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

 
Date: September 5th 2020

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ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16464 4774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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


249/11:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 221 8

253/10:08:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 221 8

254/20:33:53 536 0 4 1 4 1 4
N/A -1 4 0 1 229 4
000/00:03:43 072 -0 1 -0 0 222 4

Coasting Arc #1 (Orbit 399)
---------------------------------------

Vector Time (GMT): 2020/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4146439
05                 A    =         6792917
76  meter
 Y    =        1978483
61  meter          E    =           
0006976
 Z    =        4999048
67                 I    =           51
40779
 XDOT =      -5018
715262                 Wp   =          114
94336
 YDOT =       5433
267967  meter/sec      RA   =          325
23733  deg
 ZDOT =       2007
324474                 TA   =          315
45005
                                          MA   =          315
50611
                                          Ha   =            229
106  n
mi
                                          Hp   =            221
834

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13603802
65                 X    =         4099724
74
 Y    =        6491087
95  feet           Y    =         2024591
16  meter
 Z    =       16401078
31                 Z    =         5019076
55
 XDOT =     -16465
601253                 XDOT =       -5088
848978
 YDOT =      17825
682308  feet/sec       YDOT =        5376
753075  meter/sec
 ZDOT =       6585
710218                 ZDOT =        1982
775247

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10678171
47                 X    =        -3254706
67
 Y    =      -10494696
92  feet           Y    =        -3198783
62  meter
 Z    =       16493363
20                 Z    =         5027177
10
 XDOT =      20610
287340                 XDOT =        6282
015581
 YDOT =     -10772
885399  feet/sec       YDOT =       -3283
575470  meter/sec
 ZDOT =       6472
181836                 ZDOT =        1972
721024


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   20246
55183427  
00016717  00000-0  10270-3 0  9006
2 25544  51
6452 325
6138 0001476  80
3768 279
7549 15
49236240  4006


Satellite: ISS
Catalog Number: 25544
Epoch time:      20246
55183427   =   yrday
fracday
Element set:     900
Inclination:       51
6452  deg
RA of node:       325
6138  deg
Eccentricity:     
0001476     
Arg of perigee:    80
3768  deg
Mean anomaly:     279
7549  deg
Mean motion:   15
49236240  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             400
Checksum:              306


Coasting Arc #2 (Orbit 414)
---------------------------------------

Vector Time (GMT): 2020/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4245763
27                 A    =         6792947
74  meter
 Y    =       -1702075
27  meter          E    =           
0014534
 Z    =       -5035309
12                 I    =           51
37907
 XDOT =       4596
075351                 Wp   =           76
07268
 YDOT =      -5807
135072  meter/sec      RA   =          320
27333  deg
 ZDOT =      -1913
671515                 TA   =          175
25823
                                          MA   =          175
24445
                                          Ha   =            229
334  n
mi
                                          Hp   =            221
732

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13929669
53                 X    =        -4201956
24
 Y    =       -5584236
46  feet           Y    =        -1749309
85  meter
 Z    =      -16520043
04                 Z    =        -5055826
61
 XDOT =      15078
987371                 XDOT =        4669
966305
 YDOT =     -19052
280420  feet/sec       YDOT =       -5755
325449  meter/sec
 ZDOT =      -6278
449851                 ZDOT =       -1891
165972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11444108
59                 X    =         3488164
30
 Y    =        9545615
20  feet           Y    =         2909503
51  meter
 Z    =      -16614596
63                 Z    =        -5064129
05
 XDOT =     -19530
990495                 XDOT =       -5953
045903
 YDOT =      12675
749244  feet/sec       YDOT =        3863
568370  meter/sec
 ZDOT =      -6174
350387                 ZDOT =       -1881
941998


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   20247
51943139  
00016717  00000-0  10270-3 0  9018
2 25544  51
6439 320
8269 0001544  80
8223 279
3102 15
49189967  4150


Satellite: ISS
Catalog Number: 25544
Epoch time:      20247
51943139   =   yrday
fracday
Element set:     901
Inclination:       51
6439  deg
RA of node:       320
8269  deg
Eccentricity:     
0001544     
Arg of perigee:    80
8223  deg
Mean anomaly:     279
3102  deg
Mean motion:   15
49189967  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             415
Checksum:              312


Coasting Arc #3 (Orbit 430)
---------------------------------------

Vector Time (GMT): 2020/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4318540
85                 A    =         6792720
87  meter
 Y    =        1404643
75  meter          E    =           
0006705
 Z    =        5047087
41                 I    =           51
35318
 XDOT =      -4155
681721                 Wp   =          115
29927
 YDOT =       6173
192348  meter/sec      RA   =          315
30730  deg
 ZDOT =       1833
035670                 TA   =          316
84200
                                          MA   =          316
89454
                                          Ha   =            229
147  n
mi
                                          Hp   =            221
797

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14168441
10                 X    =         4277997
05
 Y    =        4608411
27  feet           Y    =         1452710
45  meter
 Z    =       16558685
73                 Z    =         5067966
46
 XDOT =     -13634
126380                 XDOT =       -4233
307130
 YDOT =      20253
255735  feet/sec       YDOT =        6126
286642  meter/sec
 ZDOT =       6013
896556                 ZDOT =        1812
660149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12117524
33                 X    =        -3693421
42
 Y    =       -8482428
76  feet           Y    =        -2585444
29  meter
 Z    =       16654916
91                 Z    =         5076418
67
 XDOT =      18336
344069                 XDOT =        5588
917672
 YDOT =     -14541
058533  feet/sec       YDOT =       -4432
114641  meter/sec
 ZDOT =       5919
623690                 ZDOT =        1804
301301


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   20248
55153175  
00016717  00000-0  10270-3 0  9027
2 25544  51
6436 315
7204 0001586  84
1134 276
0197 15
49231543  4317


Satellite: ISS
Catalog Number: 25544
Epoch time:      20248
55153175   =   yrday
fracday
Element set:     902
Inclination:       51
6436  deg
RA of node:       315
7204  deg
Eccentricity:     
0001586     
Arg of perigee:    84
1134  deg
Mean anomaly:     276
0197  deg
Mean motion:   15
49231543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             431
Checksum:              288


Coasting Arc #4 (Orbit 445)
---------------------------------------

Vector Time (GMT): 2020/249/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4031443
11                 A    =         6792053
00  meter
 Y    =        1683446
47  meter          E    =           
0005243
 Z    =        5196712
86                 I    =           51
32867
 XDOT =      -4162
754223                 Wp   =          113
62608
 YDOT =       6326
381389  meter/sec      RA   =          310
48975  deg
 ZDOT =       1176
925928                 TA   =          325
01315
                                          MA   =          325
04759
                                          Ha   =            229
116  n
mi
                                          Hp   =            221
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13226519
39                 X    =         3987076
09
 Y    =        5523118
34  feet           Y    =         1728281
26  meter
 Z    =       17049582
86                 Z    =         5216188
09
 XDOT =     -13657
330129                 XDOT =       -4238
905154
 YDOT =      20755
844451  feet/sec       YDOT =        6279
404786  meter/sec
 ZDOT =       3861
305538                 ZDOT =        1156
519546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9148068
98                 X    =        -2788331
42
 Y    =      -10894511
62  feet           Y    =        -3320647
14  meter
 Z    =       17139322
56                 Z    =         5224065
52
 XDOT =      20848
679103                 XDOT =        6354
677391
 YDOT =     -11564
971046  feet/sec       YDOT =       -3525
003175  meter/sec
 ZDOT =       3766
901239                 ZDOT =        1148
151498


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   20249
51912500  
00016717  00000-0  10270-3 0  9030
2 25544  51
6437 310
9326 0001529  88
8021 271
3304 15
49239958  4465


Satellite: ISS
Catalog Number: 25544
Epoch time:      20249
51912500   =   yrday
fracday
Element set:     903
Inclination:       51
6437  deg
RA of node:       310
9326  deg
Eccentricity:     
0001529     
Arg of perigee:    88
8021  deg
Mean anomaly:     271
3304  deg
Mean motion:   15
49239958  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             446
Checksum:              299


Coasting Arc #5 (Orbit 460)
---------------------------------------

Vector Time (GMT): 2020/250/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4118870
45                 A    =         6792126
52  meter
 Y    =       -1429175
27  meter          E    =           
0015809
 Z    =       -5222180
05                 I    =           51
30679
 XDOT =       3666
622940                 Wp   =           82
23938
 YDOT =      -6625
027429  meter/sec      RA   =          305
51972  deg
 ZDOT =      -1079
594055                 TA   =          177
34588
                                          MA   =          177
33748
                                          Ha   =            229
339  n
mi
                                          Hp   =            221
698

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13513354
50                 X    =        -4077216
47
 Y    =       -4688895
23  feet           Y    =        -1475002
86  meter
 Z    =      -17133136
66                 Z    =        -5242086
67
 XDOT =      12029
602820                 XDOT =        3745
677532
 YDOT =     -21735
654296  feet/sec       YDOT =       -6583
582672  meter/sec
 ZDOT =      -3541
975245                 ZDOT =       -1061
590585

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9958683
78                 X    =         3035406
82
 Y    =       10112822
52  feet           Y    =         3082388
30  meter
 Z    =      -17224874
41                 Z    =        -5250141
72
 XDOT =     -19660
724786                 XDOT =       -5992
588915
 YDOT =      13474
091003  feet/sec       YDOT =        4106
902938  meter/sec
 ZDOT =      -3458
655947                 ZDOT =       -1054
198333


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   20250
48671710  
00016717  00000-0  10270-3 0  9044
2 25544  51
6431 306
1449 0001562  88
4526 271
6803 15
49196025  4616


Satellite: ISS
Catalog Number: 25544
Epoch time:      20250
48671710   =   yrday
fracday
Element set:     904
Inclination:       51
6431  deg
RA of node:       306
1449  deg
Eccentricity:     
0001562     
Arg of perigee:    88
4526  deg
Mean anomaly:     271
6803  deg
Mean motion:   15
49196025  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             461
Checksum:              294


Coasting Arc #6 (Orbit 476)
---------------------------------------

Vector Time (GMT): 2020/251/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4177594
93                 A    =         6791925
52  meter
 Y    =        1159780
84  meter          E    =           
0005007
 Z    =        5224285
71                 I    =           51
28812
 XDOT =      -3159
055575                 Wp   =          111
21360
 YDOT =       6912
313710  meter/sec      RA   =          300
54851  deg
 ZDOT =        989
067511                 TA   =          329
25196
                                          MA   =          329
28128
                                          Ha   =            229
149  n
mi
                                          Hp   =            221
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13706020
12                 X    =         4138938
74
 Y    =        3805055
24  feet           Y    =         1206281
83  meter
 Z    =       17140044
98                 Z    =         5244484
95
 XDOT =     -10364
355562                 XDOT =       -3240
920699
 YDOT =      22678
194587  feet/sec       YDOT =        6876
529202  meter/sec
 ZDOT =       3244
972150                 ZDOT =         973
522807

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10681264
57                 X    =        -3255649
44
 Y    =       -9221929
48  feet           Y    =        -2810844
11  meter
 Z    =       17233141
87                 Z    =         5252661
64
 XDOT =      18370
065164                 XDOT =        5599
195862
 YDOT =     -15332
101238  feet/sec       YDOT =       -4673
224457  meter/sec
 ZDOT =       3172
993995                 ZDOT =         967
128570


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   20251
51881123  
00016717  00000-0  10270-3 0  9051
2 25544  51
6432 301
0380 0001641  89
2550 270
8789 15
49240091  4773


Satellite: ISS
Catalog Number: 25544
Epoch time:      20251
51881123   =   yrday
fracday
Element set:     905
Inclination:       51
6432  deg
RA of node:       301
0380  deg
Eccentricity:     
0001641     
Arg of perigee:    89
2550  deg
Mean anomaly:     270
8789  deg
Mean motion:   15
49240091  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             477
Checksum:              288


Coasting Arc #7 (Orbit 491)
---------------------------------------

Vector Time (GMT): 2020/252/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4234252
96                 A    =         6792003
63  meter
 Y    =        -901643
73  meter          E    =           
0016145
 Z    =       -5247702
08                 I    =           51
27078
 XDOT =       2620
819063                 Wp   =           84
04307
 YDOT =      -7129
958687  meter/sec      RA   =          295
57613  deg
 ZDOT =       -890
366065                 TA   =          177
37913
                                          MA   =          177
37066
                                          Ha   =            229
396  n
mi
                                          Hp   =            221
626

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13891906
04                 X    =        -4198365
35
 Y    =       -2958148
72  feet           Y    =         -948793
71  meter
 Z    =      -17216870
33                 Z    =        -5268183
32
 XDOT =       8598
487738                 XDOT =        2704
678529
 YDOT =     -23392
252911  feet/sec       YDOT =       -7100
181955  meter/sec
 ZDOT =      -2921
148508                 ZDOT =        -877
431153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11354232
02                 X    =         3460769
92
 Y    =        8340108
09  feet           Y    =         2542064
95  meter
 Z    =      -17311277
64                 Z    =        -5276477
43
 XDOT =     -16833
845794                 XDOT =       -5130
956198
 YDOT =      16983
665967  feet/sec       YDOT =        5176
621387  meter/sec
 ZDOT =      -2861
209694                 ZDOT =        -872
096715


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   20252
48640135  
00016717  00000-0  10270-3 0  9065
2 25544  51
6422 296
2505 0001728  92
6543 267
4804 15
49198502  4928


Satellite: ISS
Catalog Number: 25544
Epoch time:      20252
48640135   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:       296
2505  deg
Eccentricity:     
0001728     
Arg of perigee:    92
6543  deg
Mean anomaly:     267
4804  deg
Mean motion:   15
49198502  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             492
Checksum:              307


Coasting Arc #8 (Orbit 506)
---------------------------------------

Vector Time (GMT): 2020/253/10:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2607661
53                 A    =         6803584
25  meter
 Y    =        6272760
92  meter          E    =           
0012886
 Z    =        -257977
72                 I    =           51
29717
 XDOT =      -4342
034342                 Wp   =          131
56583
 YDOT =      -2042
285693  meter/sec      RA   =          290
82960  deg
 ZDOT =      -5971
384024                 TA   =           51
22140
                                          MA   =           51
10635
                                          Ha   =            229
333  n
mi
                                          Hp   =            221
751

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8555319
97                 X    =        -2676358
50
 Y    =       20579924
27  feet           Y    =         6243216
07  meter
 Z    =        -846383
61                 Z    =         -270811
76
 XDOT =     -14245
519494                 XDOT =       -4289
868481
 YDOT =      -6700
412378  feet/sec       YDOT =       -2090
549874  meter/sec
 ZDOT =     -19591
154934                 ZDOT =       -5992
349279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19774918
08                 X    =         6027395
03
 Y    =      -10274982
72  feet           Y    =        -3131814
73  meter
 Z    =        -905810
72                 Z    =         -276091
11
 XDOT =       5756
861183                 XDOT =        1754
691289
 YDOT =      12760
333158  feet/sec       YDOT =        3889
349547  meter/sec
 ZDOT =     -19687
749963                 ZDOT =       -6000
826189


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   20253
45398845  
00016717  00000-0  10270-3 0  9072
2 25544  51
6426 291
4626 0001733  96
8781 263
2566 15
49226103  5074


Satellite: ISS
Catalog Number: 25544
Epoch time:      20253
45398845   =   yrday
fracday
Element set:     907
Inclination:       51
6426  deg
RA of node:       291
4626  deg
Eccentricity:     
0001733     
Arg of perigee:    96
8781  deg
Mean anomaly:     263
2566  deg
Mean motion:   15
49226103  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             507
Checksum:              320


Coasting Arc #9 (Orbit 522)
---------------------------------------

Vector Time (GMT): 2020/254/10:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2103303
12                 A    =         6803676
64  meter
 Y    =       -6455847
04  meter          E    =           
0014010
 Z    =         323595
65                 I    =           51
28664
 XDOT =       4470
267395                 Wp   =           53
48783
 YDOT =       1764
109143  meter/sec      RA   =          285
85627  deg
 ZDOT =       5966
277022                 TA   =          310
00993
                                          MA   =          310
13281
                                          Ha   =            229
411  n
mi
                                          Hp   =            221
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6900600
77                 X    =         2173766
17
 Y    =      -21180600
52  feet           Y    =        -6431932
41  meter
 Z    =        1061665
53                 Z    =          333983
88
 XDOT =      14666
231612                 XDOT =        4421
227523
 YDOT =       5787
759655  feet/sec       YDOT =        1813
824713  meter/sec
 ZDOT =      19574
399677                 ZDOT =        5987
872765

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18686164
17                 X    =        -5695542
84
 Y    =       12122658
76  feet           Y    =         3694986
39  meter
 Z    =        1109809
21                 Z    =          338269
85
 XDOT =      -6766
838150                 XDOT =       -2062
532268
 YDOT =     -12281
257541  feet/sec       YDOT =       -3743
327299  meter/sec
 ZDOT =      19673
917633                 ZDOT =        5996
610095


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   20254
48608038  
00016717  00000-0  10270-3 0  9085
2 25544  51
6430 286
3554 0001747  91
3566 268
7785 15
49189925  5239


Satellite: ISS
Catalog Number: 25544
Epoch time:      20254
48608038   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:       286
3554  deg
Eccentricity:     
0001747     
Arg of perigee:    91
3566  deg
Mean anomaly:     268
7785  deg
Mean motion:   15
49189925  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             523
Checksum:              338


Coasting Arc #10 (Orbit 528)
---------------------------------------

Vector Time (GMT): 2020/254/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3927120
79                 A    =         6792573
85  meter
 Y    =       -1754849
05  meter          E    =           
0015203
 Z    =       -5270447
45                 I    =           51
24493
 XDOT =       2328
279768                 Wp   =           94
81500
 YDOT =      -7253
915047  meter/sec      RA   =          283
68099  deg
 ZDOT =        680
870351                 TA   =          181
73692
                                          MA   =          181
74220
                                          Ha   =            229
352  n
mi
                                          Hp   =            222
393

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12884254
56                 X    =        -3881604
82
 Y    =       -5757378
77  feet           Y    =        -1798510
44  meter
 Z    =      -17291494
27                 Z    =        -5289413
34
 XDOT =       7638
713149                 XDOT =        2405
914901
 YDOT =     -23798
933882  feet/sec       YDOT =       -7227
444468  meter/sec
 ZDOT =       2233
826610                 ZDOT =         692
368814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -998805
14                 X    =         -304435
81
 Y    =      -13968673
08  feet           Y    =        -4257651
56  meter
 Z    =      -17378888
36                 Z    =        -5297085
17
 XDOT =      23544
342458                 XDOT =        7176
315581
 YDOT =      -4527
119118  feet/sec       YDOT =       -1379
865907  meter/sec
 ZDOT =       2287
113189                 ZDOT =         697
112100


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   20254
87311373  
00016717  00000-0  10270-3 0  9092
2 25544  51
6443 284
4426 0000634  84
4296 275
6926 15
48972191  5291


Satellite: ISS
Catalog Number: 25544
Epoch time:      20254
87311373   =   yrday
fracday
Element set:     909
Inclination:       51
6443  deg
RA of node:       284
4426  deg
Eccentricity:     
0000634     
Arg of perigee:    84
4296  deg
Mean anomaly:     275
6926  deg
Mean motion:   15
48972191  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             529
Checksum:              327


Coasting Arc #11 (Orbit 544)
---------------------------------------

Vector Time (GMT): 2020/255/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4057504
90                 A    =         6792480
57  meter
 Y    =        1406005
33  meter          E    =           
0003548
 Z    =        5260153
69                 I    =           51
23746
 XDOT =      -1693
411844                 Wp   =           66
64869
 YDOT =       7442
242038  meter/sec      RA   =          278
70890  deg
 ZDOT =       -681
273344                 TA   =           29
90852
                                          MA   =           29
88825
                                          Ha   =            229
122  n
mi
                                          Hp   =            222
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13312023
94                 X    =         4015930
20
 Y    =        4612878
37  feet           Y    =         1451146
79  meter
 Z    =       17257722
07                 Z    =         5279762
44
 XDOT =      -5555
813136                 XDOT =       -1773
198145
 YDOT =      24416
804586  feet/sec       YDOT =        7422
858981  meter/sec
 ZDOT =      -2235
148768                 ZDOT =        -689
693033

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2446293
70                 X    =          745630
32
 Y    =       13761419
89  feet           Y    =         4194480
78  meter
 Z    =       17348099
87                 Z    =         5287700
84
 XDOT =     -22994
210202                 XDOT =       -7008
635270
 YDOT =       6961
722352  feet/sec       YDOT =        2121
932973  meter/sec
 ZDOT =      -2274
228137                 ZDOT =        -693
184736


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   20255
90538213  
00016717  00000-0  10270-3 0  9103
2 25544  51
6436 279
3372 0000535  85
9083 274
2128 15
48999124  5458


Satellite: ISS
Catalog Number: 25544
Epoch time:      20255
90538213   =   yrday
fracday
Element set:     910
Inclination:       51
6436  deg
RA of node:       279
3372  deg
Eccentricity:     
0000535     
Arg of perigee:    85
9083  deg
Mean anomaly:     274
2128  deg
Mean motion:   15
48999124  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             545
Checksum:              315


Coasting Arc #12 (Orbit 559)
---------------------------------------

Vector Time (GMT): 2020/256/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4172742
44                 A    =         6792550
70  meter
 Y    =       -1046282
71  meter          E    =           
0015112
 Z    =       -5269892
44                 I    =           51
23335
 XDOT =       1037
857779                 Wp   =           94
98723
 YDOT =      -7547
801513  meter/sec      RA   =          273
73635  deg
 ZDOT =        677
153072                 TA   =          181
53006
                                          MA   =          181
53469
                                          Ha   =            229
305  n
mi
                                          Hp   =            222
413

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13690099
86                 X    =        -4135134
50
 Y    =       -3432686
05  feet           Y    =        -1092735
05  meter
 Z    =      -17289673
38                 Z    =        -5290070
52
 XDOT =       3405
045206                 XDOT =        1118
893226
 YDOT =     -24763
128325  feet/sec       YDOT =       -7535
742343  meter/sec
 ZDOT =       2221
630815                 ZDOT =         682
391403

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3892065
07                 X    =        -1186301
43
 Y    =      -13447255
60  feet           Y    =        -4098723
51  meter
 Z    =      -17382695
98                 Z    =        -5298245
74
 XDOT =      22103
310469                 XDOT =        6737
089031
 YDOT =      -9299
058892  feet/sec       YDOT =       -2834
353150  meter/sec
 ZDOT =       2246
022947                 ZDOT =         684
587794


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   20256
87313512  
00016717  00000-0  10270-3 0  9114
2 25544  51
6434 274
5510 0000529  87
4982 272
6229 15
48978226  5606


Satellite: ISS
Catalog Number: 25544
Epoch time:      20256
87313512   =   yrday
fracday
Element set:     911
Inclination:       51
6434  deg
RA of node:       274
5510  deg
Eccentricity:     
0000529     
Arg of perigee:    87
4982  deg
Mean anomaly:     272
6229  deg
Mean motion:   15
48978226  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             560
Checksum:              314


Coasting Arc #13 (Orbit 575)
---------------------------------------

Vector Time (GMT): 2020/257/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4239966
40                 A    =         6792472
73  meter
 Y    =         681746
40  meter          E    =           
0003387
 Z    =        5260075
65                 I    =           51
23273
 XDOT =       -381
029549                 Wp   =           67
02177
 YDOT =       7623
042931  meter/sec      RA   =          268
76329  deg
 ZDOT =       -679
220162                 TA   =           29
51556
                                          MA   =           29
49644
                                          Ha   =            229
065  n
mi
                                          Hp   =            222
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13910650
92                 X    =         4206477
58
 Y    =        2236700
78  feet           Y    =          728973
60  meter
 Z    =       17257466
03                 Z    =         5280590
20
 XDOT =      -1250
096947                 XDOT =        -462
945156
 YDOT =      25009
983368  feet/sec       YDOT =        7618
323952  meter/sec
 ZDOT =      -2228
412605                 ZDOT =        -681
270147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5259222
82                 X    =         1603011
12
 Y    =       12945107
61  feet           Y    =         3945668
80  meter
 Z    =       17352058
60                 Z    =         5288907
46
 XDOT =     -21062
200071                 XDOT =       -6419
758582
 YDOT =      11564
178039  feet/sec       YDOT =        3524
761466  meter/sec
 ZDOT =      -2238
079892                 ZDOT =        -682
166751


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   20257
90540068  
00016717  00000-0  10270-3 0  9128
2 25544  51
6438 269
4453 0000403  92
8482 267
2714 15
49000092  5769


Satellite: ISS
Catalog Number: 25544
Epoch time:      20257
90540068   =   yrday
fracday
Element set:     912
Inclination:       51
6438  deg
RA of node:       269
4453  deg
Eccentricity:     
0000403     
Arg of perigee:    92
8482  deg
Mean anomaly:     267
2714  deg
Mean motion:   15
49000092  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             576
Checksum:              301


Coasting Arc #14 (Orbit 590)
---------------------------------------

Vector Time (GMT): 2020/258/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4290666
31                 A    =         6792522
10  meter
 Y    =        -310749
93  meter          E    =           
0015058
 Z    =       -5269816
75                 I    =           51
23417
 XDOT =       -280
800117                 Wp   =           94
79308
 YDOT =      -7613
626336  meter/sec      RA   =          263
78959  deg
 ZDOT =        678
036035                 TA   =          181
73233
                                          MA   =          181
73755
                                          Ha   =            229
271  n
mi
                                          Hp   =            222
415

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14076989
20                 X    =        -4261275
04
 Y    =       -1019520
75  feet           Y    =         -358567
12  meter
 Z    =      -17289425
04                 Z    =        -5290587
51
 XDOT =       -921
260225                 XDOT =        -198
934863
 YDOT =     -24979
089030  feet/sec       YDOT =       -7616
308677  meter/sec
 ZDOT =       2224
527674                 ZDOT =         676
871193

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6598621
64                 X    =        -2011259
88
 Y    =      -12342517
96  feet           Y    =        -3761999
47  meter
 Z    =      -17385215
24                 Z    =        -5299013
61
 XDOT =      19710
684110                 XDOT =        6007
816517
 YDOT =     -13661
843640  feet/sec       YDOT =       -4164
129941  meter/sec
 ZDOT =       2219
342000                 ZDOT =         676
455442


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   20258
87314890  
00016717  00000-0  10270-3 0  9138
2 25544  51
6432 264
6581 0000481  79
6984 280
4221 15
48986738  5914


Satellite: ISS
Catalog Number: 25544
Epoch time:      20258
87314890   =   yrday
fracday
Element set:     913
Inclination:       51
6432  deg
RA of node:       264
6581  deg
Eccentricity:     
0000481     
Arg of perigee:    79
6984  deg
Mean anomaly:     280
4221  deg
Mean motion:   15
48986738  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             591
Checksum:              336


Coasting Arc #15 (Orbit 606)
---------------------------------------

Vector Time (GMT): 2020/259/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4293948
20                 A    =         6792494
71  meter
 Y    =         -57101
72  meter          E    =           
0003452
 Z    =        5260136
10                 I    =           51
23821
 XDOT =        938
878575                 Wp   =           66
98098
 YDOT =       7574
327611  meter/sec      RA   =          258
81648  deg
 ZDOT =       -682
515015                 TA   =           29
58783
                                          MA   =           29
56830
                                          Ha   =            229
099  n
mi
                                          Hp   =            222
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14087756
57                 X    =         4268717
12
 Y    =        -187341
61  feet           Y    =           -9224
43  meter
 Z    =       17257664
37                 Z    =         5280932
93
 XDOT =       3080
310287                 XDOT =         857
425621
 YDOT =      24850
156203  feet/sec       YDOT =        7584
371344  meter/sec
 ZDOT =      -2239
222489                 ZDOT =        -678
152708

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7824732
37                 X    =         2384978
43
 Y    =       11573829
05  feet           Y    =         3527703
10  meter
 Z    =       17353587
70                 Z    =         5289373
53
 XDOT =     -18227
358998                 XDOT =       -5555
699023
 YDOT =      15658
758872  feet/sec       YDOT =        4772
789704  meter/sec
 ZDOT =      -2219
261517                 ZDOT =        -676
430910


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   20259
90541094  
00016717  00000-0  10270-3 0  9142
2 25544  51
6424 259
5521 0000464  87
1354 272
9849 15
48991850  6079


Satellite: ISS
Catalog Number: 25544
Epoch time:      20259
90541094   =   yrday
fracday
Element set:     914
Inclination:       51
6424  deg
RA of node:       259
5521  deg
Eccentricity:     
0000464     
Arg of perigee:    87
1354  deg
Mean anomaly:     272
9849  deg
Mean motion:   15
48991850  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             607
Checksum:              325


Coasting Arc #16 (Orbit 621)
---------------------------------------

Vector Time (GMT): 2020/260/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4279887
68                 A    =         6792516
17  meter
 Y    =         429953
58  meter          E    =           
0015031
 Z    =       -5270174
00                 I    =           51
24518
 XDOT =      -1588
320339                 Wp   =           95
02001
 YDOT =      -7451
027635  meter/sec      RA   =          253
84329  deg
 ZDOT =        682
397025                 TA   =          181
54682
                                          MA   =          181
55147
                                          Ha   =            229
257  n
mi
                                          Hp   =            222
426

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14041626
24                 X    =        -4258778
14
 Y    =        1410608
87  feet           Y    =          382210
36  meter
 Z    =      -17290597
12                 Z    =        -5290912
65
 XDOT =      -5211
024735                 XDOT =       -1508
197332
 YDOT =     -24445
628725  feet/sec       YDOT =       -7468
341314  meter/sec
 ZDOT =       2238
835383                 ZDOT =         674
876917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9007306
36                 X    =        -2745426
98
 Y    =      -10710189
82  feet           Y    =        -3264465
86  meter
 Z    =      -17386261
81                 Z    =        -5299332
60
 XDOT =      16473
966129                 XDOT =        5021
264876
 YDOT =     -17430
831102  feet/sec       YDOT =       -5312
917320  meter/sec
 ZDOT =       2204
281176                 ZDOT =         671
864902


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   20260
87315675  
00016717  00000-0  10270-3 0  9155
2 25544  51
6416 254
7648 0000443  84
4819 275
6381 15
48988253  6221


Satellite: ISS
Catalog Number: 25544
Epoch time:      20260
87315675   =   yrday
fracday
Element set:     915
Inclination:       51
6416  deg
RA of node:       254
7648  deg
Eccentricity:     
0000443     
Arg of perigee:    84
4819  deg
Mean anomaly:     275
6381  deg
Mean motion:   15
48988253  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             622
Checksum:              330
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