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

 
Date: February 6th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


037/01:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 216 1

039/16:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 215 6

040/11:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 215 5

044/15:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 7
000/00:00:00 000 0 0 0 0 215 1

Coasting Arc #1 (Orbit 3462)
---------------------------------------

Vector Time (GMT): 2019/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3167300
52                 A    =         6791913
49  meter
 Y    =       -5986717
40  meter          E    =           
0015206
 Z    =        -368643
93                 I    =           51
33256
 XDOT =       4392
050434                 Wp   =           25
88808
 YDOT =       1962
280560  meter/sec      RA   =          300
37760  deg
 ZDOT =       5975
107059                 TA   =          330
12047
                                          MA   =          330
20719
                                          Ha   =            222
984  n
mi
                                          Hp   =            216
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10391405
91                 X    =         3235800
90
 Y    =      -19641461
29  feet           Y    =        -5950915
43  meter
 Z    =       -1209461
71                 Z    =         -353092
45
 XDOT =      14409
614284                 XDOT =        4340
758321
 YDOT =       6437
928348  feet/sec       YDOT =        2011
108730  meter/sec
 ZDOT =      19603
369617                 ZDOT =        5996
316808

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21407932
70                 X    =         6525137
89
 Y    =       -5969519
86  feet           Y    =        -1819509
65  meter
 Z    =       -1138580
89                 Z    =         -347039
46
 XDOT =       4717
111713                 XDOT =        1437
775650
 YDOT =      13230
313694  feet/sec       YDOT =        4032
599614  meter/sec
 ZDOT =      19698
806039                 ZDOT =        6004
196081


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   19035
50067092  
00016717  00000-0  10270-3 0  9004
2 25544  51
6415 301
1063 0005380 349
1232  10
9803 15
53223109 34636


Satellite: ISS
Catalog Number: 25544
Epoch time:      19035
50067092   =   yrday
fracday
Element set:     900
Inclination:       51
6415  deg
RA of node:       301
1063  deg
Eccentricity:     
0005380     
Arg of perigee:   349
1232  deg
Mean anomaly:      10
9803  deg
Mean motion:   15
53223109  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3463
Checksum:              264


Coasting Arc #2 (Orbit 3478)
---------------------------------------

Vector Time (GMT): 2019/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3620337
72                 A    =         6791499
78  meter
 Y    =        5646293
53  meter          E    =           
0005605
 Z    =       -1061025
63                 I    =           51
31533
 XDOT =      -3583
458193                 Wp   =          114
04674
 YDOT =      -3393
910273  meter/sec      RA   =          295
39061  deg
 ZDOT =      -5860
510584                 TA   =           77
49980
                                          MA   =           77
43710
                                          Ha   =            223
044  n
mi
                                          Hp   =            216
137

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11877748
43                 X    =        -3678053
37
 Y    =       18524585
09  feet           Y    =         5605485
67  meter
 Z    =       -3481055
22                 Z    =        -1078751
63
 XDOT =     -11756
752601                 XDOT =       -3516
773921
 YDOT =     -11134
876224  feet/sec       YDOT =       -3433
610242  meter/sec
 ZDOT =     -19227
396929                 ZDOT =       -5877
755163

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21523929
99                 X    =        -6560493
86
 Y    =        4515942
14  feet           Y    =         1376459
16  meter
 Z    =       -3561686
41                 Z    =        -1085602
02
 XDOT =        131
754337                 XDOT =          40
158722
 YDOT =     -14529
700980  feet/sec       YDOT =       -4428
652859  meter/sec
 ZDOT =     -19304
781564                 ZDOT =       -5884
097421


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   19036
53010002  
00016717  00000-0  10270-3 0  9018
2 25544  51
6415 295
9825 0005210 351
4829   8
6234 15
53208675 34792


Satellite: ISS
Catalog Number: 25544
Epoch time:      19036
53010002   =   yrday
fracday
Element set:     901
Inclination:       51
6415  deg
RA of node:       295
9825  deg
Eccentricity:     
0005210     
Arg of perigee:   351
4829  deg
Mean anomaly:       8
6234  deg
Mean motion:   15
53208675  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3479
Checksum:              294


Coasting Arc #3 (Orbit 3487)
---------------------------------------

Vector Time (GMT): 2019/037/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4324587
68                 A    =         6780302
57  meter
 Y    =         460951
43  meter          E    =           
0003937
 Z    =        5199035
89                 I    =           51
26896
 XDOT =      -2088
017577                 Wp   =           40
15416
 YDOT =       7298
705814  meter/sec      RA   =          292
59101  deg
 ZDOT =       1092
209428                 TA   =           39
34176
                                          MA   =           39
31317
                                          Ha   =            222
862  n
mi
                                          Hp   =            216
051

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14188279
79                 X    =         4293858
47
 Y    =        1512307
85  feet           Y    =          509140
31  meter
 Z    =       17057204
36                 Z    =         5219967
87
 XDOT =      -6850
451368                 XDOT =       -2174
783776
 YDOT =      23945
885218  feet/sec       YDOT =        7274
871033  meter/sec
 ZDOT =       3583
364265                 ZDOT =        1081
855987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12274510
23                 X    =        -3741270
72
 Y    =       -7050005
28  feet           Y    =        -2148841
61  meter
 Z    =       17151571
45                 Z    =         5227798
98
 XDOT =      15416
664953                 XDOT =        4698
999478
 YDOT =     -18259
133920  feet/sec       YDOT =       -5565
384019  meter/sec
 ZDOT =       3535
805886                 ZDOT =        1077
713634


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   19037
10915057  
00016717  00000-0  10270-3 0  9027
2 25544  51
6400 293
0977 0005088 353
3260   6
7823 15
53244720 34880


Satellite: ISS
Catalog Number: 25544
Epoch time:      19037
10915057   =   yrday
fracday
Element set:     902
Inclination:       51
6400  deg
RA of node:       293
0977  deg
Eccentricity:     
0005088     
Arg of perigee:   353
3260  deg
Mean anomaly:       6
7823  deg
Mean motion:   15
53244720  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3488
Checksum:              301


Coasting Arc #4 (Orbit 3502)
---------------------------------------

Vector Time (GMT): 2019/038/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3865393
55                 A    =         6780105
44  meter
 Y    =       -1819454
74  meter          E    =           
0015104
 Z    =       -5277098
26                 I    =           51
25638
 XDOT =       2687
922434                 Wp   =           73
69042
 YDOT =      -7151
719758  meter/sec      RA   =          287
57443  deg
 ZDOT =        502
295725                 TA   =          201
10327
                                          MA   =          201
16565
                                          Ha   =            223
175  n
mi
                                          Hp   =            215
766

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12681737
36                 X    =        -3819128
08
 Y    =       -5969339
70  feet           Y    =        -1862421
80  meter
 Z    =      -17313314
51                 Z    =        -5295761
95
 XDOT =       8818
643155                 XDOT =        2765
255402
 YDOT =     -23463
647500  feet/sec       YDOT =       -7121
229117  meter/sec
 ZDOT =       1647
951853                 ZDOT =         515
540417

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9279626
91                 X    =         2828430
28
 Y    =       10364989
06  feet           Y    =         3159248
67  meter
 Z    =      -17397294
74                 Z    =        -5302695
44
 XDOT =     -16439
290090                 XDOT =       -5010
695619
 YDOT =      17556
143734  feet/sec       YDOT =        5351
112610  meter/sec
 ZDOT =       1708
512848                 ZDOT =         520
754716


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   19038
07423716  
00016717  00000-0  10270-3 0  9031
2 25544  51
6402 288
2933 0005239 358
0324   2
0806 15
53215453 35030


Satellite: ISS
Catalog Number: 25544
Epoch time:      19038
07423716   =   yrday
fracday
Element set:     903
Inclination:       51
6402  deg
RA of node:       288
2933  deg
Eccentricity:     
0005239     
Arg of perigee:   358
0324  deg
Mean anomaly:       2
0806  deg
Mean motion:   15
53215453  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3503
Checksum:              285


Coasting Arc #5 (Orbit 3518)
---------------------------------------

Vector Time (GMT): 2019/039/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3370013
39                 A    =         6781344
22  meter
 Y    =        3168427
58  meter          E    =           
0010124
 Z    =        4957041
19                 I    =           51
25085
 XDOT =      -3189
956528                 Wp   =           31
74105
 YDOT =       6657
103943  meter/sec      RA   =          282
55875  deg
 ZDOT =      -2075
989660                 TA   =           78
62765
                                          MA   =           78
51393
                                          Ha   =            223
159  n
mi
                                          Hp   =            215
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11056474
38                 X    =         3310254
69
 Y    =       10395103
61  feet           Y    =         3205779
56  meter
 Z    =       16263258
51                 Z    =         4973265
76
 XDOT =     -10465
736641                 XDOT =       -3254
077294
 YDOT =      21840
892200  feet/sec       YDOT =        6621
072989  meter/sec
 ZDOT =      -6810
989699                 ZDOT =       -2091
640997

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6312821
78                 X    =        -1924148
08
 Y    =      -13714146
42  feet           Y    =        -4180071
83  meter
 Z    =       16336090
45                 Z    =         4979240
37
 XDOT =      16774
728923                 XDOT =        5112
937376
 YDOT =     -15960
274365  feet/sec       YDOT =       -4864
691627  meter/sec
 ZDOT =      -6882
329868                 ZDOT =       -2097
734144


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   19039
10365996  
00016717  00000-0  10270-3 0  9042
2 25544  51
6391 283
1691 0005250   2
1504 357
9669 15
53259652 35197


Satellite: ISS
Catalog Number: 25544
Epoch time:      19039
10365996   =   yrday
fracday
Element set:     904
Inclination:       51
6391  deg
RA of node:       283
1691  deg
Eccentricity:     
0005250     
Arg of perigee:     2
1504  deg
Mean anomaly:     357
9669  deg
Mean motion:   15
53259652  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3519
Checksum:              323


Coasting Arc #6 (Orbit 3527)
---------------------------------------

Vector Time (GMT): 2019/039/16:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2552402
99                 A    =         6784690
17  meter
 Y    =       -4757932
05  meter          E    =           
0007976
 Z    =       -4113127
81                 I    =           51
25490
 XDOT =       3959
111464                 Wp   =           70
65105
 YDOT =      -5371
273651  meter/sec      RA   =          279
47146  deg
 ZDOT =       3765
075185                 TA   =          238
36555
                                          MA   =          238
44339
                                          Ha   =            223
242  n
mi
                                          Hp   =            215
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8374025
56                 X    =        -2479029
90
 Y    =      -15610013
28  feet           Y    =        -4786064
79  meter
 Z    =      -13494513
81                 Z    =        -4125347
67
 XDOT =      12989
210841                 XDOT =        4000
592066
 YDOT =     -17622
288881  feet/sec       YDOT =       -5326
767950  meter/sec
 ZDOT =      12352
608876                 ZDOT =        3784
407709

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13142628
74                 X    =        -4005873
24
 Y    =      -11814888
31  feet           Y    =        -3601177
96  meter
 Z    =      -13549112
35                 Z    =        -4129769
45
 XDOT =       5205
290955                 XDOT =        1586
572683
 YDOT =     -20024
508090  feet/sec       YDOT =       -6103
470066  meter/sec
 ZDOT =      12440
401034                 ZDOT =        3791
834235


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   19039
68271119  
00016717  00000-0  10270-3 0  9059
2 25544  51
6362 280
2831 0005125   4
5569 355
5629 15
53240765 35282


Satellite: ISS
Catalog Number: 25544
Epoch time:      19039
68271119   =   yrday
fracday
Element set:     905
Inclination:       51
6362  deg
RA of node:       280
2831  deg
Eccentricity:     
0005125     
Arg of perigee:     4
5569  deg
Mean anomaly:     355
5629  deg
Mean motion:   15
53240765  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3528
Checksum:              315


Coasting Arc #7 (Orbit 3540)
---------------------------------------

Vector Time (GMT): 2019/040/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3834608
29                 A    =         6780881
13  meter
 Y    =        2415043
86  meter          E    =           
0009863
 Z    =        5042260
72                 I    =           51
24372
 XDOT =      -2130
771893                 Wp   =           29
72276
 YDOT =       7145
371259  meter/sec      RA   =          275
48100  deg
 ZDOT =      -1791
975287                 TA   =           77
76940
                                          MA   =           77
65896
                                          Ha   =            223
221  n
mi
                                          Hp   =            215
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12580735
85                 X    =         3782825
55
 Y    =        7923372
26  feet           Y    =         2457635
91  meter
 Z    =       16542850
13                 Z    =         5060761
54
 XDOT =      -6990
721433                 XDOT =       -2201
810831
 YDOT =      23442
819092  feet/sec       YDOT =        7121
146167  meter/sec
 ZDOT =      -5879
184014                 ZDOT =       -1802
498560

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1690914
75                 X    =          515390
82
 Y    =       14677744
25  feet           Y    =         4473776
45  meter
 Z    =       16626041
74                 Z    =         5067617
52
 XDOT =     -21521
214446                 XDOT =       -6559
666163
 YDOT =       9230
258165  feet/sec       YDOT =        2813
382689  meter/sec
 ZDOT =      -5927
419684                 ZDOT =       -1806
677520


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   19040
51911462  
00016717  00000-0  10270-3 0  9066
2 25544  51
6410 276
1237 0005494   4
5406 355
5795 15
53288655 35418


Satellite: ISS
Catalog Number: 25544
Epoch time:      19040
51911462   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:       276
1237  deg
Eccentricity:     
0005494     
Arg of perigee:     4
5406  deg
Mean anomaly:     355
5795  deg
Mean motion:   15
53288655  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3541
Checksum:              308


Coasting Arc #8 (Orbit 3555)
---------------------------------------

Vector Time (GMT): 2019/041/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3544241
93                 A    =         6783388
92  meter
 Y    =       -3699195
13  meter          E    =           
0009906
 Z    =       -4453357
74                 I    =           51
24945
 XDOT =       2647
723596                 Wp   =           77
09969
 YDOT =      -6419
744144  meter/sec      RA   =          270
46690  deg
 ZDOT =       3233
641036                 TA   =          225
63035
                                          MA   =          225
71154
                                          Ha   =            223
433  n
mi
                                          Hp   =            215
359

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11628090
31                 X    =        -3480981
46
 Y    =      -12136466
95  feet           Y    =        -3738475
86  meter
 Z    =      -14610753
74                 Z    =        -4470420
21
 XDOT =       8686
757205                 XDOT =        2703
607212
 YDOT =     -21062
152704  feet/sec       YDOT =       -6389
822796  meter/sec
 ZDOT =      10609
058518                 ZDOT =        3246
638592

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1888447
46                 X    =          575598
79
 Y    =      -16634199
41  feet           Y    =        -5070103
98  meter
 Z    =      -14687328
39                 Z    =        -4476697
69
 XDOT =      20459
860321                 XDOT =        6236
165426
 YDOT =      -7073
123156  feet/sec       YDOT =       -2155
887938  meter/sec
 ZDOT =      10668
361637                 ZDOT =        3251
716627


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   19041
48419605  
00016717  00000-0  10270-3 0  9076
2 25544  51
6408 271
3187 0005571   8
6557 351
4690 15
53255092 35568


Satellite: ISS
Catalog Number: 25544
Epoch time:      19041
48419605   =   yrday
fracday
Element set:     907
Inclination:       51
6408  deg
RA of node:       271
3187  deg
Eccentricity:     
0005571     
Arg of perigee:     8
6557  deg
Mean anomaly:     351
4690  deg
Mean motion:   15
53255092  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3556
Checksum:              318


Coasting Arc #9 (Orbit 3571)
---------------------------------------

Vector Time (GMT): 2019/042/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3210574
11                 A    =         6786509
40  meter
 Y    =        4834533
37  meter          E    =           
0014688
 Z    =        3512194
27                 I    =           51
26035
 XDOT =      -3169
289664                 Wp   =           65
84202
 YDOT =       5365
172248  meter/sec      RA   =          265
45964  deg
 ZDOT =      -4467
296149                 TA   =           72
56840
                                          MA   =           72
40787
                                          Ha   =            223
547  n
mi
                                          Hp   =            215
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10533379
62                 X    =         3139214
30
 Y    =       15861329
96  feet           Y    =         4870037
43  meter
 Z    =       11522947
08                 Z    =         3527616
28
 XDOT =     -10397
931967                 XDOT =       -3207
349617
 YDOT =      17602
271155  feet/sec       YDOT =        5329
518012  meter/sec
 ZDOT =     -14656
483429                 ZDOT =       -4482
783879

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5118309
76                 X    =        -1560060
82
 Y    =       18295909
11  feet           Y    =         5576593
10  meter
 Z    =       11592014
44                 Z    =         3533246
00
 XDOT =     -18708
294681                 XDOT =       -5702
288219
 YDOT =       4139
927982  feet/sec       YDOT =        1261
850049  meter/sec
 ZDOT =     -14726
897665                 ZDOT =       -4488
758408


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   19042
51361357  
00016717  00000-0  10270-3 0  9082
2 25544  51
6402 266
1936 0005702  12
8847 347
2450 15
53280812 35724


Satellite: ISS
Catalog Number: 25544
Epoch time:      19042
51361357   =   yrday
fracday
Element set:     908
Inclination:       51
6402  deg
RA of node:       266
1936  deg
Eccentricity:     
0005702     
Arg of perigee:    12
8847  deg
Mean anomaly:     347
2450  deg
Mean motion:   15
53280812  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3572
Checksum:              300


Coasting Arc #10 (Orbit 3586)
---------------------------------------

Vector Time (GMT): 2019/043/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2868865
04                 A    =         6789528
92  meter
 Y    =       -5680812
95  meter          E    =           
0010861
 Z    =       -2353929
42                 I    =           51
27347
 XDOT =       3674
513425                 Wp   =           30
52894
 YDOT =      -4068
180602  meter/sec      RA   =          260
45972  deg
 ZDOT =       5359
638343                 TA   =          303
06878
                                          MA   =          303
17303
                                          Ha   =            223
611  n
mi
                                          Hp   =            215
244

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9412286
88                 X    =        -2793693
42
 Y    =      -18637837
77  feet           Y    =        -5712474
37  meter
 Z    =       -7722865
55                 Z    =        -2367682
36
 XDOT =      12055
490238                 XDOT =        3693
698020
 YDOT =     -13347
049218  feet/sec       YDOT =       -4026
982172  meter/sec
 ZDOT =      17584
115297                 ZDOT =        5377
534287

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7599781
32                 X    =         2316413
35
 Y    =      -19422932
75  feet           Y    =        -5920109
90  meter
 Z    =       -7784330
46                 Z    =        -2372663
92
 XDOT =      16489
417093                 XDOT =        5025
974330
 YDOT =       -601
703977  feet/sec       YDOT =        -183
399372  meter/sec
 ZDOT =      17665
253734                 ZDOT =        5384
369338


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   19043
47869224  
00016717  00000-0  10270-3 0  9095
2 25544  51
6399 261
3891 0005631  14
7718 345
3597 15
53238269 35871


Satellite: ISS
Catalog Number: 25544
Epoch time:      19043
47869224   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       261
3891  deg
Eccentricity:     
0005631     
Arg of perigee:    14
7718  deg
Mean anomaly:     345
3597  deg
Mean motion:   15
53238269  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3587
Checksum:              350


Coasting Arc #11 (Orbit 3602)
---------------------------------------

Vector Time (GMT): 2019/044/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2436160
92                 A    =         6791490
70  meter
 Y    =        6259441
12  meter          E    =           
0013285
 Z    =         982306
76                 I    =           51
28721
 XDOT =      -4199
578045                 Wp   =          100
25448
 YDOT =       2566
836586  meter/sec      RA   =          255
46574  deg
 ZDOT =      -5875
544772                 TA   =           69
05801
                                          MA   =           68
91588
                                          Ha   =            223
754  n
mi
                                          Hp   =            215
104

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7992653
93                 X    =         2361213
58
 Y    =       20536224
16  feet           Y    =         6286264
94  meter
 Z    =        3222791
20                 Z    =          993958
43
 XDOT =     -13778
143192                 XDOT =       -4199
429215
 YDOT =       8421
379876  feet/sec       YDOT =        2519
874698  meter/sec
 ZDOT =     -19276
721694                 ZDOT =       -5895
944196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9600608
49                 X    =        -2926265
47
 Y    =       19826997
69  feet           Y    =         6043268
90  meter
 Z    =        3274733
87                 Z    =          998138
88
 XDOT =     -14017
055702                 XDOT =       -4272
398578
 YDOT =      -3553
204205  feet/sec       YDOT =       -1083
016642  meter/sec
 ZDOT =     -19369
002038                 ZDOT =       -5903
671821


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   19044
50810728  
00016717  00000-0  10270-3 0  9107
2 25544  51
6405 256
2636 0005596  19
7238 340
4129 15
53240048 36035


Satellite: ISS
Catalog Number: 25544
Epoch time:      19044
50810728   =   yrday
fracday
Element set:     910
Inclination:       51
6405  deg
RA of node:       256
2636  deg
Eccentricity:     
0005596     
Arg of perigee:    19
7238  deg
Mean anomaly:     340
4129  deg
Mean motion:   15
53240048  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3603
Checksum:              296


Coasting Arc #12 (Orbit 3605)
---------------------------------------

Vector Time (GMT): 2019/044/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4437334
31                 A    =         6783126
22  meter
 Y    =        2390544
90  meter          E    =           
0012997
 Z    =        4534821
89                 I    =           51
25756
 XDOT =       -618
592124                 Wp   =           51
22312
 YDOT =       7000
242400  meter/sec      RA   =          254
52448  deg
 ZDOT =      -3070
930321                 TA   =           69
73630
                                          MA   =           69
59663
                                          Ha   =            223
655  n
mi
                                          Hp   =            215
069

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14558183
43                 X    =         4388245
39
 Y    =        7842995
07  feet           Y    =         2439891
86  meter
 Z    =       14878024
59                 Z    =         4556257
28
 XDOT =      -2029
501718                 XDOT =        -681
908138
 YDOT =      22966
674542  feet/sec       YDOT =        6992
970803  meter/sec
 ZDOT =     -10075
230711                 ZDOT =       -3074
089061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16247753
50                 X    =         4952315
27
 Y    =        2565944
10  feet           Y    =          782099
76  meter
 Z    =       14974489
28                 Z    =         4564224
33
 XDOT =       6006
323713                 XDOT =        1830
727468
 YDOT =      21118
165531  feet/sec       YDOT =        6436
816854  meter/sec
 ZDOT =     -10090
172010                 ZDOT =       -3075
484429


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   19044
70112389  
00016717  00000-0  10270-3 0  9118
2 25544  51
6374 255
2972 0005210  24
9586 335
1817 15
53224674 36064


Satellite: ISS
Catalog Number: 25544
Epoch time:      19044
70112389   =   yrday
fracday
Element set:     911
Inclination:       51
6374  deg
RA of node:       255
2972  deg
Eccentricity:     
0005210     
Arg of perigee:    24
9586  deg
Mean anomaly:     335
1817  deg
Mean motion:   15
53224674  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3606
Checksum:              306


Coasting Arc #13 (Orbit 3620)
---------------------------------------

Vector Time (GMT): 2019/045/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4467759
35                 A    =         6786095
79  meter
 Y    =       -3560322
29  meter          E    =           
0008803
 Z    =       -3666307
06                 I    =           51
27822
 XDOT =       1388
241384                 Wp   =           66
04526
 YDOT =      -6175
603226  meter/sec      RA   =          249
51848  deg
 ZDOT =       4317
119474                 TA   =          250
14443
                                          MA   =          250
23933
                                          Ha   =            223
718  n
mi
                                          Hp   =            214
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14658003
13                 X    =        -4409806
14
 Y    =      -11680847
42  feet           Y    =        -3609959
86  meter
 Z    =      -12028566
46                 Z    =        -3687868
70
 XDOT =       4554
597716                 XDOT =        1436
225674
 YDOT =     -20261
165438  feet/sec       YDOT =       -6159
810646  meter/sec
 ZDOT =      14163
777803                 ZDOT =        4323
979477

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17744316
12                 X    =        -5408467
55
 Y    =       -5839276
55  feet           Y    =        -1779811
49  meter
 Z    =      -12125500
32                 Z    =        -3695852
50
 XDOT =      -3340
912667                 XDOT =       -1018
310181
 YDOT =     -19245
457260  feet/sec       YDOT =       -5866
015373  meter/sec
 ZDOT =      14195
325658                 ZDOT =        4326
735261


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   19045
66619744  
00016717  00000-0  10270-3 0  9122
2 25544  51
6379 250
4936 0005260  27
9732 332
1702 15
53251022 36211


Satellite: ISS
Catalog Number: 25544
Epoch time:      19045
66619744   =   yrday
fracday
Element set:     912
Inclination:       51
6379  deg
RA of node:       250
4936  deg
Eccentricity:     
0005260     
Arg of perigee:    27
9732  deg
Mean anomaly:     332
1702  deg
Mean motion:   15
53251022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3621
Checksum:              297


Coasting Arc #14 (Orbit 3636)
---------------------------------------

Vector Time (GMT): 2019/046/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4377529
90                 A    =         6789201
78  meter
 Y    =        4545329
22  meter          E    =           
0015952
 Z    =        2491822
83                 I    =           51
30059
 XDOT =      -2258
985201                 Wp   =           86
48581
 YDOT =       5084
472843  meter/sec      RA   =          244
51919  deg
 ZDOT =      -5275
817021                 TA   =           65
44111
                                          MA   =           65
27493
                                          Ha   =            223
775  n
mi
                                          Hp   =            214
865

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14361974
74                 X    =         4314273
73
 Y    =       14912497
45  feet           Y    =         4593928
10  meter
 Z    =        8175271
75                 Z    =         2512933
25
 XDOT =      -7411
368769                 XDOT =       -2290
046794
 YDOT =      16681
341348  feet/sec       YDOT =        5059
037668  meter/sec
 ZDOT =     -17309
110962                 ZDOT =       -5286
865520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18773782
24                 X    =         5722248
83
 Y    =        8639132
44  feet           Y    =         2633207
57  meter
 Z    =        8270094
18                 Z    =         2520724
71
 XDOT =        -51
602109                 XDOT =         -15
728323
 YDOT =      16824
014713  feet/sec       YDOT =        5127
959685  meter/sec
 ZDOT =     -17359
444531                 ZDOT =       -5291
158693


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   19046
69560899  
00016717  00000-0  10270-3 0  9133
2 25544  51
6373 245
3681 0005165  31
1858 328
9600 15
53248252 36373


Satellite: ISS
Catalog Number: 25544
Epoch time:      19046
69560899   =   yrday
fracday
Element set:     913
Inclination:       51
6373  deg
RA of node:       245
3681  deg
Eccentricity:     
0005165     
Arg of perigee:    31
1858  deg
Mean anomaly:     328
9600  deg
Mean motion:   15
53248252  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3637
Checksum:              330


Coasting Arc #15 (Orbit 3651)
---------------------------------------

Vector Time (GMT): 2019/047/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4168488
74                 A    =         6791237
74  meter
 Y    =       -5221653
52  meter          E    =           
0014445
 Z    =       -1180138
68                 I    =           51
32417
 XDOT =       3165
074823                 Wp   =           36
84611
 YDOT =      -3835
084751  meter/sec      RA   =          239
52729  deg
 ZDOT =       5837
608568                 TA   =          310
28051
                                          MA   =          310
40671
                                          Ha   =            223
829  n
mi
                                          Hp   =            214
761

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13676144
17                 X    =        -4104056
61
 Y    =      -17131409
20  feet           Y    =        -5267908
20  meter
 Z    =       -3871846
05                 Z    =        -1200230
72
 XDOT =      10384
103749                 XDOT =        3179
369381
 YDOT =     -12582
299053  feet/sec       YDOT =       -3799
610796  meter/sec
 ZDOT =      19152
259081                 ZDOT =        5853
017650

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19160140
62                 X    =        -5840010
86
 Y    =      -10616242
29  feet           Y    =        -3235830
65  meter
 Z    =       -3962032
76                 Z    =        -1207627
59
 XDOT =       3896
364525                 XDOT =        1187
611907
 YDOT =     -14147
858159  feet/sec       YDOT =       -4312
267167  meter/sec
 ZDOT =      19222
148651                 ZDOT =        5858
910909


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   19047
66067990  
00016717  00000-0  10270-3 0  9146
2 25544  51
6387 240
5636 0005298  34
2830 325
8664 15
53259027 36521


Satellite: ISS
Catalog Number: 25544
Epoch time:      19047
66067990   =   yrday
fracday
Element set:     914
Inclination:       51
6387  deg
RA of node:       240
5636  deg
Eccentricity:     
0005298     
Arg of perigee:    34
2830  deg
Mean anomaly:     325
8664  deg
Mean motion:   15
53259027  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3652
Checksum:              331


Coasting Arc #16 (Orbit 3667)
---------------------------------------

Vector Time (GMT): 2019/048/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3759549
78                 A    =         6791781
66  meter
 Y    =        5646996
15  meter          E    =           
0012033
 Z    =        -267296
10                 I    =           51
34308
 XDOT =      -4113
562523                 Wp   =          110
70044
 YDOT =       2466
270596  meter/sec      RA   =          234
53976  deg
 ZDOT =      -5977
303401                 TA   =           72
18945
                                          MA   =           72
05820
                                          Ha   =            223
933  n
mi
                                          Hp   =            214
638

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12334480
90                 X    =         3697422
40
 Y    =       18526890
26  feet           Y    =         5688690
68  meter
 Z    =        -876955
71                 Z    =         -249185
06
 XDOT =     -13495
940037                 XDOT =       -4111
801717
 YDOT =       8091
438964  feet/sec       YDOT =        2420
279669  meter/sec
 ZDOT =     -19610
575464                 ZDOT =       -5997
280734

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18693398
13                 X    =         5697747
75
 Y    =       12086265
98  feet           Y    =         3683893
87  meter
 Z    =        -795722
35                 Z    =         -242536
17
 XDOT =      -8160
115314                 XDOT =       -2487
203148
 YDOT =      11376
978257  feet/sec       YDOT =        3467
702973  meter/sec
 ZDOT =     -19700
957834                 ZDOT =       -6004
851948


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   19048
69008663  
00016717  00000-0  10270-3 0  9153
2 25544  51
6378 235
4383 0005348  37
9934 322
1595 15
53275232 36680


Satellite: ISS
Catalog Number: 25544
Epoch time:      19048
69008663   =   yrday
fracday
Element set:     915
Inclination:       51
6378  deg
RA of node:       235
4383  deg
Eccentricity:     
0005348     
Arg of perigee:    37
9934  deg
Mean anomaly:     322
1595  deg
Mean motion:   15
53275232  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3668
Checksum:              337


Coasting Arc #17 (Orbit 3683)
---------------------------------------

Vector Time (GMT): 2019/049/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3178119
28                 A    =         6790692
67  meter
 Y    =       -5758723
51  meter          E    =           
0018993
 Z    =        1647893
27                 I    =           51
36000
 XDOT =       5018
092978                 Wp   =           57
92863
 YDOT =      -1129
248608  meter/sec      RA   =          229
55291  deg
 ZDOT =       5693
272581                 TA   =          320
19913
                                          MA   =          320
33830
                                          Ha   =            223
974  n
mi
                                          Hp   =            214
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10426900
52                 X    =        -3121491
71
 Y    =      -18893449
83  feet           Y    =        -5793946
78  meter
 Z    =        5406473
99                 Z    =         1632593
37
 XDOT =      16463
559640                 XDOT =        5002
693696
 YDOT =      -3704
883886  feet/sec       YDOT =       -1073
218693  meter/sec
 ZDOT =      18678
715817                 ZDOT =        5717
610485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17340927
66                 X    =        -5285514
75
 Y    =      -12872900
83  feet           Y    =        -3923660
17  meter
 Z    =        5337912
92                 Z    =         1626995
86
 XDOT =      12404
188425                 XDOT =        3780
796632
 YDOT =      -8865
755488  feet/sec       YDOT =       -2702
282273  meter/sec
 ZDOT =      18788
667960                 ZDOT =        5726
785994


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   19049
71949236  
00016717  00000-0  10270-3 0  9168
2 25544  51
6383 230
3135 0005333  42
5697 317
5868 15
53276391 36843


Satellite: ISS
Catalog Number: 25544
Epoch time:      19049
71949236   =   yrday
fracday
Element set:     916
Inclination:       51
6383  deg
RA of node:       230
3135  deg
Eccentricity:     
0005333     
Arg of perigee:    42
5697  deg
Mean anomaly:     317
5868  deg
Mean motion:   15
53276391  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3684
Checksum:              335
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