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

 
Date: August 26th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16550 5887 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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


239/14:44:31 000 0 0 0 0 0 0
N/A 0 0 0 0 227 5
000/00:00:00 000 0 0 0 0 221 4

240/02:16:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 7
000/00:00:00 000 0 0 0 0 221 1

249/18:11:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 7
000/00:00:00 000 0 0 0 0 219 3

250/16:32:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 0
000/00:00:00 000 0 0 0 0 219 0

Coasting Arc #1 (Orbit 2615)
---------------------------------------

Vector Time (GMT): 2019/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6472569
26                 A    =         6799919
23  meter
 Y    =       -1949698
39  meter          E    =           
0003180
 Z    =        -729347
03                 I    =           51
74237
 XDOT =       1988
659053                 Wp   =          120
80614
 YDOT =      -4381
479419  meter/sec      RA   =           11
88297  deg
 ZDOT =      -5956
581592                 TA   =           67
04563
                                          MA   =           67
01207
                                          Ha   =            227
268  n
mi
                                          Hp   =            221
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21235463
44                 X    =        -6446743
39
 Y    =       -6396648
26  feet           Y    =        -2021934
79  meter
 Z    =       -2392870
85                 Z    =         -760725
34
 XDOT =       6524
471960                 XDOT =        2066
439661
 YDOT =     -14374
932477  feet/sec       YDOT =       -4358
805743  meter/sec
 ZDOT =     -19542
590524                 ZDOT =       -5946
732768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16150965
46                 X    =         4922814
27
 Y    =       15175823
59  feet           Y    =         4625591
03  meter
 Z    =       -2535456
65                 Z    =         -772807
19
 XDOT =     -11254
363706                 XDOT =       -3430
330058
 YDOT =       8730
884564  feet/sec       YDOT =        2661
173615  meter/sec
 ZDOT =     -19497
305115                 ZDOT =       -5942
778599


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   19238
53075622  
00016717  00000-0  10270-3 0  9000
2 25544  51
6413  12
3176 0007394 328
2730  31
7974 15
50404173 26166


Satellite: ISS
Catalog Number: 25544
Epoch time:      19238
53075622   =   yrday
fracday
Element set:     900
Inclination:       51
6413  deg
RA of node:        12
3176  deg
Eccentricity:     
0007394     
Arg of perigee:   328
2730  deg
Mean anomaly:      31
7974  deg
Mean motion:   15
50404173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2616
Checksum:              290


Coasting Arc #2 (Orbit 2631)
---------------------------------------

Vector Time (GMT): 2019/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6458231
53                 A    =         6799566
49  meter
 Y    =        1727219
73  meter          E    =           
0015896
 Z    =        1184114
65                 I    =           51
70994
 XDOT =      -2254
329171                 Wp   =           30
55073
 YDOT =       4392
107807  meter/sec      RA   =            6
93475  deg
 ZDOT =       5867
426844                 TA   =          342
28820
                                          MA   =          342
34355
                                          Ha   =            227
357  n
mi
                                          Hp   =            221
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21188423
67                 X    =         6432685
60
 Y    =        5666731
41  feet           Y    =         1799297
36  meter
 Z    =        3884890
60                 Z    =         1215423
83
 XDOT =      -7396
093080                 XDOT =       -2331
775698
 YDOT =      14409
802515  feet/sec       YDOT =        4366
465147  meter/sec
 ZDOT =      19250
088071                 ZDOT =        5856
288328

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16671753
25                 X    =        -5081550
39
 Y    =      -14212247
34  feet           Y    =        -4331892
99  meter
 Z    =        4027180
95                 Z    =         1227484
75
 XDOT =      11952
552781                 XDOT =        3643
138088
 YDOT =      -8561
758979  feet/sec       YDOT =       -2609
624137  meter/sec
 ZDOT =      19198
935522                 ZDOT =        5851
835547


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   19239
56207620  
00016717  00000-0  10270-3 0  9010
2 25544  51
6431   7
2053 0007339 331
8719  28
2034 15
50397433 26325


Satellite: ISS
Catalog Number: 25544
Epoch time:      19239
56207620   =   yrday
fracday
Element set:     901
Inclination:       51
6431  deg
RA of node:         7
2053  deg
Eccentricity:     
0007339     
Arg of perigee:   331
8719  deg
Mean anomaly:      28
2034  deg
Mean motion:   15
50397433  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2632
Checksum:              289


Coasting Arc #3 (Orbit 2632)
---------------------------------------

Vector Time (GMT): 2019/239/14:44:31
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2842341
56                 A    =         6789783
22  meter
 Y    =       -3644763
58  meter          E    =           
0008959
 Z    =       -4979853
03                 I    =           51
67431
 XDOT =       6921
016795                 Wp   =           68
48984
 YDOT =       2475
319343  meter/sec      RA   =            6
34310  deg
 ZDOT =       2144
919730                 TA   =          222
39648
                                          MA   =          222
46573
                                          Ha   =            227
469  n
mi
                                          Hp   =            221
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9325267
59                 X    =         2907076
08
 Y    =      -11957885
77  feet           Y    =        -3612616
46  meter
 Z    =      -16338100
48                 Z    =        -4965889
07
 XDOT =      22706
748014                 XDOT =        6882
404018
 YDOT =       8121
126455  feet/sec       YDOT =        2552
499082  meter/sec
 ZDOT =       7037
138222                 ZDOT =        2178
445166

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5825736
36                 X    =        -1775684
44
 Y    =       14074705
69  feet           Y    =         4289970
29  meter
 Z    =      -16274170
66                 Z    =        -4960367
22
 XDOT =     -22987
349728                 XDOT =       -7006
544197
 YDOT =      -1225
932486  feet/sec       YDOT =        -373
664222  meter/sec
 ZDOT =       7189
433815                 ZDOT =        2191
339427


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   19239
62653297  
00016717  00000-0  10270-3 0  9023
2 25544  51
6439   6
8885 0007503 332
0649  28
0098 15
50410139 26337


Satellite: ISS
Catalog Number: 25544
Epoch time:      19239
62653297   =   yrday
fracday
Element set:     902
Inclination:       51
6439  deg
RA of node:         6
8885  deg
Eccentricity:     
0007503     
Arg of perigee:   332
0649  deg
Mean anomaly:      28
0098  deg
Mean motion:   15
50410139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2633
Checksum:              314


Coasting Arc #4 (Orbit 2640)
---------------------------------------

Vector Time (GMT): 2019/240/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -645486
45                 A    =         6788197
26  meter
 Y    =        4171618
89  meter          E    =           
0007963
 Z    =        5317218
05                 I    =           51
65305
 XDOT =      -7616
301921                 Wp   =          353
34462
 YDOT =       -774
978739  meter/sec      RA   =            3
98085  deg
 ZDOT =       -308
894703                 TA   =           99
64700
                                          MA   =           99
55703
                                          Ha   =            227
675  n
mi
                                          Hp   =            221
090

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2117737
71                 X    =         -717914
35
 Y    =       13686413
67  feet           Y    =         4163995
57  meter
 Z    =       17444941
10                 Z    =         5313906
71
 XDOT =     -24987
867195                 XDOT =       -7605
569418
 YDOT =      -2542
581166  feet/sec       YDOT =        -860
089576  meter/sec
 ZDOT =      -1013
434064                 ZDOT =        -345
865121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -34829
77                 X    =          -10616
11
 Y    =       13868755
61  feet           Y    =         4227196
71  meter
 Z    =       17429432
21                 Z    =         5312490
94
 XDOT =     -24056
101863                 XDOT =       -7332
299848
 YDOT =       1456
229650  feet/sec       YDOT =         443
858797  meter/sec
 ZDOT =      -1181
583426                 ZDOT =        -360
146628


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   19240
14219220  
00016717  00000-0  10270-3 0  9037
2 25544  51
6436   4
3348 0007936 335
1736  24
9032 15
50424942 26411


Satellite: ISS
Catalog Number: 25544
Epoch time:      19240
14219220   =   yrday
fracday
Element set:     903
Inclination:       51
6436  deg
RA of node:         4
3348  deg
Eccentricity:     
0007936     
Arg of perigee:   335
1736  deg
Mean anomaly:      24
9032  deg
Mean motion:   15
50424942  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2641
Checksum:              282


Coasting Arc #5 (Orbit 2655)
---------------------------------------

Vector Time (GMT): 2019/241/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         863800
21                 A    =         6788477
72  meter
 Y    =       -4194395
66  meter          E    =           
0012990
 Z    =       -5276622
55                 I    =           51
62122
 XDOT =       7591
039625                 Wp   =           63
19985
 YDOT =        527
936334  meter/sec      RA   =          359
02067  deg
 ZDOT =        830
320513                 TA   =          214
71145
                                          MA   =          214
79629
                                          Ha   =            227
851  n
mi
                                          Hp   =            220
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2833990
20                 X    =          936269
34
 Y    =      -13761140
62  feet           Y    =        -4184330
92  meter
 Z    =      -17311753
76                 Z    =        -5272250
54
 XDOT =      24904
985646                 XDOT =        7580
538758
 YDOT =       1732
074587  feet/sec       YDOT =         612
765982  meter/sec
 ZDOT =       2724
148664                 ZDOT =         867
168670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         487363
36                 X    =          148548
35
 Y    =      -14066503
55  feet           Y    =        -4287470
28  meter
 Z    =      -17291421
70                 Z    =        -5270425
33
 XDOT =      23777
684488                 XDOT =        7247
438232
 YDOT =      -2701
427139  feet/sec       YDOT =        -823
394992  meter/sec
 ZDOT =       2891
759560                 ZDOT =         881
408314


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   19241
10905272  
00016717  00000-0  10270-3 0  9044
2 25544  51
6445 359
5422 0007936 340
1471  19
9370 15
50402726 26562


Satellite: ISS
Catalog Number: 25544
Epoch time:      19241
10905272   =   yrday
fracday
Element set:     904
Inclination:       51
6445  deg
RA of node:       359
5422  deg
Eccentricity:     
0007936     
Arg of perigee:   340
1471  deg
Mean anomaly:      19
9370  deg
Mean motion:   15
50402726  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2656
Checksum:              300


Coasting Arc #6 (Orbit 2671)
---------------------------------------

Vector Time (GMT): 2019/242/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1118610
39                 A    =         6788801
42  meter
 Y    =        4245256
69  meter          E    =           
0010318
 Z    =        5179254
22                 I    =           51
58881
 XDOT =      -7532
674760                 Wp   =            6
91210
 YDOT =       -305
337192  meter/sec      RA   =          354
05894  deg
 ZDOT =      -1366
323746                 TA   =           96
30183
                                          MA   =           96
18429
                                          Ha   =            227
962  n
mi
                                          Hp   =            220
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3669981
59                 X    =        -1191156
37
 Y    =       13928007
51  feet           Y    =         4232342
21  meter
 Z    =       16992303
88                 Z    =         5173644
15
 XDOT =     -24713
499869                 XDOT =       -7522
063844
 YDOT =      -1001
762442  feet/sec       YDOT =        -389
513599  meter/sec
 ZDOT =      -4482
689456                 ZDOT =       -1402
888132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1031421
95                 X    =         -314377
41
 Y    =       14397082
88  feet           Y    =         4388230
86  meter
 Z    =       16966340
87                 Z    =         5171340
70
 XDOT =     -23363
921479                 XDOT =       -7121
323267
 YDOT =       3844
746038  feet/sec       YDOT =        1171
878592  meter/sec
 ZDOT =      -4649
021030                 ZDOT =       -1417
021610


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   19242
14036744  
00016717  00000-0  10270-3 0  9059
2 25544  51
6440 354
4308 0008008 342
8941  17
1939 15
50432941 26727


Satellite: ISS
Catalog Number: 25544
Epoch time:      19242
14036744   =   yrday
fracday
Element set:     905
Inclination:       51
6440  deg
RA of node:       354
4308  deg
Eccentricity:     
0008008     
Arg of perigee:   342
8941  deg
Mean anomaly:      17
1939  deg
Mean motion:   15
50432941  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2672
Checksum:              300


Coasting Arc #7 (Orbit 2686)
---------------------------------------

Vector Time (GMT): 2019/243/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1316002
43                 A    =         6789422
36  meter
 Y    =       -4342518
06  meter          E    =           
0011570
 Z    =       -5058280
35                 I    =           51
55825
 XDOT =       7423
359140                 Wp   =           66
13834
 YDOT =         81
179288  meter/sec      RA   =          349
09524  deg
 ZDOT =       1869
594868                 TA   =          221
98488
                                          MA   =          222
07363
                                          Ha   =            228
081  n
mi
                                          Hp   =            220
578

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4317593
27                 X    =         1389033
82
 Y    =      -14247106
49  feet           Y    =        -4327393
61  meter
 Z    =      -16595407
98                 Z    =        -5051710
13
 XDOT =      24354
852823                 XDOT =        7412
818353
 YDOT =        266
336248  feet/sec       YDOT =         164
133716  meter/sec
 ZDOT =       6133
841431                 ZDOT =        1905
628550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1347430
65                 X    =          410696
86
 Y    =      -14859742
00  feet           Y    =        -4529249
36  meter
 Z    =      -16565075
29                 Z    =        -5049034
95
 XDOT =      22746
182432                 XDOT =        6933
036405
 YDOT =      -4928
773925  feet/sec       YDOT =       -1502
290292  meter/sec
 ZDOT =       6297
767065                 ZDOT =        1919
559401


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   19243
10722537  
00016717  00000-0  10270-3 0  9069
2 25544  51
6448 349
6387 0008016 346
1694  13
9235 15
50407129 26878


Satellite: ISS
Catalog Number: 25544
Epoch time:      19243
10722537   =   yrday
fracday
Element set:     906
Inclination:       51
6448  deg
RA of node:       349
6387  deg
Eccentricity:     
0008016     
Arg of perigee:   346
1694  deg
Mean anomaly:      13
9235  deg
Mean motion:   15
50407129  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2687
Checksum:              321


Coasting Arc #8 (Orbit 2702)
---------------------------------------

Vector Time (GMT): 2019/244/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1543735
46                 A    =         6790061
57  meter
 Y    =        4466869
07  meter          E    =           
0012419
 Z    =        4875814
90                 I    =           51
52855
 XDOT =      -7280
421871                 Wp   =           21
07874
 YDOT =        100
502026  meter/sec      RA   =          344
12923  deg
 ZDOT =      -2383
892863                 TA   =           92
40994
                                          MA   =           92
26775
                                          Ha   =            228
212  n
mi
                                          Hp   =            220
293

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5064748
89                 X    =        -1617254
28
 Y    =       14655082
26  feet           Y    =         4449195
28  meter
 Z    =       15996768
05                 Z    =         4868137
16
 XDOT =     -23885
898528                 XDOT =       -7269
425124
 YDOT =        329
731057  feet/sec       YDOT =          19
148504  meter/sec
 ZDOT =      -7821
170811                 ZDOT =       -2419
231316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1723196
33                 X    =         -525230
24
 Y    =       15446171
91  feet           Y    =         4707993
20  meter
 Z    =       15961393
21                 Z    =         4865032
65
 XDOT =     -22014
133884                 XDOT =       -6709
908008
 YDOT =       5837
239263  feet/sec       YDOT =        1779
190527  meter/sec
 ZDOT =      -7981
935893                 ZDOT =       -2432
894060


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   19244
13853533  
00016717  00000-0  10270-3 0  9075
2 25544  51
6451 344
5268 0008157 349
7194  10
3789 15
50447088 27036


Satellite: ISS
Catalog Number: 25544
Epoch time:      19244
13853533   =   yrday
fracday
Element set:     907
Inclination:       51
6451  deg
RA of node:       344
5268  deg
Eccentricity:     
0008157     
Arg of perigee:   349
7194  deg
Mean anomaly:      10
3789  deg
Mean motion:   15
50447088  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2703
Checksum:              325


Coasting Arc #9 (Orbit 2717)
---------------------------------------

Vector Time (GMT): 2019/245/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1696923
52                 A    =         6790974
56  meter
 Y    =       -4627180
26  meter          E    =           
0010098
 Z    =       -4677530
76                 I    =           51
49858
 XDOT =       7099
712049                 Wp   =           62
60527
 YDOT =       -272
620823  meter/sec      RA   =          339
16184  deg
 ZDOT =       2854
627526                 TA   =          235
79634
                                          MA   =          235
89208
                                          Ha   =            228
367  n
mi
                                          Hp   =            220
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5567334
37                 X    =         1771260
58
 Y    =      -15181037
59  feet           Y    =        -4607788
81  meter
 Z    =      -15346229
54                 Z    =        -4669106
86
 XDOT =      23293
018533                 XDOT =        7088
366796
 YDOT =       -894
425272  feet/sec       YDOT =        -193
290037  meter/sec
 ZDOT =       9365
575873                 ZDOT =        2889
087526

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1812761
35                 X    =          552529
66
 Y    =      -16104709
42  feet           Y    =        -4908715
43  meter
 Z    =      -15307452
64                 Z    =        -4665711
57
 XDOT =      21142
088183                 XDOT =        6444
108478
 YDOT =      -6642
116364  feet/sec       YDOT =       -2024
517068  meter/sec
 ZDOT =       9522
346304                 ZDOT =        2902
411153


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   19245
10538900  
00016717  00000-0  10270-3 0  9082
2 25544  51
6442 339
7344 0008149 353
7947   6
3101 15
50411224 27181


Satellite: ISS
Catalog Number: 25544
Epoch time:      19245
10538900   =   yrday
fracday
Element set:     908
Inclination:       51
6442  deg
RA of node:       339
7344  deg
Eccentricity:     
0008149     
Arg of perigee:   353
7947  deg
Mean anomaly:       6
3101  deg
Mean motion:   15
50411224  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2718
Checksum:              297


Coasting Arc #10 (Orbit 2733)
---------------------------------------

Vector Time (GMT): 2019/246/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1872595
74                 A    =         6791869
79  meter
 Y    =        4809732
20  meter          E    =           
0014152
 Z    =        4414066
70                 I    =           51
47058
 XDOT =      -6889
546570                 Wp   =           36
09371
 YDOT =        387
607300  meter/sec      RA   =          334
19286  deg
 ZDOT =      -3328
461057                 TA   =           87
72303
                                          MA   =           87
56100
                                          Ha   =            228
461  n
mi
                                          Hp   =            219
917

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6143686
82                 X    =        -1947681
43
 Y    =       15779961
28  feet           Y    =         4788371
99  meter
 Z    =       14481846
14                 Z    =         4404787
64
 XDOT =     -22603
499244                 XDOT =       -6877
201074
 YDOT =       1271
677495  feet/sec       YDOT =         310
632329  meter/sec
 ZDOT =     -10920
147824                 ZDOT =       -3361
897872

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1930984
40                 X    =         -588564
04
 Y    =       16859941
84  feet           Y    =         5138910
27  meter
 Z    =       14439168
74                 Z    =         4401058
63
 XDOT =     -20197
850399                 XDOT =       -6156
304802
 YDOT =       7216
185292  feet/sec       YDOT =        2199
493277  meter/sec
 ZDOT =     -11072
261837                 ZDOT =       -3374
825408


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   19246
13669632  
00016717  00000-0  10270-3 0  9094
2 25544  51
6437 334
6226 0008245 357
0824   3
0278 15
50450453 27340


Satellite: ISS
Catalog Number: 25544
Epoch time:      19246
13669632   =   yrday
fracday
Element set:     909
Inclination:       51
6437  deg
RA of node:       334
6226  deg
Eccentricity:     
0008245     
Arg of perigee:   357
0824  deg
Mean anomaly:       3
0278  deg
Mean motion:   15
50450453  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2734
Checksum:              308


Coasting Arc #11 (Orbit 2748)
---------------------------------------

Vector Time (GMT): 2019/247/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1961349
68                 A    =         6792937
53  meter
 Y    =       -5013395
58  meter          E    =           
0009142
 Z    =       -4144942
03                 I    =           51
44415
 XDOT =       6659
524061                 Wp   =           50
79851
 YDOT =       -486
626310  meter/sec      RA   =          329
22193  deg
 ZDOT =       3751
037191                 TA   =          257
92837
                                          MA   =          258
03082
                                          Ha   =            228
568  n
mi
                                          Hp   =            219
848

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6434874
29                 X    =         2037398
98
 Y    =      -16448148
22  feet           Y    =        -4991037
38  meter
 Z    =      -13598891
18                 Z    =        -4135229
55
 XDOT =      21848
832221                 XDOT =        6646
250246
 YDOT =      -1596
543012  feet/sec       YDOT =        -412
228840  meter/sec
 ZDOT =      12306
552465                 ZDOT =        3783
354457

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1730328
33                 X    =          527404
07
 Y    =      -17611583
34  feet           Y    =        -5368010
60  meter
 Z    =      -13554229
03                 Z    =        -4131329
01
 XDOT =      19194
192486                 XDOT =        5850
389870
 YDOT =      -7670
265987  feet/sec       YDOT =       -2337
897073  meter/sec
 ZDOT =      12453
573434                 ZDOT =        3795
849183


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   19247
10354693  
00016717  00000-0  10270-3 0  9102
2 25544  51
6435 329
8296 0008191    
1567 359
9585 15
50416094 27494


Satellite: ISS
Catalog Number: 25544
Epoch time:      19247
10354693   =   yrday
fracday
Element set:     910
Inclination:       51
6435  deg
RA of node:       329
8296  deg
Eccentricity:     
0008191     
Arg of perigee:      
1567  deg
Mean anomaly:     359
9585  deg
Mean motion:   15
50416094  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2749
Checksum:              330


Coasting Arc #12 (Orbit 2764)
---------------------------------------

Vector Time (GMT): 2019/248/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2068792
54                 A    =         6793969
13  meter
 Y    =        5231488
35  meter          E    =           
0015426
 Z    =        3807111
12                 I    =           51
42008
 XDOT =      -6406
899752                 Wp   =           50
37849
 YDOT =        515
135951  meter/sec      RA   =          324
24932  deg
 ZDOT =      -4168
430604                 TA   =           83
81903
                                          MA   =           83
64331
                                          Ha   =            228
694  n
mi
                                          Hp   =            219
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6787377
09                 X    =        -2145631
63
 Y    =       17163675
70  feet           Y    =         5207924
16  meter
 Z    =       12490522
04                 Z    =         3796874
88
 XDOT =     -21020
012309                 XDOT =       -6391
936048
 YDOT =       1690
078578  feet/sec       YDOT =         443
573001  meter/sec
 ZDOT =     -13675
953424                 ZDOT =       -4199
516606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1547687
63                 X    =         -471735
19
 Y    =       18423850
79  feet           Y    =         5615589
72  meter
 Z    =       12443463
23                 Z    =         3792767
59
 XDOT =     -18173
470699                 XDOT =       -5539
273869
 YDOT =       7852
212334  feet/sec       YDOT =        2393
354319  meter/sec
 ZDOT =     -13817
369671                 ZDOT =       -4211
534276


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   19248
13484957  
00016717  00000-0  10270-3 0  9114
2 25544  51
6438 324
7166 0008393   3
8381 356
2833 15
50452760 27659


Satellite: ISS
Catalog Number: 25544
Epoch time:      19248
13484957   =   yrday
fracday
Element set:     911
Inclination:       51
6438  deg
RA of node:       324
7166  deg
Eccentricity:     
0008393     
Arg of perigee:     3
8381  deg
Mean anomaly:     356
2833  deg
Mean motion:   15
50452760  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2765
Checksum:              327


Coasting Arc #13 (Orbit 2779)
---------------------------------------

Vector Time (GMT): 2019/249/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2082080
13                 A    =         6795086
94  meter
 Y    =       -5453561
73  meter          E    =           
0010055
 Z    =       -3475154
60                 I    =           51
39527
 XDOT =       6155
505030                 Wp   =           36
65625
 YDOT =       -526
976337  meter/sec      RA   =          319
27588  deg
 ZDOT =       4529
651112                 TA   =          282
45603
                                          MA   =          282
56852
                                          Ha   =            228
801  n
mi
                                          Hp   =            219
484

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6830971
54                 X    =         2159789
03
 Y    =      -17892262
88  feet           Y    =        -5429844
02  meter
 Z    =      -11401425
85                 Z    =        -3464851
78
 XDOT =      20195
226476                 XDOT =        6138
937840
 YDOT =      -1728
924989  feet/sec       YDOT =        -458
233669  meter/sec
 ZDOT =      14861
060079                 ZDOT =        4559
511984

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1039886
31                 X    =          316957
35
 Y    =      -19151812
80  feet           Y    =        -5837472
54  meter
 Z    =      -11354050
26                 Z    =        -3460714
52
 XDOT =      17180
397360                 XDOT =        5236
585115
 YDOT =      -7929
276890  feet/sec       YDOT =       -2416
843596  meter/sec
 ZDOT =      14996
900628                 ZDOT =        4571
055311


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   19249
10169668  
00016717  00000-0  10270-3 0  9122
2 25544  51
6420 319
9235 0008266   7
6118 352
5156 15
50414462 27803


Satellite: ISS
Catalog Number: 25544
Epoch time:      19249
10169668   =   yrday
fracday
Element set:     912
Inclination:       51
6420  deg
RA of node:       319
9235  deg
Eccentricity:     
0008266     
Arg of perigee:     7
6118  deg
Mean anomaly:     352
5156  deg
Mean motion:   15
50414462  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2780
Checksum:              309


Coasting Arc #14 (Orbit 2790)
---------------------------------------

Vector Time (GMT): 2019/249/18:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918206
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4819167
62                 A    =         6790479
26  meter
 Y    =         610621
41  meter          E    =           
0009321
 Z    =        4735770
09                 I    =           51
36147
 XDOT =      -3439
798488                 Wp   =           61
15015
 YDOT =       6304
984530  meter/sec      RA   =          316
02234  deg
 ZDOT =       2687
811840                 TA   =            2
19075
                                          MA   =            2
18667
                                          Ha   =            228
672  n
mi
                                          Hp   =            219
322

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15810917
40                 X    =         4788977
64
 Y    =        2003351
09  feet           Y    =          664344
03  meter
 Z    =       15537303
43                 Z    =         4759106
39
 XDOT =     -11285
428110                 XDOT =       -3523
102851
 YDOT =      20685
644783  feet/sec       YDOT =        6266
052546  meter/sec
 ZDOT =       8818
280315                 ZDOT =        2670
900191

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5380871
97                 X    =        -1640089
78
 Y    =       14890860
09  feet           Y    =         4538734
16  meter
 Z    =       15643363
61                 Z    =         4768097
23
 XDOT =     -16628
735038                 XDOT =       -5068
438439
 YDOT =     -15190
009642  feet/sec       YDOT =       -4629
914939  meter/sec
 ZDOT =       8740
776727                 ZDOT =        2664
188746


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   19249
81071738  
00016717  00000-0  10270-3 0  9131
2 25544  51
6397 316
4087 0008159  10
9762 349
1566 15
50430147 27913


Satellite: ISS
Catalog Number: 25544
Epoch time:      19249
81071738   =   yrday
fracday
Element set:     913
Inclination:       51
6397  deg
RA of node:       316
4087  deg
Eccentricity:     
0008159     
Arg of perigee:    10
9762  deg
Mean anomaly:     349
1566  deg
Mean motion:   15
50430147  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2791
Checksum:              328


Coasting Arc #15 (Orbit 2804)
---------------------------------------

Vector Time (GMT): 2019/250/16:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918206
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5440919
32                 A    =         6794214
32  meter
 Y    =        1664240
80  meter          E    =           
0012122
 Z    =       -3728241
62                 I    =           51
35239
 XDOT =        996
863020                 Wp   =           40
78369
 YDOT =      -6278
272608  meter/sec      RA   =          311
39314  deg
 ZDOT =      -4256
226226                 TA   =          183
78458
                                          MA   =          183
79376
                                          Ha   =            228
988  n
mi
                                          Hp   =            219
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17850785
17                 X    =        -5441015
34
 Y    =        5460107
60  feet           Y    =         1603396
00  meter
 Z    =      -12231763
84                 Z    =        -3754671
67
 XDOT =       3270
547966                 XDOT =        1087
668649
 YDOT =     -20598
007245  feet/sec       YDOT =       -6266
617327  meter/sec
 ZDOT =     -13963
996804                 ZDOT =       -4251
163216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6157960
88                 X    =         1876946
48
 Y    =      -17538083
89  feet           Y    =        -5345607
97  meter
 Z    =      -12352104
42                 Z    =        -3764921
43
 XDOT =      13297
311760                 XDOT =        4053
020625
 YDOT =      14489
741556  feet/sec       YDOT =        4416
473226  meter/sec
 ZDOT =     -13940
385999                 ZDOT =       -4249
029653


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   19250
71310607  
00016717  00000-0  10270-3 0  9144
2 25544  51
6401 311
9352 0008177  15
8798 344
2607 15
50402806 28056


Satellite: ISS
Catalog Number: 25544
Epoch time:      19250
71310607   =   yrday
fracday
Element set:     914
Inclination:       51
6401  deg
RA of node:       311
9352  deg
Eccentricity:     
0008177     
Arg of perigee:    15
8798  deg
Mean anomaly:     344
2607  deg
Mean motion:   15
50402806  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2805
Checksum:              294


Coasting Arc #16 (Orbit 2820)
---------------------------------------

Vector Time (GMT): 2019/251/16:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918206
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5205541
96                 A    =         6793042
56  meter
 Y    =       -1605758
85  meter          E    =           
0014014
 Z    =        4042979
06                 I    =           51
32780
 XDOT =       -986
587553                 Wp   =           66
75348
 YDOT =       6550
596481  meter/sec      RA   =          306
41573  deg
 ZDOT =       3866
732047                 TA   =          343
00586
                                          MA   =          343
05275
                                          Ha   =            228
848  n
mi
                                          Hp   =            218
990

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17078549
72                 X    =         5203472
76
 Y    =       -5268237
69  feet           Y    =        -1547558
30  meter
 Z    =       13264366
99                 Z    =         4068260
41
 XDOT =      -3236
835805                 XDOT =       -1078
547158
 YDOT =      21491
458271  feet/sec       YDOT =        6539
049664  meter/sec
 ZDOT =      12686
128764                 ZDOT =        3861
716134

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5559913
98                 X    =        -1694661
78
 Y    =       16895314
57  feet           Y    =         5149691
88  meter
 Z    =       13379473
94                 Z    =         4078063
66
 XDOT =     -14351
369330                 XDOT =       -4374
297372
 YDOT =     -14763
976314  feet/sec       YDOT =       -4500
059980  meter/sec
 ZDOT =      12662
720660                 ZDOT =        3859
597257


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   19251
74440357  
00016717  00000-0  10270-3 0  9155
2 25544  51
6403 306
8235 0008198  18
3727 341
7718 15
50437515 28212


Satellite: ISS
Catalog Number: 25544
Epoch time:      19251
74440357   =   yrday
fracday
Element set:     915
Inclination:       51
6403  deg
RA of node:       306
8235  deg
Eccentricity:     
0008198     
Arg of perigee:    18
3727  deg
Mean anomaly:     341
7718  deg
Mean motion:   15
50437515  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2821
Checksum:              311


Coasting Arc #17 (Orbit 2835)
---------------------------------------

Vector Time (GMT): 2019/252/16:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918206
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5007143
24                 A    =         6792086
67  meter
 Y    =        1510491
38  meter          E    =           
0015751
 Z    =       -4350080
08                 I    =           51
30471
 XDOT =        930
454355                 Wp   =           46
47692
 YDOT =      -6777
257715  meter/sec      RA   =          301
43506  deg
 ZDOT =      -3421
481343                 TA   =          188
54020
                                          MA   =          188
56704
                                          Ha   =            229
193  n
mi
                                          Hp   =            218
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16427635
32                 X    =        -5002531
82
 Y    =        4955680
37  feet           Y    =         1454523
62  meter
 Z    =      -14271916
26                 Z    =        -4374391
47
 XDOT =       3052
671770                 XDOT =        1022
789924
 YDOT =     -22235
097490  feet/sec       YDOT =       -6766
336544  meter/sec
 ZDOT =     -11225
332489                 ZDOT =       -3416
737124

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5154135
67                 X    =         1570980
55
 Y    =      -16269274
53  feet           Y    =        -4958874
88  meter
 Z    =      -14382599
05                 Z    =        -4383816
19
 XDOT =      15378
510884                 XDOT =        4687
370118
 YDOT =      14783
980746  feet/sec       YDOT =        4506
157331  meter/sec
 ZDOT =     -11203
155977                 ZDOT =       -3414
721942


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   19252
71124600  
00016717  00000-0  10270-3 0  9164
2 25544  51
6396 302
0304 0008346  22
6810 337
4708 15
50407050 28362


Satellite: ISS
Catalog Number: 25544
Epoch time:      19252
71124600   =   yrday
fracday
Element set:     916
Inclination:       51
6396  deg
RA of node:       302
0304  deg
Eccentricity:     
0008346     
Arg of perigee:    22
6810  deg
Mean anomaly:     337
4708  deg
Mean motion:   15
50407050  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2836
Checksum:              280
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