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

 
Date: September 3rd 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


245/21:58:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 215 9

246/10:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 7
000/00:00:00 000 0 0 0 0 215 9

255/21:17:02 000 0 0 0 0 0 0
N/A 0 0 0 0 219 3
000/00:00:00 000 0 0 0 0 216 2

256/02:57:42 000 0 0 0 0 0 0
N/A 0 0 0 0 219 5
000/00:00:00 000 0 0 0 0 216 3

256/23:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 5
000/00:00:00 000 0 0 0 0 216 2

Coasting Arc #1 (Orbit 3330)
---------------------------------------

Vector Time (GMT): 2017/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5000706
52                 A    =         6788125
60  meter
 Y    =        4202014
62  meter          E    =           
0010703
 Z    =        1835599
01                 I    =           51
83051
 XDOT =      -4389
064557                 Wp   =           82
87955
 YDOT =       2740
201080  meter/sec      RA   =           27
27769  deg
 ZDOT =       5657
329391                 TA   =          297
24882
                                          MA   =          297
35782
                                          Ha   =            221
147  n
mi
                                          Hp   =            215
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16406517
45                 X    =         4944430
41
 Y    =       13786137
22  feet           Y    =         4257621
34  meter
 Z    =        6022306
47                 Z    =         1859753
95
 XDOT =     -14399
818102                 XDOT =       -4446
860422
 YDOT =       8990
161025  feet/sec       YDOT =        2690
796626  meter/sec
 ZDOT =      18560
791965                 ZDOT =        5635
868291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10011942
25                 X    =        -3051640
00
 Y    =      -18912995
83  feet           Y    =        -5764681
13  meter
 Z    =        6128553
69                 Z    =         1867983
16
 XDOT =      15452
739591                 XDOT =        4709
995027
 YDOT =      -2168
567232  feet/sec       YDOT =        -660
979292  meter/sec
 ZDOT =      18465
260034                 ZDOT =        5628
211258


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   17242
56063421  
00016717  00000-0  10270-3 0  9000
2 25544  51
6398  27
5636 0004825 206
9358 153
1545 15
54034441 33310


Satellite: ISS
Catalog Number: 25544
Epoch time:      17242
56063421   =   yrday
fracday
Element set:     900
Inclination:       51
6398  deg
RA of node:        27
5636  deg
Eccentricity:     
0004825     
Arg of perigee:   206
9358  deg
Mean anomaly:     153
1545  deg
Mean motion:   15
54034441  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3331
Checksum:              294


Coasting Arc #2 (Orbit 3345)
---------------------------------------

Vector Time (GMT): 2017/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3925848
67                 A    =         6784927
08  meter
 Y    =       -4430339
71  meter          E    =           
0004837
 Z    =       -3313236
83                 I    =           51
79077
 XDOT =       5816
667822                 Wp   =          151
54616
 YDOT =      -1629
414089  meter/sec      RA   =           22
31274  deg
 ZDOT =      -4720
348055                 TA   =           66
88591
                                          MA   =           66
83493
                                          Ha   =            220
974  n
mi
                                          Hp   =            215
573

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12880080
94                 X    =        -3859921
68
 Y    =      -14535235
28  feet           Y    =        -4473872
72  meter
 Z    =      -10870199
57                 Z    =        -3332146
99
 XDOT =      19083
555846                 XDOT =        5857
385048
 YDOT =      -5345
846749  feet/sec       YDOT =       -1564
140645  meter/sec
 ZDOT =     -15486
706217                 ZDOT =       -4691
993716

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6745480
57                 X    =         2056022
48
 Y    =       18161974
69  feet           Y    =         5535769
88  meter
 Z    =      -10953171
04                 Z    =        -3338526
53
 XDOT =     -18501
950462                 XDOT =       -5639
394501
 YDOT =      -2378
397802  feet/sec       YDOT =        -724
935650  meter/sec
 ZDOT =     -15360
842183                 ZDOT =       -4681
984697


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   17243
52523803  
00016717  00000-0  10270-3 0  9013
2 25544  51
6404  22
7557 0004685 211
6727 148
4144 15
54016455 33467


Satellite: ISS
Catalog Number: 25544
Epoch time:      17243
52523803   =   yrday
fracday
Element set:     901
Inclination:       51
6404  deg
RA of node:        22
7557  deg
Eccentricity:     
0004685     
Arg of perigee:   211
6727  deg
Mean anomaly:     148
4144  deg
Mean motion:   15
54016455  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3346
Checksum:              294


Coasting Arc #3 (Orbit 3361)
---------------------------------------

Vector Time (GMT): 2017/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2535235
99                 A    =         6781152
47  meter
 Y    =        4456137
57  meter          E    =           
0009161
 Z    =        4437316
17                 I    =           51
74870
 XDOT =      -6884
040281                 Wp   =          139
90493
 YDOT =        596
175177  meter/sec      RA   =           17
33623  deg
 ZDOT =       3323
791702                 TA   =          276
53906
                                          MA   =          276
64335
                                          Ha   =            220
798  n
mi
                                          Hp   =            215
681

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8317703
39                 X    =         2463663
74
 Y    =       14619873
93  feet           Y    =         4484088
29  meter
 Z    =       14558123
92                 Z    =         4449457
46
 XDOT =     -22585
433994                 XDOT =       -6906
340446
 YDOT =       1955
955305  feet/sec       YDOT =         519
068584  meter/sec
 ZDOT =      10904
828418                 ZDOT =        3290
297275

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2718604
88                 X    =         -828630
77
 Y    =      -16552599
96  feet           Y    =        -5045232
47  meter
 Z    =       14611108
70                 Z    =         4453465
93
 XDOT =      20749
850531                 XDOT =        6324
554442
 YDOT =       6117
551096  feet/sec       YDOT =        1864
629574  meter/sec
 ZDOT =      10756
387265                 ZDOT =        3278
546838


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   17244
55414166  
00016717  00000-0  10270-3 0  9029
2 25544  51
6412  17
6274 0004664 215
8513 144
2327 15
54048451 33627


Satellite: ISS
Catalog Number: 25544
Epoch time:      17244
55414166   =   yrday
fracday
Element set:     902
Inclination:       51
6412  deg
RA of node:        17
6274  deg
Eccentricity:     
0004664     
Arg of perigee:   215
8513  deg
Mean anomaly:     144
2327  deg
Mean motion:   15
54048451  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3362
Checksum:              290


Coasting Arc #4 (Orbit 3376)
---------------------------------------

Vector Time (GMT): 2017/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -873155
06                 A    =         6778403
79  meter
 Y    =       -4344248
18  meter          E    =           
0010530
 Z    =       -5138419
60                 I    =           51
70751
 XDOT =       7487
122198                 Wp   =           93
83894
 YDOT =        361
251926  meter/sec      RA   =           12
34935  deg
 ZDOT =      -1581
163909                 TA   =          160
93418
                                          MA   =          160
89474
                                          Ha   =            220
750  n
mi
                                          Hp   =            215
757

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2864681
95                 X    =         -799551
98
 Y    =      -14252782
75  feet           Y    =        -4353601
10  meter
 Z    =      -16858332
02                 Z    =        -5142482
10
 XDOT =      24564
049207                 XDOT =        7490
206563
 YDOT =       1185
209730  feet/sec       YDOT =         444
995198  meter/sec
 ZDOT =      -5187
545634                 ZDOT =       -1544
786714

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2046274
91                 X    =         -623704
59
 Y    =       14372887
51  feet           Y    =         4380856
11  meter
 Z    =      -16875557
50                 Z    =        -5143669
93
 XDOT =     -21817
480617                 XDOT =       -6649
968092
 YDOT =      -8994
514405  feet/sec       YDOT =       -2741
527991  meter/sec
 ZDOT =      -5026
513769                 ZDOT =       -1532
081397


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   17245
51873675  
00016717  00000-0  10270-3 0  9031
2 25544  51
6409  12
8207 0004563 219
2033 140
8789 15
54034000 33774


Satellite: ISS
Catalog Number: 25544
Epoch time:      17245
51873675   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:        12
8207  deg
Eccentricity:     
0004563     
Arg of perigee:   219
2033  deg
Mean anomaly:     140
8789  deg
Mean motion:   15
54034000  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3377
Checksum:              299


Coasting Arc #5 (Orbit 3383)
---------------------------------------

Vector Time (GMT): 2017/245/21:58:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2742332
05                 A    =         6780572
07  meter
 Y    =        4176765
23  meter          E    =           
0008021
 Z    =        4582940
17                 I    =           51
69974
 XDOT =      -6932
090535                 Wp   =          144
01526
 YDOT =       1191
490229  meter/sec      RA   =           10
29501  deg
 ZDOT =       3053
064022                 TA   =          275
45038
                                          MA   =          275
54187
                                          Ha   =            220
469  n
mi
                                          Hp   =            215
854

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8997152
40                 X    =         2673161
12
 Y    =       13703298
01  feet           Y    =         4207045
34  meter
 Z    =       15035892
94                 Z    =         4596093
19
 XDOT =     -22743
079184                 XDOT =       -6959
729006
 YDOT =       3909
088678  feet/sec       YDOT =        1113
816494  meter/sec
 ZDOT =      10016
614245                 ZDOT =        3019
323277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4540461
04                 X    =        -1383932
52
 Y    =       15696514
38  feet           Y    =         4784297
58  meter
 Z    =       15093404
33                 Z    =         4600469
64
 XDOT =     -16736
753388                 XDOT =       -5101
362433
 YDOT =     -14357
698026  feet/sec       YDOT =       -4376
226358  meter/sec
 ZDOT =       9866
987626                 ZDOT =        3007
457828


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   17245
96887827  
00016717  00000-0  10270-3 0  9045
2 25544  51
6389  10
5808 0004318 225
2993 134
7809 15
54053466 33843


Satellite: ISS
Catalog Number: 25544
Epoch time:      17245
96887827   =   yrday
fracday
Element set:     904
Inclination:       51
6389  deg
RA of node:        10
5808  deg
Eccentricity:     
0004318     
Arg of perigee:   225
2993  deg
Mean anomaly:     134
7809  deg
Mean motion:   15
54053466  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3384
Checksum:              342


Coasting Arc #6 (Orbit 3390)
---------------------------------------

Vector Time (GMT): 2017/246/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6669176
52                 A    =         6788961
79  meter
 Y    =         -90856
03  meter          E    =           
0004670
 Z    =       -1254801
91                 I    =           51
71257
 XDOT =       1163
152785                 Wp   =           33
48309
 YDOT =       4817
130418  meter/sec      RA   =            7
76012  deg
 ZDOT =       5847
454656                 TA   =          312
89269
                                          MA   =          312
93188
                                          Ha   =            220
653  n
mi
                                          Hp   =            215
868

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21880500
38                 X    =         6675791
96
 Y    =        -298084
09  feet           Y    =          -16239
84  meter
 Z    =       -4116804
16                 Z    =        -1222389
44
 XDOT =       3816
118060                 XDOT =        1080
796187
 YDOT =      15804
233654  feet/sec       YDOT =        4829
677456  meter/sec
 ZDOT =      19184
562521                 ZDOT =        5852
904500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14842518
88                 X    =        -4523999
75
 Y    =      -16115399
02  feet           Y    =        -4911973
62  meter
 Z    =       -3973257
51                 Z    =        -1211048
89
 XDOT =       8132
927393                 XDOT =        2478
916269
 YDOT =     -12214
364219  feet/sec       YDOT =       -3722
938214  meter/sec
 ZDOT =      19207
848826                 ZDOT =        5854
552322


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   17246
41902137  
00016717  00000-0  10270-3 0  9059
2 25544  51
6402   8
3329 0004499 222
0393 138
0415 15
54039350 33915


Satellite: ISS
Catalog Number: 25544
Epoch time:      17246
41902137   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:         8
3329  deg
Eccentricity:     
0004499     
Arg of perigee:   222
0393  deg
Mean anomaly:     138
0415  deg
Mean motion:   15
54039350  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3391
Checksum:              288


Coasting Arc #7 (Orbit 3406)
---------------------------------------

Vector Time (GMT): 2017/247/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6733876
59                 A    =         6789406
12  meter
 Y    =        -676748
03  meter          E    =           
0011949
 Z    =        -439971
16                 I    =           51
68191
 XDOT =        860
593774                 Wp   =          159
22184
 YDOT =      -4703
448753  meter/sec      RA   =            2
79405  deg
 ZDOT =      -5997
743797                 TA   =           25
52104
                                          MA   =           25
46210
                                          Ha   =            220
393  n
mi
                                          Hp   =            215
908

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22092770
98                 X    =        -6723671
41
 Y    =       -2220301
95  feet           Y    =         -751993
81  meter
 Z    =       -1443474
92                 Z    =         -472656
99
 XDOT =       2823
470387                 XDOT =         942
258760
 YDOT =     -15431
262313  feet/sec       YDOT =       -4693
368870  meter/sec
 ZDOT =     -19677
637130                 ZDOT =       -5993
364627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13390460
74                 X    =         4081412
43
 Y    =       17699644
81  feet           Y    =         5394851
74  meter
 Z    =       -1588088
38                 Z    =         -484049
34
 XDOT =     -12031
516984                 XDOT =       -3667
206377
 YDOT =       7354
824699  feet/sec       YDOT =        2241
750568  meter/sec
 ZDOT =     -19657
422286                 ZDOT =       -5991
582313


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   17247
44791163  
00016717  00000-0  10270-3 0  9069
2 25544  51
6402   3
2040 0004348 227
6828 132
3956 15
54068384 34070


Satellite: ISS
Catalog Number: 25544
Epoch time:      17247
44791163   =   yrday
fracday
Element set:     906
Inclination:       51
6402  deg
RA of node:         3
2040  deg
Eccentricity:     
0004348     
Arg of perigee:   227
6828  deg
Mean anomaly:     132
3956  deg
Mean motion:   15
54068384  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3407
Checksum:              303


Coasting Arc #8 (Orbit 3422)
---------------------------------------

Vector Time (GMT): 2017/248/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6307088
11                 A    =         6787573
85  meter
 Y    =        1399252
12  meter          E    =           
0009844
 Z    =        2069426
27                 I    =           51
64423
 XDOT =      -2820
053135                 Wp   =           78
43539
 YDOT =       4491
988780  meter/sec      RA   =          357
82502  deg
 ZDOT =       5537
140138                 TA   =          304
45781
                                          MA   =          304
55078
                                          Ha   =            220
336  n
mi
                                          Hp   =            215
909

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20692546
30                 X    =         6280920
40
 Y    =        4590722
18  feet           Y    =         1469636
17  meter
 Z    =        6789456
27                 Z    =         2100000
11
 XDOT =      -9252
142832                 XDOT =       -2896
970565
 YDOT =      14737
495999  feet/sec       YDOT =        4460
023496  meter/sec
 ZDOT =      18166
470268                 ZDOT =        5523
254091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10988734
78                 X    =        -3349366
36
 Y    =      -18073482
96  feet           Y    =        -5508797
61  meter
 Z    =        6924582
34                 Z    =         2110612
70
 XDOT =      15803
998709                 XDOT =        4817
058807
 YDOT =      -2647
398198  feet/sec       YDOT =        -806
926971  meter/sec
 ZDOT =      18104
204580                 ZDOT =        5518
161556


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   17248
47679575  
00016717  00000-0  10270-3 0  9076
2 25544  51
6410 358
0764 0004475 229
6460 130
4302 15
54083462 34234


Satellite: ISS
Catalog Number: 25544
Epoch time:      17248
47679575   =   yrday
fracday
Element set:     907
Inclination:       51
6410  deg
RA of node:       358
0764  deg
Eccentricity:     
0004475     
Arg of perigee:   229
6460  deg
Mean anomaly:     130
4302  deg
Mean motion:   15
54083462  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3423
Checksum:              314


Coasting Arc #9 (Orbit 3437)
---------------------------------------

Vector Time (GMT): 2017/249/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5400073
46                 A    =         6784195
75  meter
 Y    =       -2127579
77  meter          E    =           
0002602
 Z    =       -3511894
78                 I    =           51
60003
 XDOT =       4577
463730                 Wp   =          142
20286
 YDOT =      -4178
062294  meter/sec      RA   =          352
84638  deg
 ZDOT =      -4511
173280                 TA   =           79
14040
                                          MA   =           79
11112
                                          Ha   =            220
162  n
mi
                                          Hp   =            215
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17716776
44                 X    =        -5358822
03
 Y    =       -6980248
58  feet           Y    =        -2187736
81  meter
 Z    =      -11521964
52                 Z    =        -3538026
01
 XDOT =      15017
925623                 XDOT =        4645
756609
 YDOT =     -13707
553459  feet/sec       YDOT =       -4126
492629  meter/sec
 ZDOT =     -14800
437271                 ZDOT =       -4488
771235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7483365
85                 X    =         2280929
91
 Y    =       17433775
51  feet           Y    =         5313814
78  meter
 Z    =      -11637285
38                 Z    =        -3547044
58
 XDOT =     -19106
742158                 XDOT =       -5823
735010
 YDOT =      -1603
126049  feet/sec       YDOT =        -488
632820  meter/sec
 ZDOT =     -14700
532693                 ZDOT =       -4480
722365


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
44137155  
00016717  00000-0  10270-3 0  9088
2 25544  51
6409 353
2692 0004429 234
4540 125
6200 15
54059124 34388


Satellite: ISS
Catalog Number: 25544
Epoch time:      17249
44137155   =   yrday
fracday
Element set:     908
Inclination:       51
6409  deg
RA of node:       353
2692  deg
Eccentricity:     
0004429     
Arg of perigee:   234
4540  deg
Mean anomaly:     125
6200  deg
Mean motion:   15
54059124  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3438
Checksum:              300


Coasting Arc #10 (Orbit 3453)
---------------------------------------

Vector Time (GMT): 2017/250/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4119832
30                 A    =         6780418
73  meter
 Y    =        2832221
57  meter          E    =           
0006943
 Z    =        4579875
60                 I    =           51
55677
 XDOT =      -5960
464963                 Wp   =          145
75104
 YDOT =       3748
007128  meter/sec      RA   =          347
85490  deg
 ZDOT =       3036
091087                 TA   =          273
84115
                                          MA   =          273
92053
                                          Ha   =            219
947  n
mi
                                          Hp   =            216
108

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13516510
17                 X    =         4065608
76
 Y    =        9292065
52  feet           Y    =         2877989
71  meter
 Z    =       15025838
60                 Z    =         4599756
34
 XDOT =     -19555
331244                 XDOT =       -6016
680957
 YDOT =      12296
611313  feet/sec       YDOT =        3681
039184  meter/sec
 ZDOT =       9960
928762                 ZDOT =        3007
000147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3142437
68                 X    =         -957815
00
 Y    =      -16016423
45  feet           Y    =        -4881805
87  meter
 Z    =       15113358
98                 Z    =         4606551
82
 XDOT =      21471
976492                 XDOT =        6544
658435
 YDOT =       5088
542578  feet/sec       YDOT =        1550
987778  meter/sec
 ZDOT =       9831
500273                 ZDOT =        2996
641283


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
47024375  
00016717  00000-0  10270-3 0  9093
2 25544  51
6422 348
1408 0004451 239
3651 120
7063 15
54097954 34547


Satellite: ISS
Catalog Number: 25544
Epoch time:      17250
47024375   =   yrday
fracday
Element set:     909
Inclination:       51
6422  deg
RA of node:       348
1408  deg
Eccentricity:     
0004451     
Arg of perigee:   239
3651  deg
Mean anomaly:     120
7063  deg
Mean motion:   15
54097954  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3454
Checksum:              304


Coasting Arc #11 (Orbit 3468)
---------------------------------------

Vector Time (GMT): 2017/251/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2556958
81                 A    =         6777942
65  meter
 Y    =       -3534278
20  meter          E    =           
0010147
 Z    =       -5196472
34                 I    =           51
51643
 XDOT =       6871
861853                 Wp   =           87
62849
 YDOT =      -3151
475819  meter/sec      RA   =          342
85338  deg
 ZDOT =      -1239
616447                 TA   =          170
45162
                                          MA   =          170
43232
                                          Ha   =            219
928  n
mi
                                          Hp   =            216
036

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8388972
47                 X    =        -2492005
62
 Y    =      -11595400
92  feet           Y    =        -3562509
31  meter
 Z    =      -17048793
75                 Z    =        -5208735
06
 XDOT =      22545
478521                 XDOT =        6912
613211
 YDOT =     -10339
487595  feet/sec       YDOT =       -3074
402269  meter/sec
 ZDOT =      -4066
983093                 ZDOT =       -1206
135725

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1906558
47                 X    =         -581119
02
 Y    =       14119497
89  feet           Y    =         4303622
96  meter
 Z    =      -17102466
61                 Z    =        -5212831
82
 XDOT =     -22501
561558                 XDOT =       -6858
475963
 YDOT =      -7777
745528  feet/sec       YDOT =       -2370
656837  meter/sec
 ZDOT =      -3918
240666                 ZDOT =       -1194
279755


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
43480741  
00016717  00000-0  10270-3 0  9105
2 25544  51
6420 343
3342 0004268 243
4957 116
5758 15
54088023 34697


Satellite: ISS
Catalog Number: 25544
Epoch time:      17251
43480741   =   yrday
fracday
Element set:     910
Inclination:       51
6420  deg
RA of node:       343
3342  deg
Eccentricity:     
0004268     
Arg of perigee:   243
4957  deg
Mean anomaly:     116
5758  deg
Mean motion:   15
54088023  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3469
Checksum:              306


Coasting Arc #12 (Orbit 3484)
---------------------------------------

Vector Time (GMT): 2017/252/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         874012
15                 A    =         6777602
91  meter
 Y    =        4172712
35  meter          E    =           
0001217
 Z    =        5269839
07                 I    =           51
48402
 XDOT =      -7259
553996                 Wp   =          260
10254
 YDOT =       2374
622478  meter/sec      RA   =          337
84421  deg
 ZDOT =       -676
578762                 TA   =          196
37046
                                          MA   =          196
37439
                                          Ha   =            219
758  n
mi
                                          Hp   =            216
166

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2867493
94                 X    =          801688
42
 Y    =       13690001
13  feet           Y    =         4182082
36  meter
 Z    =       17289498
27                 Z    =         5273908
63
 XDOT =     -23817
434371                 XDOT =       -7282
281609
 YDOT =       7790
756160  feet/sec       YDOT =        2293
314041  meter/sec
 ZDOT =      -2219
746593                 ZDOT =        -711
899033

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7161018
07                 X    =         2182678
31
 Y    =      -11989997
85  feet           Y    =        -3654551
34  meter
 Z    =       17306795
63                 Z    =         5275111
31
 XDOT =      21987
873299                 XDOT =        6701
903782
 YDOT =       9703
541495  feet/sec       YDOT =        2957
639448  meter/sec
 ZDOT =      -2376
483214                 ZDOT =        -724
352084


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
46366909  
00016717  00000-0  10270-3 0  9119
2 25544  51
6416 338
2055 0004269 247
8281 112
2419 15
54100410 34855


Satellite: ISS
Catalog Number: 25544
Epoch time:      17252
46366909   =   yrday
fracday
Element set:     911
Inclination:       51
6416  deg
RA of node:       338
2055  deg
Eccentricity:     
0004269     
Arg of perigee:   247
8281  deg
Mean anomaly:     112
2419  deg
Mean motion:   15
54100410  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3485
Checksum:              298


Coasting Arc #13 (Orbit 3499)
---------------------------------------

Vector Time (GMT): 2017/253/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         796736
98                 A    =         6779578
67  meter
 Y    =       -4716899
10  meter          E    =           
0008451
 Z    =       -4811979
94                 I    =           51
46141
 XDOT =       7099
615696                 Wp   =          125
55283
 YDOT =      -1380
552569  meter/sec      RA   =          332
83634  deg
 ZDOT =       2527
101962                 TA   =          169
39809
                                          MA   =          169
38027
                                          Ha   =            219
709  n
mi
                                          Hp   =            216
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2613966
48                 X    =          872797
79
 Y    =      -15475390
76  feet           Y    =        -4707564
65  meter
 Z    =      -15787335
77                 Z    =        -4807924
40
 XDOT =      23292
702416                 XDOT =        7102
250235
 YDOT =      -4529
371944  feet/sec       YDOT =       -1301
144843  meter/sec
 ZDOT =       8291
016935                 ZDOT =        2561
596466

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12245078
24                 X    =        -3732299
85
 Y    =        9847355
64  feet           Y    =         3001474
00  meter
 Z    =      -15768581
31                 Z    =        -4806263
58
 XDOT =     -19742
011451                 XDOT =       -6017
365090
 YDOT =     -11018
878615  feet/sec       YDOT =       -3358
554202  meter/sec
 ZDOT =       8443
916418                 ZDOT =        2573
705724


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
42822146  
00016717  00000-0  10270-3 0  9127
2 25544  51
6421 333
3986 0004257 250
9572 109
1119 15
54118077 35003


Satellite: ISS
Catalog Number: 25544
Epoch time:      17253
42822146   =   yrday
fracday
Element set:     912
Inclination:       51
6421  deg
RA of node:       333
3986  deg
Eccentricity:     
0004257     
Arg of perigee:   250
9572  deg
Mean anomaly:     109
1119  deg
Mean motion:   15
54118077  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3500
Checksum:              294


Coasting Arc #14 (Orbit 3515)
---------------------------------------

Vector Time (GMT): 2017/254/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2318084
54                 A    =         6783216
82  meter
 Y    =        5079318
48  meter          E    =           
0007326
 Z    =        3846234
52                 I    =           51
44451
 XDOT =      -6462
779762                 Wp   =           85
94652
 YDOT =        180
148712  meter/sec      RA   =          327
83299  deg
 ZDOT =      -4125
648301                 TA   =           47
54746
                                          MA   =           47
48555
                                          Ha   =            219
734  n
mi
                                          Hp   =            216
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7605264
24                 X    =        -2393393
81
 Y    =       16664430
72  feet           Y    =         5052975
31  meter
 Z    =       12618879
67                 Z    =         3834790
57
 XDOT =     -21203
345675                 XDOT =       -6444
273370
 YDOT =        591
039080  feet/sec       YDOT =         107
980644  meter/sec
 ZDOT =     -13535
591540                 ZDOT =       -4156
997790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16635562
53                 X    =         5070519
46
 Y    =       -7752335
20  feet           Y    =        -2362911
77  meter
 Z    =       12567369
56                 Z    =         3830534
24
 XDOT =      15930
848445                 XDOT =        4855
722606
 YDOT =      11979
039013  feet/sec       YDOT =        3651
211091  meter/sec
 ZDOT =     -13674
359090                 ZDOT =       -4167
944650


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
45707205  
00016717  00000-0  10270-3 0  9130
2 25544  51
6420 328
2697 0004115 255
0320 105
0377 15
54089900 35164


Satellite: ISS
Catalog Number: 25544
Epoch time:      17254
45707205   =   yrday
fracday
Element set:     913
Inclination:       51
6420  deg
RA of node:       328
2697  deg
Eccentricity:     
0004115     
Arg of perigee:   255
0320  deg
Mean anomaly:     105
0377  deg
Mean motion:   15
54089900  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3516
Checksum:              288


Coasting Arc #15 (Orbit 3530)
---------------------------------------

Vector Time (GMT): 2017/255/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3570625
85                 A    =         6786860
28  meter
 Y    =       -5202418
12  meter          E    =           
0002986
 Z    =       -2494371
17                 I    =           51
42967
 XDOT =       5420
028383                 Wp   =          356
27110
 YDOT =       1184
920459  meter/sec      RA   =          322
83857  deg
 ZDOT =       5289
844268                 TA   =          335
68106
                                          MA   =          335
69515
                                          Ha   =            219
566  n
mi
                                          Hp   =            216
299

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11714651
74                 X    =         3640651
80
 Y    =      -17068300
90  feet           Y    =        -5162097
56  meter
 Z    =       -8183632
44                 Z    =        -2476855
66
 XDOT =      17782
245351                 XDOT =        5380
679824
 YDOT =       3887
534315  feet/sec       YDOT =        1245
311229  meter/sec
 ZDOT =      17355
132114                 ZDOT =        5316
077607

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19914173
66                 X    =        -6069840
13
 Y    =        5767373
96  feet           Y    =         1757895
58  meter
 Z    =       -8105238
19                 Z    =        -2470476
60
 XDOT =     -10797
321986                 XDOT =       -3291
023741
 YDOT =     -12740
939766  feet/sec       YDOT =       -3883
438441  meter/sec
 ZDOT =      17471
022283                 ZDOT =        5325
167592


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
42161399  
00016717  00000-0  10270-3 0  9147
2 25544  51
6421 323
4621 0004255 262
0199  98
0470 15
54086797 35319


Satellite: ISS
Catalog Number: 25544
Epoch time:      17255
42161399   =   yrday
fracday
Element set:     914
Inclination:       51
6421  deg
RA of node:       323
4621  deg
Eccentricity:     
0004255     
Arg of perigee:   262
0199  deg
Mean anomaly:      98
0470  deg
Mean motion:   15
54086797  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3531
Checksum:              310


Coasting Arc #16 (Orbit 3538)
---------------------------------------

Vector Time (GMT): 2017/255/21:17:02
000
Vector Time (MET): N/A
Weight (LBS)     : 909986
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3205199
64                 A    =         6777398
29  meter
 Y    =        2812443
49  meter          E    =           
0002028
 Z    =        5269328
99                 I    =           51
38502
 XDOT =      -5580
329060                 Wp   =          232
45288
 YDOT =       5223
651422  meter/sec      RA   =          320
51695  deg
 ZDOT =        605
256944                 TA   =          211
74283
                                          MA   =          211
75505
                                          Ha   =            219
299  n
mi
                                          Hp   =            216
185

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10515746
85                 X    =         3147915
98
 Y    =        9227176
81  feet           Y    =         2847966
22  meter
 Z    =       17287824
76                 Z    =         5284759
64
 XDOT =     -18308
166206                 XDOT =       -5641
266632
 YDOT =      17137
963982  feet/sec       YDOT =        5160
907690  meter/sec
 ZDOT =       1985
751130                 ZDOT =         578
001002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -272174
13                 X    =          -82958
68
 Y    =       13903182
94  feet           Y    =         4237690
16  meter
 Z    =       17355634
06                 Z    =         5289997
26
 XDOT =     -23914
401713                 XDOT =       -7289
109642
 YDOT =      -2799
636663  feet/sec       YDOT =        -853
329255  meter/sec
 ZDOT =       1864
252225                 ZDOT =         568
224078


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
93603514  
00016717  00000-0  10270-3 0  9154
2 25544  51
6405 320
9010 0004236 268
8872  91
1795 15
54148200 35396


Satellite: ISS
Catalog Number: 25544
Epoch time:      17255
93603514   =   yrday
fracday
Element set:     915
Inclination:       51
6405  deg
RA of node:       320
9010  deg
Eccentricity:     
0004236     
Arg of perigee:   268
8872  deg
Mean anomaly:      91
1795  deg
Mean motion:   15
54148200  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3539
Checksum:              304


Coasting Arc #17 (Orbit 3541)
---------------------------------------

Vector Time (GMT): 2017/256/02:57:42
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2957693
55                 A    =         6786179
49  meter
 Y    =       -5447387
56  meter          E    =           
0002502
 Z    =       -2758517
30                 I    =           51
40674
 XDOT =       5685
907001                 Wp   =          353
94322
 YDOT =        496
828025  meter/sec      RA   =          319
30415  deg
 ZDOT =       5117
355061                 TA   =          334
71135
                                          MA   =          334
72359
                                          Ha   =            219
450  n
mi
                                          Hp   =            216
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9703719
00                 X    =         3031787
45
 Y    =      -17872006
42  feet           Y    =        -5413898
47  meter
 Z    =       -9050253
60                 Z    =        -2743969
43
 XDOT =      18654
550527                 XDOT =        5655
071041
 YDOT =       1630
013207  feet/sec       YDOT =         560
239568  meter/sec
 ZDOT =      16789
222642                 ZDOT =        5144
900628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2556672
98                 X    =         -779273
93
 Y    =      -20204253
67  feet           Y    =        -6158256
52  meter
 Z    =       -8984955
37                 Z    =        -2738614
40
 XDOT =      14511
904102                 XDOT =        4423
228370
 YDOT =      -9353
836007  feet/sec       YDOT =       -2851
049215  meter/sec
 ZDOT =      16911
035047                 ZDOT =        5154
483482


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
12894216  
00016717  00000-0  10270-3 0  9168
2 25544  51
6393 319
9376 0004311 268
7301  91
3357 15
54117362 35420


Satellite: ISS
Catalog Number: 25544
Epoch time:      17256
12894216   =   yrday
fracday
Element set:     916
Inclination:       51
6393  deg
RA of node:       319
9376  deg
Eccentricity:     
0004311     
Arg of perigee:   268
7301  deg
Mean anomaly:      91
3357  deg
Mean motion:   15
54117362  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3542
Checksum:              312


Coasting Arc #18 (Orbit 3554)
---------------------------------------

Vector Time (GMT): 2017/256/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2048486
51                 A    =         6785039
19  meter
 Y    =       -5629165
54  meter          E    =           
0001203
 Z    =       -3185251
23                 I    =           51
38629
 XDOT =       5961
576572                 Wp   =           13
02424
 YDOT =       -538
989855  meter/sec      RA   =          315
12754  deg
 ZDOT =       4788
025230                 TA   =          310
04481
                                          MA   =          310
05537
                                          Ha   =            219
471  n
mi
                                          Hp   =            216
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6720756
26                 X    =         2126753
49
 Y    =      -18468390
87  feet           Y    =        -5605820
50  meter
 Z    =      -10450299
31                 Z    =        -3175109
94
 XDOT =      19558
978254                 XDOT =        5943
902722
 YDOT =      -1768
339418  feet/sec       YDOT =        -472
422034  meter/sec
 ZDOT =      15708
744192                 ZDOT =        4816
941846

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13401926
21                 X    =         4084907
11
 Y    =      -14408123
04  feet           Y    =        -4391595
90  meter
 Z    =      -10404477
20                 Z    =        -3171284
65
 XDOT =      17575
130985                 XDOT =        5356
899924
 YDOT =       4915
184627  feet/sec       YDOT =        1498
148274  meter/sec
 ZDOT =      15836
796971                 ZDOT =        4827
055717


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
96487479  
00016717  00000-0  10270-3 0  9170
2 25544  51
6427 315
7724 0004177 273
3752  86
6923 15
54136968 35554


Satellite: ISS
Catalog Number: 25544
Epoch time:      17256
96487479   =   yrday
fracday
Element set:     917
Inclination:       51
6427  deg
RA of node:       315
7724  deg
Eccentricity:     
0004177     
Arg of perigee:   273
3752  deg
Mean anomaly:      86
6923  deg
Mean motion:   15
54136968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3555
Checksum:              358
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