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

 
Date: July 7th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16271 6957 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


187/16:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 4
000/00:00:00 000 0 0 0 0 217 2

190/22:57:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 217 3

Coasting Arc #1 (Orbit 1808)
---------------------------------------

Vector Time (GMT): 2019/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -926620
03                 A    =         6797944
95  meter
 Y    =        6618005
86  meter          E    =           
0015752
 Z    =       -1221521
92                 I    =           51
27447
 XDOT =      -4680
054521                 Wp   =          129
03119
 YDOT =      -1718
168124  meter/sec      RA   =          269
54178  deg
 ZDOT =      -5819
009079                 TA   =           64
29443
                                          MA   =           64
13186
                                          Ha   =            228
540  n
mi
                                          Hp   =            217
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3040091
96                 X    =         -994622
24
 Y    =       21712617
64  feet           Y    =         6607263
70  meter
 Z    =       -4007617
85                 Z    =        -1226187
16
 XDOT =     -15354
509584                 XDOT =       -4632
228702
 YDOT =      -5637
034527  feet/sec       YDOT =       -1770
235483  meter/sec
 ZDOT =     -19091
237136                 ZDOT =       -5841
626680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21855610
06                 X    =         6661589
95
 Y    =       -1684316
47  feet           Y    =         -513379
66  meter
 Z    =       -4029430
67                 Z    =        -1228170
47
 XDOT =      -2386
070838                 XDOT =        -727
274391
 YDOT =      14484
023279  feet/sec       YDOT =        4414
730295  meter/sec
 ZDOT =     -19193
639903                 ZDOT =       -5850
221442


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   19186
52989687  
00016717  00000-0  10270-3 0  9006
2 25544  51
6419 270
2719 0007197 112
6297 247
5616 15
50949612 18099


Satellite: ISS
Catalog Number: 25544
Epoch time:      19186
52989687   =   yrday
fracday
Element set:     900
Inclination:       51
6419  deg
RA of node:       270
2719  deg
Eccentricity:     
0007197     
Arg of perigee:   112
6297  deg
Mean anomaly:     247
5616  deg
Mean motion:   15
50949612  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1809
Checksum:              349


Coasting Arc #2 (Orbit 1824)
---------------------------------------

Vector Time (GMT): 2019/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         852990
24                 A    =         6797150
38  meter
 Y    =       -6485145
52  meter          E    =           
0019352
 Z    =        1825678
53                 I    =           51
27338
 XDOT =       4729
901472                 Wp   =           82
42436
 YDOT =       2215
108958  meter/sec      RA   =          264
55932  deg
 ZDOT =       5609
786166                 TA   =          297
73313
                                          MA   =          297
92928
                                          Ha   =            228
502  n
mi
                                          Hp   =            217
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2798524
40                 X    =          916577
64
 Y    =      -21276724
15  feet           Y    =        -6475251
47  meter
 Z    =        5989758
94                 Z    =         1829975
59
 XDOT =      15518
049450                 XDOT =        4677
531270
 YDOT =       7267
417840  feet/sec       YDOT =        2267
708520  meter/sec
 ZDOT =      18404
810257                 ZDOT =        5632
634886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21340454
01                 X    =        -6504570
38
 Y    =        2207815
44  feet           Y    =          672942
15  meter
 Z    =        6009868
17                 Z    =         1831807
82
 XDOT =       3695
338838                 XDOT =        1126
339278
 YDOT =     -15096
646372  feet/sec       YDOT =       -4601
457814  meter/sec
 ZDOT =      18508
224554                 ZDOT =        5641
306844


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   19187
56083456  
00016717  00000-0  10270-3 0  9011
2 25544  51
6420 265
1574 0007153 115
8194 244
3696 15
50957651 18259


Satellite: ISS
Catalog Number: 25544
Epoch time:      19187
56083456   =   yrday
fracday
Element set:     901
Inclination:       51
6420  deg
RA of node:       265
1574  deg
Eccentricity:     
0007153     
Arg of perigee:   115
8194  deg
Mean anomaly:     244
3696  deg
Mean motion:   15
50957651  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1825
Checksum:              324


Coasting Arc #3 (Orbit 1827)
---------------------------------------

Vector Time (GMT): 2019/187/16:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4133531
30                 A    =         6786678
71  meter
 Y    =       -1076846
16  meter          E    =           
0010011
 Z    =        5266160
61                 I    =           51
23648
 XDOT =       1284
141855                 Wp   =          113
58192
 YDOT =       7543
626775  meter/sec      RA   =          263
52652  deg
 ZDOT =        529
856388                 TA   =          331
30803
                                          MA   =          331
36307
                                          Ha   =            228
392  n
mi
                                          Hp   =            217
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13561454
40                 X    =         4119686
11
 Y    =       -3532959
85  feet           Y    =        -1030700
15  meter
 Z    =       17277429
81                 Z    =         5286205
61
 XDOT =       4213
063829                 XDOT =        1197
117722
 YDOT =      24749
431677  feet/sec       YDOT =        7557
500305  meter/sec
 ZDOT =       1738
373977                 ZDOT =         535
883680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13599217
90                 X    =        -4145041
62
 Y    =        2881469
72  feet           Y    =          878271
97  meter
 Z    =       17368443
69                 Z    =         5293901
64
 XDOT =      -2796
707518                 XDOT =        -852
436452
 YDOT =     -23931
210555  feet/sec       YDOT =       -7294
232977  meter/sec
 ZDOT =       1764
993058                 ZDOT =         537
969884


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   19187
75413487  
00016717  00000-0  10270-3 0  9024
2 25544  51
6394 264
1994 0007200 114
1621 246
0283 15
50960296 18287


Satellite: ISS
Catalog Number: 25544
Epoch time:      19187
75413487   =   yrday
fracday
Element set:     902
Inclination:       51
6394  deg
RA of node:       264
1994  deg
Eccentricity:     
0007200     
Arg of perigee:   114
1621  deg
Mean anomaly:     246
0283  deg
Mean motion:   15
50960296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1828
Checksum:              315


Coasting Arc #4 (Orbit 1842)
---------------------------------------

Vector Time (GMT): 2019/188/16:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4221137
66                 A    =         6786672
70  meter
 Y    =         592868
69  meter          E    =           
0021586
 Z    =       -5299683
82                 I    =           51
24147
 XDOT =      -1342
567663                 Wp   =           99
94677
 YDOT =      -7525
239035  meter/sec      RA   =          258
53251  deg
 ZDOT =        224
630548                 TA   =          172
22875
                                          MA   =          172
19525
                                          Ha   =            228
550  n
mi
                                          Hp   =            217
055

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13848876
85                 X    =        -4201711
07
 Y    =        1945107
26  feet           Y    =          545774
11  meter
 Z    =      -17387414
11                 Z    =        -5320140
96
 XDOT =      -4404
749552                 XDOT =       -1259
409615
 YDOT =     -24689
104445  feet/sec       YDOT =       -7539
787624  meter/sec
 ZDOT =        736
976863                 ZDOT =         218
310203

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13785149
09                 X    =         4201713
44
 Y    =       -1519017
51  feet           Y    =         -462996
54  meter
 Z    =      -17480253
20                 Z    =        -5327981
17
 XDOT =       3534
411547                 XDOT =        1077
288639
 YDOT =      23808
211154  feet/sec       YDOT =        7256
742760  meter/sec
 ZDOT =        709
002586                 ZDOT =         216
103988


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   19188
72063648  
00016717  00000-0  10270-3 0  9033
2 25544  51
6397 259
4045 0007230 116
8414 243
3477 15
50942295 18437


Satellite: ISS
Catalog Number: 25544
Epoch time:      19188
72063648   =   yrday
fracday
Element set:     903
Inclination:       51
6397  deg
RA of node:       259
4045  deg
Eccentricity:     
0007230     
Arg of perigee:   116
8414  deg
Mean anomaly:     243
3477  deg
Mean motion:   15
50942295  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1843
Checksum:              324


Coasting Arc #5 (Orbit 1858)
---------------------------------------

Vector Time (GMT): 2019/189/16:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4328234
02                 A    =         6786875
60  meter
 Y    =        -130801
15  meter          E    =           
0009298
 Z    =        5217793
42                 I    =           51
24885
 XDOT =       1396
961858                 Wp   =          100
74015
 YDOT =       7479
640640  meter/sec      RA   =          253
53888  deg
 ZDOT =       -971
523432                 TA   =          358
60492
                                          MA   =          358
60751
                                          Ha   =            228
287  n
mi
                                          Hp   =            217
301

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14200242
85                 X    =         4304030
16
 Y    =        -429137
64  feet           Y    =          -82535
59  meter
 Z    =       17118744
82                 Z    =         5238759
31
 XDOT =       4583
208195                 XDOT =        1317
937613
 YDOT =      24539
503413  feet/sec       YDOT =        7494
820681  meter/sec
 ZDOT =      -3187
412835                 ZDOT =        -964
928874

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14089372
01                 X    =        -4294440
59
 Y    =         235277
14  feet           Y    =           71712
47  meter
 Z    =       17213852
60                 Z    =         5246782
27
 XDOT =      -4251
267289                 XDOT =       -1295
786270
 YDOT =     -23572
569470  feet/sec       YDOT =       -7184
919174  meter/sec
 ZDOT =      -3158
169352                 ZDOT =        -962
610019


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   19189
75156909  
00016717  00000-0  10270-3 0  9041
2 25544  51
6384 254
2895 0007090 120
3202 239
8651 15
50964498 18598


Satellite: ISS
Catalog Number: 25544
Epoch time:      19189
75156909   =   yrday
fracday
Element set:     904
Inclination:       51
6384  deg
RA of node:       254
2895  deg
Eccentricity:     
0007090     
Arg of perigee:   120
3202  deg
Mean anomaly:     239
8651  deg
Mean motion:   15
50964498  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1859
Checksum:              343


Coasting Arc #6 (Orbit 1873)
---------------------------------------

Vector Time (GMT): 2019/190/16:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4506022
16                 A    =         6787604
87  meter
 Y    =        -313268
65  meter          E    =           
0020153
 Z    =       -5084756
08                 I    =           51
26162
 XDOT =      -1411
340383                 Wp   =          110
07734
 YDOT =      -7321
568009  meter/sec      RA   =          248
54677  deg
 ZDOT =       1700
518639                 TA   =          176
49245
                                          MA   =          176
47830
                                          Ha   =            228
446  n
mi
                                          Hp   =            217
214

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14783537
28                 X    =        -4477485
48
 Y    =       -1027784
29  feet           Y    =         -363498
14  meter
 Z    =      -16682270
61                 Z    =        -5106575
20
 XDOT =      -4630
381833                 XDOT =       -1337
623727
 YDOT =     -24020
892417  feet/sec       YDOT =       -7336
938585  meter/sec
 ZDOT =       5579
129394                 ZDOT =        1693
841311

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14674581
71                 X    =         4472812
50
 Y    =         977220
10  feet           Y    =          297856
69  meter
 Z    =      -16781214
51                 Z    =        -5114914
18
 XDOT =       4823
629674                 XDOT =        1470
242325
 YDOT =      22933
842804  feet/sec       YDOT =        6990
235287  meter/sec
 ZDOT =       5549
478427                 ZDOT =        1691
481024


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   19190
71806846  
00016717  00000-0  10270-3 0  9052
2 25544  51
6385 249
4947 0007101 123
4777 236
7054 15
50942633 18744


Satellite: ISS
Catalog Number: 25544
Epoch time:      19190
71806846   =   yrday
fracday
Element set:     905
Inclination:       51
6385  deg
RA of node:       249
4947  deg
Eccentricity:     
0007101     
Arg of perigee:   123
4777  deg
Mean anomaly:     236
7054  deg
Mean motion:   15
50942633  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1874
Checksum:              330


Coasting Arc #7 (Orbit 1877)
---------------------------------------

Vector Time (GMT): 2019/190/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2872077
76                 A    =         6787776
04  meter
 Y    =        3572788
35  meter          E    =           
0018167
 Z    =       -5021608
25                 I    =           51
26963
 XDOT =      -4216
373654                 Wp   =           92
29777
 YDOT =      -6086
032480  meter/sec      RA   =          247
32415  deg
 ZDOT =      -1925
359477                 TA   =          158
91821
                                          MA   =          158
84323
                                          Ha   =            228
274  n
mi
                                          Hp   =            217
288

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9422827
31                 X    =        -2887424
24
 Y    =       11721746
55  feet           Y    =         3540585
42  meter
 Z    =      -16475092
68                 Z    =        -5035596
57
 XDOT =     -13833
246895                 XDOT =       -4138
652264
 YDOT =     -19967
298163  feet/sec       YDOT =       -6132
748183  meter/sec
 ZDOT =      -6316
796186                 ZDOT =       -1945
652697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11873355
63                 X    =        -3618998
80
 Y    =       -9116328
26  feet           Y    =        -2778656
85  meter
 Z    =      -16538853
67                 Z    =        -5041042
60
 XDOT =      19071
663493                 XDOT =        5813
043033
 YDOT =     -13253
675804  feet/sec       YDOT =       -4039
720385  meter/sec
 ZDOT =      -6408
320472                 ZDOT =       -1953
256080


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   19190
97580125  
00016717  00000-0  10270-3 0  9060
2 25544  51
6425 248
2172 0006901 124
4552 235
7252 15
50988453 18788


Satellite: ISS
Catalog Number: 25544
Epoch time:      19190
97580125   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:       248
2172  deg
Eccentricity:     
0006901     
Arg of perigee:   124
4552  deg
Mean anomaly:     235
7252  deg
Mean motion:   15
50988453  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1878
Checksum:              322


Coasting Arc #8 (Orbit 1893)
---------------------------------------

Vector Time (GMT): 2019/191/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3038412
12                 A    =         6787023
48  meter
 Y    =       -3149793
93  meter          E    =           
0011021
 Z    =        5181088
72                 I    =           51
28173
 XDOT =       4347
500831                 Wp   =          127
11371
 YDOT =       6200
506372  meter/sec      RA   =          242
33326  deg
 ZDOT =       1211
654792                 TA   =          311
15597
                                          MA   =          311
25100
                                          Ha   =            228
161  n
mi
                                          Hp   =            217
480

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9968543
71                 X    =         3048241
46
 Y    =      -10333969
59  feet           Y    =        -3115761
87  meter
 Z    =       16998322
56                 Z    =         5195871
66
 XDOT =      14263
454170                 XDOT =        4271
956358
 YDOT =      20342
868676  feet/sec       YDOT =        6248
700651  meter/sec
 ZDOT =       3975
245381                 ZDOT =        1232
590416

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10659699
42                 X    =         3249076
38
 Y    =        9499481
07  feet           Y    =         2895441
83  meter
 Z    =       17065650
55                 Z    =         5201610
29
 XDOT =     -19158
070638                 XDOT =       -5839
379930
 YDOT =      14137
943162  feet/sec       YDOT =        4309
245076  meter/sec
 ZDOT =       4069
691568                 ZDOT =        1240
441990


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   19192
00673021  
00016717  00000-0  10270-3 0  9075
2 25544  51
6432 243
1024 0006909 128
6475 231
5295 15
50985163 18948


Satellite: ISS
Catalog Number: 25544
Epoch time:      19192
00673021   =   yrday
fracday
Element set:     907
Inclination:       51
6432  deg
RA of node:       243
1024  deg
Eccentricity:     
0006909     
Arg of perigee:   128
6475  deg
Mean anomaly:     231
5295  deg
Mean motion:   15
50985163  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1894
Checksum:              307


Coasting Arc #9 (Orbit 1908)
---------------------------------------

Vector Time (GMT): 2019/192/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3291566
12                 A    =         6786578
80  meter
 Y    =        2721291
86  meter          E    =           
0020136
 Z    =       -5291260
23                 I    =           51
29630
 XDOT =      -4422
409975                 Wp   =          100
29286
 YDOT =      -6224
187747  meter/sec      RA   =          237
34244  deg
 ZDOT =       -455
031645                 TA   =          165
36438
                                          MA   =          165
30600
                                          Ha   =            228
162  n
mi
                                          Hp   =            217
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10799101
44                 X    =        -3296049
85
 Y    =        8928122
90  feet           Y    =         2684458
85  meter
 Z    =      -17359777
67                 Z    =        -5307259
92
 XDOT =     -14509
219079                 XDOT =       -4350
270360
 YDOT =     -20420
563475  feet/sec       YDOT =       -6273
238823  meter/sec
 ZDOT =      -1492
885973                 ZDOT =        -476
339547

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9459676
20                 X    =        -2883309
31
 Y    =      -10213380
17  feet           Y    =        -3113038
28  meter
 Z    =      -17432591
40                 Z    =        -5313453
86
 XDOT =      18910
567969                 XDOT =        5763
941117
 YDOT =     -14830
761409  feet/sec       YDOT =       -4520
416078  meter/sec
 ZDOT =      -1589
037535                 ZDOT =        -484
338641


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   19192
97322422  
00016717  00000-0  10270-3 0  9088
2 25544  51
6427 238
3073 0006806 131
1140 229
0600 15
50994354 19097


Satellite: ISS
Catalog Number: 25544
Epoch time:      19192
97322422   =   yrday
fracday
Element set:     908
Inclination:       51
6427  deg
RA of node:       238
3073  deg
Eccentricity:     
0006806     
Arg of perigee:   131
1140  deg
Mean anomaly:     229
0600  deg
Mean motion:   15
50994354  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1909
Checksum:              299


Coasting Arc #10 (Orbit 1924)
---------------------------------------

Vector Time (GMT): 2019/193/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3553734
51                 A    =         6786499
60  meter
 Y    =       -2324692
73  meter          E    =           
0008442
 Z    =        5287246
54                 I    =           51
31428
 XDOT =       4492
642231                 Wp   =          121
21055
 YDOT =       6208
992346  meter/sec      RA   =          232
35351  deg
 ZDOT =       -293
638729                 TA   =          331
57784
                                          MA   =          331
62385
                                          Ha   =            228
005  n
mi
                                          Hp   =            217
651

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11659233
94                 X    =         3553783
40
 Y    =       -7626944
66  feet           Y    =        -2284952
87  meter
 Z    =       17346609
39                 Z    =         5304508
95
 XDOT =      14739
639864                 XDOT =        4424
303923
 YDOT =      20370
709796  feet/sec       YDOT =        6258
850162  meter/sec
 ZDOT =       -963
381657                 ZDOT =        -271
980358

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8394406
93                 X    =         2558615
23
 Y    =       10995992
74  feet           Y    =         3351578
59  meter
 Z    =       17425124
22                 Z    =         5311177
86
 XDOT =     -18516
891672                 XDOT =       -5643
948582
 YDOT =      15487
193108  feet/sec       YDOT =        4720
496459  meter/sec
 ZDOT =       -865
618587                 ZDOT =        -263
840545


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   19194
00414985  
00016717  00000-0  10270-3 0  9091
2 25544  51
6419 233
1931 0006825 135
6072 224
5627 15
50996120 19258


Satellite: ISS
Catalog Number: 25544
Epoch time:      19194
00414985   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:       233
1931  deg
Eccentricity:     
0006825     
Arg of perigee:   135
6072  deg
Mean anomaly:     224
5627  deg
Mean motion:   15
50996120  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1925
Checksum:              313


Coasting Arc #11 (Orbit 1939)
---------------------------------------

Vector Time (GMT): 2019/194/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3885960
05                 A    =         6786848
08  meter
 Y    =        1953918
70  meter          E    =           
0019852
 Z    =       -5227096
84                 I    =           51
33618
 XDOT =      -4484
168749                 Wp   =          111
05704
 YDOT =      -6107
288213  meter/sec      RA   =          227
36508  deg
 ZDOT =       1046
952795                 TA   =          169
06077
                                          MA   =          169
01754
                                          Ha   =            228
027  n
mi
                                          Hp   =            217
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12749212
77                 X    =        -3882130
40
 Y    =        6410494
44  feet           Y    =         1910485
40  meter
 Z    =      -17149267
86                 Z    =        -5245963
62
 XDOT =     -14711
839729                 XDOT =       -4420
627503
 YDOT =     -20037
034821  feet/sec       YDOT =       -6157
078216  meter/sec
 ZDOT =       3434
884498                 ZDOT =        1025
323933

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7463365
96                 X    =        -2274833
95
 Y    =      -12041005
57  feet           Y    =        -3670098
50  meter
 Z    =      -17235040
09                 Z    =        -5253240
22
 XDOT =      17829
228682                 XDOT =        5434
348902
 YDOT =     -15845
402874  feet/sec       YDOT =       -4829
678796  meter/sec
 ZDOT =       3337
224927                 ZDOT =        1017
186158


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   19194
97064212  
00016717  00000-0  10270-3 0  9103
2 25544  51
6415 228
3978 0006713 139
1561 221
0094 15
50994218 19402


Satellite: ISS
Catalog Number: 25544
Epoch time:      19194
97064212   =   yrday
fracday
Element set:     910
Inclination:       51
6415  deg
RA of node:       228
3978  deg
Eccentricity:     
0006713     
Arg of perigee:   139
1561  deg
Mean anomaly:     221
0094  deg
Mean motion:   15
50994218  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1940
Checksum:              309


Coasting Arc #12 (Orbit 1955)
---------------------------------------

Vector Time (GMT): 2019/195/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4216888
38                 A    =         6787443
32  meter
 Y    =       -1624260
59  meter          E    =           
0008598
 Z    =        5056665
37                 I    =           51
36206
 XDOT =       4447
039831                 Wp   =          105
59110
 YDOT =       5988
860447  meter/sec      RA   =          222
37917  deg
 ZDOT =      -1784
544362                 TA   =            1
74014
                                          MA   =            1
73715
                                          Ha   =            227
763  n
mi
                                          Hp   =            217
894

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13834935
62                 X    =         4210175
75
 Y    =       -5328938
94  feet           Y    =        -1577142
74  meter
 Z    =       16590109
48                 Z    =         5077132
62
 XDOT =      14590
025691                 XDOT =        4388
408385
 YDOT =      19648
492280  feet/sec       YDOT =        6038
262826  meter/sec
 ZDOT =      -5854
804337                 ZDOT =       -1763
083998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6705115
46                 X    =         2043719
19
 Y    =       13105319
99  feet           Y    =         3994501
53  meter
 Z    =       16683128
63                 Z    =         5085017
61
 XDOT =     -17091
072177                 XDOT =       -5209
358800
 YDOT =      16075
273699  feet/sec       YDOT =        4899
743423  meter/sec
 ZDOT =      -5757
876103                 ZDOT =       -1755
000636


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   19196
00156300  
00016717  00000-0  10270-3 0  9110
2 25544  51
6417 223
2829 0006587 143
3862 216
7740 15
51014033 19568


Satellite: ISS
Catalog Number: 25544
Epoch time:      19196
00156300   =   yrday
fracday
Element set:     911
Inclination:       51
6417  deg
RA of node:       223
2829  deg
Eccentricity:     
0006587     
Arg of perigee:   143
3862  deg
Mean anomaly:     216
7740  deg
Mean motion:   15
51014033  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1956
Checksum:              292


Coasting Arc #13 (Orbit 1970)
---------------------------------------

Vector Time (GMT): 2019/196/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4593244
46                 A    =         6788508
09  meter
 Y    =        1344825
66  meter          E    =           
0017401
 Z    =       -4830804
41                 I    =           51
38898
 XDOT =      -4318
634118                 Wp   =          121
74101
 YDOT =      -5802
677289  meter/sec      RA   =          217
39448  deg
 ZDOT =       2488
551477                 TA   =          172
87468
                                          MA   =          172
84991
                                          Ha   =            227
899  n
mi
                                          Hp   =            217
830

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15069699
66                 X    =        -4584476
32
 Y    =        4412157
67  feet           Y    =         1293510
57  meter
 Z    =      -15849095
84                 Z    =        -4853094
81
 XDOT =     -14168
747105                 XDOT =       -4265
513756
 YDOT =     -19037
655148  feet/sec       YDOT =       -5850
674665  meter/sec
 ZDOT =       8164
538966                 ZDOT =        2467
701597

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6167537
04                 X    =        -1879865
29
 Y    =      -14328422
14  feet           Y    =        -4367303
07  meter
 Z    =      -15950380
18                 Z    =        -4861675
88
 XDOT =      16156
157435                 XDOT =        4924
396786
 YDOT =     -15946
612259  feet/sec       YDOT =       -4860
527417  meter/sec
 ZDOT =       8070
342188                 ZDOT =        2459
840299


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   19196
96805139  
00016717  00000-0  10270-3 0  9127
2 25544  51
6399 218
4866 0006648 146
0859 214
0719 15
50994996 19716


Satellite: ISS
Catalog Number: 25544
Epoch time:      19196
96805139   =   yrday
fracday
Element set:     912
Inclination:       51
6399  deg
RA of node:       218
4866  deg
Eccentricity:     
0006648     
Arg of perigee:   146
0859  deg
Mean anomaly:     214
0719  deg
Mean motion:   15
50994996  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1971
Checksum:              367


Coasting Arc #14 (Orbit 1986)
---------------------------------------

Vector Time (GMT): 2019/197/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4950351
45                 A    =         6789672
41  meter
 Y    =       -1110056
72  meter          E    =           
0011553
 Z    =        4501268
70                 I    =           51
42027
 XDOT =       4144
604052                 Wp   =          101
85979
 YDOT =       5624
002137  meter/sec      RA   =          212
41481  deg
 ZDOT =      -3166
598974                 TA   =           20
03986
                                          MA   =           19
99454
                                          Ha   =            227
607  n
mi
                                          Hp   =            218
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16241310
54                 X    =         4940532
27
 Y    =       -3641918
38  feet           Y    =        -1054753
99  meter
 Z    =       14767941
92                 Z    =         4525291
18
 XDOT =      13597
782324                 XDOT =        4096
788096
 YDOT =      18451
450582  feet/sec       YDOT =        5670
083119  meter/sec
 ZDOT =     -10389
104244                 ZDOT =       -3146
581729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5811127
30                 X    =         1771231
60
 Y    =       15493191
81  feet           Y    =         4722324
86  meter
 Z    =       14877084
83                 Z    =         4534535
46
 XDOT =     -15281
703921                 XDOT =       -4657
863355
 YDOT =      15635
205520  feet/sec       YDOT =        4765
610642  meter/sec
 ZDOT =     -10298
648738                 ZDOT =       -3139
028135


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   19197
99896962  
00016717  00000-0  10270-3 0  9136
2 25544  51
6398 213
3724 0006529 150
5951 209
5569 15
51019836 19874


Satellite: ISS
Catalog Number: 25544
Epoch time:      19197
99896962   =   yrday
fracday
Element set:     913
Inclination:       51
6398  deg
RA of node:       213
3724  deg
Eccentricity:     
0006529     
Arg of perigee:   150
5951  deg
Mean anomaly:     209
5569  deg
Mean motion:   15
51019836  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1987
Checksum:              364


Coasting Arc #15 (Orbit 2001)
---------------------------------------

Vector Time (GMT): 2019/198/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5323374
51                 A    =         6791150
14  meter
 Y    =         939983
98  meter          E    =           
0013200
 Z    =       -4125484
03                 I    =           51
45307
 XDOT =      -3881
269182                 Wp   =          130
73917
 YDOT =      -5405
112358  meter/sec      RA   =          207
43645  deg
 ZDOT =       3776
235752                 TA   =          178
39164
                                          MA   =          178
38739
                                          Ha   =            227
738  n
mi
                                          Hp   =            218
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17465139
45                 X    =        -5313451
16
 Y    =        3083936
95  feet           Y    =          880510
30  meter
 Z    =      -13535052
59                 Z    =        -4151318
21
 XDOT =     -12733
822774                 XDOT =       -3838
881661
 YDOT =     -17733
308262  feet/sec       YDOT =       -5448
278924  meter/sec
 ZDOT =      12389
224907                 ZDOT =        3757
484647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5714718
42                 X    =        -1741846
17
 Y    =      -16694093
19  feet           Y    =        -5088359
61  meter
 Z    =      -13652423
14                 Z    =        -4161258
57
 XDOT =      14336
334924                 XDOT =        4369
714885
 YDOT =     -14971
453032  feet/sec       YDOT =       -4563
298884  meter/sec
 ZDOT =      12304
477966                 ZDOT =        3750
404884


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   19198
96545543  
00016717  00000-0  10270-3 0  9141
2 25544  51
6392 208
5759 0006640 154
6502 205
4976 15
50998546 20022


Satellite: ISS
Catalog Number: 25544
Epoch time:      19198
96545543   =   yrday
fracday
Element set:     914
Inclination:       51
6392  deg
RA of node:       208
5759  deg
Eccentricity:     
0006640     
Arg of perigee:   154
6502  deg
Mean anomaly:     205
4976  deg
Mean motion:   15
50998546  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2002
Checksum:              337


Coasting Arc #16 (Orbit 2017)
---------------------------------------

Vector Time (GMT): 2019/199/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5657572
13                 A    =         6792601
34  meter
 Y    =        -807744
73  meter          E    =           
0014964
 Z    =        3654517
73                 I    =           51
48888
 XDOT =       3561
274970                 Wp   =          109
82633
 YDOT =       5218
348668  meter/sec      RA   =          202
46244  deg
 ZDOT =      -4350
282091                 TA   =           26
66293
                                          MA   =           26
58606
                                          Ha   =            227
451  n
mi
                                          Hp   =            218
343

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18561588
34                 X    =         5648432
86
 Y    =       -2650081
15  feet           Y    =         -744529
30  meter
 Z    =       11989887
55                 Z    =         3681977
19
 XDOT =      11683
972998                 XDOT =        3523
787995
 YDOT =      17120
566496  feet/sec       YDOT =        5257
964228  meter/sec
 ZDOT =     -14272
579038                 ZDOT =       -4333
073603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5762411
41                 X    =         1756383
00
 Y    =       17757897
01  feet           Y    =         5412607
01  meter
 Z    =       12114644
18                 Z    =         3692543
55
 XDOT =     -13564
770441                 XDOT =       -4134
542030
 YDOT =      14106
757687  feet/sec       YDOT =        4299
739743  meter/sec
 ZDOT =     -14194
801834                 ZDOT =       -4326
575599


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   19199
99636908  
00016717  00000-0  10270-3 0  9152
2 25544  51
6398 203
4603 0006473 158
2235 201
9192 15
51023146 20181


Satellite: ISS
Catalog Number: 25544
Epoch time:      19199
99636908   =   yrday
fracday
Element set:     915
Inclination:       51
6398  deg
RA of node:       203
4603  deg
Eccentricity:     
0006473     
Arg of perigee:   158
2235  deg
Mean anomaly:     201
9192  deg
Mean motion:   15
51023146  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2018
Checksum:              317


Coasting Arc #17 (Orbit 2032)
---------------------------------------

Vector Time (GMT): 2019/200/22:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5978517
48                 A    =         6794150
67  meter
 Y    =         743438
73  meter          E    =           
0008608
 Z    =       -3153155
93                 I    =           51
52314
 XDOT =      -3169
014940                 Wp   =          130
11056
 YDOT =      -5021
843811  meter/sec      RA   =          197
49216  deg
 ZDOT =       4827
891647                 TA   =          193
56696
                                          MA   =          193
59012
                                          Ha   =            227
632  n
mi
                                          Hp   =            218
354

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19614558
68                 X    =        -5971070
56
 Y    =        2439103
46  feet           Y    =          676624
69  meter
 Z    =      -10344999
78                 Z    =        -3182178
54
 XDOT =     -10397
030642                 XDOT =       -3136
074415
 YDOT =     -16475
865523  feet/sec       YDOT =       -5057
098229  meter/sec
 ZDOT =      15839
539524                 ZDOT =        4812
577633

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6059370
61                 X    =        -1846896
16
 Y    =      -18740823
13  feet           Y    =        -5712202
89  meter
 Z    =      -10476866
63                 Z    =        -3193348
95
 XDOT =      12846
937543                 XDOT =        3915
746563
 YDOT =     -12963
935967  feet/sec       YDOT =       -3951
407683  meter/sec
 ZDOT =      15770
333530                 ZDOT =        4806
797660


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   19200
96285162  
00016717  00000-0  10270-3 0  9165
2 25544  51
6379 198
6646 0006716 161
2548 198
8851 15
50995132 20338


Satellite: ISS
Catalog Number: 25544
Epoch time:      19200
96285162   =   yrday
fracday
Element set:     916
Inclination:       51
6379  deg
RA of node:       198
6646  deg
Eccentricity:     
0006716     
Arg of perigee:   161
2548  deg
Mean anomaly:     198
8851  deg
Mean motion:   15
50995132  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2033
Checksum:              337
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