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

 
Date: October 7th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16550 5887 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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


281/10:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 218 7

284/20:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 5
000/00:00:00 000 0 0 0 0 219 1

289/19:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 219 5

292/20:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 8
000/00:00:00 000 0 0 0 0 220 1

Coasting Arc #1 (Orbit 3268)
---------------------------------------

Vector Time (GMT): 2019/280/13:28:14
231
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6573236
01                 A    =         6800717
94  meter
 Y    =        1675407
57  meter          E    =           
0016074
 Z    =         429561
57                 I    =           51
77145
 XDOT =       -793
829522                 Wp   =           74
70864
 YDOT =      -4699
028648  meter/sec      RA   =          162
84144  deg
 ZDOT =       5997
080370                 TA   =          289
90590
                                          MA   =          290
07902
                                          Ha   =            229
584  n
mi
                                          Hp   =            218
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21565734
93                 X    =        -6593568
94
 Y    =        5496744
01  feet           Y    =         1601787
34  meter
 Z    =        1409322
74                 Z    =          397581
67
 XDOT =      -2604
427564                 XDOT =        -770
355221
 YDOT =     -15416
760657  feet/sec       YDOT =       -4707
774271  meter/sec
 ZDOT =      19675
460532                 ZDOT =        5993
281469

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13899626
28                 X    =         4236606
09
 Y    =      -17392101
91  feet           Y    =        -5301112
66  meter
 Z    =        1263522
28                 Z    =          385121
59
 XDOT =      10208
890042                 XDOT =        3111
669685
 YDOT =       9635
699089  feet/sec       YDOT =        2936
961082  meter/sec
 ZDOT =      19658
367979                 ZDOT =        5991
870560


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   19280
62500140  
00016717  00000-0  10270-3 0  9005
2 25544  51
6419 163
7081 0007023 124
4880 235
6935 15
50197240 32690


Satellite: ISS
Catalog Number: 25544
Epoch time:      19280
62500140   =   yrday
fracday
Element set:     900
Inclination:       51
6419  deg
RA of node:       163
7081  deg
Eccentricity:     
0007023     
Arg of perigee:   124
4880  deg
Mean anomaly:     235
6935  deg
Mean motion:   15
50197240  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3269
Checksum:              289


Coasting Arc #2 (Orbit 3281)
---------------------------------------

Vector Time (GMT): 2019/281/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         866641
76                 A    =         6788960
41  meter
 Y    =        4159312
68  meter          E    =           
0020972
 Z    =       -5313194
49                 I    =           51
76155
 XDOT =      -7255
930348                 Wp   =          105
33111
 YDOT =       2327
718784  meter/sec      RA   =          158
44632  deg
 ZDOT =        635
373978                 TA   =          170
76094
                                          MA   =          170
72230
                                          Ha   =            229
577  n
mi
                                          Hp   =            218
673

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2843312
87                 X    =          845875
35
 Y    =       13646038
98  feet           Y    =         4168887
65  meter
 Z    =      -17431740
45                 Z    =        -5309035
34
 XDOT =     -23805
545761                 XDOT =       -7284
506604
 YDOT =       7636
872652  feet/sec       YDOT =        2246
418109  meter/sec
 ZDOT =       2084
560295                 ZDOT =         600
057721

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2276128
51                 X    =         -693763
97
 Y    =      -13775766
79  feet           Y    =        -4198853
72  meter
 Z    =      -17412979
97                 Z    =        -5307476
29
 XDOT =      23165
981926                 XDOT =        7060
991291
 YDOT =      -6272
731664  feet/sec       YDOT =       -1911
928611  meter/sec
 ZDOT =       1923
507837                 ZDOT =         586
285189


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   19281
46306287  
00016717  00000-0  10270-3 0  9015
2 25544  51
6432 159
5552 0007056 126
7711 233
4089 15
50193012 32829


Satellite: ISS
Catalog Number: 25544
Epoch time:      19281
46306287   =   yrday
fracday
Element set:     901
Inclination:       51
6432  deg
RA of node:       159
5552  deg
Eccentricity:     
0007056     
Arg of perigee:   126
7711  deg
Mean anomaly:     233
4089  deg
Mean motion:   15
50193012  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3282
Checksum:              298


Coasting Arc #3 (Orbit 3297)
---------------------------------------

Vector Time (GMT): 2019/282/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -749434
92                 A    =         6789081
83  meter
 Y    =       -4237861
59  meter          E    =           
0008772
 Z    =        5243115
26                 I    =           51
79297
 XDOT =       7132
094539                 Wp   =          107
23859
 YDOT =      -2602
081296  meter/sec      RA   =          153
49827  deg
 ZDOT =      -1084
789574                 TA   =          353
12588
                                          MA   =          353
13790
                                          Ha   =            229
500  n
mi
                                          Hp   =            218
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2458776
00                 X    =         -727458
49
 Y    =      -13903745
39  feet           Y    =        -4246119
04  meter
 Z    =       17201821
73                 Z    =         5239528
46
 XDOT =      23399
260299                 XDOT =        7165
931024
 YDOT =      -8537
012127  feet/sec       YDOT =       -2522
136070  meter/sec
 ZDOT =      -3559
020912                 ZDOT =       -1050
062001

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2118451
07                 X    =          645703
89
 Y    =       13979528
02  feet           Y    =         4260960
14  meter
 Z    =       17185672
74                 Z    =         5238193
05
 XDOT =     -22670
129610                 XDOT =       -6909
855505
 YDOT =       7611
755344  feet/sec       YDOT =        2320
063029  meter/sec
 ZDOT =      -3400
619087                 ZDOT =       -1036
508698


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   19282
49451613  
00016717  00000-0  10270-3 0  9024
2 25544  51
6432 154
4443 0006957 130
5924 229
5833 15
50225910 32983


Satellite: ISS
Catalog Number: 25544
Epoch time:      19282
49451613   =   yrday
fracday
Element set:     902
Inclination:       51
6432  deg
RA of node:       154
4443  deg
Eccentricity:     
0006957     
Arg of perigee:   130
5924  deg
Mean anomaly:     229
5833  deg
Mean motion:   15
50225910  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3298
Checksum:              311


Coasting Arc #4 (Orbit 3312)
---------------------------------------

Vector Time (GMT): 2019/283/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         645095
95                 A    =         6789557
04  meter
 Y    =        4372150
53  meter          E    =           
0019936
 Z    =       -5171897
22                 I    =           51
82304
 XDOT =      -6936
275878                 Wp   =          112
52111
 YDOT =       2833
823344  meter/sec      RA   =          148
55231  deg
 ZDOT =       1527
730696                 TA   =          172
21711
                                          MA   =          172
18613
                                          Ha   =            229
453  n
mi
                                          Hp   =            218
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2116456
54                 X    =          621279
74
 Y    =       14344325
88  feet           Y    =         4379230
83  meter
 Z    =      -16968166
73                 Z    =        -5168821
79
 XDOT =     -22756
810625                 XDOT =       -6974
869914
 YDOT =       9297
320684  feet/sec       YDOT =        2756
041351  meter/sec
 ZDOT =       5012
239815                 ZDOT =        1493
942651

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2007919
94                 X    =         -612014
00
 Y    =      -14376224
47  feet           Y    =        -4381873
22  meter
 Z    =      -16954355
87                 Z    =        -5167687
67
 XDOT =      21883
354378                 XDOT =        6670
046414
 YDOT =      -8796
281479  feet/sec       YDOT =       -2681
106595  meter/sec
 ZDOT =       4858
091793                 ZDOT =        1480
746378


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   19283
46150411  
00016717  00000-0  10270-3 0  9035
2 25544  51
6426 149
6529 0006977 133
8045 226
3684 15
50198738 33133


Satellite: ISS
Catalog Number: 25544
Epoch time:      19283
46150411   =   yrday
fracday
Element set:     903
Inclination:       51
6426  deg
RA of node:       149
6529  deg
Eccentricity:     
0006977     
Arg of perigee:   133
8045  deg
Mean anomaly:     226
3684  deg
Mean motion:   15
50198738  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3313
Checksum:              322


Coasting Arc #5 (Orbit 3328)
---------------------------------------

Vector Time (GMT): 2019/284/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -566525
92                 A    =         6789922
91  meter
 Y    =       -4502291
71  meter          E    =           
0009464
 Z    =        5042309
89                 I    =           51
85277
 XDOT =       6752
767216                 Wp   =          102
12070
 YDOT =      -3055
984803  meter/sec      RA   =          143
60874  deg
 ZDOT =      -1968
814987                 TA   =            6
93864
                                          MA   =            6
92554
                                          Ha   =            229
335  n
mi
                                          Hp   =            218
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1858680
83                 X    =         -540630
88
 Y    =      -14771298
25  feet           Y    =        -4508481
73  meter
 Z    =       16543011
46                 Z    =         5039621
22
 XDOT =      22154
748084                 XDOT =        6796
001754
 YDOT =     -10026
196861  feet/sec       YDOT =       -2980
229042  meter/sec
 ZDOT =      -6459
366755                 ZDOT =       -1935
906934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1994993
35                 X    =          608073
97
 Y    =       14766994
15  feet           Y    =         4500979
82  meter
 Z    =       16530972
75                 Z    =         5038640
49
 XDOT =     -21104
129155                 XDOT =       -6432
538567
 YDOT =       9918
323280  feet/sec       YDOT =        3023
104936  meter/sec
 ZDOT =      -6309
203076                 ZDOT =       -1923
045098


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   19284
49295295  
00016717  00000-0  10270-3 0  9040
2 25544  51
6428 144
5420 0006840 138
5667 221
6004 15
50235607 33298


Satellite: ISS
Catalog Number: 25544
Epoch time:      19284
49295295   =   yrday
fracday
Element set:     904
Inclination:       51
6428  deg
RA of node:       144
5420  deg
Eccentricity:     
0006840     
Arg of perigee:   138
5667  deg
Mean anomaly:     221
6004  deg
Mean motion:   15
50235607  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3329
Checksum:              312


Coasting Arc #6 (Orbit 3334)
---------------------------------------

Vector Time (GMT): 2019/284/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3774885
37                 A    =         6789569
87  meter
 Y    =        2220646
83  meter          E    =           
0018169
 Z    =       -5202950
87                 I    =           51
86131
 XDOT =      -5146
119725                 Wp   =          100
27591
 YDOT =       5483
488084  meter/sec      RA   =          141
59117  deg
 ZDOT =      -1400
584242                 TA   =          156
30427
                                          MA   =          156
22050
                                          Ha   =            229
461  n
mi
                                          Hp   =            219
136

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12384794
51                 X    =         3775046
25
 Y    =        7285586
72  feet           Y    =         2262860
66  meter
 Z    =      -17070048
79                 Z    =        -5184613
50
 XDOT =     -16883
594899                 XDOT =       -5200
251865
 YDOT =      17990
446471  feet/sec       YDOT =        5425
637731  meter/sec
 ZDOT =      -4595
092658                 ZDOT =       -1425
714476

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7018463
56                 X    =         2139227
69
 Y    =       12650983
42  feet           Y    =         3856019
75  meter
 Z    =      -16986561
22                 Z    =        -5177503
86
 XDOT =     -22758
225115                 XDOT =       -6936
707015
 YDOT =       6334
046640  feet/sec       YDOT =        1930
617416  meter/sec
 ZDOT =      -4709
924150                 ZDOT =       -1435
584881


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   19284
87974684  
00016717  00000-0  10270-3 0  9059
2 25544  51
6422 142
6217 0007206 142
7062 217
4590 15
50176077 33353


Satellite: ISS
Catalog Number: 25544
Epoch time:      19284
87974684   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:       142
6217  deg
Eccentricity:     
0007206     
Arg of perigee:   142
7062  deg
Mean anomaly:     217
4590  deg
Mean motion:   15
50176077  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3335
Checksum:              316


Coasting Arc #7 (Orbit 3350)
---------------------------------------

Vector Time (GMT): 2019/285/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3629924
13                 A    =         6789064
37  meter
 Y    =       -2257865
17  meter          E    =           
0010577
 Z    =        5269172
90                 I    =           51
88596
 XDOT =       4984
656138                 Wp   =          137
93600
 YDOT =      -5744
968924  meter/sec      RA   =          136
64946  deg
 ZDOT =        963
404952                 TA   =          302
82287
                                          MA   =          302
92467
                                          Ha   =            229
436  n
mi
                                          Hp   =            219
039

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11909199
91                 X    =        -3630001
38
 Y    =       -7407694
12  feet           Y    =        -2298457
46  meter
 Z    =       17287312
67                 Z    =         5251539
84
 XDOT =      16353
858721                 XDOT =        5043
847813
 YDOT =     -18848
323241  feet/sec       YDOT =       -5688
895924  meter/sec
 ZDOT =       3160
777400                 ZDOT =         987
763265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6762849
68                 X    =        -2061316
58
 Y    =      -12399030
96  feet           Y    =        -3779224
64  meter
 Z    =       17207034
89                 Z    =         5244704
23
 XDOT =      22629
756858                 XDOT =        6897
549890
 YDOT =      -7761
957730  feet/sec       YDOT =       -2365
844716  meter/sec
 ZDOT =       3272
119679                 ZDOT =         997
342078


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   19285
91119073  
00016717  00000-0  10270-3 0  9069
2 25544  51
6426 137
5104 0007163 145
5085 214
6532 15
50225594 33515


Satellite: ISS
Catalog Number: 25544
Epoch time:      19285
91119073   =   yrday
fracday
Element set:     906
Inclination:       51
6426  deg
RA of node:       137
5104  deg
Eccentricity:     
0007163     
Arg of perigee:   145
5085  deg
Mean anomaly:     214
6532  deg
Mean motion:   15
50225594  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3351
Checksum:              298


Coasting Arc #8 (Orbit 3365)
---------------------------------------

Vector Time (GMT): 2019/286/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3491781
50                 A    =         6788967
51  meter
 Y    =        2367281
05  meter          E    =           
0019022
 Z    =       -5334609
28                 I    =           51
90712
 XDOT =      -4781
481764                 Wp   =          105
63417
 YDOT =       5949
394287  meter/sec      RA   =          131
70903  deg
 ZDOT =       -496
086987                 TA   =          159
67660
                                          MA   =          159
60079
                                          Ha   =            229
306  n
mi
                                          Hp   =            219
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11455976
05                 X    =         3490963
46
 Y    =        7766670
12  feet           Y    =         2406323
56  meter
 Z    =      -17501998
94                 Z    =        -5317649
37
 XDOT =     -15687
276127                 XDOT =       -4845
244480
 YDOT =      19519
010129  feet/sec       YDOT =        5895
567817  meter/sec
 ZDOT =      -1627
581978                 ZDOT =        -519
469516

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6406354
56                 X    =         1952656
87
 Y    =       12378031
88  feet           Y    =         3772824
12  meter
 Z    =      -17424794
60                 Z    =        -5311077
39
 XDOT =     -22233
512815                 XDOT =       -6776
774706
 YDOT =       9095
385254  feet/sec       YDOT =        2772
273425  meter/sec
 ZDOT =      -1734
504736                 ZDOT =        -528
677043


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   19286
87816906  
00016717  00000-0  10270-3 0  9075
2 25544  51
6410 132
7189 0007100 148
7680 211
3893 15
50181801 33667


Satellite: ISS
Catalog Number: 25544
Epoch time:      19286
87816906   =   yrday
fracday
Element set:     907
Inclination:       51
6410  deg
RA of node:       132
7189  deg
Eccentricity:     
0007100     
Arg of perigee:   148
7680  deg
Mean anomaly:     211
3893  deg
Mean motion:   15
50181801  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3366
Checksum:              316


Coasting Arc #9 (Orbit 3381)
---------------------------------------

Vector Time (GMT): 2019/287/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3383773
84                 A    =         6788720
82  meter
 Y    =       -2461082
05  meter          E    =           
0008619
 Z    =        5341184
97                 I    =           51
92828
 XDOT =       4561
595628                 Wp   =          139
04267
 YDOT =      -6162
049081  meter/sec      RA   =          126
77021  deg
 ZDOT =         44
189425                 TA   =          310
50031
                                          MA   =          310
57539
                                          Ha   =            229
283  n
mi
                                          Hp   =            219
269

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11101620
21                 X    =        -3381946
95
 Y    =       -8074416
16  feet           Y    =        -2498911
16  meter
 Z    =       17523572
72                 Z    =         5324752
10
 XDOT =      14965
864920                 XDOT =        4629
947766
 YDOT =     -20216
696459  feet/sec       YDOT =       -6110
655914  meter/sec
 ZDOT =        144
978428                 ZDOT =          66
514969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6161497
87                 X    =        -1878024
55
 Y    =      -12373112
34  feet           Y    =        -3771324
64  meter
 Z    =       17448776
57                 Z    =         5318387
10
 XDOT =      21761
936640                 XDOT =        6633
038288
 YDOT =     -10458
766889  feet/sec       YDOT =       -3187
832148  meter/sec
 ZDOT =        247
114215                 ZDOT =          75
320413


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   19287
90960833  
00016717  00000-0  10270-3 0  9080
2 25544  51
6411 127
6077 0007118 152
8392 207
3132 15
50229831 33827


Satellite: ISS
Catalog Number: 25544
Epoch time:      19287
90960833   =   yrday
fracday
Element set:     908
Inclination:       51
6411  deg
RA of node:       127
6077  deg
Eccentricity:     
0007118     
Arg of perigee:   152
8392  deg
Mean anomaly:     207
3132  deg
Mean motion:   15
50229831  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3382
Checksum:              311


Coasting Arc #10 (Orbit 3396)
---------------------------------------

Vector Time (GMT): 2019/288/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3296944
58                 A    =         6788904
69  meter
 Y    =        2617272
86  meter          E    =           
0019029
 Z    =       -5341895
78                 I    =           51
94704
 XDOT =      -4307
091724                 Wp   =          112
45390
 YDOT =       6306
319858  meter/sec      RA   =          121
83163  deg
 ZDOT =        425
667310                 TA   =          161
63328
                                          MA   =          161
56448
                                          Ha   =            229
124  n
mi
                                          Hp   =            219
572

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10816747
30                 X    =         3293381
08
 Y    =        8586853
23  feet           Y    =         2654121
38  meter
 Z    =      -17525904
78                 Z    =        -5325888
85
 XDOT =     -14130
878359                 XDOT =       -4379
358417
 YDOT =      20690
025781  feet/sec       YDOT =        6257
750875  meter/sec
 ZDOT =       1396
546294                 ZDOT =         404
568627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5888099
63                 X    =         1794692
77
 Y    =       12594219
46  feet           Y    =         3838718
09  meter
 Z    =      -17453060
70                 Z    =        -5319692
90
 XDOT =     -21032
339688                 XDOT =       -6410
657137
 YDOT =      11661
331345  feet/sec       YDOT =        3554
373794  meter/sec
 ZDOT =       1299
973572                 ZDOT =         396
231945


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   19288
87658115  
00016717  00000-0  10270-3 0  9095
2 25544  51
6406 122
8153 0007011 155
7641 204
3840 15
50190548 33975


Satellite: ISS
Catalog Number: 25544
Epoch time:      19288
87658115   =   yrday
fracday
Element set:     909
Inclination:       51
6406  deg
RA of node:       122
8153  deg
Eccentricity:     
0007011     
Arg of perigee:   155
7641  deg
Mean anomaly:     204
3840  deg
Mean motion:   15
50190548  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3397
Checksum:              314


Coasting Arc #11 (Orbit 3411)
---------------------------------------

Vector Time (GMT): 2019/289/19:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2234403
76                 A    =         6800189
32  meter
 Y    =       -6308517
57  meter          E    =           
0019862
 Z    =        1139579
92                 I    =           52
00154
 XDOT =       4852
824590                 Wp   =          134
66648
 YDOT =        643
530908  meter/sec      RA   =          117
14811  deg
 ZDOT =      -5903
197370                 TA   =           33
03452
                                          MA   =           32
91059
                                          Ha   =            229
086  n
mi
                                          Hp   =            219
478

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7330720
98                 X    =         2299245
77
 Y    =      -20697236
11  feet           Y    =        -6283168
29  meter
 Z    =        3738779
28                 Z    =         1150591
85
 XDOT =      15921
340520                 XDOT =        4873
942992
 YDOT =       2111
321878  feet/sec       YDOT =         697
916464  meter/sec
 ZDOT =     -19367
445438                 ZDOT =       -5879
572267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19737392
23                 X    =         6015957
15
 Y    =       -9600495
01  feet           Y    =        -2926230
88  meter
 Z    =        3789375
50                 Z    =         1155001
65
 XDOT =       9242
987672                 XDOT =        2817
262643
 YDOT =      11337
363670  feet/sec       YDOT =        3455
628447  meter/sec
 ZDOT =     -19259
742339                 ZDOT =       -5870
369465


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   19289
84355005  
00016717  00000-0  10270-3 0  9107
2 25544  51
6414 118
0229 0007113 158
2342 201
9112 15
50209461 34122


Satellite: ISS
Catalog Number: 25544
Epoch time:      19289
84355005   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:       118
0229  deg
Eccentricity:     
0007113     
Arg of perigee:   158
2342  deg
Mean anomaly:     201
9112  deg
Mean motion:   15
50209461  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3412
Checksum:              273


Coasting Arc #12 (Orbit 3426)
---------------------------------------

Vector Time (GMT): 2019/290/19:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2000919
17                 A    =         6800577
34  meter
 Y    =        6455539
10  meter          E    =           
0008902
 Z    =        -754212
07                 I    =           52
01658
 XDOT =      -4723
847187                 Wp   =           81
02009
 YDOT =       -773
271870  meter/sec      RA   =          112
21983  deg
 ZDOT =       5975
098223                 TA   =          270
89100
                                          MA   =          270
99299
                                          Ha   =            228
957  n
mi
                                          Hp   =            219
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6564695
43                 X    =        -2069294
53
 Y    =       21179590
23  feet           Y    =         6432781
09  meter
 Z    =       -2474449
06                 Z    =         -764098
24
 XDOT =     -15498
186309                 XDOT =       -4743
873611
 YDOT =      -2536
981201  feet/sec       YDOT =        -826
209124  meter/sec
 ZDOT =      19603
340628                 ZDOT =        5952
102323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19353998
64                 X    =        -5899098
79
 Y    =       10810448
45  feet           Y    =         3295024
69  meter
 Z    =       -2519942
02                 Z    =         -768078
33
 XDOT =      -8774
246207                 XDOT =       -2674
390244
 YDOT =     -11209
567936  feet/sec       YDOT =       -3416
676307  meter/sec
 ZDOT =      19498
508159                 ZDOT =        5943
145287


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   19290
81051600  
00016717  00000-0  10270-3 0  9111
2 25544  51
6411 113
2311 0006866 161
7189 198
4209 15
50178955 34276


Satellite: ISS
Catalog Number: 25544
Epoch time:      19290
81051600   =   yrday
fracday
Element set:     911
Inclination:       51
6411  deg
RA of node:       113
2311  deg
Eccentricity:     
0006866     
Arg of perigee:   161
7189  deg
Mean anomaly:     198
4209  deg
Mean motion:   15
50178955  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3427
Checksum:              301


Coasting Arc #13 (Orbit 3442)
---------------------------------------

Vector Time (GMT): 2019/291/19:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1776471
12                 A    =         6800669
85  meter
 Y    =       -6545580
66  meter          E    =           
0018909
 Z    =         319773
80                 I    =           52
02868
 XDOT =       4634
789555                 Wp   =          143
40084
 YDOT =        954
901581  meter/sec      RA   =          107
29316  deg
 ZDOT =      -6033
639510                 TA   =           33
17417
                                          MA   =           33
05575
                                          Ha   =            228
894  n
mi
                                          Hp   =            219
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5828317
31                 X    =         1847980
35
 Y    =      -21475002
16  feet           Y    =        -6525315
07  meter
 Z    =        1049126
63                 Z    =          328577
13
 XDOT =      15206
002476                 XDOT =        4653
075853
 YDOT =       3132
879203  feet/sec       YDOT =        1006
833301  meter/sec
 ZDOT =     -19795
405216                 ZDOT =       -6011
080501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18830842
03                 X    =         5739640
65
 Y    =      -11851480
59  feet           Y    =        -3612331
28  meter
 Z    =        1089708
04                 Z    =          332143
01
 XDOT =       8296
357618                 XDOT =        2528
729802
 YDOT =      11322
578096  feet/sec       YDOT =        3451
121804  meter/sec
 ZDOT =     -19692
570353                 ZDOT =       -6002
295444


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   19291
84194518  
00016717  00000-0  10270-3 0  9122
2 25544  51
6410 108
1200 0007028 165
3527 194
7828 15
50221479 34436


Satellite: ISS
Catalog Number: 25544
Epoch time:      19291
84194518   =   yrday
fracday
Element set:     912
Inclination:       51
6410  deg
RA of node:       108
1200  deg
Eccentricity:     
0007028     
Arg of perigee:   165
3527  deg
Mean anomaly:     194
7828  deg
Mean motion:   15
50221479  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3443
Checksum:              302


Coasting Arc #14 (Orbit 3458)
---------------------------------------

Vector Time (GMT): 2019/292/19:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1513598
47                 A    =         6800802
08  meter
 Y    =        6628427
29  meter          E    =           
0010322
 Z    =          75530
92                 I    =           52
03819
 XDOT =      -4575
689762                 Wp   =           79
89094
 YDOT =      -1121
602029  meter/sec      RA   =          102
36631  deg
 ZDOT =       6036
467445                 TA   =          280
91635
                                          MA   =          281
03248
                                          Ha   =            228
755  n
mi
                                          Hp   =            220
007

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4965874
25                 X    =        -1587973
87
 Y    =       21746808
69  feet           Y    =         6611085
30  meter
 Z    =         247804
87                 Z    =           67997
69
 XDOT =     -15012
105519                 XDOT =       -4592
129984
 YDOT =      -3679
796684  feet/sec       YDOT =       -1172
862591  meter/sec
 ZDOT =      19804
683217                 ZDOT =        6014
200086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18167177
45                 X    =        -5537355
69
 Y    =       12944238
13  feet           Y    =         3945403
78  meter
 Z    =         212991
46                 Z    =           64919
80
 XDOT =      -7925
341323                 XDOT =       -2415
644035
 YDOT =     -11491
259662  feet/sec       YDOT =       -3502
535945  meter/sec
 ZDOT =      19703
183537                 ZDOT =        6005
530342


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   19292
87337120  
00016717  00000-0  10270-3 0  9135
2 25544  51
6415 103
0083 0006749 168
7069 191
4234 15
50187981 34592


Satellite: ISS
Catalog Number: 25544
Epoch time:      19292
87337120   =   yrday
fracday
Element set:     913
Inclination:       51
6415  deg
RA of node:       103
0083  deg
Eccentricity:     
0006749     
Arg of perigee:   168
7069  deg
Mean anomaly:     191
4234  deg
Mean motion:   15
50187981  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3459
Checksum:              321


Coasting Arc #15 (Orbit 3458)
---------------------------------------

Vector Time (GMT): 2019/292/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4028100
67                 A    =         6788825
72  meter
 Y    =        1164009
32  meter          E    =           
0017712
 Z    =       -5353457
93                 I    =           51
99901
 XDOT =      -1800
002743                 Wp   =          114
07305
 YDOT =       7430
761350  meter/sec      RA   =          102
12389  deg
 ZDOT =        254
955270                 TA   =          158
38839
                                          MA   =          158
31355
                                          Ha   =            228
781  n
mi
                                          Hp   =            220
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13215553
39                 X    =         4040789
63
 Y    =        3818928
20  feet           Y    =         1209125
37  meter
 Z    =      -17563838
36                 Z    =        -5333859
72
 XDOT =      -5905
520810                 XDOT =       -1884
200346
 YDOT =      24379
138289  feet/sec       YDOT =        7410
161669  meter/sec
 ZDOT =        836
467422                 ZDOT =         246
006919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10610175
57                 X    =         3233981
51
 Y    =        8932463
57  feet           Y    =         2722614
90  meter
 Z    =      -17474517
19                 Z    =        -5326232
84
 XDOT =     -14704
430617                 XDOT =       -4481
910452
 YDOT =      19062
737749  feet/sec       YDOT =        5810
322466  meter/sec
 ZDOT =        795
143305                 ZDOT =         242
359679


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   19292
87337017  
00016717  00000-0  10270-3 0  9141
2 25544  51
6418 103
0085 0006844 168
3952 191
7357 15
50205698 34595


Satellite: ISS
Catalog Number: 25544
Epoch time:      19292
87337017   =   yrday
fracday
Element set:     914
Inclination:       51
6418  deg
RA of node:       103
0085  deg
Eccentricity:     
0006844     
Arg of perigee:   168
3952  deg
Mean anomaly:     191
7357  deg
Mean motion:   15
50205698  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3459
Checksum:              330


Coasting Arc #16 (Orbit 3474)
---------------------------------------

Vector Time (GMT): 2019/293/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4014504
37                 A    =         6788829
87  meter
 Y    =       -1317500
29  meter          E    =           
0006518
 Z    =        5309969
31                 I    =           52
00505
 XDOT =       1510
156010                 Wp   =          144
58796
 YDOT =      -7481
165043  meter/sec      RA   =           97
19096  deg
 ZDOT =       -719
214334                 TA   =          312
22176
                                          MA   =          312
27705
                                          Ha   =            228
753  n
mi
                                          Hp   =            219
976

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13170946
10                 X    =        -4025266
61
 Y    =       -4322507
50  feet           Y    =        -1362453
52  meter
 Z    =       17421159
15                 Z    =         5290441
91
 XDOT =       4954
580084                 XDOT =        1597
193925
 YDOT =     -24544
504734  feet/sec       YDOT =       -7463
790747  meter/sec
 ZDOT =      -2359
627081                 ZDOT =        -711
667109

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10522541
45                 X    =        -3207270
63
 Y    =       -9193844
70  feet           Y    =        -2802283
86  meter
 Z    =       17332167
20                 Z    =         5282844
56
 XDOT =      13541
845760                 XDOT =        4127
554588
 YDOT =     -19851
987199  feet/sec       YDOT =       -6050
885698  meter/sec
 ZDOT =      -2324
671461                 ZDOT =        -708
559861


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   19293
90479063  
00016717  00000-0  10270-3 0  9155
2 25544  51
6415  97
8978 0006776 171
2769 188
8501 15
50248281 34757


Satellite: ISS
Catalog Number: 25544
Epoch time:      19293
90479063   =   yrday
fracday
Element set:     915
Inclination:       51
6415  deg
RA of node:        97
8978  deg
Eccentricity:     
0006776     
Arg of perigee:   171
2769  deg
Mean anomaly:     188
8501  deg
Mean motion:   15
50248281  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3475
Checksum:              356


Coasting Arc #17 (Orbit 3489)
---------------------------------------

Vector Time (GMT): 2019/294/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4046561
96                 A    =         6789242
15  meter
 Y    =        1506974
61  meter          E    =           
0017033
 Z    =       -5253147
81                 I    =           52
00970
 XDOT =      -1224
283074                 Wp   =          121
68160
 YDOT =       7457
057118  meter/sec      RA   =           92
25727  deg
 ZDOT =       1190
281523                 TA   =          159
73849
                                          MA   =          159
67082
                                          Ha   =            228
556  n
mi
                                          Hp   =            220
335

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13276121
93                 X    =         4054926
96
 Y    =        4944142
44  feet           Y    =         1552272
88  meter
 Z    =      -17234736
90                 Z    =        -5233470
58
 XDOT =      -4016
676752                 XDOT =       -1313
360853
 YDOT =      24465
410491  feet/sec       YDOT =        7442
868258  meter/sec
 ZDOT =       3905
123108                 ZDOT =        1184
117972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10541067
39                 X    =         3212917
34
 Y    =        9626449
52  feet           Y    =         2934141
81  meter
 Z    =      -17145071
65                 Z    =        -5225817
84
 XDOT =     -12264
694115                 XDOT =       -3738
278766
 YDOT =      20368
470739  feet/sec       YDOT =        6208
309881  meter/sec
 ZDOT =       3876
465200                 ZDOT =        1181
546593


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   19294
87174664  
00016717  00000-0  10270-3 0  9162
2 25544  51
6421  93
1057 0006738 175
2507 184
8709 15
50215636 34904


Satellite: ISS
Catalog Number: 25544
Epoch time:      19294
87174664   =   yrday
fracday
Element set:     916
Inclination:       51
6421  deg
RA of node:        93
1057  deg
Eccentricity:     
0006738     
Arg of perigee:   175
2507  deg
Mean anomaly:     184
8709  deg
Mean motion:   15
50215636  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3490
Checksum:              330
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