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

 
Date: February 7th 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 3 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


039/16:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 215 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 3494)
---------------------------------------

Vector Time (GMT): 2019/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3900795
76                 A    =         6789494
71  meter
 Y    =       -5006121
34  meter          E    =           
0015833
 Z    =        2385382
32                 I    =           51
29550
 XDOT =       2805
192869                 Wp   =           54
04195
 YDOT =       4739
144902  meter/sec      RA   =          290
39803  deg
 ZDOT =       5342
790525                 TA   =          332
75585
                                          MA   =          332
83882
                                          Ha   =            223
126  n
mi
                                          Hp   =            215
934

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12797886
35                 X    =         3944899
17
 Y    =      -16424282
60  feet           Y    =        -4962253
24  meter
 Z    =        7826057
48                 Z    =         2404437
68
 XDOT =       9203
388677                 XDOT =        2726
038338
 YDOT =      15548
375664  feet/sec       YDOT =        4770
072123  meter/sec
 ZDOT =      17528
840306                 ZDOT =        5356
224319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20604479
14                 X    =         6280245
24
 Y    =       -2763410
83  feet           Y    =         -842287
62  meter
 Z    =        7912593
10                 Z    =         2411758
38
 XDOT =      -4634
644499                 XDOT =       -1412
639643
 YDOT =      15952
953037  feet/sec       YDOT =        4862
460086  meter/sec
 ZDOT =      17588
888456                 ZDOT =        5361
093201


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
55952712  
00016717  00000-0  10270-3 0  9003
2 25544  51
6416 290
8572 0005497 356
1839   3
9271 15
53225255 34956


Satellite: ISS
Catalog Number: 25544
Epoch time:      19037
55952712   =   yrday
fracday
Element set:     900
Inclination:       51
6416  deg
RA of node:       290
8572  deg
Eccentricity:     
0005497     
Arg of perigee:   356
1839  deg
Mean anomaly:       3
9271  deg
Mean motion:   15
53225255  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3495
Checksum:              323


Coasting Arc #2 (Orbit 3509)
---------------------------------------

Vector Time (GMT): 2019/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4090542
21                 A    =         6786488
88  meter
 Y    =        4084921
63  meter          E    =           
0007990
 Z    =       -3565229
69                 I    =           51
27443
 XDOT =      -2048
315332                 Wp   =           39
71623
 YDOT =      -5908
781501  meter/sec      RA   =          285
39995  deg
 ZDOT =      -4419
441323                 TA   =          182
57103
                                          MA   =          182
57514
                                          Ha   =            223
264  n
mi
                                          Hp   =            215
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13420414
09                 X    =        -4118599
48
 Y    =       13401973
84  feet           Y    =         4039021
28  meter
 Z    =      -11696947
80                 Z    =        -3585167
84
 XDOT =      -6720
194658                 XDOT =       -1960
622790
 YDOT =     -19385
766081  feet/sec       YDOT =       -5931
197084  meter/sec
 ZDOT =     -14499
479405                 ZDOT =       -4429
177753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18903205
66                 X    =        -5761697
09
 Y    =         516048
81  feet           Y    =          157291
68  meter
 Z    =      -11787345
51                 Z    =        -3592782
91
 XDOT =       8598
899427                 XDOT =        2620
944545
 YDOT =     -17233
851063  feet/sec       YDOT =       -5252
877804  meter/sec
 ZDOT =     -14542
730720                 ZDOT =       -4432
624323


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
52461150  
00016717  00000-0  10270-3 0  9013
2 25544  51
6410 286
0534 0005470 358
4225   1
6909 15
53228406 35102


Satellite: ISS
Catalog Number: 25544
Epoch time:      19038
52461150   =   yrday
fracday
Element set:     901
Inclination:       51
6410  deg
RA of node:       286
0534  deg
Eccentricity:     
0005470     
Arg of perigee:   358
4225  deg
Mean anomaly:       1
6909  deg
Mean motion:   15
53228406  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3510
Checksum:              279


Coasting Arc #3 (Orbit 3525)
---------------------------------------

Vector Time (GMT): 2019/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4179233
25                 A    =         6783388
78  meter
 Y    =       -2918883
98  meter          E    =           
0008950
 Z    =        4466569
23                 I    =           51
25553
 XDOT =       1355
150563                 Wp   =           75
79268
 YDOT =       6840
427097  meter/sec      RA   =          280
39318  deg
 ZDOT =       3198
978173                 TA   =          341
87432
                                          MA   =          341
90620
                                          Ha   =            223
277  n
mi
                                          Hp   =            215
679

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13711395
17                 X    =         4189866
79
 Y    =       -9576391
01  feet           Y    =        -2872089
16  meter
 Z    =       14654098
52                 Z    =         4486895
92
 XDOT =       4446
032030                 XDOT =        1263
019746
 YDOT =      22442
346118  feet/sec       YDOT =        6855
066385  meter/sec
 ZDOT =      10495
335213                 ZDOT =        3205
336682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16502756
83                 X    =         5030040
28
 Y    =        2159524
78  feet           Y    =          658223
15  meter
 Z    =       14746107
81                 Z    =         4494613
66
 XDOT =     -11805
081362                 XDOT =       -3598
188799
 YDOT =      18283
424634  feet/sec       YDOT =        5572
787828  meter/sec
 ZDOT =      10523
263292                 ZDOT =        3207
490651


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
55403589  
00016717  00000-0  10270-3 0  9020
2 25544  51
6403 280
9283 0005531   3
9348 356
1847 15
53222757 35263


Satellite: ISS
Catalog Number: 25544
Epoch time:      19039
55403589   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:       280
9283  deg
Eccentricity:     
0005531     
Arg of perigee:     3
9348  deg
Mean anomaly:     356
1847  deg
Mean motion:   15
53222757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3526
Checksum:              317


Coasting Arc #4 (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    =       -2553098
11                 A    =         6784690
42  meter
 Y    =       -4757012
05  meter          E    =           
0008001
 Z    =       -4113758
76                 I    =           51
25469
 XDOT =       3958
574943                 Wp   =           70
51185
 YDOT =      -5372
296470  meter/sec      RA   =          279
47142  deg
 ZDOT =       3764
182575                 TA   =          238
49369
                                          MA   =          238
57188
                                          Ha   =            223
254  n
mi
                                          Hp   =            215
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8376306
13                 X    =        -2479732
19
 Y    =      -15606994
92  feet           Y    =        -4785152
60  meter
 Z    =      -13496583
87                 Z    =        -4125982
02
 XDOT =      12987
450602                 XDOT =        4000
071358
 YDOT =     -17625
644588  feet/sec       YDOT =       -5327
796680  meter/sec
 ZDOT =      12349
680364                 ZDOT =        3783
512530

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13143720
53                 X    =        -4006206
02
 Y    =      -11811275
08  feet           Y    =        -3600076
64  meter
 Z    =      -13551197
83                 Z    =        -4130405
10
 XDOT =       5202
766824                 XDOT =        1585
803328
 YDOT =     -20026
982124  feet/sec       YDOT =       -6104
224152  meter/sec
 ZDOT =      12437
461053                 ZDOT =        3790
938129


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
68271314  
00016717  00000-0  10270-3 0  9034
2 25544  51
6361 280
2831 0005154   4
6976 355
4224 15
53239909 35284


Satellite: ISS
Catalog Number: 25544
Epoch time:      19039
68271314   =   yrday
fracday
Element set:     903
Inclination:       51
6361  deg
RA of node:       280
2831  deg
Eccentricity:     
0005154     
Arg of perigee:     4
6976  deg
Mean anomaly:     355
4224  deg
Mean motion:   15
53239909  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3528
Checksum:              312


Coasting Arc #5 (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    =        3835059
43                 A    =         6780882
86  meter
 Y    =        2413592
97  meter          E    =           
0009893
 Z    =        5042607
73                 I    =           51
24351
 XDOT =      -2129
766201                 Wp   =           29
71673
 YDOT =       7146
009455  meter/sec      RA   =          275
48095  deg
 ZDOT =      -1790
646092                 TA   =           77
76228
                                          MA   =           77
65151
                                          Ha   =            223
234  n
mi
                                          Hp   =            215
537

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12582215
98                 X    =         3783291
20
 Y    =        7918612
12  feet           Y    =         2456190
14  meter
 Z    =       16543988
63                 Z    =         5061110
78
 XDOT =      -6987
421920                 XDOT =       -2200
818807
 YDOT =      23444
912909  feet/sec       YDOT =        7121
795532  meter/sec
 ZDOT =      -5874
823135                 ZDOT =       -1801
164512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1695540
43                 X    =          516800
72
 Y    =       14675892
38  feet           Y    =         4473212
00  meter
 Z    =       16627190
44                 Z    =         5067967
65
 XDOT =     -21520
918370                 XDOT =       -6559
575919
 YDOT =       9233
780160  feet/sec       YDOT =        2814
456193  meter/sec
 ZDOT =      -5923
036988                 ZDOT =       -1805
341674


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
51911709  
00016717  00000-0  10270-3 0  9048
2 25544  51
6409 276
1237 0005523   4
6912 355
4291 15
53287541 35415


Satellite: ISS
Catalog Number: 25544
Epoch time:      19040
51911709   =   yrday
fracday
Element set:     904
Inclination:       51
6409  deg
RA of node:       276
1237  deg
Eccentricity:     
0005523     
Arg of perigee:     4
6912  deg
Mean anomaly:     355
4291  deg
Mean motion:   15
53287541  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3541
Checksum:              297


Coasting Arc #6 (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    =       -3545016
25                 A    =         6783389
63  meter
 Y    =       -3697372
53  meter          E    =           
0009935
 Z    =       -4454264
83                 I    =           51
24923
 XDOT =       2646
459116                 Wp   =           76
98841
 YDOT =      -6421
065479  meter/sec      RA   =          270
46683  deg
 ZDOT =       3232
035772                 TA   =          225
72329
                                          MA   =          225
80484
                                          Ha   =            223
447  n
mi
                                          Hp   =            215
352

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11630630
74                 X    =        -3481771
70
 Y    =      -12130487
30  feet           Y    =        -3736662
01  meter
 Z    =      -14613729
74                 Z    =        -4471331
10
 XDOT =       8682
608648                 XDOT =        2702
365398
 YDOT =     -21066
487793  feet/sec       YDOT =       -6391
158145  meter/sec
 ZDOT =      10603
791903                 ZDOT =        3245
027241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1882246
57                 X    =          573708
75
 Y    =      -16632287
45  feet           Y    =        -5069521
22  meter
 Z    =      -14690321
73                 Z    =        -4477610
06
 XDOT =      20460
677672                 XDOT =        6236
414554
 YDOT =      -7078
608609  feet/sec       YDOT =       -2157
559904  meter/sec
 ZDOT =      10663
067704                 ZDOT =        3250
103036


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
48419931  
00016717  00000-0  10270-3 0  9056
2 25544  51
6406 271
3187 0005600   8
8042 351
3208 15
53253664 35567


Satellite: ISS
Catalog Number: 25544
Epoch time:      19041
48419931   =   yrday
fracday
Element set:     905
Inclination:       51
6406  deg
RA of node:       271
3187  deg
Eccentricity:     
0005600     
Arg of perigee:     8
8042  deg
Mean anomaly:     351
3208  deg
Mean motion:   15
53253664  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3556
Checksum:              297


Coasting Arc #7 (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    =        3211739
16                 A    =         6786509
64  meter
 Y    =        4832602
15  meter          E    =           
0014716
 Z    =        3513795
78                 I    =           51
26013
 XDOT =      -3167
806867                 Wp   =           65
75650
 YDOT =       5367
411480  meter/sec      RA   =          265
45956  deg
 ZDOT =      -4465
648628                 TA   =           72
63061
                                          MA   =           72
46971
                                          Ha   =            223
562  n
mi
                                          Hp   =            215
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10537201
96                 X    =         3140393
08
 Y    =       15854993
94  feet           Y    =         4868119
31  meter
 Z    =       11528201
38                 Z    =         3529223
48
 XDOT =     -10393
067148                 XDOT =       -3205
899973
 YDOT =      17609
617717  feet/sec       YDOT =        5331
773640  meter/sec
 ZDOT =     -14651
078176                 ZDOT =       -4481
129235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5111043
13                 X    =        -1557845
94
 Y    =       18294613
44  feet           Y    =         5576198
18  meter
 Z    =       11597294
61                 Z    =         3534855
40
 XDOT =     -18710
769298                 XDOT =       -5703
042482
 YDOT =       4147
861398  feet/sec       YDOT =        1264
268154  meter/sec
 ZDOT =     -14721
460517                 ZDOT =       -4487
101165


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
51361789  
00016717  00000-0  10270-3 0  9069
2 25544  51
6400 266
1936 0005731  13
0293 347
1006 15
53279079 35721


Satellite: ISS
Catalog Number: 25544
Epoch time:      19042
51361789   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:       266
1936  deg
Eccentricity:     
0005731     
Arg of perigee:    13
0293  deg
Mean anomaly:     347
1006  deg
Mean motion:   15
53279079  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3572
Checksum:              304


Coasting Arc #8 (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    =       -2870637
03                 A    =         6789529
81  meter
 Y    =       -5678862
13  meter          E    =           
0010885
 Z    =       -2356479
50                 I    =           51
27325
 XDOT =       3672
788439                 Wp   =           30
58665
 YDOT =      -4071
634250  meter/sec      RA   =          260
45962  deg
 ZDOT =       5358
196080                 TA   =          302
98017
                                          MA   =          303
08476
                                          Ha   =            223
627  n
mi
                                          Hp   =            215
237

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9418100
49                 X    =        -2795474
70
 Y    =      -18631437
45  feet           Y    =        -5710543
42  meter
 Z    =       -7731231
96                 Z    =        -2370241
07
 XDOT =      12049
830835                 XDOT =        3692
018787
 YDOT =     -13358
380086  feet/sec       YDOT =       -4030
454855  meter/sec
 ZDOT =      17579
383464                 ZDOT =        5376
083756

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7591172
84                 X    =         2313789
48
 Y    =      -19422934
55  feet           Y    =        -5920110
45  meter
 Z    =       -7792735
99                 Z    =        -2375225
93
 XDOT =      16494
079400                 XDOT =        5027
395401
 YDOT =       -612
837531  feet/sec       YDOT =        -186
792880  meter/sec
 ZDOT =      17660
484954                 ZDOT =        5382
915814


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
47869775  
00016717  00000-0  10270-3 0  9074
2 25544  51
6397 261
3890 0005660  14
9309 345
2009 15
53236190 35876


Satellite: ISS
Catalog Number: 25544
Epoch time:      19043
47869775   =   yrday
fracday
Element set:     907
Inclination:       51
6397  deg
RA of node:       261
3890  deg
Eccentricity:     
0005660     
Arg of perigee:    14
9309  deg
Mean anomaly:     345
2009  deg
Mean motion:   15
53236190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3587
Checksum:              334


Coasting Arc #9 (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    =        2438667
72                 A    =         6791494
49  meter
 Y    =        6257932
99  meter          E    =           
0013313
 Z    =         985780
78                 I    =           51
28700
 XDOT =      -4197
736123                 Wp   =          100
10738
 YDOT =       2571
587356  meter/sec      RA   =          255
46562  deg
 ZDOT =      -5874
766896                 TA   =           69
16686
                                          MA   =           69
02433
                                          Ha   =            223
770  n
mi
                                          Hp   =            215
097

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8000878
36                 X    =         2363720
19
 Y    =       20531276
22  feet           Y    =         6284784
84  meter
 Z    =        3234188
92                 Z    =          997444
63
 XDOT =     -13772
100141                 XDOT =       -4197
644332
 YDOT =       8436
966391  feet/sec       YDOT =        2524
645747  meter/sec
 ZDOT =     -19274
169605                 ZDOT =       -5895
157511

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9591435
70                 X    =        -2923469
60
 Y    =       19829590
87  feet           Y    =         6044059
30  meter
 Z    =        3286186
67                 Z    =         1001629
70
 XDOT =     -14024
169529                 XDOT =       -4274
566872
 YDOT =      -3538
842352  feet/sec       YDOT =       -1078
639149  meter/sec
 ZDOT =     -19366
410683                 ZDOT =       -5902
881976


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
50811428  
00016717  00000-0  10270-3 0  9082
2 25544  51
6403 256
2635 0005625  19
8814 340
2556 15
53237730 36032


Satellite: ISS
Catalog Number: 25544
Epoch time:      19044
50811428   =   yrday
fracday
Element set:     908
Inclination:       51
6403  deg
RA of node:       256
2635  deg
Eccentricity:     
0005625     
Arg of perigee:    19
8814  deg
Mean anomaly:     340
2556  deg
Mean motion:   15
53237730  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3603
Checksum:              298


Coasting Arc #10 (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    =        4437735
27                 A    =         6783126
20  meter
 Y    =        2386220
08  meter          E    =           
0013024
 Z    =        4536698
95                 I    =           51
25733
 XDOT =       -615
083166                 Wp   =           51
17706
 YDOT =       7002
135860  meter/sec      RA   =          254
52440  deg
 ZDOT =      -3067
331327                 TA   =           69
74242
                                          MA   =           69
60246
                                          Ha   =            223
671  n
mi
                                          Hp   =            215
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14559498
92                 X    =         4388685
56
 Y    =        7828806
03  feet           Y    =         2435571
75  meter
 Z    =       14884182
89                 Z    =         4558136
38
 XDOT =      -2017
989389                 XDOT =        -678
438095
 YDOT =      22972
886681  feet/sec       YDOT =        6994
903285  meter/sec
 ZDOT =     -10063
422988                 ZDOT =       -3070
473117

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16244216
85                 X    =         4951237
30
 Y    =        2552144
36  feet           Y    =          777893
60  meter
 Z    =       14980657
23                 Z    =         4566104
32
 XDOT =       6018
168919                 XDOT =        1834
337886
 YDOT =      21120
462098  feet/sec       YDOT =        6437
516847  meter/sec
 ZDOT =     -10078
288006                 ZDOT =       -3071
862184


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
70113121  
00016717  00000-0  10270-3 0  9090
2 25544  51
6372 255
2972 0005241  25
1043 335
0363 15
53222172 36063


Satellite: ISS
Catalog Number: 25544
Epoch time:      19044
70113121   =   yrday
fracday
Element set:     909
Inclination:       51
6372  deg
RA of node:       255
2972  deg
Eccentricity:     
0005241     
Arg of perigee:    25
1043  deg
Mean anomaly:     335
0363  deg
Mean motion:   15
53222172  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3606
Checksum:              267


Coasting Arc #11 (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    =       -4468859
33                 A    =         6786093
60  meter
 Y    =       -3555534
37  meter          E    =           
0008840
 Z    =       -3669640
18                 I    =           51
27798
 XDOT =       1383
854724                 Wp   =           66
09066
 YDOT =      -6179
097186  meter/sec      RA   =          249
51838  deg
 ZDOT =       4313
493424                 TA   =          250
04898
                                          MA   =          250
14421
                                          Ha   =            223
734  n
mi
                                          Hp   =            214
863

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14661611
99                 X    =        -4410943
39
 Y    =      -11665139
00  feet           Y    =        -3605184
44  meter
 Z    =      -12039501
92                 Z    =        -3691207
26
 XDOT =       4540
205789                 XDOT =        1431
896024
 YDOT =     -20272
628564  feet/sec       YDOT =       -6163
353342  meter/sec
 ZDOT =      14151
881311                 ZDOT =        4320
332256

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17742129
11                 X    =        -5407800
95
 Y    =       -5823325
10  feet           Y    =        -1774949
49  meter
 Z    =      -12136460
76                 Z    =        -3699193
24
 XDOT =      -3357
169157                 XDOT =       -1023
265159
 YDOT =     -19251
344900  feet/sec       YDOT =       -5867
809926  meter/sec
 ZDOT =      14183
333993                 ZDOT =        4323
080201


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
66620640  
00016717  00000-0  10270-3 0  9107
2 25544  51
6377 250
4935 0005290  28
1224 332
0213 15
53248188 36215


Satellite: ISS
Catalog Number: 25544
Epoch time:      19045
66620640   =   yrday
fracday
Element set:     910
Inclination:       51
6377  deg
RA of node:       250
4935  deg
Eccentricity:     
0005290     
Arg of perigee:    28
1224  deg
Mean anomaly:     332
0213  deg
Mean motion:   15
53248188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3621
Checksum:              286


Coasting Arc #12 (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    =        4379646
87                 A    =         6789200
59  meter
 Y    =        4540609
39  meter          E    =           
0015983
 Z    =        2496705
05                 I    =           51
30035
 XDOT =      -2253
791577                 Wp   =           86
36369
 YDOT =       5089
872009  meter/sec      RA   =          244
51906  deg
 ZDOT =      -5272
829160                 TA   =           65
50323
                                          MA   =           65
33665
                                          Ha   =            223
793  n
mi
                                          Hp   =            214
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14368920
17                 X    =         4316419
60
 Y    =       14897012
42  feet           Y    =         4589232
10  meter
 Z    =        8191289
53                 Z    =         2517825
83
 XDOT =      -7394
329321                 XDOT =       -2284
928444
 YDOT =      16699
055148  feet/sec       YDOT =        5064
494492  meter/sec
 ZDOT =     -17299
308269                 ZDOT =       -5283
852613

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18774476
27                 X    =         5722460
37
 Y    =        8622220
01  feet           Y    =         2628052
66  meter
 Z    =        8286159
12                 Z    =         2525621
30
 XDOT =        -30
554523                 XDOT =          -9
313018
 YDOT =      16834
233796  feet/sec       YDOT =        5131
074461  meter/sec
 ZDOT =     -17349
529342                 ZDOT =       -5288
136543


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
69561992  
00016717  00000-0  10270-3 0  9116
2 25544  51
6371 245
3680 0005196  31
3488 328
7973 15
53245071 36372


Satellite: ISS
Catalog Number: 25544
Epoch time:      19046
69561992   =   yrday
fracday
Element set:     911
Inclination:       51
6371  deg
RA of node:       245
3680  deg
Eccentricity:     
0005196     
Arg of perigee:    31
3488  deg
Mean anomaly:     328
7973  deg
Mean motion:   15
53245071  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3637
Checksum:              332


Coasting Arc #13 (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    =       -4172053
91                 A    =         6791241
09  meter
 Y    =       -5217339
45  meter          E    =           
0014457
 Z    =       -1186679
06                 I    =           51
32395
 XDOT =       3159
124588                 Wp   =           36
88903
 YDOT =      -3842
561673  meter/sec      RA   =          239
52714  deg
 ZDOT =       5835
897316                 TA   =          310
16500
                                          MA   =          310
29151
                                          Ha   =            223
847  n
mi
                                          Hp   =            214
755

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13687840
92                 X    =        -4107637
98
 Y    =      -17117255
40  feet           Y    =        -5263634
08  meter
 Z    =       -3893304
02                 Z    =        -1206788
46
 XDOT =      10364
581980                 XDOT =        3173
511510
 YDOT =     -12606
829636  feet/sec       YDOT =       -3807
153741  meter/sec
 ZDOT =      19146
644739                 ZDOT =        5851
277719

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19165409
51                 X    =        -5841616
82
 Y    =      -10598749
48  feet           Y    =        -3230498
84  meter
 Z    =       -3983569
45                 Z    =        -1214191
97
 XDOT =       3870
261567                 XDOT =        1179
655726
 YDOT =     -14162
698982  feet/sec       YDOT =       -4316
790650  meter/sec
 ZDOT =      19216
405581                 ZDOT =        5857
160421


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
66069288  
00016717  00000-0  10270-3 0  9126
2 25544  51
6385 240
5635 0005328  34
4457 325
7039 15
53255550 36521


Satellite: ISS
Catalog Number: 25544
Epoch time:      19047
66069288   =   yrday
fracday
Element set:     912
Inclination:       51
6385  deg
RA of node:       240
5635  deg
Eccentricity:     
0005328     
Arg of perigee:    34
4457  deg
Mean anomaly:     325
7039  deg
Mean motion:   15
53255550  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3652
Checksum:              321


Coasting Arc #14 (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    =        3764969
17                 A    =         6791794
49  meter
 Y    =        5643762
31  meter          E    =           
0012078
 Z    =        -259455
17                 I    =           51
34288
 XDOT =      -4107
255237                 Wp   =          110
56753
 YDOT =       2475
753753  meter/sec      RA   =          234
53959  deg
 ZDOT =      -5977
715210                 TA   =           72
23751
                                          MA   =           72
10574
                                          Ha   =            223
952  n
mi
                                          Hp   =            214
631

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12352261
04                 X    =         3702839
46
 Y    =       18516280
55  feet           Y    =         5685517
43  meter
 Z    =        -851230
89                 Z    =         -241317
81
 XDOT =     -13475
246841                 XDOT =       -4105
598943
 YDOT =       8122
551684  feet/sec       YDOT =        2429
832774  meter/sec
 ZDOT =     -19611
926542                 ZDOT =       -5997
662159

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18705330
45                 X    =         5701384
72
 Y    =       12069527
43  feet           Y    =         3678791
96  meter
 Z    =        -769878
45                 Z    =         -234658
95
 XDOT =      -8129
963061                 XDOT =       -2478
012741
 YDOT =      11396
413405  feet/sec       YDOT =        3473
626806  meter/sec
 ZDOT =     -19702
172634                 ZDOT =       -6005
222219


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
69010202  
00016717  00000-0  10270-3 0  9133
2 25544  51
6377 235
4382 0005378  38
1607 321
9925 15
53271378 36682


Satellite: ISS
Catalog Number: 25544
Epoch time:      19048
69010202   =   yrday
fracday
Element set:     913
Inclination:       51
6377  deg
RA of node:       235
4382  deg
Eccentricity:     
0005378     
Arg of perigee:    38
1607  deg
Mean anomaly:     321
9925  deg
Mean motion:   15
53271378  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3668
Checksum:              319


Coasting Arc #15 (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    =       -3185867
84                 A    =         6790717
37  meter
 Y    =       -5756965
03  meter          E    =           
0019028
 Z    =        1639102
35                 I    =           51
35984
 XDOT =       5011
838220                 Wp   =           57
86657
 YDOT =      -1140
628920  meter/sec      RA   =          229
55276  deg
 ZDOT =       5696
512690                 TA   =          320
16117
                                          MA   =          320
30070
                                          Ha   =            223
993  n
mi
                                          Hp   =            214
565

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10452322
31                 X    =        -3129216
66
 Y    =      -18887680
55  feet           Y    =        -5792274
82  meter
 Z    =        5377632
40                 Z    =         1623764
87
 XDOT =      16443
038781                 XDOT =        4996
550923
 YDOT =      -3742
220865  feet/sec       YDOT =       -1084
668323  meter/sec
 ZDOT =      18689
346097                 ZDOT =        5720
820485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17361510
70                 X    =        -5291788
46
 Y    =      -12857214
28  feet           Y    =        -3918878
91  meter
 Z    =        5308901
55                 Z    =         1618153
19
 XDOT =      12371
140785                 XDOT =        3770
723711
 YDOT =      -8889
728965  feet/sec       YDOT =       -2709
589388  meter/sec
 ZDOT =      18799
163317                 ZDOT =        5729
984979


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
71951040  
00016717  00000-0  10270-3 0  9142
2 25544  51
6381 230
3134 0005364  42
7351 317
4217 15
53272095 36847


Satellite: ISS
Catalog Number: 25544
Epoch time:      19049
71951040   =   yrday
fracday
Element set:     914
Inclination:       51
6381  deg
RA of node:       230
3134  deg
Eccentricity:     
0005364     
Arg of perigee:    42
7351  deg
Mean anomaly:     317
4217  deg
Mean motion:   15
53272095  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3684
Checksum:              293


Coasting Arc #16 (Orbit 3698)
---------------------------------------

Vector Time (GMT): 2019/050/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2372859
64                 A    =         6788189
05  meter
 Y    =        5641181
00  meter          E    =           
0008221
 Z    =       -2946386
75                 I    =           51
37457
 XDOT =      -5817
995477                 Wp   =           77
08716
 YDOT =       -147
478147  meter/sec      RA   =          224
56294  deg
 ZDOT =      -4977
830517                 TA   =          136
64090
                                          MA   =          136
57620
                                          Ha   =            224
046  n
mi
                                          Hp   =            214
515

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7784972
58                 X    =         2323913
48
 Y    =       18507811
67  feet           Y    =         5667442
10  meter
 Z    =       -9666623
21                 Z    =        -2934979
90
 XDOT =     -19087
911669                 XDOT =       -5791
735135
 YDOT =       -483
852189  feet/sec       YDOT =        -212
392540  meter/sec
 ZDOT =     -16331
464952                 ZDOT =       -5006
027503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15033775
61                 X    =         4582294
81
 Y    =       13345946
12  feet           Y    =         4067844
38  meter
 Z    =       -9615602
34                 Z    =        -2930835
59
 XDOT =     -16375
821763                 XDOT =       -4991
350473
 YDOT =       6612
191073  feet/sec       YDOT =        2015
395839  meter/sec
 ZDOT =     -16458
738876                 ZDOT =       -5016
623609


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   19050
68457963  
00016717  00000-0  10270-3 0  9156
2 25544  51
6389 225
5085 0005359  45
6795 314
4796 15
53269738 36999


Satellite: ISS
Catalog Number: 25544
Epoch time:      19050
68457963   =   yrday
fracday
Element set:     915
Inclination:       51
6389  deg
RA of node:       225
5085  deg
Eccentricity:     
0005359     
Arg of perigee:    45
6795  deg
Mean anomaly:     314
4796  deg
Mean motion:   15
53269738  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3699
Checksum:              369


Coasting Arc #17 (Orbit 3714)
---------------------------------------

Vector Time (GMT): 2019/051/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1387587
09                 A    =         6784964
12  meter
 Y    =       -5291021
13  meter          E    =           
0014836
 Z    =        4000547
33                 I    =           51
38952
 XDOT =       6468
992727                 Wp   =           84
67483
 YDOT =       1279
554356  meter/sec      RA   =          219
56809  deg
 ZDOT =       3924
856058                 TA   =          324
39196
                                          MA   =          324
49085
                                          Ha   =            224
049  n
mi
                                          Hp   =            214
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4552451
07                 X    =        -1347750
17
 Y    =      -17358993
20  feet           Y    =        -5306314
98  meter
 Z    =       13125155
30                 Z    =         3993904
40
 XDOT =      21223
729420                 XDOT =        6435
139354
 YDOT =       4198
012979  feet/sec       YDOT =        1351
706238  meter/sec
 ZDOT =      12876
824338                 ZDOT =        3956
196793

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11875629
99                 X    =        -3619692
02
 Y    =      -13483471
16  feet           Y    =        -4109762
01  meter
 Z    =       13095593
74                 Z    =         3991536
97
 XDOT =      19815
942532                 XDOT =        6039
899284
 YDOT =      -4773
447996  feet/sec       YDOT =       -1454
946949  meter/sec
 ZDOT =      13018
211100                 ZDOT =        3967
950743


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   19051
71398267  
00016717  00000-0  10270-3 0  9163
2 25544  51
6398 220
3833 0005400  49
1160 311
0460 15
53304400 37151


Satellite: ISS
Catalog Number: 25544
Epoch time:      19051
71398267   =   yrday
fracday
Element set:     916
Inclination:       51
6398  deg
RA of node:       220
3833  deg
Eccentricity:     
0005400     
Arg of perigee:    49
1160  deg
Mean anomaly:     311
0460  deg
Mean motion:   15
53304400  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3715
Checksum:              278
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