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

 
Date: February 15th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


050/05:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 9
000/00:00:00 000 0 0 0 0 214 5

054/08:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 2
000/00:00:00 000 0 0 0 0 214 1

057/02:24:53 072 -3 0 3 0 3 0
N/A -0 1 -0 3 224 4
000/00:07:46 144 -0 3 -0 2 215 7

057/14:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 3
000/00:00:00 000 0 0 0 0 215 7

060/17:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 224 6
000/00:00:00 000 0 0 0 0 215 6

Coasting Arc #1 (Orbit 3633)
---------------------------------------

Vector Time (GMT): 2019/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3694101
45                 A    =         6791113
16  meter
 Y    =       -5539495
48  meter          E    =           
0014246
 Z    =       -1303255
95                 I    =           51
30431
 XDOT =       3438
820952                 Wp   =           33
54134
 YDOT =      -3648
486094  meter/sec      RA   =          245
32261  deg
 ZDOT =       5802
594689                 TA   =          312
21070
                                          MA   =          312
33153
                                          Ha   =            223
769  n
mi
                                          Hp   =            214
911

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12119755
41                 X    =        -3625552
31
 Y    =      -18174197
77  feet           Y    =        -5580422
21  meter
 Z    =       -4275774
12                 Z    =        -1321033
76
 XDOT =      11282
220972                 XDOT =        3451
178482
 YDOT =     -11970
098734  feet/sec       YDOT =       -3609
961754  meter/sec
 ZDOT =      19037
384150                 ZDOT =        5819
328884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         778477
40                 X    =          237279
91
 Y    =      -21815043
10  feet           Y    =        -6649225
14  meter
 Z    =       -4355461
82                 Z    =        -1327544
76
 XDOT =      14450
791214                 XDOT =        4404
601162
 YDOT =      -3273
291026  feet/sec       YDOT =        -997
699105  meter/sec
 ZDOT =      19113
236262                 ZDOT =        5825
714413


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   19046
50258410  
00016717  00000-0  10270-3 0  9002
2 25544  51
6368 246
3319 0005511  26
3589 333
7842 15
53257573 36343


Satellite: ISS
Catalog Number: 25544
Epoch time:      19046
50258410   =   yrday
fracday
Element set:     900
Inclination:       51
6368  deg
RA of node:       246
3319  deg
Eccentricity:     
0005511     
Arg of perigee:    26
3589  deg
Mean anomaly:     333
7842  deg
Mean motion:   15
53257573  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3634
Checksum:              309


Coasting Arc #2 (Orbit 3649)
---------------------------------------

Vector Time (GMT): 2019/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3262249
00                 A    =         6791767
52  meter
 Y    =        5952814
94  meter          E    =           
0011675
 Z    =        -139597
91                 I    =           51
32180
 XDOT =      -4255
748079                 Wp   =          107
81020
 YDOT =       2201
766740  meter/sec      RA   =          240
33317  deg
 ZDOT =      -5980
656382                 TA   =           73
69900
                                          MA   =           73
57062
                                          Ha   =            223
895  n
mi
                                          Hp   =            214
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10702916
67                 X    =         3196118
57
 Y    =       19530232
75  feet           Y    =         5988925
93  meter
 Z    =        -457998
39                 Z    =         -123912
04
 XDOT =     -13962
428080                 XDOT =       -4251
002500
 YDOT =       7223
644161  feet/sec       YDOT =        2154
202584  meter/sec
 ZDOT =     -19621
576058                 ZDOT =       -6001
317208

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2313641
90                 X    =         -705198
05
 Y    =       22151498
31  feet           Y    =         6751776
68  meter
 Z    =        -387766
46                 Z    =         -118191
22
 XDOT =     -13867
417468                 XDOT =       -4226
788844
 YDOT =      -1765
192626  feet/sec       YDOT =        -538
030712  meter/sec
 ZDOT =     -19715
013360                 ZDOT =       -6009
136072


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   19047
53199069  
00016717  00000-0  10270-3 0  9011
2 25544  51
6370 241
2062 0005675  29
7223 330
4250 15
53286579 36501


Satellite: ISS
Catalog Number: 25544
Epoch time:      19047
53199069   =   yrday
fracday
Element set:     901
Inclination:       51
6370  deg
RA of node:       241
2062  deg
Eccentricity:     
0005675     
Arg of perigee:    29
7223  deg
Mean anomaly:     330
4250  deg
Mean motion:   15
53286579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3650
Checksum:              306


Coasting Arc #3 (Orbit 3665)
---------------------------------------

Vector Time (GMT): 2019/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2686499
44                 A    =         6790887
20  meter
 Y    =       -6035469
90  meter          E    =           
0019025
 Z    =        1527484
73                 I    =           51
33449
 XDOT =       5037
972399                 Wp   =           54
51994
 YDOT =       -781
211114  meter/sec      RA   =          235
34362  deg
 ZDOT =       5734
279489                 TA   =          322
24885
                                          MA   =          322
38217
                                          Ha   =            223
966  n
mi
                                          Hp   =            214
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8813974
56                 X    =        -2626228
92
 Y    =      -19801410
42  feet           Y    =        -6065175
21  meter
 Z    =        5011432
85                 Z    =         1514581
49
 XDOT =      16528
780837                 XDOT =        5018
480502
 YDOT =      -2563
028589  feet/sec       YDOT =        -724
981953  meter/sec
 ZDOT =      18813
252916                 ZDOT =        5758
704070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3628593
75                 X    =         1105995
38
 Y    =      -21382006
68  feet           Y    =        -6517235
63  meter
 Z    =        4953741
96                 Z    =         1509900
55
 XDOT =      13507
500655                 XDOT =        4117
086200
 YDOT =       6706
898817  feet/sec       YDOT =        2044
262760  meter/sec
 ZDOT =      18923
554071                 ZDOT =        5767
899281


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   19048
56139548  
00016717  00000-0  10270-3 0  9022
2 25544  51
6355 236
0800 0005585  35
0639 325
0880 15
53263123 36663


Satellite: ISS
Catalog Number: 25544
Epoch time:      19048
56139548   =   yrday
fracday
Element set:     902
Inclination:       51
6355  deg
RA of node:       236
0800  deg
Eccentricity:     
0005585     
Arg of perigee:    35
0639  deg
Mean anomaly:     325
0880  deg
Mean motion:   15
53263123  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3666
Checksum:              309


Coasting Arc #4 (Orbit 3680)
---------------------------------------

Vector Time (GMT): 2019/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1901219
43                 A    =         6788366
65  meter
 Y    =        5865627
37  meter          E    =           
0008010
 Z    =       -2848972
83                 I    =           51
34553
 XDOT =      -5730
205577                 Wp   =           74
38159
 YDOT =       -588
993405  meter/sec      RA   =          230
35234  deg
 ZDOT =      -5046
392602                 TA   =          138
10474
                                          MA   =          138
04341
                                          Ha   =            224
049  n
mi
                                          Hp   =            214
516

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6237596
54                 X    =         1849325
33
 Y    =       19244184
29  feet           Y    =         5886597
89  meter
 Z    =       -9347023
71                 Z    =        -2839863
91
 XDOT =     -18799
887063                 XDOT =       -5698
681582
 YDOT =      -1932
393061  feet/sec       YDOT =        -652
896454  meter/sec
 ZDOT =     -16556
406174                 ZDOT =       -5074
150364

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5101968
62                 X    =        -1555080
04
 Y    =       19595243
27  feet           Y    =         5972630
15  meter
 Z    =       -9306419
79                 Z    =        -2836596
75
 XDOT =     -13248
900359                 XDOT =       -4038
264829
 YDOT =     -11356
948482  feet/sec       YDOT =       -3461
597897  meter/sec
 ZDOT =     -16681
643449                 ZDOT =       -5084
564923


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   19049
52646023  
00016717  00000-0  10270-3 0  9031
2 25544  51
6348 231
2749 0005701  39
2063 320
9501 15
53287629 36819


Satellite: ISS
Catalog Number: 25544
Epoch time:      19049
52646023   =   yrday
fracday
Element set:     903
Inclination:       51
6348  deg
RA of node:       231
2749  deg
Eccentricity:     
0005701     
Arg of perigee:    39
2063  deg
Mean anomaly:     320
9501  deg
Mean motion:   15
53287629  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3681
Checksum:              304


Coasting Arc #5 (Orbit 3692)
---------------------------------------

Vector Time (GMT): 2019/050/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2505857
22                 A    =         6779922
59  meter
 Y    =       -3467682
36  meter          E    =           
0007008
 Z    =        5253724
32                 I    =           51
33763
 XDOT =       5646
103198                 Wp   =           66
23326
 YDOT =       5147
114705  meter/sec      RA   =          226
59489  deg
 ZDOT =        706
333007                 TA   =           17
00778
                                          MA   =           16
98431
                                          Ha   =            223
907  n
mi
                                          Hp   =            214
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8221316
33                 X    =         2518928
70
 Y    =      -11376910
63  feet           Y    =        -3439586
74  meter
 Z    =       17236628
35                 Z    =         5265928
39
 XDOT =      18523
960625                 XDOT =        5584
696216
 YDOT =      16886
859267  feet/sec       YDOT =        5209
910063  meter/sec
 ZDOT =       2317
365507                 ZDOT =         733
609387

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5270944
04                 X    =         1606583
74
 Y    =       12935570
20  feet           Y    =         3942761
80  meter
 Z    =       17292011
65                 Z    =         5270605
15
 XDOT =     -23227
217277                 XDOT =       -7079
655826
 YDOT =       6211
595422  feet/sec       YDOT =        1893
294285  meter/sec
 ZDOT =       2440
054639                 ZDOT =         743
728654


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   19050
29851099  
00016717  00000-0  10270-3 0  9049
2 25544  51
6386 227
4344 0005643  40
2449 319
9120 15
53305359 36933


Satellite: ISS
Catalog Number: 25544
Epoch time:      19050
29851099   =   yrday
fracday
Element set:     904
Inclination:       51
6386  deg
RA of node:       227
4344  deg
Eccentricity:     
0005643     
Arg of perigee:    40
2449  deg
Mean anomaly:     319
9120  deg
Mean motion:   15
53305359  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3693
Checksum:              316


Coasting Arc #6 (Orbit 3707)
---------------------------------------

Vector Time (GMT): 2019/051/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3549567
97                 A    =         6780048
43  meter
 Y    =        2455089
48  meter          E    =           
0018523
 Z    =       -5244607
29                 I    =           51
36297
 XDOT =      -5178
366180                 Wp   =           82
58803
 YDOT =      -5562
867365  meter/sec      RA   =          221
58355  deg
 ZDOT =        905
763093                 TA   =          196
09648
                                          MA   =          196
15541
                                          Ha   =            224
114  n
mi
                                          Hp   =            214
232

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11645564
22                 X    =        -3551283
02
 Y    =        8054755
51  feet           Y    =         2415385
70  meter
 Z    =      -17206716
84                 Z    =        -5261853
63
 XDOT =     -16989
390355                 XDOT =       -5120
175330
 YDOT =     -18250
877183  feet/sec       YDOT =       -5620
450031  meter/sec
 ZDOT =       2971
663692                 ZDOT =         880
751065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -873491
48                 X    =         -266240
20
 Y    =      -14037197
08  feet           Y    =        -4278537
67  meter
 Z    =      -17284775
59                 Z    =        -5268399
60
 XDOT =      23413
673547                 XDOT =        7136
487697
 YDOT =      -4957
148274  feet/sec       YDOT =       -1510
938794  meter/sec
 ZDOT =       2859
204945                 ZDOT =         871
485667


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   19051
26357232  
00016717  00000-0  10270-3 0  9058
2 25544  51
6400 222
6293 0005783  43
5138 316
6469 15
53291304 37087


Satellite: ISS
Catalog Number: 25544
Epoch time:      19051
26357232   =   yrday
fracday
Element set:     905
Inclination:       51
6400  deg
RA of node:       222
6293  deg
Eccentricity:     
0005783     
Arg of perigee:    43
5138  deg
Mean anomaly:     316
6469  deg
Mean motion:   15
53291304  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3708
Checksum:              299


Coasting Arc #7 (Orbit 3723)
---------------------------------------

Vector Time (GMT): 2019/052/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4543672
38                 A    =         6781676
43  meter
 Y    =       -1423768
90  meter          E    =           
0012757
 Z    =        4822990
74                 I    =           51
39435
 XDOT =       4437
214675                 Wp   =           53
87232
 YDOT =       5749
365669  meter/sec      RA   =          216
57635  deg
 ZDOT =      -2471
032944                 TA   =           60
53384
                                          MA   =           60
40662
                                          Ha   =            224
001  n
mi
                                          Hp   =            214
246

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14907061
63                 X    =         4535828
84
 Y    =       -4671157
81  feet           Y    =        -1373001
73  meter
 Z    =       15823460
43                 Z    =         4845042
75
 XDOT =      14557
790929                 XDOT =        4384
596477
 YDOT =      18862
748258  feet/sec       YDOT =        5798
691236  meter/sec
 ZDOT =      -8107
063463                 ZDOT =       -2449
607553

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3458315
64                 X    =        -1054094
61
 Y    =       15129968
34  feet           Y    =         4611614
35  meter
 Z    =       15923134
51                 Z    =         4853371
40
 XDOT =     -22558
929572                 XDOT =       -6875
961734
 YDOT =       3315
420106  feet/sec       YDOT =        1010
540048  meter/sec
 ZDOT =      -8010
789925                 ZDOT =       -2441
688769


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   19052
29296696  
00016717  00000-0  10270-3 0  9069
2 25544  51
6399 217
5042 0005833  46
1423 314
0211 15
53322585 37242


Satellite: ISS
Catalog Number: 25544
Epoch time:      19052
29296696   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       217
5042  deg
Eccentricity:     
0005833     
Arg of perigee:    46
1423  deg
Mean anomaly:     314
0211  deg
Mean motion:   15
53322585  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3724
Checksum:              305


Coasting Arc #8 (Orbit 3738)
---------------------------------------

Vector Time (GMT): 2019/053/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5402232
80                 A    =         6784605
91  meter
 Y    =         500944
73  meter          E    =           
0011515
 Z    =       -4082844
91                 I    =           51
43155
 XDOT =      -3414
756380                 Wp   =           83
88272
 YDOT =      -5684
838469  meter/sec      RA   =          211
57691  deg
 ZDOT =       3831
279240                 TA   =          225
84789
                                          MA   =          225
94263
                                          Ha   =            224
151  n
mi
                                          Hp   =            214
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17723860
88                 X    =        -5387601
19
 Y    =        1643519
46  feet           Y    =          440614
54  meter
 Z    =      -13395160
48                 Z    =        -4109050
95
 XDOT =     -11203
268963                 XDOT =       -3369
542990
 YDOT =     -18651
044846  feet/sec       YDOT =       -5722
771430  meter/sec
 ZDOT =      12569
813778                 ZDOT =        3814
802403

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7225867
92                 X    =         2202444
54
 Y    =      -16169051
08  feet           Y    =        -4928326
77  meter
 Z    =      -13513524
53                 Z    =        -4118922
28
 XDOT =      20610
137999                 XDOT =        6281
970062
 YDOT =      -1204
408132  feet/sec       YDOT =        -367
103599  meter/sec
 ZDOT =      12495
860614                 ZDOT =        3808
738315


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   19053
25802486  
00016717  00000-0  10270-3 0  9077
2 25544  51
6402 212
6998 0005759  49
3718 310
7934 15
53284529 37398


Satellite: ISS
Catalog Number: 25544
Epoch time:      19053
25802486   =   yrday
fracday
Element set:     907
Inclination:       51
6402  deg
RA of node:       212
6998  deg
Eccentricity:     
0005759     
Arg of perigee:    49
3718  deg
Mean anomaly:     310
7934  deg
Mean motion:   15
53284529  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3739
Checksum:              339


Coasting Arc #9 (Orbit 3754)
---------------------------------------

Vector Time (GMT): 2019/054/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6071356
31                 A    =         6787849
18  meter
 Y    =         367276
30  meter          E    =           
0017826
 Z    =        3000111
01                 I    =           51
47198
 XDOT =       2125
518853                 Wp   =           83
82669
 YDOT =       5465
184800  meter/sec      RA   =          206
58657  deg
 ZDOT =      -4943
288109                 TA   =           61
73947
                                          MA   =           61
55966
                                          Ha   =            224
202  n
mi
                                          Hp   =            214
112

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19919148
01                 X    =         6052225
44
 Y    =        1204974
74  feet           Y    =          435063
79  meter
 Z    =        9842883
90                 Z    =         3029556
44
 XDOT =       6973
487051                 XDOT =        2088
259034
 YDOT =      17930
396325  feet/sec       YDOT =        5488
744991  meter/sec
 ZDOT =     -16218
136839                 ZDOT =       -4933
054353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10507705
75                 X    =        -3202748
71
 Y    =       16887212
23  feet           Y    =         5147222
29  meter
 Z    =        9975819
16                 Z    =         3040629
68
 XDOT =     -17907
695769                 XDOT =       -5458
265670
 YDOT =      -1537
142776  feet/sec       YDOT =        -468
521118  meter/sec
 ZDOT =     -16172
344508                 ZDOT =       -4929
330606


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   19054
28741688  
00016717  00000-0  10270-3 0  9088
2 25544  51
6409 207
5749 0005854  53
6604 306
5088 15
53291739 37552


Satellite: ISS
Catalog Number: 25544
Epoch time:      19054
28741688   =   yrday
fracday
Element set:     908
Inclination:       51
6409  deg
RA of node:       207
5749  deg
Eccentricity:     
0005854     
Arg of perigee:    53
6604  deg
Mean anomaly:     306
5088  deg
Mean motion:   15
53291739  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3755
Checksum:              344


Coasting Arc #10 (Orbit 3755)
---------------------------------------

Vector Time (GMT): 2019/054/08:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2187742
34                 A    =         6779792
67  meter
 Y    =        3635524
04  meter          E    =           
0019572
 Z    =       -5304623
08                 I    =           51
44557
 XDOT =      -6746
283246                 Wp   =           81
89743
 YDOT =      -3598
988005  meter/sec      RA   =          206
17070  deg
 ZDOT =        319
460680                 TA   =          191
14073
                                          MA   =          191
18413
                                          Ha   =            224
187  n
mi
                                          Hp   =            214
100

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7177632
36                 X    =        -2202466
66
 Y    =       11927572
31  feet           Y    =         3610976
30  meter
 Z    =      -17403619
04                 Z    =        -5315286
30
 XDOT =     -22133
475215                 XDOT =       -6707
088690
 YDOT =     -11807
703430  feet/sec       YDOT =       -3674
210475  meter/sec
 ZDOT =       1048
099343                 ZDOT =         286
785810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12284648
49                 X    =        -3744360
86
 Y    =       -6417534
58  feet           Y    =        -1956064
54  meter
 Z    =      -17452048
73                 Z    =        -5319384
45
 XDOT =      10146
871313                 XDOT =        3092
766376
 YDOT =     -21840
166635  feet/sec       YDOT =       -6656
882790  meter/sec
 ZDOT =        900
827617                 ZDOT =         274
572258


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   19054
35175202  
00016717  00000-0  10270-3 0  9090
2 25544  51
6388 207
2523 0005703  52
7714 307
3958 15
53302404 37568


Satellite: ISS
Catalog Number: 25544
Epoch time:      19054
35175202   =   yrday
fracday
Element set:     909
Inclination:       51
6388  deg
RA of node:       207
2523  deg
Eccentricity:     
0005703     
Arg of perigee:    52
7714  deg
Mean anomaly:     307
3958  deg
Mean motion:   15
53302404  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3756
Checksum:              302


Coasting Arc #11 (Orbit 3771)
---------------------------------------

Vector Time (GMT): 2019/055/08:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3474262
64                 A    =         6780937
90  meter
 Y    =       -2939992
35  meter          E    =           
0011333
 Z    =        5020277
26                 I    =           51
47983
 XDOT =       6223
785628                 Wp   =           56
51348
 YDOT =       4052
805989  meter/sec      RA   =          201
16820  deg
 ZDOT =      -1924
455232                 TA   =           52
23684
                                          MA   =           52
13422
                                          Ha   =            224
127  n
mi
                                          Hp   =            214
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11398499
48                 X    =         3482494
82
 Y    =       -9645644
20  feet           Y    =        -2901094
26  meter
 Z    =       16470725
93                 Z    =         5037173
97
 XDOT =      20419
244185                 XDOT =        6187
351268
 YDOT =      13296
607574  feet/sec       YDOT =        4122
200824  meter/sec
 ZDOT =      -6313
829500                 ZDOT =       -1894
311620

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10414120
15                 X    =         3174223
82
 Y    =       10582223
86  feet           Y    =         3225461
83  meter
 Z    =       16547256
40                 Z    =         5043603
75
 XDOT =     -11053
399128                 XDOT =       -3369
076054
 YDOT =      20585
608138  feet/sec       YDOT =        6274
493361  meter/sec
 ZDOT =      -6178
005665                 ZDOT =       -1883
056127


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   19055
38114000  
00016717  00000-0  10270-3 0  9105
2 25544  51
6388 202
1271 0005714  56
5132 303
6566 15
53299900 37728


Satellite: ISS
Catalog Number: 25544
Epoch time:      19055
38114000   =   yrday
fracday
Element set:     910
Inclination:       51
6388  deg
RA of node:       202
1271  deg
Eccentricity:     
0005714     
Arg of perigee:    56
5132  deg
Mean anomaly:     303
6566  deg
Mean motion:   15
53299900  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3772
Checksum:              287


Coasting Arc #12 (Orbit 3786)
---------------------------------------

Vector Time (GMT): 2019/056/08:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4634606
77                 A    =         6783438
70  meter
 Y    =        2297878
25  meter          E    =           
0013559
 Z    =       -4400144
21                 I    =           51
51784
 XDOT =      -5338
129656                 Wp   =           92
32566
 YDOT =      -4334
992607  meter/sec      RA   =          196
17210  deg
 ZDOT =       3367
175114                 TA   =          211
81266
                                          MA   =          211
89463
                                          Ha   =            224
242  n
mi
                                          Hp   =            213
956

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15205402
78                 X    =        -4638584
62
 Y    =        7538970
64  feet           Y    =         2246028
30  meter
 Z    =      -14436168
67                 Z    =        -4422666
96
 XDOT =     -17513
548739                 XDOT =       -5305
613488
 YDOT =     -14222
416691  feet/sec       YDOT =       -4394
505262  meter/sec
 ZDOT =      11047
162447                 ZDOT =        3341
324047

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8830194
75                 X    =        -2691443
36
 Y    =      -14391508
45  feet           Y    =        -4386531
78  meter
 Z    =      -14538069
44                 Z    =        -4431203
57
 XDOT =      11579
949507                 XDOT =        3529
568610
 YDOT =     -18119
323533  feet/sec       YDOT =       -5522
769813  meter/sec
 ZDOT =      10930
729747                 ZDOT =        3331
686427


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   19056
34619044  
00016717  00000-0  10270-3 0  9111
2 25544  51
6370 197
3220 0005708  61
0004 299
1720 15
53299907 37874


Satellite: ISS
Catalog Number: 25544
Epoch time:      19056
34619044   =   yrday
fracday
Element set:     911
Inclination:       51
6370  deg
RA of node:       197
3220  deg
Eccentricity:     
0005708     
Arg of perigee:    61
0004  deg
Mean anomaly:     299
1720  deg
Mean motion:   15
53299907  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3787
Checksum:              309


Coasting Arc #13 (Orbit 3798)
---------------------------------------

Vector Time (GMT): 2019/057/02:28:46
144
Vector Time (MET): N/A
Weight (LBS)     : 900432
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1721238
25                 A    =         6781587
21  meter
 Y    =        3915401
64  meter          E    =           
0017418
 Z    =       -5277785
72                 I    =           51
53306
 XDOT =      -7291
081160                 Wp   =           87
59243
 YDOT =      -2204
577263  meter/sec      RA   =          192
36570  deg
 ZDOT =        745
181589                 TA   =          189
53448
                                          MA   =          189
56759
                                          Ha   =            224
353  n
mi
                                          Hp   =            215
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5647107
12                 X    =        -1739257
20
 Y    =       12845805
89  feet           Y    =         3896052
50  meter
 Z    =      -17315569
95                 Z    =        -5286190
74
 XDOT =     -23920
869947                 XDOT =       -7269
506704
 YDOT =      -7232
865035  feet/sec       YDOT =       -2285
990552  meter/sec
 ZDOT =       2444
821485                 ZDOT =         709
817199

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2748166
83                 X    =          837641
25
 Y    =      -13712243
88  feet           Y    =        -4179491
93  meter
 Z    =      -17353831
20                 Z    =        -5289447
75
 XDOT =      23916
172371                 XDOT =        7289
649339
 YDOT =       1912
863835  feet/sec       YDOT =         583
040897  meter/sec
 ZDOT =       2285
242858                 ZDOT =         696
542023


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   19057
11823249  
00016717  00000-0  10270-3 0  9122
2 25544  51
6393 193
4790 0003629  51
8036 308
3442 15
52732656 37999


Satellite: ISS
Catalog Number: 25544
Epoch time:      19057
11823249   =   yrday
fracday
Element set:     912
Inclination:       51
6393  deg
RA of node:       193
4790  deg
Eccentricity:     
0003629     
Arg of perigee:    51
8036  deg
Mean anomaly:     308
3442  deg
Mean motion:   15
52732656  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3799
Checksum:              325


Coasting Arc #14 (Orbit 3806)
---------------------------------------

Vector Time (GMT): 2019/057/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900432
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2331709
82                 A    =         6782049
72  meter
 Y    =        3754148
97  meter          E    =           
0016407
 Z    =       -5158883
83                 I    =           51
55228
 XDOT =      -7115
574215                 Wp   =           93
37746
 YDOT =      -2408
806345  meter/sec      RA   =          189
78738  deg
 ZDOT =       1466
284977                 TA   =          190
76362
                                          MA   =          190
79878
                                          Ha   =            224
269  n
mi
                                          Hp   =            215
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7649966
61                 X    =        -2348457
81
 Y    =       12316761
71  feet           Y    =         3727980
26  meter
 Z    =      -16925471
87                 Z    =        -5170251
12
 XDOT =     -23345
059760                 XDOT =       -7095
231728
 YDOT =      -7902
907957  feet/sec       YDOT =       -2488
263849  meter/sec
 ZDOT =       4810
646249                 ZDOT =        1431
770159

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3293017
80                 X    =        -1003711
83
 Y    =       14058098
74  feet           Y    =         4284908
50  meter
 Z    =      -16977105
17                 Z    =        -5174621
65
 XDOT =     -23650
618539                 XDOT =       -7208
708531
 YDOT =         69
227468  feet/sec       YDOT =          21
100532  meter/sec
 ZDOT =       4654
908943                 ZDOT =        1418
816246


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   19057
63311043  
00016717  00000-0  10270-3 0  9134
2 25544  51
6400 190
9155 0003318  58
0296 302
1178 15
52746926 38070


Satellite: ISS
Catalog Number: 25544
Epoch time:      19057
63311043   =   yrday
fracday
Element set:     913
Inclination:       51
6400  deg
RA of node:       190
9155  deg
Eccentricity:     
0003318     
Arg of perigee:    58
0296  deg
Mean anomaly:     302
1178  deg
Mean motion:   15
52746926  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3807
Checksum:              298


Coasting Arc #15 (Orbit 3822)
---------------------------------------

Vector Time (GMT): 2019/058/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900432
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3466165
03                 A    =         6783837
72  meter
 Y    =       -3446549
05  meter          E    =           
0011196
 Z    =        4697769
45                 I    =           51
59188
 XDOT =       6576
333849                 Wp   =           62
32983
 YDOT =       2781
182320  meter/sec      RA   =          184
79979  deg
 ZDOT =      -2801
590421                 TA   =           55
50591
                                          MA   =           55
40022
                                          Ha   =            224
183  n
mi
                                          Hp   =            215
704

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11371932
51                 X    =         3481628
90
 Y    =      -11307575
61  feet           Y    =        -3407701
30  meter
 Z    =       15412629
44                 Z    =         4714644
23
 XDOT =      21575
898455                 XDOT =        6558
353482
 YDOT =       9124
613911  feet/sec       YDOT =        2854
622821  meter/sec
 ZDOT =      -9191
569622                 ZDOT =       -2769
689340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6906655
24                 X    =         2105148
52
 Y    =      -14391533
48  feet           Y    =        -4386539
40  meter
 Z    =       15489129
71                 Z    =         4721086
73
 XDOT =      22386
248252                 XDOT =        6823
328467
 YDOT =        969
861741  feet/sec       YDOT =         295
613859  meter/sec
 ZDOT =      -9047
645728                 ZDOT =       -2757
722418


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   19058
66286628  
00016717  00000-0  10270-3 0  9149
2 25544  51
6404 185
7923 0003382  59
6160 300
5326 15
52767376 38234


Satellite: ISS
Catalog Number: 25544
Epoch time:      19058
66286628   =   yrday
fracday
Element set:     914
Inclination:       51
6404  deg
RA of node:       185
7923  deg
Eccentricity:     
0003382     
Arg of perigee:    59
6160  deg
Mean anomaly:     300
5326  deg
Mean motion:   15
52767376  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3823
Checksum:              327


Coasting Arc #16 (Orbit 3837)
---------------------------------------

Vector Time (GMT): 2019/059/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900432
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4466316
42                 A    =         6786414
17  meter
 Y    =        3184551
88  meter          E    =           
0009868
 Z    =       -4004905
01                 I    =           51
63246
 XDOT =      -5766
128256                 Wp   =           94
87041
 YDOT =      -3116
756401  meter/sec      RA   =          179
82065  deg
 ZDOT =       3959
727503                 TA   =          216
35843
                                          MA   =          216
42551
                                          Ha   =            224
304  n
mi
                                          Hp   =            215
556

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14653269
08                 X    =        -4482141
78
 Y    =       10448004
85  feet           Y    =         3134517
75  meter
 Z    =      -13139452
12                 Z    =        -4026638
88
 XDOT =     -18917
743623                 XDOT =       -5750
081066
 YDOT =     -10225
578743  feet/sec       YDOT =       -3181
147376  meter/sec
 ZDOT =      12991
231966                 ZDOT =        3931
757436

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10048240
38                 X    =        -3062703
67
 Y    =       14843017
07  feet           Y    =         4524151
60  meter
 Z    =      -13237900
57                 Z    =        -4034912
09
 XDOT =     -20286
309627                 XDOT =       -6183
267174
 YDOT =      -2281
404499  feet/sec       YDOT =        -695
372091  meter/sec
 ZDOT =      12865
073864                 ZDOT =        3921
274514


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   19059
62826191  
00016717  00000-0  10270-3 0  9152
2 25544  51
6391 180
9910 0003431  65
3715 294
7794 15
52764615 38389


Satellite: ISS
Catalog Number: 25544
Epoch time:      19059
62826191   =   yrday
fracday
Element set:     915
Inclination:       51
6391  deg
RA of node:       180
9910  deg
Eccentricity:     
0003431     
Arg of perigee:    65
3715  deg
Mean anomaly:     294
7794  deg
Mean motion:   15
52764615  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3838
Checksum:              335


Coasting Arc #17 (Orbit 3853)
---------------------------------------

Vector Time (GMT): 2019/060/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900432
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5319066
38                 A    =         6789259
75  meter
 Y    =       -2900402
33  meter          E    =           
0016079
 Z    =        3050267
62                 I    =           51
67570
 XDOT =       4736
262365                 Wp   =           90
01163
 YDOT =       3482
160395  meter/sec      RA   =          174
84816  deg
 ZDOT =      -4925
587364                 TA   =           55
01375
                                          MA   =           54
86289
                                          Ha   =            224
269  n
mi
                                          Hp   =            215
608

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17451005
18                 X    =         5336287
98
 Y    =       -9515755
69  feet           Y    =        -2840824
37  meter
 Z    =       10007439
69                 Z    =         3076147
08
 XDOT =      15538
918520                 XDOT =        4720
897127
 YDOT =      11424
410746  feet/sec       YDOT =        3535
038433  meter/sec
 ZDOT =     -16160
063530                 ZDOT =       -4902
618349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12756251
00                 X    =         3888105
30
 Y    =      -15165956
51  feet           Y    =        -4622583
54  meter
 Z    =       10124616
58                 Z    =         3085983
13
 XDOT =      17616
125432                 XDOT =        5369
395032
 YDOT =       4049
377242  feet/sec       YDOT =        1234
250183  meter/sec
 ZDOT =     -16056
514573                 ZDOT =       -4894
025642


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   19060
65801361  
00016717  00000-0  10270-3 0  9160
2 25544  51
6396 175
8681 0003428  66
2531 293
8980 15
52766996 38543


Satellite: ISS
Catalog Number: 25544
Epoch time:      19060
65801361   =   yrday
fracday
Element set:     916
Inclination:       51
6396  deg
RA of node:       175
8681  deg
Eccentricity:     
0003428     
Arg of perigee:    66
2531  deg
Mean anomaly:     293
8980  deg
Mean motion:   15
52766996  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3854
Checksum:              347


Coasting Arc #18 (Orbit 3855)
---------------------------------------

Vector Time (GMT): 2019/060/17:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900432
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6113669
44                 A    =         6790727
20  meter
 Y    =       -1431852
94  meter          E    =           
0017522
 Z    =        2563818
09                 I    =           51
68250
 XDOT =       3276
730168                 Wp   =           74
14685
 YDOT =      -4508
871022  meter/sec      RA   =          174
35716  deg
 ZDOT =       5270
279361                 TA   =          314
65609
                                          MA   =          314
79879
                                          Ha   =            224
631  n
mi
                                          Hp   =            215
583

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20057970
61                 X    =        -6109657
02
 Y    =       -4697680
25  feet           Y    =        -1500197
70  meter
 Z    =        8411476
66                 Z    =         2534130
62
 XDOT =      10750
427060                 XDOT =        3301
306556
 YDOT =     -14792
883932  feet/sec       YDOT =       -4472
090655  meter/sec
 ZDOT =      17290
942787                 ZDOT =        5286
256070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14066891
75                 X    =        -4287588
60
 Y    =       15124495
82  feet           Y    =         4609946
33  meter
 Z    =        8277409
44                 Z    =         2522954
40
 XDOT =      -6453
400057                 XDOT =       -1966
996337
 YDOT =     -15551
004572  feet/sec       YDOT =       -4739
946193  meter/sec
 ZDOT =      17363
484924                 ZDOT =        5292
390205


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   19060
78673426  
00016717  00000-0  10270-3 0  9174
2 25544  51
6387 175
2283 0003887  66
6891 293
4670 15
52722957 38560


Satellite: ISS
Catalog Number: 25544
Epoch time:      19060
78673426   =   yrday
fracday
Element set:     917
Inclination:       51
6387  deg
RA of node:       175
2283  deg
Eccentricity:     
0003887     
Arg of perigee:    66
6891  deg
Mean anomaly:     293
4670  deg
Mean motion:   15
52722957  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3856
Checksum:              358
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