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

 
Date: April 19th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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


114/10:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 217 2

116/09:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 5

118/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 4

118/11:34:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 5

Coasting Arc #1 (Orbit 612)
---------------------------------------

Vector Time (GMT): 2019/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944647
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1986598
64                 A    =         6785271
84  meter
 Y    =       -4685918
21  meter          E    =           
0009527
 Z    =       -4497015
99                 I    =           51
27396
 XDOT =       4795
913072                 Wp   =          118
90070
 YDOT =      -5064
675275  meter/sec      RA   =          292
14065  deg
 ZDOT =       3159
365554                 TA   =          183
02578
                                          MA   =          183
03155
                                          Ha   =            223
268  n
mi
                                          Hp   =            217
273

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6517712
09                 X    =        -1912207
40
 Y    =      -15373747
39  feet           Y    =        -4707718
08  meter
 Z    =      -14753989
48                 Z    =        -4506485
31
 XDOT =      15734
622941                 XDOT =        4836
844600
 YDOT =     -16616
388696  feet/sec       YDOT =       -5010
814955  meter/sec
 ZDOT =      10365
372551                 ZDOT =        3182
762375

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12588395
10                 X    =        -3836942
83
 Y    =      -10913964
98  feet           Y    =        -3326576
53  meter
 Z    =      -14796302
33                 Z    =        -4509912
95
 XDOT =       5841
552735                 XDOT =        1780
505274
 YDOT =     -20931
825101  feet/sec       YDOT =       -6380
020291  meter/sec
 ZDOT =      10471
643940                 ZDOT =        3191
757073


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   19109
51036417  
00016717  00000-0  10270-3 0  9004
2 25544  51
6370 292
8820 0001448 207
3206 152
7870 15
52570009  6136


Satellite: ISS
Catalog Number: 25544
Epoch time:      19109
51036417   =   yrday
fracday
Element set:     900
Inclination:       51
6370  deg
RA of node:       292
8820  deg
Eccentricity:     
0001448     
Arg of perigee:   207
3206  deg
Mean anomaly:     152
7870  deg
Mean motion:   15
52570009  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             613
Checksum:              284


Coasting Arc #2 (Orbit 628)
---------------------------------------

Vector Time (GMT): 2019/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944647
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1452764
89                 A    =         6787911
18  meter
 Y    =        5468509
85  meter          E    =           
0010696
 Z    =        3740537
88                 I    =           51
27160
 XDOT =      -4839
134414                 Wp   =           89
41651
 YDOT =       4185
036106  meter/sec      RA   =          287
13912  deg
 ZDOT =      -4228
286804                 TA   =           45
59976
                                          MA   =           45
51225
                                          Ha   =            223
145  n
mi
                                          Hp   =            217
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4766289
03                 X    =         1373336
73
 Y    =       17941305
27  feet           Y    =         5484311
72  meter
 Z    =       12272105
92                 Z    =         3747401
86
 XDOT =     -15876
425244                 XDOT =       -4865
034007
 YDOT =      13730
433420  feet/sec       YDOT =        4130
776539  meter/sec
 ZDOT =     -13872
332033                 ZDOT =       -4251
856969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12415685
83                 X    =         3784301
04
 Y    =       13773528
19  feet           Y    =         4198171
39  meter
 Z    =       12302568
68                 Z    =         3749822
93
 XDOT =      -6689
500122                 XDOT =       -2038
959637
 YDOT =      18547
421423  feet/sec       YDOT =        5653
254050  meter/sec
 ZDOT =     -13979
288923                 ZDOT =       -4260
887264


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   19110
54023024  
00016717  00000-0  10270-3 0  9010
2 25544  51
6373 287
7594 0001440 215
9681 144
1374 15
52568973  6292


Satellite: ISS
Catalog Number: 25544
Epoch time:      19110
54023024   =   yrday
fracday
Element set:     901
Inclination:       51
6373  deg
RA of node:       287
7594  deg
Eccentricity:     
0001440     
Arg of perigee:   215
9681  deg
Mean anomaly:     144
1374  deg
Mean motion:   15
52568973  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             629
Checksum:              306


Coasting Arc #3 (Orbit 643)
---------------------------------------

Vector Time (GMT): 2019/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944647
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -997748
20                 A    =         6790481
17  meter
 Y    =       -6098774
85  meter          E    =           
0003579
 Z    =       -2815820
39                 I    =           51
27122
 XDOT =       4825
863855                 Wp   =           73
31329
 YDOT =      -3124
352582  meter/sec      RA   =          282
14205  deg
 ZDOT =       5063
419013                 TA   =          254
57981
                                          MA   =          254
61935
                                          Ha   =            223
254  n
mi
                                          Hp   =            217
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3273452
09                 X    =         -915797
89
 Y    =      -20009103
84  feet           Y    =        -6109474
19  meter
 Z    =       -9238255
88                 Z    =        -2820468
04
 XDOT =      15832
886664                 XDOT =        4835
846895
 YDOT =     -10250
500597  feet/sec       YDOT =       -3070
330516  meter/sec
 ZDOT =      16612
267102                 ZDOT =        5086
885927

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12338313
74                 X    =        -3760718
03
 Y    =      -16076958
90  feet           Y    =        -4900257
07  meter
 Z    =       -9258644
78                 Z    =        -2822034
93
 XDOT =       7785
834855                 XDOT =        2373
122464
 YDOT =     -15591
433588  feet/sec       YDOT =       -4752
268958  meter/sec
 ZDOT =      16718
645834                 ZDOT =        5095
843250


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   19111
50572992  
00016717  00000-0  10270-3 0  9021
2 25544  51
6371 282
9572 0001424 208
0804 152
0271 15
52573533  6444


Satellite: ISS
Catalog Number: 25544
Epoch time:      19111
50572992   =   yrday
fracday
Element set:     902
Inclination:       51
6371  deg
RA of node:       282
9572  deg
Eccentricity:     
0001424     
Arg of perigee:   208
0804  deg
Mean anomaly:     152
0271  deg
Mean motion:   15
52573533  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             644
Checksum:              289


Coasting Arc #4 (Orbit 659)
---------------------------------------

Vector Time (GMT): 2019/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944647
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         568636
81                 A    =         6792539
86  meter
 Y    =        6539558
13  meter          E    =           
0013594
 Z    =        1718514
95                 I    =           51
27241
 XDOT =      -4811
655968                 Wp   =          121
07167
 YDOT =       1911
825580  meter/sec      RA   =          277
14975  deg
 ZDOT =      -5656
630905                 TA   =           39
98431
                                          MA   =           39
88429
                                          Ha   =            223
083  n
mi
                                          Hp   =            217
408

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1865606
32                 X    =          487119
63
 Y    =       21455243
20  feet           Y    =         6545461
21  meter
 Z    =        5638172
41                 Z    =         1721079
30
 XDOT =     -15786
272861                 XDOT =       -4805
199757
 YDOT =       6272
393635  feet/sec       YDOT =        1858
054441  meter/sec
 ZDOT =     -18558
500344                 ZDOT =       -5679
988766

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12116391
99                 X    =         3693076
28
 Y    =       17801054
33  feet           Y    =         5425761
36  meter
 Z    =        5649110
16                 Z    =         1721848
78
 XDOT =      -9274
377179                 XDOT =       -2826
830164
 YDOT =      12263
161791  feet/sec       YDOT =        3737
811714  meter/sec
 ZDOT =     -18664
264143                 ZDOT =       -5688
867711


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   19112
53559226  
00016717  00000-0  10270-3 0  9031
2 25544  51
6371 277
8351 0001420 222
0970 138
0073 15
52594629  6609


Satellite: ISS
Catalog Number: 25544
Epoch time:      19112
53559226   =   yrday
fracday
Element set:     903
Inclination:       51
6371  deg
RA of node:       277
8351  deg
Eccentricity:     
0001420     
Arg of perigee:   222
0970  deg
Mean anomaly:     138
0073  deg
Mean motion:   15
52594629  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             660
Checksum:              294


Coasting Arc #5 (Orbit 674)
---------------------------------------

Vector Time (GMT): 2019/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944647
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -195668
06                 A    =         6793675
52  meter
 Y    =       -6763257
67  meter          E    =           
0009485
 Z    =        -561703
21                 I    =           51
27488
 XDOT =       4795
249140                 Wp   =           41
94610
 YDOT =       -627
165848  meter/sec      RA   =          272
15980  deg
 ZDOT =       5946
351320                 TA   =          311
96644
                                          MA   =          312
04722
                                          Ha   =            223
171  n
mi
                                          Hp   =            217
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -641955
59                 X    =         -117296
38
 Y    =      -22189165
58  feet           Y    =        -6765007
55  meter
 Z    =       -1842858
30                 Z    =         -562463
53
 XDOT =      15732
444684                 XDOT =        4773
021492
 YDOT =      -2057
630736  feet/sec       YDOT =        -573
666458  meter/sec
 ZDOT =      19509
026639                 ZDOT =        5969
591105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11757687
62                 X    =        -3583743
19
 Y    =      -18828641
24  feet           Y    =        -5738969
85  meter
 Z    =       -1845630
97                 Z    =         -562548
32
 XDOT =      11049
957609                 XDOT =        3368
027079
 YDOT =      -8801
888838  feet/sec       YDOT =       -2682
815718  meter/sec
 ZDOT =      19614
132571                 ZDOT =        5978
387608


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   19113
50108790  
00016717  00000-0  10270-3 0  9046
2 25544  51
6389 273
0330 0001396 215
3510 144
7549 15
52587374  6757


Satellite: ISS
Catalog Number: 25544
Epoch time:      19113
50108790   =   yrday
fracday
Element set:     904
Inclination:       51
6389  deg
RA of node:       273
0330  deg
Eccentricity:     
0001396     
Arg of perigee:   215
3510  deg
Mean anomaly:     144
7549  deg
Mean motion:   15
52587374  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             675
Checksum:              307


Coasting Arc #6 (Orbit 689)
---------------------------------------

Vector Time (GMT): 2019/114/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944647
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4042791
69                 A    =         6782567
98  meter
 Y    =        1852251
80  meter          E    =           
0012820
 Z    =       -5132792
71                 I    =           51
23632
 XDOT =      -1509
681752                 Wp   =           81
97765
 YDOT =      -7360
896910  meter/sec      RA   =          267
43902  deg
 ZDOT =      -1468
620910                 TA   =          173
78906
                                          MA   =          173
77315
                                          Ha   =            223
158  n
mi
                                          Hp   =            217
205

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13263752
26                 X    =        -4038271
17
 Y    =        6076941
61  feet           Y    =         1807067
91  meter
 Z    =      -16839871
09                 Z    =        -5152420
19
 XDOT =      -4953
024120                 XDOT =       -1420
124105
 YDOT =     -24149
924245  feet/sec       YDOT =       -7377
278433  meter/sec
 ZDOT =      -4818
310072                 ZDOT =       -1475
737147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11517410
93                 X    =        -3510506
85
 Y    =        8786554
75  feet           Y    =         2678141
89  meter
 Z    =      -16928771
45                 Z    =        -5159889
54
 XDOT =      -9406
853170                 XDOT =       -2867
208846
 YDOT =     -21665
543364  feet/sec       YDOT =       -6603
657617  meter/sec
 ZDOT =      -4849
768075                 ZDOT =       -1478
209309


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   19114
46657975  
00016717  00000-0  10270-3 0  9057
2 25544  51
6376 268
2324 0001169 221
1919 138
9145 15
52588534  6901


Satellite: ISS
Catalog Number: 25544
Epoch time:      19114
46657975   =   yrday
fracday
Element set:     905
Inclination:       51
6376  deg
RA of node:       268
2324  deg
Eccentricity:     
0001169     
Arg of perigee:   221
1919  deg
Mean anomaly:     138
9145  deg
Mean motion:   15
52588534  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             690
Checksum:              332


Coasting Arc #7 (Orbit 705)
---------------------------------------

Vector Time (GMT): 2019/115/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944647
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4188697
99                 A    =         6781975
31  meter
 Y    =        -702305
31  meter          E    =           
0001928
 Z    =        5286057
44                 I    =           51
23544
 XDOT =       1110
864657                 Wp   =          124
70974
 YDOT =       7585
636149  meter/sec      RA   =          262
42758  deg
 ZDOT =        126
459978                 TA   =          324
07176
                                          MA   =          324
08473
                                          Ha   =            223
056  n
mi
                                          Hp   =            217
462

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13742447
48                 X    =         4170563
20
 Y    =       -2304151
29  feet           Y    =         -655565
90  meter
 Z    =       17342708
12                 Z    =         5306360
60
 XDOT =       3644
569085                 XDOT =        1025
343080
 YDOT =      24887
257708  feet/sec       YDOT =        7597
580431  meter/sec
 ZDOT =        414
894941                 ZDOT =         131
648663

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12709208
16                 X    =         3873766
65
 Y    =       -5426395
76  feet           Y    =        -1653965
43  meter
 Z    =       17434556
44                 Z    =         5314052
80
 XDOT =       8966
479294                 XDOT =        2732
982889
 YDOT =      22418
223149  feet/sec       YDOT =        6833
074416  meter/sec
 ZDOT =        437
636224                 ZDOT =         133
391521


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   19115
49643781  
00016717  00000-0  10270-3 0  9062
2 25544  51
6365 263
1101 0001176 225
5118 134
5938 15
52542489  7062


Satellite: ISS
Catalog Number: 25544
Epoch time:      19115
49643781   =   yrday
fracday
Element set:     906
Inclination:       51
6365  deg
RA of node:       263
1101  deg
Eccentricity:     
0001176     
Arg of perigee:   225
5118  deg
Mean anomaly:     134
5938  deg
Mean motion:   15
52542489  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             706
Checksum:              308


Coasting Arc #8 (Orbit 720)
---------------------------------------

Vector Time (GMT): 2019/116/09:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944647
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4082949
18                 A    =         6781973
22  meter
 Y    =       -1182590
18  meter          E    =           
0001856
 Z    =        5283292
87                 I    =           51
24115
 XDOT =       1836
678062                 Wp   =          128
14393
 YDOT =       7440
216816  meter/sec      RA   =          257
60290  deg
 ZDOT =        244
809107                 TA   =          319
50255
                                          MA   =          319
51636
                                          Ha   =            222
981  n
mi
                                          Hp   =            217
511

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13395502
55                 X    =         4070206
41
 Y    =       -3879889
05  feet           Y    =        -1137003
14  meter
 Z    =       17333638
01                 Z    =         5303095
39
 XDOT =       6025
846659                 XDOT =        1752
153786
 YDOT =      24410
160157  feet/sec       YDOT =        7460
283226  meter/sec
 ZDOT =        803
179485                 ZDOT =         253
525877

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13137181
55                 X    =         4004212
94
 Y    =       -4334985
80  feet           Y    =        -1321303
67  meter
 Z    =       17423271
60                 Z    =         5310613
18
 XDOT =       6543
609033                 XDOT =        1994
492033
 YDOT =      23229
771977  feet/sec       YDOT =        7080
434499  meter/sec
 ZDOT =        841
903052                 ZDOT =         256
612050


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   19116
46192531  
00016717  00000-0  10270-3 0  9073
2 25544  51
6369 258
3087 0001174 237
8725 122
2313 15
52548688  7218


Satellite: ISS
Catalog Number: 25544
Epoch time:      19116
46192531   =   yrday
fracday
Element set:     907
Inclination:       51
6369  deg
RA of node:       258
3087  deg
Eccentricity:     
0001174     
Arg of perigee:   237
8725  deg
Mean anomaly:     122
2313  deg
Mean motion:   15
52548688  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             721
Checksum:              315


Coasting Arc #9 (Orbit 735)
---------------------------------------

Vector Time (GMT): 2019/117/09:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944647
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4363532
84                 A    =         6782214
73  meter
 Y    =          42227
06  meter          E    =           
0013451
 Z    =       -5203848
83                 I    =           51
25150
 XDOT =      -1398
707860                 Wp   =          101
80423
 YDOT =      -7444
477696  meter/sec      RA   =          252
59180  deg
 ZDOT =       1112
185322                 TA   =          178
93229
                                          MA   =          178
92941
                                          Ha   =            223
086  n
mi
                                          Hp   =            217
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14316052
61                 X    =        -4338403
27
 Y    =         138540
22  feet           Y    =           -6428
47  meter
 Z    =      -17072994
85                 Z    =        -5224984
24
 XDOT =      -4588
936548                 XDOT =       -1320
760027
 YDOT =     -24424
139424  feet/sec       YDOT =       -7459
683202  meter/sec
 ZDOT =       3648
901974                 ZDOT =        1105
580168

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14175208
67                 X    =        -4320603
60
 Y    =         871698
28  feet           Y    =          265693
64  meter
 Z    =      -17168555
85                 Z    =        -5232975
82
 XDOT =      -5806
749548                 XDOT =       -1769
897262
 YDOT =     -23118
937115  feet/sec       YDOT =       -7046
652033  meter/sec
 ZDOT =       3619
704691                 ZDOT =        1103
285990


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   19117
42740939  
00016717  00000-0  10270-3 0  9082
2 25544  51
6377 253
5066 0001093 235
3398 124
7651 15
52600220  7369


Satellite: ISS
Catalog Number: 25544
Epoch time:      19117
42740939   =   yrday
fracday
Element set:     908
Inclination:       51
6377  deg
RA of node:       253
5066  deg
Eccentricity:     
0001093     
Arg of perigee:   235
3398  deg
Mean anomaly:     124
7651  deg
Mean motion:   15
52600220  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             736
Checksum:              305


Coasting Arc #10 (Orbit 751)
---------------------------------------

Vector Time (GMT): 2019/118/09:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944647
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4633604
63                 A    =         6783840
91  meter
 Y    =        1057744
25  meter          E    =           
0005827
 Z    =        4837319
79                 I    =           51
26629
 XDOT =        881
176505                 Wp   =           60
11668
 YDOT =       7223
059435  meter/sec      RA   =          247
58314  deg
 ZDOT =      -2418
435171                 TA   =           53
75870
                                          MA   =           53
70486
                                          Ha   =            222
980  n
mi
                                          Hp   =            217
459

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15202114
94                 X    =         4597935
19
 Y    =        3470289
53  feet           Y    =         1109361
03  meter
 Z    =       15870471
75                 Z    =         4859741
52
 XDOT =       2890
999031                 XDOT =         812
088152
 YDOT =      23697
701560  feet/sec       YDOT =        7232
527063  meter/sec
 ZDOT =      -7934
498594                 ZDOT =       -2414
322562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15298699
11                 X    =         4663043
49
 Y    =        2423177
64  feet           Y    =          738584
55  meter
 Z    =       15971759
36                 Z    =         4868192
25
 XDOT =       4746
326352                 XDOT =        1446
680272
 YDOT =      22322
452645  feet/sec       YDOT =        6803
883566  meter/sec
 ZDOT =      -7916
531590                 ZDOT =       -2412
958829


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   19118
45725882  
00016717  00000-0  10270-3 0  9097
2 25544  51
6364 248
3841 0001112 237
0549 123
0496 15
52563040  7522


Satellite: ISS
Catalog Number: 25544
Epoch time:      19118
45725882   =   yrday
fracday
Element set:     909
Inclination:       51
6364  deg
RA of node:       248
3841  deg
Eccentricity:     
0001112     
Arg of perigee:   237
0549  deg
Mean anomaly:     123
0496  deg
Mean motion:   15
52563040  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             752
Checksum:              303


Coasting Arc #11 (Orbit 752)
---------------------------------------

Vector Time (GMT): 2019/118/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964789
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2171345
00                 A    =         6793613
51  meter
 Y    =       -6405653
32  meter          E    =           
0011799
 Z    =         573205
35                 I    =           51
30201
 XDOT =       4719
485913                 Wp   =           50
88089
 YDOT =      -1060
840276  meter/sec      RA   =          247
38186  deg
 ZDOT =       5947
482395                 TA   =          315
33068
                                          MA   =          315
42568
                                          Ha   =            223
032  n
mi
                                          Hp   =            217
414

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7123835
30                 X    =        -2102338
10
 Y    =      -21015922
95  feet           Y    =        -6429548
97  meter
 Z    =        1880594
97                 Z    =          562825
37
 XDOT =      15483
877666                 XDOT =        4702
108130
 YDOT =      -3480
447099  feet/sec       YDOT =       -1008
160823  meter/sec
 ZDOT =      19512
737518                 ZDOT =        5970
365743

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13967544
14                 X    =        -4257307
46
 Y    =      -17248131
44  feet           Y    =        -5257230
46  meter
 Z    =        1834218
27                 Z    =          559069
73
 XDOT =      11942
674966                 XDOT =        3640
127330
 YDOT =      -7558
212350  feet/sec       YDOT =       -2303
743124  meter/sec
 ZDOT =      19616
296579                 ZDOT =        5979
047197


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   19118
52162300  
00016717  00000-0  10270-3 0  9107
2 25544  51
6385 248
0639 0001229 234
3169 125
7869 15
52611019  7538


Satellite: ISS
Catalog Number: 25544
Epoch time:      19118
52162300   =   yrday
fracday
Element set:     910
Inclination:       51
6385  deg
RA of node:       248
0639  deg
Eccentricity:     
0001229     
Arg of perigee:   234
3169  deg
Mean anomaly:     125
7869  deg
Mean motion:   15
52611019  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             753
Checksum:              299


Coasting Arc #12 (Orbit 752)
---------------------------------------

Vector Time (GMT): 2019/118/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964789
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4517027
70                 A    =         6788926
36  meter
 Y    =        3770720
76  meter          E    =           
0011407
 Z    =        3375650
51                 I    =           51
28628
 XDOT =      -1509
411098                 Wp   =           94
03671
 YDOT =       5942
667991  meter/sec      RA   =          247
23142  deg
 ZDOT =      -4605
688120                 TA   =           46
33931
                                          MA   =           46
24480
                                          Ha   =            222
983  n
mi
                                          Hp   =            217
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14819644
68                 X    =         4458129
63
 Y    =       12371131
12  feet           Y    =         3820904
02  meter
 Z    =       11074968
86                 Z    =         3397449
52
 XDOT =      -4952
136148                 XDOT =       -1553
379588
 YDOT =      19496
942229  feet/sec       YDOT =        5925
542838  meter/sec
 ZDOT =     -15110
525327                 ZDOT =       -4613
127107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18887488
60                 X    =         5756906
52
 Y    =        3707280
82  feet           Y    =         1129979
19  meter
 Z    =       11173206
00                 Z    =         3405593
19
 XDOT =       5443
463256                 XDOT =        1659
167600
 YDOT =      18035
583531  feet/sec       YDOT =        5497
245860  meter/sec
 ZDOT =     -15144
676459                 ZDOT =       -4616
097385


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   19118
52162396  
00016717  00000-0  10270-3 0  9113
2 25544  51
6383 248
0639 0001276 234
6466 125
4567 15
52579220  7530


Satellite: ISS
Catalog Number: 25544
Epoch time:      19118
52162396   =   yrday
fracday
Element set:     911
Inclination:       51
6383  deg
RA of node:       248
0639  deg
Eccentricity:     
0001276     
Arg of perigee:   234
6466  deg
Mean anomaly:     125
4567  deg
Mean motion:   15
52579220  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             753
Checksum:              317


Coasting Arc #13 (Orbit 767)
---------------------------------------

Vector Time (GMT): 2019/119/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964789
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4511714
64                 A    =         6791330
27  meter
 Y    =       -4483194
05  meter          E    =           
0004366
 Z    =       -2377566
28                 I    =           51
30956
 XDOT =       2189
074137                 Wp   =           41
88858
 YDOT =      -5033
562501  meter/sec      RA   =          242
23836  deg
 ZDOT =       5346
264706                 TA   =          291
45780
                                          MA   =          291
50436
                                          Ha   =            222
970  n
mi
                                          Hp   =            217
444

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14802213
39                 X    =        -4449698
02
 Y    =      -14708641
89  feet           Y    =        -4533300
48  meter
 Z    =       -7800414
30                 Z    =        -2399331
90
 XDOT =       7182
001761                 XDOT =        2219
228873
 YDOT =     -16514
312667  feet/sec       YDOT =       -5008
914059  meter/sec
 ZDOT =      17540
238536                 ZDOT =        5356
971765

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20116744
43                 X    =        -6131583
70
 Y    =       -5406211
70  feet           Y    =        -1647813
33  meter
 Z    =       -7898455
51                 Z    =        -2407449
24
 XDOT =      -2495
270084                 XDOT =        -760
558322
 YDOT =     -16370
484477  feet/sec       YDOT =       -4989
723668  meter/sec
 ZDOT =      17589
078530                 ZDOT =        5361
151136


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   19119
48710387  
00016717  00000-0  10270-3 0  9129
2 25544  51
6395 243
2621 0001273 245
0702 115
0318 15
52596445  7680


Satellite: ISS
Catalog Number: 25544
Epoch time:      19119
48710387   =   yrday
fracday
Element set:     912
Inclination:       51
6395  deg
RA of node:       243
2621  deg
Eccentricity:     
0001273     
Arg of perigee:   245
0702  deg
Mean anomaly:     115
0318  deg
Mean motion:   15
52596445  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             768
Checksum:              303


Coasting Arc #14 (Orbit 783)
---------------------------------------

Vector Time (GMT): 2019/120/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964789
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4396599
01                 A    =         6793094
35  meter
 Y    =        5022193
15  meter          E    =           
0013019
 Z    =        1225766
57                 I    =           51
33257
 XDOT =      -2956
163648                 Wp   =          125
92874
 YDOT =       4017
992758  meter/sec      RA   =          237
25041  deg
 ZDOT =      -5823
246278                 TA   =           40
69570
                                          MA   =           40
59849
                                          Ha   =            222
944  n
mi
                                          Hp   =            217
459

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14424537
43                 X    =         4334158
52
 Y    =       16477011
64  feet           Y    =         5071009
89  meter
 Z    =        4021543
88                 Z    =         1246971
99
 XDOT =      -9698
699633                 XDOT =       -2972
587985
 YDOT =      13182
390938  feet/sec       YDOT =        3984
842908  meter/sec
 ZDOT =     -19105
138707                 ZDOT =       -5837
646289

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20811380
31                 X    =         6343308
72
 Y    =        6757852
92  feet           Y    =         2059793
57  meter
 Z    =        4117023
34                 Z    =         1254868
72
 XDOT =       -960
252042                 XDOT =        -292
684822
 YDOT =      14706
583020  feet/sec       YDOT =        4482
566504  meter/sec
 ZDOT =     -19170
587207                 ZDOT =       -5843
194981


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   19120
51694608  
00016717  00000-0  10270-3 0  9133
2 25544  51
6401 238
1398 0001269 248
1773 111
9244 15
52606112  7843


Satellite: ISS
Catalog Number: 25544
Epoch time:      19120
51694608   =   yrday
fracday
Element set:     913
Inclination:       51
6401  deg
RA of node:       238
1398  deg
Eccentricity:     
0001269     
Arg of perigee:   248
1773  deg
Mean anomaly:     111
9244  deg
Mean motion:   15
52606112  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             784
Checksum:              300


Coasting Arc #15 (Orbit 798)
---------------------------------------

Vector Time (GMT): 2019/121/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964789
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4178055
01                 A    =         6793750
67  meter
 Y    =       -5349995
43  meter          E    =           
0011049
 Z    =         -37695
43                 I    =           51
35432
 XDOT =       3756
283832                 Wp   =           42
24702
 YDOT =      -2968
361955  meter/sec      RA   =          232
26651  deg
 ZDOT =       5987
179413                 TA   =          317
34560
                                          MA   =          317
43134
                                          Ha   =            222
976  n
mi
                                          Hp   =            217
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13707529
57                 X    =        -4117736
21
 Y    =      -17552478
44  feet           Y    =        -5396380
10  meter
 Z    =        -123672
66                 Z    =          -57844
44
 XDOT =      12323
765853                 XDOT =        3760
115031
 YDOT =      -9738
720325  feet/sec       YDOT =       -2926
335003  meter/sec
 ZDOT =      19642
977078                 ZDOT =        6005
435593

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20905086
57                 X    =        -6371870
39
 Y    =       -7676754
82  feet           Y    =        -2339874
87  meter
 Z    =        -214363
87                 Z    =          -65338
11
 XDOT =       4657
896580                 XDOT =        1419
726878
 YDOT =     -13180
467774  feet/sec       YDOT =       -4017
406578  meter/sec
 ZDOT =      19725
777044                 ZDOT =        6012
416843


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   19121
48242032  
00016717  00000-0  10270-3 0  9141
2 25544  51
6407 233
3384 0001108 257
1732 102
9296 15
52607561  7990


Satellite: ISS
Catalog Number: 25544
Epoch time:      19121
48242032   =   yrday
fracday
Element set:     914
Inclination:       51
6407  deg
RA of node:       233
3384  deg
Eccentricity:     
0001108     
Arg of perigee:   257
1732  deg
Mean anomaly:     102
9296  deg
Mean motion:   15
52607561  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             799
Checksum:              295


Coasting Arc #16 (Orbit 814)
---------------------------------------

Vector Time (GMT): 2019/122/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964789
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3793352
35                 A    =         6793146
27  meter
 Y    =        5504060
94  meter          E    =           
0008842
 Z    =       -1184712
36                 I    =           51
37338
 XDOT =      -4585
584206                 Wp   =          149
27570
 YDOT =       1909
599734  meter/sec      RA   =          227
28439  deg
 ZDOT =      -5837
630263                 TA   =           43
63184
                                          MA   =           43
56195
                                          Ha   =            222
957  n
mi
                                          Hp   =            217
463

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12445381
72                 X    =         3737277
20
 Y    =       18057942
71  feet           Y    =         5546167
31  meter
 Z    =       -3886851
58                 Z    =        -1166421
71
 XDOT =     -15044
567606                 XDOT =       -4578
240719
 YDOT =       6265
090992  feet/sec       YDOT =        1858
361485  meter/sec
 ZDOT =     -19152
330259                 ZDOT =       -5859
887819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20270094
01                 X    =         6178324
66
 Y    =        8410292
85  feet           Y    =         2563457
26  meter
 Z    =       -3804562
94                 Z    =        -1159630
79
 XDOT =      -8522
996288                 XDOT =       -2597
809269
 YDOT =      11872
793029  feet/sec       YDOT =        3618
827315  meter/sec
 ZDOT =     -19253
145140                 ZDOT =       -5868
358639


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   19122
51225733  
00016717  00000-0  10270-3 0  9156
2 25544  51
6404 228
2167 0001197 257
3270 102
7748 15
52620042  8154


Satellite: ISS
Catalog Number: 25544
Epoch time:      19122
51225733   =   yrday
fracday
Element set:     915
Inclination:       51
6404  deg
RA of node:       228
2167  deg
Eccentricity:     
0001197     
Arg of perigee:   257
3270  deg
Mean anomaly:     102
7748  deg
Mean motion:   15
52620042  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             815
Checksum:              284


Coasting Arc #17 (Orbit 830)
---------------------------------------

Vector Time (GMT): 2019/123/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964789
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3269241
14                 A    =         6791454
30  meter
 Y    =       -5476038
87  meter          E    =           
0012716
 Z    =        2316680
11                 I    =           51
39249
 XDOT =       5377
761459                 Wp   =           71
64669
 YDOT =       -922
742687  meter/sec      RA   =          222
30122  deg
 ZDOT =       5387
400983                 TA   =          314
26035
                                          MA   =          314
36464
                                          Ha   =            222
950  n
mi
                                          Hp   =            217
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10725856
77                 X    =        -3219016
88
 Y    =      -17966006
78  feet           Y    =        -5512316
98  meter
 Z    =        7600656
52                 Z    =         2300921
09
 XDOT =      17643
574342                 XDOT =        5361
510685
 YDOT =      -3027
371021  feet/sec       YDOT =        -862
695640  meter/sec
 ZDOT =      17675
200077                 ZDOT =        5413
485120

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18952621
68                 X    =        -5776759
09
 Y    =       -8927013
47  feet           Y    =        -2720953
70  meter
 Z    =        7529803
77                 Z    =         2295084
19
 XDOT =      12223
761818                 XDOT =        3725
802602
 YDOT =     -10886
404394  feet/sec       YDOT =       -3318
176059  meter/sec
 ZDOT =      17793
252054                 ZDOT =        5423
383226


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   19123
54209071  
00016717  00000-0  10270-3 0  9168
2 25544  51
6417 223
0949 0001139 264
9413  95
1609 15
52632802  8314


Satellite: ISS
Catalog Number: 25544
Epoch time:      19123
54209071   =   yrday
fracday
Element set:     916
Inclination:       51
6417  deg
RA of node:       223
0949  deg
Eccentricity:     
0001139     
Arg of perigee:   264
9413  deg
Mean anomaly:      95
1609  deg
Mean motion:   15
52632802  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             831
Checksum:              296


Coasting Arc #18 (Orbit 844)
---------------------------------------

Vector Time (GMT): 2019/124/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964789
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2559307
43                 A    =         6788995
99  meter
 Y    =        5318982
33  meter          E    =           
0003554
 Z    =       -3356705
06                 I    =           51
40935
 XDOT =      -6096
324369                 Wp   =           94
56601
 YDOT =          8
379593  meter/sec      RA   =          217
31605  deg
 ZDOT =      -4639
373511                 TA   =          124
66475
                                          MA   =          124
63124
                                          Ha   =            222
948  n
mi
                                          Hp   =            217
494

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8396677
92                 X    =         2515944
17
 Y    =       17450729
44  feet           Y    =         5347359
89  meter
 Z    =      -11012811
88                 Z    =        -3344377
90
 XDOT =     -20001
064204                 XDOT =       -6073
429030
 YDOT =         27
492103  feet/sec       YDOT =         -59
665686  meter/sec
 ZDOT =     -15221
041703                 ZDOT =       -4668
932151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16915495
01                 X    =         5155842
88
 Y    =        9492853
97  feet           Y    =         2893421
89  meter
 Z    =      -10957460
27                 Z    =        -3339833
89
 XDOT =     -15630
989725                 XDOT =       -4764
325668
 YDOT =      10146
642013  feet/sec       YDOT =        3092
696485  meter/sec
 ZDOT =     -15354
750605                 ZDOT =       -4680
127984


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   19124
50755699  
00016717  00000-0  10270-3 0  9178
2 25544  51
6415 218
2937 0001175 271
4179  88
6839 15
52620805  8454


Satellite: ISS
Catalog Number: 25544
Epoch time:      19124
50755699   =   yrday
fracday
Element set:     917
Inclination:       51
6415  deg
RA of node:       218
2937  deg
Eccentricity:     
0001175     
Arg of perigee:   271
4179  deg
Mean anomaly:      88
6839  deg
Mean motion:   15
52620805  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             845
Checksum:              336
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