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

 
Date: January 22nd 2019

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) : 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


025/12:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 217 5

026/08:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 217 4

033/17:40:00 000 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

Coasting Arc #1 (Orbit 3245)
---------------------------------------

Vector Time (GMT): 2019/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5776207
29                 A    =         6787824
50  meter
 Y    =        1536952
93  meter          E    =           
0008526
 Z    =        3210827
32                 I    =           51
71479
 XDOT =      -3883
546342                 Wp   =           82
10909
 YDOT =      -4546
037243  meter/sec      RA   =           10
18807  deg
 ZDOT =      -4798
271818                 TA   =           60
81428
                                          MA   =           60
72901
                                          Ha   =            221
293  n
mi
                                          Hp   =            217
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18950811
32                 X    =        -5808560
63
 Y    =        5042496
50  feet           Y    =         1472178
22  meter
 Z    =       10534210
37                 Z    =         3182690
95
 XDOT =     -12741
293773                 XDOT =       -3809
115927
 YDOT =     -14914
820352  feet/sec       YDOT =       -4589
049234  meter/sec
 ZDOT =     -15742
361609                 ZDOT =       -4816
955703

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13800187
30                 X    =        -4206297
09
 Y    =      -14027788
91  feet           Y    =        -4275670
06  meter
 Z    =       10406996
56                 Z    =         3172052
55
 XDOT =       5678
974544                 XDOT =        1730
951441
 YDOT =     -17357
631686  feet/sec       YDOT =       -5290
606138  meter/sec
 ZDOT =     -15826
055497                 ZDOT =       -4823
781716


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   19021
53873460  
00016717  00000-0  10270-3 0  9006
2 25544  51
6382  10
6069 0004825 294
9592  65
1058 15
53181150 32468


Satellite: ISS
Catalog Number: 25544
Epoch time:      19021
53873460   =   yrday
fracday
Element set:     900
Inclination:       51
6382  deg
RA of node:        10
6069  deg
Eccentricity:     
0004825     
Arg of perigee:   294
9592  deg
Mean anomaly:      65
1058  deg
Mean motion:   15
53181150  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3246
Checksum:              298


Coasting Arc #2 (Orbit 3260)
---------------------------------------

Vector Time (GMT): 2019/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6405229
77                 A    =         6790496
83  meter
 Y    =       -1003881
92  meter          E    =           
0007459
 Z    =       -2003281
55                 I    =           51
69050
 XDOT =       2469
557420                 Wp   =            1
62535
 YDOT =       4648
106155  meter/sec      RA   =            5
22153  deg
 ZDOT =       5574
621579                 TA   =          336
27458
                                          MA   =          336
30896
                                          Ha   =            221
465  n
mi
                                          Hp   =            217
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21014533
38                 X    =         6425709
97
 Y    =       -3293575
84  feet           Y    =         -932139
57  meter
 Z    =       -6572446
02                 Z    =        -1972118
54
 XDOT =       8102
222508                 XDOT =        2390
319816
 YDOT =      15249
692108  feet/sec       YDOT =        4675
279173  meter/sec
 ZDOT =      18289
440877                 ZDOT =        5586
425177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13573940
96                 X    =         4137337
20
 Y    =       16432811
01  feet           Y    =         5008720
80  meter
 Z    =       -6431652
24                 Z    =        -1960367
60
 XDOT =      -7849
692572                 XDOT =       -2392
586296
 YDOT =      13652
752947  feet/sec       YDOT =        4161
359098  meter/sec
 ZDOT =      18342
067676                 ZDOT =        5590
662228


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   19022
50386641  
00016717  00000-0  10270-3 0  9015
2 25544  51
6380   5
8033 0004651 297
9214  62
1467 15
53166513 32618


Satellite: ISS
Catalog Number: 25544
Epoch time:      19022
50386641   =   yrday
fracday
Element set:     901
Inclination:       51
6380  deg
RA of node:         5
8033  deg
Eccentricity:     
0004651     
Arg of perigee:   297
9214  deg
Mean anomaly:      62
1467  deg
Mean motion:   15
53166513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3261
Checksum:              287


Coasting Arc #3 (Orbit 3276)
---------------------------------------

Vector Time (GMT): 2019/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6740883
18                 A    =         6791940
58  meter
 Y    =         475018
73  meter          E    =           
0008282
 Z    =         638837
78                 I    =           51
66344
 XDOT =       -902
814049                 Wp   =          131
56019
 YDOT =      -4724
186316  meter/sec      RA   =             
25645  deg
 ZDOT =      -5968
845685                 TA   =           41
54838
                                          MA   =           41
48547
                                          Ha   =            221
519  n
mi
                                          Hp   =            217
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22115758
47                 X    =        -6748797
02
 Y    =        1558460
40  feet           Y    =          399593
22  meter
 Z    =        2095924
48                 Z    =          606074
80
 XDOT =      -2961
988350                 XDOT =        -820
927244
 YDOT =     -15499
298938  feet/sec       YDOT =       -4733
824273  meter/sec
 ZDOT =     -19582
827049                 ZDOT =       -5973
032277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12939494
41                 X    =        -3943957
90
 Y    =      -18019525
00  feet           Y    =        -5492351
22  meter
 Z    =        1947992
30                 Z    =          593748
05
 XDOT =      10395
235767                 XDOT =        3168
467862
 YDOT =      -9600
656741  feet/sec       YDOT =       -2926
280175  meter/sec
 ZDOT =     -19601
068427                 ZDOT =       -5974
405657


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   19023
53333781  
00016717  00000-0  10270-3 0  9027
2 25544  51
6391    
6780 0004834 302
8928  57
1759 15
53178894 32773


Satellite: ISS
Catalog Number: 25544
Epoch time:      19023
53333781   =   yrday
fracday
Element set:     902
Inclination:       51
6391  deg
RA of node:          
6780  deg
Eccentricity:     
0004834     
Arg of perigee:   302
8928  deg
Mean anomaly:      57
1759  deg
Mean motion:   15
53178894  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3277
Checksum:              324


Coasting Arc #4 (Orbit 3292)
---------------------------------------

Vector Time (GMT): 2019/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6742089
69                 A    =         6791763
92  meter
 Y    =          41384
64  meter          E    =           
0012644
 Z    =         751064
32                 I    =           51
63001
 XDOT =       -696
458487                 Wp   =           32
18478
 YDOT =       4786
140576  meter/sec      RA   =          355
29178  deg
 ZDOT =       5952
506173                 TA   =          335
93318
                                          MA   =          335
99221
                                          Ha   =            221
544  n
mi
                                          Hp   =            217
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22119716
83                 X    =         6737477
67
 Y    =         135776
38  feet           Y    =          116753
61  meter
 Z    =        2464121
77                 Z    =          783802
85
 XDOT =      -2284
968791                 XDOT =        -778
839951
 YDOT =      15702
560945  feet/sec       YDOT =        4777
891719  meter/sec
 ZDOT =      19529
219729                 ZDOT =        5948
922998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11806262
34                 X    =         3598548
76
 Y    =       18685891
88  feet           Y    =         5695459
85  meter
 Z    =        2611860
99                 Z    =          796095
23
 XDOT =     -13164
296634                 XDOT =       -4012
477614
 YDOT =       5574
742324  feet/sec       YDOT =        1699
181460  meter/sec
 ZDOT =      19512
392587                 ZDOT =        5947
377260


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   19024
56280591  
00016717  00000-0  10270-3 0  9032
2 25544  51
6393 355
5540 0004754 305
1801  54
8906 15
53200446 32933


Satellite: ISS
Catalog Number: 25544
Epoch time:      19024
56280591   =   yrday
fracday
Element set:     903
Inclination:       51
6393  deg
RA of node:       355
5540  deg
Eccentricity:     
0004754     
Arg of perigee:   305
1801  deg
Mean anomaly:      54
8906  deg
Mean motion:   15
53200446  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3293
Checksum:              299


Coasting Arc #5 (Orbit 3307)
---------------------------------------

Vector Time (GMT): 2019/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6426529
19                 A    =         6790145
48  meter
 Y    =        -598293
68  meter          E    =           
0001528
 Z    =       -2106509
77                 I    =           51
59150
 XDOT =       2255
230244                 Wp   =          161
25523
 YDOT =      -4819
352418  meter/sec      RA   =          350
32237  deg
 ZDOT =      -5513
974168                 TA   =           42
06990
                                          MA   =           42
05817
                                          Ha   =            221
814  n
mi
                                          Hp   =            217
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21084413
35                 X    =        -6409129
23
 Y    =       -1962905
77  feet           Y    =         -670062
36  meter
 Z    =       -6911121
30                 Z    =        -2137684
53
 XDOT =       7399
049356                 XDOT =        2335
737262
 YDOT =     -15811
523681  feet/sec       YDOT =       -4793
682818  meter/sec
 ZDOT =     -18090
466430                 ZDOT =       -5502
823710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10014511
70                 X    =        -3052423
17
 Y    =      -18605159
08  feet           Y    =        -5670852
49  meter
 Z    =       -7051715
69                 Z    =        -2149362
94
 XDOT =      15974
453001                 XDOT =        4869
013275
 YDOT =      -1764
257501  feet/sec       YDOT =        -537
745686  meter/sec
 ZDOT =     -18039
493456                 ZDOT =       -5498
437605


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   19025
52793381  
00016717  00000-0  10270-3 0  9046
2 25544  51
6393 350
7498 0004927 311
0289  49
0437 15
53174380 33089


Satellite: ISS
Catalog Number: 25544
Epoch time:      19025
52793381   =   yrday
fracday
Element set:     904
Inclination:       51
6393  deg
RA of node:       350
7498  deg
Eccentricity:     
0004927     
Arg of perigee:   311
0289  deg
Mean anomaly:      49
0437  deg
Mean motion:   15
53174380  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3308
Checksum:              319


Coasting Arc #6 (Orbit 3308)
---------------------------------------

Vector Time (GMT): 2019/025/12:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4245062
01                 A    =         6783501
75  meter
 Y    =        2849427
97  meter          E    =           
0004560
 Z    =        4454406
01                 I    =           51
56893
 XDOT =      -5891
891861                 Wp   =           92
00464
 YDOT =       3659
005043  meter/sec      RA   =          350
13715  deg
 ZDOT =       3271
316950                 TA   =          324
98465
                                          MA   =          325
01462
                                          Ha   =            221
601  n
mi
                                          Hp   =            217
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13927368
82                 X    =         4191246
82
 Y    =        9348516
98  feet           Y    =         2896598
40  meter
 Z    =       14614192
93                 Z    =         4474895
75
 XDOT =     -19330
353874                 XDOT =       -5948
259909
 YDOT =      12004
609722  feet/sec       YDOT =        3592
802687  meter/sec
 ZDOT =      10732
667159                 ZDOT =        3242
559961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3854556
29                 X    =         1174868
76
 Y    =       16242203
96  feet           Y    =         4950623
77  meter
 Z    =       14706264
42                 Z    =         4482469
40
 XDOT =     -21224
097644                 XDOT =       -6469
104962
 YDOT =      -4571
957829  feet/sec       YDOT =       -1393
532746  meter/sec
 ZDOT =      10602
403486                 ZDOT =        3231
612583


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   19025
59227437  
00016717  00000-0  10270-3 0  9058
2 25544  51
6399 350
4300 0004949 309
2210  50
8502 15
53203285 33092


Satellite: ISS
Catalog Number: 25544
Epoch time:      19025
59227437   =   yrday
fracday
Element set:     905
Inclination:       51
6399  deg
RA of node:       350
4300  deg
Eccentricity:     
0004949     
Arg of perigee:   309
2210  deg
Mean anomaly:      50
8502  deg
Mean motion:   15
53203285  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3309
Checksum:              294


Coasting Arc #7 (Orbit 3321)
---------------------------------------

Vector Time (GMT): 2019/026/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4758958
72                 A    =         6784358
67  meter
 Y    =        2291978
16  meter          E    =           
0005923
 Z    =        4252122
05                 I    =           51
54318
 XDOT =      -5267
260160                 Wp   =           85
41513
 YDOT =       4259
150833  meter/sec      RA   =          345
97365  deg
 ZDOT =       3595
471471                 TA   =          327
78897
                                          MA   =          327
82514
                                          Ha   =            221
790  n
mi
                                          Hp   =            217
434

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15613381
62                 X    =         4712321
38
 Y    =        7519613
40  feet           Y    =         2344935
46  meter
 Z    =       13950531
67                 Z    =         4275125
59
 XDOT =     -17281
037270                 XDOT =       -5331
960219
 YDOT =      13973
591973  feet/sec       YDOT =        4199
886956  meter/sec
 ZDOT =      11796
166244                 ZDOT =        3569
728321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10317181
95                 X    =        -3144677
06
 Y    =       13819550
51  feet           Y    =         4212199
00  meter
 Z    =       14054016
70                 Z    =         4283664
29
 XDOT =      -9435
500839                 XDOT =       -2875
940656
 YDOT =     -18934
576424  feet/sec       YDOT =       -5771
258894  meter/sec
 ZDOT =      11679
431611                 ZDOT =        3559
890755


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   19026
42871717  
00016717  00000-0  10270-3 0  9068
2 25544  51
6389 346
2662 0004845 313
4971  46
5778 15
53162712 33222


Satellite: ISS
Catalog Number: 25544
Epoch time:      19026
42871717   =   yrday
fracday
Element set:     906
Inclination:       51
6389  deg
RA of node:       346
2662  deg
Eccentricity:     
0004845     
Arg of perigee:   313
4971  deg
Mean anomaly:      46
5778  deg
Mean motion:   15
53162712  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3322
Checksum:              324


Coasting Arc #8 (Orbit 3336)
---------------------------------------

Vector Time (GMT): 2019/027/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3647988
43                 A    =         6781696
05  meter
 Y    =       -2897202
70  meter          E    =           
0011197
 Z    =       -4938442
49                 I    =           51
50276
 XDOT =       6157
743716                 Wp   =           51
12291
 YDOT =      -3981
287913  meter/sec      RA   =          340
98174  deg
 ZDOT =      -2209
506474                 TA   =          197
22649
                                          MA   =          197
26452
                                          Ha   =            222
030  n
mi
                                          Hp   =            217
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11968465
97                 X    =        -3591332
09
 Y    =       -9505258
20  feet           Y    =        -2937680
30  meter
 Z    =      -16202239
12                 Z    =        -4956025
17
 XDOT =      20202
571246                 XDOT =        6212
538350
 YDOT =     -13061
968220  feet/sec       YDOT =       -3912
121368  meter/sec
 ZDOT =      -7249
036989                 ZDOT =       -2179
461776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11404649
95                 X    =         3476137
31
 Y    =      -10048077
41  feet           Y    =        -3062653
99  meter
 Z    =      -16281178
20                 Z    =        -4962503
12
 XDOT =       8651
992388                 XDOT =        2637
127280
 YDOT =      21363
870393  feet/sec       YDOT =        6511
707696  meter/sec
 ZDOT =      -7112
943687                 ZDOT =       -2168
025236


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   19027
39384042  
00016717  00000-0  10270-3 0  9076
2 25544  51
6393 341
4622 0004761 318
3350  41
7439 15
53174230 33377


Satellite: ISS
Catalog Number: 25544
Epoch time:      19027
39384042   =   yrday
fracday
Element set:     907
Inclination:       51
6393  deg
RA of node:       341
4622  deg
Eccentricity:     
0004761     
Arg of perigee:   318
3350  deg
Mean anomaly:      41
7439  deg
Mean motion:   15
53174230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3337
Checksum:              297


Coasting Arc #9 (Orbit 3352)
---------------------------------------

Vector Time (GMT): 2019/028/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2401356
55                 A    =         6780276
43  meter
 Y    =        3525364
28  meter          E    =           
0002650
 Z    =        5270532
25                 I    =           51
46564
 XDOT =      -6741
242637                 Wp   =          351
04834
 YDOT =       3590
290743  meter/sec      RA   =          335
98242  deg
 ZDOT =        672
571132                 TA   =           92
52813
                                          MA   =           92
49780
                                          Ha   =            222
125  n
mi
                                          Hp   =            217
209

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7878466
38                 X    =         2336155
47
 Y    =       11566155
79  feet           Y    =         3551853
33  meter
 Z    =       17291772
48                 Z    =         5282038
66
 XDOT =     -22116
937784                 XDOT =       -6784
156194
 YDOT =      11779
169104  feet/sec       YDOT =        3514
665519  meter/sec
 ZDOT =       2206
598201                 ZDOT =         639
720918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12630993
02                 X    =        -3849926
67
 Y    =        5875597
39  feet           Y    =         1790882
08  meter
 Z    =       17343210
72                 Z    =         5286210
63
 XDOT =      -7777
459912                 XDOT =       -2370
569781
 YDOT =     -22768
694805  feet/sec       YDOT =       -6939
898177  meter/sec
 ZDOT =       2057
911346                 ZDOT =         627
251378


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
42330330  
00016717  00000-0  10270-3 0  9083
2 25544  51
6382 336
3374 0004923 321
8048  38
2754 15
53167714 33533


Satellite: ISS
Catalog Number: 25544
Epoch time:      19028
42330330   =   yrday
fracday
Element set:     908
Inclination:       51
6382  deg
RA of node:       336
3374  deg
Eccentricity:     
0004923     
Arg of perigee:   321
8048  deg
Mean anomaly:      38
2754  deg
Mean motion:   15
53167714  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3353
Checksum:              300


Coasting Arc #10 (Orbit 3367)
---------------------------------------

Vector Time (GMT): 2019/029/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1135032
56                 A    =         6780476
27  meter
 Y    =       -4154128
93  meter          E    =           
0011690
 Z    =       -5246974
49                 I    =           51
43604
 XDOT =       6970
298335                 Wp   =           78
53821
 YDOT =      -3042
073669  meter/sec      RA   =          330
98019  deg
 ZDOT =        904
633084                 TA   =          200
12713
                                          MA   =          200
17326
                                          Ha   =            222
288  n
mi
                                          Hp   =            217
054

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3723860
10                 X    =        -1063009
01
 Y    =      -13629031
92  feet           Y    =        -4166418
83  meter
 Z    =      -17214483
22                 Z    =        -5252313
14
 XDOT =      22868
432856                 XDOT =        6999
403468
 YDOT =      -9980
556656  feet/sec       YDOT =       -2963
964216  meter/sec
 ZDOT =       2967
956313                 ZDOT =         938
562361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13997877
81                 X    =         4266553
16
 Y    =       -1693045
25  feet           Y    =         -516040
19  meter
 Z    =      -17238013
00                 Z    =        -5254146
36
 XDOT =       6608
030285                 XDOT =        2014
127631
 YDOT =      22986
116782  feet/sec       YDOT =        7006
168395  meter/sec
 ZDOT =       3121
428112                 ZDOT =         951
411289


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
38842373  
00016717  00000-0  10270-3 0  9095
2 25544  51
6380 331
5336 0004945 325
4594  34
6236 15
53159496 33685


Satellite: ISS
Catalog Number: 25544
Epoch time:      19029
38842373   =   yrday
fracday
Element set:     909
Inclination:       51
6380  deg
RA of node:       331
5336  deg
Eccentricity:     
0004945     
Arg of perigee:   325
4594  deg
Mean anomaly:      34
6236  deg
Mean motion:   15
53159496  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3368
Checksum:              334


Coasting Arc #11 (Orbit 3383)
---------------------------------------

Vector Time (GMT): 2019/030/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -123421
31                 A    =         6782136
84  meter
 Y    =        4745998
73  meter          E    =           
0008601
 Z    =        4843316
09                 I    =           51
41355
 XDOT =      -6892
891290                 Wp   =           23
89502
 YDOT =       2312
033674  meter/sec      RA   =          325
97710  deg
 ZDOT =      -2431
994182                 TA   =           90
09804
                                          MA   =           89
99947
                                          Ha   =            222
398  n
mi
                                          Hp   =            216
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -404925
57                 X    =         -200009
02
 Y    =       15570861
96  feet           Y    =         4744190
15  meter
 Z    =       15890144
64                 Z    =         4842530
70
 XDOT =     -22614
472735                 XDOT =       -6906
419713
 YDOT =       7585
412315  feet/sec       YDOT =        2234
876997  meter/sec
 ZDOT =      -7978
983538                 ZDOT =       -2465
509540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15395841
26                 X    =        -4692652
42
 Y    =       -2390887
48  feet           Y    =         -728742
50  meter
 Z    =       15885972
82                 Z    =         4842044
51
 XDOT =      -4974
643897                 XDOT =       -1516
271460
 YDOT =     -22189
748143  feet/sec       YDOT =       -6763
435234  meter/sec
 ZDOT =      -8130
483185                 ZDOT =       -2478
171275


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
41788304  
00016717  00000-0  10270-3 0  9106
2 25544  51
6383 326
4086 0005028 328
7275  31
3577 15
53186202 33843


Satellite: ISS
Catalog Number: 25544
Epoch time:      19030
41788304   =   yrday
fracday
Element set:     910
Inclination:       51
6383  deg
RA of node:       326
4086  deg
Eccentricity:     
0005028     
Arg of perigee:   328
7275  deg
Mean anomaly:      31
3577  deg
Mean motion:   15
53186202  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3384
Checksum:              303


Coasting Arc #12 (Orbit 3398)
---------------------------------------

Vector Time (GMT): 2019/031/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1250993
27                 A    =         6784972
66  meter
 Y    =       -5246630
40  meter          E    =           
0005241
 Z    =       -4118865
27                 I    =           51
39638
 XDOT =       6519
222554                 Wp   =           65
28008
 YDOT =      -1404
228509  meter/sec      RA   =          320
97790  deg
 ZDOT =       3774
686746                 TA   =          243
76746
                                          MA   =          243
82134
                                          Ha   =            222
586  n
mi
                                          Hp   =            216
853

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4104308
63                 X    =         1329576
39
 Y    =      -17213354
32  feet           Y    =        -5232201
37  meter
 Z    =      -13513337
52                 Z    =        -4112597
88
 XDOT =      21388
525440                 XDOT =        6516
105516
 YDOT =      -4607
048913  feet/sec       YDOT =       -1331
343597  meter/sec
 ZDOT =      12384
142868                 ZDOT =        3806
346487

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16685556
82                 X    =         5085757
72
 Y    =        5959780
75  feet           Y    =         1816541
17  meter
 Z    =      -13484376
66                 Z    =        -4110038
01
 XDOT =       2803
005475                 XDOT =         854
356069
 YDOT =      20451
729705  feet/sec       YDOT =        6233
687214  meter/sec
 ZDOT =      12527
146342                 ZDOT =        3818
274205


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
38299899  
00016717  00000-0  10270-3 0  9110
2 25544  51
6388 321
6045 0005112 333
6906  26
3986 15
53166832 33991


Satellite: ISS
Catalog Number: 25544
Epoch time:      19031
38299899   =   yrday
fracday
Element set:     911
Inclination:       51
6388  deg
RA of node:       321
6045  deg
Eccentricity:     
0005112     
Arg of perigee:   333
6906  deg
Mean anomaly:      26
3986  deg
Mean motion:   15
53166832  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3399
Checksum:              335


Coasting Arc #13 (Orbit 3414)
---------------------------------------

Vector Time (GMT): 2019/032/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2258948
48                 A    =         6788062
37  meter
 Y    =        5607059
60  meter          E    =           
0011461
 Z    =        3082791
77                 I    =           51
38141
 XDOT =      -5912
912106                 Wp   =           72
14836
 YDOT =        304
916526  meter/sec      RA   =          315
98355  deg
 ZDOT =      -4868
922481                 TA   =           72
29810
                                          MA   =           72
17302
                                          Ha   =            222
675  n
mi
                                          Hp   =            216
698

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7411248
30                 X    =        -2336454
48
 Y    =       18395864
84  feet           Y    =         5581364
98  meter
 Z    =       10114146
23                 Z    =         3071630
86
 XDOT =     -19399
317933                 XDOT =       -5892
232299
 YDOT =       1000
382303  feet/sec       YDOT =         238
910044  meter/sec
 ZDOT =     -15974
155120                 ZDOT =       -4897
594338

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17678548
70                 X    =        -5388421
64
 Y    =       -9046207
47  feet           Y    =        -2757284
04  meter
 Z    =       10063073
34                 Z    =         3067224
75
 XDOT =         18
258171                 XDOT =           5
565091
 YDOT =     -18016
935638  feet/sec       YDOT =       -5491
561983  meter/sec
 ZDOT =     -16103
533726                 ZDOT =       -4908
357080


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
41245467  
00016717  00000-0  10270-3 0  9128
2 25544  51
6383 316
4798 0005195 337
0156  23
0763 15
53195200 34156


Satellite: ISS
Catalog Number: 25544
Epoch time:      19032
41245467   =   yrday
fracday
Element set:     912
Inclination:       51
6383  deg
RA of node:       316
4798  deg
Eccentricity:     
0005195     
Arg of perigee:   337
0156  deg
Mean anomaly:      23
0763  deg
Mean motion:   15
53195200  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3415
Checksum:              298


Coasting Arc #14 (Orbit 3429)
---------------------------------------

Vector Time (GMT): 2019/033/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3048182
44                 A    =         6790628
20  meter
 Y    =       -5769806
75  meter          E    =           
0010866
 Z    =       -1857077
57                 I    =           51
36712
 XDOT =       5144
865781                 Wp   =           14
76851
 YDOT =        917
482641  meter/sec      RA   =          310
99450  deg
 ZDOT =       5611
728556                 TA   =          324
71969
                                          MA   =          324
79156
                                          Ha   =            222
768  n
mi
                                          Hp   =            216
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10000598
57                 X    =         3121495
93
 Y    =      -18929812
16  feet           Y    =        -5735309
86  meter
 Z    =       -6092774
17                 Z    =        -1842093
13
 XDOT =      16879
480910                 XDOT =        5106
965869
 YDOT =       3010
113650  feet/sec       YDOT =         974
804019  meter/sec
 ZDOT =      18411
182927                 ZDOT =        5636
627753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18185586
08                 X    =         5542966
64
 Y    =       11334115
79  feet           Y    =         3454638
49  meter
 Z    =       -6024444
82                 Z    =        -1836250
78
 XDOT =      -3343
687382                 XDOT =       -1019
155914
 YDOT =      15179
735300  feet/sec       YDOT =        4626
783319  meter/sec
 ZDOT =      18523
385863                 ZDOT =        5645
928011


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
37756805  
00016717  00000-0  10270-3 0  9138
2 25544  51
6386 311
6760 0005135 340
5883  19
5073 15
53189892 34306


Satellite: ISS
Catalog Number: 25544
Epoch time:      19033
37756805   =   yrday
fracday
Element set:     913
Inclination:       51
6386  deg
RA of node:       311
6760  deg
Eccentricity:     
0005135     
Arg of perigee:   340
5883  deg
Mean anomaly:      19
5073  deg
Mean motion:   15
53189892  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3430
Checksum:              318


Coasting Arc #15 (Orbit 3435)
---------------------------------------

Vector Time (GMT): 2019/033/17:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5298582
45                 A    =         6789653
39  meter
 Y    =        3557477
64  meter          E    =           
0002487
 Z    =       -2320786
34                 I    =           51
35623
 XDOT =      -1214
141005                 Wp   =           67
04779
 YDOT =      -5316
074839  meter/sec      RA   =          309
21983  deg
 ZDOT =      -5380
546323                 TA   =          138
90008
                                          MA   =          138
88134
                                          Ha   =            222
747  n
mi
                                          Hp   =            216
485

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17383800
68                 X    =        -5326696
57
 Y    =       11671514
58  feet           Y    =         3498068
07  meter
 Z    =       -7614128
40                 Z    =        -2346592
38
 XDOT =      -3983
402248                 XDOT =       -1128
469886
 YDOT =     -17441
190416  feet/sec       YDOT =       -5329
173037  meter/sec
 ZDOT =     -17652
711032                 ZDOT =       -5386
236094

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6907645
08                 X    =        -2105450
22
 Y    =       19720851
40  feet           Y    =         6010915
51  meter
 Z    =       -7730988
91                 Z    =        -2356405
42
 XDOT =     -12093
544098                 XDOT =       -3686
112241
 YDOT =     -11161
408552  feet/sec       YDOT =       -3401
997327  meter/sec
 ZDOT =     -17677
704838                 ZDOT =       -5388
164435


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
76361131  
00016717  00000-0  10270-3 0  9146
2 25544  51
6385 309
7527 0005247 340
2937  19
8012 15
53207790 34365


Satellite: ISS
Catalog Number: 25544
Epoch time:      19033
76361131   =   yrday
fracday
Element set:     914
Inclination:       51
6385  deg
RA of node:       309
7527  deg
Eccentricity:     
0005247     
Arg of perigee:   340
2937  deg
Mean anomaly:      19
8012  deg
Mean motion:   15
53207790  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3436
Checksum:              305


Coasting Arc #16 (Orbit 3451)
---------------------------------------

Vector Time (GMT): 2019/034/17:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5176291
21                 A    =         6786729
03  meter
 Y    =       -2654965
09  meter          E    =           
0011543
 Z    =        3481541
87                 I    =           51
32595
 XDOT =        144
482577                 Wp   =           66
90479
 YDOT =       6204
788244  meter/sec      RA   =          304
22520  deg
 ZDOT =       4509
362147                 TA   =          334
22490
                                          MA   =          334
28237
                                          Ha   =            222
630  n
mi
                                          Hp   =            216
435

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16982582
70                 X    =         5188684
14
 Y    =       -8710515
37  feet           Y    =        -2597010
95  meter
 Z    =       11422381
47                 Z    =         3506715
72
 XDOT =        474
024204                 XDOT =          53
184781
 YDOT =      20356
916811  feet/sec       YDOT =        6205
893405  meter/sec
 ZDOT =      14794
495234                 ZDOT =        4509
842321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8041934
16                 X    =         2451181
53
 Y    =      -17233507
93  feet           Y    =        -5252773
22  meter
 Z    =       11536268
52                 Z    =         3516254
64
 XDOT =      11497
069839                 XDOT =        3504
306887
 YDOT =      15285
847660  feet/sec       YDOT =        4659
126367  meter/sec
 ZDOT =      14795
892150                 ZDOT =        4509
787927


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
79306136  
00016717  00000-0  10270-3 0  9155
2 25544  51
6381 304
6273 0005114 342
7465  17
3513 15
53219983 34523


Satellite: ISS
Catalog Number: 25544
Epoch time:      19034
79306136   =   yrday
fracday
Element set:     915
Inclination:       51
6381  deg
RA of node:       304
6273  deg
Eccentricity:     
0005114     
Arg of perigee:   342
7465  deg
Mean anomaly:      17
3513  deg
Mean motion:   15
53219983  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3452
Checksum:              302


Coasting Arc #17 (Orbit 3466)
---------------------------------------

Vector Time (GMT): 2019/035/17:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914275
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4921310
53                 A    =         6783638
31  meter
 Y    =        1551399
01  meter          E    =           
0011301
 Z    =       -4415075
26                 I    =           51
29693
 XDOT =        804
320428                 Wp   =           43
12966
 YDOT =      -6860
442663  meter/sec      RA   =          299
22326  deg
 ZDOT =      -3304
150834                 TA   =          193
28595
                                          MA   =          193
31573
                                          Ha   =            222
963  n
mi
                                          Hp   =            216
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16146031
94                 X    =        -4916847
60
 Y    =        5089891
78  feet           Y    =         1496390
43  meter
 Z    =      -14485155
07                 Z    =        -4438969
62
 XDOT =       2638
846547                 XDOT =         897
025319
 YDOT =     -22508
013986  feet/sec       YDOT =       -6850
929854  meter/sec
 ZDOT =     -10840
389874                 ZDOT =       -3300
018685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9340115
70                 X    =        -2846867
26
 Y    =       14007994
26  feet           Y    =         4269636
65  meter
 Z    =      -14593128
47                 Z    =        -4447985
56
 XDOT =     -10940
298069                 XDOT =       -3334
602851
 YDOT =     -18577
980083  feet/sec       YDOT =       -5662
568329  meter/sec
 ZDOT =     -10820
918991                 ZDOT =       -3298
216108


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
75817208  
00016717  00000-0  10270-3 0  9160
2 25544  51
6373 299
8233 0005054 349
9371  10
1679 15
53211004 34679


Satellite: ISS
Catalog Number: 25544
Epoch time:      19035
75817208   =   yrday
fracday
Element set:     916
Inclination:       51
6373  deg
RA of node:       299
8233  deg
Eccentricity:     
0005054     
Arg of perigee:   349
9371  deg
Mean anomaly:      10
1679  deg
Mean motion:   15
53211004  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3467
Checksum:              313
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