZDOT =        511
857643                 ZDOT =         191
879851

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13125020
58                 X    =         4000506
27
 Y    =        4398591
28  feet           Y    =         1340690
62  meter
 Z    =      -17451840
65                 Z    =        -5319321
03
 XDOT =      -6840
562990                 XDOT =       -2085
003599
 YDOT =      23106
668371  feet/sec       YDOT =        7042
912519  meter/sec
 ZDOT =        671
323183                 ZDOT =         204
619306


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   17323
51575518  
00016717  00000-0  10270-3 0  9044
2 25544  51
6419 343
9915 0004050 131
3534 228
7967 15
54166221  5909


Satellite: ISS
Catalog Number: 25544
Epoch time:      17323
51575518   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:       343
9915  deg
Eccentricity:     
0004050     
Arg of perigee:   131
3534  deg
Mean anomaly:     228
7967  deg
Mean motion:   15
54166221  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             590
Checksum:              307


Coasting Arc #6 (Orbit 597)
---------------------------------------

Vector Time (GMT): 2017/323/23:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6510606
04                 A    =         6789078
16  meter
 Y    =        1839683
74  meter          E    =           
0014760
 Z    =        -478538
01                 I    =           51
54014
 XDOT =       -901
409415                 Wp   =          136
63196
 YDOT =      -4714
866425  meter/sec      RA   =          341
00078  deg
 ZDOT =      -5982
018761                 TA   =           48
53763
                                          MA   =           48
41098
                                          Ha   =            222
061  n
mi
                                          Hp   =            213
517

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21360256
03                 X    =        -6528369
43
 Y    =        6035707
80  feet           Y    =         1766778
40  meter
 Z    =       -1570006
59                 Z    =         -510208
32
 XDOT =      -2957
379970                 XDOT =        -819
561117
 YDOT =     -15468
721867  feet/sec       YDOT =       -4724
488636  meter/sec
 ZDOT =     -19626
045803                 ZDOT =       -5986
199086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6211353
54                 X    =        -1893220
56
 Y    =       21299000
12  feet           Y    =         6491935
24  meter
 Z    =       -1710820
88                 Z    =         -521458
21
 XDOT =     -13060
856497                 XDOT =       -3980
949060
 YDOT =      -5357
706139  feet/sec       YDOT =       -1633
028831  meter/sec
 ZDOT =     -19643
737238                 ZDOT =       -5987
411110


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   17324
03015331  
00016717  00000-0  10270-3 0  9055
2 25544  51
6394 341
4266 0003792 132
7619 227
3853 15
54175283  5989


Satellite: ISS
Catalog Number: 25544
Epoch time:      17324
03015331   =   yrday
fracday
Element set:     905
Inclination:       51
6394  deg
RA of node:       341
4266  deg
Eccentricity:     
0003792     
Arg of perigee:   132
7619  deg
Mean anomaly:     227
3853  deg
Mean motion:   15
54175283  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             598
Checksum:              308


Coasting Arc #7 (Orbit 613)
---------------------------------------

Vector Time (GMT): 2017/324/23:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6363430
82                 A    =         6787087
09  meter
 Y    =        -973611
52  meter          E    =           
0015724
 Z    =        2133149
66                 I    =           51
50210
 XDOT =      -1049
438796                 Wp   =           83
47770
 YDOT =       5248
580866  meter/sec      RA   =          336
01980  deg
 ZDOT =       5493
049315                 TA   =          300
21974
                                          MA   =          300
37534
                                          Ha   =            221
962  n
mi
                                          Hp   =            213
492

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20877397
69                 X    =         6363483
04
 Y    =       -3194263
51  feet           Y    =         -902451
13  meter
 Z    =        6998522
49                 Z    =         2164061
95
 XDOT =      -3443
040668                 XDOT =       -1134
734936
 YDOT =      17219
753499  feet/sec       YDOT =        5236
368055  meter/sec
 ZDOT =      18021
815339                 ZDOT =        5487
744518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8011056
92                 X    =         2441770
15
 Y    =      -19492344
50  feet           Y    =        -5941266
60  meter
 Z    =        7135814
15                 Z    =         2174996
15
 XDOT =      11493
751350                 XDOT =        3503
295412
 YDOT =      11351
268660  feet/sec       YDOT =        3459
866687  meter/sec
 ZDOT =      17997
338623                 ZDOT =        5485
588812


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   17325
05894654  
00016717  00000-0  10270-3 0  9062
2 25544  51
6382 336
2969 0003862 139
4686 220
6755 15
54211249  6143


Satellite: ISS
Catalog Number: 25544
Epoch time:      17325
05894654   =   yrday
fracday
Element set:     906
Inclination:       51
6382  deg
RA of node:       336
2969  deg
Eccentricity:     
0003862     
Arg of perigee:   139
4686  deg
Mean anomaly:     220
6755  deg
Mean motion:   15
54211249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             614
Checksum:              329


Coasting Arc #8 (Orbit 628)
---------------------------------------

Vector Time (GMT): 2017/325/23:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5749151
86                 A    =         6783481
66  meter
 Y    =         -98412
02  meter          E    =           
0008154
 Z    =       -3604019
09                 I    =           51
46050
 XDOT =       2849
324561                 Wp   =          104
27002
 YDOT =      -5586
527097  meter/sec      RA   =          331
02866  deg
 ZDOT =      -4403
056227                 TA   =          118
49429
                                          MA   =          118
41215
                                          Ha   =            221
931  n
mi
                                          Hp   =            213
466

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18862046
78                 X    =        -5730117
23
 Y    =        -322874
09  feet           Y    =         -162596
29  meter
 Z    =      -11824209
62                 Z    =        -3631900
97
 XDOT =       9348
177694                 XDOT =        2932
971107
 YDOT =     -18328
500975  feet/sec       YDOT =       -5554
196006  meter/sec
 ZDOT =     -14445
722528                 ZDOT =       -4389
012054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9692876
64                 X    =        -2954388
80
 Y    =       16093156
47  feet           Y    =         4905194
09  meter
 Z    =      -11947863
69                 Z    =        -3641708
85
 XDOT =      -9957
040492                 XDOT =       -3034
905942
 YDOT =     -16649
955127  feet/sec       YDOT =       -5074
906323  meter/sec
 ZDOT =     -14382
424908                 ZDOT =       -4383
763112


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   17326
02343840  
00016717  00000-0  10270-3 0  9077
2 25544  51
6381 331
4876 0003828 139
9503 220
1933 15
54206091  6299


Satellite: ISS
Catalog Number: 25544
Epoch time:      17326
02343840   =   yrday
fracday
Element set:     907
Inclination:       51
6381  deg
RA of node:       331
4876  deg
Eccentricity:     
0003828     
Arg of perigee:   139
9503  deg
Mean anomaly:     220
1933  deg
Mean motion:   15
54206091  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             629
Checksum:              300


Coasting Arc #9 (Orbit 644)
---------------------------------------

Vector Time (GMT): 2017/326/23:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4762318
00                 A    =         6779845
88  meter
 Y    =        1265386
53  meter          E    =           
0011536
 Z    =        4651623
46                 I    =           51
41998
 XDOT =      -4312
876627                 Wp   =          124
65772
 YDOT =       5661
275927  meter/sec      RA   =          326
02511  deg
 ZDOT =       2863
960446                 TA   =          296
75765
                                          MA   =          296
87564
                                          Ha   =            221
844  n
mi
                                          Hp   =            213
652

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15624402
88                 X    =         4725218
52
 Y    =        4151530
61  feet           Y    =         1318434
27  meter
 Z    =       15261231
82                 Z    =         4674667
65
 XDOT =     -14149
857700                 XDOT =       -4389
773911
 YDOT =      18573
739918  feet/sec       YDOT =        5612
616241  meter/sec
 ZDOT =       9396
195690                 ZDOT =        2842
823122

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11175782
38                 X    =         3406378
47
 Y    =      -11547111
82  feet           Y    =        -3519559
68  meter
 Z    =       15363217
94                 Z    =         4682708
83
 XDOT =       8481
290698                 XDOT =        2585
097405
 YDOT =      20633
822910  feet/sec       YDOT =        6289
189223  meter/sec
 ZDOT =       9301
429874                 ZDOT =        2835
075826


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   17327
05222419  
00016717  00000-0  10270-3 0  9080
2 25544  51
6381 326
3578 0003809 144
0037 216
1373 15
54187770  6452


Satellite: ISS
Catalog Number: 25544
Epoch time:      17327
05222419   =   yrday
fracday
Element set:     908
Inclination:       51
6381  deg
RA of node:       326
3578  deg
Eccentricity:     
0003809     
Arg of perigee:   144
0037  deg
Mean anomaly:     216
1373  deg
Mean motion:   15
54187770  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             645
Checksum:              306


Coasting Arc #10 (Orbit 659)
---------------------------------------

Vector Time (GMT): 2017/327/23:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3504172
09                 A    =         6777427
19  meter
 Y    =       -2538408
59  meter          E    =           
0016612
 Z    =       -5230545
37                 I    =           51
38493
 XDOT =       5368
135021                 Wp   =           94
97881
 YDOT =      -5368
109549  meter/sec      RA   =          321
01109  deg
 ZDOT =       -995
328814                 TA   =          165
46819
                                          MA   =          165
42037
                                          Ha   =            221
971  n
mi
                                          Hp   =            213
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11496627
58                 X    =        -3450118
74
 Y    =       -8328112
17  feet           Y    =        -2577292
08  meter
 Z    =      -17160581
93                 Z    =        -5247436
64
 XDOT =      17611
991540                 XDOT =        5432
598567
 YDOT =     -17611
907969  feet/sec       YDOT =       -5307
718896  meter/sec
 ZDOT =      -3265
514481                 ZDOT =        -969
095512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12709710
59                 X    =        -3873919
79
 Y    =        6118146
98  feet           Y    =         1864811
20  meter
 Z    =      -17235051
63                 Z    =        -5253243
74
 XDOT =      -6784
065566                 XDOT =       -2067
783185
 YDOT =     -22923
518611  feet/sec       YDOT =       -6987
088473  meter/sec
 ZDOT =      -3148
207126                 ZDOT =        -959
573532


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   17328
01670687  
00016717  00000-0  10270-3 0  9092
2 25544  51
6376 321
5493 0004085 146
4583 213
6829 15
54209353  6605


Satellite: ISS
Catalog Number: 25544
Epoch time:      17328
01670687   =   yrday
fracday
Element set:     909
Inclination:       51
6376  deg
RA of node:       321
5493  deg
Eccentricity:     
0004085     
Arg of perigee:   146
4583  deg
Mean anomaly:     213
6829  deg
Mean motion:   15
54209353  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             660
Checksum:              321


Coasting Arc #11 (Orbit 668)
---------------------------------------

Vector Time (GMT): 2017/328/13:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5409288
94                 A    =         6781946
96  meter
 Y    =         479957
50  meter          E    =           
0009134
 Z    =       -4069889
36                 I    =           51
38680
 XDOT =       2332
782386                 Wp   =           94
58202
 YDOT =      -6205
335013  meter/sec      RA   =          318
16293  deg
 ZDOT =      -3840
465556                 TA   =          135
54892
                                          MA   =          135
47558
                                          Ha   =            221
832  n
mi
                                          Hp   =            213
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17747010
96                 X    =        -5394484
17
 Y    =        1574663
73  feet           Y    =          419550
15  meter
 Z    =      -13352655
37                 Z    =        -4096130
32
 XDOT =       7653
485520                 XDOT =        2420
654036
 YDOT =     -20358
710672  feet/sec       YDOT =       -6178
756705  meter/sec
 ZDOT =     -12599
952611                 ZDOT =       -3828
920421

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1215275
04                 X    =         -370415
83
 Y    =      -17687143
80  feet           Y    =        -5391041
43  meter
 Z    =      -13469128
41                 Z    =        -4105390
34
 XDOT =      18909
030275                 XDOT =        5763
472428
 YDOT =       8235
814734  feet/sec       YDOT =        2510
276331  meter/sec
 ZDOT =     -12547
650993                 ZDOT =       -3824
524023


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   17328
59539495  
00016717  00000-0  10270-3 0  9108
2 25544  51
6387 318
6666 0003813 147
1267 213
0123 15
54211752  6697


Satellite: ISS
Catalog Number: 25544
Epoch time:      17328
59539495   =   yrday
fracday
Element set:     910
Inclination:       51
6387  deg
RA of node:       318
6666  deg
Eccentricity:     
0003813     
Arg of perigee:   147
1267  deg
Mean anomaly:     213
0123  deg
Mean motion:   15
54211752  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             669
Checksum:              319


Coasting Arc #12 (Orbit 684)
---------------------------------------

Vector Time (GMT): 2017/329/13:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4550012
76                 A    =         6778495
99  meter
 Y    =         917808
72  meter          E    =           
0009615
 Z    =        4936160
78                 I    =           51
35288
 XDOT =      -3638
725275                 Wp   =          133
92051
 YDOT =       6400
629834  meter/sec      RA   =          313
15225  deg
 ZDOT =       2154
791473                 TA   =          294
95130
                                          MA   =          295
05116
                                          Ha   =            221
571  n
mi
                                          Hp   =            213
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14927863
40                 X    =         4515433
72
 Y    =        3011183
48  feet           Y    =          968496
51  meter
 Z    =       16194753
20                 Z    =         4958179
61
 XDOT =     -11938
075048                 XDOT =       -3720
495421
 YDOT =      20999
441711  feet/sec       YDOT =        6359
481818  meter/sec
 ZDOT =       7069
525830                 ZDOT =        2136
917175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3058021
51                 X    =         -932084
96
 Y    =       14811798
36  feet           Y    =         4514636
14  meter
 Z    =       16292252
66                 Z    =         4965878
61
 XDOT =     -19883
080030                 XDOT =       -6060
362793
 YDOT =     -11825
648560  feet/sec       YDOT =       -3604
457681  meter/sec
 ZDOT =       6989
130504                 ZDOT =        2130
286978


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   17329
62416776  
00016717  00000-0  10270-3 0  9110
2 25544  51
6397 313
5384 0003716 153
8520 206
2821 15
54252037  6855


Satellite: ISS
Catalog Number: 25544
Epoch time:      17329
62416776   =   yrday
fracday
Element set:     911
Inclination:       51
6397  deg
RA of node:       313
5384  deg
Eccentricity:     
0003716     
Arg of perigee:   153
8520  deg
Mean anomaly:     206
2821  deg
Mean motion:   15
54252037  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             685
Checksum:              309


Coasting Arc #13 (Orbit 699)
---------------------------------------

Vector Time (GMT): 2017/330/13:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3484097
90                 A    =         6777105
51  meter
 Y    =       -2426997
31  meter          E    =           
0016701
 Z    =       -5296237
30                 I    =           51
32579
 XDOT =       4588
992486                 Wp   =           99
85739
 YDOT =      -6125
246033  meter/sec      RA   =          308
13071  deg
 ZDOT =       -215
336778                 TA   =          168
09792
                                          MA   =          168
05840
                                          Ha   =            221
721  n
mi
                                          Hp   =            213
703

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11430767
38                 X    =        -3430972
82
 Y    =       -7962589
61  feet           Y    =        -2465661
66  meter
 Z    =      -17376106
64                 Z    =        -5313033
19
 XDOT =      15055
749625                 XDOT =        4658
191575
 YDOT =     -20095
951551  feet/sec       YDOT =       -6073
541860  meter/sec
 ZDOT =       -706
485493                 ZDOT =        -192
876762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7803331
54                 X    =         2378455
45
 Y    =      -11427755
04  feet           Y    =        -3483179
73  meter
 Z    =      -17450180
22                 Z    =        -5318814
93
 XDOT =      19473
529921                 XDOT =        5935
531920
 YDOT =      14205
498074  feet/sec       YDOT =        4329
835813  meter/sec
 ZDOT =       -605
813367                 ZDOT =        -184
651914


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   17330
58863928  
00016717  00000-0  10270-3 0  9123
2 25544  51
6393 308
7291 0003675 154
5107 205
6228 15
54219373  7005


Satellite: ISS
Catalog Number: 25544
Epoch time:      17330
58863928   =   yrday
fracday
Element set:     912
Inclination:       51
6393  deg
RA of node:       308
7291  deg
Eccentricity:     
0003675     
Arg of perigee:   154
5107  deg
Mean anomaly:     205
6228  deg
Mean motion:   15
54219373  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             700
Checksum:              312


Coasting Arc #14 (Orbit 715)
---------------------------------------

Vector Time (GMT): 2017/331/13:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2318397
64                 A    =         6778095
54  meter
 Y    =        3862606
74  meter          E    =           
0005786
 Z    =        5059272
01                 I    =           51
30960
 XDOT =      -5177
669233                 Wp   =           93
24289
 YDOT =       5388
639209  meter/sec      RA   =          303
10896  deg
 ZDOT =      -1740
013651                 TA   =           13
65502
                                          MA   =           13
63937
                                          Ha   =            221
567  n
mi
                                          Hp   =            213
907

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7606291
46                 X    =         2250456
87
 Y    =       12672594
29  feet           Y    =         3888152
66  meter
 Z    =       16598661
44                 Z    =         5070369
26
 XDOT =     -16987
103782                 XDOT =       -5229
089389
 YDOT =      17679
262496  feet/sec       YDOT =        5330
451501  meter/sec
 ZDOT =      -5708
706204                 ZDOT =       -1765
290251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12432891
48                 X    =        -3789545
32
 Y    =        7890449
51  feet           Y    =         2405009
01  meter
 Z    =       16647218
79                 Z    =         5074072
29
 XDOT =     -17625
753341                 XDOT =       -5372
329618
 YDOT =     -15480
371863  feet/sec       YDOT =       -4718
417344  meter/sec
 ZDOT =      -5821
729762                 ZDOT =       -1774
463232


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   17331
61740381  
00016717  00000-0  10270-3 0  9136
2 25544  51
6392 303
6009 0003670 158
0931 202
0379 15
54228336  7168


Satellite: ISS
Catalog Number: 25544
Epoch time:      17331
61740381   =   yrday
fracday
Element set:     913
Inclination:       51
6392  deg
RA of node:       303
6009  deg
Eccentricity:     
0003670     
Arg of perigee:   158
0931  deg
Mean anomaly:     202
0379  deg
Mean motion:   15
54228336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             716
Checksum:              288


Coasting Arc #15 (Orbit 730)
---------------------------------------

Vector Time (GMT): 2017/332/13:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1159980
60                 A    =         6781203
25  meter
 Y    =       -5129632
89  meter          E    =           
0011003
 Z    =       -4292699
65                 I    =           51
30317
 XDOT =       5397
581225                 Wp   =          125
31054
 YDOT =      -4152
382963  meter/sec      RA   =          298
09054  deg
 ZDOT =       3503
549157                 TA   =          180
57389
                                          MA   =          180
57515
                                          Ha   =            221
562  n
mi
                                          Hp   =            213
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3805710
64                 X    =        -1081681
32
 Y    =      -16829504
22  feet           Y    =        -5142166
72  meter
 Z    =      -14083660
28                 Z    =        -4298144
46
 XDOT =      17708
599820                 XDOT =        5426
594347
 YDOT =     -13623
303686  feet/sec       YDOT =       -4091
861351  meter/sec
 ZDOT =      11494
583850                 ZDOT =        3529
839732

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16630721
56                 X    =         5069043
93
 Y    =       -4525311
60  feet           Y    =        -1379314
98  meter
 Z    =      -14106941
14                 Z    =        -4299795
66
 XDOT =      14131
816707                 XDOT =        4307
377732
 YDOT =      15738
217623  feet/sec       YDOT =        4797
008732  meter/sec
 ZDOT =      11611
882576                 ZDOT =        3539
301809


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   17332
58186491  
00016717  00000-0  10270-3 0  9140
2 25544  51
6394 298
7921 0003623 163
1787 196
9486 15
54232758  7311


Satellite: ISS
Catalog Number: 25544
Epoch time:      17332
58186491   =   yrday
fracday
Element set:     914
Inclination:       51
6394  deg
RA of node:       298
7921  deg
Eccentricity:     
0003623     
Arg of perigee:   163
1787  deg
Mean anomaly:     196
9486  deg
Mean motion:   15
54232758  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             731
Checksum:              345


Coasting Arc #16 (Orbit 746)
---------------------------------------

Vector Time (GMT): 2017/333/13:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934927
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          56756
27                 A    =         6785060
14  meter
 Y    =        6060953
79  meter          E    =           
0014747
 Z    =        3031293
86                 I    =           51
30223
 XDOT =      -5341
023196                 Wp   =          109
07597
 YDOT =       2510
542901  meter/sec      RA   =          293
08130  deg
 ZDOT =      -4904
892379                 TA   =           35
95594
                                          MA   =           35
85680
                                          Ha   =            221
437  n
mi
                                          Hp   =            214
034

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         186208
23                 X    =          -25747
97
 Y    =       19885019
01  feet           Y    =         6061127
12  meter
 Z    =        9945189
85                 Z    =         3031369
29
 XDOT =     -17523
041983                 XDOT =       -5344
873807
 YDOT =       8236
689308  feet/sec       YDOT =        2450
794487  meter/sec
 ZDOT =     -16092
166599                 ZDOT =       -4930
847196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19834968
49                 X    =        -6045698
40
 Y    =        1426951
92  feet           Y    =          434934
95  meter
 Z    =        9944510
48                 Z    =         3031086
79
 XDOT =      -9257
648525                 XDOT =       -2821
731270
 YDOT =     -15391
874131  feet/sec       YDOT =       -4691
443235  meter/sec
 ZDOT =     -16207
692245                 ZDOT =       -4940
104596


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   17333
61061781  
00016717  00000-0  10270-3 0  9150
2 25544  51
6399 293
6625 0003527 165
2374 194
8882 15
54256131  7474


Satellite: ISS
Catalog Number: 25544
Epoch time:      17333
61061781   =   yrday
fracday
Element set:     915
Inclination:       51
6399  deg
RA of node:       293
6625  deg
Eccentricity:     
0003527     
Arg of perigee:   165
2374  deg
Mean anomaly:     194
8882  deg
Mean motion:   15
54256131  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             747
Checksum:              328


Coasting Arc #17 (Orbit 747)
---------------------------------------

Vector Time (GMT): 2017/333/15:53:19
725
Vector Time (MET): N/A
Weight (LBS)     : 934788
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2930841
07                 A    =         6778831
69  meter
 Y    =       -3474046
27  meter          E    =           
0014079
 Z    =       -5041986
66                 I    =           51
27964
 XDOT =       4158
892709                 Wp   =          116
79113
 YDOT =      -6164
466474  meter/sec      RA   =          292
64116  deg
 ZDOT =       1827
685843                 TA   =          171
03480
                                          MA   =          171
00963
                                          Ha   =            221
479  n
mi
                                          Hp   =            214
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9615620
32                 X    =        -2867283
58
 Y    =      -11397789
60  feet           Y    =        -3506465
47  meter
 Z    =      -16541950
98                 Z    =        -5056069
73
 XDOT =      13644
661118                 XDOT =        4218
638160
 YDOT =     -20224
627541  feet/sec       YDOT =       -6117
624871  meter/sec
 ZDOT =       5996
344630                 ZDOT =        1848
033829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3587168
42                 X    =         1093368
94
 Y    =      -14403161
78  feet           Y    =        -4390083
71  meter
 Z    =      -16603826
60                 Z    =        -5060846
35
 XDOT =      23305
134455                 XDOT =        7103
404982
 YDOT =      -1222
036780  feet/sec       YDOT =        -372
476810  meter/sec
 ZDOT =       6087
615126                 ZDOT =        1855
505090


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   17333
67491471  
00016717  00000-0  10270-3 0  9160
2 25544  51
6416 293
3427 0003253 182
7310 177
3826 15
54014398  7483


Satellite: ISS
Catalog Number: 25544
Epoch time:      17333
67491471   =   yrday
fracday
Element set:     916
Inclination:       51
6416  deg
RA of node:       293
3427  deg
Eccentricity:     
0003253     
Arg of perigee:   182
7310  deg
Mean anomaly:     177
3826  deg
Mean motion:   15
54014398  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             748
Checksum:              317
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