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

 
Date: September 21st 2020

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ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13864 993 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 431 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


263/20:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 7

267/16:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 7

270/23:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 5

274/02:26:58 371 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 222 7

277/05:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 222 6

277/09:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 6

Coasting Arc #1 (Orbit 647)
---------------------------------------

Vector Time (GMT): 2020/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3161999
50                 A    =         6793093
24  meter
 Y    =       -3068928
77  meter          E    =           
0004849
 Z    =        5166899
16                 I    =           51
26335
 XDOT =       4037
729088                 Wp   =          120
33101
 YDOT =       6378
720029  meter/sec      RA   =          245
69495  deg
 ZDOT =       1314
390221                 TA   =          316
94692
                                          MA   =          316
98484
                                          Ha   =            229
281  n
mi
                                          Hp   =            222
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10374014
09                 X    =         3170984
25
 Y    =      -10068663
96  feet           Y    =        -3033518
26  meter
 Z    =       16951768
90                 Z    =         5182281
10
 XDOT =      13247
142676                 XDOT =        3959
715652
 YDOT =      20927
559150  feet/sec       YDOT =        6423
436745  meter/sec
 ZDOT =       4312
303875                 ZDOT =        1333
813846

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10776954
47                 X    =        -3284815
72
 Y    =        9510175
17  feet           Y    =         2898701
39  meter
 Z    =       17022762
75                 Z    =         5188538
09
 XDOT =     -11396
327729                 XDOT =       -3473
600692
 YDOT =     -20812
876139  feet/sec       YDOT =       -6343
764647  meter/sec
 ZDOT =       4401
815193                 ZDOT =        1341
673271


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   20262
55072138  
00016717  00000-0  10270-3 0  9000
2 25544  51
6397 246
4652 0000624  87
0610 273
0612 15
48939992  6484


Satellite: ISS
Catalog Number: 25544
Epoch time:      20262
55072138   =   yrday
fracday
Element set:     900
Inclination:       51
6397  deg
RA of node:       246
4652  deg
Eccentricity:     
0000624     
Arg of perigee:    87
0610  deg
Mean anomaly:     273
0612  deg
Mean motion:   15
48939992  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             648
Checksum:              308


Coasting Arc #2 (Orbit 662)
---------------------------------------

Vector Time (GMT): 2020/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2888150
18                 A    =         6793100
56  meter
 Y    =        3336820
50  meter          E    =           
0014571
 Z    =       -5177338
36                 I    =           51
27856
 XDOT =      -4568
027208                 Wp   =           80
21409
 YDOT =      -5992
601728  meter/sec      RA   =          240
72435  deg
 ZDOT =      -1314
764102                 TA   =          177
06275
                                          MA   =          177
05418
                                          Ha   =            229
417  n
mi
                                          Hp   =            222
461

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9475558
33                 X    =        -2900100
09
 Y    =       10947573
82  feet           Y    =         3304455
84  meter
 Z    =      -16986018
25                 Z    =        -5191397
32
 XDOT =     -14986
965904                 XDOT =       -4494
290199
 YDOT =     -19660
766823  feet/sec       YDOT =       -6043
272514  meter/sec
 ZDOT =      -4313
530517                 ZDOT =       -1336
774330

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9745148
39                 X    =         2970321
23
 Y    =      -10604667
01  feet           Y    =        -3232302
51  meter
 Z    =      -17050909
50                 Z    =        -5197117
22
 XDOT =      13470
270354                 XDOT =        4105
738404
 YDOT =      19473
273098  feet/sec       YDOT =        5935
453640  meter/sec
 ZDOT =      -4414
994691                 ZDOT =       -1345
690382


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   20263
51847812  
00016717  00000-0  10270-3 0  9017
2 25544  51
6398 241
6783 0000685  84
9141 275
2087 15
48942530  6638


Satellite: ISS
Catalog Number: 25544
Epoch time:      20263
51847812   =   yrday
fracday
Element set:     901
Inclination:       51
6398  deg
RA of node:       241
6783  deg
Eccentricity:     
0000685     
Arg of perigee:    84
9141  deg
Mean anomaly:     275
2087  deg
Mean motion:   15
48942530  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             663
Checksum:              319


Coasting Arc #3 (Orbit 668)
---------------------------------------

Vector Time (GMT): 2020/263/20:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          43010
30                 A    =         6798670
99  meter
 Y    =       -5693205
96  meter          E    =           
0012122
 Z    =        3706108
53                 I    =           51
30469
 XDOT =       5695
067139                 Wp   =           94
23884
 YDOT =       2833
209595  meter/sec      RA   =          239
00507  deg
 ZDOT =       4273
181004                 TA   =          310
10720
                                          MA   =          310
21338
                                          Ha   =            229
319  n
mi
                                          Hp   =            222
684

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         141109
89                 X    =           88667
91
 Y    =      -18678497
25  feet           Y    =        -5692469
38  meter
 Z    =       12159148
71                 Z    =         3706428
83
 XDOT =      18684
603474                 XDOT =        5642
205189
 YDOT =       9295
307070  feet/sec       YDOT =        2896
600713  meter/sec
 ZDOT =      14019
622716                 ZDOT =        4300
717048

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15532169
07                 X    =         4734205
13
 Y    =      -10374028
43  feet           Y    =        -3162003
87  meter
 Z    =       12160687
76                 Z    =         3706577
63
 XDOT =       1901
423124                 XDOT =         579
553768
 YDOT =      19479
889559  feet/sec       YDOT =        5937
470338  meter/sec
 ZDOT =      14146
617237                 ZDOT =        4311
888934


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   20263
90558061  
00016717  00000-0  10270-3 0  9026
2 25544  51
6416 239
7640 0000487  62
1525 297
9674 15
48937273  6690


Satellite: ISS
Catalog Number: 25544
Epoch time:      20263
90558061   =   yrday
fracday
Element set:     902
Inclination:       51
6416  deg
RA of node:       239
7640  deg
Eccentricity:     
0000487     
Arg of perigee:    62
1525  deg
Mean anomaly:     297
9674  deg
Mean motion:   15
48937273  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             669
Checksum:              330


Coasting Arc #4 (Orbit 683)
---------------------------------------

Vector Time (GMT): 2020/264/20:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         443144
67                 A    =         6798617
97  meter
 Y    =        5678699
47  meter          E    =           
0006031
 Z    =       -3717942
46                 I    =           51
32237
 XDOT =      -5910
629315                 Wp   =           79
03259
 YDOT =      -2329
466578  meter/sec      RA   =          234
03651  deg
 ZDOT =      -4267
262756                 TA   =          145
40715
                                          MA   =          145
36790
                                          Ha   =            229
273  n
mi
                                          Hp   =            222
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1453886
70                 X    =          397670
66
 Y    =       18630903
78  feet           Y    =         5683400
54  meter
 Z    =      -12197973
95                 Z    =        -3715900
61
 XDOT =     -19391
828461                 XDOT =       -5863
413052
 YDOT =      -7642
606882  feet/sec       YDOT =       -2395
299731  meter/sec
 ZDOT =     -14000
205892                 ZDOT =       -4295
859802

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14399625
96                 X    =        -4389005
99
 Y    =       11920719
20  feet           Y    =         3633435
21  meter
 Z    =      -12188607
65                 Z    =        -3715087
61
 XDOT =      -3902
954203                 XDOT =       -1189
620441
 YDOT =     -19148
166468  feet/sec       YDOT =       -5836
361140  meter/sec
 ZDOT =     -14132
113499                 ZDOT =       -4307
468195


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   20264
87333706  
00016717  00000-0  10270-3 0  9031
2 25544  51
6409 234
9775 0000330  74
1688 285
9498 15
48949146  6848


Satellite: ISS
Catalog Number: 25544
Epoch time:      20264
87333706   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:       234
9775  deg
Eccentricity:     
0000330     
Arg of perigee:    74
1688  deg
Mean anomaly:     285
9498  deg
Mean motion:   15
48949146  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             684
Checksum:              343


Coasting Arc #5 (Orbit 699)
---------------------------------------

Vector Time (GMT): 2020/265/20:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -951491
78                 A    =         6798652
05  meter
 Y    =       -5616477
16  meter          E    =           
0011954
 Z    =        3701510
39                 I    =           51
34381
 XDOT =       6094
331783                 Wp   =           94
74828
 YDOT =       1798
671330  meter/sec      RA   =          229
06849  deg
 ZDOT =       4282
824584                 TA   =          309
49681
                                          MA   =          309
60246
                                          Ha   =            229
233  n
mi
                                          Hp   =            222
736

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3121692
18                 X    =         -906595
95
 Y    =      -18426762
35  feet           Y    =        -5626866
26  meter
 Z    =       12144062
95                 Z    =         3696997
61
 XDOT =      19994
526847                 XDOT =        6052
961799
 YDOT =       5901
152658  feet/sec       YDOT =        1866
591363  meter/sec
 ZDOT =      14051
261757                 ZDOT =        4312
328257

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13049615
32                 X    =         3977522
75
 Y    =      -13397844
06  feet           Y    =        -4083662
87  meter
 Z    =       12123288
02                 Z    =         3695178
19
 XDOT =       5905
916614                 XDOT =        1800
123384
 YDOT =      18628
671593  feet/sec       YDOT =        5678
019101  meter/sec
 ZDOT =      14187
372963                 ZDOT =        4324
311279


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   20265
90561030  
00016717  00000-0  10270-3 0  9040
2 25544  51
6413 229
8710 0000247  64
2276 295
8899 15
48955980  7002


Satellite: ISS
Catalog Number: 25544
Epoch time:      20265
90561030   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:       229
8710  deg
Eccentricity:     
0000247     
Arg of perigee:    64
2276  deg
Mean anomaly:     295
8899  deg
Mean motion:   15
48955980  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             700
Checksum:              316


Coasting Arc #6 (Orbit 714)
---------------------------------------

Vector Time (GMT): 2020/266/20:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1426827
65                 A    =         6798609
45  meter
 Y    =        5516883
17  meter          E    =           
0006127
 Z    =       -3714252
33                 I    =           51
36565
 XDOT =      -6219
084187                 Wp   =           79
31696
 YDOT =      -1267
350958  meter/sec      RA   =          224
10207  deg
 ZDOT =      -4276
413223                 TA   =          145
03293
                                          MA   =          144
99268
                                          Ha   =            229
304  n
mi
                                          Hp   =            222
651

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4681193
08                 X    =         1383072
04
 Y    =       18100010
41  feet           Y    =         5532594
25  meter
 Z    =      -12185867
21                 Z    =        -3707427
68
 XDOT =     -20403
819510                 XDOT =       -6183
677513
 YDOT =      -4157
975583  feet/sec       YDOT =       -1336
699328  meter/sec
 ZDOT =     -14030
227111                 ZDOT =       -4306
537350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11619894
15                 X    =        -3541743
74
 Y    =       14671999
85  feet           Y    =         4472025
55  meter
 Z    =      -12154414
23                 Z    =        -3704665
46
 XDOT =      -7788
936116                 XDOT =       -2374
067728
 YDOT =     -17893
155093  feet/sec       YDOT =       -5453
833672  meter/sec
 ZDOT =     -14169
224179                 ZDOT =       -4318
779530


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   20266
87336517  
00016717  00000-0  10270-3 0  9058
2 25544  51
6401 225
0838 0000463  74
6037 285
5164 15
48963172  7157


Satellite: ISS
Catalog Number: 25544
Epoch time:      20266
87336517   =   yrday
fracday
Element set:     905
Inclination:       51
6401  deg
RA of node:       225
0838  deg
Eccentricity:     
0000463     
Arg of perigee:    74
6037  deg
Mean anomaly:     285
5164  deg
Mean motion:   15
48963172  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             715
Checksum:              309


Coasting Arc #7 (Orbit 727)
---------------------------------------

Vector Time (GMT): 2020/267/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1919439
88                 A    =         6798861
71  meter
 Y    =        5409183
25  meter          E    =           
0005841
 Z    =       -3650153
27                 I    =           51
39055
 XDOT =      -6257
598677                 Wp   =           81
26940
 YDOT =       -710
571239  meter/sec      RA   =          219
94228  deg
 ZDOT =      -4348
688896                 TA   =          142
10312
                                          MA   =          142
06199
                                          Ha   =            229
309  n
mi
                                          Hp   =            222
706

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6297374
93                 X    =         1876540
57
 Y    =       17746664
21  feet           Y    =         5430407
89  meter
 Z    =      -11975568
46                 Z    =        -3640933
59
 XDOT =     -20530
179385                 XDOT =       -6228
064209
 YDOT =      -2331
270469  feet/sec       YDOT =        -780
383109  meter/sec
 ZDOT =     -14267
352022                 ZDOT =       -4379
014297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18856599
94                 X    =        -5747491
66
 Y    =        -214878
29  feet           Y    =          -65494
90  meter
 Z    =      -11933051
90                 Z    =        -3637194
22
 XDOT =       9299
978666                 XDOT =        2834
633498
 YDOT =     -16958
772595  feet/sec       YDOT =       -5169
033887  meter/sec
 ZDOT =     -14407
298836                 ZDOT =       -4391
344685


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   20267
71208666  
00016717  00000-0  10270-3 0  9066
2 25544  51
6434 220
9383 0000405  73
0441 287
0753 15
48948045  7287


Satellite: ISS
Catalog Number: 25544
Epoch time:      20267
71208666   =   yrday
fracday
Element set:     906
Inclination:       51
6434  deg
RA of node:       220
9383  deg
Eccentricity:     
0000405     
Arg of perigee:    73
0441  deg
Mean anomaly:     287
0753  deg
Mean motion:   15
48948045  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             728
Checksum:              307


Coasting Arc #8 (Orbit 743)
---------------------------------------

Vector Time (GMT): 2020/268/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2397247
09                 A    =         6798937
49  meter
 Y    =       -5215439
66  meter          E    =           
0012430
 Z    =        3633703
82                 I    =           51
41690
 XDOT =       6296
702581                 Wp   =           93
03131
 YDOT =        156
020485  meter/sec      RA   =          214
97965  deg
 ZDOT =       4364
429329                 TA   =          310
14531
                                          MA   =          310
25412
                                          Ha   =            229
391  n
mi
                                          Hp   =            222
664

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7864983
90                 X    =        -2356398
80
 Y    =      -17111022
49  feet           Y    =        -5242018
95  meter
 Z    =       11921600
47                 Z    =         3622158
19
 XDOT =      20658
473034                 XDOT =        6273
289988
 YDOT =        511
878231  feet/sec       YDOT =         226
303873  meter/sec
 ZDOT =      14318
993862                 ZDOT =        4394
959435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18779674
22                 X    =         5724044
70
 Y    =       -1798925
98  feet           Y    =         -548312
64  meter
 Z    =       11868332
73                 Z    =         3617467
82
 XDOT =      -7456
981821                 XDOT =       -2272
888059
 YDOT =      17848
050190  feet/sec       YDOT =        5440
085698  meter/sec
 ZDOT =      14459
909463                 ZDOT =        4407
380404


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   20268
74435885  
00016717  00000-0  10270-3 0  9076
2 25544  51
6429 215
8325 0000537  70
6787 289
4421 15
48940387  7449


Satellite: ISS
Catalog Number: 25544
Epoch time:      20268
74435885   =   yrday
fracday
Element set:     907
Inclination:       51
6429  deg
RA of node:       215
8325  deg
Eccentricity:     
0000537     
Arg of perigee:    70
6787  deg
Mean anomaly:     289
4421  deg
Mean motion:   15
48940387  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             744
Checksum:              339


Coasting Arc #9 (Orbit 758)
---------------------------------------

Vector Time (GMT): 2020/269/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2833214
77                 A    =         6798888
35  meter
 Y    =        4993878
63  meter          E    =           
0005679
 Z    =       -3646931
38                 I    =           51
44557
 XDOT =      -6279
531347                 Wp   =           81
66619
 YDOT =        383
439879  meter/sec      RA   =          210
01918  deg
 ZDOT =      -4358
396788                 TA   =          141
61783
                                          MA   =          141
57741
                                          Ha   =            229
265  n
mi
                                          Hp   =            222
771

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9295324
04                 X    =         2794875
82
 Y    =       16384116
23  feet           Y    =         5025347
22  meter
 Z    =      -11964997
98                 Z    =        -3633261
98
 XDOT =     -20602
136966                 XDOT =       -6262
181817
 YDOT =       1258
004851  feet/sec       YDOT =         313
314573  meter/sec
 ZDOT =     -14299
202060                 ZDOT =       -4388
858111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18509257
42                 X    =        -5641621
66
 Y    =        3708833
39  feet           Y    =         1130452
42  meter
 Z    =      -11901908
87                 Z    =        -3627701
82
 XDOT =       5567
933403                 XDOT =        1697
106101
 YDOT =     -18497
853389  feet/sec       YDOT =       -5638
145713  meter/sec
 ZDOT =     -14439
822481                 ZDOT =       -4401
257892


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   20269
71211108  
00016717  00000-0  10270-3 0  9085
2 25544  51
6432 211
0461 0000274  70
1287 289
9893 15
48948807  7599


Satellite: ISS
Catalog Number: 25544
Epoch time:      20269
71211108   =   yrday
fracday
Element set:     908
Inclination:       51
6432  deg
RA of node:       211
0461  deg
Eccentricity:     
0000274     
Arg of perigee:    70
1287  deg
Mean anomaly:     289
9893  deg
Mean motion:   15
48948807  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             759
Checksum:              318


Coasting Arc #10 (Orbit 774)
---------------------------------------

Vector Time (GMT): 2020/270/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3268693
72                 A    =         6798943
06  meter
 Y    =       -4720018
93  meter          E    =           
0012346
 Z    =        3631586
32                 I    =           51
47573
 XDOT =       6222
678362                 Wp   =           92
54256
 YDOT =       -934
043943  meter/sec      RA   =          205
05978  deg
 ZDOT =       4373
442392                 TA   =          310
55885
                                          MA   =          310
66627
                                          Ha   =            229
364  n
mi
                                          Hp   =            222
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10724060
75                 X    =        -3233310
21
 Y    =      -15485626
43  feet           Y    =        -4756373
84  meter
 Z    =       11914653
28                 Z    =         3615794
46
 XDOT =      20415
611425                 XDOT =        6211
417041
 YDOT =      -3064
448633  feet/sec       YDOT =        -864
520301  meter/sec
 ZDOT =      14348
564279                 ZDOT =        4403
642292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18014421
69                 X    =         5490795
73
 Y    =       -5658861
42  feet           Y    =        -1724820
96  meter
 Z    =       11841746
75                 Z    =         3609364
41
 XDOT =      -3588
711465                 XDOT =       -1093
839254
 YDOT =      18986
118927  feet/sec       YDOT =        5786
969049  meter/sec
 ZDOT =      14487
997352                 ZDOT =        4415
941593


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   20270
74437997  
00016717  00000-0  10270-3 0  9097
2 25544  51
6434 205
9395 0000486  56
7159 303
4038 15
48946908  7753


Satellite: ISS
Catalog Number: 25544
Epoch time:      20270
74437997   =   yrday
fracday
Element set:     909
Inclination:       51
6434  deg
RA of node:       205
9395  deg
Eccentricity:     
0000486     
Arg of perigee:    56
7159  deg
Mean anomaly:     303
4038  deg
Mean motion:   15
48946908  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             775
Checksum:              344


Coasting Arc #11 (Orbit 778)
---------------------------------------

Vector Time (GMT): 2020/270/23:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4612916
49                 A    =         6795382
08  meter
 Y    =        1980080
10  meter          E    =           
0010802
 Z    =       -4590871
04                 I    =           51
47308
 XDOT =      -5090
445608                 Wp   =          111
44476
 YDOT =      -4842
526250  meter/sec      RA   =          203
50030  deg
 ZDOT =       3028
173808                 TA   =          188
93947
                                          MA   =          188
95872
                                          Ha   =            229
302  n
mi
                                          Hp   =            222
472

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15134240
47                 X    =        -4612415
77
 Y    =        6496325
80  feet           Y    =         1928497
77  meter
 Z    =      -15061912
85                 Z    =        -4613277
55
 XDOT =     -16700
937034                 XDOT =       -5050
625765
 YDOT =     -15887
553315  feet/sec       YDOT =       -4899
228490  meter/sec
 ZDOT =       9934
953439                 ZDOT =        3003
543435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14754122
74                 X    =        -4497056
61
 Y    =        7101842
65  feet           Y    =         2164641
64  meter
 Z    =      -15165368
29                 Z    =        -4622404
25
 XDOT =     -16883
169255                 XDOT =       -5145
989989
 YDOT =     -14115
755383  feet/sec       YDOT =       -4302
482241  meter/sec
 ZDOT =       9821
232387                 ZDOT =        2993
511631


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   20271
00244721  
00016717  00000-0  10270-3 0  9100
2 25544  51
6427 204
6591 0000636 128
1407 231
9801 15
48970621  7792


Satellite: ISS
Catalog Number: 25544
Epoch time:      20271
00244721   =   yrday
fracday
Element set:     910
Inclination:       51
6427  deg
RA of node:       204
6591  deg
Eccentricity:     
0000636     
Arg of perigee:   128
1407  deg
Mean anomaly:     231
9801  deg
Mean motion:   15
48970621  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             779
Checksum:              286


Coasting Arc #12 (Orbit 794)
---------------------------------------

Vector Time (GMT): 2020/271/23:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4421657
53                 A    =         6795477
64  meter
 Y    =       -2360974
28  meter          E    =           
0008823
 Z    =        4582677
44                 I    =           51
50445
 XDOT =       5498
315345                 Wp   =           70
37188
 YDOT =       4390
710146  meter/sec      RA   =          198
54436  deg
 ZDOT =      -3035
369744                 TA   =           50
07118
                                          MA   =           49
99368
                                          Ha   =            229
282  n
mi
                                          Hp   =            222
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14506750
42                 X    =         4425470
09
 Y    =       -7745978
61  feet           Y    =        -2311506
54  meter
 Z    =       15035030
97                 Z    =         4604165
44
 XDOT =      18039
092338                 XDOT =        5463
552488
 YDOT =      14405
217014  feet/sec       YDOT =        4452
001696  meter/sec
 ZDOT =      -9958
562151                 ZDOT =       -3008
745886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13931217
21                 X    =         4246235
01
 Y    =       -8565843
73  feet           Y    =        -2610869
17  meter
 Z    =       15134254
43                 Z    =         4612920
75
 XDOT =      18285
415750                 XDOT =        5573
394721
 YDOT =      12316
895849  feet/sec       YDOT =        3754
189855  meter/sec
 ZDOT =      -9835
613453                 ZDOT =       -2997
894981


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   20272
03471612  
00016717  00000-0  10270-3 0  9116
2 25544  51
6425 199
5532 0000752 125
8777 234
2443 15
48939768  7953


Satellite: ISS
Catalog Number: 25544
Epoch time:      20272
03471612   =   yrday
fracday
Element set:     911
Inclination:       51
6425  deg
RA of node:       199
5532  deg
Eccentricity:     
0000752     
Arg of perigee:   125
8777  deg
Mean anomaly:     234
2443  deg
Mean motion:   15
48939768  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             795
Checksum:              323


Coasting Arc #13 (Orbit 809)
---------------------------------------

Vector Time (GMT): 2020/272/23:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4195275
03                 A    =         6795336
00  meter
 Y    =        2743826
17  meter          E    =           
0010790
 Z    =       -4598508
72                 I    =           51
53765
 XDOT =      -5854
888671                 Wp   =          111
81691
 YDOT =      -3886
955314  meter/sec      RA   =          193
59182  deg
 ZDOT =       3024
032458                 TA   =          188
49170
                                          MA   =          188
50997
                                          Ha   =            229
267  n
mi
                                          Hp   =            222
495

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13764025
70                 X    =        -4203308
64
 Y    =        9002054
37  feet           Y    =         2696866
32  meter
 Z    =      -15086970
87                 Z    =        -4618907
41
 XDOT =     -19208
952333                 XDOT =       -5825
677410
 YDOT =     -12752
478063  feet/sec       YDOT =       -3952
265310  meter/sec
 ZDOT =       9921
366332                 ZDOT =        2995
663015

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12946593
51                 X    =        -3946121
70
 Y    =       10000992
09  feet           Y    =         3048302
39  meter
 Z    =      -15181170
91                 Z    =        -4627220
89
 XDOT =     -19449
577118                 XDOT =       -5928
231106
 YDOT =     -10325
610642  feet/sec       YDOT =       -3147
246124  meter/sec
 ZDOT =       9790
336433                 ZDOT =        2984
094545


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   20273
00246576  
00016717  00000-0  10270-3 0  9124
2 25544  51
6434 194
7676 0000623 135
4597 224
6603 15
48979947  8105


Satellite: ISS
Catalog Number: 25544
Epoch time:      20273
00246576   =   yrday
fracday
Element set:     912
Inclination:       51
6434  deg
RA of node:       194
7676  deg
Eccentricity:     
0000623     
Arg of perigee:   135
4597  deg
Mean anomaly:     224
6603  deg
Mean motion:   15
48979947  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             810
Checksum:              323


Coasting Arc #14 (Orbit 825)
---------------------------------------

Vector Time (GMT): 2020/273/23:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3941950
67                 A    =         6795388
74  meter
 Y    =       -3084810
60  meter          E    =           
0008712
 Z    =        4590366
63                 I    =           51
57159
 XDOT =       6177
682438                 Wp   =           69
50724
 YDOT =       3371
592484  meter/sec      RA   =          188
64003  deg
 ZDOT =      -3031
619848                 TA   =           50
86335
                                          MA   =           50
78595
                                          Ha   =            229
212  n
mi
                                          Hp   =            222
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12932909
02                 X    =         3953855
57
 Y    =      -10120769
67  feet           Y    =        -3040661
89  meter
 Z    =       15060257
96                 Z    =         4609544
30
 XDOT =      20267
987000                 XDOT =        6154
247032
 YDOT =      11061
655130  feet/sec       YDOT =        3440
544446  meter/sec
 ZDOT =      -9946
259344                 ZDOT =       -3001
668279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11842150
49                 X    =         3609487
47
 Y    =      -11259576
88  feet           Y    =        -3431919
03  meter
 Z    =       15148824
52                 Z    =         4617361
71
 XDOT =      20447
485858                 XDOT =        6232
393689
 YDOT =       8276
122121  feet/sec       YDOT =        2522
562022  meter/sec
 ZDOT =      -9807
905201                 ZDOT =       -2989
449505


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   20274
03473190  
00016717  00000-0  10270-3 0  9133
2 25544  51
6442 189
6615 0000602 126
4597 233
6608 15
48964273  8265


Satellite: ISS
Catalog Number: 25544
Epoch time:      20274
03473190   =   yrday
fracday
Element set:     913
Inclination:       51
6442  deg
RA of node:       189
6615  deg
Eccentricity:     
0000602     
Arg of perigee:   126
4597  deg
Mean anomaly:     233
6608  deg
Mean motion:   15
48964273  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             826
Checksum:              312


Coasting Arc #15 (Orbit 827)
---------------------------------------

Vector Time (GMT): 2020/274/02:26:58
371
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6293696
83                 A    =         6803572
92  meter
 Y    =       -2090910
16  meter          E    =           
0014197
 Z    =        1488510
07                 I    =           51
60095
 XDOT =       2773
032289                 Wp   =           62
79348
 YDOT =      -4218
190466  meter/sec      RA   =          188
13093  deg
 ZDOT =       5763
568933                 TA   =          313
43326
                                          MA   =          313
55131
                                          Ha   =            229
363  n
mi
                                          Hp   =            222
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20648611
66                 X    =        -6277078
23
 Y    =       -6859941
47  feet           Y    =        -2161197
73  meter
 Z    =        4883563
21                 Z    =         1457978
26
 XDOT =       9097
874964                 XDOT =        2791
999096
 YDOT =     -13839
207564  feet/sec       YDOT =       -4187
073844  meter/sec
 ZDOT =      18909
346893                 ZDOT =        5777
085718

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19450526
79                 X    =        -5928520
56
 Y    =        9821331
18  feet           Y    =         2993541
74  meter
 Z    =        4742532
19                 Z    =         1445523
81
 XDOT =      -2767
065641                 XDOT =        -843
401607
 YDOT =     -14699
883251  feet/sec       YDOT =       -4480
524415  meter/sec
 ZDOT =      18971
762623                 ZDOT =        5782
593248


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   20274
16376505  
00016717  00000-0  10270-3 0  9140
2 25544  51
6430 189
0251 0000477  98
8774 261
2430 15
48941391  8289


Satellite: ISS
Catalog Number: 25544
Epoch time:      20274
16376505   =   yrday
fracday
Element set:     914
Inclination:       51
6430  deg
RA of node:       189
0251  deg
Eccentricity:     
0000477     
Arg of perigee:    98
8774  deg
Mean anomaly:     261
2430  deg
Mean motion:   15
48941391  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             828
Checksum:              313


Coasting Arc #16 (Orbit 842)
---------------------------------------

Vector Time (GMT): 2020/275/02:26:58
371
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6447314
18                 A    =         6803445
66  meter
 Y    =        1551834
65  meter          E    =           
0008789
 Z    =       -1505183
21                 I    =           51
63463
 XDOT =      -2406
403194                 Wp   =          140
15112
 YDOT =       4434
025794  meter/sec      RA   =          183
18246  deg
 ZDOT =      -5761
423828                 TA   =           56
24671
                                          MA   =           56
16300
                                          Ha   =            229
359  n
mi
                                          Hp   =            222
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21152605
57                 X    =         6436793
28
 Y    =        5091321
04  feet           Y    =         1623874
17  meter
 Z    =       -4938265
11                 Z    =        -1473890
20
 XDOT =      -7895
023602                 XDOT =       -2427
821082
 YDOT =      14547
328722  feet/sec       YDOT =        4406
995346  meter/sec
 ZDOT =     -18902
309148                 ZDOT =       -5773
165719

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18353314
16                 X    =         5594090
16
 Y    =      -11743806
60  feet           Y    =        -3579512
25  meter
 Z    =       -4793704
28                 Z    =        -1461121
06
 XDOT =       4247
688479                 XDOT =        1294
695448
 YDOT =      14341
324545  feet/sec       YDOT =        4371
235721  meter/sec
 ZDOT =     -18956
529181                 ZDOT =       -5777
950094


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   20275
13151208  
00016717  00000-0  10270-3 0  9150
2 25544  51
6432 184
2387 0000562  96
5771 263
5443 15
48975923  8439


Satellite: ISS
Catalog Number: 25544
Epoch time:      20275
13151208   =   yrday
fracday
Element set:     915
Inclination:       51
6432  deg
RA of node:       184
2387  deg
Eccentricity:     
0000562     
Arg of perigee:    96
5771  deg
Mean anomaly:     263
5443  deg
Mean motion:   15
48975923  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             843
Checksum:              313


Coasting Arc #17 (Orbit 858)
---------------------------------------

Vector Time (GMT): 2020/276/02:26:58
371
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6561185
50                 A    =         6803602
52  meter
 Y    =        -972140
16  meter          E    =           
0014367
 Z    =        1484310
44                 I    =           51
66762
 XDOT =       1999
240118                 Wp   =           62
66054
 YDOT =      -4626
480105  meter/sec      RA   =          178
23644  deg
 ZDOT =       5770
749919                 TA   =          313
50400
                                          MA   =          313
62332
                                          Ha   =            229
431  n
mi
                                          Hp   =            222
663

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21526199
15                 X    =        -6557037
11
 Y    =       -3189436
21  feet           Y    =        -1045488
70  meter
 Z    =        4869784
90                 Z    =         1452448
60
 XDOT =       6559
186740                 XDOT =        2022
794918
 YDOT =     -15178
740501  feet/sec       YDOT =       -4603
990908  meter/sec
 ZDOT =      18932
906557                 ZDOT =        5780
519205

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17009038
01                 X    =        -5184354
79
 Y    =       13625505
03  feet           Y    =         4153053
93  meter
 Z    =        4722583
72                 Z    =         1439443
52
 XDOT =      -5751
302144                 XDOT =       -1752
996894
 YDOT =     -13800
071829  feet/sec       YDOT =       -4206
261893  meter/sec
 ZDOT =      18978
017881                 ZDOT =        5784
499850


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   20276
16377752  
00016717  00000-0  10270-3 0  9169
2 25544  51
6423 179
1337 0000617  88
0637 272
0583 15
48933826  8598


Satellite: ISS
Catalog Number: 25544
Epoch time:      20276
16377752   =   yrday
fracday
Element set:     916
Inclination:       51
6423  deg
RA of node:       179
1337  deg
Eccentricity:     
0000617     
Arg of perigee:    88
0637  deg
Mean anomaly:     272
0583  deg
Mean motion:   15
48933826  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             859
Checksum:              331


Coasting Arc #18 (Orbit 873)
---------------------------------------

Vector Time (GMT): 2020/277/02:26:58
371
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6619368
09                 A    =         6803432
81  meter
 Y    =         414942
83  meter          E    =           
0008840
 Z    =       -1500945
22                 I    =           51
70201
 XDOT =      -1601
622619                 Wp   =          140
21015
 YDOT =       4775
266696  meter/sec      RA   =          173
29215  deg
 ZDOT =      -5768
675964                 TA   =           56
12469
                                          MA   =           56
04063
                                          Ha   =            229
357  n
mi
                                          Hp   =            222
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21717086
90                 X    =         6621526
95
 Y    =        1361361
00  feet           Y    =          488977
29  meter
 Z    =       -4924360
94                 Z    =        -1468785
23
 XDOT =      -5254
667384                 XDOT =       -1626
880699
 YDOT =      15666
885487  feet/sec       YDOT =        4757
214466  meter/sec
 ZDOT =     -18926
102244                 ZDOT =       -5776
517907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15539267
97                 X    =         4736368
88
 Y    =      -15279321
86  feet           Y    =        -4657137
30  meter
 Z    =       -4775769
30                 Z    =        -1455654
48
 XDOT =       7122
927715                 XDOT =        2171
068367
 YDOT =      13144
139988  feet/sec       YDOT =        4006
333868  meter/sec
 ZDOT =     -18962
314649                 ZDOT =       -5779
713505


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   20277
13152296  
00016717  00000-0  10270-3 0  9172
2 25544  51
6430 174
3469 0000581  99
4889 260
6326 15
48982619  8743


Satellite: ISS
Catalog Number: 25544
Epoch time:      20277
13152296   =   yrday
fracday
Element set:     917
Inclination:       51
6430  deg
RA of node:       174
3469  deg
Eccentricity:     
0000581     
Arg of perigee:    99
4889  deg
Mean anomaly:     260
6326  deg
Mean motion:   15
48982619  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             874
Checksum:              339


Coasting Arc #19 (Orbit 875)
---------------------------------------

Vector Time (GMT): 2020/277/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2449731
15                 A    =         6794678
05  meter
 Y    =        4149289
47  meter          E    =           
0011927
 Z    =       -4801972
06                 I    =           51
67495
 XDOT =      -7093
720262                 Wp   =          107
68648
 YDOT =      -1158
669941  meter/sec      RA   =          172
53360  deg
 ZDOT =       2619
527042                 TA   =          188
18270
                                          MA   =          188
20217
                                          Ha   =            229
364  n
mi
                                          Hp   =            222
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8037175
69                 X    =        -2472622
08
 Y    =       13613154
43  feet           Y    =         4121766
41  meter
 Z    =      -15754501
51                 Z    =        -4813928
04
 XDOT =     -23273
360438                 XDOT =       -7092
960808
 YDOT =      -3801
410568  feet/sec       YDOT =       -1237
992536  meter/sec
 ZDOT =       8594
248826                 ZDOT =        2585
069935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14886513
31                 X    =         4537409
26
 Y    =        5153907
50  feet           Y    =         1570911
01  meter
 Z    =      -15809726
22                 Z    =        -4818804
55
 XDOT =       1147
749922                 XDOT =         349
834176
 YDOT =      22541
041026  feet/sec       YDOT =        6870
509305  meter/sec
 ZDOT =       8435
038128                 ZDOT =        2570
999621


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   20277
26055565  
00016717  00000-0  10270-3 0  9188
2 25544  51
6403 173
7096 0000563  86
6444 273
4771 15
48945586  8767


Satellite: ISS
Catalog Number: 25544
Epoch time:      20277
26055565   =   yrday
fracday
Element set:     918
Inclination:       51
6403  deg
RA of node:       173
7096  deg
Eccentricity:     
0000563     
Arg of perigee:    86
6444  deg
Mean anomaly:     273
4771  deg
Mean motion:   15
48945586  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             876
Checksum:              339


Coasting Arc #20 (Orbit 877)
---------------------------------------

Vector Time (GMT): 2020/277/09:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937176
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5977439
06                 A    =         6802528
51  meter
 Y    =        2501484
50  meter          E    =           
0006802
 Z    =       -2064472
24                 I    =           51
70715
 XDOT =      -3547
012158                 Wp   =           43
73485
 YDOT =      -3913
921632  meter/sec      RA   =          171
86074  deg
 ZDOT =       5543
259854                 TA   =          293
51063
                                          MA   =          293
58210
                                          Ha   =            229
259  n
mi
                                          Hp   =            222
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19611020
55                 X    =        -5994938
97
 Y    =        8206970
14  feet           Y    =         2434542
46  meter
 Z    =       -6773202
90                 Z    =        -2093551
49
 XDOT =     -11637
178997                 XDOT =       -3529
908309
 YDOT =     -12840
950235  feet/sec       YDOT =       -3953
490759  meter/sec
 ZDOT =      18186
548077                 ZDOT =        5526
071457

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21063894
92                 X    =         6420275
17
 Y    =        2533930
86  feet           Y    =          772342
12  meter
 Z    =       -6907553
03                 Z    =        -2105422
16
 XDOT =       4064
071657                 XDOT =        1238
729041
 YDOT =      15438
918388  feet/sec       YDOT =        4705
782325  meter/sec
 ZDOT =      18107
113821                 ZDOT =        5519
048293


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   20277
38958909  
00016717  00000-0  10270-3 0  9196
2 25544  51
6416 173
0715 0000438  71
4028 288
7170 15
48958259  8788


Satellite: ISS
Catalog Number: 25544
Epoch time:      20277
38958909   =   yrday
fracday
Element set:     919
Inclination:       51
6416  deg
RA of node:       173
0715  deg
Eccentricity:     
0000438     
Arg of perigee:    71
4028  deg
Mean anomaly:     288
7170  deg
Mean motion:   15
48958259  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             878
Checksum:              348
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