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

 
Date: May 7th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14255 723 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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


130/00:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 1
000/00:00:00 000 0 0 0 0 222 8

132/16:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 0
000/00:00:00 000 0 0 0 0 222 6

132/22:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 1
000/00:00:00 000 0 0 0 0 222 8

135/18:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 1
000/00:00:00 000 0 0 0 0 222 6

Coasting Arc #1 (Orbit 2554)
---------------------------------------

Vector Time (GMT): 2020/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1618892
22                 A    =         6791314
21  meter
 Y    =       -3935052
67  meter          E    =           
0001334
 Z    =        5292025
59                 I    =           51
52725
 XDOT =       7306
346432                 Wp   =           68
48972
 YDOT =       2235
241336  meter/sec      RA   =          193
59745  deg
 ZDOT =       -572
417150                 TA   =           26
98951
                                          MA   =           26
98257
                                          Ha   =            227
946  n
mi
                                          Hp   =            222
651

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5311326
17                 X    =         1637068
71
 Y    =      -12910277
77  feet           Y    =        -3916847
57  meter
 Z    =       17362288
67                 Z    =         5299933
72
 XDOT =      23970
952861                 XDOT =        7283
588803
 YDOT =       7333
468951  feet/sec       YDOT =        2316
818872  meter/sec
 ZDOT =      -1878
009021                 ZDOT =        -536
980330

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5210503
86                 X    =        -1588161
58
 Y    =      -12902354
92  feet           Y    =        -3932637
78  meter
 Z    =       17398689
97                 Z    =         5303120
70
 XDOT =      21424
264065                 XDOT =        6530
115687
 YDOT =     -10967
825535  feet/sec       YDOT =       -3342
993223  meter/sec
 ZDOT =      -1715
397766                 ZDOT =        -522
853239


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   20127
54749777  
00016717  00000-0  10270-3 0  9009
2 25544  51
6425 194
5676 0001458 248
5349 111
5646 15
49374633 25552


Satellite: ISS
Catalog Number: 25544
Epoch time:      20127
54749777   =   yrday
fracday
Element set:     900
Inclination:       51
6425  deg
RA of node:       194
5676  deg
Eccentricity:     
0001458     
Arg of perigee:   248
5349  deg
Mean anomaly:     111
5646  deg
Mean motion:   15
49374633  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2555
Checksum:              335


Coasting Arc #2 (Orbit 2569)
---------------------------------------

Vector Time (GMT): 2020/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1430284
19                 A    =         6791502
14  meter
 Y    =        4028768
03  meter          E    =           
0013324
 Z    =       -5288742
38                 I    =           51
55919
 XDOT =      -7425
323333                 Wp   =           97
80161
 YDOT =      -1700
556961  meter/sec      RA   =          188
64206  deg
 ZDOT =        712
455806                 TA   =          179
02780
                                          MA   =          179
02520
                                          Ha   =            228
069  n
mi
                                          Hp   =            222
645

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4692533
44                 X    =        -1449538
56
 Y    =       13217742
88  feet           Y    =         4012666
21  meter
 Z    =      -17351516
98                 Z    =        -5295736
82
 XDOT =     -24361
297023                 XDOT =       -7409
216105
 YDOT =      -5579
255123  feet/sec       YDOT =       -1783
502190  meter/sec
 ZDOT =       2337
453431                 ZDOT =         676
424787

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6086991
70                 X    =         1855315
07
 Y    =       12591985
50  feet           Y    =         3838037
18  meter
 Z    =      -17383732
96                 Z    =        -5298561
81
 XDOT =     -20289
079733                 XDOT =       -6184
111503
 YDOT =      12807
431001  feet/sec       YDOT =        3903
704969  meter/sec
 ZDOT =       2172
079345                 ZDOT =         662
049784


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   20128
51500711  
00016717  00000-0  10270-3 0  9011
2 25544  51
6413 189
7795 0001388 253
6855 106
4142 15
49332805 25704


Satellite: ISS
Catalog Number: 25544
Epoch time:      20128
51500711   =   yrday
fracday
Element set:     901
Inclination:       51
6413  deg
RA of node:       189
7795  deg
Eccentricity:     
0001388     
Arg of perigee:   253
6855  deg
Mean anomaly:     106
4142  deg
Mean motion:   15
49332805  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2570
Checksum:              299


Coasting Arc #3 (Orbit 2585)
---------------------------------------

Vector Time (GMT): 2020/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1236428
73                 A    =         6791433
60  meter
 Y    =       -4104290
05  meter          E    =           
0001987
 Z    =        5266662
59                 I    =           51
59311
 XDOT =       7524
255658                 Wp   =           48
61914
 YDOT =       1165
608136  meter/sec      RA   =          183
68891  deg
 ZDOT =       -856
584435                 TA   =           49
59169
                                          MA   =           49
57435
                                          Ha   =            227
947  n
mi
                                          Hp   =            222
649

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4056524
70                 X    =         1256649
31
 Y    =      -13465518
52  feet           Y    =        -4090350
81  meter
 Z    =       17279076
75                 Z    =         5272717
55
 XDOT =      24685
878143                 XDOT =        7514
823136
 YDOT =       3824
173675  feet/sec       YDOT =        1249
697050  meter/sec
 ZDOT =      -2810
316387                 ZDOT =        -820
056671

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6923000
17                 X    =        -2110130
45
 Y    =      -12201732
49  feet           Y    =        -3719088
06  meter
 Z    =       17306988
99                 Z    =         5275170
24
 XDOT =      19054
792629                 XDOT =        5807
900793
 YDOT =     -14566
528931  feet/sec       YDOT =       -4439
878018  meter/sec
 ZDOT =      -2642
622371                 ZDOT =        -805
471299


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   20129
54701223  
00016717  00000-0  10270-3 0  9027
2 25544  51
6415 184
6721 0001378 260
0071 100
0923 15
49376539 25866


Satellite: ISS
Catalog Number: 25544
Epoch time:      20129
54701223   =   yrday
fracday
Element set:     902
Inclination:       51
6415  deg
RA of node:       184
6721  deg
Eccentricity:     
0001378     
Arg of perigee:   260
0071  deg
Mean anomaly:     100
0923  deg
Mean motion:   15
49376539  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2586
Checksum:              287


Coasting Arc #4 (Orbit 2593)
---------------------------------------

Vector Time (GMT): 2020/130/00:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6603524
83                 A    =         6802744
52  meter
 Y    =        1077349
05  meter          E    =           
0008427
 Z    =       -1205591
42                 I    =           51
64861
 XDOT =      -1813
776805                 Wp   =          149
64657
 YDOT =       4596
968893  meter/sec      RA   =          181
06975  deg
 ZDOT =      -5851
836501                 TA   =           43
42234
                                          MA   =           43
35599
                                          Ha   =            228
077  n
mi
                                          Hp   =            222
754

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21665107
72                 X    =         6596842
98
 Y    =        3534609
76  feet           Y    =         1151157
13  meter
 Z    =       -3955352
44                 Z    =        -1173529
67
 XDOT =      -5950
711304                 XDOT =       -1836
621324
 YDOT =      15081
918939  feet/sec       YDOT =        4576
558807  meter/sec
 ZDOT =     -19198
938652                 ZDOT =       -5860
702291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14412222
46                 X    =        -4392845
41
 Y    =       16592197
29  feet           Y    =         5057301
73  meter
 Z    =       -3808149
77                 Z    =        -1160724
05
 XDOT =      -8557
473293                 XDOT =       -2608
317860
 YDOT =     -11829
397188  feet/sec       YDOT =       -3605
600263  meter/sec
 ZDOT =     -19239
776020                 ZDOT =       -5864
283731


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   20130
06301554  
00016717  00000-0  10270-3 0  9030
2 25544  51
6420 182
1197 0001406 272
3947  87
7042 15
49329617 25949


Satellite: ISS
Catalog Number: 25544
Epoch time:      20130
06301554   =   yrday
fracday
Element set:     903
Inclination:       51
6420  deg
RA of node:       182
1197  deg
Eccentricity:     
0001406     
Arg of perigee:   272
3947  deg
Mean anomaly:      87
7042  deg
Mean motion:   15
49329617  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2594
Checksum:              293


Coasting Arc #5 (Orbit 2609)
---------------------------------------

Vector Time (GMT): 2020/131/00:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6641206
91                 A    =         6802482
89  meter
 Y    =        -591602
04  meter          E    =           
0012685
 Z    =        1315291
63                 I    =           51
68025
 XDOT =       1580
619185                 Wp   =           55
62393
 YDOT =      -4720
825453  meter/sec      RA   =          176
12127  deg
 ZDOT =       5824
396220                 TA   =          318
65744
                                          MA   =          318
75339
                                          Ha   =            227
996  n
mi
                                          Hp   =            222
676

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21788736
60                 X    =        -6640486
87
 Y    =       -1940951
56  feet           Y    =         -665864
87  meter
 Z    =        4315261
27                 Z    =         1283032
54
 XDOT =       5185
758482                 XDOT =        1604
999461
 YDOT =     -15488
272482  feet/sec       YDOT =       -4703
014215  meter/sec
 ZDOT =      19108
911483                 ZDOT =        5832
132999

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12819333
03                 X    =         3907332
71
 Y    =      -17760565
45  feet           Y    =        -5413420
35  meter
 Z    =        4167113
03                 Z    =         1270136
05
 XDOT =       9432
316692                 XDOT =        2874
970128
 YDOT =      11326
374725  feet/sec       YDOT =        3452
279016  meter/sec
 ZDOT =      19144
577252                 ZDOT =        5835
267146


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   20131
09501795  
00016717  00000-0  10270-3 0  9044
2 25544  51
6404 177
0112 0001367 277
9708  82
1287 15
49382711 26106


Satellite: ISS
Catalog Number: 25544
Epoch time:      20131
09501795   =   yrday
fracday
Element set:     904
Inclination:       51
6404  deg
RA of node:       177
0112  deg
Eccentricity:     
0001367     
Arg of perigee:   277
9708  deg
Mean anomaly:      82
1287  deg
Mean motion:   15
49382711  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2610
Checksum:              294


Coasting Arc #6 (Orbit 2624)
---------------------------------------

Vector Time (GMT): 2020/132/00:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6640253
62                 A    =         6802437
33  meter
 Y    =         130823
51  meter          E    =           
0007528
 Z    =       -1454077
96                 I    =           51
71278
 XDOT =      -1357
773220                 Wp   =          150
17523
 YDOT =       4832
067993  meter/sec      RA   =          171
17647  deg
 ZDOT =      -5784
986011                 TA   =           45
63648
                                          MA   =           45
57483
                                          Ha   =            228
053  n
mi
                                          Hp   =            222
752

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21785609
00                 X    =         6645360
33
 Y    =         429211
01  feet           Y    =          205108
29  meter
 Z    =       -4770596
99                 Z    =        -1421809
56
 XDOT =      -4454
636550                 XDOT =       -1383
605583
 YDOT =      15853
241448  feet/sec       YDOT =        4816
740680  meter/sec
 ZDOT =     -18979
612897                 ZDOT =       -5791
643736

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11199434
78                 X    =        -3413587
72
 Y    =       18728640
33  feet           Y    =         5708489
57  meter
 Z    =       -4622366
21                 Z    =        -1408897
22
 XDOT =     -10250
289364                 XDOT =       -3124
288198
 YDOT =     -10805
305033  feet/sec       YDOT =       -3293
456974  meter/sec
 ZDOT =     -19010
333681                 ZDOT =       -5794
349706


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   20132
06252240  
00016717  00000-0  10270-3 0  9051
2 25544  51
6400 172
2233 0001451 280
5001  79
5985 15
49342632 26252


Satellite: ISS
Catalog Number: 25544
Epoch time:      20132
06252240   =   yrday
fracday
Element set:     905
Inclination:       51
6400  deg
RA of node:       172
2233  deg
Eccentricity:     
0001451     
Arg of perigee:   280
5001  deg
Mean anomaly:      79
5985  deg
Mean motion:   15
49342632  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2625
Checksum:              267


Coasting Arc #7 (Orbit 2634)
---------------------------------------

Vector Time (GMT): 2020/132/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3854999
35                 A    =         6796623
23  meter
 Y    =       -3985597
94  meter          E    =           
0009919
 Z    =        3923746
64                 I    =           51
71317
 XDOT =       6187
446708                 Wp   =           77
37053
 YDOT =       1968
621985  meter/sec      RA   =          168
00399  deg
 ZDOT =      -4068
579091                 TA   =           55
24470
                                          MA   =           55
15135
                                          Ha   =            227
989  n
mi
                                          Hp   =            222
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12647635
66                 X    =         3880221
58
 Y    =      -13076108
73  feet           Y    =        -3942348
04  meter
 Z    =       12873184
52                 Z    =         3942533
58
 XDOT =      20300
022009                 XDOT =        6184
736037
 YDOT =       6458
733546  feet/sec       YDOT =        2037
799745  meter/sec
 ZDOT =     -13348
356597                 ZDOT =       -4038
529120

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16451725
62                 X    =        -5014485
97
 Y    =       -7619408
44  feet           Y    =        -2322395
69  meter
 Z    =       12959611
34                 Z    =         3950089
54
 XDOT =      -1086
825938                 XDOT =        -331
264546
 YDOT =     -20182
302715  feet/sec       YDOT =       -6151
565867  meter/sec
 ZDOT =     -13210
353515                 ZDOT =       -4026
515751


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   20132
70752452  
00016717  00000-0  10270-3 0  9063
2 25544  51
6382 169
0302 0001251 286
1629  73
9383 15
49367818 26352


Satellite: ISS
Catalog Number: 25544
Epoch time:      20132
70752452   =   yrday
fracday
Element set:     906
Inclination:       51
6382  deg
RA of node:       169
0302  deg
Eccentricity:     
0001251     
Arg of perigee:   286
1629  deg
Mean anomaly:      73
9383  deg
Mean motion:   15
49367818  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2635
Checksum:              309


Coasting Arc #8 (Orbit 2638)
---------------------------------------

Vector Time (GMT): 2020/132/22:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6431466
60                 A    =         6801351
23  meter
 Y    =         256620
09  meter          E    =           
0005177
 Z    =       -2191394
19                 I    =           51
74148
 XDOT =      -2061
886726                 Wp   =          147
88148
 YDOT =       4930
697653  meter/sec      RA   =          166
71118  deg
 ZDOT =      -5484
213286                 TA   =           56
35137
                                          MA   =           56
30200
                                          Ha   =            228
071  n
mi
                                          Hp   =            222
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21100612
20                 X    =         6438763
57
 Y    =         841929
43  feet           Y    =          328582
38  meter
 Z    =       -7189613
48                 Z    =        -2160134
79
 XDOT =      -6764
720230                 XDOT =       -2090
230758
 YDOT =      16176
829571  feet/sec       YDOT =        4907
482329  meter/sec
 ZDOT =     -17992
825741                 ZDOT =       -5494
297421

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19262247
93                 X    =        -5871133
17
 Y    =        8772396
08  feet           Y    =         2673826
32  meter
 Z    =       -7045998
45                 Z    =        -2147620
33
 XDOT =       -713
967835                 XDOT =        -217
617396
 YDOT =     -16029
374410  feet/sec       YDOT =       -4885
753320  meter/sec
 ZDOT =     -18039
298456                 ZDOT =       -5498
378170


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   20132
96552506  
00016717  00000-0  10270-3 0  9070
2 25544  51
6425 167
7552 0001453 282
7283  77
3705 15
49335404 26390


Satellite: ISS
Catalog Number: 25544
Epoch time:      20132
96552506   =   yrday
fracday
Element set:     907
Inclination:       51
6425  deg
RA of node:       167
7552  deg
Eccentricity:     
0001453     
Arg of perigee:   282
7283  deg
Mean anomaly:      77
3705  deg
Mean motion:   15
49335404  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2639
Checksum:              314


Coasting Arc #9 (Orbit 2654)
---------------------------------------

Vector Time (GMT): 2020/133/22:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6391891
46                 A    =         6801077
93  meter
 Y    =         201646
64  meter          E    =           
0012820
 Z    =        2295583
90                 I    =           51
77327
 XDOT =       1797
171255                 Wp   =           67
57763
 YDOT =      -5097
047926  meter/sec      RA   =          161
76891  deg
 ZDOT =       5432
348815                 TA   =          317
89475
                                          MA   =          317
99318
                                          Ha   =            228
101  n
mi
                                          Hp   =            222
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20970772
52                 X    =        -6404821
91
 Y    =         661570
34  feet           Y    =          130095
42  meter
 Z    =        7531443
24                 Z    =         2264503
20
 XDOT =       5896
231150                 XDOT =        1827
647144
 YDOT =     -16722
598183  feet/sec       YDOT =       -5076
780838  meter/sec
 ZDOT =      17822
666715                 ZDOT =        5441
152264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18295604
03                 X    =         5576500
11
 Y    =      -10373663
41  feet           Y    =        -3161892
61  meter
 Z    =        7388612
39                 Z    =         2252049
06
 XDOT =       1918
578614                 XDOT =         584
782761
 YDOT =      16153
176186  feet/sec       YDOT =        4923
488102  meter/sec
 ZDOT =      17863
268076                 ZDOT =        5444
724110


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   20133
99752426  
00016717  00000-0  10270-3 0  9088
2 25544  51
6425 162
6466 0001471 296
8216  63
2783 15
49364600 26558


Satellite: ISS
Catalog Number: 25544
Epoch time:      20133
99752426   =   yrday
fracday
Element set:     908
Inclination:       51
6425  deg
RA of node:       162
6466  deg
Eccentricity:     
0001471     
Arg of perigee:   296
8216  deg
Mean anomaly:      63
2783  deg
Mean motion:   15
49364600  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2655
Checksum:              320


Coasting Arc #10 (Orbit 2669)
---------------------------------------

Vector Time (GMT): 2020/134/22:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6320899
72                 A    =         6800888
10  meter
 Y    =        -628530
13  meter          E    =           
0004263
 Z    =       -2426420
50                 I    =           51
80307
 XDOT =      -1533
672091                 Wp   =          140
50939
 YDOT =       5246
030872  meter/sec      RA   =          156
82997  deg
 ZDOT =      -5362
559647                 TA   =           66
49504
                                          MA   =           66
45025
                                          Ha   =            228
104  n
mi
                                          Hp   =            222
757

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20737859
98                 X    =         6339244
50
 Y    =       -2062106
73  feet           Y    =         -557742
55  meter
 Z    =       -7960697
19                 Z    =        -2395671
57
 XDOT =      -5031
732582                 XDOT =       -1566
172561
 YDOT =      17211
387376  feet/sec       YDOT =        5228
699005  meter/sec
 ZDOT =     -17593
699629                 ZDOT =       -5370
088099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17239455
40                 X    =        -5254586
01
 Y    =       11804348
85  feet           Y    =         3597965
53  meter
 Z    =       -7819357
15                 Z    =        -2383340
06
 XDOT =      -3106
317984                 XDOT =        -946
805722
 YDOT =     -16195
333771  feet/sec       YDOT =       -4936
337733  meter/sec
 ZDOT =     -17628
453131                 ZDOT =       -5373
152514


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   20134
96502332  
00016717  00000-0  10270-3 0  9096
2 25544  51
6415 157
8585 0001465 294
9486  65
1511 15
49339985 26701


Satellite: ISS
Catalog Number: 25544
Epoch time:      20134
96502332   =   yrday
fracday
Element set:     909
Inclination:       51
6415  deg
RA of node:       157
8585  deg
Eccentricity:     
0001465     
Arg of perigee:   294
9486  deg
Mean anomaly:      65
1511  deg
Mean motion:   15
49339985  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2670
Checksum:              331


Coasting Arc #11 (Orbit 2682)
---------------------------------------

Vector Time (GMT): 2020/135/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4961002
29                 A    =         6794969
49  meter
 Y    =        1371606
70  meter          E    =           
0008345
 Z    =       -4444706
16                 I    =           51
80972
 XDOT =      -4445
950976                 Wp   =           62
37670
 YDOT =       5256
763708  meter/sec      RA   =          152
66628  deg
 ZDOT =      -3341
231557                 TA   =          173
88269
                                          MA   =          173
87249
                                          Ha   =            228
122  n
mi
                                          Hp   =            222
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16276254
24                 X    =         4966885
69
 Y    =        4500021
99  feet           Y    =         1427117
39  meter
 Z    =      -14582369
30                 Z    =        -4420593
18
 XDOT =     -14586
453333                 XDOT =       -4488
173455
 YDOT =      17246
600091  feet/sec       YDOT =        5206
810087  meter/sec
 ZDOT =     -10962
045792                 ZDOT =       -3362
930394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12610778
26                 X    =        -3843765
21
 Y    =      -11373388
05  feet           Y    =        -3466608
68  meter
 Z    =      -14471574
22                 Z    =        -4410935
82
 XDOT =      19881
178603                 XDOT =        6059
783238
 YDOT =      -7973
288641  feet/sec       YDOT =       -2430
258378  meter/sec
 ZDOT =     -11061
940015                 ZDOT =       -3371
679317


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   20135
80352329  
00016717  00000-0  10270-3 0  9101
2 25544  51
6417 153
7083 0001304 306
7740  53
3290 15
49383931 26835


Satellite: ISS
Catalog Number: 25544
Epoch time:      20135
80352329   =   yrday
fracday
Element set:     910
Inclination:       51
6417  deg
RA of node:       153
7083  deg
Eccentricity:     
0001304     
Arg of perigee:   306
7740  deg
Mean anomaly:      53
3290  deg
Mean motion:   15
49383931  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2683
Checksum:              290


Coasting Arc #12 (Orbit 2698)
---------------------------------------

Vector Time (GMT): 2020/136/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4970558
07                 A    =         6794761
99  meter
 Y    =       -1050261
59  meter          E    =           
0007814
 Z    =        4507130
44                 I    =           51
83832
 XDOT =       4116
571427                 Wp   =          108
93719
 YDOT =      -5599
475557  meter/sec      RA   =          147
72978  deg
 ZDOT =       3227
994634                 TA   =          308
63266
                                          MA   =          308
70258
                                          Ha   =            228
274  n
mi
                                          Hp   =            222
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16307605
20                 X    =        -4980337
40
 Y    =       -3445740
11  feet           Y    =        -1105900
87  meter
 Z    =       14787173
37                 Z    =         4482961
57
 XDOT =      13505
811767                 XDOT =        4163
200701
 YDOT =     -18370
982800  feet/sec       YDOT =       -5553
180607  meter/sec
 ZDOT =      10590
533577                 ZDOT =        3248
104255

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13291218
23                 X    =         4051163
32
 Y    =       10218964
55  feet           Y    =         3114740
39  meter
 Z    =       14676099
29                 Z    =         4473275
06
 XDOT =     -19325
425744                 XDOT =       -5890
389767
 YDOT =       9759
281278  feet/sec       YDOT =        2974
628934  meter/sec
 ZDOT =      10683
148204                 ZDOT =        3256
223573


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   20136
83552046  
00016717  00000-0  10270-3 0  9114
2 25544  51
6419 148
6007 0001329 306
8244  53
2784 15
49367327 26998


Satellite: ISS
Catalog Number: 25544
Epoch time:      20136
83552046   =   yrday
fracday
Element set:     911
Inclination:       51
6419  deg
RA of node:       148
6007  deg
Eccentricity:     
0001329     
Arg of perigee:   306
8244  deg
Mean anomaly:      53
2784  deg
Mean motion:   15
49367327  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2699
Checksum:              316


Coasting Arc #13 (Orbit 2713)
---------------------------------------

Vector Time (GMT): 2020/137/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4963617
47                 A    =         6794410
08  meter
 Y    =         753368
62  meter          E    =           
0009294
 Z    =       -4587447
34                 I    =           51
86625
 XDOT =      -3757
012833                 Wp   =           62
12178
 YDOT =       5903
919391  meter/sec      RA   =          142
79501  deg
 ZDOT =      -3096
088718                 TA   =          176
92496
                                          MA   =          176
91925
                                          Ha   =            228
139  n
mi
                                          Hp   =            222
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16284834
23                 X    =         4977107
46
 Y    =        2471681
83  feet           Y    =          808951
01  meter
 Z    =      -15050680
26                 Z    =        -4563303
12
 XDOT =     -12326
157587                 XDOT =       -3807
713891
 YDOT =      19369
814274  feet/sec       YDOT =        5861
622486  meter/sec
 ZDOT =     -10157
771385                 ZDOT =       -3114
461703

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13853191
96                 X    =        -4222452
91
 Y    =       -9095189
09  feet           Y    =        -2772213
63  meter
 Z    =      -14939699
50                 Z    =        -4553620
41
 XDOT =      18568
509509                 XDOT =        5659
681698
 YDOT =     -11461
256863  feet/sec       YDOT =       -3493
391092  meter/sec
 ZDOT =     -10242
427074                 ZDOT =       -3121
891772


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   20137
80301483  
00016717  00000-0  10270-3 0  9120
2 25544  51
6429 143
8125 0001424 315
1770  44
9265 15
49391731 27145


Satellite: ISS
Catalog Number: 25544
Epoch time:      20137
80301483   =   yrday
fracday
Element set:     912
Inclination:       51
6429  deg
RA of node:       143
8125  deg
Eccentricity:     
0001424     
Arg of perigee:   315
1770  deg
Mean anomaly:      44
9265  deg
Mean motion:   15
49391731  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2714
Checksum:              289


Coasting Arc #14 (Orbit 2729)
---------------------------------------

Vector Time (GMT): 2020/138/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4933347
53                 A    =         6794232
17  meter
 Y    =        -449921
06  meter          E    =           
0007233
 Z    =        4645204
64                 I    =           51
89076
 XDOT =       3374
713980                 Wp   =          109
95932
 YDOT =      -6202
467611  meter/sec      RA   =          137
86182  deg
 ZDOT =       2977
128925                 TA   =          310
42149
                                          MA   =          310
48457
                                          Ha   =            228
376  n
mi
                                          Hp   =            222
489

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16185523
40                 X    =        -4950513
64
 Y    =       -1476118
96  feet           Y    =         -505185
51  meter
 Z    =       15240172
71                 Z    =         4621198
47
 XDOT =      11071
896260                 XDOT =        3429
359698
 YDOT =     -20349
303187  feet/sec       YDOT =       -6164
423781  meter/sec
 ZDOT =       9767
483349                 ZDOT =        2993
654466

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14318444
24                 X    =         4364261
80
 Y    =        7904685
26  feet           Y    =         2409348
07  meter
 Z    =       15129807
16                 Z    =         4611565
22
 XDOT =     -17686
280919                 XDOT =       -5390
778424
 YDOT =      13156
611388  feet/sec       YDOT =        4010
135151  meter/sec
 ZDOT =       9843
671035                 ZDOT =        3000
350932


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   20138
83500914  
00016717  00000-0  10270-3 0  9135
2 25544  51
6422 138
7046 0001360 320
5655  39
5396 15
49366763 27304


Satellite: ISS
Catalog Number: 25544
Epoch time:      20138
83500914   =   yrday
fracday
Element set:     913
Inclination:       51
6422  deg
RA of node:       138
7046  deg
Eccentricity:     
0001360     
Arg of perigee:   320
5655  deg
Mean anomaly:      39
5396  deg
Mean motion:   15
49366763  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2730
Checksum:              303


Coasting Arc #15 (Orbit 2744)
---------------------------------------

Vector Time (GMT): 2020/139/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4893622
11                 A    =         6793896
24  meter
 Y    =         169938
15  meter          E    =           
0010136
 Z    =       -4719556
63                 I    =           51
91400
 XDOT =      -2964
640973                 Wp   =           62
72014
 YDOT =       6456
580011  meter/sec      RA   =          132
93082  deg
 ZDOT =      -2841
668848                 TA   =          179
12784
                                          MA   =          179
12607
                                          Ha   =            228
151  n
mi
                                          Hp   =            222
627

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16055190
64                 X    =         4914283
26
 Y    =         557539
85  feet           Y    =          224777
93  meter
 Z    =      -15484109
67                 Z    =        -4695734
87
 XDOT =      -9726
512378                 XDOT =       -3022
816672
 YDOT =      21183
005285  feet/sec       YDOT =        6423
102183  meter/sec
 ZDOT =      -9323
060524                 ZDOT =       -2856
210967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14688721
79                 X    =        -4477122
40
 Y    =       -6760295
45  feet           Y    =        -2060538
05  meter
 Z    =      -15374573
40                 Z    =        -4686169
97
 XDOT =      16607
059129                 XDOT =        5061
831622
 YDOT =     -14729
459305  feet/sec       YDOT =       -4489
539196  meter/sec
 ZDOT =      -9390
154867                 ZDOT =       -2862
119203


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   20139
80250187  
00016717  00000-0  10270-3 0  9148
2 25544  51
6422 133
9168 0001537 319
3784  40
7252 15
49391747 27452


Satellite: ISS
Catalog Number: 25544
Epoch time:      20139
80250187   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:       133
9168  deg
Eccentricity:     
0001537     
Arg of perigee:   319
3784  deg
Mean anomaly:      40
7252  deg
Mean motion:   15
49391747  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2745
Checksum:              314


Coasting Arc #16 (Orbit 2760)
---------------------------------------

Vector Time (GMT): 2020/140/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4829876
12                 A    =         6793720
85  meter
 Y    =         111800
66  meter          E    =           
0006453
 Z    =        4772299
37                 I    =           51
93583
 XDOT =       2535
230181                 Wp   =          111
55523
 YDOT =      -6701
476293  meter/sec      RA   =          128
00035  deg
 ZDOT =       2717
556502                 TA   =          311
64600
                                          MA   =          311
70124
                                          Ha   =            228
394  n
mi
                                          Hp   =            222
481

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15846050
26                 X    =        -4853948
77
 Y    =         366800
05  feet           Y    =           57654
58  meter
 Z    =       15657150
16                 Z    =         4748778
92
 XDOT =       8317
684321                 XDOT =        2596
779131
 YDOT =     -21986
470779  feet/sec       YDOT =       -6672
781608  meter/sec
 ZDOT =       8915
867789                 ZDOT =        2730
020820

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14952289
87                 X    =         4557457
95
 Y    =        5571036
57  feet           Y    =         1698051
95  meter
 Z    =       15548980
08                 Z    =         4739329
13
 XDOT =     -15411
377977                 XDOT =       -4697
388007
 YDOT =      16269
433412  feet/sec       YDOT =        4958
923304  meter/sec
 ZDOT =       8973
436188                 ZDOT =        2735
103350


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   20140
83449381  
00016717  00000-0  10270-3 0  9150
2 25544  51
6428 128
8086 0001500 324
7319  35
3731 15
49368907 27616


Satellite: ISS
Catalog Number: 25544
Epoch time:      20140
83449381   =   yrday
fracday
Element set:     915
Inclination:       51
6428  deg
RA of node:       128
8086  deg
Eccentricity:     
0001500     
Arg of perigee:   324
7319  deg
Mean anomaly:      35
3731  deg
Mean motion:   15
49368907  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2761
Checksum:              310


Coasting Arc #17 (Orbit 2775)
---------------------------------------

Vector Time (GMT): 2020/141/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4762135
34                 A    =         6793391
60  meter
 Y    =        -370359
96  meter          E    =           
0011057
 Z    =       -4841194
58                 I    =           51
95464
 XDOT =      -2083
970042                 Wp   =           63
50541
 YDOT =       6896
366990  meter/sec      RA   =          123
07133  deg
 ZDOT =      -2577
278893                 TA   =          181
17078
                                          MA   =          181
17337
                                          Ha   =            228
201  n
mi
                                          Hp   =            222
581

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15623803
59                 X    =         4789439
01
 Y    =       -1215091
74  feet           Y    =         -316953
26  meter
 Z    =      -15883184
33                 Z    =        -4817995
33
 XDOT =      -6837
172053                 XDOT =       -2148
413227
 YDOT =      22625
875952  feet/sec       YDOT =        6872
702468  meter/sec
 ZDOT =      -8455
639413                 ZDOT =       -2587
558053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15140364
12                 X    =        -4614782
98
 Y    =       -4441570
83  feet           Y    =        -1353790
79  meter
 Z    =      -15776471
53                 Z    =        -4808668
52
 XDOT =      14038
191194                 XDOT =        4278
840676
 YDOT =     -17646
989868  feet/sec       YDOT =       -5378
802512  meter/sec
 ZDOT =      -8503
187902                 ZDOT =       -2591
771672


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   20141
80198229  
00016717  00000-0  10270-3 0  9161
2 25544  51
6426 124
0199 0001681 327
5793  32
5253 15
49397570 27766


Satellite: ISS
Catalog Number: 25544
Epoch time:      20141
80198229   =   yrday
fracday
Element set:     916
Inclination:       51
6426  deg
RA of node:       124
0199  deg
Eccentricity:     
0001681     
Arg of perigee:   327
5793  deg
Mean anomaly:      32
5253  deg
Mean motion:   15
49397570  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2776
Checksum:              321
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