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

 
Date: January 28th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


033/17:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 216 5

039/16:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 215 6

040/11:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 215 6

Coasting Arc #1 (Orbit 3354)
---------------------------------------

Vector Time (GMT): 2019/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3855230
45                 A    =         6781426
77  meter
 Y    =        2569009
56  meter          E    =           
0002096
 Z    =        4950341
58                 I    =           51
46796
 XDOT =      -5791
242222                 Wp   =           71
59812
 YDOT =       4541
947359  meter/sec      RA   =          335
36453  deg
 ZDOT =       2152
935654                 TA   =          357
36831
                                          MA   =          357
36942
                                          Ha   =            221
993  n
mi
                                          Hp   =            217
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12648393
85                 X    =         3802170
83
 Y    =        8428509
07  feet           Y    =         2611824
72  meter
 Z    =       16241278
15                 Z    =         4968939
76
 XDOT =     -19000
138525                 XDOT =       -5852
058776
 YDOT =      14901
402096  feet/sec       YDOT =        4476
845585  meter/sec
 ZDOT =       7063
437186                 ZDOT =        2124
656659

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         703841
38                 X    =          214530
85
 Y    =       15093209
76  feet           Y    =         4600410
33  meter
 Z    =       16324839
19                 Z    =         4975810
99
 XDOT =     -22216
977183                 XDOT =       -6771
734645
 YDOT =      -6465
486818  feet/sec       YDOT =       -1970
680382  meter/sec
 ZDOT =       6935
246997                 ZDOT =        2113
863285


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   19028
55195016  
00016717  00000-0  10270-3 0  9009
2 25544  51
6399 335
6965 0005126 321
6683  38
4105 15
53235487 33555


Satellite: ISS
Catalog Number: 25544
Epoch time:      19028
55195016   =   yrday
fracday
Element set:     900
Inclination:       51
6399  deg
RA of node:       335
6965  deg
Eccentricity:     
0005126     
Arg of perigee:   321
6683  deg
Mean anomaly:      38
4105  deg
Mean motion:   15
53235487  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3355
Checksum:              318


Coasting Arc #2 (Orbit 3369)
---------------------------------------

Vector Time (GMT): 2019/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2682361
63                 A    =         6780168
76  meter
 Y    =       -3317727
68  meter          E    =           
0012980
 Z    =       -5280262
99                 I    =           51
43346
 XDOT =       6382
613173                 Wp   =           65
13224
 YDOT =      -4187
983213  meter/sec      RA   =          330
36241  deg
 ZDOT =       -606
762016                 TA   =          199
02743
                                          MA   =          199
07596
                                          Ha   =            222
275  n
mi
                                          Hp   =            216
932

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8800399
05                 X    =        -2619414
27
 Y    =      -10884933
34  feet           Y    =        -3347371
64  meter
 Z    =      -17323697
47                 Z    =        -5293139
91
 XDOT =      20940
331932                 XDOT =        6431
917289
 YDOT =     -13740
102405  feet/sec       YDOT =       -4116
332693  meter/sec
 ZDOT =      -1990
689030                 ZDOT =        -575
638434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3334183
94                 X    =         1016259
27
 Y    =      -13520772
97  feet           Y    =        -4121131
60  meter
 Z    =      -17381346
53                 Z    =        -5297834
42
 XDOT =      22679
936667                 XDOT =        6912
844696
 YDOT =       7988
214657  feet/sec       YDOT =        2434
807827  meter/sec
 ZDOT =      -1849
722753                 ZDOT =        -563
795495


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   19029
51705944  
00016717  00000-0  10270-3 0  9014
2 25544  51
6398 330
8918 0005110 326
2721  33
8105 15
53199543 33704


Satellite: ISS
Catalog Number: 25544
Epoch time:      19029
51705944   =   yrday
fracday
Element set:     901
Inclination:       51
6398  deg
RA of node:       330
8918  deg
Eccentricity:     
0005110     
Arg of perigee:   326
2721  deg
Mean anomaly:      33
8105  deg
Mean motion:   15
53199543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3370
Checksum:              302


Coasting Arc #3 (Orbit 3385)
---------------------------------------

Vector Time (GMT): 2019/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1446758
76                 A    =         6780366
26  meter
 Y    =        4070553
33  meter          E    =           
0006502
 Z    =        5226564
79                 I    =           51
40660
 XDOT =      -6669
831453                 Wp   =            3
61821
 YDOT =       3648
914962  meter/sec      RA   =          325
35778  deg
 ZDOT =       -989
146899                 TA   =           95
92013
                                          MA   =           95
84601
                                          Ha   =            222
381  n
mi
                                          Hp   =            216
909

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4746583
86                 X    =         1375745
81
 Y    =       13354833
77  feet           Y    =         4086334
76  meter
 Z    =       17147522
26                 Z    =         5233420
15
 XDOT =     -21882
649123                 XDOT =       -6705
334284
 YDOT =      11971
505780  feet/sec       YDOT =        3574
129783  meter/sec
 ZDOT =      -3245
232609                 ZDOT =       -1021
632044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7558321
84                 X    =        -2303776
50
 Y    =       11946144
64  feet           Y    =         3641184
89  meter
 Z    =       17177909
14                 Z    =         5235826
70
 XDOT =     -22114
890764                 XDOT =       -6740
618705
 YDOT =      -9083
898840  feet/sec       YDOT =       -2768
772366  meter/sec
 ZDOT =      -3392
260945                 ZDOT =       -1033
961136


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   19030
54650498  
00016717  00000-0  10270-3 0  9023
2 25544  51
6405 325
7679 0005226 329
7068  30
3781 15
53214998 33861


Satellite: ISS
Catalog Number: 25544
Epoch time:      19030
54650498   =   yrday
fracday
Element set:     902
Inclination:       51
6405  deg
RA of node:       325
7679  deg
Eccentricity:     
0005226     
Arg of perigee:   329
7068  deg
Mean anomaly:      30
3781  deg
Mean motion:   15
53214998  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3386
Checksum:              328


Coasting Arc #4 (Orbit 3400)
---------------------------------------

Vector Time (GMT): 2019/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -272802
98                 A    =         6782162
00  meter
 Y    =       -4772129
72  meter          E    =           
0008785
 Z    =       -4818531
65                 I    =           51
38590
 XDOT =       6633
630307                 Wp   =           82
18795
 YDOT =      -2901
099717  meter/sec      RA   =          320
35238  deg
 ZDOT =       2502
694325                 TA   =          212
50025
                                          MA   =          212
55437
                                          Ha   =            222
539  n
mi
                                          Hp   =            216
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -895022
90                 X    =         -196014
09
 Y    =      -15656593
57  feet           Y    =        -4774750
85  meter
 Z    =      -15808830
86                 Z    =        -4819670
49
 XDOT =      21763
878961                 XDOT =        6653
421727
 YDOT =      -9518
043691  feet/sec       YDOT =       -2826
807279  meter/sec
 ZDOT =       8210
939387                 ZDOT =        2534
965372

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11572868
32                 X    =         3527410
26
 Y    =      -10576200
46  feet           Y    =        -3223625
90  meter
 Z    =      -15813343
24                 Z    =        -4819907
02
 XDOT =      20387
988663                 XDOT =        6214
258944
 YDOT =       9839
206781  feet/sec       YDOT =        2998
990227  meter/sec
 ZDOT =       8356
896022                 ZDOT =        2547
181907


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   19031
51160818  
00016717  00000-0  10270-3 0  9034
2 25544  51
6406 320
9629 0005205 334
6950  25
3947 15
53213160 34012


Satellite: ISS
Catalog Number: 25544
Epoch time:      19031
51160818   =   yrday
fracday
Element set:     903
Inclination:       51
6406  deg
RA of node:       320
9629  deg
Eccentricity:     
0005205     
Arg of perigee:   334
6950  deg
Mean anomaly:      25
3947  deg
Mean motion:   15
53213160  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3401
Checksum:              280


Coasting Arc #5 (Orbit 3416)
---------------------------------------

Vector Time (GMT): 2019/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -837798
91                 A    =         6785082
25  meter
 Y    =        5377074
57  meter          E    =           
0011073
 Z    =        4050283
53                 I    =           51
37059
 XDOT =      -6338
271506                 Wp   =           50
09733
 YDOT =       1928
331460  meter/sec      RA   =          315
35218  deg
 ZDOT =      -3857
080767                 TA   =           80
05984
                                          MA   =           79
93488
                                          Ha   =            222
684  n
mi
                                          Hp   =            216
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2748684
08                 X    =         -917538
20
 Y    =       17641320
77  feet           Y    =         5367259
71  meter
 Z    =       13288331
79                 Z    =         4046020
45
 XDOT =     -20794
854022                 XDOT =       -6340
628437
 YDOT =       6326
546784  feet/sec       YDOT =        1857
439464  meter/sec
 ZDOT =     -12654
464459                 ZDOT =       -3887
874691

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15254292
94                 X    =        -4649508
49
 Y    =        9306297
19  feet           Y    =         2836559
38  meter
 Z    =       13268406
23                 Z    =         4044210
22
 XDOT =     -17586
074680                 XDOT =       -5360
235563
 YDOT =     -10519
942822  feet/sec       YDOT =       -3206
478572  meter/sec
 ZDOT =     -12793
625294                 ZDOT =       -3899
496990


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   19032
54105046  
00016717  00000-0  10270-3 0  9041
2 25544  51
6405 315
8393 0005209 337
9854  22
1074 15
53207542 34175


Satellite: ISS
Catalog Number: 25544
Epoch time:      19032
54105046   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:       315
8393  deg
Eccentricity:     
0005209     
Arg of perigee:   337
9854  deg
Mean anomaly:      22
1074  deg
Mean motion:   15
53207542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3417
Checksum:              290


Coasting Arc #6 (Orbit 3431)
---------------------------------------

Vector Time (GMT): 2019/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1771896
48                 A    =         6788141
98  meter
 Y    =       -5812725
58  meter          E    =           
0006985
 Z    =       -3019117
12                 I    =           51
35867
 XDOT =       5824
671690                 Wp   =           20
85826
 YDOT =       -776
360645  meter/sec      RA   =          310
35603  deg
 ZDOT =       4923
111408                 TA   =          304
41569
                                          MA   =          304
48170
                                          Ha   =            222
746  n
mi
                                          Hp   =            216
522

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5813308
66                 X    =         1851429
15
 Y    =      -19070621
97  feet           Y    =        -5792466
20  meter
 Z    =       -9905239
88                 Z    =        -3010317
14
 XDOT =      19109
815256                 XDOT =        5809
007133
 YDOT =      -2547
114976  feet/sec       YDOT =        -711
312848  meter/sec
 ZDOT =      16151
940316                 ZDOT =        4951
366705

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18178115
28                 X    =         5540689
54
 Y    =       -8236425
69  feet           Y    =        -2510462
55  meter
 Z    =       -9864804
79                 Z    =        -3006792
50
 XDOT =      13898
846538                 XDOT =        4236
368425
 YDOT =      11216
429383  feet/sec       YDOT =        3418
767676  meter/sec
 ZDOT =      16279
497973                 ZDOT =        4961
990982


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   19033
50615065  
00016717  00000-0  10270-3 0  9056
2 25544  51
6412 311
0349 0005242 340
8064  19
2890 15
53218606 34328


Satellite: ISS
Catalog Number: 25544
Epoch time:      19033
50615065   =   yrday
fracday
Element set:     905
Inclination:       51
6412  deg
RA of node:       311
0349  deg
Eccentricity:     
0005242     
Arg of perigee:   340
8064  deg
Mean anomaly:      19
2890  deg
Mean motion:   15
53218606  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3432
Checksum:              278


Coasting Arc #7 (Orbit 3435)
---------------------------------------

Vector Time (GMT): 2019/033/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1927003
44                 A    =         6788616
69  meter
 Y    =        5880973
58  meter          E    =           
0011558
 Z    =        2784343
89                 I    =           51
35445
 XDOT =      -5704
343062                 Wp   =           76
60881
 YDOT =        550
795823  meter/sec      RA   =          309
22691  deg
 ZDOT =      -5090
766105                 TA   =           71
70048
                                          MA   =           71
57477
                                          Ha   =            222
689  n
mi
                                          Hp   =            216
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6322189
76                 X    =        -2006147
38
 Y    =       19294532
74  feet           Y    =         5858981
88  meter
 Z    =        9134986
52                 Z    =         2774791
42
 XDOT =     -18715
036293                 XDOT =       -5685
350781
 YDOT =       1807
072909  feet/sec       YDOT =         487
112223  meter/sec
 ZDOT =     -16701
988534                 ZDOT =       -5118
428814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5149139
85                 X    =         1569457
83
 Y    =       19660477
60  feet           Y    =         5992513
57  meter
 Z    =        9091151
46                 Z    =         2770982
97
 XDOT =     -13188
365034                 XDOT =       -4019
813662
 YDOT =      11266
171938  feet/sec       YDOT =        3433
929207  meter/sec
 ZDOT =     -16826
843925                 ZDOT =       -5128
822028


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   19033
76350690  
00016717  00000-0  10270-3 0  9065
2 25544  51
6399 309
7515 0005443 339
1281  20
9649 15
53256327 34363


Satellite: ISS
Catalog Number: 25544
Epoch time:      19033
76350690   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       309
7515  deg
Eccentricity:     
0005443     
Arg of perigee:   339
1281  deg
Mean anomaly:      20
9649  deg
Mean motion:   15
53256327  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3436
Checksum:              322


Coasting Arc #8 (Orbit 3450)
---------------------------------------

Vector Time (GMT): 2019/034/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2659876
83                 A    =         6791041
58  meter
 Y    =       -6055620
97  meter          E    =           
0012141
 Z    =       -1509913
10                 I    =           51
34048
 XDOT =       5024
072556                 Wp   =           17
36666
 YDOT =        781
063123  meter/sec      RA   =          304
23600  deg
 ZDOT =       5741
266308                 TA   =          326
07336
                                          MA   =          326
15096
                                          Ha   =            222
836  n
mi
                                          Hp   =            216
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8726630
00                 X    =         2734728
92
 Y    =      -19867522
88  feet           Y    =        -6025457
83  meter
 Z    =       -4953783
14                 Z    =        -1496811
07
 XDOT =      16483
177678                 XDOT =        4987
077986
 YDOT =       2562
543056  feet/sec       YDOT =         837
038872  meter/sec
 ZDOT =      18836
175550                 ZDOT =        5765
580852

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3835608
35                 X    =        -1169093
43
 Y    =      -21371711
76  feet           Y    =        -6514097
74  meter
 Z    =       -4893929
82                 Z    =        -1491669
81
 XDOT =      13439
795508                 XDOT =        4096
449671
 YDOT =      -6732
726708  feet/sec       YDOT =       -2052
135101  meter/sec
 ZDOT =      18945
760303                 ZDOT =        5774
667740


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   19034
72860595  
00016717  00000-0  10270-3 0  9073
2 25544  51
6383 304
9465 0005183 344
4128  15
6864 15
53215074 34518


Satellite: ISS
Catalog Number: 25544
Epoch time:      19034
72860595   =   yrday
fracday
Element set:     907
Inclination:       51
6383  deg
RA of node:       304
9465  deg
Eccentricity:     
0005183     
Arg of perigee:   344
4128  deg
Mean anomaly:      15
6864  deg
Mean motion:   15
53215074  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3451
Checksum:              315


Coasting Arc #9 (Orbit 3466)
---------------------------------------

Vector Time (GMT): 2019/035/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3249260
20                 A    =         6791820
30  meter
 Y    =        5960835
69  meter          E    =           
0008394
 Z    =          96811
72                 I    =           51
32534
 XDOT =      -4248
778900                 Wp   =          111
86272
 YDOT =      -2212
117393  meter/sec      RA   =          299
24887  deg
 ZDOT =      -5981
737928                 TA   =           67
09078
                                          MA   =           67
00220
                                          Ha   =            222
926  n
mi
                                          Hp   =            216
147

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10660302
51                 X    =        -3316144
70
 Y    =       19556547
54  feet           Y    =         5924126
22  meter
 Z    =         317623
77                 Z    =           80866
03
 XDOT =     -13939
563319                 XDOT =       -4194
671485
 YDOT =      -7257
602996  feet/sec       YDOT =       -2259
327683  meter/sec
 ZDOT =     -19625
124437                 ZDOT =       -6002
244888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2464863
05                 X    =          751290
26
 Y    =       22137432
67  feet           Y    =         6747489
48  meter
 Z    =         244971
84                 Z    =           74667
42
 XDOT =     -13861
830262                 XDOT =       -4225
085864
 YDOT =       1781
173543  feet/sec       YDOT =         542
901696  meter/sec
 ZDOT =     -19717
361473                 ZDOT =       -6009
851777


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   19035
75804100  
00016717  00000-0  10270-3 0  9088
2 25544  51
6378 299
8221 0005414 348
7418  11
3612 15
53269740 34670


Satellite: ISS
Catalog Number: 25544
Epoch time:      19035
75804100   =   yrday
fracday
Element set:     908
Inclination:       51
6378  deg
RA of node:       299
8221  deg
Eccentricity:     
0005414     
Arg of perigee:   348
7418  deg
Mean anomaly:      11
3612  deg
Mean motion:   15
53269740  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3467
Checksum:              312


Coasting Arc #10 (Orbit 3482)
---------------------------------------

Vector Time (GMT): 2019/036/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3645425
60                 A    =         6791255
09  meter
 Y    =       -5570463
16  meter          E    =           
0016422
 Z    =        1291903
45                 I    =           51
30690
 XDOT =       3467
821514                 Wp   =           42
73625
 YDOT =       3623
262872  meter/sec      RA   =          294
25969  deg
 ZDOT =       5805
940984                 TA   =          331
39117
                                          MA   =          331
48118
                                          Ha   =            222
966  n
mi
                                          Hp   =            216
110

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11960057
74                 X    =         3701169
99
 Y    =      -18275797
77  feet           Y    =        -5529385
76  meter
 Z    =        4238528
39                 Z    =         1309746
56
 XDOT =      11377
367171                 XDOT =        3398
846207
 YDOT =      11887
345381  feet/sec       YDOT =        3661
656924  meter/sec
 ZDOT =      19048
362810                 ZDOT =        5822
618280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1065753
78                 X    =         -324841
75
 Y    =      -21799483
17  feet           Y    =        -6644482
47  meter
 Z    =        4319674
83                 Z    =         1316636
89
 XDOT =      14496
347868                 XDOT =        4418
486830
 YDOT =       3100
809102  feet/sec       YDOT =         945
126614  meter/sec
 ZDOT =      19123
163499                 ZDOT =        5828
740235


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   19036
78747777  
00016717  00000-0  10270-3 0  9099
2 25544  51
6371 294
6968 0005083 352
3415   7
7658 15
53215923 34835


Satellite: ISS
Catalog Number: 25544
Epoch time:      19036
78747777   =   yrday
fracday
Element set:     909
Inclination:       51
6371  deg
RA of node:       294
6968  deg
Eccentricity:     
0005083     
Arg of perigee:   352
3415  deg
Mean anomaly:       7
7658  deg
Mean motion:   15
53215923  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3483
Checksum:              348


Coasting Arc #11 (Orbit 3497)
---------------------------------------

Vector Time (GMT): 2019/037/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3929391
48                 A    =         6788919
46  meter
 Y    =        4881554
82  meter          E    =           
0004457
 Z    =       -2618307
61                 I    =           51
28764
 XDOT =      -2683
823180                 Wp   =           58
98934
 YDOT =      -4945
440456  meter/sec      RA   =          289
26654  deg
 ZDOT =      -5196
878299                 TA   =          150
61939
                                          MA   =          150
59433
                                          Ha   =            223
148  n
mi
                                          Hp   =            215
810

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12891704
34                 X    =        -3970968
43
 Y    =       16015599
81  feet           Y    =         4837381
06  meter
 Z    =       -8590248
06                 Z    =        -2637495
76
 XDOT =      -8805
194161                 XDOT =       -2603
079544
 YDOT =     -16225
198346  feet/sec       YDOT =       -4975
001564  meter/sec
 ZDOT =     -17050
125653                 ZDOT =       -5209
718662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -638938
39                 X    =         -194748
42
 Y    =       20512994
41  feet           Y    =         6252360
70  meter
 Z    =       -8677364
68                 Z    =        -2644860
75
 XDOT =     -15200
096026                 XDOT =       -4632
989269
 YDOT =      -7704
250604  feet/sec       YDOT =       -2348
255584  meter/sec
 ZDOT =     -17107
476212                 ZDOT =       -5214
358750


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   19037
75257045  
00016717  00000-0  10270-3 0  9103
2 25544  51
6379 289
8923 0005232 357
8205   2
2923 15
53250459 34987


Satellite: ISS
Catalog Number: 25544
Epoch time:      19037
75257045   =   yrday
fracday
Element set:     910
Inclination:       51
6379  deg
RA of node:       289
8923  deg
Eccentricity:     
0005232     
Arg of perigee:   357
8205  deg
Mean anomaly:       2
2923  deg
Mean motion:   15
53250459  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3498
Checksum:              324


Coasting Arc #12 (Orbit 3513)
---------------------------------------

Vector Time (GMT): 2019/038/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4084430
50                 A    =         6785907
13  meter
 Y    =       -3916712
43  meter          E    =           
0012132
 Z    =        3731756
12                 I    =           51
26619
 XDOT =       1959
373512                 Wp   =           72
11973
 YDOT =       6088
350836  meter/sec      RA   =          284
26584  deg
 ZDOT =       4237
831864                 TA   =          332
76972
                                          MA   =          332
83328
                                          Ha   =            223
039  n
mi
                                          Hp   =            215
808

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13400362
53                 X    =         4109798
37
 Y    =      -12850106
40  feet           Y    =        -3870895
45  meter
 Z    =       12243294
35                 Z    =         3751658
07
 XDOT =       6428
390788                 XDOT =        1870
561708
 YDOT =      19974
904319  feet/sec       YDOT =        6109
765554  meter/sec
 ZDOT =      13903
647848                 ZDOT =        4247
133522

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2613113
65                 X    =          796477
04
 Y    =      -18320738
27  feet           Y    =        -5584161
02  meter
 Z    =       12333506
94                 Z    =         3759252
92
 XDOT =      15935
919823                 XDOT =        4857
268362
 YDOT =      11677
617975  feet/sec       YDOT =        3559
337959  meter/sec
 ZDOT =      13944
921597                 ZDOT =        4250
412103


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   19038
78200149  
00016717  00000-0  10270-3 0  9111
2 25544  51
6365 284
7667 0004991    
7682 359
3477 15
53243958 35140


Satellite: ISS
Catalog Number: 25544
Epoch time:      19038
78200149   =   yrday
fracday
Element set:     911
Inclination:       51
6365  deg
RA of node:       284
7667  deg
Eccentricity:     
0004991     
Arg of perigee:      
7682  deg
Mean anomaly:     359
3477  deg
Mean motion:   15
53243958  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3514
Checksum:              335


Coasting Arc #13 (Orbit 3527)
---------------------------------------

Vector Time (GMT): 2019/039/16:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2566827
10                 A    =         6784675
58  meter
 Y    =       -4738278
48  meter          E    =           
0007995
 Z    =       -4126875
93                 I    =           51
25470
 XDOT =       3947
242157                 Wp   =           70
96035
 YDOT =      -5393
355970  meter/sec      RA   =          279
47230  deg
 ZDOT =       3745
820944                 TA   =          237
81947
                                          MA   =          237
89703
                                          Ha   =            223
253  n
mi
                                          Hp   =            215
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8421348
76                 X    =        -2493605
93
 Y    =      -15545533
06  feet           Y    =        -4766573
37  meter
 Z    =      -13539619
20                 Z    =        -4139166
23
 XDOT =      12950
269544                 XDOT =        3989
064096
 YDOT =     -17694
737436  feet/sec       YDOT =       -5348
981093  meter/sec
 ZDOT =      12289
438794                 ZDOT =        3765
096643

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13164635
94                 X    =        -4012581
03
 Y    =      -11738181
67  feet           Y    =        -3577797
77  meter
 Z    =      -13594537
61                 Z    =        -4143615
06
 XDOT =       5149
819359                 XDOT =        1569
664941
 YDOT =     -20077
713203  feet/sec       YDOT =       -6119
686984  meter/sec
 ZDOT =      12376
977055                 ZDOT =        3772
502606


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   19039
68275357  
00016717  00000-0  10270-3 0  9125
2 25544  51
6361 280
2834 0005128   4
2479 355
8716 15
53229196 35289


Satellite: ISS
Catalog Number: 25544
Epoch time:      19039
68275357   =   yrday
fracday
Element set:     912
Inclination:       51
6361  deg
RA of node:       280
2834  deg
Eccentricity:     
0005128     
Arg of perigee:     4
2479  deg
Mean anomaly:     355
8716  deg
Mean motion:   15
53229196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3528
Checksum:              328


Coasting Arc #14 (Orbit 3540)
---------------------------------------

Vector Time (GMT): 2019/040/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3843489
14                 A    =         6780884
02  meter
 Y    =        2385179
63  meter          E    =           
0009799
 Z    =        5049739
58                 I    =           51
24357
 XDOT =      -2110
343879                 Wp   =           29
35732
 YDOT =       7158
123214  meter/sec      RA   =          275
48206  deg
 ZDOT =      -1764
948791                 TA   =           77
86337
                                          MA   =           77
75361
                                          Ha   =            223
233  n
mi
                                          Hp   =            215
573

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12609872
51                 X    =         3792003
36
 Y    =        7825392
48  feet           Y    =         2427872
64  meter
 Z    =       16567387
08                 Z    =         5068284
27
 XDOT =      -6923
700390                 XDOT =       -2181
658208
 YDOT =      23484
656213  feet/sec       YDOT =        7134
125024  meter/sec
 ZDOT =      -5790
514407                 ZDOT =       -1775
373504

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1785285
59                 X    =          544155
05
 Y    =       14638587
90  feet           Y    =         4461841
59  meter
 Z    =       16650779
75                 Z    =         5075157
67
 XDOT =     -21514
774371                 XDOT =       -6557
703228
 YDOT =       9301
331442  feet/sec       YDOT =        2835
045824  meter/sec
 ZDOT =      -5838
306878                 ZDOT =       -1779
515936


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   19040
51916333  
00016717  00000-0  10270-3 0  9136
2 25544  51
6410 276
1241 0005497   4
2564 355
8634 15
53276563 35418


Satellite: ISS
Catalog Number: 25544
Epoch time:      19040
51916333   =   yrday
fracday
Element set:     913
Inclination:       51
6410  deg
RA of node:       276
1241  deg
Eccentricity:     
0005497     
Arg of perigee:     4
2564  deg
Mean anomaly:     355
8634  deg
Mean motion:   15
53276563  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3541
Checksum:              298


Coasting Arc #15 (Orbit 3555)
---------------------------------------

Vector Time (GMT): 2019/041/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3557018
37                 A    =         6783364
85  meter
 Y    =       -3668009
10  meter          E    =           
0009961
 Z    =       -4469006
20                 I    =           51
24921
 XDOT =       2625
856893                 Wp   =           77
28246
 YDOT =      -6442
478500  meter/sec      RA   =          270
46796  deg
 ZDOT =       3205
989293                 TA   =          225
13328
                                          MA   =          225
21422
                                          Ha   =            223
447  n
mi
                                          Hp   =            215
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11670007
79                 X    =        -3494029
68
 Y    =      -12034150
60  feet           Y    =        -3707434
24  meter
 Z    =      -14662093
84                 Z    =        -4486131
40
 XDOT =       8615
016053                 XDOT =        2682
130670
 YDOT =     -21136
740487  feet/sec       YDOT =       -6412
799501  meter/sec
 ZDOT =      10518
337577                 ZDOT =        3218
881580

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1783344
41                 X    =          543563
38
 Y    =      -16600293
83  feet           Y    =        -5059769
56  meter
 Z    =      -14738954
70                 Z    =        -4492433
39
 XDOT =      20473
764236                 XDOT =        6240
403339
 YDOT =      -7167
896740  feet/sec       YDOT =       -2184
774926  meter/sec
 ZDOT =      10577
168251                 ZDOT =        3223
920883


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   19041
48425230  
00016717  00000-0  10270-3 0  9145
2 25544  51
6407 271
3191 0005575   8
3800 351
7445 15
53242953 35567


Satellite: ISS
Catalog Number: 25544
Epoch time:      19041
48425230   =   yrday
fracday
Element set:     914
Inclination:       51
6407  deg
RA of node:       271
3191  deg
Eccentricity:     
0005575     
Arg of perigee:     8
3800  deg
Mean anomaly:     351
7445  deg
Mean motion:   15
53242953  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3556
Checksum:              296


Coasting Arc #16 (Orbit 3571)
---------------------------------------

Vector Time (GMT): 2019/042/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3228095
23                 A    =         6786470
55  meter
 Y    =        4804694
06  meter          E    =           
0014650
 Z    =        3536982
61                 I    =           51
26006
 XDOT =      -3146
508478                 Wp   =           65
32943
 YDOT =       5399
289068  meter/sec      RA   =          265
46065  deg
 ZDOT =      -4442
198800                 TA   =           72
72084
                                          MA   =           72
56059
                                          Ha   =            223
561  n
mi
                                          Hp   =            215
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10590863
61                 X    =         3156947
39
 Y    =       15763431
96  feet           Y    =         4840395
24  meter
 Z    =       11604273
66                 Z    =         3552490
25
 XDOT =     -10323
190546                 XDOT =       -3185
073536
 YDOT =      17714
202980  feet/sec       YDOT =        5363
886764  meter/sec
 ZDOT =     -14574
143044                 ZDOT =       -4457
577097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5007066
25                 X    =        -1526153
79
 Y    =       18274699
84  feet           Y    =         5570128
51  meter
 Z    =       11673730
32                 Z    =         3558153
00
 XDOT =     -18745
697410                 XDOT =       -5713
688571
 YDOT =       4261
231587  feet/sec       YDOT =        1298
823388  meter/sec
 ZDOT =     -14644
067171                 ZDOT =       -4463
511674


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   19042
51367812  
00016717  00000-0  10270-3 0  9152
2 25544  51
6401 266
1941 0005706  12
5894 347
5399 15
53268461 35723


Satellite: ISS
Catalog Number: 25544
Epoch time:      19042
51367812   =   yrday
fracday
Element set:     915
Inclination:       51
6401  deg
RA of node:       266
1941  deg
Eccentricity:     
0005706     
Arg of perigee:    12
5894  deg
Mean anomaly:     347
5399  deg
Mean motion:   15
53268461  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3572
Checksum:              319


Coasting Arc #17 (Orbit 3586)
---------------------------------------

Vector Time (GMT): 2019/043/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2891789
57                 A    =         6789498
28  meter
 Y    =       -5655197
55  meter          E    =           
0010748
 Z    =       -2387513
18                 I    =           51
27320
 XDOT =       3651
488061                 Wp   =           30
65022
 YDOT =      -4113
548492  meter/sec      RA   =          260
46064  deg
 ZDOT =       5340
578757                 TA   =          302
54113
                                          MA   =          302
64491
                                          Ha   =            223
626  n
mi
                                          Hp   =            215
272

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9487498
57                 X    =        -2816739
55
 Y    =      -18553797
73  feet           Y    =        -5687116
01  meter
 Z    =       -7833048
50                 Z    =        -2401377
78
 XDOT =      11979
947707                 XDOT =        3671
274264
 YDOT =     -13495
894001  feet/sec       YDOT =       -4072
604184  meter/sec
 ZDOT =      17521
583848                 ZDOT =        5358
364316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7487500
21                 X    =         2282190
06
 Y    =      -19422118
66  feet           Y    =        -5919861
77  meter
 Z    =       -7895019
66                 Z    =        -2406401
99
 XDOT =      16549
923005                 XDOT =        5044
416532
 YDOT =       -748
905223  feet/sec       YDOT =        -228
266312  meter/sec
 ZDOT =      17602
228932                 ZDOT =        5365
159378


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   19043
47876489  
00016717  00000-0  10270-3 0  9164
2 25544  51
6398 261
3895 0005634  14
4959 345
6354 15
53225336 35876


Satellite: ISS
Catalog Number: 25544
Epoch time:      19043
47876489   =   yrday
fracday
Element set:     916
Inclination:       51
6398  deg
RA of node:       261
3895  deg
Eccentricity:     
0005634     
Arg of perigee:    14
4959  deg
Mean anomaly:     345
6354  deg
Mean motion:   15
53225336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3587
Checksum:              354
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