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

 
Date: August 30th 2020

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ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19920 769 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 3
000/00:03:43 072 -0 1 -0 0 222 4

Coasting Arc #1 (Orbit 321)
---------------------------------------

Vector Time (GMT): 2020/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3356679
76                 A    =         6793645
51  meter
 Y    =       -3343249
16  meter          E    =           
0013307
 Z    =       -4881723
70                 I    =           51
56482
 XDOT =       6571
569162                 Wp   =           72
46705
 YDOT =      -3091
711701  meter/sec      RA   =          350
02628  deg
 ZDOT =      -2402
769735                 TA   =          173
90092
                                          MA   =          173
88471
                                          Ha   =            229
271  n
mi
                                          Hp   =            221
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11012728
86                 X    =        -3295332
77
 Y    =      -10968665
21  feet           Y    =        -3380442
77  meter
 Z    =      -16016153
88                 Z    =        -4897880
03
 XDOT =      21560
266280                 XDOT =        6617
324320
 YDOT =     -10143
411094  feet/sec       YDOT =       -3017
967800  meter/sec
 ZDOT =      -7883
102805                 ZDOT =       -2370
737039

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5565443
91                 X    =         1696347
30
 Y    =       14430197
33  feet           Y    =         4398324
15  meter
 Z    =      -16090501
47                 Z    =        -4904384
85
 XDOT =     -22816
164454                 XDOT =       -6954
366926
 YDOT =        180
159168  feet/sec       YDOT =          54
912514  meter/sec
 ZDOT =      -7735
100900                 ZDOT =       -2357
658754


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   20241
52030229  
00016717  00000-0  10270-3 0  9009
2 25544  51
6448 350
5068 0001358  72
9939 287
1360 15
49179357  3228


Satellite: ISS
Catalog Number: 25544
Epoch time:      20241
52030229   =   yrday
fracday
Element set:     900
Inclination:       51
6448  deg
RA of node:       350
5068  deg
Eccentricity:     
0001358     
Arg of perigee:    72
9939  deg
Mean anomaly:     287
1360  deg
Mean motion:   15
49179357  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             322
Checksum:              301


Coasting Arc #2 (Orbit 337)
---------------------------------------

Vector Time (GMT): 2020/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3557914
00                 A    =         6793409
93  meter
 Y    =        3077412
10  meter          E    =           
0007656
 Z    =        4896138
80                 I    =           51
53220
 XDOT =      -6344
084479                 Wp   =          113
16142
 YDOT =       3610
985461  meter/sec      RA   =          345
07229  deg
 ZDOT =       2334
600805                 TA   =          313
91087
                                          MA   =          313
97405
                                          Ha   =            229
130  n
mi
                                          Hp   =            221
886

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11672946
19                 X    =         3499454
80
 Y    =       10096496
39  feet           Y    =         3116872
27  meter
 Z    =       16063447
49                 Z    =         4913279
53
 XDOT =     -20813
925457                 XDOT =       -6395
332058
 YDOT =      11847
065162  feet/sec       YDOT =        3539
754775  meter/sec
 ZDOT =       7659
451459                 ZDOT =        2303
659872

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6758649
36                 X    =        -2060036
32
 Y    =      -13783190
10  feet           Y    =        -4201116
34  meter
 Z    =       16142353
83                 Z    =         4920189
45
 XDOT =      22818
876117                 XDOT =        6955
193440
 YDOT =      -2363
932991  feet/sec       YDOT =        -720
526776  meter/sec
 ZDOT =       7516
466370                 ZDOT =        2291
018950


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   20242
55241598  
00016717  00000-0  10270-3 0  9017
2 25544  51
6456 345
3997 0001426  74
0707 286
0600 15
49221925  3383


Satellite: ISS
Catalog Number: 25544
Epoch time:      20242
55241598   =   yrday
fracday
Element set:     901
Inclination:       51
6456  deg
RA of node:       345
3997  deg
Eccentricity:     
0001426     
Arg of perigee:    74
0707  deg
Mean anomaly:     286
0600  deg
Mean motion:   15
49221925  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             338
Checksum:              304


Coasting Arc #3 (Orbit 352)
---------------------------------------

Vector Time (GMT): 2020/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3736287
05                 A    =         6793404
90  meter
 Y    =       -2822716
06  meter          E    =           
0013741
 Z    =       -4934483
93                 I    =           51
49932
 XDOT =       6058
958703                 Wp   =           73
37900
 YDOT =      -4092
716041  meter/sec      RA   =          340
11708  deg
 ZDOT =      -2247
895665                 TA   =          174
57351
                                          MA   =          174
55861
                                          Ha   =            229
293  n
mi
                                          Hp   =            221
824

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12258159
61                 X    =        -3680476
47
 Y    =       -9260879
46  feet           Y    =        -2864185
82  meter
 Z    =      -16189251
72                 Z    =        -4952497
45
 XDOT =      19878
473436                 XDOT =        6115
193149
 YDOT =     -13427
546065  feet/sec       YDOT =       -4024
645995  meter/sec
 ZDOT =      -7374
985776                 ZDOT =       -2218
327624

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7847255
80                 X    =         2391843
57
 Y    =       13105506
35  feet           Y    =         3994558
34  meter
 Z    =      -16272200
73                 Z    =        -4959766
78
 XDOT =     -22531
090113                 XDOT =       -6867
476266
 YDOT =       4509
303820  feet/sec       YDOT =        1374
435804  meter/sec
 ZDOT =      -7238
320510                 ZDOT =       -2206
240091


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   20243
52002196  
00016717  00000-0  10270-3 0  9025
2 25544  51
6455 340
6132 0001434  73
8175 286
3133 15
49183430  3535


Satellite: ISS
Catalog Number: 25544
Epoch time:      20243
52002196   =   yrday
fracday
Element set:     902
Inclination:       51
6455  deg
RA of node:       340
6132  deg
Eccentricity:     
0001434     
Arg of perigee:    73
8175  deg
Mean anomaly:     286
3133  deg
Mean motion:   15
49183430  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             353
Checksum:              274


Coasting Arc #4 (Orbit 368)
---------------------------------------

Vector Time (GMT): 2020/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3894690
27                 A    =         6793164
20  meter
 Y    =        2539230
90  meter          E    =           
0007343
 Z    =        4948048
02                 I    =           51
46748
 XDOT =      -5752
701182                 Wp   =          114
09172
 YDOT =       4572
616214  meter/sec      RA   =          335
15938  deg
 ZDOT =       2175
982837                 TA   =          314
59668
                                          MA   =          314
65658
                                          Ha   =            229
125  n
mi
                                          Hp   =            221
854

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12777855
20                 X    =         3841972
06
 Y    =        8330810
04  feet           Y    =         2582489
44  meter
 Z    =       16233753
33                 Z    =         4966838
43
 XDOT =     -18873
691542                 XDOT =       -5813
975468
 YDOT =      15002
021701  feet/sec       YDOT =        4507
942828  meter/sec
 ZDOT =       7139
051304                 ZDOT =        2147
890117

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8887070
66                 X    =        -2708779
14
 Y    =      -12283257
50  feet           Y    =        -3743936
89  meter
 Z    =       16320302
91                 Z    =         4974428
33
 XDOT =      22117
803172                 XDOT =        6741
506407
 YDOT =      -6665
804725  feet/sec       YDOT =       -2031
737280  meter/sec
 ZDOT =       7009
182218                 ZDOT =        2136
398740


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   20244
55213190  
00016717  00000-0  10270-3 0  9038
2 25544  51
6453 335
5069 0001468  77
5622 282
5693 15
49228300  3692


Satellite: ISS
Catalog Number: 25544
Epoch time:      20244
55213190   =   yrday
fracday
Element set:     903
Inclination:       51
6453  deg
RA of node:       335
5069  deg
Eccentricity:     
0001468     
Arg of perigee:    77
5622  deg
Mean anomaly:     282
5693  deg
Mean motion:   15
49228300  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             369
Checksum:              304


Coasting Arc #5 (Orbit 383)
---------------------------------------

Vector Time (GMT): 2020/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4034153
45                 A    =         6793186
54  meter
 Y    =       -2269614
56  meter          E    =           
0014043
 Z    =       -4985074
70                 I    =           51
43623
 XDOT =       5393
787027                 Wp   =           74
93367
 YDOT =      -5006
444529  meter/sec      RA   =          330
19971  deg
 ZDOT =      -2086
926492                 TA   =          174
65272
                                          MA   =          174
63771
                                          Ha   =            229
290  n
mi
                                          Hp   =            221
811

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13235411
58                 X    =        -3984259
92
 Y    =       -7446242
00  feet           Y    =        -2314448
59  meter
 Z    =      -16355231
97                 Z    =        -5004549
40
 XDOT =      17696
151663                 XDOT =        5459
506625
 YDOT =     -16425
342944  feet/sec       YDOT =       -4945
759965  meter/sec
 ZDOT =      -6846
871692                 ZDOT =       -2060
566252

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9826309
13                 X    =         2995059
02
 Y    =       11450914
86  feet           Y    =         3490238
85  meter
 Z    =      -16444952
12                 Z    =        -5012421
41
 XDOT =     -21421
421988                 XDOT =       -6529
249422
 YDOT =       8730
723002  feet/sec       YDOT =        2661
124371  meter/sec
 ZDOT =      -6724
990767                 ZDOT =       -2049
777186


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   20245
51973545  
00016717  00000-0  10270-3 0  9043
2 25544  51
6446 330
7203 0001396  80
1934 279
9374 15
49182827  3843


Satellite: ISS
Catalog Number: 25544
Epoch time:      20245
51973545   =   yrday
fracday
Element set:     904
Inclination:       51
6446  deg
RA of node:       330
7203  deg
Eccentricity:     
0001396     
Arg of perigee:    80
1934  deg
Mean anomaly:     279
9374  deg
Mean motion:   15
49182827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             384
Checksum:              320


Coasting Arc #6 (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    =        4149165
28                 A    =         6792930
76  meter
 Y    =        1975554
36  meter          E    =           
0006954
 Z    =        4997989
41                 I    =           51
40783
 XDOT =      -5015
842696                 Wp   =          115
06714
 YDOT =       5434
608906  meter/sec      RA   =          325
23732  deg
 ZDOT =       2010
758621                 TA   =          315
29135
                                          MA   =          315
34739
                                          Ha   =            229
098  n
mi
                                          Hp   =            221
851

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13612746
99                 X    =         4102488
68
 Y    =        6481477
55  feet           Y    =         2021692
60  meter
 Z    =       16397603
04                 Z    =         5018030
63
 XDOT =     -16456
176823                 XDOT =       -5086
008301
 YDOT =      17830
081714  feet/sec       YDOT =        5378
125959  meter/sec
 ZDOT =       6596
977102                 ZDOT =        1986
223270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10689758
86                 X    =        -3258238
50
 Y    =      -10488490
61  feet           Y    =        -3196891
94  meter
 Z    =       16489949
60                 Z    =         5026136
64
 XDOT =      20603
310251                 XDOT =        6279
888965
 YDOT =     -10779
218867  feet/sec       YDOT =       -3285
505911  meter/sec
 ZDOT =       6483
512660                 ZDOT =        1976
174659


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
55184057  
00016717  00000-0  10270-3 0  9051
2 25544  51
6452 325
6136 0001442  80
1900 279
9413 15
49233355  4009


Satellite: ISS
Catalog Number: 25544
Epoch time:      20246
55184057   =   yrday
fracday
Element set:     905
Inclination:       51
6452  deg
RA of node:       325
6136  deg
Eccentricity:     
0001442     
Arg of perigee:    80
1900  deg
Mean anomaly:     279
9413  deg
Mean motion:   15
49233355  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             400
Checksum:              284


Coasting Arc #7 (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    =       -4249019
87                 A    =         6792962
43  meter
 Y    =       -1697939
19  meter          E    =           
0014492
 Z    =       -5033940
09                 I    =           51
37912
 XDOT =       4592
276171                 Wp   =           76
01109
 YDOT =      -5808
676660  meter/sec      RA   =          320
27335  deg
 ZDOT =      -1918
202171                 TA   =          175
27400
                                          MA   =          175
26030
                                          Ha   =            229
327  n
mi
                                          Hp   =            221
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13940353
90                 X    =        -4205265
49
 Y    =       -5570666
65  feet           Y    =        -1745210
48  meter
 Z    =      -16515551
49                 Z    =        -5054473
54
 XDOT =      15066
522871                 XDOT =        4666
206653
 YDOT =     -19057
338124  feet/sec       YDOT =       -5756
909301  meter/sec
 ZDOT =      -6293
314210                 ZDOT =       -1895
714987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11458462
42                 X    =         3492539
35
 Y    =        9535975
69  feet           Y    =         2906565
39  meter
 Z    =      -16610178
85                 Z    =        -5062782
51
 XDOT =     -19521
472194                 XDOT =       -5950
144725
 YDOT =      12683
301870  feet/sec       YDOT =        3865
870410  meter/sec
 ZDOT =      -6189
299349                 ZDOT =       -1886
498442


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
51943958  
00016717  00000-0  10270-3 0  9062
2 25544  51
6440 320
8267 0001511  80
5855 279
5466 15
49186884  4152


Satellite: ISS
Catalog Number: 25544
Epoch time:      20247
51943958   =   yrday
fracday
Element set:     906
Inclination:       51
6440  deg
RA of node:       320
8267  deg
Eccentricity:     
0001511     
Arg of perigee:    80
5855  deg
Mean anomaly:     279
5466  deg
Mean motion:   15
49186884  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             415
Checksum:              328


Coasting Arc #8 (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    =        4322241
26                 A    =         6792737
63  meter
 Y    =        1399173
37  meter          E    =           
0006687
 Z    =        5045485
45                 I    =           51
35323
 XDOT =      -4150
791203                 Wp   =          115
40421
 YDOT =       6174
750741  meter/sec      RA   =          315
30736  deg
 ZDOT =       1838
735375                 TA   =          316
67967
                                          MA   =          316
73223
                                          Ha   =            229
139  n
mi
                                          Hp   =            221
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14180581
57                 X    =         4281766
14
 Y    =        4590463
82  feet           Y    =         1447281
83  meter
 Z    =       16553429
94                 Z    =         5066382
64
 XDOT =     -13618
081374                 XDOT =       -4228
462088
 YDOT =      20258
368572  feet/sec       YDOT =        6127
899471  meter/sec
 ZDOT =       6032
596375                 ZDOT =        1818
383499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12134376
81                 X    =        -3698558
05
 Y    =       -8468776
98  feet           Y    =        -2581283
22  meter
 Z    =       16649745
06                 Z    =         5074842
29
 XDOT =      18323
586095                 XDOT =        5585
029042
 YDOT =     -14549
334228  feet/sec       YDOT =       -4434
637073  meter/sec
 ZDOT =       5938
432492                 ZDOT =        1810
034224


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
55154209  
00016717  00000-0  10270-3 0  9071
2 25544  51
6436 315
7203 0001552  83
8703 276
2624 15
49228175  4311


Satellite: ISS
Catalog Number: 25544
Epoch time:      20248
55154209   =   yrday
fracday
Element set:     907
Inclination:       51
6436  deg
RA of node:       315
7203  deg
Eccentricity:     
0001552     
Arg of perigee:    83
8703  deg
Mean anomaly:     276
2624  deg
Mean motion:   15
49228175  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             431
Checksum:              296


Coasting Arc #9 (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    =        4035927
24                 A    =         6792068
96  meter
 Y    =        1676658
35  meter          E    =           
0005225
 Z    =        5195472
44                 I    =           51
32872
 XDOT =      -4157
230132                 Wp   =          113
79972
 YDOT =       6328
649948  meter/sec      RA   =          310
48985  deg
 ZDOT =       1184
034707                 TA   =          324
76998
                                          MA   =          324
80451
                                          Ha   =            229
109  n
mi
                                          Hp   =            221
822

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13241231
09                 X    =         3991641
82
 Y    =        5500847
62  feet           Y    =         1721543
74  meter
 Z    =       17045513
27                 Z    =         5214969
66
 XDOT =     -13639
206470                 XDOT =       -4233
441371
 YDOT =      20763
287232  feet/sec       YDOT =        6281
734784  meter/sec
 ZDOT =       3884
628305                 ZDOT =        1163
655013

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9171342
53                 X    =        -2795425
20
 Y    =      -10881412
83  feet           Y    =        -3316654
63  meter
 Z    =       17135354
65                 Z    =         5222856
10
 XDOT =      20837
041754                 XDOT =        6351
130327
 YDOT =     -11578
090760  feet/sec       YDOT =       -3529
002064  meter/sec
 ZDOT =       3790
346979                 ZDOT =        1155
297759


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
51913750  
00016717  00000-0  10270-3 0  9083
2 25544  51
6437 310
9325 0001495  88
5855 271
5466 15
49236383  4468


Satellite: ISS
Catalog Number: 25544
Epoch time:      20249
51913750   =   yrday
fracday
Element set:     908
Inclination:       51
6437  deg
RA of node:       310
9325  deg
Eccentricity:     
0001495     
Arg of perigee:    88
5855  deg
Mean anomaly:     271
5466  deg
Mean motion:   15
49236383  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             446
Checksum:              325


Coasting Arc #10 (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    =       -4123560
61                 A    =         6792143
47  meter
 Y    =       -1420672
31  meter          E    =           
0015766
 Z    =       -5220783
60                 I    =           51
30684
 XDOT =       3659
964222                 Wp   =           82
14224
 YDOT =      -6627
348355  meter/sec      RA   =          305
51987  deg
 ZDOT =      -1088
070025                 TA   =          177
36030
                                          MA   =          177
35197
                                          Ha   =            229
333  n
mi
                                          Hp   =            221
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13528742
16                 X    =        -4082008
15
 Y    =       -4660998
40  feet           Y    =        -1466552
92  meter
 Z    =      -17128555
10                 Z    =        -5240713
24
 XDOT =      12007
756633                 XDOT =        3739
086434
 YDOT =     -21743
268882  feet/sec       YDOT =       -6585
977683  meter/sec
 ZDOT =      -3569
783545                 ZDOT =       -1070
098736

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9984817
67                 X    =         3043372
43
 Y    =       10094574
28  feet           Y    =         3076826
24  meter
 Z    =      -17220399
43                 Z    =        -5248777
75
 XDOT =     -19645
971706                 XDOT =       -5988
092176
 YDOT =      13488
564554  feet/sec       YDOT =        4111
314476  meter/sec
 ZDOT =      -3486
612549                 ZDOT =       -1062
719505


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
48673191  
00016717  00000-0  10270-3 0  9094
2 25544  51
6430 306
1447 0001528  88
1696 271
9629 15
49192269  4615


Satellite: ISS
Catalog Number: 25544
Epoch time:      20250
48673191   =   yrday
fracday
Element set:     909
Inclination:       51
6430  deg
RA of node:       306
1447  deg
Eccentricity:     
0001528     
Arg of perigee:    88
1696  deg
Mean anomaly:     271
9629  deg
Mean motion:   15
49192269  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             461
Checksum:              323


Coasting Arc #11 (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    =        4182325
01                 A    =         6791943
77  meter
 Y    =        1149460
72  meter          E    =           
0004991
 Z    =        5222828
55                 I    =           51
28817
 XDOT =      -3151
108809                 Wp   =          111
38938
 YDOT =       6914
477060  meter/sec      RA   =          300
54869  deg
 ZDOT =        999
011192                 TA   =          328
97946
                                          MA   =          329
00892
                                          Ha   =            229
143  n
mi
                                          Hp   =            221
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13721538
76                 X    =         4143790
95
 Y    =        3771196
58  feet           Y    =         1196015
28  meter
 Z    =       17135264
29                 Z    =         5243051
07
 XDOT =     -10338
283495                 XDOT =       -3233
047016
 YDOT =      22685
292192  feet/sec       YDOT =        6878
781010  meter/sec
 ZDOT =       3277
595774                 ZDOT =         983
504912

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10709735
15                 X    =        -3264327
27
 Y    =       -9197894
46  feet           Y    =        -2803518
23  meter
 Z    =       17228468
94                 Z    =         5251237
33
 XDOT =      18351
439938                 XDOT =        5593
518893
 YDOT =     -15347
440177  feet/sec       YDOT =       -4677
899766  meter/sec
 ZDOT =       3205
794718                 ZDOT =         977
126230


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
51882862  
00016717  00000-0  10270-3 0  9108
2 25544  51
6432 301
0379 0001608  88
9115 271
2220 15
49236070  4774


Satellite: ISS
Catalog Number: 25544
Epoch time:      20251
51882862   =   yrday
fracday
Element set:     910
Inclination:       51
6432  deg
RA of node:       301
0379  deg
Eccentricity:     
0001608     
Arg of perigee:    88
9115  deg
Mean anomaly:     271
2220  deg
Mean motion:   15
49236070  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             477
Checksum:              286


Coasting Arc #12 (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    =       -4238759
81                 A    =         6792022
30  meter
 Y    =        -889337
02  meter          E    =           
0016103
 Z    =       -5246150
88                 I    =           51
27084
 XDOT =       2611
607197                 Wp   =           83
91514
 YDOT =      -7131
921540  meter/sec      RA   =          295
57637  deg
 ZDOT =       -901
824408                 TA   =          177
39576
                                          MA   =          177
38737
                                          Ha   =            229
391  n
mi
                                          Hp   =            221
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13906692
28                 X    =        -4203017
01
 Y    =       -2917772
38  feet           Y    =         -936538
21  meter
 Z    =      -17211781
11                 Z    =        -5266654
37
 XDOT =       8568
265081                 XDOT =        2695
544955
 YDOT =     -23398
692717  feet/sec       YDOT =       -7102
247384  meter/sec
 ZDOT =      -2958
741495                 ZDOT =        -888
934054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11384287
83                 X    =         3469930
93
 Y    =        8309341
73  feet           Y    =         2532687
36  meter
 Z    =      -17306291
50                 Z    =        -5274957
65
 XDOT =     -16811
390081                 XDOT =       -5124
111697
 YDOT =      16999
622094  feet/sec       YDOT =        5181
484814  meter/sec
 ZDOT =      -2899
008067                 ZDOT =        -883
617659


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
48642128  
00016717  00000-0  10270-3 0  9115
2 25544  51
6422 296
2504 0001695  92
3356 267
7988 15
49194405  4923


Satellite: ISS
Catalog Number: 25544
Epoch time:      20252
48642128   =   yrday
fracday
Element set:     911
Inclination:       51
6422  deg
RA of node:       296
2504  deg
Eccentricity:     
0001695     
Arg of perigee:    92
3356  deg
Mean anomaly:     267
7988  deg
Mean motion:   15
49194405  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             492
Checksum:              322


Coasting Arc #13 (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    =       -2599177
53                 A    =         6803599
70  meter
 Y    =        6276756
40  meter          E    =           
0012880
 Z    =        -246298
39                 I    =           51
29721
 XDOT =      -4348
480118                 Wp   =          131
54315
 YDOT =      -2026
714987  meter/sec      RA   =          290
82967  deg
 ZDOT =      -5972
001561                 TA   =           51
11780
                                          MA   =           51
00298
                                          Ha   =            229
328  n
mi
                                          Hp   =            221
769

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8527485
32                 X    =        -2667976
54
 Y    =       20593032
82  feet           Y    =         6247305
85  meter
 Z    =        -808065
59                 Z    =         -259091
46
 XDOT =     -14266
667055                 XDOT =       -4296
484895
 YDOT =      -6649
327384  feet/sec       YDOT =       -2075
052203  meter/sec
 ZDOT =     -19593
180974                 ZDOT =       -5992
998542

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19762216
39                 X    =         6023523
56
 Y    =      -10302745
45  feet           Y    =        -3140276
81  meter
 Z    =        -867303
96                 Z    =         -264354
25
 XDOT =       5803
855583                 XDOT =        1769
015182
 YDOT =      12735
697152  feet/sec       YDOT =        3881
840492  meter/sec
 ZDOT =     -19689
922910                 ZDOT =       -6001
488503


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
45401106  
00016717  00000-0  10270-3 0  9123
2 25544  51
6426 291
4625 0001700  96
5616 263
5728 15
49221741  5077


Satellite: ISS
Catalog Number: 25544
Epoch time:      20253
45401106   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:       291
4625  deg
Eccentricity:     
0001700     
Arg of perigee:    96
5616  deg
Mean anomaly:     263
5728  deg
Mean motion:   15
49221741  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             507
Checksum:              284


Coasting Arc #14 (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    =        2093502
82                 A    =         6803694
07  meter
 Y    =       -6459697
60  meter          E    =           
0013970
 Z    =         310508
74                 I    =           51
28668
 XDOT =       4476
120561                 Wp   =           53
24710
 YDOT =       1746
090967  meter/sec      RA   =          285
85636  deg
 ZDOT =       5967
169250                 TA   =          310
10902
                                          MA   =          310
23137
                                          Ha   =            229
407  n
mi
                                          Hp   =            221
806

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6868447
57                 X    =         2164073
23
 Y    =      -21193233
59  feet           Y    =        -6435891
97  meter
 Z    =        1018729
45                 Z    =          320849
62
 XDOT =      14685
434912                 XDOT =        4427
277405
 YDOT =       5728
644905  feet/sec       YDOT =        1795
873092  meter/sec
 ZDOT =      19577
326935                 ZDOT =        5988
793904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18669356
15                 X    =        -5690419
76
 Y    =       12152527
31  feet           Y    =         3704090
32  meter
 Z    =        1066654
96                 Z    =          325116
43
 XDOT =      -6816
769449                 XDOT =       -2077
751328
 YDOT =     -12248
613837  feet/sec       YDOT =       -3733
377497  meter/sec
 ZDOT =      19676
978877                 ZDOT =        5997
543162


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
48610597  
00016717  00000-0  10270-3 0  9134
2 25544  51
6429 286
3553 0001714  90
8432 269
2915 15
49185211  5231


Satellite: ISS
Catalog Number: 25544
Epoch time:      20254
48610597   =   yrday
fracday
Element set:     913
Inclination:       51
6429  deg
RA of node:       286
3553  deg
Eccentricity:     
0001714     
Arg of perigee:    90
8432  deg
Mean anomaly:     269
2915  deg
Mean motion:   15
49185211  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             523
Checksum:              309


Coasting Arc #15 (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    =       -3932482
61                 A    =         6792580
07  meter
 Y    =       -1738067
35  meter          E    =           
0015182
 Z    =       -5272000
26                 I    =           51
24493
 XDOT =       2316
825325                 Wp   =           94
66158
 YDOT =      -7259
025436  meter/sec      RA   =          283
68135  deg
 ZDOT =        665
440739                 TA   =          181
74115
                                          MA   =          181
74645
                                          Ha   =            229
348  n
mi
                                          Hp   =            222
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12901845
82                 X    =        -3887146
35
 Y    =       -5702320
69  feet           Y    =        -1781789
70  meter
 Z    =      -17296588
77                 Z    =        -5290992
63
 XDOT =       7601
132956                 XDOT =        2394
593403
 YDOT =     -23815
700250  feet/sec       YDOT =       -7232
682206  meter/sec
 ZDOT =       2183
204523                 ZDOT =         676
883883

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1055592
67                 X    =         -321744
65
 Y    =      -13957960
70  feet           Y    =        -4254386
42  meter
 Z    =      -17384105
59                 Z    =        -5298675
38
 XDOT =      23542
187659                 XDOT =        7175
658798
 YDOT =      -4563
707574  feet/sec       YDOT =       -1391
018069  meter/sec
 ZDOT =       2236
236198                 ZDOT =         681
604793


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
87314047  
00016717  00000-0  10270-3 0  9149
2 25544  51
6443 284
4425 0000605  82
9024 277
2195 15
48967645  5294


Satellite: ISS
Catalog Number: 25544
Epoch time:      20254
87314047   =   yrday
fracday
Element set:     914
Inclination:       51
6443  deg
RA of node:       284
4425  deg
Eccentricity:     
0000605     
Arg of perigee:    82
9024  deg
Mean anomaly:     277
2195  deg
Mean motion:   15
48967645  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             529
Checksum:              317


Coasting Arc #16 (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    =        4061862
59                 A    =         6792487
23  meter
 Y    =        1386857
03  meter          E    =           
0003499
 Z    =        5261915
32                 I    =           51
23747
 XDOT =      -1680
149080                 Wp   =           66
62791
 YDOT =       7446
772007  meter/sec      RA   =          278
70931  deg
 ZDOT =       -664
023857                 TA   =           29
76267
                                          MA   =           29
74277
                                          Ha   =            229
118  n
mi
                                          Hp   =            222
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13326320
85                 X    =         4020493
14
 Y    =        4550055
86  feet           Y    =         1432048
37  meter
 Z    =       17263501
72                 Z    =         5281545
74
 XDOT =      -5512
300130                 XDOT =       -1760
070810
 YDOT =      24431
666691  feet/sec       YDOT =        7427
536507  meter/sec
 ZDOT =      -2178
555960                 ZDOT =        -672
379449

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2508038
91                 X    =          764450
26
 Y    =       13743050
74  feet           Y    =         4188881
86  meter
 Z    =       17353980
08                 Z    =         5289493
13
 XDOT =     -22987
365848                 XDOT =       -7006
549110
 YDOT =       7002
094796  feet/sec       YDOT =        2134
238494  meter/sec
 ZDOT =      -2217
339905                 ZDOT =        -675
845203


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
90541204  
00016717  00000-0  10270-3 0  9152
2 25544  51
6436 279
3372 0000507  84
0225 276
0983 15
48994169  5458


Satellite: ISS
Catalog Number: 25544
Epoch time:      20255
90541204   =   yrday
fracday
Element set:     915
Inclination:       51
6436  deg
RA of node:       279
3372  deg
Eccentricity:     
0000507     
Arg of perigee:    84
0225  deg
Mean anomaly:     276
0983  deg
Mean motion:   15
48994169  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             545
Checksum:              314
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