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

 
Date: September 9th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14325 6884 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


253/21:33:29 000 0 0 0 0 0 0
N/A 0 0 0 0 229 2
000/00:00:00 000 0 0 0 0 218 7

254/16:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 218 5

257/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 5
000/00:00:00 000 0 0 0 0 218 1

260/17:57:24 933 -1 0 2 4 2 4
N/A -2 1 -0 2 229 7
000/00:00:49 866 -0 5 -0 0 219 0

264/20:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 219 0

Coasting Arc #1 (Orbit 2832)
---------------------------------------

Vector Time (GMT): 2019/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4140654
64                 A    =         6788497
33  meter
 Y    =       -1302366
60  meter          E    =           
0019605
 Z    =       -5235727
51                 I    =           51
29923
 XDOT =       3378
317125                 Wp   =           60
94457
 YDOT =      -6792
333745  meter/sec      RA   =          302
35845  deg
 ZDOT =       -975
613272                 TA   =          199
61083
                                          MA   =          199
68634
                                          Ha   =            229
060  n
mi
                                          Hp   =            218
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13584824
94                 X    =        -4100351
48
 Y    =       -4272856
30  feet           Y    =        -1348445
12  meter
 Z    =      -17177583
69                 Z    =        -5255743
11
 XDOT =      11083
717601                 XDOT =        3458
758816
 YDOT =     -22284
559530  feet/sec       YDOT =       -6754
105272  meter/sec
 ZDOT =      -3200
830946                 ZDOT =        -959
007287

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12206832
48                 X    =         3720642
54
 Y    =        7118070
66  feet           Y    =         2169587
94  meter
 Z    =      -17268481
75                 Z    =        -5263433
24
 XDOT =     -15194
004936                 XDOT =       -4631
132704
 YDOT =      18423
888112  feet/sec       YDOT =        5615
601096  meter/sec
 ZDOT =      -3124
712128                 ZDOT =        -952
412257


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   19252
51777156  
00016717  00000-0  10270-3 0  9005
2 25544  51
6428 302
9886 0008146  21
1715 338
9772 15
50415467 28333


Satellite: ISS
Catalog Number: 25544
Epoch time:      19252
51777156   =   yrday
fracday
Element set:     900
Inclination:       51
6428  deg
RA of node:       302
9886  deg
Eccentricity:     
0008146     
Arg of perigee:    21
1715  deg
Mean anomaly:     338
9772  deg
Mean motion:   15
50415467  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2833
Checksum:              322


Coasting Arc #2 (Orbit 2848)
---------------------------------------

Vector Time (GMT): 2019/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3976593
79                 A    =         6788133
18  meter
 Y    =        1526041
41  meter          E    =           
0008901
 Z    =        5279950
52                 I    =           51
28057
 XDOT =      -3217
124228                 Wp   =           41
74606
 YDOT =       6947
516627  meter/sec      RA   =          297
37416  deg
 ZDOT =        421
081400                 TA   =           44
25342
                                          MA   =           44
18227
                                          Ha   =            228
993  n
mi
                                          Hp   =            218
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13046567
56                 X    =         3933586
86
 Y    =        5006697
53  feet           Y    =         1570270
24  meter
 Z    =       17322672
30                 Z    =         5299162
56
 XDOT =     -10554
869514                 XDOT =       -3296
619618
 YDOT =      22793
689721  feet/sec       YDOT =        6911
096008  meter/sec
 ZDOT =       1381
500657                 ZDOT =         405
260634

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11651090
88                 X    =        -3551252
50
 Y    =       -7516807
89  feet           Y    =        -2291123
05  meter
 Z    =       17409899
52                 Z    =         5306537
37
 XDOT =      14403
284380                 XDOT =        4390
121079
 YDOT =     -19339
688543  feet/sec       YDOT =       -5894
737068  meter/sec
 ZDOT =       1308
957967                 ZDOT =         398
970388


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   19253
54905715  
00016717  00000-0  10270-3 0  9014
2 25544  51
6419 297
8768 0008170  25
0978 335
0568 15
50447337 28494


Satellite: ISS
Catalog Number: 25544
Epoch time:      19253
54905715   =   yrday
fracday
Element set:     901
Inclination:       51
6419  deg
RA of node:       297
8768  deg
Eccentricity:     
0008170     
Arg of perigee:    25
0978  deg
Mean anomaly:     335
0568  deg
Mean motion:   15
50447337  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2849
Checksum:              342


Coasting Arc #3 (Orbit 2854)
---------------------------------------

Vector Time (GMT): 2019/253/21:33:29
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -639676
99                 A    =         6797255
89  meter
 Y    =        6238157
67  meter          E    =           
0017463
 Z    =        2614918
47                 I    =           51
30572
 XDOT =      -5384
639833                 Wp   =           75
11347
 YDOT =       1640
401194  meter/sec      RA   =          295
36698  deg
 ZDOT =      -5196
954112                 TA   =           75
34095
                                          MA   =           75
14742
                                          Ha   =            229
245  n
mi
                                          Hp   =            218
676

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2098677
79                 X    =         -722087
99
 Y    =       20466396
57  feet           Y    =         6230543
70  meter
 Z    =        8579128
85                 Z    =         2611610
73
 XDOT =     -17666
141183                 XDOT =       -5377
339474
 YDOT =       5381
893681  feet/sec       YDOT =        1580
226916  meter/sec
 ZDOT =     -17050
374383                 ZDOT =       -5223
092696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16630247
93                 X    =        -5068899
57
 Y    =       12123518
35  feet           Y    =         3695248
39  meter
 Z    =        8563553
33                 Z    =         2610171
05
 XDOT =     -14876
073631                 XDOT =       -4534
227243
 YDOT =      -8200
245576  feet/sec       YDOT =       -2499
434852  meter/sec
 ZDOT =     -17169
369959                 ZDOT =       -5233
223964


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   19253
93579122  
00016717  00000-0  10270-3 0  9027
2 25544  51
6430 295
9616 0008338  26
1724 333
9846 15
50421513 28556


Satellite: ISS
Catalog Number: 25544
Epoch time:      19253
93579122   =   yrday
fracday
Element set:     902
Inclination:       51
6430  deg
RA of node:       295
9616  deg
Eccentricity:     
0008338     
Arg of perigee:    26
1724  deg
Mean anomaly:     333
9846  deg
Mean motion:   15
50421513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2855
Checksum:              317


Coasting Arc #4 (Orbit 2866)
---------------------------------------

Vector Time (GMT): 2019/254/16:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2436534
71                 A    =         6790580
51  meter
 Y    =       -4214744
77  meter          E    =           
0015007
 Z    =       -4744981
64                 I    =           51
26996
 XDOT =       4490
532877                 Wp   =           75
04128
 YDOT =      -5591
473981  meter/sec      RA   =          291
38341  deg
 ZDOT =       2671
680110                 TA   =          221
48589
                                          MA   =          221
59990
                                          Ha   =            229
282  n
mi
                                          Hp   =            218
483

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7993880
29                 X    =        -2366174
92
 Y    =      -13827902
77  feet           Y    =        -4241598
71  meter
 Z    =      -15567525
06                 Z    =        -4756646
11
 XDOT =      14732
719414                 XDOT =        4539
747229
 YDOT =     -18344
730910  feet/sec       YDOT =       -5540
982331  meter/sec
 ZDOT =       8765
354693                 ZDOT =        2693
613060

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15920183
32                 X    =         4852471
88
 Y    =        -132579
48  feet           Y    =          -40410
22  meter
 Z    =      -15620212
53                 Z    =        -4761040
78
 XDOT =       8835
059355                 XDOT =        2692
926091
 YDOT =      20601
122597  feet/sec       YDOT =        6279
222167  meter/sec
 ZDOT =       8865
551413                 ZDOT =        2702
220071


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   19254
70925353  
00016717  00000-0  10270-3 0  9035
2 25544  51
6403 292
1260 0008424  28
6368 331
5244 15
50420587 28676


Satellite: ISS
Catalog Number: 25544
Epoch time:      19254
70925353   =   yrday
fracday
Element set:     903
Inclination:       51
6403  deg
RA of node:       292
1260  deg
Eccentricity:     
0008424     
Arg of perigee:    28
6368  deg
Mean anomaly:     331
5244  deg
Mean motion:   15
50420587  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2867
Checksum:              305


Coasting Arc #5 (Orbit 2882)
---------------------------------------

Vector Time (GMT): 2019/255/16:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2430877
18                 A    =         6791493
90  meter
 Y    =        4479670
77  meter          E    =           
0016576
 Z    =        4483297
47                 I    =           51
26225
 XDOT =      -4275
838156                 Wp   =           50
27816
 YDOT =       5513
880310  meter/sec      RA   =          286
39809  deg
 ZDOT =      -3172
756638                 TA   =           71
86245
                                          MA   =           71
68200
                                          Ha   =            229
315  n
mi
                                          Hp   =            218
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7975318
84                 X    =         2358826
40
 Y    =       14697082
58  feet           Y    =         4506452
05  meter
 Z    =       14708981
21                 Z    =         4494930
28
 XDOT =     -14028
340406                 XDOT =       -4321
766840
 YDOT =      18090
158499  feet/sec       YDOT =        5465
807813  meter/sec
 ZDOT =     -10409
306555                 ZDOT =       -3193
638839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16675176
00                 X    =        -5082593
64
 Y    =         -16090
80  feet           Y    =           -4904
48  meter
 Z    =       14761514
89                 Z    =         4499309
74
 XDOT =      -9333
097930                 XDOT =       -2844
728249
 YDOT =     -19639
919920  feet/sec       YDOT =       -5986
247592  meter/sec
 ZDOT =     -10504
701087                 ZDOT =       -3201
832891


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   19255
74053616  
00016717  00000-0  10270-3 0  9045
2 25544  51
6404 287
0133 0008500  31
7543 328
4118 15
50449424 28838


Satellite: ISS
Catalog Number: 25544
Epoch time:      19255
74053616   =   yrday
fracday
Element set:     904
Inclination:       51
6404  deg
RA of node:       287
0133  deg
Eccentricity:     
0008500     
Arg of perigee:    31
7543  deg
Mean anomaly:     328
4118  deg
Mean motion:   15
50449424  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2883
Checksum:              297


Coasting Arc #6 (Orbit 2897)
---------------------------------------

Vector Time (GMT): 2019/256/16:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2510810
08                 A    =         6792528
31  meter
 Y    =       -4695667
81  meter          E    =           
0013202
 Z    =       -4225315
20                 I    =           51
25646
 XDOT =       4046
799344                 Wp   =           71
31338
 YDOT =      -5401
478484  meter/sec      RA   =          281
41371  deg
 ZDOT =       3611
492555                 TA   =          235
84579
                                          MA   =          235
97106
                                          Ha   =            229
433  n
mi
                                          Hp   =            218
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8237565
87                 X    =        -2437591
07
 Y    =      -15405734
27  feet           Y    =        -4723336
46  meter
 Z    =      -13862582
69                 Z    =        -4237333
41
 XDOT =      13276
900734                 XDOT =        4089
356974
 YDOT =     -17721
386104  feet/sec       YDOT =       -5355
986024  meter/sec
 ZDOT =      11848
728855                 ZDOT =        3631
254119

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17425619
58                 X    =         5311328
85
 Y    =        -184444
92  feet           Y    =          -56218
81  meter
 Z    =      -13916863
90                 Z    =        -4241860
12
 XDOT =       9696
490546                 XDOT =        2955
490318
 YDOT =      18576
048846  feet/sec       YDOT =        5661
979688  meter/sec
 ZDOT =      11939
001598                 ZDOT =        3639
007687


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
70736374  
00016717  00000-0  10270-3 0  9052
2 25544  51
6397 282
2208 0008534  35
2698 324
9016 15
50425372 28986


Satellite: ISS
Catalog Number: 25544
Epoch time:      19256
70736374   =   yrday
fracday
Element set:     905
Inclination:       51
6397  deg
RA of node:       282
2208  deg
Eccentricity:     
0008534     
Arg of perigee:    35
2698  deg
Mean anomaly:     324
9016  deg
Mean motion:   15
50425372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2898
Checksum:              332


Coasting Arc #7 (Orbit 2909)
---------------------------------------

Vector Time (GMT): 2019/257/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951803
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3963097
04                 A    =         6792131
70  meter
 Y    =        3452017
55  meter          E    =           
0016396
 Z    =       -4319941
29                 I    =           51
25293
 XDOT =      -1923
245471                 Wp   =           54
87250
 YDOT =      -6542
097598  meter/sec      RA   =          277
67221  deg
 ZDOT =      -3463
467347                 TA   =          179
63233
                                          MA   =          179
63113
                                          Ha   =            229
470  n
mi
                                          Hp   =            218
057

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13002286
88                 X    =        -3980420
17
 Y    =       11325516
88  feet           Y    =         3407602
10  meter
 Z    =      -14173035
74                 Z    =        -4339234
87
 XDOT =      -6309
860468                 XDOT =       -1833
123375
 YDOT =     -21463
574795  feet/sec       YDOT =       -6563
101134  meter/sec
 ZDOT =     -11363
081846                 ZDOT =       -3472
590154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16282219
89                 X    =         4962820
62
 Y    =       -5451085
37  feet           Y    =        -1661490
82  meter
 Z    =      -14261021
09                 Z    =        -4346759
23
 XDOT =      -2951
748715                 XDOT =        -899
693008
 YDOT =      21017
232212  feet/sec       YDOT =        6406
052378  meter/sec
 ZDOT =     -11404
067769                 ZDOT =       -3475
959856


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
48082527  
00016717  00000-0  10270-3 0  9063
2 25544  51
6418 278
3858 0008347  39
9196 320
2567 15
50438338 29104


Satellite: ISS
Catalog Number: 25544
Epoch time:      19257
48082527   =   yrday
fracday
Element set:     906
Inclination:       51
6418  deg
RA of node:       278
3858  deg
Eccentricity:     
0008347     
Arg of perigee:    39
9196  deg
Mean anomaly:     320
2567  deg
Mean motion:   15
50438338  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2910
Checksum:              341


Coasting Arc #8 (Orbit 2925)
---------------------------------------

Vector Time (GMT): 2019/258/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951803
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3824776
55                 A    =         6791091
80  meter
 Y    =       -3237065
25  meter          E    =           
0013863
 Z    =        4570615
52                 I    =           51
24568
 XDOT =       2101
110669                 Wp   =           78
72223
 YDOT =       6736
934474  meter/sec      RA   =          272
68607  deg
 ZDOT =       3007
963406                 TA   =          341
06627
                                          MA   =          341
11776
                                          Ha   =            229
431  n
mi
                                          Hp   =            218
005

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12548479
51                 X    =         3838488
58
 Y    =      -10620292
82  feet           Y    =        -3194216
75  meter
 Z    =       14995457
75                 Z    =         4589228
50
 XDOT =       6893
407707                 XDOT =        2011
009144
 YDOT =      22102
803391  feet/sec       YDOT =        6759
927107  meter/sec
 ZDOT =       9868
646345                 ZDOT =        3017
950253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15497896
82                 X    =        -4723758
95
 Y    =        5245737
89  feet           Y    =         1598900
91  meter
 Z    =       15080322
90                 Z    =         4596482
42
 XDOT =       2240
216744                 XDOT =         682
818064
 YDOT =     -21928
787478  feet/sec       YDOT =       -6683
894423  meter/sec
 ZDOT =       9913
562921                 ZDOT =        3021
653978


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
51210542  
00016717  00000-0  10270-3 0  9079
2 25544  51
6411 273
2730 0008510  43
7233 316
4590 15
50451640 29268


Satellite: ISS
Catalog Number: 25544
Epoch time:      19258
51210542   =   yrday
fracday
Element set:     907
Inclination:       51
6411  deg
RA of node:       273
2730  deg
Eccentricity:     
0008510     
Arg of perigee:    43
7233  deg
Mean anomaly:     316
4590  deg
Mean motion:   15
50451640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2926
Checksum:              281


Coasting Arc #9 (Orbit 2940)
---------------------------------------

Vector Time (GMT): 2019/259/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951803
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3747400
18                 A    =         6790220
20  meter
 Y    =        3010100
63  meter          E    =           
0019526
 Z    =       -4814893
42                 I    =           51
24382
 XDOT =      -2286
791296                 Wp   =           61
30186
 YDOT =      -6853
932110  meter/sec      RA   =          267
69934  deg
 ZDOT =      -2503
615474                 TA   =          183
86547
                                          MA   =          183
88058
                                          Ha   =            229
606  n
mi
                                          Hp   =            217
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12294620
02                 X    =        -3757393
30
 Y    =        9875658
24  feet           Y    =         2968138
18  meter
 Z    =      -15796894
43                 Z    =        -4833121
55
 XDOT =      -7502
596115                 XDOT =       -2197
817460
 YDOT =     -22486
653905  feet/sec       YDOT =       -6879
007402  meter/sec
 ZDOT =      -8213
961530                 ZDOT =       -2514
507073

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14898739
71                 X    =         4541135
86
 Y    =       -4907319
38  feet           Y    =        -1495750
95  meter
 Z    =      -15879985
90                 Z    =        -4840219
70
 XDOT =      -1374
833237                 XDOT =        -419
049171
 YDOT =      22579
920585  feet/sec       YDOT =        6882
359794  meter/sec
 ZDOT =      -8262
998972                 ZDOT =       -2518
562087


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
47892948  
00016717  00000-0  10270-3 0  9082
2 25544  51
6427 268
4803 0008468  46
6049 313
5806 15
50442491 29410


Satellite: ISS
Catalog Number: 25544
Epoch time:      19259
47892948   =   yrday
fracday
Element set:     908
Inclination:       51
6427  deg
RA of node:       268
4803  deg
Eccentricity:     
0008468     
Arg of perigee:    46
6049  deg
Mean anomaly:     313
5806  deg
Mean motion:   15
50442491  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2941
Checksum:              346


Coasting Arc #10 (Orbit 2956)
---------------------------------------

Vector Time (GMT): 2019/260/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951803
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3682689
27                 A    =         6789404
78  meter
 Y    =       -2752350
53  meter          E    =           
0011807
 Z    =        4985062
93                 I    =           51
24185
 XDOT =       2506
219357                 Wp   =           79
22900
 YDOT =       6970
281830  meter/sec      RA   =          262
71172  deg
 ZDOT =       1995
105956                 TA   =          351
27803
                                          MA   =          351
29853
                                          Ha   =            229
568  n
mi
                                          Hp   =            217
780

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12082313
87                 X    =         3688978
28
 Y    =       -9030021
44  feet           Y    =        -2711132
46  meter
 Z    =       16355193
35                 Z    =         5002967
74
 XDOT =       8222
504452                 XDOT =        2418
398187
 YDOT =      22868
378707  feet/sec       YDOT =        6997
817296  meter/sec
 ZDOT =       6545
623215                 ZDOT =        2007
066349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14322392
69                 X    =        -4365465
29
 Y    =        4440370
80  feet           Y    =         1353425
02  meter
 Z    =       16436791
65                 Z    =         5009934
09
 XDOT =        374
881056                 XDOT =         114
263746
 YDOT =     -23242
651730  feet/sec       YDOT =       -7084
360247  meter/sec
 ZDOT =       6599
526908                 ZDOT =        2011
535801


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
51020793  
00016717  00000-0  10270-3 0  9091
2 25544  51
6408 263
3675 0008635  50
6982 309
4933 15
50452074 29577


Satellite: ISS
Catalog Number: 25544
Epoch time:      19260
51020793   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:       263
3675  deg
Eccentricity:     
0008635     
Arg of perigee:    50
6982  deg
Mean anomaly:     309
4933  deg
Mean motion:   15
50452074  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2957
Checksum:              322


Coasting Arc #11 (Orbit 2960)
---------------------------------------

Vector Time (GMT): 2019/260/17:57:49
866
Vector Time (MET): N/A
Weight (LBS)     : 951554
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3649670
80                 A    =         6790597
38  meter
 Y    =        2785739
16  meter          E    =           
0019108
 Z    =       -5020666
14                 I    =           51
24405
 XDOT =      -2627
470705                 Wp   =           64
81264
 YDOT =      -6918
211153  meter/sec      RA   =          261
26569  deg
 ZDOT =      -1926
427751                 TA   =          186
32785
                                          MA   =          186
35202
                                          Ha   =            229
681  n
mi
                                          Hp   =            219
015

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11973985
58                 X    =        -3656162
67
 Y    =        9139564
17  feet           Y    =         2744889
20  meter
 Z    =      -16472001
76                 Z    =        -5038411
05
 XDOT =      -8620
310713                 XDOT =       -2540
556388
 YDOT =     -22697
543152  feet/sec       YDOT =       -6947
107594  meter/sec
 ZDOT =      -6320
301020                 ZDOT =       -1938
979387

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8057889
21                 X    =        -2456044
63
 Y    =      -12621710
68  feet           Y    =        -3847097
42  meter
 Z    =      -16552874
27                 Z    =        -5045316
08
 XDOT =      22444
981168                 XDOT =        6841
230260
 YDOT =      -5956
797072  feet/sec       YDOT =       -1815
631748  meter/sec
 ZDOT =      -6376
900718                 ZDOT =       -1943
679339


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
76803073  
00016717  00000-0  10270-3 0  9100
2 25544  51
6420 262
0900 0006899  44
3962 315
7740 15
50022642 29611


Satellite: ISS
Catalog Number: 25544
Epoch time:      19260
76803073   =   yrday
fracday
Element set:     910
Inclination:       51
6420  deg
RA of node:       262
0900  deg
Eccentricity:     
0006899     
Arg of perigee:    44
3962  deg
Mean anomaly:     315
7740  deg
Mean motion:   15
50022642  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2961
Checksum:              295


Coasting Arc #12 (Orbit 2976)
---------------------------------------

Vector Time (GMT): 2019/261/17:57:49
866
Vector Time (MET): N/A
Weight (LBS)     : 951554
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3564379
88                 A    =         6790113
24  meter
 Y    =       -2687486
72  meter          E    =           
0009088
 Z    =        5108298
79                 I    =           51
24894
 XDOT =       2969
217259                 Wp   =           79
14603
 YDOT =       6897
225973  meter/sec      RA   =          256
28281  deg
 ZDOT =       1556
153972                 TA   =          355
76829
                                          MA   =          355
77597
                                          Ha   =            229
499  n
mi
                                          Hp   =            219
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11694159
72                 X    =         3569353
67
 Y    =       -8817213
65  feet           Y    =        -2647599
11  meter
 Z    =       16759510
47                 Z    =         5125625
69
 XDOT =       9741
526440                 XDOT =        2884
310787
 YDOT =      22628
694138  feet/sec       YDOT =        6929
955232  meter/sec
 ZDOT =       5105
492034                 ZDOT =        1570
370720

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7972242
99                 X    =         2429939
66
 Y    =       12177313
94  feet           Y    =         3711645
29  meter
 Z    =       16838473
39                 Z    =         5132366
69
 XDOT =     -22372
747645                 XDOT =       -6819
213482
 YDOT =       7495
410557  feet/sec       YDOT =        2284
601138  meter/sec
 ZDOT =       5169
678604                 ZDOT =        1575
718039


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
79960114  
00016717  00000-0  10270-3 0  9115
2 25544  51
6422 256
9797 0006695  47
6624 312
5092 15
50033042 29772


Satellite: ISS
Catalog Number: 25544
Epoch time:      19261
79960114   =   yrday
fracday
Element set:     911
Inclination:       51
6422  deg
RA of node:       256
9797  deg
Eccentricity:     
0006695     
Arg of perigee:    47
6624  deg
Mean anomaly:     312
5092  deg
Mean motion:   15
50033042  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2977
Checksum:              321


Coasting Arc #13 (Orbit 2991)
---------------------------------------

Vector Time (GMT): 2019/262/17:57:49
866
Vector Time (MET): N/A
Weight (LBS)     : 951554
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3525329
22                 A    =         6789794
01  meter
 Y    =        2605511
32  meter          E    =           
0020307
 Z    =       -5202932
46                 I    =           51
25810
 XDOT =      -3293
900260                 Wp   =           71
21238
 YDOT =      -6800
631459  meter/sec      RA   =          251
30011  deg
 ZDOT =      -1171
131333                 TA   =          187
44814
                                          MA   =          187
47836
                                          Ha   =            229
730  n
mi
                                          Hp   =            218
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11566040
73                 X    =        -3528929
53
 Y    =        8548265
49  feet           Y    =         2566068
17  meter
 Z    =      -17069988
38                 Z    =        -5220066
29
 XDOT =     -10806
759384                 XDOT =       -3211
920049
 YDOT =     -22311
783002  feet/sec       YDOT =       -6837
007862  meter/sec
 ZDOT =      -3842
294398                 ZDOT =       -1186
932540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7918953
78                 X    =        -2413697
11
 Y    =      -11893888
71  feet           Y    =        -3625257
28  meter
 Z    =      -17148067
73                 Z    =        -5226731
04
 XDOT =      21992
269261                 XDOT =        6703
243671
 YDOT =      -8987
434464  feet/sec       YDOT =       -2739
370025  meter/sec
 ZDOT =      -3913
707060                 ZDOT =       -1192
897912


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
76669780  
00016717  00000-0  10270-3 0  9129
2 25544  51
6434 252
1887 0006848  50
6545 309
5212 15
50030373 29920


Satellite: ISS
Catalog Number: 25544
Epoch time:      19262
76669780   =   yrday
fracday
Element set:     912
Inclination:       51
6434  deg
RA of node:       252
1887  deg
Eccentricity:     
0006848     
Arg of perigee:    50
6545  deg
Mean anomaly:     309
5212  deg
Mean motion:   15
50030373  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2992
Checksum:              323


Coasting Arc #14 (Orbit 3007)
---------------------------------------

Vector Time (GMT): 2019/263/17:57:49
866
Vector Time (MET): N/A
Weight (LBS)     : 951554
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3496792
20                 A    =         6789492
03  meter
 Y    =       -2503304
50  meter          E    =           
0008698
 Z    =        5246313
20                 I    =           51
26867
 XDOT =       3629
405846                 Wp   =           74
15101
 YDOT =       6709
891180  meter/sec      RA   =          246
31792  deg
 ZDOT =        783
820987                 TA   =            8
32746
                                          MA   =            8
31303
                                          Ha   =            229
613  n
mi
                                          Hp   =            218
956

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11472415
34                 X    =         3499041
03
 Y    =       -8212941
29  feet           Y    =        -2464188
12  meter
 Z    =       17212313
66                 Z    =         5263305
05
 XDOT =      11907
499495                 XDOT =        3550
296749
 YDOT =      22014
078676  feet/sec       YDOT =        6750
035460  meter/sec
 ZDOT =       2571
591164                 ZDOT =         801
259051

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7790725
08                 X    =         2374613
00
 Y    =       11649114
57  feet           Y    =         3550650
12  meter
 Z    =       17289742
40                 Z    =         5269913
48
 XDOT =     -21585
230756                 XDOT =       -6579
178334
 YDOT =      10508
020564  feet/sec       YDOT =        3202
844668  meter/sec
 ZDOT =       2650
469863                 ZDOT =         807
863214


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
79826511  
00016717  00000-0  10270-3 0  9131
2 25544  51
6431 247
0781 0006809  54
4516 305
7269 15
50038007 30081


Satellite: ISS
Catalog Number: 25544
Epoch time:      19263
79826511   =   yrday
fracday
Element set:     913
Inclination:       51
6431  deg
RA of node:       247
0781  deg
Eccentricity:     
0006809     
Arg of perigee:    54
4516  deg
Mean anomaly:     305
7269  deg
Mean motion:   15
50038007  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3008
Checksum:              306


Coasting Arc #15 (Orbit 3022)
---------------------------------------

Vector Time (GMT): 2019/264/17:57:49
866
Vector Time (MET): N/A
Weight (LBS)     : 951554
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3509528
55                 A    =         6789379
07  meter
 Y    =        2432243
53  meter          E    =           
0020955
 Z    =       -5296635
08                 I    =           51
28226
 XDOT =      -3936
400934                 Wp   =           77
74025
 YDOT =      -6543
430612  meter/sec      RA   =          241
33728  deg
 ZDOT =       -393
501525                 TA   =          188
46020
                                          MA   =          188
49558
                                          Ha   =            229
790  n
mi
                                          Hp   =            218
750

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11514201
29                 X    =        -3510737
45
 Y    =        7979801
60  feet           Y    =         2392990
60  meter
 Z    =      -17377411
66                 Z    =        -5313686
19
 XDOT =     -12914
701228                 XDOT =       -3861
026412
 YDOT =     -21467
948203  feet/sec       YDOT =       -6587
028788  meter/sec
 ZDOT =      -1291
015501                 ZDOT =        -412
439983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7756056
47                 X    =        -2364046
01
 Y    =      -11549514
19  feet           Y    =        -3520291
93  meter
 Z    =      -17455108
45                 Z    =        -5320317
06
 XDOT =      20872
261437                 XDOT =        6361
865286
 YDOT =     -11921
035941  feet/sec       YDOT =       -3633
531755  meter/sec
 ZDOT =      -1376
747358                 ZDOT =        -419
632595


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
76536055  
00016717  00000-0  10270-3 0  9141
2 25544  51
6427 242
2878 0006822  57
3029 302
8778 15
50030806 30235


Satellite: ISS
Catalog Number: 25544
Epoch time:      19264
76536055   =   yrday
fracday
Element set:     914
Inclination:       51
6427  deg
RA of node:       242
2878  deg
Eccentricity:     
0006822     
Arg of perigee:    57
3029  deg
Mean anomaly:     302
8778  deg
Mean motion:   15
50030806  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3023
Checksum:              310


Coasting Arc #16 (Orbit 3024)
---------------------------------------

Vector Time (GMT): 2019/264/20:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951554
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -544976
52                 A    =         6797372
68  meter
 Y    =       -6031125
87  meter          E    =           
0019292
 Z    =        3065198
32                 I    =           51
30870
 XDOT =       5574
644020                 Wp   =           74
97381
 YDOT =       1985
988898  meter/sec      RA   =          240
92113  deg
 ZDOT =       4877
940740                 TA   =          320
37820
                                          MA   =          320
51902
                                          Ha   =            229
785  n
mi
                                          Hp   =            218
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1787980
71                 X    =         -492383
37
 Y    =      -19787158
38  feet           Y    =        -6036926
04  meter
 Z    =       10056424
93                 Z    =         3062678
91
 XDOT =      18289
514501                 XDOT =        5528
327289
 YDOT =       6515
711608  feet/sec       YDOT =        2048
069655  meter/sec
 ZDOT =      16003
742584                 ZDOT =        4904
907928

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16103467
52                 X    =         4908336
90
 Y    =      -11646020
29  feet           Y    =        -3549706
99  meter
 Z    =       10045334
21                 Z    =         3061817
87
 XDOT =       2768
928065                 XDOT =         843
969274
 YDOT =      17797
614811  feet/sec       YDOT =        5424
712994  meter/sec
 ZDOT =      16126
268779                 ZDOT =        4915
286724


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
89430587  
00016717  00000-0  10270-3 0  9159
2 25544  51
6413 241
6483 0006774  56
8438 303
3361 15
50009691 30253


Satellite: ISS
Catalog Number: 25544
Epoch time:      19264
89430587   =   yrday
fracday
Element set:     915
Inclination:       51
6413  deg
RA of node:       241
6483  deg
Eccentricity:     
0006774     
Arg of perigee:    56
8438  deg
Mean anomaly:     303
3361  deg
Mean motion:   15
50009691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3025
Checksum:              316


Coasting Arc #17 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2019/265/20:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951554
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         712988
92                 A    =         6796564
83  meter
 Y    =        5867856
19  meter          E    =           
0010943
 Z    =       -3366965
24                 I    =           51
32292
 XDOT =      -5779
492102                 Wp   =           73
91250
 YDOT =      -1944
129990  meter/sec      RA   =          235
94481  deg
 ZDOT =      -4621
649546                 TA   =          145
43288
                                          MA   =          145
36168
                                          Ha   =            229
785  n
mi
                                          Hp   =            218
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2339202
48                 X    =          663674
77
 Y    =       19251496
67  feet           Y    =         5875553
52  meter
 Z    =      -11046473
89                 Z    =        -3363621
70
 XDOT =     -18961
588262                 XDOT =       -5734
873238
 YDOT =      -6378
379231  feet/sec       YDOT =       -2008
510969  meter/sec
 ZDOT =     -15162
892210                 ZDOT =       -4649
615847

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15152478
52                 X    =        -4618475
45
 Y    =       12117033
98  feet           Y    =         3693271
96  meter
 Z    =      -11031611
86                 Z    =        -3362435
29
 XDOT =      -3531
652647                 XDOT =       -1076
447727
 YDOT =     -18307
969995  feet/sec       YDOT =       -5580
269254  meter/sec
 ZDOT =     -15289
982813                 ZDOT =       -4660
386761


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
86139899  
00016717  00000-0  10270-3 0  9160
2 25544  51
6410 236
8569 0006631  60
2114 299
9695 15
50009791 30401


Satellite: ISS
Catalog Number: 25544
Epoch time:      19265
86139899   =   yrday
fracday
Element set:     916
Inclination:       51
6410  deg
RA of node:       236
8569  deg
Eccentricity:     
0006631     
Arg of perigee:    60
2114  deg
Mean anomaly:     299
9695  deg
Mean motion:   15
50009791  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3040
Checksum:              335


Coasting Arc #18 (Orbit 3055)
---------------------------------------

Vector Time (GMT): 2019/266/20:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951554
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -886054
51                 A    =         6795829
54  meter
 Y    =       -5678247
69  meter          E    =           
0018086
 Z    =        3609401
69                 I    =           51
33983
 XDOT =       6015
573660                 Wp   =           82
97252
 YDOT =       1856
112210  meter/sec      RA   =          230
96869  deg
 ZDOT =       4379
982372                 TA   =          319
95817
                                          MA   =          320
09136
                                          Ha   =            229
828  n
mi
                                          Hp   =            218
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2907002
99                 X    =         -840025
32
 Y    =      -18629421
54  feet           Y    =        -5687898
70  meter
 Z    =       11841869
07                 Z    =         3605209
53
 XDOT =      19736
134054                 XDOT =        5973
095460
 YDOT =       6089
606987  feet/sec       YDOT =        1923
145210  meter/sec
 ZDOT =      14370
020904                 ZDOT =        4409
100554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14109192
32                 X    =         4300481
82
 Y    =      -12525189
71  feet           Y    =        -3817677
82  meter
 Z    =       11823121
04                 Z    =         3603687
29
 XDOT =       4497
668083                 XDOT =        1370
889232
 YDOT =      18807
919516  feet/sec       YDOT =        5732
653868  meter/sec
 ZDOT =      14502
375912                 ZDOT =        4420
324178


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
89296345  
00016717  00000-0  10270-3 0  9175
2 25544  51
6407 231
7454 0006712  63
4669 296
7169 15
50014281 30562


Satellite: ISS
Catalog Number: 25544
Epoch time:      19266
89296345   =   yrday
fracday
Element set:     917
Inclination:       51
6407  deg
RA of node:       231
7454  deg
Eccentricity:     
0006712     
Arg of perigee:    63
4669  deg
Mean anomaly:     296
7169  deg
Mean motion:   15
50014281  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3056
Checksum:              331
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