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

 
Date: October 15th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15204 0235 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 562 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


292/20:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 8
000/00:00:00 000 0 0 0 0 220 1

297/21:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 1
000/00:00:00 000 0 0 0 0 220 7

301/10:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 8
000/00:00:00 000 0 0 0 0 221 2

Coasting Arc #1 (Orbit 3375)
---------------------------------------

Vector Time (GMT): 2019/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5165202
69                 A    =         6793200
18  meter
 Y    =       -1099545
31  meter          E    =           
0011450
 Z    =       -4280551
63                 I    =           51
93281
 XDOT =      -1597
545847                 Wp   =          105
89044
 YDOT =       6551
794042  meter/sec      RA   =          128
57618  deg
 ZDOT =      -3621
757725                 TA   =          127
22229
                                          MA   =          127
11776
                                          Ha   =            229
214  n
mi
                                          Hp   =            219
438

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16946203
06                 X    =         5197907
25
 Y    =       -3607432
12  feet           Y    =        -1041601
86  meter
 Z    =      -14043804
55                 Z    =        -4255380
92
 XDOT =      -5241
292148                 XDOT =       -1653
098286
 YDOT =      21495
387277  feet/sec       YDOT =        6533
618242  meter/sec
 ZDOT =     -11882
407234                 ZDOT =       -3629
653653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14472727
25                 X    =        -4411287
27
 Y    =        9692245
40  feet           Y    =         2954196
40  meter
 Z    =      -13928975
41                 Z    =        -4245551
70
 XDOT =      -2504
450521                 XDOT =        -763
356519
 YDOT =     -20815
745540  feet/sec       YDOT =       -6344
639241  meter/sec
 ZDOT =     -11918
761651                 ZDOT =       -3632
838551


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   19287
52282763  
00016717  00000-0  10270-3 0  9009
2 25544  51
6385 129
5249 0006775 149
7252 210
4292 15
50191586 33767


Satellite: ISS
Catalog Number: 25544
Epoch time:      19287
52282763   =   yrday
fracday
Element set:     900
Inclination:       51
6385  deg
RA of node:       129
5249  deg
Eccentricity:     
0006775     
Arg of perigee:   149
7252  deg
Mean anomaly:     210
4292  deg
Mean motion:   15
50191586  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3376
Checksum:              330


Coasting Arc #2 (Orbit 3391)
---------------------------------------

Vector Time (GMT): 2019/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4965504
15                 A    =         6792446
12  meter
 Y    =        1112278
57  meter          E    =           
0014779
 Z    =        4494552
98                 I    =           51
95045
 XDOT =       1447
314345                 Wp   =          128
94169
 YDOT =      -6782
832322  meter/sec      RA   =          123
63982  deg
 ZDOT =       3261
292558                 TA   =          288
26892
                                          MA   =          288
42969
                                          Ha   =            229
189  n
mi
                                          Hp   =            219
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16291024
13                 X    =        -4999405
52
 Y    =        3649207
91  feet           Y    =         1056561
54  meter
 Z    =       14745908
72                 Z    =         4470349
39
 XDOT =       4748
406645                 XDOT =        1507
212424
 YDOT =     -22253
386883  feet/sec       YDOT =       -6766
312303  meter/sec
 ZDOT =      10699
778734                 ZDOT =        3268
469183

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13688204
43                 X    =         4172164
71
 Y    =       -9725834
37  feet           Y    =        -2964434
32  meter
 Z    =       14635477
94                 Z    =         4460893
68
 XDOT =       3618
867703                 XDOT =        1103
030876
 YDOT =      21324
893596  feet/sec       YDOT =        6499
827568  meter/sec
 ZDOT =      10732
884898                 ZDOT =        3271
383317


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   19288
55427249  
00016717  00000-0  10270-3 0  9014
2 25544  51
6389 124
4128 0006690 153
5493 206
6000 15
50174515 33922


Satellite: ISS
Catalog Number: 25544
Epoch time:      19288
55427249   =   yrday
fracday
Element set:     901
Inclination:       51
6389  deg
RA of node:       124
4128  deg
Eccentricity:     
0006690     
Arg of perigee:   153
5493  deg
Mean anomaly:     206
6000  deg
Mean motion:   15
50174515  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3392
Checksum:              310


Coasting Arc #3 (Orbit 3406)
---------------------------------------

Vector Time (GMT): 2019/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4779948
12                 A    =         6791507
23  meter
 Y    =       -1040039
41  meter          E    =           
0013027
 Z    =       -4720874
13                 I    =           51
96436
 XDOT =      -1284
460516                 Wp   =          102
11873
 YDOT =       6986
288251  meter/sec      RA   =          118
70321  deg
 ZDOT =      -2848
949116                 TA   =          139
72528
                                          MA   =          139
62870
                                          Ha   =            229
071  n
mi
                                          Hp   =            219
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15682244
50                 X    =         4814154
89
 Y    =       -3412202
78  feet           Y    =         -986395
61  meter
 Z    =      -15488432
19                 Z    =        -4697571
18
 XDOT =      -4214
109306                 XDOT =       -1348
648770
 YDOT =      22920
893211  feet/sec       YDOT =        6971
565475  meter/sec
 ZDOT =      -9346
945918                 ZDOT =       -2855
344939

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13062298
58                 X    =        -3981388
61
 Y    =        9499198
04  feet           Y    =         2895355
56  meter
 Z    =      -15382101
43                 Z    =        -4688464
51
 XDOT =      -4768
820859                 XDOT =       -1453
536598
 YDOT =     -21691
336210  feet/sec       YDOT =       -6611
519277  meter/sec
 ZDOT =      -9376
524210                 ZDOT =       -2857
964579


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   19289
52124806  
00016717  00000-0  10270-3 0  9026
2 25544  51
6381 119
6195 0006797 156
3406 203
8058 15
50202293 34071


Satellite: ISS
Catalog Number: 25544
Epoch time:      19289
52124806   =   yrday
fracday
Element set:     902
Inclination:       51
6381  deg
RA of node:       119
6195  deg
Eccentricity:     
0006797     
Arg of perigee:   156
3406  deg
Mean anomaly:     203
8058  deg
Mean motion:   15
50202293  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3407
Checksum:              311


Coasting Arc #4 (Orbit 3422)
---------------------------------------

Vector Time (GMT): 2019/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4609095
20                 A    =         6790903
55  meter
 Y    =         988912
50  meter          E    =           
0012981
 Z    =        4884759
19                 I    =           51
97679
 XDOT =       1069
744944                 Wp   =          139
65909
 YDOT =      -7182
705697  meter/sec      RA   =          113
76861  deg
 ZDOT =       2450
240494                 TA   =          286
32609
                                          MA   =          286
46880
                                          Ha   =            229
092  n
mi
                                          Hp   =            219
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15121703
40                 X    =        -4643539
02
 Y    =        3244463
59  feet           Y    =          937177
88  meter
 Z    =       16026112
81                 Z    =         4862285
65
 XDOT =       3509
661889                 XDOT =        1138
082314
 YDOT =     -23565
307405  feet/sec       YDOT =       -7170
360894  meter/sec
 ZDOT =       8038
846766                 ZDOT =        2455
603216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12461846
34                 X    =         3798370
76
 Y    =       -9336567
34  feet           Y    =        -2845785
72  meter
 Z    =       15923556
32                 Z    =         4853499
97
 XDOT =       6071
225890                 XDOT =        1850
509651
 YDOT =      21930
930030  feet/sec       YDOT =        6684
547473  meter/sec
 ZDOT =       8063
747542                 ZDOT =        2457
830251


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   19290
55268921  
00016717  00000-0  10270-3 0  9039
2 25544  51
6378 114
5078 0006745 159
9934 200
1482 15
50172617 34234


Satellite: ISS
Catalog Number: 25544
Epoch time:      19290
55268921   =   yrday
fracday
Element set:     903
Inclination:       51
6378  deg
RA of node:       114
5078  deg
Eccentricity:     
0006745     
Arg of perigee:   159
9934  deg
Mean anomaly:     200
1482  deg
Mean motion:   15
50172617  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3423
Checksum:              317


Coasting Arc #5 (Orbit 3437)
---------------------------------------

Vector Time (GMT): 2019/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4466688
60                 A    =         6790139
12  meter
 Y    =        -862478
54  meter          E    =           
0014717
 Z    =       -5052219
13                 I    =           51
98677
 XDOT =       -844
509073                 Wp   =          103
38353
 YDOT =       7335
929403  meter/sec      RA   =          108
83389  deg
 ZDOT =      -2007
187285                 TA   =          147
21601
                                          MA   =          147
12460
                                          Ha   =            228
960  n
mi
                                          Hp   =            219
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14654490
17                 X    =         4500542
58
 Y    =       -2829654
00  feet           Y    =         -812339
62  meter
 Z    =      -16575522
07                 Z    =        -5030438
87
 XDOT =      -2770
699059                 XDOT =        -916
728759
 YDOT =      24068
009851  feet/sec       YDOT =        7326
081687  meter/sec
 ZDOT =      -6585
260120                 ZDOT =       -2011
465154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12062600
73                 X    =        -3676680
70
 Y    =        8974405
26  feet           Y    =         2735398
72  meter
 Z    =      -16476124
24                 Z    =        -5021922
67
 XDOT =      -7364
791871                 XDOT =       -2244
788562
 YDOT =     -21975
893548  feet/sec       YDOT =       -6698
252354  meter/sec
 ZDOT =      -6605
244731                 ZDOT =       -2013
278594


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   19291
51966310  
00016717  00000-0  10270-3 0  9044
2 25544  51
6376 109
7154 0006941 163
2139 196
9242 15
50205626 34385


Satellite: ISS
Catalog Number: 25544
Epoch time:      19291
51966310   =   yrday
fracday
Element set:     904
Inclination:       51
6376  deg
RA of node:       109
7154  deg
Eccentricity:     
0006941     
Arg of perigee:   163
2139  deg
Mean anomaly:     196
9242  deg
Mean motion:   15
50205626  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3438
Checksum:              313


Coasting Arc #6 (Orbit 3453)
---------------------------------------

Vector Time (GMT): 2019/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4342818
03                 A    =         6789722
04  meter
 Y    =         761350
44  meter          E    =           
0010969
 Z    =        5160844
40                 I    =           51
99546
 XDOT =        578
906821                 Wp   =          149
76955
 YDOT =      -7477
288687  meter/sec      RA   =          103
89987  deg
 ZDOT =       1579
552160                 TA   =          285
00746
                                          MA   =          285
12884
                                          Ha   =            228
959  n
mi
                                          Hp   =            219
948

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14248090
64                 X    =        -4376077
94
 Y    =        2497868
89  feet           Y    =          712599
98  meter
 Z    =       16931904
19                 Z    =         5139667
40
 XDOT =       1899
300594                 XDOT =         654
804260
 YDOT =     -24531
787030  feet/sec       YDOT =       -7470
390582  meter/sec
 ZDOT =       5182
257743                 ZDOT =        1582
548632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11695294
03                 X    =         3564725
62
 Y    =       -8702363
88  feet           Y    =        -2652480
51  meter
 Z    =       16835253
95                 Z    =         5131385
41
 XDOT =       8755
059532                 XDOT =        2668
542145
 YDOT =      21887
073396  feet/sec       YDOT =        6671
179971  meter/sec
 ZDOT =       5196
427613                 ZDOT =        1583
871137


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   19292
55110165  
00016717  00000-0  10270-3 0  9059
2 25544  51
6383 104
6035 0006825 167
2989 192
8335 15
50174734 34544


Satellite: ISS
Catalog Number: 25544
Epoch time:      19292
55110165   =   yrday
fracday
Element set:     905
Inclination:       51
6383  deg
RA of node:       104
6035  deg
Eccentricity:     
0006825     
Arg of perigee:   167
2989  deg
Mean anomaly:     192
8335  deg
Mean motion:   15
50174734  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3454
Checksum:              317


Coasting Arc #7 (Orbit 3458)
---------------------------------------

Vector Time (GMT): 2019/292/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4036470
87                 A    =         6788875
36  meter
 Y    =        1129345
11  meter          E    =           
0017682
 Z    =       -5354608
88                 I    =           51
99897
 XDOT =      -1776
214677                 Wp   =          113
85656
 YDOT =       7437
501372  meter/sec      RA   =          102
12420  deg
 ZDOT =        223
323107                 TA   =          158
30407
                                          MA   =          158
22907
                                          Ha   =            228
805  n
mi
                                          Hp   =            220
097

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13243014
67                 X    =         4049552
42
 Y    =        3705200
50  feet           Y    =         1174556
96  meter
 Z    =      -17567614
42                 Z    =        -5334969
05
 XDOT =      -5827
475973                 XDOT =       -1860
335762
 YDOT =      24401
251220  feet/sec       YDOT =        7417
168134  meter/sec
 ZDOT =        732
687359                 ZDOT =         214
490498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10681728
89                 X    =         3255790
96
 Y    =        8839891
17  feet           Y    =         2694398
83  meter
 Z    =      -17478101
07                 Z    =        -5327325
21
 XDOT =     -14648
342339                 XDOT =       -4464
814745
 YDOT =      19109
869603  feet/sec       YDOT =        5824
688255  meter/sec
 ZDOT =        691
890758                 ZDOT =         210
888303


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   19292
87342429  
00016717  00000-0  10270-3 0  9065
2 25544  51
6417 103
0085 0006832 168
4577 191
6731 15
50187073 34596


Satellite: ISS
Catalog Number: 25544
Epoch time:      19292
87342429   =   yrday
fracday
Element set:     906
Inclination:       51
6417  deg
RA of node:       103
0085  deg
Eccentricity:     
0006832     
Arg of perigee:   168
4577  deg
Mean anomaly:     191
6731  deg
Mean motion:   15
50187073  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3459
Checksum:              325


Coasting Arc #8 (Orbit 3474)
---------------------------------------

Vector Time (GMT): 2019/293/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4023166
79                 A    =         6788874
48  meter
 Y    =       -1274361
41  meter          E    =           
0006547
 Z    =        5314052
97                 I    =           52
00498
 XDOT =       1480
668245                 Wp   =          145
20125
 YDOT =      -7490
629651  meter/sec      RA   =           97
19147  deg
 ZDOT =       -680
157438                 TA   =          311
23505
                                          MA   =          311
29144
                                          Ha   =            228
783  n
mi
                                          Hp   =            220
013

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13199366
12                 X    =        -4034430
61
 Y    =       -4180975
77  feet           Y    =        -1319414
33  meter
 Z    =       17434556
99                 Z    =         5294482
27
 XDOT =       4857
835451                 XDOT =        1567
624469
 YDOT =     -24575
556598  feet/sec       YDOT =       -7473
585566  meter/sec
 ZDOT =      -2231
487658                 ZDOT =        -672
753654

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10604355
11                 X    =        -3232207
44
 Y    =       -9074887
62  feet           Y    =        -2766025
75  meter
 Z    =       17345364
48                 Z    =         5286867
09
 XDOT =      13472
953572                 XDOT =        4106
556249
 YDOT =     -19912
911164  feet/sec       YDOT =       -6069
455323  meter/sec
 ZDOT =      -2197
185757                 ZDOT =        -669
702219


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   19293
90485799  
00016717  00000-0  10270-3 0  9079
2 25544  51
6413  97
8979 0006766 171
3158 188
8111 15
50227017 34759


Satellite: ISS
Catalog Number: 25544
Epoch time:      19293
90485799   =   yrday
fracday
Element set:     907
Inclination:       51
6413  deg
RA of node:        97
8979  deg
Eccentricity:     
0006766     
Arg of perigee:   171
3158  deg
Mean anomaly:     188
8111  deg
Mean motion:   15
50227017  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3475
Checksum:              352


Coasting Arc #9 (Orbit 3489)
---------------------------------------

Vector Time (GMT): 2019/294/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4055041
51                 A    =         6789274
23  meter
 Y    =        1454771
93  meter          E    =           
0017044
 Z    =       -5261359
39                 I    =           52
00957
 XDOT =      -1188
452573                 Wp   =          121
34252
 YDOT =       7470
121080  meter/sec      RA   =           92
25799  deg
 ZDOT =       1143
655109                 TA   =          159
62618
                                          MA   =          159
55810
                                          Ha   =            228
591  n
mi
                                          Hp   =            220
375

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13303941
95                 X    =         4064029
51
 Y    =        4772873
79  feet           Y    =         1500168
51  meter
 Z    =      -17261677
79                 Z    =        -5241639
46
 XDOT =      -3899
122614                 XDOT =       -1277
452612
 YDOT =      24508
271259  feet/sec       YDOT =        7456
333337  meter/sec
 ZDOT =       3752
149309                 ZDOT =        1137
665800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10631560
81                 X    =         3240499
74
 Y    =        9478366
76  feet           Y    =         2889006
19  meter
 Z    =      -17171813
94                 Z    =        -5233968
89
 XDOT =     -12181
807920                 XDOT =       -3713
015054
 YDOT =      20446
260946  feet/sec       YDOT =        6232
020336  meter/sec
 ZDOT =       3724
285410                 ZDOT =        1135
162193


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   19294
87182781  
00016717  00000-0  10270-3 0  9082
2 25544  51
6419  93
1059 0006733 175
2984 184
8231 15
50192460 34906


Satellite: ISS
Catalog Number: 25544
Epoch time:      19294
87182781   =   yrday
fracday
Element set:     908
Inclination:       51
6419  deg
RA of node:        93
1059  deg
Eccentricity:     
0006733     
Arg of perigee:   175
2984  deg
Mean anomaly:     184
8231  deg
Mean motion:   15
50192460  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3490
Checksum:              332


Coasting Arc #10 (Orbit 3505)
---------------------------------------

Vector Time (GMT): 2019/295/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4108259
91                 A    =         6789541
86  meter
 Y    =       -1599404
20  meter          E    =           
0005769
 Z    =        5158941
65                 I    =           52
01004
 XDOT =        899
027269                 Wp   =          132
46735
 YDOT =      -7444
272518  meter/sec      RA   =           87
32543  deg
 ZDOT =      -1594
641702                 TA   =          332
82134
                                          MA   =          332
85152
                                          Ha   =            228
587  n
mi
                                          Hp   =            220
276

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13478543
01                 X    =        -4115129
09
 Y    =       -5247389
11  feet           Y    =        -1645383
96  meter
 Z    =       16925661
57                 Z    =         5138968
41
 XDOT =       2949
564530                 XDOT =         989
950427
 YDOT =     -24423
466267  feet/sec       YDOT =       -7433
710610  meter/sec
 ZDOT =      -5231
764113                 ZDOT =       -1590
053528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10782463
26                 X    =        -3286494
80
 Y    =       -9798839
14  feet           Y    =        -2986686
17  meter
 Z    =       16834650
91                 Z    =         5131201
60
 XDOT =      10884
703440                 XDOT =        3317
657609
 YDOT =     -20913
671712  feet/sec       YDOT =       -6374
487138  meter/sec
 ZDOT =      -5210
280909                 ZDOT =       -1588
093621


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   19295
90325938  
00016717  00000-0  10270-3 0  9091
2 25544  51
6409  87
9948 0006712 178
0891 182
0286 15
50233162 35061


Satellite: ISS
Catalog Number: 25544
Epoch time:      19295
90325938   =   yrday
fracday
Element set:     909
Inclination:       51
6409  deg
RA of node:        87
9948  deg
Eccentricity:     
0006712     
Arg of perigee:   178
0891  deg
Mean anomaly:     182
0286  deg
Mean motion:   15
50233162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3506
Checksum:              336


Coasting Arc #11 (Orbit 3520)
---------------------------------------

Vector Time (GMT): 2019/296/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4208257
07                 A    =         6790195
25  meter
 Y    =        1763292
02  meter          E    =           
0015482
 Z    =       -5042079
60                 I    =           52
01080
 XDOT =       -626
705236                 Wp   =          129
56323
 YDOT =       7346
702339  meter/sec      RA   =           82
39231  deg
 ZDOT =       2040
782336                 TA   =          160
24978
                                          MA   =          160
18976
                                          Ha   =            228
326  n
mi
                                          Hp   =            220
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13806617
70                 X    =         4212718
54
 Y    =        5785078
79  feet           Y    =         1810376
45  meter
 Z    =      -16542255
91                 Z    =        -5021626
50
 XDOT =      -2056
119540                 XDOT =        -718
724705
 YDOT =      24103
354132  feet/sec       YDOT =        7339
179652  meter/sec
 ZDOT =       6695
480105                 ZDOT =        2037
514193

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11069507
27                 X    =         3373985
82
 Y    =       10228890
97  feet           Y    =         3117765
97  meter
 Z    =      -16449068
60                 Z    =        -5013676
11
 XDOT =      -9538
650067                 XDOT =       -2907
380540
 YDOT =      21093
350002  feet/sec       YDOT =        6429
253081  meter/sec
 ZDOT =       6680
014706                 ZDOT =        2036
068482


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   19296
87022451  
00016717  00000-0  10270-3 0  9104
2 25544  51
6425  83
2026 0006583 182
8139 177
2975 15
50201472 35216


Satellite: ISS
Catalog Number: 25544
Epoch time:      19296
87022451   =   yrday
fracday
Element set:     910
Inclination:       51
6425  deg
RA of node:        83
2026  deg
Eccentricity:     
0006583     
Arg of perigee:   182
8139  deg
Mean anomaly:     177
2975  deg
Mean motion:   15
50201472  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3521
Checksum:              304


Coasting Arc #12 (Orbit 3536)
---------------------------------------

Vector Time (GMT): 2019/297/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4323668
74                 A    =         6790706
38  meter
 Y    =       -1887345
09  meter          E    =           
0006271
 Z    =        4878506
04                 I    =           52
00572
 XDOT =        369
642051                 Wp   =          118
01015
 YDOT =      -7245
954185  meter/sec      RA   =           77
45955  deg
 ZDOT =      -2476
081217                 TA   =          356
18231
                                          MA   =          356
18710
                                          Ha   =            228
318  n
mi
                                          Hp   =            220
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14185264
89                 X    =        -4325939
93
 Y    =       -6192077
05  feet           Y    =        -1935707
80  meter
 Z    =       16005597
24                 Z    =         4857497
61
 XDOT =       1212
736387                 XDOT =         462
668525
 YDOT =     -23772
815569  feet/sec       YDOT =       -7241
300594  meter/sec
 ZDOT =      -8123
626041                 ZDOT =       -2474
059223

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11464234
70                 X    =        -3494298
74
 Y    =      -10544641
25  feet           Y    =        -3214006
65  meter
 Z    =       15909888
90                 Z    =         4849334
14
 XDOT =       8241
366167                 XDOT =        2511
968408
 YDOT =     -21200
143603  feet/sec       YDOT =       -6461
803770  meter/sec
 ZDOT =      -8113
841720                 ZDOT =       -2473
098956


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   19297
90165158  
00016717  00000-0  10270-3 0  9112
2 25544  51
6409  78
0909 0006523 185
4027 174
7054 15
50242034 35375


Satellite: ISS
Catalog Number: 25544
Epoch time:      19297
90165158   =   yrday
fracday
Element set:     911
Inclination:       51
6409  deg
RA of node:        78
0909  deg
Eccentricity:     
0006523     
Arg of perigee:   185
4027  deg
Mean anomaly:     174
7054  deg
Mean motion:   15
50242034  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3537
Checksum:              311


Coasting Arc #13 (Orbit 3537)
---------------------------------------

Vector Time (GMT): 2019/297/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1818957
60                 A    =         6794673
73  meter
 Y    =        5341758
25  meter          E    =           
0013221
 Z    =        3782248
43                 I    =           52
01680
 XDOT =      -4446
733502                 Wp   =          125
96595
 YDOT =      -4549
186712  meter/sec      RA   =           77
24747  deg
 ZDOT =       4268
437286                 TA   =          278
97543
                                          MA   =          279
12504
                                          Ha   =            228
146  n
mi
                                          Hp   =            220
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5967708
65                 X    =        -1896927
80
 Y    =       17525453
57  feet           Y    =         5320981
65  meter
 Z    =       12408951
53                 Z    =         3773222
79
 XDOT =     -14589
020675                 XDOT =       -4416
266654
 YDOT =     -14925
153256  feet/sec       YDOT =       -4598
742612  meter/sec
 ZDOT =      14004
059338                 ZDOT =        4246
910721

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6169157
87                 X    =        -1880359
32
 Y    =       17485053
08  feet           Y    =         5329444
18  meter
 Z    =       12367358
54                 Z    =         3769570
88
 XDOT =     -13307
338329                 XDOT =       -4056
076723
 YDOT =     -14572
978477  feet/sec       YDOT =       -4441
843840  meter/sec
 ZDOT =      13906
192542                 ZDOT =        4238
607487


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   19297
96611577  
00016717  00000-0  10270-3 0  9120
2 25544  51
6391  77
7719 0006537 187
2126 172
8931 15
50237040 35380


Satellite: ISS
Catalog Number: 25544
Epoch time:      19297
96611577   =   yrday
fracday
Element set:     912
Inclination:       51
6391  deg
RA of node:        77
7719  deg
Eccentricity:     
0006537     
Arg of perigee:   187
2126  deg
Mean anomaly:     172
8931  deg
Mean motion:   15
50237040  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3538
Checksum:              334


Coasting Arc #14 (Orbit 3552)
---------------------------------------

Vector Time (GMT): 2019/298/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1698576
45                 A    =         6793768
08  meter
 Y    =       -5162076
42  meter          E    =           
0007069
 Z    =       -4079101
87                 I    =           52
00485
 XDOT =       4683
445477                 Wp   =          125
40513
 YDOT =       4626
394296  meter/sec      RA   =           72
31592  deg
 ZDOT =      -3913
184686                 TA   =          104
21442
                                          MA   =          104
13588
                                          Ha   =            228
127  n
mi
                                          Hp   =            220
866

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5572757
40                 X    =         1775988
41
 Y    =      -16935946
27  feet           Y    =        -5142649
19  meter
 Z    =      -13382880
15                 Z    =        -4070662
29
 XDOT =      15365
634766                 XDOT =        4650
372124
 YDOT =      15178
458977  feet/sec       YDOT =        4678
582690  meter/sec
 ZDOT =     -12838
532434                 ZDOT =       -3890
514519

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5485301
43                 X    =         1671919
88
 Y    =      -16995100
22  feet           Y    =        -5180106
55  meter
 Z    =      -13343965
64                 Z    =        -4067240
73
 XDOT =      14370
665132                 XDOT =        4380
178732
 YDOT =      14615
101348  feet/sec       YDOT =        4454
682891  meter/sec
 ZDOT =     -12735
465362                 ZDOT =       -3881
769842


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   19298
93307951  
00016717  00000-0  10270-3 0  9137
2 25544  51
6389  72
9791 0006477 189
7495 170
3529 15
50208562 35533


Satellite: ISS
Catalog Number: 25544
Epoch time:      19298
93307951   =   yrday
fracday
Element set:     913
Inclination:       51
6389  deg
RA of node:        72
9791  deg
Eccentricity:     
0006477     
Arg of perigee:   189
7495  deg
Mean anomaly:     170
3529  deg
Mean motion:   15
50208562  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3553
Checksum:              354


Coasting Arc #15 (Orbit 3568)
---------------------------------------

Vector Time (GMT): 2019/299/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1577856
33                 A    =         6792790
29  meter
 Y    =        4996420
13  meter          E    =           
0011971
 Z    =        4322162
91                 I    =           51
99153
 XDOT =      -4945
043691                 Wp   =          140
26613
 YDOT =      -4648
257406  meter/sec      RA   =           67
38458  deg
 ZDOT =       3553
756605                 TA   =          273
59740
                                          MA   =          273
73430
                                          Ha   =            227
877  n
mi
                                          Hp   =            221
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5176693
99                 X    =        -1654605
63
 Y    =       16392454
48  feet           Y    =         4978346
58  meter
 Z    =       14180324
50                 Z    =         4314311
35
 XDOT =     -16223
896625                 XDOT =       -4909
960573
 YDOT =     -15250
188341  feet/sec       YDOT =       -4703
359980  meter/sec
 ZDOT =      11659
306446                 ZDOT =        3529
820406

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4816664
19                 X    =        -1468119
25
 Y    =       16532895
68  feet           Y    =         5039226
60  meter
 Z    =       14144095
38                 Z    =         4311120
27
 XDOT =     -15512
286880                 XDOT =       -4728
145041
 YDOT =     -14441
371149  feet/sec       YDOT =       -4401
729926  meter/sec
 ZDOT =      11550
479564                 ZDOT =        3520
586171


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   19299
96450342  
00016717  00000-0  10270-3 0  9145
2 25544  51
6397  67
8681 0006519 195
3375 164
7579 15
50249092 35692


Satellite: ISS
Catalog Number: 25544
Epoch time:      19299
96450342   =   yrday
fracday
Element set:     914
Inclination:       51
6397  deg
RA of node:        67
8681  deg
Eccentricity:     
0006519     
Arg of perigee:   195
3375  deg
Mean anomaly:     164
7579  deg
Mean motion:   15
50249092  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3569
Checksum:              361


Coasting Arc #16 (Orbit 3583)
---------------------------------------

Vector Time (GMT): 2019/300/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1525934
88                 A    =         6791961
45  meter
 Y    =       -4795312
19  meter          E    =           
0007771
 Z    =       -4566438
52                 I    =           51
97551
 XDOT =       5204
299672                 Wp   =          109
52595
 YDOT =       4649
661362  meter/sec      RA   =           62
45013  deg
 ZDOT =      -3150
504197                 TA   =          129
02087
                                          MA   =          128
95166
                                          Ha   =            227
820  n
mi
                                          Hp   =            221
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5006348
03                 X    =         1601625
87
 Y    =      -15732651
55  feet           Y    =        -4777825
12  meter
 Z    =      -14981753
67                 Z    =        -4558841
82
 XDOT =      17074
473990                 XDOT =        5167
222831
 YDOT =      15254
794496  feet/sec       YDOT =        4707
652052  meter/sec
 ZDOT =     -10336
299859                 ZDOT =       -3125
313253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4396392
46                 X    =         1340020
42
 Y    =      -15946815
48  feet           Y    =        -4860589
36  meter
 Z    =      -14946691
87                 Z    =        -4555751
68
 XDOT =      16647
998432                 XDOT =        5074
309922
 YDOT =      14149
183484  feet/sec       YDOT =        4312
671126  meter/sec
 ZDOT =     -10221
765205                 ZDOT =       -3115
594034


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   19300
93146297  
00016717  00000-0  10270-3 0  9157
2 25544  51
6406  63
0752 0006328 197
6919 162
4012 15
50220333 35848


Satellite: ISS
Catalog Number: 25544
Epoch time:      19300
93146297   =   yrday
fracday
Element set:     915
Inclination:       51
6406  deg
RA of node:        63
0752  deg
Eccentricity:     
0006328     
Arg of perigee:   197
6919  deg
Mean anomaly:     162
4012  deg
Mean motion:   15
50220333  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3584
Checksum:              299


Coasting Arc #17 (Orbit 3592)
---------------------------------------

Vector Time (GMT): 2019/301/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          66355
49                 A    =         6795062
70  meter
 Y    =        5744726
77  meter          E    =           
0012026
 Z    =        3626933
77                 I    =           51
97902
 XDOT =      -5611
796438                 Wp   =          126
55520
 YDOT =      -2744
679254  meter/sec      RA   =           59
76047  deg
 ZDOT =       4432
829934                 TA   =          276
10374
                                          MA   =          276
24076
                                          Ha   =            227
782  n
mi
                                          Hp   =            221
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         217701
73                 X    =          -15506
79
 Y    =       18847528
79  feet           Y    =         5745011
22  meter
 Z    =       11899389
02                 Z    =         3627057
07
 XDOT =     -18411
405636                 XDOT =       -5602
220402
 YDOT =      -9004
853196  feet/sec       YDOT =       -2807
380623  meter/sec
 ZDOT =      14543
405295                 ZDOT =        4405
592503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6377375
40                 X    =        -1943824
02
 Y    =      -17737084
52  feet           Y    =        -5406263
36  meter
 Z    =       11899458
39                 Z    =         3626954
92
 XDOT =      19153
879880                 XDOT =        5838
102587
 YDOT =       2824
653463  feet/sec       YDOT =         860
954376  meter/sec
 ZDOT =      14419
379993                 ZDOT =        4395
027022


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   19301
51163684  
00016717  00000-0  10270-3 0  9162
2 25544  51
6421  60
1965 0006809 199
6610 160
4279 15
50256513 35935


Satellite: ISS
Catalog Number: 25544
Epoch time:      19301
51163684   =   yrday
fracday
Element set:     916
Inclination:       51
6421  deg
RA of node:        60
1965  deg
Eccentricity:     
0006809     
Arg of perigee:   199
6610  deg
Mean anomaly:     160
4279  deg
Mean motion:   15
50256513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3593
Checksum:              311


Coasting Arc #18 (Orbit 3607)
---------------------------------------

Vector Time (GMT): 2019/302/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -134241
90                 A    =         6794154
81  meter
 Y    =       -5536418
87  meter          E    =           
0005730
 Z    =       -3935540
52                 I    =           51
95782
 XDOT =       5859
311406                 Wp   =          139
59997
 YDOT =       2759
562423  meter/sec      RA   =           54
82772  deg
 ZDOT =      -4089
514987                 TA   =           87
75152
                                          MA   =           87
68591
                                          Ha   =            227
729  n
mi
                                          Hp   =            221
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -440426
18                 X    =          -53204
85
 Y    =      -18164103
90  feet           Y    =        -5537466
98  meter
 Z    =      -12911878
35                 Z    =        -3935995
76
 XDOT =      19223
462619                 XDOT =        5847
882875
 YDOT =       9053
682489  feet/sec       YDOT =        2825
021444  meter/sec
 ZDOT =     -13417
043919                 ZDOT =       -4061
079594

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6646377
12                 X    =         2025815
75
 Y    =       16908973
18  feet           Y    =         5153855
03  meter
 Z    =      -12913463
73                 Z    =        -3936023
75
 XDOT =     -20023
089990                 XDOT =       -6103
037829
 YDOT =      -2258
374704  feet/sec       YDOT =        -688
352610  meter/sec
 ZDOT =     -13287
565706                 ZDOT =       -4050
050027


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   19302
47859469  
00016717  00000-0  10270-3 0  9172
2 25544  51
6420  55
4054 0006782 203
0519 157
0329 15
50227096 36087


Satellite: ISS
Catalog Number: 25544
Epoch time:      19302
47859469   =   yrday
fracday
Element set:     917
Inclination:       51
6420  deg
RA of node:        55
4054  deg
Eccentricity:     
0006782     
Arg of perigee:   203
0519  deg
Mean anomaly:     157
0329  deg
Mean motion:   15
50227096  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3608
Checksum:              313
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