[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: July 2nd 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) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 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


182/20:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 214 8

183/15:38:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 4
000/00:00:00 000 0 0 0 0 214 9

190/12:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 214 0

Coasting Arc #1 (Orbit 2381)
---------------------------------------

Vector Time (GMT): 2017/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2999606
35                 A    =         6784033
52  meter
 Y    =        4904404
25  meter          E    =           
0011562
 Z    =        3597652
89                 I    =           51
46521
 XDOT =      -6250
269631                 Wp   =           63
15492
 YDOT =       -580
847335  meter/sec      RA   =          331
34451  deg
 ZDOT =      -4403
376370                 TA   =           74
14477
                                          MA   =           74
01735
                                          Ha   =            221
296  n
mi
                                          Hp   =            215
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9841228
17                 X    =        -3071701
27
 Y    =       16090565
12  feet           Y    =         4870457
23  meter
 Z    =       11803323
12                 Z    =         3582907
10
 XDOT =     -20506
133960                 XDOT =       -6221
920611
 YDOT =      -1905
667108  feet/sec       YDOT =        -650
583239  meter/sec
 ZDOT =     -14446
772868                 ZDOT =       -4433
669238

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17299757
46                 X    =         5272966
08
 Y    =        7617671
91  feet           Y    =         2321866
40  meter
 Z    =       11737289
33                 Z    =         3577525
79
 XDOT =       1465
757977                 XDOT =         446
763032
 YDOT =      19218
377456  feet/sec       YDOT =        5857
761449  meter/sec
 ZDOT =     -14580
385011                 ZDOT =       -4444
101351


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   17181
53973971  
00016717  00000-0  10270-3 0  9009
2 25544  51
6393 331
7738 0004820 339
7641  20
3320 15
54084338 23824


Satellite: ISS
Catalog Number: 25544
Epoch time:      17181
53973971   =   yrday
fracday
Element set:     900
Inclination:       51
6393  deg
RA of node:       331
7738  deg
Eccentricity:     
0004820     
Arg of perigee:   339
7641  deg
Mean anomaly:      20
3320  deg
Mean motion:   15
54084338  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2382
Checksum:              307


Coasting Arc #2 (Orbit 2396)
---------------------------------------

Vector Time (GMT): 2017/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4174579
46                 A    =         6787420
79  meter
 Y    =       -4875827
70  meter          E    =           
0009723
 Z    =       -2191058
37                 I    =           51
44927
 XDOT =       5045
715686                 Wp   =           16
68941
 YDOT =       1871
694089  meter/sec      RA   =          326
35373  deg
 ZDOT =       5463
522407                 TA   =          318
91241
                                          MA   =          318
98559
                                          Ha   =            221
395  n
mi
                                          Hp   =            215
031

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13696126
83                 X    =         4239435
03
 Y    =      -15996810
04  feet           Y    =        -4828781
92  meter
 Z    =       -7188511
71                 Z    =        -2170622
49
 XDOT =      16554
185322                 XDOT =        4997
871889
 YDOT =       6140
728639  feet/sec       YDOT =        1927
850756  meter/sec
 ZDOT =      17924
942281                 ZDOT =        5487
916789

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17924794
49                 X    =        -5463477
36
 Y    =      -11112403
96  feet           Y    =        -3387060
73  meter
 Z    =       -7097375
80                 Z    =        -2163280
14
 XDOT =       2724
716966                 XDOT =         830
493731
 YDOT =     -15879
934340  feet/sec       YDOT =       -4840
203987  meter/sec
 ZDOT =      18032
264673                 ZDOT =        5496
234272


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   17182
50428815  
00016717  00000-0  10270-3 0  9010
2 25544  51
6400 326
9665 0004851 344
0468  16
0532 15
54101136 23977


Satellite: ISS
Catalog Number: 25544
Epoch time:      17182
50428815   =   yrday
fracday
Element set:     901
Inclination:       51
6400  deg
RA of node:       326
9665  deg
Eccentricity:     
0004851     
Arg of perigee:   344
0468  deg
Mean anomaly:      16
0532  deg
Mean motion:   15
54101136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2397
Checksum:              291


Coasting Arc #3 (Orbit 2402)
---------------------------------------

Vector Time (GMT): 2017/182/20:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3749399
77                 A    =         6778162
69  meter
 Y    =       -2365207
54  meter          E    =           
0014504
 Z    =       -5139863
78                 I    =           51
40817
 XDOT =       5357
930822                 Wp   =           57
79844
 YDOT =      -5267
501811  meter/sec      RA   =          324
53209  deg
 ZDOT =      -1480
026894                 TA   =          197
86019
                                          MA   =          197
91121
                                          Ha   =            221
497  n
mi
                                          Hp   =            214
810

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12301180
33                 X    =        -3697705
86
 Y    =       -7759867
25  feet           Y    =        -2406846
41  meter
 Z    =      -16863070
16                 Z    =        -5157951
80
 XDOT =      17578
513197                 XDOT =        5423
624427
 YDOT =     -17281
830090  feet/sec       YDOT =       -5207
218357  meter/sec
 ZDOT =      -4855
731280                 ZDOT =       -1453
840669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13536414
55                 X    =         4125899
15
 Y    =       -5061245
91  feet           Y    =        -1542667
75  meter
 Z    =      -16942460
97                 Z    =        -5164062
10
 XDOT =       2828
516211                 XDOT =         862
131741
 YDOT =      23478
392200  feet/sec       YDOT =        7156
213943  meter/sec
 ZDOT =      -4739
142232                 ZDOT =       -1444
490552


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   17182
89010600  
00016717  00000-0  10270-3 0  9022
2 25544  51
6398 325
0476 0005156 346
5389  13
5625 15
54090427 24034


Satellite: ISS
Catalog Number: 25544
Epoch time:      17182
89010600   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       325
0476  deg
Eccentricity:     
0005156     
Arg of perigee:   346
5389  deg
Mean anomaly:      13
5625  deg
Mean motion:   15
54090427  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2403
Checksum:              300


Coasting Arc #4 (Orbit 2414)
---------------------------------------

Vector Time (GMT): 2017/183/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         466307
46                 A    =         6780703
09  meter
 Y    =       -5045194
40  meter          E    =           
0008030
 Z    =       -4512285
87                 I    =           51
39808
 XDOT =       6632
066145                 Wp   =           78
93675
 YDOT =      -2196
433356  meter/sec      RA   =          320
59593  deg
 ZDOT =       3147
487706                 TA   =          222
74100
                                          MA   =          222
80348
                                          Ha   =            221
406  n
mi
                                          Hp   =            214
867

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1529880
11                 X    =          544607
94
 Y    =      -16552475
06  feet           Y    =        -5039541
62  meter
 Z    =      -14804087
49                 Z    =        -4509830
97
 XDOT =      21758
747194                 XDOT =        6640
845399
 YDOT =      -7206
146181  feet/sec       YDOT =       -2122
220290  meter/sec
 ZDOT =      10326
403236                 ZDOT =        3179
725323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8594074
10                 X    =        -2619473
79
 Y    =       14241342
86  feet           Y    =         4340761
30  meter
 Z    =      -14792295
77                 Z    =        -4508691
75
 XDOT =     -21641
327069                 XDOT =       -6596
276491
 YDOT =      -2206
962995  feet/sec       YDOT =        -672
682321  meter/sec
 ZDOT =      10469
111875                 ZDOT =        3190
985299


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   17183
66174305  
00016717  00000-0  10270-3 0  9032
2 25544  51
6414 321
1996 0004975 346
9590  13
1433 15
54132899 24159


Satellite: ISS
Catalog Number: 25544
Epoch time:      17183
66174305   =   yrday
fracday
Element set:     903
Inclination:       51
6414  deg
RA of node:       321
1996  deg
Eccentricity:     
0004975     
Arg of perigee:   346
9590  deg
Mean anomaly:      13
1433  deg
Mean motion:   15
54132899  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2415
Checksum:              315


Coasting Arc #5 (Orbit 2430)
---------------------------------------

Vector Time (GMT): 2017/184/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1846459
65                 A    =         6784532
69  meter
 Y    =        5584204
58  meter          E    =           
0012670
 Z    =        3377007
99                 I    =           51
38684
 XDOT =      -6073
612110                 Wp   =           66
75352
 YDOT =        792
505484  meter/sec      RA   =          315
59166  deg
 ZDOT =      -4612
659034                 TA   =           73
65973
                                          MA   =           73
52044
                                          Ha   =            221
592  n
mi
                                          Hp   =            214
751

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6057938
49                 X    =        -1925170
31
 Y    =       18320881
16  feet           Y    =         5563115
77  meter
 Z    =       11079422
55                 Z    =         3367847
86
 XDOT =     -19926
548916                 XDOT =       -6059
616680
 YDOT =       2600
083610  feet/sec       YDOT =         724
664959  meter/sec
 ZDOT =     -15133
395782                 ZDOT =       -4642
128688

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13179096
43                 X    =         4016988
59
 Y    =      -14127356
89  feet           Y    =        -4306018
38  meter
 Z    =       11037939
75                 Z    =         3364364
04
 XDOT =      18088
257102                 XDOT =        5513
300765
 YDOT =       4900
256395  feet/sec       YDOT =        1493
598149  meter/sec
 ZDOT =     -15263
615624                 ZDOT =       -4652
350042


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   17184
69058890  
00016717  00000-0  10270-3 0  9047
2 25544  51
6420 316
0706 0005179 350
7756   9
3300 15
54128601 24316


Satellite: ISS
Catalog Number: 25544
Epoch time:      17184
69058890   =   yrday
fracday
Element set:     904
Inclination:       51
6420  deg
RA of node:       316
0706  deg
Eccentricity:     
0005179     
Arg of perigee:   350
7756  deg
Mean anomaly:       9
3300  deg
Mean motion:   15
54128601  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2431
Checksum:              297


Coasting Arc #6 (Orbit 2445)
---------------------------------------

Vector Time (GMT): 2017/185/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2948302
02                 A    =         6787920
20  meter
 Y    =       -5797984
04  meter          E    =           
0011439
 Z    =       -1920126
95                 I    =           51
37451
 XDOT =       5194
369763                 Wp   =           19
50556
 YDOT =        798
065735  meter/sec      RA   =          310
59636  deg
 ZDOT =       5586
196795                 TA   =          319
24700
                                          MA   =          319
33251
                                          Ha   =            221
769  n
mi
                                          Hp   =            214
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9672906
90                 X    =         3022244
51
 Y    =      -19022257
34  feet           Y    =        -5764600
47  meter
 Z    =       -6299629
09                 Z    =        -1905626
09
 XDOT =      17041
895548                 XDOT =        5157
924531
 YDOT =       2618
325901  feet/sec       YDOT =         855
948278  meter/sec
 ZDOT =      18327
417305                 ZDOT =        5611
341004

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16499692
71                 X    =        -5029106
34
 Y    =       13564194
26  feet           Y    =         4134366
41  meter
 Z    =       -6234541
17                 Z    =        -1900288
15
 XDOT =     -13480
224207                 XDOT =       -4108
772338
 YDOT =      -7953
534907  feet/sec       YDOT =       -2424
237440  meter/sec
 ZDOT =      18438
244731                 ZDOT =        5619
976994


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   17185
65512920  
00016717  00000-0  10270-3 0  9054
2 25544  51
6413 311
2629 0005332 353
7983   6
3103 15
54085385 24460


Satellite: ISS
Catalog Number: 25544
Epoch time:      17185
65512920   =   yrday
fracday
Element set:     905
Inclination:       51
6413  deg
RA of node:       311
2629  deg
Eccentricity:     
0005332     
Arg of perigee:   353
7983  deg
Mean anomaly:       6
3103  deg
Mean motion:   15
54085385  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2446
Checksum:              298


Coasting Arc #7 (Orbit 2461)
---------------------------------------

Vector Time (GMT): 2017/186/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3798797
41                 A    =         6789315
87  meter
 Y    =        5619482
21  meter          E    =           
0009675
 Z    =         229204
72                 I    =           51
35864
 XDOT =      -4084
619467                 Wp   =          109
07350
 YDOT =      -2508
943322  meter/sec      RA   =          305
60691  deg
 ZDOT =      -5981
046271                 TA   =           68
44839
                                          MA   =           68
34530
                                          Ha   =            221
807  n
mi
                                          Hp   =            214
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12463246
09                 X    =        -3862466
97
 Y    =       18436621
41  feet           Y    =         5576645
45  meter
 Z    =         751984
00                 Z    =          210597
44
 XDOT =     -13400
982504                 XDOT =       -4027
207282
 YDOT =      -8231
441345  feet/sec       YDOT =       -2554
298534  meter/sec
 ZDOT =     -19622
855220                 ZDOT =       -6000
748935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18582866
95                 X    =         5664057
85
 Y    =      -12248948
44  feet           Y    =        -3733479
48  meter
 Z    =         668812
72                 Z    =          203854
12
 XDOT =       8209
220132                 XDOT =        2502
170296
 YDOT =      11336
914481  feet/sec       YDOT =        3455
491534  meter/sec
 ZDOT =     -19709
347818                 ZDOT =       -6007
409215


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   17186
68397056  
00016717  00000-0  10270-3 0  9060
2 25544  51
6408 306
1347 0005234 359
3669    
7476 15
54125832 24629


Satellite: ISS
Catalog Number: 25544
Epoch time:      17186
68397056   =   yrday
fracday
Element set:     906
Inclination:       51
6408  deg
RA of node:       306
1347  deg
Eccentricity:     
0005234     
Arg of perigee:   359
3669  deg
Mean anomaly:        
7476  deg
Mean motion:   15
54125832  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2462
Checksum:              323


Coasting Arc #8 (Orbit 2477)
---------------------------------------

Vector Time (GMT): 2017/187/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4319517
86                 A    =         6788495
29  meter
 Y    =       -5017770
94  meter          E    =           
0017333
 Z    =        1452277
87                 I    =           51
33778
 XDOT =       2890
981421                 Wp   =           45
94064
 YDOT =       4165
030334  meter/sec      RA   =          300
61595  deg
 ZDOT =       5760
940869                 TA   =          329
98492
                                          MA   =          330
08417
                                          Ha   =            221
936  n
mi
                                          Hp   =            214
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14171646
54                 X    =         4368252
44
 Y    =      -16462503
08  feet           Y    =        -4969194
87  meter
 Z    =        4764691
16                 Z    =         1473378
36
 XDOT =       9484
847183                 XDOT =        2816
208373
 YDOT =      13664
797685  feet/sec       YDOT =        4196
940383  meter/sec
 ZDOT =      18900
724637                 ZDOT =        5774
803268

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19199303
46                 X    =        -5851947
70
 Y    =       10115887
00  feet           Y    =         3083322
36  meter
 Z    =        4858747
96                 Z    =         1480946
38
 XDOT =      -2947
800792                 XDOT =        -898
489681
 YDOT =     -14749
855779  feet/sec       YDOT =       -4495
756041  meter/sec
 ZDOT =      18961
139057                 ZDOT =        5779
355185


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   17187
71280880  
00016717  00000-0  10270-3 0  9072
2 25544  51
6411 301
0058 0005401   3
4612 356
6577 15
54097648 24782


Satellite: ISS
Catalog Number: 25544
Epoch time:      17187
71280880   =   yrday
fracday
Element set:     907
Inclination:       51
6411  deg
RA of node:       301
0058  deg
Eccentricity:     
0005401     
Arg of perigee:     3
4612  deg
Mean anomaly:     356
6577  deg
Mean motion:   15
54097648  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2478
Checksum:              308


Coasting Arc #9 (Orbit 2492)
---------------------------------------

Vector Time (GMT): 2017/188/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4591086
39                 A    =         6785390
44  meter
 Y    =        3991802
76  meter          E    =           
0006391
 Z    =       -3014174
12                 I    =           51
31227
 XDOT =      -1668
282404                 Wp   =           51
69085
 YDOT =      -5630
135227  meter/sec      RA   =          295
61889  deg
 ZDOT =      -4918
395367                 TA   =          162
97208
                                          MA   =          162
95063
                                          Ha   =            222
053  n
mi
                                          Hp   =            214
046

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15062619
38                 X    =        -4620741
28
 Y    =       13096465
76  feet           Y    =         3940296
74  meter
 Z    =       -9889022
70                 Z    =        -3036547
52
 XDOT =      -5473
367468                 XDOT =       -1581
309767
 YDOT =     -18471
572268  feet/sec       YDOT =       -5648
304109  meter/sec
 ZDOT =     -16136
467740                 ZDOT =       -4926
288863

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18642455
90                 X    =         5682220
56
 Y    =       -6991518
17  feet           Y    =        -2131014
74  meter
 Z    =       -9988503
37                 Z    =        -3044495
83
 XDOT =      -1974
562889                 XDOT =        -601
846768
 YDOT =      17821
785533  feet/sec       YDOT =        5432
080231  meter/sec
 ZDOT =     -16170
277563                 ZDOT =       -4928
700601


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   17188
67734019  
00016717  00000-0  10270-3 0  9087
2 25544  51
6413 296
1979 0005419   8
0094 352
1144 15
54132420 24930


Satellite: ISS
Catalog Number: 25544
Epoch time:      17188
67734019   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:       296
1979  deg
Eccentricity:     
0005419     
Arg of perigee:     8
0094  deg
Mean anomaly:     352
1144  deg
Mean motion:   15
54132420  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2493
Checksum:              311


Coasting Arc #10 (Orbit 2508)
---------------------------------------

Vector Time (GMT): 2017/189/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4604480
05                 A    =         6781559
58  meter
 Y    =       -2602352
48  meter          E    =           
0010832
 Z    =        4233768
57                 I    =           51
28553
 XDOT =        524
125960                 Wp   =           76
80904
 YDOT =       6765
949626  meter/sec      RA   =          290
61140  deg
 ZDOT =       3583
460022                 TA   =          336
40786
                                          MA   =          336
45751
                                          Ha   =            221
960  n
mi
                                          Hp   =            214
008

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15106561
86                 X    =         4612672
66
 Y    =       -8537901
85  feet           Y    =        -2550816
84  meter
 Z    =       13890316
83                 Z    =         4256155
03
 XDOT =       1719
573359                 XDOT =         431
021855
 YDOT =      22197
997459  feet/sec       YDOT =        6771
289684  meter/sec
 ZDOT =      11756
758604                 ZDOT =        3585
780845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17008113
12                 X    =        -5184072
88
 Y    =        3009999
41  feet           Y    =          917447
82  meter
 Z    =       13989598
72                 Z    =         4264029
69
 XDOT =       6112
548032                 XDOT =        1863
104640
 YDOT =     -20225
250236  feet/sec       YDOT =       -6164
656272  meter/sec
 ZDOT =      11765
778468                 ZDOT =        3586
209277


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   17189
70617152  
00016717  00000-0  10270-3 0  9091
2 25544  51
6404 291
0699 0005402  11
3110 348
8164 15
54143503 25097


Satellite: ISS
Catalog Number: 25544
Epoch time:      17189
70617152   =   yrday
fracday
Element set:     909
Inclination:       51
6404  deg
RA of node:       291
0699  deg
Eccentricity:     
0005402     
Arg of perigee:    11
3110  deg
Mean anomaly:     348
8164  deg
Mean motion:   15
54143503  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2509
Checksum:              292


Coasting Arc #11 (Orbit 2521)
---------------------------------------

Vector Time (GMT): 2017/190/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3298937
97                 A    =         6787582
01  meter
 Y    =        5587360
69  meter          E    =           
0005514
 Z    =       -1996992
14                 I    =           51
29748
 XDOT =      -3451
565374                 Wp   =           91
00470
 YDOT =      -4012
952765  meter/sec      RA   =          286
28283  deg
 ZDOT =      -5539
365634                 TA   =          111
13870
                                          MA   =          111
07976
                                          Ha   =            222
080  n
mi
                                          Hp   =            213
965

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10823287
29                 X    =        -3351471
83
 Y    =       18331235
85  feet           Y    =         5550176
26  meter
 Z    =       -6551811
48                 Z    =        -2013144
02
 XDOT =     -11324
033380                 XDOT =       -3379
527763
 YDOT =     -13165
855527  feet/sec       YDOT =       -4051
146989  meter/sec
 ZDOT =     -18173
771766                 ZDOT =       -5555
957634

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21021295
10                 X    =         6407290
75
 Y    =        3214088
56  feet           Y    =          979654
19  meter
 Z    =       -6624105
71                 Z    =        -2019027
42
 XDOT =      -7839
207349                 XDOT =       -2389
390400
 YDOT =      13755
974477  feet/sec       YDOT =        4192
821021  meter/sec
 ZDOT =     -18246
291103                 ZDOT =       -5561
469528


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   17190
54209594  
00016717  00000-0  10270-3 0  9104
2 25544  51
6416 286
9017 0005130  13
5219 346
6070 15
54133459 25225


Satellite: ISS
Catalog Number: 25544
Epoch time:      17190
54209594   =   yrday
fracday
Element set:     910
Inclination:       51
6416  deg
RA of node:       286
9017  deg
Eccentricity:     
0005130     
Arg of perigee:    13
5219  deg
Mean anomaly:     346
6070  deg
Mean motion:   15
54133459  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2522
Checksum:              293


Coasting Arc #12 (Orbit 2537)
---------------------------------------

Vector Time (GMT): 2017/191/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3713842
02                 A    =         6784132
32  meter
 Y    =       -4499864
85  meter          E    =           
0014639
 Z    =        3444767
85                 I    =           51
27852
 XDOT =       2589
884171                 Wp   =           70
71041
 YDOT =       5620
762459  meter/sec      RA   =          281
28012  deg
 ZDOT =       4539
111588                 TA   =          329
95554
                                          MA   =          330
03945
                                          Ha   =            222
057  n
mi
                                          Hp   =            213
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12184521
07                 X    =         3747151
93
 Y    =      -14763336
13  feet           Y    =        -4458148
32  meter
 Z    =       11301731
79                 Z    =         3462888
65
 XDOT =       8496
995312                 XDOT =        2504
790384
 YDOT =      18440
821716  feet/sec       YDOT =        5649
247965  meter/sec
 ZDOT =      14892
098385                 ZDOT =        4551
486264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18297239
31                 X    =        -5576998
54
 Y    =       -5458681
13  feet           Y    =        -1663806
01  meter
 Z    =       11382513
91                 Z    =         3469390
24
 XDOT =      13360
596354                 XDOT =        4072
309769
 YDOT =     -13543
987017  feet/sec       YDOT =       -4128
207243  meter/sec
 ZDOT =      14945
731177                 ZDOT =        4555
458863


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   17191
57092112  
00016717  00000-0  10270-3 0  9115
2 25544  51
6422 281
7730 0005276  17
1889 342
9442 15
54158222 25385


Satellite: ISS
Catalog Number: 25544
Epoch time:      17191
57092112   =   yrday
fracday
Element set:     911
Inclination:       51
6422  deg
RA of node:       281
7730  deg
Eccentricity:     
0005276     
Arg of perigee:    17
1889  deg
Mean anomaly:     342
9442  deg
Mean motion:   15
54158222  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2538
Checksum:              304


Coasting Arc #13 (Orbit 2552)
---------------------------------------

Vector Time (GMT): 2017/192/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4012802
42                 A    =         6780442
36  meter
 Y    =        3036757
22  meter          E    =           
0014075
 Z    =       -4558360
61                 I    =           51
25902
 XDOT =      -1704
567208                 Wp   =           53
12947
 YDOT =      -6817
518243  meter/sec      RA   =          276
26754  deg
 ZDOT =      -3039
482509                 TA   =          186
26726
                                          MA   =          186
28488
                                          Ha   =            222
280  n
mi
                                          Hp   =            213
642

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13165362
26                 X    =        -4024320
07
 Y    =        9963114
25  feet           Y    =         2991819
42  meter
 Z    =      -14955251
35                 Z    =        -4577880
91
 XDOT =      -5592
412100                 XDOT =       -1613
441156
 YDOT =     -22367
185836  feet/sec       YDOT =       -6836
070034  meter/sec
 ZDOT =      -9972
055476                 ZDOT =       -3047
542026

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14379234
42                 X    =         4382790
65
 Y    =        7951563
73  feet           Y    =         2423636
63  meter
 Z    =      -15041948
13                 Z    =        -4584785
79
 XDOT =     -17670
895937                 XDOT =       -5386
089081
 YDOT =      13015
221547  feet/sec       YDOT =        3967
039528  meter/sec
 ZDOT =     -10006
449264                 ZDOT =       -3049
965736


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   17192
53544485  
00016717  00000-0  10270-3 0  9128
2 25544  51
6407 276
9659 0005303  20
3315 339
8048 15
54128689 25533


Satellite: ISS
Catalog Number: 25544
Epoch time:      17192
53544485   =   yrday
fracday
Element set:     912
Inclination:       51
6407  deg
RA of node:       276
9659  deg
Eccentricity:     
0005303     
Arg of perigee:    20
3315  deg
Mean anomaly:     339
8048  deg
Mean motion:   15
54128689  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2553
Checksum:              325


Coasting Arc #14 (Orbit 2568)
---------------------------------------

Vector Time (GMT): 2017/193/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4178244
67                 A    =         6777726
34  meter
 Y    =       -1306550
40  meter          E    =           
0006069
 Z    =        5168992
41                 I    =           51
24782
 XDOT =        827
917995                 Wp   =           64
97382
 YDOT =       7527
905733  meter/sec      RA   =          271
24463  deg
 ZDOT =       1234
960768                 TA   =           13
12420
                                          MA   =           13
10842
                                          Ha   =            222
125  n
mi
                                          Hp   =            213
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13708151
79                 X    =         4167436
29
 Y    =       -4286582
67  feet           Y    =        -1259887
32  meter
 Z    =       16958636
51                 Z    =         5189262
34
 XDOT =       2716
266388                 XDOT =         737
678699
 YDOT =      24697
853456  feet/sec       YDOT =        7536
659408  meter/sec
 ZDOT =       4051
708556                 ZDOT =        1238
763959

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9579050
33                 X    =        -2919694
54
 Y    =      -10558381
21  feet           Y    =        -3218194
59  meter
 Z    =       17048341
55                 Z    =         5196334
50
 XDOT =      20539
432260                 XDOT =        6260
418953
 YDOT =     -12074
397684  feet/sec       YDOT =       -3680
276414  meter/sec
 ZDOT =       4067
211788                 ZDOT =        1239
686153


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   17193
56426629  
00016717  00000-0  10270-3 0  9132
2 25544  51
6407 271
8373 0005319  23
5336 336
6059 15
54170979 25698


Satellite: ISS
Catalog Number: 25544
Epoch time:      17193
56426629   =   yrday
fracday
Element set:     913
Inclination:       51
6407  deg
RA of node:       271
8373  deg
Eccentricity:     
0005319     
Arg of perigee:    23
5336  deg
Mean anomaly:     336
6059  deg
Mean motion:   15
54170979  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2569
Checksum:              334


Coasting Arc #15 (Orbit 2583)
---------------------------------------

Vector Time (GMT): 2017/194/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4263582
31                 A    =         6777503
21  meter
 Y    =        -511693
85  meter          E    =           
0017388
 Z    =       -5257972
52                 I    =           51
24624
 XDOT =         58
796827                 Wp   =           78
31319
 YDOT =      -7624
010291  meter/sec      RA   =          266
21728  deg
 ZDOT =        699
704496                 TA   =          198
38528
                                          MA   =          198
44820
                                          Ha   =            222
424  n
mi
                                          Hp   =            213
378

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13988130
95                 X    =        -4232003
26
 Y    =       -1678785
59  feet           Y    =         -559195
17  meter
 Z    =      -17250566
01                 Z    =        -5278606
72
 XDOT =        192
902976                 XDOT =         140
647377
 YDOT =     -25013
157123  feet/sec       YDOT =       -7622
895181  meter/sec
 ZDOT =       2295
618426                 ZDOT =         700
188362

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4505007
82                 X    =         1373126
38
 Y    =       13230378
25  feet           Y    =         4032619
29  meter
 Z    =      -17341572
95                 Z    =        -5285711
43
 XDOT =     -21649
268708                 XDOT =       -6598
697102
 YDOT =      10361
886839  feet/sec       YDOT =        3158
303108  meter/sec
 ZDOT =       2299
035909                 ZDOT =         700
746145


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   17194
52878585  
00016717  00000-0  10270-3 0  9142
2 25544  51
6400 267
0292 0005494  26
7655 333
3780 15
54134169 25844


Satellite: ISS
Catalog Number: 25544
Epoch time:      17194
52878585   =   yrday
fracday
Element set:     914
Inclination:       51
6400  deg
RA of node:       267
0292  deg
Eccentricity:     
0005494     
Arg of perigee:    26
7655  deg
Mean anomaly:     333
3780  deg
Mean motion:   15
54134169  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2584
Checksum:              330


Coasting Arc #16 (Orbit 2599)
---------------------------------------

Vector Time (GMT): 2017/195/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4227906
30                 A    =         6779398
53  meter
 Y    =        2306290
44  meter          E    =           
0012468
 Z    =        4766819
47                 I    =           51
25641
 XDOT =       -984
024375                 Wp   =           47
83747
 YDOT =       7158
061610  meter/sec      RA   =          261
19203  deg
 ZDOT =      -2577
871362                 TA   =           67
74930
                                          MA   =           67
61711
                                          Ha   =            222
333  n
mi
                                          Hp   =            213
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13871083
66                 X    =         4178647
93
 Y    =        7566569
69  feet           Y    =         2353294
05  meter
 Z    =       15639171
50                 Z    =         4787237
59
 XDOT =      -3228
426428                 XDOT =       -1051
472685
 YDOT =      23484
454102  feet/sec       YDOT =        7146
680610  meter/sec
 ZDOT =      -8457
583209                 ZDOT =       -2582
814782

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         576017
53                 X    =          175570
14
 Y    =      -15700717
62  feet           Y    =        -4785578
73  meter
 Z    =       15728931
75                 Z    =         4794178
40
 XDOT =      21261
170473                 XDOT =        6480
404760
 YDOT =      -7756
921632  feet/sec       YDOT =       -2364
309714  meter/sec
 ZDOT =      -8480
591933                 ZDOT =       -2584
884421


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   17195
55760232  
00016717  00000-0  10270-3 0  9156
2 25544  51
6402 261
9002 0005549  30
1066 330
0405 15
54187204 26009


Satellite: ISS
Catalog Number: 25544
Epoch time:      17195
55760232   =   yrday
fracday
Element set:     915
Inclination:       51
6402  deg
RA of node:       261
9002  deg
Eccentricity:     
0005549     
Arg of perigee:    30
1066  deg
Mean anomaly:     330
0405  deg
Mean motion:   15
54187204  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2600
Checksum:              269
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