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

 
Date: February 14th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 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 0 -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

Coasting Arc #1 (Orbit 3602)
---------------------------------------

Vector Time (GMT): 2019/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4127272
78                 A    =         6785782
70  meter
 Y    =       -3863081
47  meter          E    =           
0008598
 Z    =       -3756805
05                 I    =           51
26700
 XDOT =       1893
840522                 Wp   =           62
88375
 YDOT =      -6111
742936  meter/sec      RA   =          255
31715  deg
 ZDOT =       4215
359859                 TA   =          251
91974
                                          MA   =          252
01342
                                          Ha   =            223
637  n
mi
                                          Hp   =            215
034

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13540921
20                 X    =        -4065519
71
 Y    =      -12674151
80  feet           Y    =        -3908890
30  meter
 Z    =      -12325475
88                 Z    =        -3776703
50
 XDOT =       6213
387541                 XDOT =        1941
567365
 YDOT =     -20051
650054  feet/sec       YDOT =       -6090
297757  meter/sec
 ZDOT =      13829
920796                 ZDOT =        4224
675346

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2913432
76                 X    =         -888014
31
 Y    =      -18256264
73  feet           Y    =        -5564509
49  meter
 Z    =      -12414859
41                 Z    =        -3784049
15
 XDOT =      15762
476552                 XDOT =        4804
402853
 YDOT =     -11924
180120  feet/sec       YDOT =       -3634
490101  meter/sec
 ZDOT =      13872
550396                 ZDOT =        4228
353361


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   19044
50810224  
00016717  00000-0  10270-3 0  9007
2 25544  51
6390 256
2621 0005598  18
8550 341
2809 15
53262466 36033


Satellite: ISS
Catalog Number: 25544
Epoch time:      19044
50810224   =   yrday
fracday
Element set:     900
Inclination:       51
6390  deg
RA of node:       256
2621  deg
Eccentricity:     
0005598     
Arg of perigee:    18
8550  deg
Mean anomaly:     341
2809  deg
Mean motion:   15
53262466  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3603
Checksum:              294


Coasting Arc #2 (Orbit 3618)
---------------------------------------

Vector Time (GMT): 2019/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3954906
79                 A    =         6788818
52  meter
 Y    =        4859602
85  meter          E    =           
0015596
 Z    =        2603763
38                 I    =           51
28641
 XDOT =      -2654
574651                 Wp   =           81
43251
 YDOT =       4964
519570  meter/sec      RA   =          250
31690  deg
 ZDOT =      -5204
484650                 TA   =           69
10782
                                          MA   =           68
94092
                                          Ha   =            223
742  n
mi
                                          Hp   =            214
886

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12975415
99                 X    =         3887623
95
 Y    =       15943578
89  feet           Y    =         4903453
18  meter
 Z    =        8542530
78                 Z    =         2622811
15
 XDOT =      -8709
234419                 XDOT =       -2684
611868
 YDOT =      16287
793865  feet/sec       YDOT =        4934
666305  meter/sec
 ZDOT =     -17075
080872                 ZDOT =       -5217
452365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         841628
66                 X    =          256528
42
 Y    =       20503251
84  feet           Y    =         6249391
16  meter
 Z    =        8627994
29                 Z    =         2629812
66
 XDOT =     -15124
315636                 XDOT =       -4609
891406
 YDOT =       7870
804230  feet/sec       YDOT =        2399
021129  meter/sec
 ZDOT =     -17134
068009                 ZDOT =       -5222
463929


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   19045
53751312  
00016717  00000-0  10270-3 0  9014
2 25544  51
6384 251
1371 0005778  22
1209 338
0192 15
53298164 36191


Satellite: ISS
Catalog Number: 25544
Epoch time:      19045
53751312   =   yrday
fracday
Element set:     901
Inclination:       51
6384  deg
RA of node:       251
1371  deg
Eccentricity:     
0005778     
Arg of perigee:    22
1209  deg
Mean anomaly:     338
0192  deg
Mean motion:   15
53298164  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3619
Checksum:              299


Coasting Arc #3 (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    =       -3695039
79                 A    =         6791121
27  meter
 Y    =       -5538476
24  meter          E    =           
0014269
 Z    =       -1304907
18                 I    =           51
30436
 XDOT =       3437
508203                 Wp   =           33
51031
 YDOT =      -3650
472339  meter/sec      RA   =          245
32298  deg
 ZDOT =       5802
134908                 TA   =          312
22330
                                          MA   =          312
34429
                                          Ha   =            223
783  n
mi
                                          Hp   =            214
911

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12122833
97                 X    =        -3626493
96
 Y    =      -18170853
80  feet           Y    =        -5579413
48  meter
 Z    =       -4281191
52                 Z    =        -1322689
55
 XDOT =      11277
914053                 XDOT =        3449
890275
 YDOT =     -11976
615287  feet/sec       YDOT =       -3611
962542  meter/sec
 ZDOT =      19035
875684                 ZDOT =        5818
862787

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         774056
07                 X    =          235932
29
 Y    =      -21814101
43  feet           Y    =        -6648938
12  meter
 Z    =       -4360899
92                 Z    =        -1329202
29
 XDOT =      14451
170353                 XDOT =        4404
716724
 YDOT =      -3280
768130  feet/sec       YDOT =        -999
978126  meter/sec
 ZDOT =      19111
699482                 ZDOT =        5825
246002


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
50258738  
00016717  00000-0  10270-3 0  9027
2 25544  51
6369 246
3322 0005539  26
3211 333
8221 15
53254151 36341


Satellite: ISS
Catalog Number: 25544
Epoch time:      19046
50258738   =   yrday
fracday
Element set:     902
Inclination:       51
6369  deg
RA of node:       246
3322  deg
Eccentricity:     
0005539     
Arg of perigee:    26
3211  deg
Mean anomaly:     333
8221  deg
Mean motion:   15
53254151  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3634
Checksum:              292


Coasting Arc #4 (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    =        3264356
96                 A    =         6791780
82  meter
 Y    =        5951758
75  meter          E    =           
0011687
 Z    =        -136598
87                 I    =           51
32186
 XDOT =      -4253
651715                 Wp   =          107
66386
 YDOT =       2205
542280  meter/sec      RA   =          240
33357  deg
 ZDOT =      -5980
728311                 TA   =           73
81290
                                          MA   =           73
68432
                                          Ha   =            223
910  n
mi
                                          Hp   =            214
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10709832
54                 X    =         3198223
61
 Y    =       19526767
56  feet           Y    =         5987893
30  meter
 Z    =        -448159
03                 Z    =         -120902
77
 XDOT =     -13955
550246                 XDOT =       -4248
948162
 YDOT =       7236
031101  feet/sec       YDOT =        2158
001331  meter/sec
 ZDOT =     -19621
812045                 ZDOT =       -6001
379056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2306037
88                 X    =         -702880
34
 Y    =       22152548
53  feet           Y    =         6752096
79  meter
 Z    =        -377880
83                 Z    =         -115178
08
 XDOT =     -13868
734957                 XDOT =       -4227
190415
 YDOT =      -1751
646882  feet/sec       YDOT =        -533
901969  meter/sec
 ZDOT =     -19715
204205                 ZDOT =       -6009
194242


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
53199663  
00016717  00000-0  10270-3 0  9033
2 25544  51
6370 241
2065 0005703  29
6993 330
4482 15
53282107 36509


Satellite: ISS
Catalog Number: 25544
Epoch time:      19047
53199663   =   yrday
fracday
Element set:     903
Inclination:       51
6370  deg
RA of node:       241
2065  deg
Eccentricity:     
0005703     
Arg of perigee:    29
6993  deg
Mean anomaly:     330
4482  deg
Mean motion:   15
53282107  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3650
Checksum:              306


Coasting Arc #5 (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    =       -2690428
72                 A    =         6790909
77  meter
 Y    =       -6034868
77  meter          E    =           
0019051
 Z    =        1522961
41                 I    =           51
33456
 XDOT =       5035
268937                 Wp   =           54
44512
 YDOT =       -787
261094  meter/sec      RA   =          235
34405  deg
 ZDOT =       5735
835226                 TA   =          322
27252
                                          MA   =          322
40595
                                          Ha   =            223
984  n
mi
                                          Hp   =            214
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8826865
87                 X    =        -2630142
66
 Y    =      -19799438
23  feet           Y    =        -6064617
94  meter
 Z    =        4996592
56                 Z    =         1510039
12
 XDOT =      16519
911211                 XDOT =        5015
837337
 YDOT =      -2582
877606  feet/sec       YDOT =        -731
061828  meter/sec
 ZDOT =      18818
357040                 ZDOT =        5760
246822

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3616858
56                 X    =         1102418
49
 Y    =      -21387465
65  feet           Y    =        -6518899
53  meter
 Z    =        4938815
65                 Z    =         1505351
01
 XDOT =      13510
710780                 XDOT =        4118
064646
 YDOT =       6686
301729  feet/sec       YDOT =        2037
984767  meter/sec
 ZDOT =      18928
600133                 ZDOT =        5769
437321


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
56140485  
00016717  00000-0  10270-3 0  9046
2 25544  51
6355 236
0803 0005613  35
0450 325
1070 15
53257373 36661


Satellite: ISS
Catalog Number: 25544
Epoch time:      19048
56140485   =   yrday
fracday
Element set:     904
Inclination:       51
6355  deg
RA of node:       236
0803  deg
Eccentricity:     
0005613     
Arg of perigee:    35
0450  deg
Mean anomaly:     325
1070  deg
Mean motion:   15
53257373  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3666
Checksum:              291


Coasting Arc #6 (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    =        1907684
53                 A    =         6788400
20  meter
 Y    =        5866337
21  meter          E    =           
0008023
 Z    =       -2843263
97                 I    =           51
34562
 XDOT =      -5727
424556                 Wp   =           74
40902
 YDOT =       -580
571989  meter/sec      RA   =          230
35283  deg
 ZDOT =      -5050
495125                 TA   =          138
00400
                                          MA   =          137
94246
                                          Ha   =            224
069  n
mi
                                          Hp   =            214
519

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6258807
53                 X    =         1855754
29
 Y    =       19246513
15  feet           Y    =         5887379
82  meter
 Z    =       -9328293
86                 Z    =        -2834123
74
 XDOT =     -18790
762979                 XDOT =       -5695
975012
 YDOT =      -1904
763744  feet/sec       YDOT =        -644
444355  meter/sec
 ZDOT =     -16569
865895                 ZDOT =       -5078
239559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5085489
00                 X    =        -1550057
05
 Y    =       19608601
38  feet           Y    =         5976701
70  meter
 Z    =       -9287548
65                 Z    =        -2830844
83
 XDOT =     -13255
109196                 XDOT =       -4040
157283
 YDOT =     -11329
925564  feet/sec       YDOT =       -3453
361312  meter/sec
 ZDOT =     -16695
043745                 ZDOT =       -5088
649333


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
52647352  
00016717  00000-0  10270-3 0  9059
2 25544  51
6349 231
2753 0005728  39
1994 320
9572 15
53280838 36819


Satellite: ISS
Catalog Number: 25544
Epoch time:      19049
52647352   =   yrday
fracday
Element set:     905
Inclination:       51
6349  deg
RA of node:       231
2753  deg
Eccentricity:     
0005728     
Arg of perigee:    39
1994  deg
Mean anomaly:     320
9572  deg
Mean motion:   15
53280838  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3681
Checksum:              332


Coasting Arc #7 (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    =        2497785
08                 A    =         6779949
98  meter
 Y    =       -3475039
72  meter          E    =           
0007034
 Z    =        5252714
55                 I    =           51
33770
 XDOT =       5650
652130                 Wp   =           66
31627
 YDOT =       5140
796365  meter/sec      RA   =          226
59554  deg
 ZDOT =        715
998949                 TA   =           16
83162
                                          MA   =           16
80829
                                          Ha   =            223
929  n
mi
                                          Hp   =            214
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8194832
94                 X    =         2510944
34
 Y    =      -11401048
94  feet           Y    =        -3447033
88  meter
 Z    =       17233315
46                 Z    =         5264879
63
 XDOT =      18538
884942                 XDOT =        5589
268513
 YDOT =      16866
129805  feet/sec       YDOT =        5203
642724  meter/sec
 ZDOT =       2349
077917                 ZDOT =         743
297483

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5305496
35                 X    =         1617115
29
 Y    =       12926137
64  feet           Y    =         3939886
75  meter
 Z    =       17288523
36                 Z    =         5269541
92
 XDOT =     -23218
270357                 XDOT =       -7076
928805
 YDOT =       6232
596689  feet/sec       YDOT =        1899
695471  meter/sec
 ZDOT =       2471
867583                 ZDOT =         753
425239


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
29852790  
00016717  00000-0  10270-3 0  9060
2 25544  51
6387 227
4348 0005670  40
2648 319
8923 15
53297592 36938


Satellite: ISS
Catalog Number: 25544
Epoch time:      19050
29852790   =   yrday
fracday
Element set:     906
Inclination:       51
6387  deg
RA of node:       227
4348  deg
Eccentricity:     
0005670     
Arg of perigee:    40
2648  deg
Mean anomaly:     319
8923  deg
Mean motion:   15
53297592  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3693
Checksum:              342


Coasting Arc #8 (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    =       -3539746
24                 A    =         6780066
94  meter
 Y    =        2465646
05  meter          E    =           
0018563
 Z    =       -5246351
74                 I    =           51
36299
 XDOT =      -5186
843882                 Wp   =           82
48012
 YDOT =      -5556
961114  meter/sec      RA   =          221
58429  deg
 ZDOT =        893
076107                 TA   =          196
08141
                                          MA   =          196
14041
                                          Ha   =            224
138  n
mi
                                          Hp   =            214
237

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11613340
69                 X    =        -3541571
59
 Y    =        8089389
94  feet           Y    =         2426051
49  meter
 Z    =      -17212440
08                 Z    =        -5263550
64
 XDOT =     -17017
204338                 XDOT =       -5128
656823
 YDOT =     -18231
499717  feet/sec       YDOT =       -5614
638605  meter/sec
 ZDOT =       2930
039720                 ZDOT =         868
022889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -919857
20                 X    =         -280372
47
 Y    =      -14027683
12  feet           Y    =        -4275637
81  meter
 Z    =      -17290285
54                 Z    =        -5270079
03
 XDOT =      23412
160021                 XDOT =        7136
026375
 YDOT =      -4987
363020  feet/sec       YDOT =       -1520
148248  meter/sec
 ZDOT =       2817
394541                 ZDOT =         858
741856


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
26359443  
00016717  00000-0  10270-3 0  9076
2 25544  51
6400 222
6298 0005810  43
5462 316
6148 15
53282460 37080


Satellite: ISS
Catalog Number: 25544
Epoch time:      19051
26359443   =   yrday
fracday
Element set:     907
Inclination:       51
6400  deg
RA of node:       222
6298  deg
Eccentricity:     
0005810     
Arg of perigee:    43
5462  deg
Mean anomaly:     316
6148  deg
Mean motion:   15
53282460  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3708
Checksum:              300


Coasting Arc #9 (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    =        4532917
88                 A    =         6781681
06  meter
 Y    =       -1437663
74  meter          E    =           
0012746
 Z    =        4828983
36                 I    =           51
39432
 XDOT =       4451
228998                 Wp   =           53
78630
 YDOT =       5744
966918  meter/sec      RA   =          216
57715  deg
 ZDOT =      -2456
024738                 TA   =           60
46242
                                          MA   =           60
33540
                                          Ha   =            224
026  n
mi
                                          Hp   =            214
253

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14871777
84                 X    =         4525201
41
 Y    =       -4716744
57  feet           Y    =        -1387016
13  meter
 Z    =       15843121
25                 Z    =         4850983
44
 XDOT =      14603
769679                 XDOT =        4398
586046
 YDOT =      18848
316661  feet/sec       YDOT =        5794
449066  meter/sec
 ZDOT =      -8057
823942                 ZDOT =       -2434
531332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3401078
34                 X    =        -1036648
68
 Y    =       15122477
64  feet           Y    =         4609331
18  meter
 Z    =       15942561
99                 Z    =         4859292
89
 XDOT =     -22570
120293                 XDOT =       -6879
372665
 YDOT =       3357
922222  feet/sec       YDOT =        1023
494693  meter/sec
 ZDOT =      -7961
242981                 ZDOT =       -2426
586861


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
29299540  
00016717  00000-0  10270-3 0  9082
2 25544  51
6399 217
5047 0005858  46
1905 313
9731 15
53312609 37240


Satellite: ISS
Catalog Number: 25544
Epoch time:      19052
29299540   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:       217
5047  deg
Eccentricity:     
0005858     
Arg of perigee:    46
1905  deg
Mean anomaly:     313
9731  deg
Mean motion:   15
53312609  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3724
Checksum:              326


Coasting Arc #10 (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    =       -5391879
19                 A    =         6784599
05  meter
 Y    =         518127
77  meter          E    =           
0011585
 Z    =       -4094470
44                 I    =           51
43146
 XDOT =      -3435
490049                 Wp   =           84
03407
 YDOT =      -5682
888066  meter/sec      RA   =          211
57774  deg
 ZDOT =       3815
460670                 TA   =          225
50037
                                          MA   =          225
59512
                                          Ha   =            224
179  n
mi
                                          Hp   =            214
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17689892
35                 X    =        -5377384
03
 Y    =        1699894
25  feet           Y    =          457912
60  meter
 Z    =      -13433301
97                 Z    =        -4120626
51
 XDOT =     -11271
292813                 XDOT =       -3390
220092
 YDOT =     -18644
645886  feet/sec       YDOT =       -5721
052570  meter/sec
 ZDOT =      12517
915583                 ZDOT =        3798
883255

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7159955
46                 X    =         2182354
42
 Y    =      -16166910
57  feet           Y    =        -4927674
34  meter
 Z    =      -13551441
78                 Z    =        -4130479
45
 XDOT =      20637
945840                 XDOT =        6290
445892
 YDOT =      -1261
700133  feet/sec       YDOT =        -384
566201  meter/sec
 ZDOT =      12443
508145                 ZDOT =        3792
781283


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
25806003  
00016717  00000-0  10270-3 0  9098
2 25544  51
6403 212
7003 0005784  49
4435 310
7220 15
53273119 37393


Satellite: ISS
Catalog Number: 25544
Epoch time:      19053
25806003   =   yrday
fracday
Element set:     909
Inclination:       51
6403  deg
RA of node:       212
7003  deg
Eccentricity:     
0005784     
Arg of perigee:    49
4435  deg
Mean anomaly:     310
7220  deg
Mean motion:   15
53273119  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3739
Checksum:              285


Coasting Arc #11 (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    =        6063470
85                 A    =         6787837
60  meter
 Y    =         347151
32  meter          E    =           
0017839
 Z    =        3018369
67                 I    =           51
47188
 XDOT =       2154
120521                 Wp   =           83
57255
 YDOT =       5466
882815  meter/sec      RA   =          206
58738  deg
 ZDOT =      -4929
021796                 TA   =           61
75406
                                          MA   =           61
57409
                                          Ha   =            224
230  n
mi
                                          Hp   =            214
122

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19893277
08                 X    =         6044476
92
 Y    =        1138947
90  feet           Y    =          414851
40  meter
 Z    =        9902787
64                 Z    =         3047777
13
 XDOT =       7067
324544                 XDOT =        2116
770292
 YDOT =      17935
967242  feet/sec       YDOT =        5490
762346  meter/sec
 ZDOT =     -16171
331351                 ZDOT =       -4918
649326

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10437136
05                 X    =        -3181239
07
 Y    =       16895524
43  feet           Y    =         5149755
84  meter
 Z    =       10035552
99                 Z    =         3058836
55
 XDOT =     -17956
496326                 XDOT =       -5473
140080
 YDOT =      -1462
686831  feet/sec       YDOT =        -445
826946  meter/sec
 ZDOT =     -16124
912775                 ZDOT =       -4914
873414


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
28746006  
00016717  00000-0  10270-3 0  9100
2 25544  51
6409 207
5755 0005879  53
7245 306
4450 15
53279545 37551


Satellite: ISS
Catalog Number: 25544
Epoch time:      19054
28746006   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:       207
5755  deg
Eccentricity:     
0005879     
Arg of perigee:    53
7245  deg
Mean anomaly:     306
4450  deg
Mean motion:   15
53279545  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3755
Checksum:              325


Coasting Arc #12 (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    =       -2162392
04                 A    =         6779825
60  meter
 Y    =        3649035
25  meter          E    =           
0019614
 Z    =       -5305823
62                 I    =           51
44560
 XDOT =      -6756
582593                 Wp   =           81
74332
 YDOT =      -3581
672768  meter/sec      RA   =          206
17182  deg
 ZDOT =        294
075628                 TA   =          191
05164
                                          MA   =          191
09479
                                          Ha   =            224
217  n
mi
                                          Hp   =            214
112

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7094462
08                 X    =        -2177263
50
 Y    =       11971900
42  feet           Y    =         3624770
17  meter
 Z    =      -17407557
80                 Z    =        -5316364
05
 XDOT =     -22167
265724                 XDOT =       -6717
457591
 YDOT =     -11750
894908  feet/sec       YDOT =       -3657
010804  meter/sec
 ZDOT =        964
815052                 ZDOT =         261
350558

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12324494
29                 X    =        -3756505
86
 Y    =       -6332102
49  feet           Y    =        -1930024
84  meter
 Z    =      -17455434
08                 Z    =        -5320416
31
 XDOT =      10094
613070                 XDOT =        3076
838064
 YDOT =     -21867
429290  feet/sec       YDOT =       -6665
192447  meter/sec
 ZDOT =        817
315316                 ZDOT =         249
117708


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
35179574  
00016717  00000-0  10270-3 0  9119
2 25544  51
6389 207
2529 0005728  52
8646 307
3029 15
53289613 37562


Satellite: ISS
Catalog Number: 25544
Epoch time:      19054
35179574   =   yrday
fracday
Element set:     911
Inclination:       51
6389  deg
RA of node:       207
2529  deg
Eccentricity:     
0005728     
Arg of perigee:    52
8646  deg
Mean anomaly:     307
3029  deg
Mean motion:   15
53289613  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3756
Checksum:              335


Coasting Arc #13 (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    =        3446213
77                 A    =         6780943
98  meter
 Y    =       -2958183
80  meter          E    =           
0011287
 Z    =        5028908
41                 I    =           51
47976
 XDOT =       6243
665013                 Wp   =           56
51783
 YDOT =       4035
893626  meter/sec      RA   =          201
16942  deg
 ZDOT =      -1895
424965                 TA   =           51
93979
                                          MA   =           51
83800
                                          Ha   =            224
160  n
mi
                                          Hp   =            214
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11306475
63                 X    =         3454609
54
 Y    =       -9705327
44  feet           Y    =        -2919598
46  meter
 Z    =       16499043
34                 Z    =         5045669
27
 XDOT =      20484
465267                 XDOT =        6207
277283
 YDOT =      13241
120819  feet/sec       YDOT =        4105
511030  meter/sec
 ZDOT =      -6218
585843                 ZDOT =       -1865
184673

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10467172
24                 X    =         3190394
10
 Y    =       10486045
66  feet           Y    =         3196146
72  meter
 Z    =       16574961
68                 Z    =         5052048
32
 XDOT =     -11000
529923                 XDOT =       -3352
961521
 YDOT =      20642
262527  feet/sec       YDOT =        6291
761618  meter/sec
 ZDOT =      -6082
324110                 ZDOT =       -1853
892389


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
38119267  
00016717  00000-0  10270-3 0  9127
2 25544  51
6389 202
1278 0005739  56
6417 303
5283 15
53285362 37722


Satellite: ISS
Catalog Number: 25544
Epoch time:      19055
38119267   =   yrday
fracday
Element set:     912
Inclination:       51
6389  deg
RA of node:       202
1278  deg
Eccentricity:     
0005739     
Arg of perigee:    56
6417  deg
Mean anomaly:     303
5283  deg
Mean motion:   15
53285362  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3772
Checksum:              323


Coasting Arc #14 (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    =       -4606143
53                 A    =         6783417
30  meter
 Y    =        2320893
72  meter          E    =           
0013682
 Z    =       -4418053
45                 I    =           51
51767
 XDOT =      -5369
320047                 Wp   =           92
44574
 YDOT =      -4319
407253  meter/sec      RA   =          196
17333  deg
 ZDOT =       3337
222952                 TA   =          211
34800
                                          MA   =          211
42964
                                          Ha   =            224
276  n
mi
                                          Hp   =            213
970

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15112019
44                 X    =        -4610293
87
 Y    =        7614480
72  feet           Y    =         2269361
10  meter
 Z    =      -14494926
03                 Z    =        -4440438
36
 XDOT =     -17615
879419                 XDOT =       -5336
830352
 YDOT =     -14171
283640  feet/sec       YDOT =       -4379
268851  meter/sec
 ZDOT =      10948
894198                 ZDOT =        3311
220310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8897212
07                 X    =        -2711870
24
 Y    =      -14291491
10  feet           Y    =        -4356046
49  meter
 Z    =      -14596205
96                 Z    =        -4448923
58
 XDOT =      11527
422287                 XDOT =        3513
558313
 YDOT =     -18211
247715  feet/sec       YDOT =       -5550
788303  meter/sec
 ZDOT =      10831
775715                 ZDOT =        3301
525238


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
34625226  
00016717  00000-0  10270-3 0  9132
2 25544  51
6370 197
3227 0005732  61
1257 299
0470 15
53284569 37878


Satellite: ISS
Catalog Number: 25544
Epoch time:      19056
34625226   =   yrday
fracday
Element set:     913
Inclination:       51
6370  deg
RA of node:       197
3227  deg
Eccentricity:     
0005732     
Arg of perigee:    61
1257  deg
Mean anomaly:     299
0470  deg
Mean motion:   15
53284569  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3787
Checksum:              324


Coasting Arc #15 (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    =       -1677510
08                 A    =         6781615
89  meter
 Y    =        3928555
33  meter          E    =           
0017488
 Z    =       -5282194
99                 I    =           51
53304
 XDOT =      -7303
934350                 Wp   =           87
41559
 YDOT =      -2174
820876  meter/sec      RA   =          192
36726  deg
 ZDOT =        704
872645                 TA   =          189
32343
                                          MA   =          189
35594
                                          Ha   =            224
388  n
mi
                                          Hp   =            215
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5503642
00                 X    =        -1695657
96
 Y    =       12888961
05  feet           Y    =         3909694
47  meter
 Z    =      -17330036
06                 Z    =        -5290387
91
 XDOT =     -23963
039207                 XDOT =       -7282
495888
 YDOT =      -7135
239093  feet/sec       YDOT =       -2256
378661  meter/sec
 ZDOT =       2312
574296                 ZDOT =         669
445488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2598780
61                 X    =          792108
33
 Y    =      -13724699
44  feet           Y    =        -4183288
39  meter
 Z    =      -17367340
23                 Z    =        -5293565
30
 XDOT =      23935
413909                 XDOT =        7295
514160
 YDOT =       1819
702496  feet/sec       YDOT =         554
645321  meter/sec
 ZDOT =       2152
709907                 ZDOT =         656
145980


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
11830221  
00016717  00000-0  10270-3 0  9142
2 25544  51
6394 193
4798 0003642  52
3397 307
8085 15
52716656 37998


Satellite: ISS
Catalog Number: 25544
Epoch time:      19057
11830221   =   yrday
fracday
Element set:     914
Inclination:       51
6394  deg
RA of node:       193
4798  deg
Eccentricity:     
0003642     
Arg of perigee:    52
3397  deg
Mean anomaly:     307
8085  deg
Mean motion:   15
52716656  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3799
Checksum:              334


Coasting Arc #16 (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    =       -2285616
44                 A    =         6782061
57  meter
 Y    =        3769659
52  meter          E    =           
0016506
 Z    =       -5168306
65                 I    =           51
55219
 XDOT =      -7134
466076                 Wp   =           93
21160
 YDOT =      -2377
978988  meter/sec      RA   =          189
78900  deg
 ZDOT =       1423
708605                 TA   =          190
51065
                                          MA   =          190
54520
                                          Ha   =            224
305  n
mi
                                          Hp   =            215
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7498741
59                 X    =        -2302495
52
 Y    =       12367649
34  feet           Y    =         3744005
52  meter
 Z    =      -16956386
63                 Z    =        -5179450
36
 XDOT =     -23407
040932                 XDOT =       -7114
260096
 YDOT =      -7801
768334  feet/sec       YDOT =       -2457
648520  meter/sec
 ZDOT =       4670
959991                 ZDOT =        1389
101686

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3133270
34                 X    =         -955020
80
 Y    =       14058915
84  feet           Y    =         4285157
55  meter
 Z    =      -17007011
08                 Z    =        -5183736
98
 XDOT =     -23676
800664                 XDOT =       -7216
688842
 YDOT =        172
753167  feet/sec       YDOT =          52
655165  meter/sec
 ZDOT =       4514
804310                 ZDOT =        1376
112354


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
63318567  
00016717  00000-0  10270-3 0  9154
2 25544  51
6401 190
9163 0003330  58
5586 301
5891 15
52729356 38074


Satellite: ISS
Catalog Number: 25544
Epoch time:      19057
63318567   =   yrday
fracday
Element set:     915
Inclination:       51
6401  deg
RA of node:       190
9163  deg
Eccentricity:     
0003330     
Arg of perigee:    58
5586  deg
Mean anomaly:     301
5891  deg
Mean motion:   15
52729356  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3807
Checksum:              322


Coasting Arc #17 (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    =        3417002
32                 A    =         6783808
05  meter
 Y    =       -3467148
81  meter          E    =           
0011092
 Z    =        4718548
37                 I    =           51
59165
 XDOT =       6609
091988                 Wp   =           62
15615
 YDOT =       2748
338731  meter/sec      RA   =          184
80145  deg
 ZDOT =      -2756
579845                 TA   =           55
19505
                                          MA   =           55
09074
                                          Ha   =            224
219  n
mi
                                          Hp   =            215
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11210637
53                 X    =         3432599
26
 Y    =      -11375160
15  feet           Y    =        -3428850
09  meter
 Z    =       15480801
74                 Z    =         4735184
67
 XDOT =      21683
372665                 XDOT =        6591
257820
 YDOT =       9016
859354  feet/sec       YDOT =        2822
146375  meter/sec
 ZDOT =      -9043
897129                 ZDOT =       -2724
519283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6731667
72                 X    =         2051812
32
 Y    =      -14401957
02  feet           Y    =        -4389716
50  meter
 Z    =       15556226
05                 Z    =         4741537
70
 XDOT =      22450
455935                 XDOT =        6842
898969
 YDOT =        845
775846  feet/sec       YDOT =         257
792478  meter/sec
 ZDOT =      -8899
250229                 ZDOT =       -2712
491470


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
66295326  
00016717  00000-0  10270-3 0  9166
2 25544  51
6405 185
7933 0003391  60
1956 299
9533 15
52749351 38230


Satellite: ISS
Catalog Number: 25544
Epoch time:      19058
66295326   =   yrday
fracday
Element set:     916
Inclination:       51
6405  deg
RA of node:       185
7933  deg
Eccentricity:     
0003391     
Arg of perigee:    60
1956  deg
Mean anomaly:     299
9533  deg
Mean motion:   15
52749351  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3823
Checksum:              340
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