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

 
Date: July 10th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14148 2991 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


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

201/16:28:21 000 0 0 0 0 0 0
N/A 0 0 0 0 227 5
000/00:00:00 000 0 0 0 0 218 5

201/22:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 4
000/00:00:00 000 0 0 0 0 218 6

202/23:35:11 000 0 0 0 0 0 0
N/A 0 0 0 0 227 4
000/00:00:00 000 0 0 0 0 218 7

203/02:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 5
000/00:00:00 000 0 0 0 0 218 7

203/20:57:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 4
000/00:00:00 000 0 0 0 0 218 9

204/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 4
000/00:00:00 000 0 0 0 0 218 9

Coasting Arc #1 (Orbit 1855)
---------------------------------------

Vector Time (GMT): 2019/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         837141
43                 A    =         6794699
92  meter
 Y    =       -6029639
73  meter          E    =           
0019214
 Z    =        3004535
36                 I    =           51
27618
 XDOT =       4961
268292                 Wp   =           96
62271
 YDOT =       3154
847969  meter/sec      RA   =          254
59132  deg
 ZDOT =       4919
580554                 TA   =          297
93920
                                          MA   =          298
13358
                                          Ha   =            228
414  n
mi
                                          Hp   =            217
291

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2746527
01                 X    =          889910
20
 Y    =      -19782282
56  feet           Y    =        -6019983
44  meter
 Z    =        9857399
47                 Z    =         3008729
46
 XDOT =      16277
126943                 XDOT =        4901
724867
 YDOT =      10350
551081  feet/sec       YDOT =        3209
994990  meter/sec
 ZDOT =      16140
356148                 ZDOT =        4943
535890

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19789379
36                 X    =        -6031802
83
 Y    =        2622304
78  feet           Y    =          799278
50  meter
 Z    =        9876964
13                 Z    =         3010498
67
 XDOT =       5921
022742                 XDOT =        1804
727732
 YDOT =     -16880
093378  feet/sec       YDOT =       -5145
052461  meter/sec
 ZDOT =      16248
727179                 ZDOT =        4952
612044


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
55827166  
00016717  00000-0  10270-3 0  9005
2 25544  51
6416 255
2474 0007124 121
7590 238
4256 15
50970751 18563


Satellite: ISS
Catalog Number: 25544
Epoch time:      19189
55827166   =   yrday
fracday
Element set:     900
Inclination:       51
6416  deg
RA of node:       255
2474  deg
Eccentricity:     
0007124     
Arg of perigee:   121
7590  deg
Mean anomaly:     238
4256  deg
Mean motion:   15
50970751  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1856
Checksum:              322


Coasting Arc #2 (Orbit 1870)
---------------------------------------

Vector Time (GMT): 2019/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -912539
58                 A    =         6793216
71  meter
 Y    =        5721100
33  meter          E    =           
0011648
 Z    =       -3553558
97                 I    =           51
28020
 XDOT =      -5120
916324                 Wp   =          108
03644
 YDOT =      -3563
761709  meter/sec      RA   =          249
60645  deg
 ZDOT =      -4438
080681                 TA   =          114
04179
                                          MA   =          113
91985
                                          Ha   =            228
421  n
mi
                                          Hp   =            217
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2993896
27                 X    =         -959185
68
 Y    =       18770014
22  feet           Y    =         5710635
18  meter
 Z    =      -11658658
03                 Z    =        -3558104
49
 XDOT =     -16800
906575                 XDOT =       -5059
127179
 YDOT =     -11692
131591  feet/sec       YDOT =       -3620
681510  meter/sec
 ZDOT =     -14560
632155                 ZDOT =       -4462
806206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18835230
80                 X    =         5740978
35
 Y    =       -2453172
19  feet           Y    =         -747726
88  meter
 Z    =      -11679776
65                 Z    =        -3559995
92
 XDOT =      -6731
005802                 XDOT =       -2051
610568
 YDOT =      17933
938923  feet/sec       YDOT =        5466
264584  meter/sec
 ZDOT =     -14672
473578                 ZDOT =       -4472
169947


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
52477387  
00016717  00000-0  10270-3 0  9011
2 25544  51
6407 250
4526 0007187 124
9708 235
2119 15
50955741 18715


Satellite: ISS
Catalog Number: 25544
Epoch time:      19190
52477387   =   yrday
fracday
Element set:     901
Inclination:       51
6407  deg
RA of node:       250
4526  deg
Eccentricity:     
0007187     
Arg of perigee:   124
9708  deg
Mean anomaly:     235
2119  deg
Mean motion:   15
50955741  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1871
Checksum:              320


Coasting Arc #3 (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    =       -2869890
06                 A    =         6787791
72  meter
 Y    =        3575952
66  meter          E    =           
0018161
 Z    =       -5020622
13                 I    =           51
26961
 XDOT =      -4218
275309                 Wp   =           92
27330
 YDOT =      -6083
669928  meter/sec      RA   =          247
32389  deg
 ZDOT =      -1928
641570                 TA   =          158
90938
                                          MA   =          158
83440
                                          Ha   =            228
280  n
mi
                                          Hp   =            217
293

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9415649
82                 X    =        -2885276
87
 Y    =       11732128
14  feet           Y    =         3543773
97  meter
 Z    =      -16471857
38                 Z    =        -5034599
93
 XDOT =     -13839
485922                 XDOT =       -4140
564254
 YDOT =     -19959
547007  feet/sec       YDOT =       -6130
406954  meter/sec
 ZDOT =      -6327
564206                 ZDOT =       -1948
944052

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11883617
42                 X    =        -3622126
59
 Y    =       -9109001
61  feet           Y    =        -2776423
69  meter
 Z    =      -16535570
88                 Z    =        -5040042
01
 XDOT =      19064
346195                 XDOT =        5810
812720
 YDOT =     -13258
964700  feet/sec       YDOT =       -4041
332441  meter/sec
 ZDOT =      -6419
130712                 ZDOT =       -1956
551041


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
97580728  
00016717  00000-0  10270-3 0  9025
2 25544  51
6425 248
2171 0006900 124
4102 235
7703 15
50984542 18783


Satellite: ISS
Catalog Number: 25544
Epoch time:      19190
97580728   =   yrday
fracday
Element set:     902
Inclination:       51
6425  deg
RA of node:       248
2171  deg
Eccentricity:     
0006900     
Arg of perigee:   124
4102  deg
Mean anomaly:     235
7703  deg
Mean motion:   15
50984542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1878
Checksum:              312


Coasting Arc #4 (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    =        3035138
70                 A    =         6787041
18  meter
 Y    =       -3154468
70  meter          E    =           
0011031
 Z    =        5180183
70                 I    =           51
28172
 XDOT =       4350
436366                 Wp   =          127
09344
 YDOT =       6197
463915  meter/sec      RA   =          242
33305  deg
 ZDOT =       1216
624862                 TA   =          311
12756
                                          MA   =          311
22273
                                          Ha   =            228
168  n
mi
                                          Hp   =            217
487

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9957804
12                 X    =         3045024
95
 Y    =      -10349306
77  feet           Y    =        -3120472
93  meter
 Z    =       16995353
36                 Z    =         5194950
88
 XDOT =      14273
085191                 XDOT =        4274
901555
 YDOT =      20332
886860  feet/sec       YDOT =        6245
691075  meter/sec
 ZDOT =       3991
551386                 ZDOT =        1237
574769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10674666
06                 X    =         3253638
21
 Y    =        9488249
87  feet           Y    =         2892018
56  meter
 Z    =       17062610
24                 Z    =         5200683
60
 XDOT =     -19148
593078                 XDOT =       -5836
491170
 YDOT =      14146
030478  feet/sec       YDOT =        4311
710090  meter/sec
 ZDOT =       4086
062624                 ZDOT =        1245
431888


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
00673907  
00016717  00000-0  10270-3 0  9034
2 25544  51
6432 243
1023 0006908 128
6023 231
5748 15
50980517 18946


Satellite: ISS
Catalog Number: 25544
Epoch time:      19192
00673907   =   yrday
fracday
Element set:     903
Inclination:       51
6432  deg
RA of node:       243
1023  deg
Eccentricity:     
0006908     
Arg of perigee:   128
6023  deg
Mean anomaly:     231
5748  deg
Mean motion:   15
50980517  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1894
Checksum:              304


Coasting Arc #5 (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    =       -3287029
86                 A    =         6786596
23  meter
 Y    =        2727691
89  meter          E    =           
0020132
 Z    =       -5290802
06                 I    =           51
29628
 XDOT =      -4426
692921                 Wp   =          100
24432
 YDOT =      -6220
629599  meter/sec      RA   =          237
34228  deg
 ZDOT =       -461
901348                 TA   =          165
34682
                                          MA   =          165
28837
                                          Ha   =            228
171  n
mi
                                          Hp   =            217
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10784218
69                 X    =        -3291587
72
 Y    =        8949120
39  feet           Y    =         2690909
20  meter
 Z    =      -17358274
47                 Z    =        -5306779
89
 XDOT =     -14523
270739                 XDOT =       -4354
559407
 YDOT =     -20408
889762  feet/sec       YDOT =       -6269
728603  meter/sec
 ZDOT =      -1515
424369                 ZDOT =        -483
230069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9479888
68                 X    =        -2889470
07
 Y    =      -10197457
24  feet           Y    =        -3108184
97  meter
 Z    =      -17430989
58                 Z    =        -5312965
62
 XDOT =      18899
363776                 XDOT =        5760
526079
 YDOT =     -14842
574472  feet/sec       YDOT =       -4524
016699  meter/sec
 ZDOT =      -1611
670680                 ZDOT =        -491
237223


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
97323614  
00016717  00000-0  10270-3 0  9048
2 25544  51
6428 238
3072 0006806 131
0714 229
1026 15
50989141 19094


Satellite: ISS
Catalog Number: 25544
Epoch time:      19192
97323614   =   yrday
fracday
Element set:     904
Inclination:       51
6428  deg
RA of node:       238
3072  deg
Eccentricity:     
0006806     
Arg of perigee:   131
0714  deg
Mean anomaly:     229
1026  deg
Mean motion:   15
50989141  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1909
Checksum:              306


Coasting Arc #6 (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    =        3547743
37                 A    =         6786515
66  meter
 Y    =       -2332986
35  meter          E    =           
0008450
 Z    =        5287641
60                 I    =           51
31424
 XDOT =       4498
696881                 Wp   =          121
29132
 YDOT =       6205
010919  meter/sec      RA   =          232
35340  deg
 ZDOT =       -284
631759                 TA   =          331
41062
                                          MA   =          331
45693
                                          Ha   =            228
015  n
mi
                                          Hp   =            217
659

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11639577
99                 X    =         3547883
53
 Y    =       -7654154
70  feet           Y    =        -2293312
97  meter
 Z    =       17347905
53                 Z    =         5304875
13
 XDOT =      14759
504202                 XDOT =        4430
358894
 YDOT =      20357
647373  feet/sec       YDOT =        6254
936443  meter/sec
 ZDOT =       -933
831229                 ZDOT =        -262
943976

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8420214
00                 X    =         2566481
23
 Y    =       10974520
46  feet           Y    =         3345033
84  meter
 Z    =       17426289
99                 Z    =         5311533
19
 XDOT =     -18504
087630                 XDOT =       -5640
045910
 YDOT =      15504
040959  feet/sec       YDOT =        4725
631684  meter/sec
 ZDOT =       -835
934385                 ZDOT =        -254
792801


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
00416549  
00016717  00000-0  10270-3 0  9055
2 25544  51
6420 233
1930 0006825 135
5626 224
6074 15
50990097 19257


Satellite: ISS
Catalog Number: 25544
Epoch time:      19194
00416549   =   yrday
fracday
Element set:     905
Inclination:       51
6420  deg
RA of node:       233
1930  deg
Eccentricity:     
0006825     
Arg of perigee:   135
5626  deg
Mean anomaly:     224
6074  deg
Mean motion:   15
50990097  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1925
Checksum:              306


Coasting Arc #7 (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    =       -3878420
97                 A    =         6786859
69  meter
 Y    =        1964205
37  meter          E    =           
0019861
 Z    =       -5228861
62                 I    =           51
33613
 XDOT =      -4492
433277                 Wp   =          110
97690
 YDOT =      -6103
098093  meter/sec      RA   =          227
36504  deg
 ZDOT =       1035
812107                 TA   =          169
03246
                                          MA   =          168
98910
                                          Ha   =            228
038  n
mi
                                          Hp   =            217
634

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12724478
24                 X    =        -3874698
33
 Y    =        6444243
33  feet           Y    =         1920855
78  meter
 Z    =      -17155057
81                 Z    =        -5247692
03
 XDOT =     -14738
954321                 XDOT =       -4428
884157
 YDOT =     -20023
287706  feet/sec       YDOT =       -6152
980470  meter/sec
 ZDOT =       3398
333683                 ZDOT =        1014
143119

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7494878
94                 X    =        -2284439
10
 Y    =      -12013444
89  feet           Y    =        -3661698
00  meter
 Z    =      -17240665
85                 Z    =        -5254954
95
 XDOT =      17815
252576                 XDOT =        5430
088985
 YDOT =     -15868
703110  feet/sec       YDOT =       -4836
780708  meter/sec
 ZDOT =       3300
491689                 ZDOT =        1005
989867


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
97066165  
00016717  00000-0  10270-3 0  9067
2 25544  51
6415 228
3977 0006713 139
1134 221
0522 15
50987665 19401


Satellite: ISS
Catalog Number: 25544
Epoch time:      19194
97066165   =   yrday
fracday
Element set:     906
Inclination:       51
6415  deg
RA of node:       228
3977  deg
Eccentricity:     
0006713     
Arg of perigee:   139
1134  deg
Mean anomaly:     221
0522  deg
Mean motion:   15
50987665  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1940
Checksum:              322


Coasting Arc #8 (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    =        4207701
72                 A    =         6787449
56  meter
 Y    =       -1636644
73  meter          E    =           
0008578
 Z    =        5060349
40                 I    =           51
36198
 XDOT =       4458
144970                 Wp   =          105
71495
 YDOT =       5984
544842  meter/sec      RA   =          222
37918  deg
 ZDOT =      -1771
185454                 TA   =            1
48235
                                          MA   =            1
47980
                                          Ha   =            227
776  n
mi
                                          Hp   =            217
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13804795
68                 X    =         4201110
36
 Y    =       -5369569
34  feet           Y    =        -1589628
94  meter
 Z    =       16602196
21                 Z    =         5080772
33
 XDOT =      14626
459874                 XDOT =        4399
496067
 YDOT =      19634
333470  feet/sec       YDOT =        6034
071306  meter/sec
 ZDOT =      -5810
975898                 ZDOT =       -1749
671189

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6742436
75                 X    =         2055094
72
 Y    =       13071097
66  feet           Y    =         3984070
57  meter
 Z    =       16695015
14                 Z    =         5088640
61
 XDOT =     -17075
785512                 XDOT =       -5204
699424
 YDOT =      16107
051198  feet/sec       YDOT =        4909
429205  meter/sec
 ZDOT =      -5713
802694                 ZDOT =       -1741
567061


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
00158715  
00016717  00000-0  10270-3 0  9077
2 25544  51
6417 223
2829 0006587 143
3424 216
8179 15
51006565 19560


Satellite: ISS
Catalog Number: 25544
Epoch time:      19196
00158715   =   yrday
fracday
Element set:     907
Inclination:       51
6417  deg
RA of node:       223
2829  deg
Eccentricity:     
0006587     
Arg of perigee:   143
3424  deg
Mean anomaly:     216
8179  deg
Mean motion:   15
51006565  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1956
Checksum:              321


Coasting Arc #9 (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    =       -4582485
83                 A    =         6788506
33  meter
 Y    =        1359291
01  meter          E    =           
0017437
 Z    =       -4836998
07                 I    =           51
38887
 XDOT =      -4333
090153                 Wp   =          121
63908
 YDOT =      -5798
396276  meter/sec      RA   =          217
39454  deg
 ZDOT =       2473
280655                 TA   =          172
81597
                                          MA   =          172
79095
                                          Ha   =            227
912  n
mi
                                          Hp   =            217
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15034402
32                 X    =        -4573850
16
 Y    =        4459616
17  feet           Y    =         1308095
49  meter
 Z    =      -15869416
23                 Z    =        -4859236
53
 XDOT =     -14216
175042                 XDOT =       -4279
942412
 YDOT =     -19023
609828  feet/sec       YDOT =       -5846
555154  meter/sec
 ZDOT =       8114
437846                 ZDOT =        2452
360622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6210419
84                 X    =        -1892935
97
 Y    =      -14287571
69  feet           Y    =        -4354851
85  meter
 Z    =      -15970465
91                 Z    =        -4867798
01
 XDOT =      16139
567711                 XDOT =        4919
340238
 YDOT =     -15988
559662  feet/sec       YDOT =       -4873
312985  meter/sec
 ZDOT =       8019
922297                 ZDOT =        2444
472316


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
96808028  
00016717  00000-0  10270-3 0  9082
2 25544  51
6399 218
4866 0006647 146
0417 214
1160 15
50987052 19711


Satellite: ISS
Catalog Number: 25544
Epoch time:      19196
96808028   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:       218
4866  deg
Eccentricity:     
0006647     
Arg of perigee:   146
0417  deg
Mean anomaly:     214
1160  deg
Mean motion:   15
50987052  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1971
Checksum:              337


Coasting Arc #10 (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    =        4938111
04                 A    =         6789662
35  meter
 Y    =       -1126662
83  meter          E    =           
0011501
 Z    =        4510601
13                 I    =           51
42012
 XDOT =       4163
218420                 Wp   =          101
83096
 YDOT =       5619
774563  meter/sec      RA   =          212
41491  deg
 ZDOT =      -3149
585140                 TA   =           19
87736
                                          MA   =           19
83258
                                          Ha   =            227
622  n
mi
                                          Hp   =            218
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16201151
72                 X    =         4928433
13
 Y    =       -3696400
35  feet           Y    =        -1071496
18  meter
 Z    =       14798560
13                 Z    =         4534564
49
 XDOT =      13658
853085                 XDOT =        4115
365712
 YDOT =      18437
580587  feet/sec       YDOT =        5666
063495  meter/sec
 ZDOT =     -10333
284580                 ZDOT =       -3129
477566

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5859584
73                 X    =         1786001
43
 Y    =       15445766
28  feet           Y    =         4707869
56  meter
 Z    =       14907435
91                 Z    =         4543786
46
 XDOT =     -15263
137496                 XDOT =       -4652
204309
 YDOT =      15689
903719  feet/sec       YDOT =        4782
282654  meter/sec
 ZDOT =     -10242
418668                 ZDOT =       -3121
889210


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
99900405  
00016717  00000-0  10270-3 0  9099
2 25544  51
6398 213
3724 0006529 150
5533 209
5987 15
51011098 19876


Satellite: ISS
Catalog Number: 25544
Epoch time:      19197
99900405   =   yrday
fracday
Element set:     909
Inclination:       51
6398  deg
RA of node:       213
3724  deg
Eccentricity:     
0006529     
Arg of perigee:   150
5533  deg
Mean anomaly:     209
5987  deg
Mean motion:   15
51011098  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1987
Checksum:              339


Coasting Arc #11 (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    =       -5309950
85                 A    =         6791132
11  meter
 Y    =         958660
04  meter          E    =           
0013267
 Z    =       -4138509
91                 I    =           51
45289
 XDOT =      -3904
513870                 Wp   =          130
67505
 YDOT =      -5400
944968  meter/sec      RA   =          207
43659  deg
 ZDOT =       3758
109969                 TA   =          178
23297
                                          MA   =          178
22828
                                          Ha   =            227
753  n
mi
                                          Hp   =            218
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17421098
60                 X    =        -5300174
07
 Y    =        3145210
11  feet           Y    =          899335
65  meter
 Z    =      -13577788
41                 Z    =        -4164279
24
 XDOT =     -12810
084875                 XDOT =       -3862
083180
 YDOT =     -17719
635721  feet/sec       YDOT =       -5444
371228  meter/sec
 ZDOT =      12329
757115                 ZDOT =        3739
246058

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5768454
02                 X    =        -1758224
79
 Y    =      -16640881
84  feet           Y    =        -5072140
79  meter
 Z    =      -13694865
86                 Z    =        -4174195
11
 XDOT =      14315
058075                 XDOT =        4363
229701
 YDOT =     -15040
395737  feet/sec       YDOT =       -4584
312621  meter/sec
 ZDOT =      12244
497667                 ZDOT =        3732
122889


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
96549547  
00016717  00000-0  10270-3 0  9105
2 25544  51
6392 208
5760 0006638 154
6015 205
5463 15
50989222 20023


Satellite: ISS
Catalog Number: 25544
Epoch time:      19198
96549547   =   yrday
fracday
Element set:     910
Inclination:       51
6392  deg
RA of node:       208
5760  deg
Eccentricity:     
0006638     
Arg of perigee:   154
6015  deg
Mean anomaly:     205
5463  deg
Mean motion:   15
50989222  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2002
Checksum:              322


Coasting Arc #12 (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    =        5643322
28                 A    =         6792577
07  meter
 Y    =        -828579
82  meter          E    =           
0014899
 Z    =        3671860
80                 I    =           51
48867
 XDOT =       3590
059617                 Wp   =          109
64995
 YDOT =       5214
166917  meter/sec      RA   =          202
46259  deg
 ZDOT =      -4331
555176                 TA   =           26
58054
                                          MA   =           26
50422
                                          Ha   =            227
468  n
mi
                                          Hp   =            218
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18514836
88                 X    =         5634332
82
 Y    =       -2718437
74  feet           Y    =         -765522
91  meter
 Z    =       12046787
42                 Z    =         3699251
41
 XDOT =      11778
410818                 XDOT =        3552
526302
 YDOT =      17106
846842  feet/sec       YDOT =        5254
104106  meter/sec
 ZDOT =     -14211
139029                 ZDOT =       -4314
206979

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5821723
94                 X    =         1774461
46
 Y    =       17699796
53  feet           Y    =         5394897
98  meter
 Z    =       12171232
83                 Z    =         3709791
77
 XDOT =     -13539
456595                 XDOT =       -4126
826370
 YDOT =      14192
738100  feet/sec       YDOT =        4325
946573  meter/sec
 ZDOT =     -14132
727081                 ZDOT =       -4307
655214


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
99641559  
00016717  00000-0  10270-3 0  9116
2 25544  51
6398 203
4604 0006472 158
1787 201
9641 15
51012918 20186


Satellite: ISS
Catalog Number: 25544
Epoch time:      19199
99641559   =   yrday
fracday
Element set:     911
Inclination:       51
6398  deg
RA of node:       203
4604  deg
Eccentricity:     
0006472     
Arg of perigee:   158
1787  deg
Mean anomaly:     201
9641  deg
Mean motion:   15
51012918  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2018
Checksum:              326


Coasting Arc #13 (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    =       -5963971
87                 A    =         6794122
66  meter
 Y    =         766404
81  meter          E    =           
0008689
 Z    =       -3175208
02                 I    =           51
52291
 XDOT =      -3203
622889                 Wp   =          130
35778
 YDOT =      -5017
456769  meter/sec      RA   =          197
49232  deg
 ZDOT =       4809
484186                 TA   =          193
02470
                                          MA   =          193
04715
                                          Ha   =            227
650  n
mi
                                          Hp   =            218
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19566836
84                 X    =        -5956675
72
 Y    =        2514451
48  feet           Y    =          699752
58  meter
 Z    =      -10417349
13                 Z    =        -3204160
33
 XDOT =     -10510
573783                 XDOT =       -3170
639438
 YDOT =     -16461
472339  feet/sec       YDOT =       -5053
097955  meter/sec
 ZDOT =      15779
147591                 ZDOT =        4794
002168

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6124340
02                 X    =        -1866698
84
 Y    =      -18679345
19  feet           Y    =        -5693464
41  meter
 Z    =      -10548898
33                 Z    =        -3215304
21
 XDOT =      12816
076227                 XDOT =        3906
340034
 YDOT =     -13067
628956  feet/sec       YDOT =       -3983
013306  meter/sec
 ZDOT =      15709
178250                 ZDOT =        4788
157531


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
96290462  
00016717  00000-0  10270-3 0  9120
2 25544  51
6379 198
6647 0006714 161
1993 198
9407 15
50984471 20332


Satellite: ISS
Catalog Number: 25544
Epoch time:      19200
96290462   =   yrday
fracday
Element set:     912
Inclination:       51
6379  deg
RA of node:       198
6647  deg
Eccentricity:     
0006714     
Arg of perigee:   161
1993  deg
Mean anomaly:     198
9407  deg
Mean motion:   15
50984471  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2033
Checksum:              336


Coasting Arc #14 (Orbit 2044)
---------------------------------------

Vector Time (GMT): 2019/201/16:28:21
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         157331
13                 A    =         6786637
59  meter
 Y    =       -4273264
06  meter          E    =           
0009197
 Z    =        5266911
78                 I    =           51
52365
 XDOT =       7527
439419                 Wp   =          150
05052
 YDOT =       1233
955219  meter/sec      RA   =          193
89872  deg
 ZDOT =        767
917131                 TA   =          292
54981
                                          MA   =          292
64713
                                          Ha   =            227
503  n
mi
                                          Hp   =            218
537

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         516178
25                 X    =          179521
10
 Y    =      -14019895
20  feet           Y    =        -4271381
02  meter
 Z    =       17279894
28                 Z    =         5267729
56
 XDOT =      24696
323553                 XDOT =        7509
351490
 YDOT =       4048
409512  feet/sec       YDOT =        1318
031134  meter/sec
 ZDOT =       2519
413159                 ZDOT =         804
438025

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         667665
30                 X    =          203504
38
 Y    =       14008557
24  feet           Y    =         4269808
25  meter
 Z    =       17283899
87                 Z    =         5268132
68
 XDOT =     -23893
770173                 XDOT =       -7282
821149
 YDOT =      -2208
174291  feet/sec       YDOT =        -673
051524  meter/sec
 ZDOT =       2685
215630                 ZDOT =         818
453724


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   19201
73609496  
00016717  00000-0  10270-3 0  9138
2 25544  51
6401 194
8314 0006583 164
2566 195
8791 15
51019640 20454


Satellite: ISS
Catalog Number: 25544
Epoch time:      19201
73609496   =   yrday
fracday
Element set:     913
Inclination:       51
6401  deg
RA of node:       194
8314  deg
Eccentricity:     
0006583     
Arg of perigee:   164
2566  deg
Mean anomaly:     195
8791  deg
Mean motion:   15
51019640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2045
Checksum:              316


Coasting Arc #15 (Orbit 2048)
---------------------------------------

Vector Time (GMT): 2019/201/22:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4421333
15                 A    =         6790060
75  meter
 Y    =       -2618614
59  meter          E    =           
0010614
 Z    =        4427792
83                 I    =           51
54208
 XDOT =       5669
655139                 Wp   =          107
97816
 YDOT =       3960
182358  meter/sec      RA   =          192
54929  deg
 ZDOT =      -3315
975917                 TA   =           15
55103
                                          MA   =           15
51844
                                          Ha   =            227
405  n
mi
                                          Hp   =            218
649

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14505686
19                 X    =         4428779
33
 Y    =       -8591255
21  feet           Y    =        -2569130
84  meter
 Z    =       14526879
36                 Z    =         4449287
46
 XDOT =      18601
230771                 XDOT =        5641
056710
 YDOT =      12992
724272  feet/sec       YDOT =        4023
424775  meter/sec
 ZDOT =     -10879
186078                 ZDOT =       -3288
504562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10969741
97                 X    =         3343577
35
 Y    =       12690071
69  feet           Y    =         3867933
85  meter
 Z    =       14624693
62                 Z    =         4457606
61
 XDOT =      -8613
388701                 XDOT =       -2625
360876
 YDOT =      19852
493821  feet/sec       YDOT =        6051
040117  meter/sec
 ZDOT =     -10754
668775                 ZDOT =       -3278
023043


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   19201
99382391  
00016717  00000-0  10270-3 0  9149
2 25544  51
6386 193
5500 0006644 166
3318 193
8014 15
50987863 20495


Satellite: ISS
Catalog Number: 25544
Epoch time:      19201
99382391   =   yrday
fracday
Element set:     914
Inclination:       51
6386  deg
RA of node:       193
5500  deg
Eccentricity:     
0006644     
Arg of perigee:   166
3318  deg
Mean anomaly:     193
8014  deg
Mean motion:   15
50987863  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2049
Checksum:              328


Coasting Arc #16 (Orbit 2063)
---------------------------------------

Vector Time (GMT): 2019/202/22:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4823285
99                 A    =         6791493
57  meter
 Y    =        2586698
60  meter          E    =           
0012091
 Z    =       -4034852
82                 I    =           51
57950
 XDOT =      -5336
009039                 Wp   =          137
86136
 YDOT =      -3841
794338  meter/sec      RA   =          187
57999  deg
 ZDOT =       3913
836184                 TA   =          172
90414
                                          MA   =          172
88701
                                          Ha   =            227
495  n
mi
                                          Hp   =            218
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15824429
09                 X    =        -4832253
99
 Y    =        8486543
97  feet           Y    =         2532711
35  meter
 Z    =      -13237706
11                 Z    =        -4058303
75
 XDOT =     -17506
591334                 XDOT =       -5311
663324
 YDOT =     -12604
312133  feet/sec       YDOT =       -3901
329467  meter/sec
 ZDOT =      12840
669894                 ZDOT =        3887
975180

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11337491
24                 X    =        -3455667
33
 Y    =      -13822400
26  feet           Y    =        -4213067
60  meter
 Z    =      -13344414
23                 Z    =        -4067377
46
 XDOT =       7999
540319                 XDOT =        2438
259889
 YDOT =     -18850
946991  feet/sec       YDOT =       -5745
768643  meter/sec
 ZDOT =      12723
440956                 ZDOT =        3878
104803


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   19202
96031043  
00016717  00000-0  10270-3 0  9153
2 25544  51
6384 188
7536 0006769 168
4310 191
6998 15
50991852 20648


Satellite: ISS
Catalog Number: 25544
Epoch time:      19202
96031043   =   yrday
fracday
Element set:     915
Inclination:       51
6384  deg
RA of node:       188
7536  deg
Eccentricity:     
0006769     
Arg of perigee:   168
4310  deg
Mean anomaly:     191
6998  deg
Mean motion:   15
50991852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2064
Checksum:              335


Coasting Arc #17 (Orbit 2064)
---------------------------------------

Vector Time (GMT): 2019/202/23:35:11
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4403203
50                 A    =         6790614
62  meter
 Y    =       -2861181
56  meter          E    =           
0011194
 Z    =        4294036
50                 I    =           51
57723
 XDOT =       5783
899414                 Wp   =          109
97774
 YDOT =       3584
540320  meter/sec      RA   =          187
42475  deg
 ZDOT =      -3538
747679                 TA   =           16
12068
                                          MA   =           16
08509
                                          Ha   =            227
443  n
mi
                                          Hp   =            218
738

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14446205
70                 X    =         4414013
11
 Y    =       -9387078
61  feet           Y    =        -2811881
68  meter
 Z    =       14088046
26                 Z    =         4315451
31
 XDOT =      18976
047946                 XDOT =        5760
575161
 YDOT =      11760
302886  feet/sec       YDOT =        3649
089759  meter/sec
 ZDOT =     -11610
064564                 ZDOT =       -3510
708563

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14138060
83                 X    =         4309280
94
 Y    =        9704087
99  feet           Y    =         2957806
02  meter
 Z    =       14185523
03                 Z    =         4323747
42
 XDOT =      -2923
503992                 XDOT =        -891
084017
 YDOT =      21063
063619  feet/sec       YDOT =        6420
021791  meter/sec
 ZDOT =     -11482
922925                 ZDOT =       -3499
994907


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   19203
02474320  
00016717  00000-0  10270-3 0  9161
2 25544  51
6383 188
4334 0006846 169
0391 191
0910 15
50968855 20658


Satellite: ISS
Catalog Number: 25544
Epoch time:      19203
02474320   =   yrday
fracday
Element set:     916
Inclination:       51
6383  deg
RA of node:       188
4334  deg
Eccentricity:     
0006846     
Arg of perigee:   169
0391  deg
Mean anomaly:     191
0910  deg
Mean motion:   15
50968855  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2065
Checksum:              313


Coasting Arc #18 (Orbit 2066)
---------------------------------------

Vector Time (GMT): 2019/203/02:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -170714
41                 A    =         6786570
37  meter
 Y    =       -4246571
45  meter          E    =           
0009052
 Z    =        5288394
00                 I    =           51
57101
 XDOT =       7630
297943                 Wp   =          154
76783
 YDOT =        442
581152  meter/sec      RA   =          186
85074  deg
 ZDOT =        593
316882                 TA   =          289
51346
                                          MA   =          289
61120
                                          Ha   =            227
524  n
mi
                                          Hp   =            218
673

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -560086
66                 X    =         -148902
99
 Y    =      -13932321
03  feet           Y    =        -4248358
88  meter
 Z    =       17350374
01                 Z    =         5287617
45
 XDOT =      25033
785903                 XDOT =        7621
899823
 YDOT =       1452
037899  feet/sec       YDOT =         527
861508  meter/sec
 ZDOT =       1946
577696                 ZDOT =         630
361020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5008822
99                 X    =         1526689
25
 Y    =      -13017203
03  feet           Y    =        -3967643
48  meter
 Z    =       17347128
35                 Z    =         5287404
72
 XDOT =      21351
717019                 XDOT =        6508
003347
 YDOT =      11070
801489  feet/sec       YDOT =        3374
380294  meter/sec
 ZDOT =       2114
840119                 ZDOT =         644
603268


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   19203
15360740  
00016717  00000-0  10270-3 0  9176
2 25544  51
6413 187
7933 0006989 169
9393 190
1899 15
51013576 20678


Satellite: ISS
Catalog Number: 25544
Epoch time:      19203
15360740   =   yrday
fracday
Element set:     917
Inclination:       51
6413  deg
RA of node:       187
7933  deg
Eccentricity:     
0006989     
Arg of perigee:   169
9393  deg
Mean anomaly:     190
1899  deg
Mean motion:   15
51013576  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2067
Checksum:              338


Coasting Arc #19 (Orbit 2078)
---------------------------------------

Vector Time (GMT): 2019/203/20:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3250598
70                 A    =         6789766
31  meter
 Y    =       -3809712
25  meter          E    =           
0013228
 Z    =        4582150
56                 I    =           51
60580
 XDOT =       6725
238158                 Wp   =          137
93442
 YDOT =      -2057
673245  meter/sec      RA   =          183
05576  deg
 ZDOT =       3045
403911                 TA   =          281
52722
                                          MA   =          281
67571
                                          Ha   =            227
432  n
mi
                                          Hp   =            218
948

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10664693
89                 X    =        -3230013
04
 Y    =      -12499055
95  feet           Y    =        -3845947
90  meter
 Z    =       15033302
35                 Z    =         4566410
36
 XDOT =      22064
429652                 XDOT =        6732
955150
 YDOT =      -6750
896472  feet/sec       YDOT =       -1982
423937  meter/sec
 ZDOT =       9991
482647                 ZDOT =        3078
090759

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15019590
51                 X    =         4577971
19
 Y    =       -6819938
29  feet           Y    =        -2078717
19  meter
 Z    =       14962039
21                 Z    =         4560429
55
 XDOT =       -200
016456                 XDOT =         -60
965016
 YDOT =      21911
987786  feet/sec       YDOT =        6678
773877  meter/sec
 ZDOT =      10140
128087                 ZDOT =        3090
711041


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   19203
92679489  
00016717  00000-0  10270-3 0  9185
2 25544  51
6406 183
9611 0006402 171
4945 188
6316 15
50960785 20793


Satellite: ISS
Catalog Number: 25544
Epoch time:      19203
92679489   =   yrday
fracday
Element set:     918
Inclination:       51
6406  deg
RA of node:       183
9611  deg
Eccentricity:     
0006402     
Arg of perigee:   171
4945  deg
Mean anomaly:     188
6316  deg
Mean motion:   15
50960785  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2079
Checksum:              342


Coasting Arc #20 (Orbit 2086)
---------------------------------------

Vector Time (GMT): 2019/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951979
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          55846
05                 A    =         6786516
30  meter
 Y    =       -4212662
82  meter          E    =           
0007329
 Z    =        5317632
28                 I    =           51
61275
 XDOT =       7666
001842                 Wp   =          154
09401
 YDOT =         52
885272  meter/sec      RA   =          180
12860  deg
 ZDOT =        -45
036902                 TA   =          296
29778
                                          MA   =          296
37305
                                          Ha   =            227
374  n
mi
                                          Hp   =            218
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         183221
96                 X    =           77119
32
 Y    =      -13821072
26  feet           Y    =        -4211919
67  meter
 Z    =       17446300
13                 Z    =         5317954
98
 XDOT =      25150
924678                 XDOT =        7665
059475
 YDOT =        173
508110  feet/sec       YDOT =         138
606623  meter/sec
 ZDOT =       -147
758866                 ZDOT =          -7
801073

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13365616
26                 X    =        -4073839
84
 Y    =        3514981
26  feet           Y    =         1071366
29  meter
 Z    =       17448043
03                 Z    =         5318163
52
 XDOT =      -6088
885488                 XDOT =       -1855
892297
 YDOT =     -23363
788282  feet/sec       YDOT =       -7121
282668  meter/sec
 ZDOT =         21
427002                 ZDOT =           6
530950


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   19204
50668446  
00016717  00000-0  10270-3 0  9192
2 25544  51
6384 181
0844 0006600 172
8080 187
3166 15
50984278 20871


Satellite: ISS
Catalog Number: 25544
Epoch time:      19204
50668446   =   yrday
fracday
Element set:     919
Inclination:       51
6384  deg
RA of node:       181
0844  deg
Eccentricity:     
0006600     
Arg of perigee:   172
8080  deg
Mean anomaly:     187
3166  deg
Mean motion:   15
50984278  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2087
Checksum:              327
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