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

 
Date: May 14th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14319 0147 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 995 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


134/18:07:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 217 1

136/05:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 217 1

137/07:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 217 1

143/14:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 5
000/00:00:00 000 0 0 0 0 216 7

143/16:02:53 424 -2 1 7 1 7 1
N/A 6 7 -0 7 223 7
000/00:19:46 849 -1 2 -0 1 221 4

143/19:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 9
000/00:00:00 000 0 0 0 0 221 4

143/21:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 6
000/00:00:00 000 0 0 0 0 221 4

144/08:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 7
000/00:00:00 000 0 0 0 0 221 2

Coasting Arc #1 (Orbit 985)
---------------------------------------

Vector Time (GMT): 2019/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2012994
91                 A    =         6782275
85  meter
 Y    =        3878313
31  meter          E    =           
0013645
 Z    =       -5199160
93                 I    =           51
66795
 XDOT =      -7268
515399                 Wp   =           74
59883
 YDOT =       2016
030715  meter/sec      RA   =          172
38847  deg
 ZDOT =      -1309
675565                 TA   =          182
80092
                                          MA   =          182
80857
                                          Ha   =            223
179  n
mi
                                          Hp   =            217
230

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6604314
00                 X    =         1994731
62
 Y    =       12724125
03  feet           Y    =         3900722
08  meter
 Z    =      -17057614
60                 Z    =        -5189426
75
 XDOT =     -23846
835298                 XDOT =       -7284
157318
 YDOT =       6614
273999  feet/sec       YDOT =        1934
661670  meter/sec
 ZDOT =      -4296
835843                 ZDOT =       -1345
021347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14068654
21                 X    =         4288125
80
 Y    =        3014282
97  feet           Y    =          918753
45  meter
 Z    =      -17013806
28                 Z    =        -5185808
15
 XDOT =      -9995
686376                 XDOT =       -3046
685208
 YDOT =      21483
231680  feet/sec       YDOT =        6548
089016  meter/sec
 ZDOT =      -4457
082998                 ZDOT =       -1358
518898


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   19133
51845042  
00016717  00000-0  10270-3 0  9003
2 25544  51
6399 173
4760 0001351 336
0126  24
0963 15
52650651  9867


Satellite: ISS
Catalog Number: 25544
Epoch time:      19133
51845042   =   yrday
fracday
Element set:     900
Inclination:       51
6399  deg
RA of node:       173
4760  deg
Eccentricity:     
0001351     
Arg of perigee:   336
0126  deg
Mean anomaly:      24
0963  deg
Mean motion:   15
52650651  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             986
Checksum:              294


Coasting Arc #2 (Orbit 1001)
---------------------------------------

Vector Time (GMT): 2019/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -833886
40                 A    =         6781581
91  meter
 Y    =       -4119308
25  meter          E    =           
0002533
 Z    =        5320415
67                 I    =           51
69862
 XDOT =       7495
897612                 Wp   =           55
19832
 YDOT =      -1614
696706  meter/sec      RA   =          167
40764  deg
 ZDOT =        -73
877381                 TA   =           35
51353
                                          MA   =           35
49667
                                          Ha   =            223
255  n
mi
                                          Hp   =            217
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2735847
77                 X    =         -813604
96
 Y    =      -13514790
86  feet           Y    =        -4128520
08  meter
 Z    =       17455431
99                 Z    =         5316414
10
 XDOT =      24592
839936                 XDOT =        7513
755359
 YDOT =      -5297
561373  feet/sec       YDOT =       -1530
772479  meter/sec
 ZDOT =       -242
379860                 ZDOT =         -37
421510

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12303494
60                 X    =        -3750105
15
 Y    =       -6275386
57  feet           Y    =        -1912737
83  meter
 Z    =       17437605
49                 Z    =         5314982
15
 XDOT =      10881
061997                 XDOT =        3316
547697
 YDOT =     -21560
759866  feet/sec       YDOT =       -6571
719607  meter/sec
 ZDOT =        -77
114530                 ZDOT =         -23
504509


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   19134
54825311  
00016717  00000-0  10270-3 0  9015
2 25544  51
6396 168
3538 0001456 346
6126  13
4987 15
52674915 10020


Satellite: ISS
Catalog Number: 25544
Epoch time:      19134
54825311   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:       168
3538  deg
Eccentricity:     
0001456     
Arg of perigee:   346
6126  deg
Mean anomaly:      13
4987  deg
Mean motion:   15
52674915  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1002
Checksum:              309


Coasting Arc #3 (Orbit 1005)
---------------------------------------

Vector Time (GMT): 2019/134/18:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2337251
20                 A    =         6782050
52  meter
 Y    =       -3658732
29  meter          E    =           
0002949
 Z    =        5207983
21                 I    =           51
70813
 XDOT =       7053
077470                 Wp   =          105
66773
 YDOT =      -2743
992670  meter/sec      RA   =          166
15136  deg
 ZDOT =       1236
216467                 TA   =          332
47162
                                          MA   =          332
48724
                                          Ha   =            223
184  n
mi
                                          Hp   =            217
119

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7668147
00                 X    =        -2321462
22
 Y    =      -12003714
86  feet           Y    =        -3684780
91  meter
 Z    =       17086559
10                 Z    =         5196667
89
 XDOT =      23140
017946                 XDOT =        7077
232474
 YDOT =      -9002
600624  feet/sec       YDOT =       -2664
985187  meter/sec
 ZDOT =       4055
828303                 ZDOT =        1270
536575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -962535
90                 X    =         -293380
94
 Y    =       14272461
64  feet           Y    =         4350246
31  meter
 Z    =       17035566
15                 Z    =         5192440
56
 XDOT =     -22856
513812                 XDOT =       -6966
665410
 YDOT =      -6573
628150  feet/sec       YDOT =       -2003
641860  meter/sec
 ZDOT =       4211
505609                 ZDOT =        1283
666910


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   19134
80570321  
00016717  00000-0  10270-3 0  9023
2 25544  51
6391 167
0741 0001729 339
0435  21
0646 15
52701450 10065


Satellite: ISS
Catalog Number: 25544
Epoch time:      19134
80570321   =   yrday
fracday
Element set:     902
Inclination:       51
6391  deg
RA of node:       167
0741  deg
Eccentricity:     
0001729     
Arg of perigee:   339
0435  deg
Mean anomaly:      21
0646  deg
Mean motion:   15
52701450  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1006
Checksum:              272


Coasting Arc #4 (Orbit 1020)
---------------------------------------

Vector Time (GMT): 2019/135/18:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1197071
29                 A    =         6781631
16  meter
 Y    =        4033888
84  meter          E    =           
0014571
 Z    =       -5330894
47                 I    =           51
73784
 XDOT =      -7281
916531                 Wp   =           84
53650
 YDOT =       2357
492257  meter/sec      RA   =          161
17262  deg
 ZDOT =        150
441320                 TA   =          186
88761
                                          MA   =          186
90766
                                          Ha   =            223
279  n
mi
                                          Hp   =            217
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3927399
23                 X    =         1177769
08
 Y    =       13234543
44  feet           Y    =         4047167
55  meter
 Z    =      -17489811
27                 Z    =        -5325126
25
 XDOT =     -23890
802266                 XDOT =       -7308
468243
 YDOT =       7734
554650  feet/sec       YDOT =        2275
912302  meter/sec
 ZDOT =        493
573886                 ZDOT =         115
003613

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4467906
86                 X    =         1361818
01
 Y    =      -13096506
16  feet           Y    =        -3991815
08  meter
 Z    =      -17463975
43                 Z    =        -5323019
71
 XDOT =      22944
265291                 XDOT =        6993
412061
 YDOT =       7391
132934  feet/sec       YDOT =        2252
817318  meter/sec
 ZDOT =        332
842620                 ZDOT =         101
450431


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   19135
77114380  
00016717  00000-0  10270-3 0  9030
2 25544  51
6384 162
2716 0001746 348
0930  12
0181 15
52663326 10215


Satellite: ISS
Catalog Number: 25544
Epoch time:      19135
77114380   =   yrday
fracday
Element set:     903
Inclination:       51
6384  deg
RA of node:       162
2716  deg
Eccentricity:     
0001746     
Arg of perigee:   348
0930  deg
Mean anomaly:      12
0181  deg
Mean motion:   15
52663326  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1021
Checksum:              279


Coasting Arc #5 (Orbit 1028)
---------------------------------------

Vector Time (GMT): 2019/136/05:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3828641
48                 A    =         6788513
49  meter
 Y    =       -4409970
77  meter          E    =           
0012031
 Z    =        3451738
83                 I    =           51
77693
 XDOT =       5944
270588                 Wp   =           84
25903
 YDOT =       1559
545813  meter/sec      RA   =          158
70587  deg
 ZDOT =      -4585
939370                 TA   =           55
37469
                                          MA   =           55
26130
                                          Ha   =            223
201  n
mi
                                          Hp   =            217
075

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12561159
72                 X    =         3860903
60
 Y    =      -14468408
04  feet           Y    =        -4366975
95  meter
 Z    =       11324602
45                 Z    =         3470415
42
 XDOT =      19502
200091                 XDOT =        5948
665790
 YDOT =       5116
620123  feet/sec       YDOT =        1626
043542  meter/sec
 ZDOT =     -15045
732841                 ZDOT =       -4557
053170

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18775455
69                 X    =         5722758
89
 Y    =       -3559289
63  feet           Y    =        -1084871
48  meter
 Z    =       11409553
30                 Z    =         3477631
85
 XDOT =      11904
745331                 XDOT =        3628
566377
 YDOT =      14831
594569  feet/sec       YDOT =        4520
670024  meter/sec
 ZDOT =     -14914
967642                 ZDOT =       -4546
082137


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   19136
28604476  
00016717  00000-0  10270-3 0  9048
2 25544  51
6390 159
7072 0001095 343
9473  16
1644 15
52649164 10292


Satellite: ISS
Catalog Number: 25544
Epoch time:      19136
28604476   =   yrday
fracday
Element set:     904
Inclination:       51
6390  deg
RA of node:       159
7072  deg
Eccentricity:     
0001095     
Arg of perigee:   343
9473  deg
Mean anomaly:      16
1644  deg
Mean motion:   15
52649164  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1029
Checksum:              314


Coasting Arc #6 (Orbit 1043)
---------------------------------------

Vector Time (GMT): 2019/137/05:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4564436
20                 A    =         6791046
16  meter
 Y    =        4392728
33  meter          E    =           
0006124
 Z    =       -2442096
26                 I    =           51
81702
 XDOT =      -5005
419235                 Wp   =           37
27570
 YDOT =      -2229
184429  meter/sec      RA   =          153
74664  deg
 ZDOT =       5357
473701                 TA   =          295
49129
                                          MA   =          295
55462
                                          Ha   =            223
223  n
mi
                                          Hp   =            217
083

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14975184
38                 X    =        -4601355
14
 Y    =       14411838
34  feet           Y    =         4341479
31  meter
 Z    =       -8012126
85                 Z    =        -2464358
42
 XDOT =     -16421
979117                 XDOT =       -5006
143941
 YDOT =      -7313
597207  feet/sec       YDOT =       -2285
162867  meter/sec
 ZDOT =      17577
013456                 ZDOT =        5333
156937

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20610239
48                 X    =        -6282000
99
 Y    =        2354387
14  feet           Y    =          717617
20  meter
 Z    =       -8113340
76                 Z    =        -2472946
26
 XDOT =      -8501
947185                 XDOT =       -2591
393502
 YDOT =     -14365
088838  feet/sec       YDOT =       -4378
479078  meter/sec
 ZDOT =      17466
992731                 ZDOT =        5323
939385


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   19137
25148092  
00016717  00000-0  10270-3 0  9054
2 25544  51
6400 154
9052 0001386 344
5670  15
5440 15
52647361 10449


Satellite: ISS
Catalog Number: 25544
Epoch time:      19137
25148092   =   yrday
fracday
Element set:     905
Inclination:       51
6400  deg
RA of node:       154
9052  deg
Eccentricity:     
0001386     
Arg of perigee:   344
5670  deg
Mean anomaly:      15
5440  deg
Mean motion:   15
52647361  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1044
Checksum:              287


Coasting Arc #7 (Orbit 1045)
---------------------------------------

Vector Time (GMT): 2019/137/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5850885
00                 A    =         6788654
49  meter
 Y    =         -88945
80  meter          E    =           
0012150
 Z    =        3429927
83                 I    =           51
81120
 XDOT =       2793
695291                 Wp   =           83
99189
 YDOT =      -5454
285705  meter/sec      RA   =          153
41453  deg
 ZDOT =       4611
359642                 TA   =          316
05286
                                          MA   =          316
14942
                                          Ha   =            223
298  n
mi
                                          Hp   =            217
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19195816
93                 X    =        -5866116
51
 Y    =        -291816
92  feet           Y    =         -154459
84  meter
 Z    =       11253044
05                 Z    =         3401468
91
 XDOT =       9165
666966                 XDOT =        2832
079208
 YDOT =     -17894
638141  feet/sec       YDOT =       -5422
830281  meter/sec
 ZDOT =      15129
132684                 ZDOT =        4625
023544

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18933087
51                 X    =        -5770805
07
 Y    =       -3603938
61  feet           Y    =        -1098480
49  meter
 Z    =       11124089
56                 Z    =         3390622
50
 XDOT =      11746
055192                 XDOT =        3580
197622
 YDOT =     -14685
642085  feet/sec       YDOT =       -4476
183708  meter/sec
 ZDOT =      15191
465968                 ZDOT =        4630
358827


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   19137
38020437  
00016717  00000-0  10270-3 0  9061
2 25544  51
6398 154
2659 0001340 343
7622  16
3487 15
52687214 10462


Satellite: ISS
Catalog Number: 25544
Epoch time:      19137
38020437   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       154
2659  deg
Eccentricity:     
0001340     
Arg of perigee:   343
7622  deg
Mean anomaly:      16
3487  deg
Mean motion:   15
52687214  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1046
Checksum:              307


Coasting Arc #8 (Orbit 1060)
---------------------------------------

Vector Time (GMT): 2019/138/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5209876
50                 A    =         6785937
83  meter
 Y    =         758923
00  meter          E    =           
0008539
 Z    =       -4290478
02                 I    =           51
83037
 XDOT =      -3769
279655                 Wp   =           60
81250
 YDOT =       5620
131307  meter/sec      RA   =          148
45252  deg
 ZDOT =      -3584
196374                 TA   =          172
65630
                                          MA   =          172
64379
                                          Ha   =            223
287  n
mi
                                          Hp   =            217
171

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17092770
68                 X    =         5221843
95
 Y    =        2489904
85  feet           Y    =          817250
74  meter
 Z    =      -14076371
47                 Z    =        -4265140
79
 XDOT =     -12366
403069                 XDOT =       -3814
435061
 YDOT =      18438
751007  feet/sec       YDOT =        5577
728386  meter/sec
 ZDOT =     -11759
174456                 ZDOT =       -3602
615702

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16592417
61                 X    =         5057368
89
 Y    =        5125626
32  feet           Y    =         1562290
90  meter
 Z    =      -13961600
97                 Z    =        -4255495
98
 XDOT =     -14625
636943                 XDOT =       -4457
894140
 YDOT =      15098
119274  feet/sec       YDOT =        4601
906755  meter/sec
 ZDOT =     -11843
090943                 ZDOT =       -3609
774120


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   19138
34563986  
00016717  00000-0  10270-3 0  9070
2 25544  51
6390 149
4639 0001430 349
9318  10
1805 15
52664157 10612


Satellite: ISS
Catalog Number: 25544
Epoch time:      19138
34563986   =   yrday
fracday
Element set:     907
Inclination:       51
6390  deg
RA of node:       149
4639  deg
Eccentricity:     
0001430     
Arg of perigee:   349
9318  deg
Mean anomaly:      10
1805  deg
Mean motion:   15
52664157  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1061
Checksum:              316


Coasting Arc #9 (Orbit 1076)
---------------------------------------

Vector Time (GMT): 2019/139/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4442853
90                 A    =         6783456
76  meter
 Y    =       -1497959
87  meter          E    =           
0006162
 Z    =        4898073
76                 I    =           51
85017
 XDOT =       4550
220216                 Wp   =          109
95220
 YDOT =      -5695
604199  meter/sec      RA   =          143
48700  deg
 ZDOT =       2380
985299                 TA   =          316
77020
                                          MA   =          316
81855
                                          Ha   =            223
414  n
mi
                                          Hp   =            216
971

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14576292
31                 X    =        -4449565
62
 Y    =       -4914566
49  feet           Y    =        -1547681
01  meter
 Z    =       16069795
79                 Z    =         4876475
20
 XDOT =      14928
544015                 XDOT =        4602
006195
 YDOT =     -18686
365483  feet/sec       YDOT =       -5644
431145  meter/sec
 ZDOT =       7811
631557                 ZDOT =        2403
214144

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13864133
52                 X    =        -4225787
90
 Y    =       -6894931
48  feet           Y    =        -2101575
12  meter
 Z    =       15972016
77                 Z    =         4868270
71
 XDOT =      16811
854005                 XDOT =        5124
253101
 YDOT =     -15440
558125  feet/sec       YDOT =       -4706
282116  meter/sec
 ZDOT =       7912
844596                 ZDOT =        2411
835033


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   19139
37543495  
00016717  00000-0  10270-3 0  9088
2 25544  51
6389 144
3414 0001475 353
8719   6
2415 15
52693442 10772


Satellite: ISS
Catalog Number: 25544
Epoch time:      19139
37543495   =   yrday
fracday
Element set:     908
Inclination:       51
6389  deg
RA of node:       144
3414  deg
Eccentricity:     
0001475     
Arg of perigee:   353
8719  deg
Mean anomaly:       6
2415  deg
Mean motion:   15
52693442  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1077
Checksum:              324


Coasting Arc #10 (Orbit 1091)
---------------------------------------

Vector Time (GMT): 2019/140/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3613472
10                 A    =         6782033
68  meter
 Y    =        2318908
71  meter          E    =           
0014470
 Z    =       -5262544
03                 I    =           51
87063
 XDOT =      -5109
816449                 Wp   =           76
23645
 YDOT =       5605
020709  meter/sec      RA   =          138
51956  deg
 ZDOT =      -1037
827003                 TA   =          183
83381
                                          MA   =          183
84491
                                          Ha   =            223
362  n
mi
                                          Hp   =            217
110

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11855223
43                 X    =         3612835
73
 Y    =        7607968
20  feet           Y    =         2359314
18  meter
 Z    =      -17265564
40                 Z    =        -5244992
13
 XDOT =     -16764
489662                 XDOT =       -5167
072354
 YDOT =      18389
175556  feet/sec       YDOT =        5547
559157  meter/sec
 ZDOT =      -3404
944237                 ZDOT =       -1062
787311

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10961523
33                 X    =         3341072
31
 Y    =        9000400
04  feet           Y    =         2743321
93  meter
 Z    =      -17186186
95                 Z    =        -5238349
78
 XDOT =     -18188
546478                 XDOT =       -5543
868967
 YDOT =      15427
019127  feet/sec       YDOT =        4702
155430  meter/sec
 ZDOT =      -3518
558793                 ZDOT =       -1072
456720


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   19140
34086883  
00016717  00000-0  10270-3 0  9091
2 25544  51
6383 139
5394 0001489 356
8679   3
2463 15
52655075 10929


Satellite: ISS
Catalog Number: 25544
Epoch time:      19140
34086883   =   yrday
fracday
Element set:     909
Inclination:       51
6383  deg
RA of node:       139
5394  deg
Eccentricity:     
0001489     
Arg of perigee:   356
8679  deg
Mean anomaly:       3
2463  deg
Mean motion:   15
52655075  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1092
Checksum:              334


Coasting Arc #11 (Orbit 1107)
---------------------------------------

Vector Time (GMT): 2019/141/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2747265
69                 A    =         6781532
51  meter
 Y    =       -3171715
88  meter          E    =           
0003384
 Z    =        5325402
98                 I    =           51
89480
 XDOT =       5478
723952                 Wp   =           48
44085
 YDOT =      -5353
474485  meter/sec      RA   =          133
55175  deg
 ZDOT =       -359
738704                 TA   =           44
99068
                                          MA   =           44
96327
                                          Ha   =            223
440  n
mi
                                          Hp   =            216
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9013338
88                 X    =        -2737462
60
 Y    =      -10405892
01  feet           Y    =        -3202383
65  meter
 Z    =       17471794
54                 Z    =         5312081
02
 XDOT =      17974
816116                 XDOT =        5539
928268
 YDOT =     -17563
892666  feet/sec       YDOT =       -5291
865295  meter/sec
 ZDOT =      -1180
245093                 ZDOT =        -332
976904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7998708
15                 X    =        -2438006
24
 Y    =      -11297841
18  feet           Y    =        -3443581
99  meter
 Z    =       17411660
55                 Z    =         5307074
14
 XDOT =      18887
634733                 XDOT =        5756
951067
 YDOT =     -15015
260035  feet/sec       YDOT =       -4576
651259  meter/sec
 ZDOT =      -1058
456408                 ZDOT =        -322
617513


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   19141
37066023  
00016717  00000-0  10270-3 0  9101
2 25544  51
6394 134
4169 0001613   1
6522 358
4635 15
52703665 11089


Satellite: ISS
Catalog Number: 25544
Epoch time:      19141
37066023   =   yrday
fracday
Element set:     910
Inclination:       51
6394  deg
RA of node:       134
4169  deg
Eccentricity:     
0001613     
Arg of perigee:     1
6522  deg
Mean anomaly:     358
4635  deg
Mean motion:   15
52703665  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1108
Checksum:              284


Coasting Arc #12 (Orbit 1122)
---------------------------------------

Vector Time (GMT): 2019/142/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1918881
81                 A    =         6782561
41  meter
 Y    =        4027815
22  meter          E    =           
0013408
 Z    =       -5120430
32                 I    =           51
91996
 XDOT =      -5634
798519                 Wp   =           95
47207
 YDOT =       4884
553637  meter/sec      RA   =          128
58628  deg
 ZDOT =       1733
283884                 TA   =          191
22817
                                          MA   =          191
25811
                                          Ha   =            223
517  n
mi
                                          Hp   =            216
882

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6295543
98                 X    =         1898571
38
 Y    =       13214616
87  feet           Y    =         4049160
65  meter
 Z    =      -16799312
08                 Z    =        -5111157
83
 XDOT =     -18486
871782                 XDOT =       -5697
419585
 YDOT =      16025
438441  feet/sec       YDOT =        4821
191001  meter/sec
 ZDOT =       5686
626916                 ZDOT =        1705
760538

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5235899
23                 X    =         1595902
09
 Y    =       13720228
26  feet           Y    =         4181925
57  meter
 Z    =      -16757611
86                 Z    =        -5107720
09
 XDOT =     -18846
350035                 XDOT =       -5744
367491
 YDOT =      13974
041999  feet/sec       YDOT =        4259
288001  meter/sec
 ZDOT =       5561
398752                 ZDOT =        1695
114340


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   19142
33609066  
00016717  00000-0  10270-3 0  9119
2 25544  51
6393 129
6148 0001775  10
2120 349
9068 15
52668462 11237


Satellite: ISS
Catalog Number: 25544
Epoch time:      19142
33609066   =   yrday
fracday
Element set:     911
Inclination:       51
6393  deg
RA of node:       129
6148  deg
Eccentricity:     
0001775     
Arg of perigee:    10
2120  deg
Mean anomaly:     349
9068  deg
Mean motion:   15
52668462  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1123
Checksum:              300


Coasting Arc #13 (Orbit 1138)
---------------------------------------

Vector Time (GMT): 2019/143/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1122831
03                 A    =         6784448
31  meter
 Y    =       -4838362
83  meter          E    =           
0009530
 Z    =        4617129
52                 I    =           51
94637
 XDOT =       5647
928810                 Wp   =           57
49990
 YDOT =      -4210
508183  meter/sec      RA   =          123
62561  deg
 ZDOT =      -3029
218679                 TA   =           62
65884
                                          MA   =           62
56187
                                          Ha   =            223
484  n
mi
                                          Hp   =            216
750

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3683828
85                 X    =        -1091071
15
 Y    =      -15873893
81  feet           Y    =        -4850742
14  meter
 Z    =       15148062
74                 Z    =         4611751
72
 XDOT =      18529
950165                 XDOT =        5709
306455
 YDOT =     -13814
003226  feet/sec       YDOT =       -4147
005510  meter/sec
 ZDOT =      -9938
381492                 ZDOT =       -3001
634540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2669353
10                 X    =         -813618
83
 Y    =      -16098171
15  feet           Y    =        -4906722
57  meter
 Z    =       15124098
12                 Z    =         4609825
11
 XDOT =      18340
317796                 XDOT =        5590
128864
 YDOT =     -12289
710818  feet/sec       YDOT =       -3745
903857  meter/sec
 ZDOT =      -9812
912738                 ZDOT =       -2990
975803


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   19143
36588003  
00016717  00000-0  10270-3 0  9121
2 25544  51
6390 124
4930 0001710  11
9786 348
1407 15
52710971 11399


Satellite: ISS
Catalog Number: 25544
Epoch time:      19143
36588003   =   yrday
fracday
Element set:     912
Inclination:       51
6390  deg
RA of node:       124
4930  deg
Eccentricity:     
0001710     
Arg of perigee:    11
9786  deg
Mean anomaly:     348
1407  deg
Mean motion:   15
52710971  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1139
Checksum:              294


Coasting Arc #14 (Orbit 1142)
---------------------------------------

Vector Time (GMT): 2019/143/14:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965984
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         225056
25                 A    =         6787826
74  meter
 Y    =       -5707744
35  meter          E    =           
0012563
 Z    =        3658854
39                 I    =           51
96178
 XDOT =       5718
038458                 Wp   =           77
01040
 YDOT =      -2602
619773  meter/sec      RA   =          122
33277  deg
 ZDOT =      -4396
333734                 TA   =           59
76720
                                          MA   =           59
64288
                                          Ha   =            223
537  n
mi
                                          Hp   =            216
737

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         738373
53                 X    =          271092
42
 Y    =      -18726195
38  feet           Y    =        -5704970
68  meter
 Z    =       12004115
44                 Z    =         3660058
71
 XDOT =      18759
968693                 XDOT =        5768
071717
 YDOT =      -8538
778782  feet/sec       YDOT =       -2538
396349  meter/sec
 ZDOT =     -14423
667107                 ZDOT =       -4368
436383

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18725467
71                 X    =        -5707522
56
 Y    =        -655129
35  feet           Y    =         -199683
43  meter
 Z    =       12010080
81                 Z    =         3660672
63
 XDOT =      -8590
252194                 XDOT =       -2618
308869
 YDOT =     -17489
586594  feet/sec       YDOT =       -5330
825994  meter/sec
 ZDOT =     -14296
914003                 ZDOT =       -4357
699388


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   19143
62332885  
00016717  00000-0  10270-3 0  9136
2 25544  51
6384 123
2126 0001999  12
4378 347
6823 15
52694857 11433


Satellite: ISS
Catalog Number: 25544
Epoch time:      19143
62332885   =   yrday
fracday
Element set:     913
Inclination:       51
6384  deg
RA of node:       123
2126  deg
Eccentricity:     
0001999     
Arg of perigee:    12
4378  deg
Mean anomaly:     347
6823  deg
Mean motion:   15
52694857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1143
Checksum:              323


Coasting Arc #15 (Orbit 1143)
---------------------------------------

Vector Time (GMT): 2019/143/16:12:46
849
Vector Time (MET): N/A
Weight (LBS)     : 965081
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1920813
31                 A    =         6787698
91  meter
 Y    =        4241197
65  meter          E    =           
0007090
 Z    =       -4945773
37                 I    =           51
94921
 XDOT =      -5266
040679                 Wp   =          117
46316
 YDOT =       5063
350388  meter/sec      RA   =          121
88227  deg
 ZDOT =       2296
167151                 TA   =          174
92230
                                          MA   =          174
91510
                                          Ha   =            223
706  n
mi
                                          Hp   =            221
381

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6301880
93                 X    =         1897268
14
 Y    =       13914690
46  feet           Y    =         4262546
51  meter
 Z    =      -16226290
59                 Z    =        -4936499
41
 XDOT =     -17277
036347                 XDOT =       -5333
422653
 YDOT =      16612
041956  feet/sec       YDOT =        5004
084788  meter/sec
 ZDOT =       7533
356796                 ZDOT =        2270
423620

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8110795
94                 X    =         2472170
60
 Y    =      -12996091
36  feet           Y    =        -3961208
65  meter
 Z    =      -16184604
38                 Z    =        -4933067
42
 XDOT =      22449
691757                 XDOT =        6842
666047
 YDOT =       4772
373873  feet/sec       YDOT =        1454
619556  meter/sec
 ZDOT =       7416
153022                 ZDOT =        2260
443441


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   19143
68769762  
00016717  00000-0  10270-3 0  9141
2 25544  51
6396 122
8911 0005395 272
3194  87
7339 15
51161361 11443


Satellite: ISS
Catalog Number: 25544
Epoch time:      19143
68769762   =   yrday
fracday
Element set:     914
Inclination:       51
6396  deg
RA of node:       122
8911  deg
Eccentricity:     
0005395     
Arg of perigee:   272
3194  deg
Mean anomaly:      87
7339  deg
Mean motion:   15
51161361  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1144
Checksum:              328


Coasting Arc #16 (Orbit 1146)
---------------------------------------

Vector Time (GMT): 2019/143/19:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965081
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4943880
28                 A    =         6790005
77  meter
 Y    =        1528164
08  meter          E    =           
0004477
 Z    =        4394775
48                 I    =           51
95937
 XDOT =        962
050118                 Wp   =          127
10903
 YDOT =      -6781
804553  meter/sec      RA   =          121
17913  deg
 ZDOT =       3435
407179                 TA   =          288
16964
                                          MA   =          288
21838
                                          Ha   =            223
869  n
mi
                                          Hp   =            221
414

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16220079
66                 X    =        -4981948
63
 Y    =        5013661
69  feet           Y    =         1472664
75  meter
 Z    =       14418554
72                 Z    =         4370667
64
 XDOT =       3156
332407                 XDOT =        1021
127357
 YDOT =     -22250
014937  feet/sec       YDOT =       -6770
716343  meter/sec
 ZDOT =      11271
020930                 ZDOT =        3440
223109

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16500897
35                 X    =         5029473
51
 Y    =       -4369569
48  feet           Y    =        -1331844
78  meter
 Z    =       14309079
54                 Z    =         4361407
44
 XDOT =      -4271
251354                 XDOT =       -1301
877413
 YDOT =      20907
728340  feet/sec       YDOT =        6372
675598  meter/sec
 ZDOT =      11293
463889                 ZDOT =        3442
247794


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   19143
88097289  
00016717  00000-0  10270-3 0  9152
2 25544  51
6398 121
9325 0005496 274
1227  85
9295 15
51135745 11474


Satellite: ISS
Catalog Number: 25544
Epoch time:      19143
88097289   =   yrday
fracday
Element set:     915
Inclination:       51
6398  deg
RA of node:       121
9325  deg
Eccentricity:     
0005496     
Arg of perigee:   274
1227  deg
Mean anomaly:      85
9295  deg
Mean motion:   15
51135745  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1147
Checksum:              340


Coasting Arc #17 (Orbit 1146)
---------------------------------------

Vector Time (GMT): 2019/143/21:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965081
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2538063
99                 A    =         6797285
30  meter
 Y    =        6171889
92  meter          E    =           
0007284
 Z    =       -1266257
79                 I    =           51
98310
 XDOT =      -4865
787571                 Wp   =          358
83614
 YDOT =       -798
774704  meter/sec      RA   =          120
88449  deg
 ZDOT =       5866
061579                 TA   =          347
47634
                                          MA   =          347
49443
                                          Ha   =            223
607  n
mi
                                          Hp   =            221
424

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8326981
60                 X    =        -2600740
40
 Y    =       20248982
68  feet           Y    =         6143157
22  meter
 Z    =       -4154389
07                 Z    =        -1278738
24
 XDOT =     -15963
869984                 XDOT =       -4884
987929
 YDOT =      -2620
651917  feet/sec       YDOT =        -853
295432  meter/sec
 ZDOT =      19245
608855                 ZDOT =        5842
378626

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2187551
84                 X    =          666765
80
 Y    =      -21773755
08  feet           Y    =        -6636640
55  meter
 Z    =       -4211540
98                 Z    =        -1283677
69
 XDOT =      14584
309597                 XDOT =        4445
297565
 YDOT =      -2232
468755  feet/sec       YDOT =        -680
456476  meter/sec
 ZDOT =      19138
266094                 ZDOT =        5833
343506


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   19143
88097144  
00016717  00000-0  10270-3 0  9163
2 25544  51
6380 121
9308 0005655 272
3684  87
6820 15
51156048 11472


Satellite: ISS
Catalog Number: 25544
Epoch time:      19143
88097144   =   yrday
fracday
Element set:     916
Inclination:       51
6380  deg
RA of node:       121
9308  deg
Eccentricity:     
0005655     
Arg of perigee:   272
3684  deg
Mean anomaly:      87
6820  deg
Mean motion:   15
51156048  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1147
Checksum:              319


Coasting Arc #18 (Orbit 1154)
---------------------------------------

Vector Time (GMT): 2019/144/08:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965081
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         452051
13                 A    =         6793696
00  meter
 Y    =       -5997028
43  meter          E    =           
0007655
 Z    =        3152602
79                 I    =           51
98062
 XDOT =       5506
891358                 Wp   =           95
23773
 YDOT =      -2152
910192  meter/sec      RA   =          118
50560  deg
 ZDOT =      -4875
517495                 TA   =           48
65211
                                          MA   =           48
58628
                                          Ha   =            223
739  n
mi
                                          Hp   =            221
217

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1483107
39                 X    =          503764
41
 Y    =      -19675290
14  feet           Y    =        -5991684
51  meter
 Z    =       10343185
02                 Z    =         3154923
58
 XDOT =      18067
228865                 XDOT =        5554
239109
 YDOT =      -7063
353649  feet/sec       YDOT =       -2091
062964  meter/sec
 ZDOT =     -15995
792305                 ZDOT =       -4848
652304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1860289
24                 X    =         -567016
16
 Y    =      -19637388
01  feet           Y    =        -5985475
86  meter
 Z    =       10354247
53                 Z    =         3155974
65
 XDOT =      15323
201337                 XDOT =        4670
511768
 YDOT =      -9837
765956  feet/sec       YDOT =       -2998
551063  meter/sec
 ZDOT =     -15873
747116                 ZDOT =       -4838
318121


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   19144
39637371  
00016717  00000-0  10270-3 0  9173
2 25544  51
6391 119
3736 0005229 273
7398  86
3155 15
51183557 11555


Satellite: ISS
Catalog Number: 25544
Epoch time:      19144
39637371   =   yrday
fracday
Element set:     917
Inclination:       51
6391  deg
RA of node:       119
3736  deg
Eccentricity:     
0005229     
Arg of perigee:   273
7398  deg
Mean anomaly:      86
3155  deg
Mean motion:   15
51183557  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1155
Checksum:              332


Coasting Arc #19 (Orbit 1169)
---------------------------------------

Vector Time (GMT): 2019/145/08:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965081
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -571212
69                 A    =         6795123
93  meter
 Y    =        6273392
56  meter          E    =           
0004091
 Z    =       -2540708
46                 I    =           52
00192
 XDOT =      -5259
575366                 Wp   =          344
88898
 YDOT =       1672
737182  meter/sec      RA   =          113
56908  deg
 ZDOT =       5314
636839                 TA   =          346
77350
                                          MA   =          346
78422
                                          Ha   =            223
799  n
mi
                                          Hp   =            221
176

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1874057
37                 X    =         -628979
74
 Y    =       20581996
59  feet           Y    =         6266682
13  meter
 Z    =       -8335657
67                 Z    =        -2543622
85
 XDOT =     -17255
824690                 XDOT =       -5303
705050
 YDOT =       5487
982879  feet/sec       YDOT =        1613
673627  meter/sec
 ZDOT =      17436
472569                 ZDOT =        5288
980772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1965547
25                 X    =          599098
80
 Y    =       20567868
20  feet           Y    =         6269086
23  meter
 Z    =       -8349448
20                 Z    =        -2544911
81
 XDOT =     -14580
302907                 XDOT =       -4444
076326
 YDOT =       8421
767762  feet/sec       YDOT =        2566
954814  meter/sec
 ZDOT =      17319
941090                 ZDOT =        5279
118044


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   19145
36275078  
00016717  00000-0  10270-3 0  9184
2 25544  51
6406 114
5777 0005152 277
1533  82
9033 15
51197639 11708


Satellite: ISS
Catalog Number: 25544
Epoch time:      19145
36275078   =   yrday
fracday
Element set:     918
Inclination:       51
6406  deg
RA of node:       114
5777  deg
Eccentricity:     
0005152     
Arg of perigee:   277
1533  deg
Mean anomaly:      82
9033  deg
Mean motion:   15
51197639  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1170
Checksum:              316


Coasting Arc #20 (Orbit 1185)
---------------------------------------

Vector Time (GMT): 2019/146/08:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965081
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         652679
89                 A    =         6796453
96  meter
 Y    =       -6497425
31  meter          E    =           
0008936
 Z    =        1866953
27                 I    =           52
01635
 XDOT =       5042
991484                 Wp   =          120
12879
 YDOT =      -1124
247413  meter/sec      RA   =          108
63547  deg
 ZDOT =      -5659
827634                 TA   =           39
45995
                                          MA   =           39
39491
                                          Ha   =            223
945  n
mi
                                          Hp   =            221
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2141338
23                 X    =          716218
82
 Y    =      -21317012
16  feet           Y    =        -6489771
49  meter
 Z    =        6125174
76                 Z    =         1870277
47
 XDOT =      16545
247650                 XDOT =        5082
680661
 YDOT =      -3688
475763  feet/sec       YDOT =       -1067
630715  meter/sec
 ZDOT =     -18568
988300                 ZDOT =       -5635
234347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2189080
94                 X    =         -667231
87
 Y    =      -21307649
13  feet           Y    =        -6494571
46  meter
 Z    =        6140856
27                 Z    =         1871732
99
 XDOT =      14046
305598                 XDOT =        4281
313946
 YDOT =      -6777
387243  feet/sec       YDOT =       -2065
747632  meter/sec
 ZDOT =     -18457
317502                 ZDOT =       -5625
790375


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   19146
39355217  
00016717  00000-0  10270-3 0  9193
2 25544  51
6386 109
4623 0005150 282
2021  77
8553 15
51173353 11869


Satellite: ISS
Catalog Number: 25544
Epoch time:      19146
39355217   =   yrday
fracday
Element set:     919
Inclination:       51
6386  deg
RA of node:       109
4623  deg
Eccentricity:     
0005150     
Arg of perigee:   282
2021  deg
Mean anomaly:      77
8553  deg
Mean motion:   15
51173353  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1186
Checksum:              306


Coasting Arc #21 (Orbit 1200)
---------------------------------------

Vector Time (GMT): 2019/147/08:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965081
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -681066
35                 A    =         6797232
50  meter
 Y    =        6654995
35  meter          E    =           
0008543
 Z    =       -1172231
84                 I    =           52
02925
 XDOT =      -4867
313371                 Wp   =            4
45215
 YDOT =        538
371685  meter/sec      RA   =          103
70361  deg
 ZDOT =       5895
496304                 TA   =          342
90090
                                          MA   =          342
92967
                                          Ha   =            223
950  n
mi
                                          Hp   =            221
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2234469
64                 X    =         -749739
72
 Y    =       21833974
25  feet           Y    =         6646995
31  meter
 Z    =       -3845905
00                 Z    =        -1175706
47
 XDOT =     -15968
875888                 XDOT =       -4901
608976
 YDOT =       1766
311301  feet/sec       YDOT =         483
749740  meter/sec
 ZDOT =      19342
179474                 ZDOT =        5871
769395

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2561151
31                 X    =          780638
92
 Y    =       21795170
20  feet           Y    =         6643167
88  meter
 Z    =       -3862296
11                 Z    =        -1177227
85
 XDOT =     -13746
755213                 XDOT =       -4190
010989
 YDOT =       5017
450165  feet/sec       YDOT =        1529
318810  meter/sec
 ZDOT =      19234
486166                 ZDOT =        5862
671383


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   19147
35992713  
00016717  00000-0  10270-3 0  9200
2 25544  51
6389 104
6666 0005198 283
9260  76
1313 15
51212237 12010


Satellite: ISS
Catalog Number: 25544
Epoch time:      19147
35992713   =   yrday
fracday
Element set:     920
Inclination:       51
6389  deg
RA of node:       104
6666  deg
Eccentricity:     
0005198     
Arg of perigee:   283
9260  deg
Mean anomaly:      76
1313  deg
Mean motion:   15
51212237  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1201
Checksum:              304


Coasting Arc #22 (Orbit 1216)
---------------------------------------

Vector Time (GMT): 2019/148/08:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965081
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         694168
63                 A    =         6797844
08  meter
 Y    =       -6743397
57  meter          E    =           
0008079
 Z    =         438794
62                 I    =           52
03711
 XDOT =       4738
968754                 Wp   =          142
64506
 YDOT =         92
695314  meter/sec      RA   =           98
77224  deg
 ZDOT =      -6020
777493                 TA   =           32
65553
                                          MA   =           32
60560
                                          Ha   =            224
218  n
mi
                                          Hp   =            221
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2277456
12                 X    =          767392
20
 Y    =      -22124007
77  feet           Y    =        -6735225
50  meter
 Z    =        1439614
90                 Z    =          442344
00
 XDOT =      15547
797750                 XDOT =        4766
825753
 YDOT =        304
118483  feet/sec       YDOT =         145
845991  meter/sec
 ZDOT =     -19753
206999                 ZDOT =       -5997
689562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2945741
27                 X    =         -897861
94
 Y    =      -22043879
42  feet           Y    =        -6718974
45  meter
 Z    =        1456367
41                 Z    =          443900
79
 XDOT =      13712
075914                 XDOT =        4179
440738
 YDOT =      -3141
539261  feet/sec       YDOT =        -957
541167  meter/sec
 ZDOT =     -19648
467995                 ZDOT =       -5988
853045


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   19148
39072528  
00016717  00000-0  10270-3 0  9219
2 25544  51
6383  99
5501 0005250 290
9866  69
0724 15
51174960 12177


Satellite: ISS
Catalog Number: 25544
Epoch time:      19148
39072528   =   yrday
fracday
Element set:     921
Inclination:       51
6383  deg
RA of node:        99
5501  deg
Eccentricity:     
0005250     
Arg of perigee:   290
9866  deg
Mean anomaly:      69
0724  deg
Mean motion:   15
51174960  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1217
Checksum:              320
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