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

 
Date: September 15th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13923 1181 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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


257/18:31:19 752 -1 3 2 0 2 0
N/A -0 3 -0 2 229 7
000/00:00:39 505 -1 4 -0 0 218 9

259/19:12:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 218 7

268/13:57:43 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 3

268/17:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 3

Coasting Arc #1 (Orbit 2894)
---------------------------------------

Vector Time (GMT): 2019/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3770083
74                 A    =         6788673
14  meter
 Y    =       -2254977
14  meter          E    =           
0019274
 Z    =       -5191136
55                 I    =           51
24755
 XDOT =       2570
140902                 Wp   =           76
19860
 YDOT =      -7099
560688  meter/sec      RA   =          282
41372  deg
 ZDOT =       1225
765111                 TA   =          205
61119
                                          MA   =          205
70678
                                          Ha   =            229
412  n
mi
                                          Hp   =            218
178

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12369041
16                 X    =        -3719372
28
 Y    =       -7398218
97  feet           Y    =        -2296853
81  meter
 Z    =      -17031287
88                 Z    =        -5209326
67
 XDOT =       8432
220808                 XDOT =        2643
385186
 YDOT =     -23292
521943  feet/sec       YDOT =       -7070
409913  meter/sec
 ZDOT =       4021
539079                 ZDOT =        1238
428343

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10993816
44                 X    =         3350915
25
 Y    =        9167591
57  feet           Y    =         2794281
91  meter
 Z    =      -17113820
58                 Z    =        -5216292
51
 XDOT =     -11162
792413                 XDOT =       -3402
419127
 YDOT =      20951
323262  feet/sec       YDOT =        6385
963330  meter/sec
 ZDOT =       4079
672442                 ZDOT =        1243
484160


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   19256
51399165  
00016717  00000-0  10270-3 0  9009
2 25544  51
6423 283
1789 0008430  35
3638 324
8070 15
50424556 28959


Satellite: ISS
Catalog Number: 25544
Epoch time:      19256
51399165   =   yrday
fracday
Element set:     900
Inclination:       51
6423  deg
RA of node:       283
1789  deg
Eccentricity:     
0008430     
Arg of perigee:    35
3638  deg
Mean anomaly:     324
8070  deg
Mean motion:   15
50424556  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2895
Checksum:              322


Coasting Arc #2 (Orbit 2910)
---------------------------------------

Vector Time (GMT): 2019/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3757618
36                 A    =         6789108
30  meter
 Y    =        2533497
93  meter          E    =           
0013789
 Z    =        5049069
60                 I    =           51
24154
 XDOT =      -2362
333939                 Wp   =           45
78448
 YDOT =       7074
136710  meter/sec      RA   =          277
42565  deg
 ZDOT =      -1779
042489                 TA   =           61
59545
                                          MA   =           61
45653
                                          Ha   =            229
376  n
mi
                                          Hp   =            218
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12328144
21                 X    =         3704483
30
 Y    =        8312001
07  feet           Y    =         2575221
68  meter
 Z    =       16565188
97                 Z    =         5067193
31
 XDOT =      -7750
439434                 XDOT =       -2432
621843
 YDOT =      23209
109940  feet/sec       YDOT =        7047
326239  meter/sec
 ZDOT =      -5836
753572                 ZDOT =       -1790
689212

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10989818
82                 X    =        -3349696
78
 Y    =       -9877541
55  feet           Y    =        -3010674
66  meter
 Z    =       16647403
48                 Z    =         5074128
58
 XDOT =      10036
160748                 XDOT =        3059
021796
 YDOT =     -21162
302004  feet/sec       YDOT =       -6450
269651  meter/sec
 ZDOT =      -5890
242487                 ZDOT =       -1795
345910


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   19257
54527116  
00016717  00000-0  10270-3 0  9013
2 25544  51
6405 278
0662 0008505  39
9102 320
2672 15
50464971 29113


Satellite: ISS
Catalog Number: 25544
Epoch time:      19257
54527116   =   yrday
fracday
Element set:     901
Inclination:       51
6405  deg
RA of node:       278
0662  deg
Eccentricity:     
0008505     
Arg of perigee:    39
9102  deg
Mean anomaly:     320
2672  deg
Mean motion:   15
50464971  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2911
Checksum:              300


Coasting Arc #3 (Orbit 2914)
---------------------------------------

Vector Time (GMT): 2019/257/18:31:39
505
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1197340
69                 A    =         6800968
55  meter
 Y    =        6666417
91  meter          E    =           
0012610
 Z    =        -602663
78                 I    =           51
27674
 XDOT =      -4641
381884                 Wp   =          103
94752
 YDOT =      -1360
489855  meter/sec      RA   =          276
09096  deg
 ZDOT =      -5935
934785                 TA   =           82
57543
                                          MA   =           82
43215
                                          Ha   =            229
743  n
mi
                                          Hp   =            218
918

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3928283
09                 X    =        -1268870
11
 Y    =       21871449
84  feet           Y    =         6652628
40  meter
 Z    =       -1977243
38                 Z    =         -608654
42
 XDOT =     -15227
630854                 XDOT =       -4596
990147
 YDOT =      -4463
549394  feet/sec       YDOT =       -1412
145469  meter/sec
 ZDOT =     -19474
851656                 ZDOT =       -5958
372846

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21902617
32                 X    =        -6675917
76
 Y    =       -3735857
27  feet           Y    =        -1138689
30  meter
 Z    =       -2004979
45                 Z    =         -611117
74
 XDOT =       4068
679423                 XDOT =        1240
133488
 YDOT =     -13534
878239  feet/sec       YDOT =       -4125
430887  meter/sec
 ZDOT =     -19576
771610                 ZDOT =       -5966
999987


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   19257
80309974  
00016717  00000-0  10270-3 0  9023
2 25544  51
6410 276
7887 0007271  45
8840 314
2908 15
50076828 29156


Satellite: ISS
Catalog Number: 25544
Epoch time:      19257
80309974   =   yrday
fracday
Element set:     902
Inclination:       51
6410  deg
RA of node:       276
7887  deg
Eccentricity:     
0007271     
Arg of perigee:    45
8840  deg
Mean anomaly:     314
2908  deg
Mean motion:   15
50076828  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2915
Checksum:              333


Coasting Arc #4 (Orbit 2930)
---------------------------------------

Vector Time (GMT): 2019/258/18:31:39
505
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         886664
39                 A    =         6800765
54  meter
 Y    =       -6665701
37  meter          E    =           
0020792
 Z    =         944068
90                 I    =           51
27361
 XDOT =       4691
184561                 Wp   =           52
97609
 YDOT =       1468
440511  meter/sec      RA   =          271
11270  deg
 ZDOT =       5884
489048                 TA   =          317
28954
                                          MA   =          317
45097
                                          Ha   =            229
787  n
mi
                                          Hp   =            218
826

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2909003
90                 X    =          956550
52
 Y    =      -21869098
98  feet           Y    =        -6655395
20  meter
 Z    =        3097338
90                 Z    =          948546
44
 XDOT =      15391
025463                 XDOT =        4645
831756
 YDOT =       4817
718211  feet/sec       YDOT =        1520
647691  meter/sec
 ZDOT =      19306
066429                 ZDOT =        5907
166780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21935163
58                 X    =         6685837
86
 Y    =        2332137
33  feet           Y    =          710835
46  meter
 Z    =        3118178
33                 Z    =          950420
76
 XDOT =      -4259
974725                 XDOT =       -1298
440296
 YDOT =      13778
402168  feet/sec       YDOT =        4199
656981  meter/sec
 ZDOT =      19409
070637                 ZDOT =        5915
884730


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   19258
83461897  
00016717  00000-0  10270-3 0  9031
2 25544  51
6410 271
6776 0007352  49
0023 311
1762 15
50074573 29313


Satellite: ISS
Catalog Number: 25544
Epoch time:      19258
83461897   =   yrday
fracday
Element set:     903
Inclination:       51
6410  deg
RA of node:       271
6776  deg
Eccentricity:     
0007352     
Arg of perigee:    49
0023  deg
Mean anomaly:     311
1762  deg
Mean motion:   15
50074573  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2931
Checksum:              308


Coasting Arc #5 (Orbit 2945)
---------------------------------------

Vector Time (GMT): 2019/259/18:31:39
505
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -627559
95                 A    =         6800368
24  meter
 Y    =        6637947
48  meter          E    =           
0011475
 Z    =       -1338851
37                 I    =           51
27379
 XDOT =      -4754
906600                 Wp   =          102
55708
 YDOT =      -1606
544383  meter/sec      RA   =          266
13448  deg
 ZDOT =      -5780
983035                 TA   =           92
05968
                                          MA   =           91
92827
                                          Ha   =            229
856  n
mi
                                          Hp   =            218
736

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2058923
72                 X    =         -695237
32
 Y    =       21778042
92  feet           Y    =         6630551
12  meter
 Z    =       -4392556
99                 Z    =        -1342064
90
 XDOT =     -15600
087270                 XDOT =       -4708
507399
 YDOT =      -5270
814904  feet/sec       YDOT =       -1659
458264  meter/sec
 ZDOT =     -18966
479774                 ZDOT =       -5803
967851

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21844424
73                 X    =        -6658180
66
 Y    =       -1100346
12  feet           Y    =         -335385
50  meter
 Z    =       -4407632
41                 Z    =        -1343446
36
 XDOT =       4528
290686                 XDOT =        1380
223001
 YDOT =     -14089
387832  feet/sec       YDOT =       -4294
445411  meter/sec
 ZDOT =     -19070
873824                 ZDOT =       -5812
802341


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   19259
80166580  
00016717  00000-0  10270-3 0  9041
2 25544  51
6419 266
8859 0007331  52
9933 307
1888 15
50075335 29467


Satellite: ISS
Catalog Number: 25544
Epoch time:      19259
80166580   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:       266
8859  deg
Eccentricity:     
0007331     
Arg of perigee:    52
9933  deg
Mean anomaly:     307
1888  deg
Mean motion:   15
50075335  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2946
Checksum:              342


Coasting Arc #6 (Orbit 2945)
---------------------------------------

Vector Time (GMT): 2019/259/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1152619
05                 A    =         6800771
94  meter
 Y    =       -6640866
39  meter          E    =           
0017340
 Z    =        -852521
73                 I    =           51
27562
 XDOT =       4635
340306                 Wp   =           44
89670
 YDOT =      -1551
237153  meter/sec      RA   =          265
97459  deg
 ZDOT =       5902
352240                 TA   =          305
84744
                                          MA   =          306
00838
                                          Ha   =            229
800  n
mi
                                          Hp   =            218
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3781558
56                 X    =        -1074132
19
 Y    =      -21787619
40  feet           Y    =        -6653317
03  meter
 Z    =       -2796987
30                 Z    =         -857929
44
 XDOT =      15207
809404                 XDOT =        4623
671668
 YDOT =      -5089
360739  feet/sec       YDOT =       -1499
466144  meter/sec
 ZDOT =      19364
672703                 ZDOT =        5924
840927

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20449203
59                 X    =         6232917
25
 Y    =       -8408037
15  feet           Y    =        -2562769
72  meter
 Z    =       -2821110
81                 Z    =         -859874
57
 XDOT =       7630
271960                 XDOT =        2325
706893
 YDOT =      12119
504216  feet/sec       YDOT =        3694
024885  meter/sec
 ZDOT =      19467
031751                 ZDOT =        5933
551278


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   19259
80166541  
00016717  00000-0  10270-3 0  9059
2 25544  51
6422 266
8862 0007345  52
4216 307
7600 15
50092891 29463


Satellite: ISS
Catalog Number: 25544
Epoch time:      19259
80166541   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:       266
8862  deg
Eccentricity:     
0007345     
Arg of perigee:    52
4216  deg
Mean anomaly:     307
7600  deg
Mean motion:   15
50092891  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2946
Checksum:              316


Coasting Arc #7 (Orbit 2961)
---------------------------------------

Vector Time (GMT): 2019/260/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1415424
85                 A    =         6801084
96  meter
 Y    =        6633010
57  meter          E    =           
0016549
 Z    =         449132
77                 I    =           51
27956
 XDOT =      -4611
462386                 Wp   =          105
22591
 YDOT =       1399
400961  meter/sec      RA   =          260
99762  deg
 ZDOT =      -5954
109078                 TA   =           69
91587
                                          MA   =           69
73784
                                          Ha   =            229
904  n
mi
                                          Hp   =            218
686

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4643782
31                 X    =         1338965
75
 Y    =       21761845
69  feet           Y    =         6648411
38  meter
 Z    =        1473532
73                 Z    =          455822
12
 XDOT =     -15129
469769                 XDOT =       -4597
846138
 YDOT =       4591
210501  feet/sec       YDOT =        1347
907919  meter/sec
 ZDOT =     -19534
478603                 ZDOT =       -5976
477092

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20072486
50                 X    =        -6118093
89
 Y    =        9599412
55  feet           Y    =         2925900
94  meter
 Z    =        1503497
69                 Z    =          458266
10
 XDOT =      -7273
371647                 XDOT =       -2216
923678
 YDOT =     -12042
507745  feet/sec       YDOT =       -3670
556361  meter/sec
 ZDOT =     -19636
277108                 ZDOT =       -5985
137263


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   19260
83318290  
00016717  00000-0  10270-3 0  9065
2 25544  51
6419 261
7758 0007278  57
3517 302
8335 15
50062366 29623


Satellite: ISS
Catalog Number: 25544
Epoch time:      19260
83318290   =   yrday
fracday
Element set:     906
Inclination:       51
6419  deg
RA of node:       261
7758  deg
Eccentricity:     
0007278     
Arg of perigee:    57
3517  deg
Mean anomaly:     302
8335  deg
Mean motion:   15
50062366  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2962
Checksum:              322


Coasting Arc #8 (Orbit 2976)
---------------------------------------

Vector Time (GMT): 2019/261/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1722905
65                 A    =         6801065
39  meter
 Y    =       -6570019
44  meter          E    =           
0018946
 Z    =        -105610
68                 I    =           51
28691
 XDOT =       4616
731550                 Wp   =           50
13363
 YDOT =      -1295
101756  meter/sec      RA   =          256
01985  deg
 ZDOT =       5979
666035                 TA   =          308
72469
                                          MA   =          308
89392
                                          Ha   =            229
821  n
mi
                                          Hp   =            218
625

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5652577
60                 X    =        -1648796
74
 Y    =      -21555181
88  feet           Y    =        -6588871
82  meter
 Z    =        -346491
72                 Z    =         -113799
50
 XDOT =      15146
757054                 XDOT =        4601
824400
 YDOT =      -4249
021510  feet/sec       YDOT =       -1243
557104  meter/sec
 ZDOT =      19618
326887                 ZDOT =        6002
056529

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19449378
37                 X    =         5928170
53
 Y    =      -10875308
02  feet           Y    =        -3314793
88  meter
 Z    =        -383291
81                 Z    =         -116827
34
 XDOT =       7084
409773                 XDOT =        2159
328099
 YDOT =      12050
798251  feet/sec       YDOT =        3673
083307  meter/sec
 ZDOT =      19720
221601                 ZDOT =        6010
723544


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   19261
80022781  
00016717  00000-0  10270-3 0  9071
2 25544  51
6426 256
9843 0007233  58
9047 301
2813 15
50098249 29777


Satellite: ISS
Catalog Number: 25544
Epoch time:      19261
80022781   =   yrday
fracday
Element set:     907
Inclination:       51
6426  deg
RA of node:       256
9843  deg
Eccentricity:     
0007233     
Arg of perigee:    58
9047  deg
Mean anomaly:     301
2813  deg
Mean motion:   15
50098249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2977
Checksum:              322


Coasting Arc #9 (Orbit 2992)
---------------------------------------

Vector Time (GMT): 2019/262/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1975418
91                 A    =         6801140
23  meter
 Y    =        6497752
33  meter          E    =           
0015234
 Z    =        -302661
38                 I    =           51
29655
 XDOT =      -4660
651088                 Wp   =          110
03512
 YDOT =       1150
620223  meter/sec      RA   =          251
04355  deg
 ZDOT =      -5967
754841                 TA   =           73
23536
                                          MA   =           73
06826
                                          Ha   =            229
945  n
mi
                                          Hp   =            218
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6481033
18                 X    =         1904082
53
 Y    =       21318085
08  feet           Y    =         6519443
97  meter
 Z    =        -992983
54                 Z    =         -293239
06
 XDOT =     -15290
850027                 XDOT =       -4644
182882
 YDOT =       3775
000733  feet/sec       YDOT =        1098
593274  meter/sec
 ZDOT =     -19579
248165                 ZDOT =       -5990
354871

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18806951
93                 X    =        -5732358
95
 Y    =       11951801
53  feet           Y    =         3642909
10  meter
 Z    =        -950556
81                 Z    =         -289729
72
 XDOT =      -6818
270632                 XDOT =       -2078
208889
 YDOT =     -12225
996271  feet/sec       YDOT =       -3726
483664  meter/sec
 ZDOT =     -19682
089715                 ZDOT =       -5999
100945


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   19262
83174193  
00016717  00000-0  10270-3 0  9081
2 25544  51
6432 251
8735 0007211  63
8268 296
3623 15
50060685 29938


Satellite: ISS
Catalog Number: 25544
Epoch time:      19262
83174193   =   yrday
fracday
Element set:     908
Inclination:       51
6432  deg
RA of node:       251
8735  deg
Eccentricity:     
0007211     
Arg of perigee:    63
8268  deg
Mean anomaly:     296
3623  deg
Mean motion:   15
50060685  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2993
Checksum:              323


Coasting Arc #10 (Orbit 3008)
---------------------------------------

Vector Time (GMT): 2019/263/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2261103
67                 A    =         6800877
89  meter
 Y    =       -6371810
61  meter          E    =           
0020262
 Z    =         646928
56                 I    =           51
30741
 XDOT =       4730
848266                 Wp   =           56
91304
 YDOT =      -1063
325166  meter/sec      RA   =          246
06696  deg
 ZDOT =       5937
343415                 TA   =          310
09645
                                          MA   =          310
27389
                                          Ha   =            229
890  n
mi
                                          Hp   =            218
493

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7418319
14                 X    =        -2192826
65
 Y    =      -20904890
45  feet           Y    =        -6396714
08  meter
 Z    =        2122469
01                 Z    =          636110
93
 XDOT =      15521
155729                 XDOT =        4713
546445
 YDOT =      -3488
599627  feet/sec       YDOT =       -1010
517990  meter/sec
 ZDOT =      19479
473145                 ZDOT =        5960
282363

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17934043
49                 X    =         5466296
45
 Y    =      -13062187
19  feet           Y    =        -3981354
65  meter
 Z    =        2073675
11                 Z    =          632056
17
 XDOT =       6761
026089                 XDOT =        2060
760752
 YDOT =      12458
143833  feet/sec       YDOT =        3797
242240  meter/sec
 ZDOT =      19583
856304                 ZDOT =        5969
159401


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   19263
86325220  
00016717  00000-0  10270-3 0  9095
2 25544  51
6426 246
7623 0007291  65
7909 294
4003 15
50108310 30099


Satellite: ISS
Catalog Number: 25544
Epoch time:      19263
86325220   =   yrday
fracday
Element set:     909
Inclination:       51
6426  deg
RA of node:       246
7623  deg
Eccentricity:     
0007291     
Arg of perigee:    65
7909  deg
Mean anomaly:     294
4003  deg
Mean motion:   15
50108310  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3009
Checksum:              298


Coasting Arc #11 (Orbit 3023)
---------------------------------------

Vector Time (GMT): 2019/264/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2484638
74                 A    =         6800718
40  meter
 Y    =        6240768
46  meter          E    =           
0013776
 Z    =       -1051410
85                 I    =           51
32034
 XDOT =      -4836
012535                 Wp   =          112
06108
 YDOT =        949
193715  meter/sec      RA   =          241
09238  deg
 ZDOT =      -5861
193618                 TA   =           79
36444
                                          MA   =           79
20931
                                          Ha   =            229
989  n
mi
                                          Hp   =            218
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8151701
89                 X    =         2419775
21
 Y    =       20474962
15  feet           Y    =         6268190
74  meter
 Z    =       -3449510
67                 Z    =        -1039499
03
 XDOT =     -15866
182858                 XDOT =       -4817
796625
 YDOT =       3114
152609  feet/sec       YDOT =         895
215706  meter/sec
 ZDOT =     -19229
637855                 ZDOT =       -5884
641119

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17073572
65                 X    =        -5204024
94
 Y    =       13947604
44  feet           Y    =         4251229
83  meter
 Z    =       -3395716
44                 Z    =        -1035014
37
 XDOT =      -6679
113834                 XDOT =       -2035
793897
 YDOT =     -12829
331494  feet/sec       YDOT =       -3910
380239  meter/sec
 ZDOT =     -19336
334963                 ZDOT =       -5893
714897


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   19264
83029507  
00016717  00000-0  10270-3 0  9104
2 25544  51
6419 241
9713 0007196  70
5854 289
6074 15
50061820 30240


Satellite: ISS
Catalog Number: 25544
Epoch time:      19264
83029507   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:       241
9713  deg
Eccentricity:     
0007196     
Arg of perigee:    70
5854  deg
Mean anomaly:     289
6074  deg
Mean motion:   15
50061820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3024
Checksum:              308


Coasting Arc #12 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2019/265/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2731679
07                 A    =         6800219
20  meter
 Y    =       -6060388
77  meter          E    =           
0020838
 Z    =        1388321
70                 I    =           51
33625
 XDOT =       4961
448790                 Wp   =           64
73676
 YDOT =       -899
817663  meter/sec      RA   =          236
11758  deg
 ZDOT =       5774
874751                 TA   =          310
44128
                                          MA   =          310
62283
                                          Ha   =            229
880  n
mi
                                          Hp   =            218
442

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8962201
69                 X    =        -2670450
75
 Y    =      -19883165
25  feet           Y    =        -6090593
95  meter
 Z    =        4554861
21                 Z    =         1375201
02
 XDOT =      16277
719127                 XDOT =        4943
090816
 YDOT =      -2952
157686  feet/sec       YDOT =        -844
437760  meter/sec
 ZDOT =      18946
439473                 ZDOT =        5798
931141

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16010661
01                 X    =         4880049
48
 Y    =      -14827573
54  feet           Y    =        -4519444
42  meter
 Z    =        4495539
69                 Z    =         1370240
50
 XDOT =       6833
220737                 XDOT =        2082
765681
 YDOT =      13215
820805  feet/sec       YDOT =        4028
182181  meter/sec
 ZDOT =      19055
913068                 ZDOT =        5808
242303


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   19265
86180302  
00016717  00000-0  10270-3 0  9110
2 25544  51
6418 236
8602 0007158  72
9071 287
2863 15
50120680 30402


Satellite: ISS
Catalog Number: 25544
Epoch time:      19265
86180302   =   yrday
fracday
Element set:     911
Inclination:       51
6418  deg
RA of node:       236
8602  deg
Eccentricity:     
0007158     
Arg of perigee:    72
9071  deg
Mean anomaly:     287
2863  deg
Mean motion:   15
50120680  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3040
Checksum:              296


Coasting Arc #13 (Orbit 3054)
---------------------------------------

Vector Time (GMT): 2019/266/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2909221
91                 A    =         6799801
50  meter
 Y    =        5881996
23  meter          E    =           
0012292
 Z    =       -1781754
85                 I    =           51
35387
 XDOT =      -5115
179150                 Wp   =          110
13678
 YDOT =        833
694436  meter/sec      RA   =          231
14372  deg
 ZDOT =      -5635
678094                 TA   =           89
46635
                                          MA   =           89
32550
                                          Ha   =            229
965  n
mi
                                          Hp   =            218
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9544691
30                 X    =         2851886
28
 Y    =       19297887
88  feet           Y    =         5914208
56  meter
 Z    =       -5845652
38                 Z    =        -1767762
36
 XDOT =     -16782
083827                 XDOT =       -5096
746588
 YDOT =       2735
217965  feet/sec       YDOT =         776
595801  meter/sec
 ZDOT =     -18489
757525                 ZDOT =       -5660
480979

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15004421
85                 X    =        -4573347
78
 Y    =       15463285
38  feet           Y    =         4713209
38  meter
 Z    =       -5782334
37                 Z    =        -1762455
52
 XDOT =      -6997
558290                 XDOT =       -2132
855767
 YDOT =     -13701
625959  feet/sec       YDOT =       -4176
255592  meter/sec
 ZDOT =     -18602
634213                 ZDOT =       -5670
082908


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   19266
82884166  
00016717  00000-0  10270-3 0  9127
2 25544  51
6416 232
0680 0007122  76
4255 283
7688 15
50081692 30559


Satellite: ISS
Catalog Number: 25544
Epoch time:      19266
82884166   =   yrday
fracday
Element set:     912
Inclination:       51
6416  deg
RA of node:       232
0680  deg
Eccentricity:     
0007122     
Arg of perigee:    76
4255  deg
Mean anomaly:     283
7688  deg
Mean motion:   15
50081692  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3055
Checksum:              320


Coasting Arc #14 (Orbit 3070)
---------------------------------------

Vector Time (GMT): 2019/267/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3102275
05                 A    =         6799159
32  meter
 Y    =       -5660999
14  meter          E    =           
0020981
 Z    =        2105331
34                 I    =           51
37258
 XDOT =       5282
143532                 Wp   =           73
27662
 YDOT =       -836
738706  meter/sec      RA   =          226
17066  deg
 ZDOT =       5493
889206                 TA   =          310
10781
                                          MA   =          310
29152
                                          Ha   =            229
919  n
mi
                                          Hp   =            218
380

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10178067
75                 X    =        -3048968
06
 Y    =      -18572831
82  feet           Y    =        -5695392
82  meter
 Z    =        6907255
05                 Z    =         2090391
41
 XDOT =      17329
867230                 XDOT =        5264
421415
 YDOT =      -2745
205727  feet/sec       YDOT =        -777
768901  meter/sec
 ZDOT =      18024
570886                 ZDOT =        5519
504802

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13833076
09                 X    =         4216321
59
 Y    =      -16066091
46  feet           Y    =        -4896944
68  meter
 Z    =        6839592
69                 Z    =         2084707
85
 XDOT =       7408
662669                 XDOT =        2258
160381
 YDOT =      14157
813555  feet/sec       YDOT =        4315
301572  meter/sec
 ZDOT =      18141
156717                 ZDOT =        5529
424567


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   19267
86034611  
00016717  00000-0  10270-3 0  9135
2 25544  51
6402 226
9564 0007167  79
9532 280
2427 15
50126730 30716


Satellite: ISS
Catalog Number: 25544
Epoch time:      19267
86034611   =   yrday
fracday
Element set:     913
Inclination:       51
6402  deg
RA of node:       226
9564  deg
Eccentricity:     
0007167     
Arg of perigee:    79
9532  deg
Mean anomaly:     280
2427  deg
Mean motion:   15
50126730  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3071
Checksum:              305


Coasting Arc #15 (Orbit 3082)
---------------------------------------

Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         845780
76                 A    =         6790595
15  meter
 Y    =       -4569620
67  meter          E    =           
0012848
 Z    =        4941264
19                 I    =           51
36275
 XDOT =       6454
183582                 Wp   =          101
88567
 YDOT =       3536
819822  meter/sec      RA   =          222
28206  deg
 ZDOT =       2158
696567                 TA   =          326
95411
                                          MA   =          327
03433
                                          Ha   =            229
889  n
mi
                                          Hp   =            218
309

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2774871
26                 X    =          872814
90
 Y    =      -14992193
80  feet           Y    =        -4560011
09  meter
 Z    =       16211496
68                 Z    =         4945438
60
 XDOT =      21175
142986                 XDOT =        6403
668444
 YDOT =      11603
739575  feet/sec       YDOT =        3608
712741  meter/sec
 ZDOT =       7082
337818                 ZDOT =        2189
925535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5840448
90                 X    =         1780168
83
 Y    =       14061684
51  feet           Y    =         4286001
44  meter
 Z    =       16230729
98                 Z    =         4947126
50
 XDOT =     -23023
958944                 XDOT =       -7017
702686
 YDOT =       1196
413135  feet/sec       YDOT =         364
666724  meter/sec
 ZDOT =       7224
243827                 ZDOT =        2201
949519


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   19268
63397622  
00016717  00000-0  10270-3 0  9146
2 25544  51
6403 223
1239 0007227  83
4453 276
7520 15
50138102 30837


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
63397622   =   yrday
fracday
Element set:     914
Inclination:       51
6403  deg
RA of node:       223
1239  deg
Eccentricity:     
0007227     
Arg of perigee:    83
4453  deg
Mean anomaly:     276
7520  deg
Mean motion:   15
50138102  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3083
Checksum:              297


Coasting Arc #16 (Orbit 3084)
---------------------------------------

Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1033001
85                 A    =         6790379
34  meter
 Y    =       -4446846
61  meter          E    =           
0012367
 Z    =        5016895
34                 I    =           51
36647
 XDOT =       6450
292468                 Wp   =          101
50550
 YDOT =       3676
599974  meter/sec      RA   =          221
63771  deg
 ZDOT =       1924
239840                 TA   =          329
72507
                                          MA   =          329
79646
                                          Ha   =            229
987  n
mi
                                          Hp   =            218
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3389113
69                 X    =         1058281
81
 Y    =      -14589391
76  feet           Y    =        -4435153
18  meter
 Z    =       16459630
37                 Z    =         5021974
94
 XDOT =      21162
376865                 XDOT =        6399
353414
 YDOT =      12062
335872  feet/sec       YDOT =        3748
447001  meter/sec
 ZDOT =       6313
122836                 ZDOT =        1955
448854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13729826
51                 X    =         4184851
12
 Y    =        5921088
07  feet           Y    =         1804747
64  meter
 Z    =       16482974
72                 Z    =         5024010
69
 XDOT =     -15330
813910                 XDOT =       -4672
832080
 YDOT =      17521
125748  feet/sec       YDOT =        5340
439128  meter/sec
 ZDOT =       6454
933928                 ZDOT =        1967
463861


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   19268
76291502  
00016717  00000-0  10270-3 0  9151
2 25544  51
6419 222
4856 0007348  83
5848 276
6140 15
50100596 30859


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
76291502   =   yrday
fracday
Element set:     915
Inclination:       51
6419  deg
RA of node:       222
4856  deg
Eccentricity:     
0007348     
Arg of perigee:    83
5848  deg
Mean anomaly:     276
6140  deg
Mean motion:   15
50100596  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3085
Checksum:              324


Coasting Arc #17 (Orbit 3099)
---------------------------------------

Vector Time (GMT): 2019/269/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965158
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1081122
61                 A    =         6789826
13  meter
 Y    =        4317847
34  meter          E    =           
0020724
 Z    =       -5145811
07                 I    =           51
39097
 XDOT =      -6653
087020                 Wp   =           81
33796
 YDOT =      -3455
327169  meter/sec      RA   =          216
66237  deg
 ZDOT =      -1503
724500                 TA   =          174
09769
                                          MA   =          174
07323
                                          Ha   =            229
923  n
mi
                                          Hp   =            218
269

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3546990
20                 X    =        -1104330
26
 Y    =       14166165
81  feet           Y    =         4305627
23  meter
 Z    =      -16882582
25                 Z    =        -5151119
50
 XDOT =     -21827
713319                 XDOT =       -6606
649844
 YDOT =     -11336
375226  feet/sec       YDOT =       -3529
467172  meter/sec
 ZDOT =      -4933
479331                 ZDOT =       -1535
929498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13386361
27                 X    =        -4080162
92
 Y    =       -5765695
84  feet           Y    =        -1757384
09  meter
 Z    =      -16906953
01                 Z    =        -5153239
28
 XDOT =      14418
913759                 XDOT =        4394
884914
 YDOT =     -18601
651990  feet/sec       YDOT =       -5669
783526  meter/sec
 ZDOT =      -5079
857135                 ZDOT =       -1548
340455


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   19269
72994825  
00016717  00000-0  10270-3 0  9167
2 25544  51
6423 217
6936 0007175  86
1098 274
0873 15
50128994 31008


Satellite: ISS
Catalog Number: 25544
Epoch time:      19269
72994825   =   yrday
fracday
Element set:     916
Inclination:       51
6423  deg
RA of node:       217
6936  deg
Eccentricity:     
0007175     
Arg of perigee:    86
1098  deg
Mean anomaly:     274
0873  deg
Mean motion:   15
50128994  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3100
Checksum:              339


Coasting Arc #18 (Orbit 3115)
---------------------------------------

Vector Time (GMT): 2019/270/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965158
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1131599
89                 A    =         6789497
83  meter
 Y    =       -4189068
80  meter          E    =           
0010693
 Z    =        5213183
00                 I    =           51
41786
 XDOT =       6874
657526                 Wp   =          101
76905
 YDOT =       3220
585013  meter/sec      RA   =          211
68894  deg
 ZDOT =       1091
620915                 TA   =          337
71727
                                          MA   =          337
76369
                                          Ha   =            229
940  n
mi
                                          Hp   =            218
338

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3712598
08                 X    =         1153036
41
 Y    =      -13743664
03  feet           Y    =        -4176294
00  meter
 Z    =       17103618
78                 Z    =         5218732
43
 XDOT =      22554
650675                 XDOT =        6832
830581
 YDOT =      10566
223796  feet/sec       YDOT =        3297
228538  meter/sec
 ZDOT =       3581
433449                 ZDOT =        1124
913490

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13041096
56                 X    =         3974926
23
 Y    =        5632948
39  feet           Y    =         1716922
67  meter
 Z    =       17129073
35                 Z    =         5220941
56
 XDOT =     -13439
495063                 XDOT =       -4096
358095
 YDOT =      19723
183184  feet/sec       YDOT =        6011
626235  meter/sec
 ZDOT =       3732
792419                 ZDOT =        1137
755129


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   19270
76144891  
00016717  00000-0  10270-3 0  9174
2 25544  51
6429 212
5823 0007238  89
8331 270
3649 15
50109312 31163


Satellite: ISS
Catalog Number: 25544
Epoch time:      19270
76144891   =   yrday
fracday
Element set:     917
Inclination:       51
6429  deg
RA of node:       212
5823  deg
Eccentricity:     
0007238     
Arg of perigee:    89
8331  deg
Mean anomaly:     270
3649  deg
Mean motion:   15
50109312  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3116
Checksum:              311
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