[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: August 2nd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16520 4497 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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


213/11:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 2
000/00:00:00 000 0 0 0 0 220 3

218/16:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 4
000/00:00:00 000 0 0 0 0 221 2

220/06:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 2
000/00:00:00 000 0 0 0 0 221 4

227/05:42:50 809 0 3 2 0 2 0
N/A 2 0 0 0 223 7
000/00:09:41 618 0 5 -0 0 223 0

227/08:46:28 979 0 4 1 5 1 5
N/A 1 4 -0 0 224 2
000/00:06:57 959 0 2 -0 0 223 9

Coasting Arc #1 (Orbit 2215)
---------------------------------------

Vector Time (GMT): 2019/212/17:27:09
770
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5814117
17                 A    =         6795247
29  meter
 Y    =       -2133037
49  meter          E    =           
0008304
 Z    =       -2786167
47                 I    =           51
89878
 XDOT =       -384
071444                 Wp   =          171
53169
 YDOT =       5664
348192  meter/sec      RA   =          139
19639  deg
 ZDOT =      -5147
933405                 TA   =           39
89260
                                          MA   =           39
83160
                                          Ha   =            226
364  n
mi
                                          Hp   =            220
353

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19075187
58                 X    =         5851070
62
 Y    =       -6998154
48  feet           Y    =        -2067813
02  meter
 Z    =       -9140969
40                 Z    =        -2757835
84
 XDOT =      -1260
076917                 XDOT =        -422
378081
 YDOT =      18583
819526  feet/sec       YDOT =        5659
839602  meter/sec
 ZDOT =     -16889
545293                 ZDOT =       -5149
891464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13087302
59                 X    =        -3989009
83
 Y    =       15617358
18  feet           Y    =         4760170
77  meter
 Z    =       -9011931
17                 Z    =        -2746836
62
 XDOT =      -7144
603536                 XDOT =       -2177
675158
 YDOT =     -15719
478272  feet/sec       YDOT =       -4791
296977  meter/sec
 ZDOT =     -16898
853838                 ZDOT =       -5150
770650


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   19212
75388456  
00016717  00000-0  10270-3 0  9008
2 25544  51
6408 140
1651 0006299 206
3851 153
6980 15
51000352 22160


Satellite: ISS
Catalog Number: 25544
Epoch time:      19212
75388456   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       140
1651  deg
Eccentricity:     
0006299     
Arg of perigee:   206
3851  deg
Mean anomaly:     153
6980  deg
Mean motion:   15
51000352  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2216
Checksum:              292


Coasting Arc #2 (Orbit 2227)
---------------------------------------

Vector Time (GMT): 2019/213/11:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -515196
65                 A    =         6788707
63  meter
 Y    =       -4772888
74  meter          E    =           
0004108
 Z    =        4796126
10                 I    =           51
89713
 XDOT =       6363
624967                 Wp   =          118
22705
 YDOT =      -3351
740195  meter/sec      RA   =          135
41658  deg
 ZDOT =      -2652
091376                 TA   =          357
85400
                                          MA   =          357
85576
                                          Ha   =            226
230  n
mi
                                          Hp   =            220
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1690277
72                 X    =         -485082
84
 Y    =      -15659083
79  feet           Y    =        -4778482
07  meter
 Z    =       15735321
84                 Z    =         4793696
25
 XDOT =      20878
034667                 XDOT =        6413
514178
 YDOT =     -10996
522948  feet/sec       YDOT =       -3280
298491  meter/sec
 ZDOT =      -8701
087191                 ZDOT =       -2621
059217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12170753
50                 X    =        -3709645
67
 Y    =       10013682
26  feet           Y    =         3052170
35  meter
 Z    =       15724605
69                 Z    =         4792859
82
 XDOT =     -19875
643320                 XDOT =       -6058
096084
 YDOT =     -10716
623054  feet/sec       YDOT =       -3266
426707  meter/sec
 ZDOT =      -8559
661839                 ZDOT =       -2608
984928


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   19213
52706378  
00016717  00000-0  10270-3 0  9012
2 25544  51
6420 136
3298 0006198 207
8530 152
2290 15
51004787 22284


Satellite: ISS
Catalog Number: 25544
Epoch time:      19213
52706378   =   yrday
fracday
Element set:     901
Inclination:       51
6420  deg
RA of node:       136
3298  deg
Eccentricity:     
0006198     
Arg of perigee:   207
8530  deg
Mean anomaly:     152
2290  deg
Mean motion:   15
51004787  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2228
Checksum:              300


Coasting Arc #3 (Orbit 2242)
---------------------------------------

Vector Time (GMT): 2019/214/11:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         229296
53                 A    =         6789975
83  meter
 Y    =        5119379
06  meter          E    =           
0010121
 Z    =       -4464143
08                 I    =           51
92510
 XDOT =      -6124
800188                 Wp   =          147
22615
 YDOT =       3172
737715  meter/sec      RA   =          130
47015  deg
 ZDOT =       3319
069462                 TA   =          156
21932
                                          MA   =          156
17252
                                          Ha   =            225
998  n
mi
                                          Hp   =            220
501

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         752285
20                 X    =          193716
86
 Y    =       16795863
04  feet           Y    =         5121744
52  meter
 Z    =      -14646138
71                 Z    =        -4463115
40
 XDOT =     -20094
488806                 XDOT =       -6175
945209
 YDOT =      10409
244473  feet/sec       YDOT =        3103
959738  meter/sec
 ZDOT =      10889
335505                 ZDOT =        3289
194244

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13467511
47                 X    =         4104897
50
 Y    =      -10070717
24  feet           Y    =        -3069554
61  meter
 Z    =      -14641827
63                 Z    =        -4462829
06
 XDOT =      19151
979705                 XDOT =        5837
523414
 YDOT =       9955
071198  feet/sec       YDOT =        3034
305701  meter/sec
 ZDOT =      10753
169857                 ZDOT =        3277
566172


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   19214
49353179  
00016717  00000-0  10270-3 0  9027
2 25544  51
6426 131
5340 0006116 211
3716 148
7071 15
51023252 22433


Satellite: ISS
Catalog Number: 25544
Epoch time:      19214
49353179   =   yrday
fracday
Element set:     902
Inclination:       51
6426  deg
RA of node:       131
5340  deg
Eccentricity:     
0006116     
Arg of perigee:   211
3716  deg
Mean anomaly:     148
7071  deg
Mean motion:   15
51023252  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2243
Checksum:              274


Coasting Arc #4 (Orbit 2258)
---------------------------------------

Vector Time (GMT): 2019/215/11:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          -4066
62                 A    =         6791469
97  meter
 Y    =       -5446944
22  meter          E    =           
0007515
 Z    =        4048373
52                 I    =           51
95043
 XDOT =       5885
164797                 Wp   =          111
72711
 YDOT =      -2935
168249  meter/sec      RA   =          125
52861  deg
 ZDOT =      -3940
107369                 TA   =           19
02790
                                          MA   =           18
99984
                                          Ha   =            225
924  n
mi
                                          Hp   =            220
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -13341
95                 X    =           37178
71
 Y    =      -17870551
91  feet           Y    =        -5446759
20  meter
 Z    =       13282065
34                 Z    =         4048453
78
 XDOT =      19308
283456                 XDOT =        5936
687682
 YDOT =      -9629
817090  feet/sec       YDOT =       -2869
068001  meter/sec
 ZDOT =     -12926
861448                 ZDOT =       -3911
395096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14601798
42                 X    =        -4450628
16
 Y    =       10301659
21  feet           Y    =         3139945
73  meter
 Z    =       13282822
13                 Z    =         4048604
18
 XDOT =     -18239
305693                 XDOT =       -5559
340375
 YDOT =      -9340
502638  feet/sec       YDOT =       -2846
985204  meter/sec
 ZDOT =     -12795
990998                 ZDOT =       -3900
218056


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   19215
52442911  
00016717  00000-0  10270-3 0  9036
2 25544  51
6422 126
4204 0006076 215
1327 144
9424 15
51012512 22590


Satellite: ISS
Catalog Number: 25544
Epoch time:      19215
52442911   =   yrday
fracday
Element set:     903
Inclination:       51
6422  deg
RA of node:       126
4204  deg
Eccentricity:     
0006076     
Arg of perigee:   215
1327  deg
Mean anomaly:     144
9424  deg
Mean motion:   15
51012512  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2259
Checksum:              270


Coasting Arc #5 (Orbit 2273)
---------------------------------------

Vector Time (GMT): 2019/216/11:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -166722
75                 A    =         6792942
65  meter
 Y    =        5777143
70  meter          E    =           
0005523
 Z    =       -3575744
79                 I    =           51
97432
 XDOT =      -5624
045524                 Wp   =          165
96397
 YDOT =       2617
661774  meter/sec      RA   =          120
58822  deg
 ZDOT =       4487
686777                 TA   =          152
13022
                                          MA   =          152
10062
                                          Ha   =            225
703  n
mi
                                          Hp   =            220
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -546990
64                 X    =         -213943
41
 Y    =       18953883
54  feet           Y    =         5775015
31  meter
 Z    =      -11731446
15                 Z    =        -3576669
26
 XDOT =     -18451
592926                 XDOT =       -5674
697233
 YDOT =       8588
129181  feet/sec       YDOT =        2554
486477  meter/sec
 ZDOT =      14723
381813                 ZDOT =        4460
244833

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15634859
70                 X    =         4765505
24
 Y    =      -10723406
44  feet           Y    =        -3268494
28  meter
 Z    =      -11736074
52                 Z    =        -3577155
51
 XDOT =      17045
822088                 XDOT =        5195
566573
 YDOT =       8862
628600  feet/sec       YDOT =        2701
329197  meter/sec
 ZDOT =      14598
303705                 ZDOT =        4449
562969


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   19216
49089291  
00016717  00000-0  10270-3 0  9042
2 25544  51
6425 121
6247 0006131 219
1637 140
9071 15
51033460 22743


Satellite: ISS
Catalog Number: 25544
Epoch time:      19216
49089291   =   yrday
fracday
Element set:     904
Inclination:       51
6425  deg
RA of node:       121
6247  deg
Eccentricity:     
0006131     
Arg of perigee:   219
1637  deg
Mean anomaly:     140
9071  deg
Mean motion:   15
51033460  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2274
Checksum:              289


Coasting Arc #6 (Orbit 2289)
---------------------------------------

Vector Time (GMT): 2019/217/11:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         284725
07                 A    =         6794502
30  meter
 Y    =       -6066177
46  meter          E    =           
0010638
 Z    =        3032175
64                 I    =           51
99544
 XDOT =       5387
258562                 Wp   =          124
34803
 YDOT =      -2237
324435  meter/sec      RA   =          115
65173  deg
 ZDOT =      -4975
295453                 TA   =           21
11615
                                          MA   =           21
07227
                                          Ha   =            225
636  n
mi
                                          Hp   =            220
958

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         934137
38                 X    =          337809
25
 Y    =      -19902157
03  feet           Y    =        -6062696
68  meter
 Z    =        9948082
81                 Z    =         3033687
59
 XDOT =      17674
732814                 XDOT =        5436
043428
 YDOT =      -7340
303263  feet/sec       YDOT =       -2176
807509  meter/sec
 ZDOT =     -16323
147813                 ZDOT =       -4949
008102

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16446393
33                 X    =        -5012860
69
 Y    =       11240047
47  feet           Y    =         3425966
47  meter
 Z    =        9955415
52                 Z    =         3034410
65
 XDOT =     -15719
687675                 XDOT =       -4791
360803
 YDOT =      -8630
452591  feet/sec       YDOT =       -2630
561950  meter/sec
 ZDOT =     -16203
341659                 ZDOT =       -4938
778538


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   19217
52178507  
00016717  00000-0  10270-3 0  9057
2 25544  51
6426 116
5104 0006152 223
0012 137
0659 15
51015389 22900


Satellite: ISS
Catalog Number: 25544
Epoch time:      19217
52178507   =   yrday
fracday
Element set:     905
Inclination:       51
6426  deg
RA of node:       116
5104  deg
Eccentricity:     
0006152     
Arg of perigee:   223
0012  deg
Mean anomaly:     137
0659  deg
Mean motion:   15
51015389  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2290
Checksum:              281


Coasting Arc #7 (Orbit 2304)
---------------------------------------

Vector Time (GMT): 2019/218/11:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -350293
55                 A    =         6795756
06  meter
 Y    =        6330034
38  meter          E    =           
0000644
 Z    =       -2447911
80                 I    =           52
01432
 XDOT =      -5159
517585                 Wp   =          223
01201
 YDOT =       1791
132043  meter/sec      RA   =          110
71616  deg
 ZDOT =       5368
707126                 TA   =          109
79325
                                          MA   =          109
78632
                                          Ha   =            225
350  n
mi
                                          Hp   =            221
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1149257
07                 X    =         -409161
32
 Y    =       20767829
32  feet           Y    =         6325788
03  meter
 Z    =       -8031206
68                 Z    =        -2449756
26
 XDOT =     -16927
551131                 XDOT =       -5205
240977
 YDOT =       5876
417464  feet/sec       YDOT =        1733
178956  meter/sec
 ZDOT =      17613
868523                 ZDOT =        5343
533380

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17074293
66                 X    =         5204244
71
 Y    =      -11872208
19  feet           Y    =        -3618649
06  meter
 Z    =       -8040085
58                 Z    =        -2450618
08
 XDOT =      14231
147006                 XDOT =        4337
653607
 YDOT =       8613
238652  feet/sec       YDOT =        2625
315141  meter/sec
 ZDOT =      17499
154101                 ZDOT =        5333
742170


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   19218
48824176  
00016717  00000-0  10270-3 0  9064
2 25544  51
6435 111
7142 0006088 227
4325 132
6312 15
51049504 23052


Satellite: ISS
Catalog Number: 25544
Epoch time:      19218
48824176   =   yrday
fracday
Element set:     906
Inclination:       51
6435  deg
RA of node:       111
7142  deg
Eccentricity:     
0006088     
Arg of perigee:   227
4325  deg
Mean anomaly:     132
6312  deg
Mean motion:   15
51049504  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2305
Checksum:              290


Coasting Arc #8 (Orbit 2307)
---------------------------------------

Vector Time (GMT): 2019/218/16:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -447364
93                 A    =         6796229
87  meter
 Y    =        6403118
66  meter          E    =           
0000525
 Z    =       -2232736
73                 I    =           52
01398
 XDOT =      -5111
590529                 Wp   =          292
60261
 YDOT =       1556
355533  meter/sec      RA   =          109
75794  deg
 ZDOT =       5486
727922                 TA   =           42
76203
                                          MA   =           42
75794
                                          Ha   =            225
386  n
mi
                                          Hp   =            221
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1467732
71                 X    =         -508087
92
 Y    =       21007607
14  feet           Y    =         6397776
42  meter
 Z    =       -7325251
73                 Z    =        -2235057
21
 XDOT =     -16770
310133                 XDOT =       -5155
265433
 YDOT =       5106
153323  feet/sec       YDOT =        1498
949839  meter/sec
 ZDOT =      18001
075860                 ZDOT =        5461
791946

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5061158
11                 X    =        -1542640
99
 Y    =      -20437622
34  feet           Y    =        -6229387
29  meter
 Z    =       -7336305
73                 Z    =        -2236105
99
 XDOT =      13035
868353                 XDOT =        3973
332674
 YDOT =      -9650
068113  feet/sec       YDOT =       -2941
340761  meter/sec
 ZDOT =      17887
459725                 ZDOT =        5452
097724


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   19218
68153179  
00016717  00000-0  10270-3 0  9075
2 25544  51
6394 110
7522 0006241 227
8541 132
2080 15
51032379 23085


Satellite: ISS
Catalog Number: 25544
Epoch time:      19218
68153179   =   yrday
fracday
Element set:     907
Inclination:       51
6394  deg
RA of node:       110
7522  deg
Eccentricity:     
0006241     
Arg of perigee:   227
8541  deg
Mean anomaly:     132
2080  deg
Mean motion:   15
51032379  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2308
Checksum:              294


Coasting Arc #9 (Orbit 2323)
---------------------------------------

Vector Time (GMT): 2019/219/16:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         465162
96                 A    =         6797132
29  meter
 Y    =       -6585632
77  meter          E    =           
0012390
 Z    =        1582950
55                 I    =           52
02775
 XDOT =       4936
626990                 Wp   =          144
00680
 YDOT =      -1042
014153  meter/sec      RA   =          104
82616  deg
 ZDOT =      -5772
707234                 TA   =           18
78945
                                          MA   =           18
74375
                                          Ha   =            225
093  n
mi
                                          Hp   =            221
299

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1526125
18                 X    =          531081
80
 Y    =      -21606406
74  feet           Y    =        -6580062
47  meter
 Z    =        5193407
32                 Z    =         1585370
02
 XDOT =      16196
282777                 XDOT =        4975
952558
 YDOT =      -3418
681605  feet/sec       YDOT =        -986
589255  meter/sec
 ZDOT =     -18939
328195                 ZDOT =       -5748
631674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5535679
78                 X    =         1687275
20
 Y    =       20938055
67  feet           Y    =         6381919
37  meter
 Z    =        5204942
27                 Z    =         1586466
40
 XDOT =     -12829
940902                 XDOT =       -3910
565987
 YDOT =       8083
514068  feet/sec       YDOT =        2463
855088  meter/sec
 ZDOT =     -18829
659105                 ZDOT =       -5739
280095


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   19219
71241594  
00016717  00000-0  10270-3 0  9080
2 25544  51
6395 105
6372 0006251 234
0872 125
9700 15
51084207 23243


Satellite: ISS
Catalog Number: 25544
Epoch time:      19219
71241594   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:       105
6372  deg
Eccentricity:     
0006251     
Arg of perigee:   234
0872  deg
Mean anomaly:     125
9700  deg
Mean motion:   15
51084207  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2324
Checksum:              297


Coasting Arc #10 (Orbit 2332)
---------------------------------------

Vector Time (GMT): 2019/220/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4101782
01                 A    =         6790795
54  meter
 Y    =       -3352814
04  meter          E    =           
0002742
 Z    =       -4250100
44                 I    =           52
01135
 XDOT =       1546
784515                 Wp   =          107
76084
 YDOT =       6542
730241  meter/sec      RA   =          101
94275  deg
 ZDOT =      -3671
372058                 TA   =          124
79847
                                          MA   =          124
77266
                                          Ha   =            225
203  n
mi
                                          Hp   =            221
425

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13457290
05                 X    =         4159613
74
 Y    =      -11000046
05  feet           Y    =        -3306621
49  meter
 Z    =      -13943899
07                 Z    =        -4230035
36
 XDOT =       5074
752346                 XDOT =        1491
340202
 YDOT =      21465
650397  feet/sec       YDOT =        6559
717615  meter/sec
 ZDOT =     -12045
183917                 ZDOT =       -3663
992815

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -506115
89                 X    =         -154264
12
 Y    =      -17446770
54  feet           Y    =        -5317775
66  meter
 Z    =      -13852293
48                 Z    =        -4222179
05
 XDOT =      18909
838985                 XDOT =        5763
718923
 YDOT =       8981
534704  feet/sec       YDOT =        2737
571778  meter/sec
 ZDOT =     -12012
122446                 ZDOT =       -3661
294922


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   19220
29229088  
00016717  00000-0  10270-3 0  9090
2 25544  51
6400 102
7619 0006056 234
1758 125
8831 15
51039242 23332


Satellite: ISS
Catalog Number: 25544
Epoch time:      19220
29229088   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:       102
7619  deg
Eccentricity:     
0006056     
Arg of perigee:   234
1758  deg
Mean anomaly:     125
8831  deg
Mean motion:   15
51039242  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2333
Checksum:              296


Coasting Arc #11 (Orbit 2348)
---------------------------------------

Vector Time (GMT): 2019/221/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4002878
29                 A    =         6789262
52  meter
 Y    =        2943581
59  meter          E    =           
0007161
 Z    =        4628008
74                 I    =           52
01376
 XDOT =      -1539
014252                 Wp   =          160
44512
 YDOT =      -6866
902459  meter/sec      RA   =           97
00508  deg
 ZDOT =       3028
554342                 TA   =          259
41143
                                          MA   =          259
49210
                                          Ha   =            224
908  n
mi
                                          Hp   =            221
480

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13132802
79                 X    =        -4057976
85
 Y    =        9657419
92  feet           Y    =         2898510
26  meter
 Z    =       15183755
72                 Z    =         4608430
78
 XDOT =      -5049
259357                 XDOT =       -1476
823089
 YDOT =     -22529
207544  feet/sec       YDOT =       -6883
765235  meter/sec
 ZDOT =       9936
201910                 ZDOT =        3021
229123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -86432
68                 X    =          -26344
68
 Y    =       16383976
99  feet           Y    =         4993836
19  meter
 Z    =       15094387
49                 Z    =         4600769
31
 XDOT =     -19970
550554                 XDOT =       -6087
023809
 YDOT =      -9253
339981  feet/sec       YDOT =       -2820
418026  meter/sec
 ZDOT =       9903
427576                 ZDOT =        3018
564725


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   19221
32317073  
00016717  00000-0  10270-3 0  9109
2 25544  51
6413  97
6476 0006271 238
6643 121
3895 15
51081604 23497


Satellite: ISS
Catalog Number: 25544
Epoch time:      19221
32317073   =   yrday
fracday
Element set:     910
Inclination:       51
6413  deg
RA of node:        97
6476  deg
Eccentricity:     
0006271     
Arg of perigee:   238
6643  deg
Mean anomaly:     121
3895  deg
Mean motion:   15
51081604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2349
Checksum:              300


Coasting Arc #12 (Orbit 2363)
---------------------------------------

Vector Time (GMT): 2019/222/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3950437
99                 A    =         6788104
38  meter
 Y    =       -2472118
61  meter          E    =           
0006247
 Z    =       -4941296
89                 I    =           52
01264
 XDOT =       1558
151070                 Wp   =           83
26346
 YDOT =       7129
267634  meter/sec      RA   =           92
06466  deg
 ZDOT =      -2322
855122                 TA   =          164
11248
                                          MA   =          164
09287
                                          Ha   =            224
786  n
mi
                                          Hp   =            221
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12960754
58                 X    =         4001790
12
 Y    =       -8110625
38  feet           Y    =        -2427654
58  meter
 Z    =      -16211603
95                 Z    =        -4921982
80
 XDOT =       5112
044192                 XDOT =        1489
596749
 YDOT =      23389
985677  feet/sec       YDOT =        7146
308817  meter/sec
 ZDOT =      -7620
915756                 ZDOT =       -2315
452329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         969045
60                 X    =          295365
10
 Y    =      -15351688
57  feet           Y    =        -4679194
68  meter
 Z    =      -16123464
72                 Z    =        -4914432
05
 XDOT =      20930
776707                 XDOT =        6379
700740
 YDOT =       9284
261788  feet/sec       YDOT =        2829
842993  meter/sec
 ZDOT =      -7587
824793                 ZDOT =       -2312
768997


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   19222
28962091  
00016717  00000-0  10270-3 0  9112
2 25544  51
6414  92
8517 0006024 242
9299 117
1238 15
51048364 23649


Satellite: ISS
Catalog Number: 25544
Epoch time:      19222
28962091   =   yrday
fracday
Element set:     911
Inclination:       51
6414  deg
RA of node:        92
8517  deg
Eccentricity:     
0006024     
Arg of perigee:   242
9299  deg
Mean anomaly:     117
1238  deg
Mean motion:   15
51048364  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2364
Checksum:              305


Coasting Arc #13 (Orbit 2379)
---------------------------------------

Vector Time (GMT): 2019/223/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3936559
08                 A    =         6787068
21  meter
 Y    =        1988196
98  meter          E    =           
0005456
 Z    =        5161626
72                 I    =           52
00956
 XDOT =      -1609
200779                 Wp   =          197
94149
 YDOT =      -7320
102483  meter/sec      RA   =           87
12527  deg
 ZDOT =       1587
743805                 TA   =          236
78644
                                          MA   =          236
83876
                                          Ha   =            224
515  n
mi
                                          Hp   =            221
655

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12915220
08                 X    =        -3983571
03
 Y    =        6522955
98  feet           Y    =         1943912
39  meter
 Z    =       16934470
88                 Z    =         5142390
64
 XDOT =      -5279
530115                 XDOT =       -1534
937948
 YDOT =     -24016
084263  feet/sec       YDOT =       -7337
682579  meter/sec
 ZDOT =       5209
133217                 ZDOT =        1580
106885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1990983
90                 X    =         -606851
89
 Y    =       14434411
07  feet           Y    =         4399608
49  meter
 Z    =       16846718
63                 Z    =         5134879
84
 XDOT =     -21757
291831                 XDOT =       -6631
622550
 YDOT =      -9058
626780  feet/sec       YDOT =       -2761
069443  meter/sec
 ZDOT =       5175
006141                 ZDOT =        1577
341872


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   19223
32049709  
00016717  00000-0  10270-3 0  9121
2 25544  51
6414  87
7380 0006165 247
4237 112
6262 15
51080022 23800


Satellite: ISS
Catalog Number: 25544
Epoch time:      19223
32049709   =   yrday
fracday
Element set:     912
Inclination:       51
6414  deg
RA of node:        87
7380  deg
Eccentricity:     
0006165     
Arg of perigee:   247
4237  deg
Mean anomaly:     112
6262  deg
Mean motion:   15
51080022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2380
Checksum:              285


Coasting Arc #14 (Orbit 2394)
---------------------------------------

Vector Time (GMT): 2019/224/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3979579
98                 A    =         6786540
30  meter
 Y    =       -1472964
10  meter          E    =           
0008674
 Z    =       -5303679
77                 I    =           52
00504
 XDOT =       1663
794085                 Wp   =           92
81043
 YDOT =       7429
602569  meter/sec      RA   =           82
18294  deg
 ZDOT =       -816
532081                 TA   =          169
42203
                                          MA   =          169
40378
                                          Ha   =            224
380  n
mi
                                          Hp   =            221
911

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13056364
75                 X    =         4021517
16
 Y    =       -4832559
37  feet           Y    =        -1428226
80  meter
 Z    =      -17400524
18                 Z    =        -5284247
06
 XDOT =       5458
642010                 XDOT =        1584
556660
 YDOT =      24375
336513  feet/sec       YDOT =        7447
765294  meter/sec
 ZDOT =      -2678
911026                 ZDOT =        -808
642104

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3232084
54                 X    =          985139
37
 Y    =      -13654734
46  feet           Y    =        -4161963
06  meter
 Z    =      -17311914
65                 Z    =        -5276671
58
 XDOT =      22358
291967                 XDOT =        6814
807392
 YDOT =       8637
397725  feet/sec       YDOT =        2632
678827  meter/sec
 ZDOT =      -2643
653213                 ZDOT =        -805
785499


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   19224
28694399  
00016717  00000-0  10270-3 0  9139
2 25544  51
6417  82
9423 0006106 250
8773 109
1717 15
51051883 23951


Satellite: ISS
Catalog Number: 25544
Epoch time:      19224
28694399   =   yrday
fracday
Element set:     913
Inclination:       51
6417  deg
RA of node:        82
9423  deg
Eccentricity:     
0006106     
Arg of perigee:   250
8773  deg
Mean anomaly:     109
1717  deg
Mean motion:   15
51051883  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2395
Checksum:              324


Coasting Arc #15 (Orbit 2410)
---------------------------------------

Vector Time (GMT): 2019/225/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4067107
40                 A    =         6786236
88  meter
 Y    =         963728
85  meter          E    =           
0003916
 Z    =        5349392
08                 I    =           51
99922
 XDOT =      -1719
479090                 Wp   =          246
29245
 YDOT =      -7465
687296  meter/sec      RA   =           77
24133  deg
 ZDOT =         36
174994                 TA   =          203
35532
                                          MA   =          203
37312
                                          Ha   =            224
118  n
mi
                                          Hp   =            221
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13343528
22                 X    =        -4103565
64
 Y    =        3161840
05  feet           Y    =          918043
45  meter
 Z    =       17550498
96                 Z    =         5329547
53
 XDOT =      -5641
335597                 XDOT =       -1636
043546
 YDOT =     -24493
724725  feet/sec       YDOT =       -7484
449205  meter/sec
 ZDOT =        118
684364                 ZDOT =          28
024832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4560845
45                 X    =        -1390145
69
 Y    =       13054200
94  feet           Y    =         3978920
45  meter
 Z    =       17460054
93                 Z    =         5321824
74
 XDOT =     -22740
114465                 XDOT =       -6931
186889
 YDOT =      -8061
564205  feet/sec       YDOT =       -2457
164770  meter/sec
 ZDOT =         82
255309                 ZDOT =          25
071418


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   19225
31781539  
00016717  00000-0  10270-3 0  9148
2 25544  51
6423  77
8281 0006190 256
0019 104
0444 15
51081398 24111


Satellite: ISS
Catalog Number: 25544
Epoch time:      19225
31781539   =   yrday
fracday
Element set:     914
Inclination:       51
6423  deg
RA of node:        77
8281  deg
Eccentricity:     
0006190     
Arg of perigee:   256
0019  deg
Mean anomaly:     104
0444  deg
Mean motion:   15
51081398  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2411
Checksum:              293


Coasting Arc #16 (Orbit 2425)
---------------------------------------

Vector Time (GMT): 2019/226/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4210692
77                 A    =         6786503
55  meter
 Y    =        -456760
49  meter          E    =           
0008920
 Z    =       -5310287
38                 I    =           51
99098
 XDOT =       1751
974592                 Wp   =          106
58091
 YDOT =       7416
153354  meter/sec      RA   =           72
29748  deg
 ZDOT =        749
867337                 TA   =          170
56732
                                          MA   =          170
55056
                                          Ha   =            223
897  n
mi
                                          Hp   =            221
907

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13814608
81                 X    =         4241281
27
 Y    =       -1498558
04  feet           Y    =         -409502
34  meter
 Z    =      -17422202
71                 Z    =        -5289759
62
 XDOT =       5747
948136                 XDOT =        1665
272467
 YDOT =      24331
211792  feet/sec       YDOT =        7435
260357  meter/sec
 ZDOT =       2460
194675                 ZDOT =         758
167267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5999536
17                 X    =         1828658
62
 Y    =      -12662711
24  feet           Y    =        -3859594
39  meter
 Z    =      -17328691
52                 Z    =        -5281785
17
 XDOT =      22817
739056                 XDOT =        6954
846864
 YDOT =       7386
962806  feet/sec       YDOT =        2251
546263  meter/sec
 ZDOT =       2497
301204                 ZDOT =         761
177407


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   19226
28425696  
00016717  00000-0  10270-3 0  9155
2 25544  51
6419  73
0321 0006028 259
7755 100
2716 15
51056989 24260


Satellite: ISS
Catalog Number: 25544
Epoch time:      19226
28425696   =   yrday
fracday
Element set:     915
Inclination:       51
6419  deg
RA of node:        73
0321  deg
Eccentricity:     
0006028     
Arg of perigee:   259
7755  deg
Mean anomaly:     100
2716  deg
Mean motion:   15
51056989  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2426
Checksum:              319


Coasting Arc #17 (Orbit 2440)
---------------------------------------

Vector Time (GMT): 2019/227/05:47:41
618
Vector Time (MET): N/A
Weight (LBS)     : 937094
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4645247
84                 A    =         6792058
60  meter
 Y    =        2623515
71  meter          E    =           
0002774
 Z    =       -4205293
05                 I    =           51
99405
 XDOT =       -389
272846                 Wp   =          186
13118
 YDOT =       6677
153160  meter/sec      RA   =           67
48043  deg
 ZDOT =       3732
704615                 TA   =          122
08717
                                          MA   =          122
06024
                                          Ha   =            223
679  n
mi
                                          Hp   =            223
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15240314
42                 X    =         4635992
18
 Y    =        8607335
00  feet           Y    =         2675410
46  meter
 Z    =      -13796893
20                 Z    =        -4182751
14
 XDOT =      -1277
141882                 XDOT =        -482
040741
 YDOT =      21906
670473  feet/sec       YDOT =        6672
281275  meter/sec
 ZDOT =      12246
406217                 ZDOT =        3730
588524

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16514345
44                 X    =         5033572
49
 Y    =       -6036950
14  feet           Y    =        -1840062
40  meter
 Z    =      -13694498
50                 Z    =        -4174083
14
 XDOT =      15304
996841                 XDOT =        4664
963037
 YDOT =      14088
648571  feet/sec       YDOT =        4294
220084  meter/sec
 ZDOT =      12236
146264                 ZDOT =        3729
577381


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   19227
25069669  
00016717  00000-0  10270-3 0  9168
2 25544  51
6411  68
2370 0007605 268
7464  91
2816 15
50666356 24412


Satellite: ISS
Catalog Number: 25544
Epoch time:      19227
25069669   =   yrday
fracday
Element set:     916
Inclination:       51
6411  deg
RA of node:        68
2370  deg
Eccentricity:     
0007605     
Arg of perigee:   268
7464  deg
Mean anomaly:      91
2816  deg
Mean motion:   15
50666356  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2441
Checksum:              324


Coasting Arc #18 (Orbit 2442)
---------------------------------------

Vector Time (GMT): 2019/227/08:49:57
959
Vector Time (MET): N/A
Weight (LBS)     : 936945
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4618371
05                 A    =         6790425
60  meter
 Y    =        1182856
82  meter          E    =           
0003940
 Z    =       -4838511
23                 I    =           51
98666
 XDOT =        868
835671                 Wp   =          150
16061
 YDOT =       7159
978948  meter/sec      RA   =           66
86200  deg
 ZDOT =       2577
262686                 TA   =          145
13570
                                          MA   =          145
10988
                                          Ha   =            224
214  n
mi
                                          Hp   =            223
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15152135
97                 X    =         4628303
00
 Y    =        3880763
84  feet           Y    =         1234558
30  meter
 Z    =      -15874380
67                 Z    =        -4816053
30
 XDOT =       2850
510732                 XDOT =         776
187536
 YDOT =      23490
744580  feet/sec       YDOT =        7169
176813  meter/sec
 ZDOT =       8455
586240                 ZDOT =        2581
258152

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2513697
48                 X    =          766174
99
 Y    =      -15542248
18  feet           Y    =        -4737277
25  meter
 Z    =      -15772233
85                 Z    =        -4807376
88
 XDOT =      22018
377141                 XDOT =        6711
201353
 YDOT =      -5045
503269  feet/sec       YDOT =       -1537
869397  meter/sec
 ZDOT =       8473
107912                 ZDOT =        2582
603291


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   19227
37958702  
00016717  00000-0  10270-3 0  9177
2 25544  51
6433  67
5991 0008867 270
9427  89
0708 15
50404284 24439


Satellite: ISS
Catalog Number: 25544
Epoch time:      19227
37958702   =   yrday
fracday
Element set:     917
Inclination:       51
6433  deg
RA of node:        67
5991  deg
Eccentricity:     
0008867     
Arg of perigee:   270
9427  deg
Mean anomaly:      89
0708  deg
Mean motion:   15
50404284  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2443
Checksum:              340
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