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

 
Date: October 16th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15204 0235 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 562 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


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

297/21:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 2
000/00:00:00 000 0 0 0 0 220 7

301/10:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 8
000/00:00:00 000 0 0 0 0 221 2

Coasting Arc #1 (Orbit 3406)
---------------------------------------

Vector Time (GMT): 2019/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4780322
62                 A    =         6791519
21  meter
 Y    =       -1041962
94  meter          E    =           
0013049
 Z    =       -4720101
08                 I    =           51
96423
 XDOT =      -1282
764517                 Wp   =          102
12473
 YDOT =       6985
914030  meter/sec      RA   =          118
70306  deg
 ZDOT =      -2850
584778                 TA   =          139
70161
                                          MA   =          139
60483
                                          Ha   =            229
084  n
mi
                                          Hp   =            219
631

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15683473
16                 X    =         4814547
11
 Y    =       -3418513
57  feet           Y    =         -988314
85  meter
 Z    =      -15485895
92                 Z    =        -4696796
27
 XDOT =      -4208
545002                 XDOT =       -1346
940766
 YDOT =      22919
665453  feet/sec       YDOT =        6971
210288  meter/sec
 ZDOT =      -9352
312265                 ZDOT =       -2856
972334

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13060857
66                 X    =        -3980949
42
 Y    =        9505460
28  feet           Y    =         2897264
29  meter
 Z    =      -15379556
56                 Z    =        -4687688
84
 XDOT =      -4772
991232                 XDOT =       -1454
807728
 YDOT =     -21688
055578  feet/sec       YDOT =       -6610
519340  meter/sec
 ZDOT =      -9381
852831                 ZDOT =       -2859
588743


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
52125135  
00016717  00000-0  10270-3 0  9000
2 25544  51
6379 119
6194 0006812 156
1555 203
9912 15
50199261 34078


Satellite: ISS
Catalog Number: 25544
Epoch time:      19289
52125135   =   yrday
fracday
Element set:     900
Inclination:       51
6379  deg
RA of node:       119
6194  deg
Eccentricity:     
0006812     
Arg of perigee:   156
1555  deg
Mean anomaly:     203
9912  deg
Mean motion:   15
50199261  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3407
Checksum:              312


Coasting Arc #2 (Orbit 3422)
---------------------------------------

Vector Time (GMT): 2019/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4609615
75                 A    =         6790920
52  meter
 Y    =         992376
04  meter          E    =           
0013010
 Z    =        4883568
65                 I    =           51
97667
 XDOT =       1066
909694                 Wp   =          139
56750
 YDOT =      -7182
116457  meter/sec      RA   =          113
76848  deg
 ZDOT =       2453
223857                 TA   =          286
38653
                                          MA   =          286
52952
                                          Ha   =            229
108  n
mi
                                          Hp   =            219
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15123411
26                 X    =        -4644092
48
 Y    =        3255826
89  feet           Y    =          940635
41  meter
 Z    =       16022206
86                 Z    =         4861092
51
 XDOT =       3500
359889                 XDOT =        1135
226194
 YDOT =     -23563
374204  feet/sec       YDOT =       -7169
803477  meter/sec
 ZDOT =       8048
634701                 ZDOT =        2458
572755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12458604
33                 X    =         3797382
60
 Y    =       -9347587
14  feet           Y    =        -2849144
56  meter
 Z    =       15919638
25                 Z    =         4852305
74
 XDOT =       6078
113964                 XDOT =        1852
609136
 YDOT =      21925
480154  feet/sec       YDOT =        6682
886351  meter/sec
 ZDOT =       8073
472395                 ZDOT =        2460
794386


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
55269493  
00016717  00000-0  10270-3 0  9012
2 25544  51
6376 114
5077 0006762 159
8044 200
3376 15
50168488 34236


Satellite: ISS
Catalog Number: 25544
Epoch time:      19290
55269493   =   yrday
fracday
Element set:     901
Inclination:       51
6376  deg
RA of node:       114
5077  deg
Eccentricity:     
0006762     
Arg of perigee:   159
8044  deg
Mean anomaly:     200
3376  deg
Mean motion:   15
50168488  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3423
Checksum:              322


Coasting Arc #3 (Orbit 3437)
---------------------------------------

Vector Time (GMT): 2019/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4467342
26                 A    =         6790161
20  meter
 Y    =        -867925
30  meter          E    =           
0014735
 Z    =       -5050743
53                 I    =           51
98665
 XDOT =       -840
282843                 Wp   =          103
39714
 YDOT =       7335
095890  meter/sec      RA   =          108
83380  deg
 ZDOT =      -2011
936288                 TA   =          147
15457
                                          MA   =          147
06291
                                          Ha   =            228
979  n
mi
                                          Hp   =            219
839

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14656634
71                 X    =         4501249
93
 Y    =       -2847523
94  feet           Y    =         -817778
77  meter
 Z    =      -16570680
88                 Z    =        -5028959
97
 XDOT =      -2756
833475                 XDOT =        -912
470454
 YDOT =      24065
275230  feet/sec       YDOT =        7325
295615  meter/sec
 ZDOT =      -6600
840839                 ZDOT =       -2016
193550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12056725
59                 X    =        -3674889
96
 Y    =        8991413
10  feet           Y    =         2740582
71  meter
 Z    =      -16471267
61                 Z    =        -5020442
37
 XDOT =      -7374
939310                 XDOT =       -2247
881502
 YDOT =     -21967
779409  feet/sec       YDOT =       -6695
779164  meter/sec
 ZDOT =      -6620
731402                 ZDOT =       -2017
998931


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
51967184  
00016717  00000-0  10270-3 0  9022
2 25544  51
6374 109
7153 0006960 163
0234 197
1151 15
50200240 34386


Satellite: ISS
Catalog Number: 25544
Epoch time:      19291
51967184   =   yrday
fracday
Element set:     902
Inclination:       51
6374  deg
RA of node:       109
7153  deg
Eccentricity:     
0006960     
Arg of perigee:   163
0234  deg
Mean anomaly:     197
1151  deg
Mean motion:   15
50200240  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3438
Checksum:              292


Coasting Arc #4 (Orbit 3453)
---------------------------------------

Vector Time (GMT): 2019/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4343453
51                 A    =         6789748
40  meter
 Y    =         769443
53  meter          E    =           
0011010
 Z    =        5159125
48                 I    =           51
99535
 XDOT =        572
924284                 Wp   =          149
64759
 YDOT =      -7476
247456  meter/sec      RA   =          103
89982  deg
 ZDOT =       1586
649806                 TA   =          285
05940
                                          MA   =          285
18121
                                          Ha   =            228
980  n
mi
                                          Hp   =            219
947

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14250175
55                 X    =        -4376795
52
 Y    =        2524421
02  feet           Y    =          720685
51  meter
 Z    =       16926264
71                 Z    =         5137945
20
 XDOT =       1879
672847                 XDOT =         648
776047
 YDOT =     -24528
370919  feet/sec       YDOT =       -7469
416508  meter/sec
 ZDOT =       5205
543983                 ZDOT =        1589
617106

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11685156
96                 X    =         3561635
84
 Y    =       -8726989
62  feet           Y    =        -2659986
44  meter
 Z    =       16829598
94                 Z    =         5129661
76
 XDOT =       8769
385863                 XDOT =        2672
908811
 YDOT =      21875
846815  feet/sec       YDOT =        6667
758109  meter/sec
 ZDOT =       5219
580713                 ZDOT =        1590
928201


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
55111439  
00016717  00000-0  10270-3 0  9032
2 25544  51
6381 104
6034 0006846 167
1054 193
0273 15
50168292 34542


Satellite: ISS
Catalog Number: 25544
Epoch time:      19292
55111439   =   yrday
fracday
Element set:     903
Inclination:       51
6381  deg
RA of node:       104
6034  deg
Eccentricity:     
0006846     
Arg of perigee:   167
1054  deg
Mean anomaly:     193
0273  deg
Mean motion:   15
50168292  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3454
Checksum:              298


Coasting Arc #5 (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    =        4038656
10                 A    =         6788894
78  meter
 Y    =        1120342
80  meter          E    =           
0017709
 Z    =       -5354894
92                 I    =           51
99882
 XDOT =      -1770
005542                 Wp   =          113
81801
 YDOT =       7439
196168  meter/sec      RA   =          102
12418  deg
 ZDOT =        215
099487                 TA   =          158
26454
                                          MA   =          158
18929
                                          Ha   =            228
828  n
mi
                                          Hp   =            220
096

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13250184
05                 X    =         4051839
54
 Y    =        3675665
36  feet           Y    =         1165579
66  meter
 Z    =      -17568552
90                 Z    =        -5335244
24
 XDOT =      -5807
104797                 XDOT =       -1854
106094
 YDOT =      24406
811575  feet/sec       YDOT =        7418
932480  meter/sec
 ZDOT =        705
706978                 ZDOT =         206
297090

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10700345
44                 X    =         3261465
29
 Y    =        8815865
34  feet           Y    =         2687075
76  meter
 Z    =      -17478989
38                 Z    =        -5327595
96
 XDOT =     -14633
606466                 XDOT =       -4460
323251
 YDOT =      19121
982930  feet/sec       YDOT =        5828
380397  meter/sec
 ZDOT =        665
048079                 ZDOT =         202
706655


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
87343845  
00016717  00000-0  10270-3 0  9046
2 25544  51
6415 103
0084 0006854 168
2583 191
8729 15
50180065 34595


Satellite: ISS
Catalog Number: 25544
Epoch time:      19292
87343845   =   yrday
fracday
Element set:     904
Inclination:       51
6415  deg
RA of node:       103
0084  deg
Eccentricity:     
0006854     
Arg of perigee:   168
2583  deg
Mean anomaly:     191
8729  deg
Mean motion:   15
50180065  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3459
Checksum:              325


Coasting Arc #6 (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    =       -4025609
15                 A    =         6788894
15  meter
 Y    =       -1262055
41  meter          E    =           
0006590
 Z    =        5315153
31                 I    =           52
00482
 XDOT =       1472
258770                 Wp   =          145
27096
 YDOT =      -7493
287460  meter/sec      RA   =           97
19151  deg
 ZDOT =       -669
039028                 TA   =          311
05897
                                          MA   =          311
11590
                                          Ha   =            228
808  n
mi
                                          Hp   =            220
014

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13207379
09                 X    =        -4037015
74
 Y    =       -4140601
72  feet           Y    =        -1307136
43  meter
 Z    =       17438167
02                 Z    =         5295570
40
 XDOT =       4830
245309                 XDOT =        1559
191332
 YDOT =     -24584
276444  feet/sec       YDOT =       -7476
337548  meter/sec
 ZDOT =      -2195
009935                 ZDOT =        -661
676152

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10627605
68                 X    =        -3239294
21
 Y    =       -9040915
76  feet           Y    =        -2755671
12  meter
 Z    =       17348917
95                 Z    =         5287950
19
 XDOT =      13453
257078                 XDOT =        4100
552758
 YDOT =     -19930
166770  feet/sec       YDOT =       -6074
714832  meter/sec
 ZDOT =      -2160
894472                 ZDOT =        -658
640635


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
90487726  
00016717  00000-0  10270-3 0  9059
2 25544  51
6412  97
8978 0006790 171
1087 189
0185 15
50218646 34755


Satellite: ISS
Catalog Number: 25544
Epoch time:      19293
90487726   =   yrday
fracday
Element set:     905
Inclination:       51
6412  deg
RA of node:        97
8978  deg
Eccentricity:     
0006790     
Arg of perigee:   171
1087  deg
Mean anomaly:     189
0185  deg
Mean motion:   15
50218646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3475
Checksum:              348


Coasting Arc #7 (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    =        4057609
83                 A    =         6789291
71  meter
 Y    =        1438837
16  meter          E    =           
0017084
 Z    =       -5263811
26                 I    =           52
00939
 XDOT =      -1177
489608                 Wp   =          121
26219
 YDOT =       7473
988818  meter/sec      RA   =           92
25811  deg
 ZDOT =       1129
406949                 TA   =          159
56888
                                          MA   =          159
50046
                                          Ha   =            228
619  n
mi
                                          Hp   =            220
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13312368
21                 X    =         4066787
73
 Y    =        4720594
37  feet           Y    =         1484263
52  meter
 Z    =      -17269721
97                 Z    =        -5244078
39
 XDOT =      -3863
154883                 XDOT =       -1266
464502
 YDOT =      24520
960688  feet/sec       YDOT =        7460
323811  meter/sec
 ZDOT =       3705
403377                 ZDOT =        1123
470955

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10659121
73                 X    =         3248900
30
 Y    =        9433139
55  feet           Y    =         2875220
93  meter
 Z    =      -17179797
95                 Z    =        -5236402
42
 XDOT =     -12156
281858                 XDOT =       -3705
234710
 YDOT =      20469
678083  feet/sec       YDOT =        6239
157880  meter/sec
 ZDOT =       3677
782443                 ZDOT =        1120
988089


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
87185268  
00016717  00000-0  10270-3 0  9063
2 25544  51
6418  93
1059 0006759 175
0888 185
0330 15
50182878 34909


Satellite: ISS
Catalog Number: 25544
Epoch time:      19294
87185268   =   yrday
fracday
Element set:     906
Inclination:       51
6418  deg
RA of node:        93
1059  deg
Eccentricity:     
0006759     
Arg of perigee:   175
0888  deg
Mean anomaly:     185
0330  deg
Mean motion:   15
50182878  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3490
Checksum:              346


Coasting Arc #8 (Orbit 3505)
---------------------------------------

Vector Time (GMT): 2019/295/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4110698
27                 A    =         6789555
69  meter
 Y    =       -1579219
40  meter          E    =           
0005797
 Z    =        5163236
20                 I    =           52
00983
 XDOT =        884
863724                 Wp   =          132
89101
 YDOT =      -7449
756051  meter/sec      RA   =           87
32563  deg
 ZDOT =      -1576
809469                 TA   =          332
22211
                                          MA   =          332
25306
                                          Ha   =            228
619  n
mi
                                          Hp   =            220
280

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13486542
89                 X    =        -4117813
85
 Y    =       -5181166
01  feet           Y    =        -1625227
81  meter
 Z    =       16939751
32                 Z    =         5143250
53
 XDOT =       2903
096206                 XDOT =         975
762633
 YDOT =     -24441
456861  feet/sec       YDOT =       -7439
352665  meter/sec
 ZDOT =      -5173
259412                 ZDOT =       -1572
290156

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10813915
59                 X    =        -3296081
47
 Y    =       -9740001
34  feet           Y    =        -2968752
41  meter
 Z    =       16848682
40                 Z    =         5135478
40
 XDOT =      10851
783457                 XDOT =        3307
623598
 YDOT =     -20945
067360  feet/sec       YDOT =       -6384
056531  meter/sec
 ZDOT =      -5152
089984                 ZDOT =       -1570
357027


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   19295
90329108  
00016717  00000-0  10270-3 0  9072
2 25544  51
6407  87
9947 0006741 177
8718 182
2462 15
50222100 35063


Satellite: ISS
Catalog Number: 25544
Epoch time:      19295
90329108   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:        87
9947  deg
Eccentricity:     
0006741     
Arg of perigee:   177
8718  deg
Mean anomaly:     182
2462  deg
Mean motion:   15
50222100  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3506
Checksum:              319


Coasting Arc #9 (Orbit 3520)
---------------------------------------

Vector Time (GMT): 2019/296/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4210374
84                 A    =         6790202
58  meter
 Y    =        1738703
38  meter          E    =           
0015549
 Z    =       -5048906
80                 I    =           52
01056
 XDOT =       -608
877205                 Wp   =          129
42669
 YDOT =       7354
073697  meter/sec      RA   =           82
39259  deg
 ZDOT =       2019
342145                 TA   =          160
17039
                                          MA   =          160
10988
                                          Ha   =            228
360  n
mi
                                          Hp   =            220
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13813565
74                 X    =         4215144
27
 Y    =        5704407
41  feet           Y    =         1785813
22  meter
 Z    =      -16564654
87                 Z    =        -5028442
66
 XDOT =      -1997
628624                 XDOT =        -700
876282
 YDOT =      24127
538375  feet/sec       YDOT =        7346
750488  meter/sec
 ZDOT =       6625
138272                 ZDOT =        2016
160655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11103990
87                 X    =         3384496
42
 Y    =       10155615
03  feet           Y    =         3095431
46  meter
 Z    =      -16471415
35                 Z    =        -5020487
40
 XDOT =      -9496
984764                 XDOT =       -2894
680956
 YDOT =      21133
866071  feet/sec       YDOT =        6441
602378  meter/sec
 ZDOT =       6610
067680                 ZDOT =        2014
748629


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   19296
87026344  
00016717  00000-0  10270-3 0  9086
2 25544  51
6424  83
2026 0006614 182
5930 177
5187 15
50189210 35219


Satellite: ISS
Catalog Number: 25544
Epoch time:      19296
87026344   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:        83
2026  deg
Eccentricity:     
0006614     
Arg of perigee:   182
5930  deg
Mean anomaly:     177
5187  deg
Mean motion:   15
50189210  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3521
Checksum:              309


Coasting Arc #10 (Orbit 3536)
---------------------------------------

Vector Time (GMT): 2019/297/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4325150
65                 A    =         6790705
62  meter
 Y    =       -1857819
27  meter          E    =           
0006251
 Z    =        4888539
45                 I    =           52
00545
 XDOT =        347
250588                 Wp   =          118
55966
 YDOT =      -7255
658160  meter/sec      RA   =           77
45992  deg
 ZDOT =      -2450
714499                 TA   =          355
36900
                                          MA   =          355
37478
                                          Ha   =            228
356  n
mi
                                          Hp   =            220
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14190126
81                 X    =        -4327800
64
 Y    =       -6095207
57  feet           Y    =        -1906200
68  meter
 Z    =       16038515
25                 Z    =         4867522
89
 XDOT =       1139
273584                 XDOT =         440
264020
 YDOT =     -23804
652755  feet/sec       YDOT =       -7251
255037  meter/sec
 ZDOT =      -8040
401899                 ZDOT =       -2448
801306

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11500873
36                 X    =        -3505466
20
 Y    =      -10454821
82  feet           Y    =        -3186629
69  meter
 Z    =       15942767
59                 Z    =         4859355
56
 XDOT =       8188
466939                 XDOT =        2495
844723
 YDOT =     -21251
863683  feet/sec       YDOT =       -6477
568051  meter/sec
 ZDOT =      -8031
113255                 ZDOT =       -2447
883320


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   19297
90169910  
00016717  00000-0  10270-3 0  9099
2 25544  51
6407  78
0910 0006556 185
1709 174
9375 15
50228236 35371


Satellite: ISS
Catalog Number: 25544
Epoch time:      19297
90169910   =   yrday
fracday
Element set:     909
Inclination:       51
6407  deg
RA of node:        78
0910  deg
Eccentricity:     
0006556     
Arg of perigee:   185
1709  deg
Mean anomaly:     174
9375  deg
Mean motion:   15
50228236  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3537
Checksum:              334


Coasting Arc #11 (Orbit 3537)
---------------------------------------

Vector Time (GMT): 2019/297/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1800659
81                 A    =         6794768
18  meter
 Y    =        5360458
90  meter          E    =           
0013268
 Z    =        3764661
40                 I    =           52
01685
 XDOT =      -4456
179752                 Wp   =          125
68378
 YDOT =      -4521
215905  meter/sec      RA   =           77
24769  deg
 ZDOT =       4288
179068                 TA   =          278
99158
                                          MA   =          279
14172
                                          Ha   =            228
183  n
mi
                                          Hp   =            220
705

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5907676
54                 X    =        -1878755
06
 Y    =       17586807
42  feet           Y    =         5339886
23  meter
 Z    =       12351251
30                 Z    =         3755724
34
 XDOT =     -14620
012310                 XDOT =       -4426
120876
 YDOT =     -14833
385514  feet/sec       YDOT =       -4570
879719  meter/sec
 ZDOT =      14068
828964                 ZDOT =        4266
605624

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6109152
22                 X    =        -1862069
60
 Y    =       17546808
90  feet           Y    =         5348267
35  meter
 Z    =       12310061
03                 Z    =         3752106
60
 XDOT =     -13334
880114                 XDOT =       -4064
471459
 YDOT =     -14485
796237  feet/sec       YDOT =       -4415
270693  meter/sec
 ZDOT =      13970
746114                 ZDOT =        4258
283416


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   19297
96616384  
00016717  00000-0  10270-3 0  9109
2 25544  51
6389  77
7719 0006571 186
9777 173
1284 15
50223730 35389


Satellite: ISS
Catalog Number: 25544
Epoch time:      19297
96616384   =   yrday
fracday
Element set:     910
Inclination:       51
6389  deg
RA of node:        77
7719  deg
Eccentricity:     
0006571     
Arg of perigee:   186
9777  deg
Mean anomaly:     173
1284  deg
Mean motion:   15
50223730  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3538
Checksum:              352


Coasting Arc #12 (Orbit 3552)
---------------------------------------

Vector Time (GMT): 2019/298/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1675643
52                 A    =         6793876
54  meter
 Y    =       -5184677
78  meter          E    =           
0007082
 Z    =       -4059896
35                 I    =           52
00493
 XDOT =       4693
931081                 Wp   =          126
30134
 YDOT =       4594
215320  meter/sec      RA   =           72
31628  deg
 ZDOT =      -3938
544763                 TA   =          103
00185
                                          MA   =          102
92277
                                          Ha   =            228
167  n
mi
                                          Hp   =            220
875

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5497518
11                 X    =         1753216
63
 Y    =      -17010097
70  feet           Y    =        -5165506
10  meter
 Z    =      -13319869
93                 Z    =        -4051567
78
 XDOT =      15400
036356                 XDOT =        4661
339971
 YDOT =      15072
884908  feet/sec       YDOT =        4646
523666  meter/sec
 ZDOT =     -12921
734786                 ZDOT =       -3915
822487

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5408866
56                 X    =         1648622
53
 Y    =      -17068451
72  feet           Y    =        -5202464
08  meter
 Z    =      -13281460
11                 Z    =        -4048189
04
 XDOT =      14399
171193                 XDOT =        4388
867380
 YDOT =      14514
735810  feet/sec       YDOT =        4424
091475  meter/sec
 ZDOT =     -12818
427413                 ZDOT =       -3907
056676


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   19298
93313652  
00016717  00000-0  10270-3 0  9110
2 25544  51
6387  72
9792 0006511 189
5070 170
5956 15
50193729 35532


Satellite: ISS
Catalog Number: 25544
Epoch time:      19298
93313652   =   yrday
fracday
Element set:     911
Inclination:       51
6387  deg
RA of node:        72
9792  deg
Eccentricity:     
0006511     
Arg of perigee:   189
5070  deg
Mean anomaly:     170
5956  deg
Mean motion:   15
50193729  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3553
Checksum:              336


Coasting Arc #13 (Orbit 3568)
---------------------------------------

Vector Time (GMT): 2019/299/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1549270
39                 A    =         6792910
72  meter
 Y    =        5023223
01  meter          E    =           
0012043
 Z    =        4301556
65                 I    =           51
99165
 XDOT =      -4956
491793                 Wp   =          139
82418
 YDOT =      -4611
486439  meter/sec      RA   =           67
38510  deg
 ZDOT =       3585
457296                 TA   =          273
66555
                                          MA   =          273
80326
                                          Ha   =            227
920  n
mi
                                          Hp   =            221
029

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5082908
10                 X    =        -1626221
44
 Y    =       16480390
45  feet           Y    =         5005468
00  meter
 Z    =       14112718
68                 Z    =         4293843
47
 XDOT =     -16261
456015                 XDOT =       -4921
972996
 YDOT =     -15129
548685  feet/sec       YDOT =       -4666
720187  meter/sec
 ZDOT =      11763
311340                 ZDOT =        3561
464112

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4720027
42                 X    =        -1438664
36
 Y    =       16618186
53  feet           Y    =         5065223
25  meter
 Z    =       14077118
67                 Z    =         4290705
77
 XDOT =     -15540
974964                 XDOT =       -4736
889169
 YDOT =     -14326
759766  feet/sec       YDOT =       -4366
796377  meter/sec
 ZDOT =      11654
221471                 ZDOT =        3552
206704


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   19299
96457081  
00016717  00000-0  10270-3 0  9120
2 25544  51
6396  67
8683 0006558 195
0872 165
0084 15
50233324 35691


Satellite: ISS
Catalog Number: 25544
Epoch time:      19299
96457081   =   yrday
fracday
Element set:     912
Inclination:       51
6396  deg
RA of node:        67
8683  deg
Eccentricity:     
0006558     
Arg of perigee:   195
0872  deg
Mean anomaly:     165
0084  deg
Mean motion:   15
50233324  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3569
Checksum:              345


Coasting Arc #14 (Orbit 3583)
---------------------------------------

Vector Time (GMT): 2019/300/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1491026
57                 A    =         6792092
36  meter
 Y    =       -4826384
54  meter          E    =           
0007699
 Z    =       -4545203
96                 I    =           51
97564
 XDOT =       5217
114520                 Wp   =          110
32032
 YDOT =       4608
726661  meter/sec      RA   =           62
45083  deg
 ZDOT =      -3189
362390                 TA   =          127
79326
                                          MA   =          127
72351
                                          Ha   =            227
866  n
mi
                                          Hp   =            221
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4891819
45                 X    =         1566964
47
 Y    =      -15834594
95  feet           Y    =        -4809286
46  meter
 Z    =      -14912086
48                 Z    =        -4537776
23
 XDOT =      17116
517454                 XDOT =        5180
683227
 YDOT =      15120
494295  feet/sec       YDOT =        4666
864263  meter/sec
 ZDOT =     -10463
787368                 ZDOT =       -3164
107625

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4276939
27                 X    =         1303611
09
 Y    =      -16043493
55  feet           Y    =        -4890056
83  meter
 Z    =      -14877792
96                 Z    =        -4534751
29
 XDOT =      16677
783195                 XDOT =        5083
388318
 YDOT =      14021
796978  feet/sec       YDOT =        4273
843719  meter/sec
 ZDOT =     -10348
958096                 ZDOT =       -3154
362428


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   19300
93154094  
00016717  00000-0  10270-3 0  9139
2 25544  51
6405  63
0754 0006367 197
4285 162
6648 15
50203026 35843


Satellite: ISS
Catalog Number: 25544
Epoch time:      19300
93154094   =   yrday
fracday
Element set:     913
Inclination:       51
6405  deg
RA of node:        63
0754  deg
Eccentricity:     
0006367     
Arg of perigee:   197
4285  deg
Mean anomaly:     162
6648  deg
Mean motion:   15
50203026  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3584
Checksum:              306


Coasting Arc #15 (Orbit 3592)
---------------------------------------

Vector Time (GMT): 2019/301/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         107096
47                 A    =         6795212
65  meter
 Y    =        5764537
34  meter          E    =           
0012063
 Z    =        3594640
77                 I    =           51
97922
 XDOT =      -5610
959912                 Wp   =          126
01605
 YDOT =      -2691
601716  meter/sec      RA   =           59
76102  deg
 ZDOT =       4466
188256                 TA   =          276
17340
                                          MA   =          276
31082
                                          Ha   =            227
829  n
mi
                                          Hp   =            221
185

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         351366
38                 X    =           25166
51
 Y    =       18912524
09  feet           Y    =         5765277
00  meter
 Z    =       11793440
84                 Z    =         3594961
81
 XDOT =     -18408
661128                 XDOT =       -5602
139507
 YDOT =      -8830
714291  feet/sec       YDOT =       -2754
297954  meter/sec
 ZDOT =      14652
848610                 ZDOT =        4438
953052

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6525697
06                 X    =        -1989032
46
 Y    =      -17753856
71  feet           Y    =        -5411375
52  meter
 Z    =       11794410
65                 Z    =         3594936
37
 XDOT =      19093
039240                 XDOT =        5819
558360
 YDOT =       2671
834266  feet/sec       YDOT =         814
375084  meter/sec
 ZDOT =      14528
828907                 ZDOT =        4428
387051


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   19301
51172151  
00016717  00000-0  10270-3 0  9149
2 25544  51
6420  60
1968 0006851 199
4216 160
6674 15
50238629 35933


Satellite: ISS
Catalog Number: 25544
Epoch time:      19301
51172151   =   yrday
fracday
Element set:     914
Inclination:       51
6420  deg
RA of node:        60
1968  deg
Eccentricity:     
0006851     
Arg of perigee:   199
4216  deg
Mean anomaly:     160
6674  deg
Mean motion:   15
50238629  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3593
Checksum:              306


Coasting Arc #16 (Orbit 3607)
---------------------------------------

Vector Time (GMT): 2019/302/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -182885
01                 A    =         6794324
09  meter
 Y    =       -5559140
62  meter          E    =           
0005787
 Z    =       -3901407
68                 I    =           51
95806
 XDOT =       5857
625057                 Wp   =          141
46981
 YDOT =       2701
019346  meter/sec      RA   =           54
82846  deg
 ZDOT =      -4130
978430                 TA   =           85
34469
                                          MA   =           85
27860
                                          Ha   =            227
780  n
mi
                                          Hp   =            221
381

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -600016
44                 X    =         -101756
07
 Y    =      -18238650
32  feet           Y    =        -5560732
18  meter
 Z    =      -12799893
97                 Z    =        -3902098
99
 XDOT =      19217
929978                 XDOT =        5847
052709
 YDOT =       8861
612026  feet/sec       YDOT =        2766
464296  meter/sec
 ZDOT =     -13553
078840                 ZDOT =       -4102
549150

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6822631
79                 X    =         2079538
17
 Y    =       16923119
38  feet           Y    =         5158166
79  meter
 Z    =      -12802554
30                 Z    =        -3902218
55
 XDOT =     -19950
954455                 XDOT =       -6081
050918
 YDOT =      -2092
734469  feet/sec       YDOT =        -637
865466  meter/sec
 ZDOT =     -13423
623310                 ZDOT =       -4091
520385


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   19302
47869126  
00016717  00000-0  10270-3 0  9151
2 25544  51
6419  55
4057 0006825 202
7986 157
2862 15
50207374 36081


Satellite: ISS
Catalog Number: 25544
Epoch time:      19302
47869126   =   yrday
fracday
Element set:     915
Inclination:       51
6419  deg
RA of node:        55
4057  deg
Eccentricity:     
0006825     
Arg of perigee:   202
7986  deg
Mean anomaly:     157
2862  deg
Mean motion:   15
50207374  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3608
Checksum:              326


Coasting Arc #17 (Orbit 3623)
---------------------------------------

Vector Time (GMT): 2019/303/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         259941
36                 A    =         6793350
27  meter
 Y    =        5364758
64  meter          E    =           
0011065
 Z    =        4159483
82                 I    =           51
93615
 XDOT =      -6108
692824                 Wp   =          141
05756
 YDOT =      -2650
292746  meter/sec      RA   =           49
89352  deg
 ZDOT =       3786
167453                 TA   =          269
99132
                                          MA   =          270
11812
                                          Ha   =            227
548  n
mi
                                          Hp   =            221
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         852825
99                 X    =          179726
74
 Y    =       17600914
17  feet           Y    =         5367216
91  meter
 Z    =       13646600
45                 Z    =         4160551
81
 XDOT =     -20041
643125                 XDOT =       -6096
994069
 YDOT =      -8695
186176  feet/sec       YDOT =       -2718
539113  meter/sec
 ZDOT =      12421
809228                 ZDOT =        3756
521271

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7110938
23                 X    =        -2167413
97
 Y    =      -16119381
35  feet           Y    =        -4913187
44  meter
 Z    =       13650981
58                 Z    =         4160819
18
 XDOT =      20733
525709                 XDOT =        6319
578636
 YDOT =       1297
316885  feet/sec       YDOT =         395
422186  meter/sec
 ZDOT =      12286
806839                 ZDOT =        3745
018725


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   19303
51012253  
00016717  00000-0  10270-3 0  9169
2 25544  51
6431  50
2945 0006847 207
2785 152
8007 15
50242009 36249


Satellite: ISS
Catalog Number: 25544
Epoch time:      19303
51012253   =   yrday
fracday
Element set:     916
Inclination:       51
6431  deg
RA of node:        50
2945  deg
Eccentricity:     
0006847     
Arg of perigee:   207
2785  deg
Mean anomaly:     152
8007  deg
Mean motion:   15
50242009  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3624
Checksum:              282


Coasting Arc #18 (Orbit 3638)
---------------------------------------

Vector Time (GMT): 2019/304/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -265623
85                 A    =         6792509
45  meter
 Y    =       -5156563
57  meter          E    =           
0005701
 Z    =       -4416162
94                 I    =           51
91134
 XDOT =       6357
717246                 Wp   =          117
25379
 YDOT =       2580
588001  meter/sec      RA   =           44
95685  deg
 ZDOT =      -3401
555140                 TA   =          118
41899
                                          MA   =          118
36153
                                          Ha   =            227
477  n
mi
                                          Hp   =            221
727

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -871469
31                 X    =         -186490
14
 Y    =      -16917859
49  feet           Y    =        -5159091
35  meter
 Z    =      -14488723
56                 Z    =        -4417261
24
 XDOT =      20858
652382                 XDOT =        6344
911096
 YDOT =       8466
496066  feet/sec       YDOT =        2651
612992  meter/sec
 ZDOT =     -11159
957810                 ZDOT =       -3370
702020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7139808
38                 X    =         2176213
59
 Y    =       15357909
74  feet           Y    =         4681090
89  meter
 Z    =      -14493249
58                 Z    =        -4417542
47
 XDOT =     -21460
333567                 XDOT =       -6541
109671
 YDOT =       -403
967681  feet/sec       YDOT =        -123
129349  meter/sec
 ZDOT =     -11019
450468                 ZDOT =       -3358
728503


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   19304
47708983  
00016717  00000-0  10270-3 0  9178
2 25544  51
6438  45
5032 0006744 210
5409 149
5350 15
50210622 36392


Satellite: ISS
Catalog Number: 25544
Epoch time:      19304
47708983   =   yrday
fracday
Element set:     917
Inclination:       51
6438  deg
RA of node:        45
5032  deg
Eccentricity:     
0006744     
Arg of perigee:   210
5409  deg
Mean anomaly:     149
5350  deg
Mean motion:   15
50210622  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3639
Checksum:              304
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