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

 
Date: July 23rd 2020

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) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 453 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


205/14:26:21 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 221 6

205/17:47:52 000 0 0 0 0 0 0
N/A 0 0 0 0 228 4
000/00:00:00 000 0 0 0 0 221 6

206/00:32:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 221 7

211/13:44:53 073 -1 5 2 2 2 2
N/A 1 6 -0 2 228 4
000/00:05:46 146 0 1 -0 1 223 1

212/08:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 223 0

215/02:37:45 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 223 1

219/03:44:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 223 0

Coasting Arc #1 (Orbit 3748)
---------------------------------------

Vector Time (GMT): 2020/204/13:00:52
427
Vector Time (MET): N/A
Weight (LBS)     : 968616
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         549354
13                 A    =         6790862
66  meter
 Y    =        4182455
99  meter          E    =           
0015744
 Z    =       -5335382
81                 I    =           51
66887
 XDOT =      -7581
467941                 Wp   =           92
29571
 YDOT =       1016
517300  meter/sec      RA   =          172
27062  deg
 ZDOT =         15
661607                 TA   =          177
85722
                                          MA   =          177
85046
                                          Ha   =            228
624  n
mi
                                          Hp   =            221
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1802342
93                 X    =          528459
38
 Y    =       13721968
46  feet           Y    =         4188483
05  meter
 Z    =      -17504536
77                 Z    =        -5332764
59
 XDOT =     -24873
582482                 XDOT =       -7592
347549
 YDOT =       3335
030511  feet/sec       YDOT =         931
675081  meter/sec
 ZDOT =         51
383226                 ZDOT =         -21
191543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8332343
30                 X    =         2539698
24
 Y    =      -11069437
61  feet           Y    =        -3373964
58  meter
 Z    =      -17492549
04                 Z    =        -5331728
95
 XDOT =      19154
302260                 XDOT =        5838
231329
 YDOT =      14602
415903  feet/sec       YDOT =        4450
816367  meter/sec
 ZDOT =       -118
526361                 ZDOT =         -36
126835


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   20204
55848199  
00016717  00000-0  10270-3 0  9004
2 25544  51
6402 173
4011 0001067 122
2027 237
9227 15
49502593 37495


Satellite: ISS
Catalog Number: 25544
Epoch time:      20204
55848199   =   yrday
fracday
Element set:     900
Inclination:       51
6402  deg
RA of node:       173
4011  deg
Eccentricity:     
0001067     
Arg of perigee:   122
2027  deg
Mean anomaly:     237
9227  deg
Mean motion:   15
49502593  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3749
Checksum:              293


Coasting Arc #2 (Orbit 3764)
---------------------------------------

Vector Time (GMT): 2020/205/13:00:52
427
Vector Time (MET): N/A
Weight (LBS)     : 968616
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -684593
26                 A    =         6790820
48  meter
 Y    =       -4155537
17  meter          E    =           
0003263
 Z    =        5324286
50                 I    =           51
70257
 XDOT =       7509
744969                 Wp   =           94
80720
 YDOT =      -1514
012933  meter/sec      RA   =          167
32447  deg
 ZDOT =       -216
222391                 TA   =          357
25209
                                          MA   =          357
25388
                                          Ha   =            228
608  n
mi
                                          Hp   =            221
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2246040
87                 X    =         -663935
61
 Y    =      -13633652
13  feet           Y    =        -4163077
75  meter
 Z    =       17468131
55                 Z    =         5321010
89
 XDOT =      24638
270897                 XDOT =        7527
167238
 YDOT =      -4967
234032  feet/sec       YDOT =       -1429
936170  meter/sec
 ZDOT =       -709
391047                 ZDOT =        -179
701718

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7760188
53                 X    =        -2365305
47
 Y    =       11455361
73  feet           Y    =         3491594
25  meter
 Z    =       17453107
21                 Z    =         5319707
08
 XDOT =     -20351
657518                 XDOT =       -6203
185211
 YDOT =     -12963
330762  feet/sec       YDOT =       -3951
223216  meter/sec
 ZDOT =       -540
981896                 ZDOT =        -164
891282


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   20205
59038393  
00016717  00000-0  10270-3 0  9017
2 25544  51
6406 168
2940 0001005 125
1545 234
9700 15
49515093 37651


Satellite: ISS
Catalog Number: 25544
Epoch time:      20205
59038393   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:       168
2940  deg
Eccentricity:     
0001005     
Arg of perigee:   125
1545  deg
Mean anomaly:     234
9700  deg
Mean motion:   15
49515093  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3765
Checksum:              292


Coasting Arc #3 (Orbit 3765)
---------------------------------------

Vector Time (GMT): 2020/205/14:26:21
000
Vector Time (MET): N/A
Weight (LBS)     : 968616
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3812419
20                 A    =         6793243
73  meter
 Y    =       -2981063
82  meter          E    =           
0008767
 Z    =        4762548
12                 I    =           51
71342
 XDOT =       6199
958748                 Wp   =          119
56014
 YDOT =      -3609
005446  meter/sec      RA   =          167
05351  deg
 ZDOT =       2696
091100                 TA   =          303
77025
                                          MA   =          303
85373
                                          Ha   =            228
639  n
mi
                                          Hp   =            221
627

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12507936
99                 X    =        -3801933
86
 Y    =       -9780393
10  feet           Y    =        -3023638
80  meter
 Z    =       15625157
87                 Z    =         4744054
54
 XDOT =      20341
072009                 XDOT =        6226
759193
 YDOT =     -11840
569047  feet/sec       YDOT =       -3539
523468  meter/sec
 ZDOT =       8845
443241                 ZDOT =        2726
272101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7904385
71                 X    =         2409256
76
 Y    =       13866537
39  feet           Y    =         4226520
60  meter
 Z    =       15539947
33                 Z    =         4736575
95
 XDOT =     -22257
988705                 XDOT =       -6784
234957
 YDOT =       2589
439196  feet/sec       YDOT =         789
261067  meter/sec
 ZDOT =       8984
663156                 ZDOT =        2738
525330


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   20205
65487704  
00016717  00000-0  10270-3 0  9029
2 25544  51
6413 167
9751 0001036 132
7711 227
3527 15
49535134 37660


Satellite: ISS
Catalog Number: 25544
Epoch time:      20205
65487704   =   yrday
fracday
Element set:     902
Inclination:       51
6413  deg
RA of node:       167
9751  deg
Eccentricity:     
0001036     
Arg of perigee:   132
7711  deg
Mean anomaly:     227
3527  deg
Mean motion:   15
49535134  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3766
Checksum:              303


Coasting Arc #4 (Orbit 3767)
---------------------------------------

Vector Time (GMT): 2020/205/17:47:52
000
Vector Time (MET): N/A
Weight (LBS)     : 983050
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2928455
01                 A    =         6794452
28  meter
 Y    =       -4275786
28  meter          E    =           
0009860
 Z    =        4387195
51                 I    =           51
72412
 XDOT =       6769
260636                 Wp   =           74
89691
 YDOT =       1124
430451  meter/sec      RA   =          166
31834  deg
 ZDOT =      -3413
691740                 TA   =           49
71308
                                          MA   =           49
62693
                                          Ha   =            228
390  n
mi
                                          Hp   =            221
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9607792
01                 X    =         2954740
51
 Y    =      -14028170
21  feet           Y    =        -4242891
60  meter
 Z    =       14393686
07                 Z    =         4401483
93
 XDOT =      22208
860354                 XDOT =        6772
765173
 YDOT =       3689
076284  feet/sec       YDOT =        1200
149041  meter/sec
 ZDOT =     -11199
776050                 ZDOT =       -3380
801514

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1814499
11                 X    =         -553059
33
 Y    =       16849441
55  feet           Y    =         5135709
78  meter
 Z    =       14459645
15                 Z    =         4407299
84
 XDOT =     -20180
842605                 XDOT =       -6151
120826
 YDOT =       7332
900448  feet/sec       YDOT =        2235
068056  meter/sec
 ZDOT =     -11048
150652                 ZDOT =       -3367
476319


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   20205
78386362  
00016717  00000-0  10270-3 0  9032
2 25544  51
6429 167
3375 0000839 126
8963 233
2264 15
49556557 37684


Satellite: ISS
Catalog Number: 25544
Epoch time:      20205
78386362   =   yrday
fracday
Element set:     903
Inclination:       51
6429  deg
RA of node:       167
3375  deg
Eccentricity:     
0000839     
Arg of perigee:   126
8963  deg
Mean anomaly:     233
2264  deg
Mean motion:   15
49556557  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3768
Checksum:              340


Coasting Arc #5 (Orbit 3771)
---------------------------------------

Vector Time (GMT): 2020/206/00:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 983050
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3157716
96                 A    =         6792132
63  meter
 Y    =        3279861
50  meter          E    =           
0013322
 Z    =       -5052269
42                 I    =           51
72324
 XDOT =      -6593
603191                 Wp   =           81
38504
 YDOT =       3358
680184  meter/sec      RA   =          164
96521  deg
 ZDOT =      -1943
102015                 TA   =          169
75204
                                          MA   =          169
72486
                                          Ha   =            228
603  n
mi
                                          Hp   =            221
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10359963
77                 X    =         3145346
33
 Y    =       10760700
47  feet           Y    =         3315104
58  meter
 Z    =      -16575687
07                 Z    =        -5036960
61
 XDOT =     -21632
556402                 XDOT =       -6621
232655
 YDOT =      11019
291942  feet/sec       YDOT =        3284
791471  meter/sec
 ZDOT =      -6375
006612                 ZDOT =       -1975
197251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1693809
84                 X    =         -516273
24
 Y    =       14919302
41  feet           Y    =         4547403
37  meter
 Z    =      -16505161
31                 Z    =        -5030773
17
 XDOT =     -21112
290118                 XDOT =       -6435
026028
 YDOT =      -9604
427800  feet/sec       YDOT =       -2927
429593  meter/sec
 ZDOT =      -6523
054838                 ZDOT =       -1988
227115


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   20206
04184098  
00016717  00000-0  10270-3 0  9045
2 25544  51
6412 166
0555 0001395 145
4889 214
6352 15
49514560 37728


Satellite: ISS
Catalog Number: 25544
Epoch time:      20206
04184098   =   yrday
fracday
Element set:     904
Inclination:       51
6412  deg
RA of node:       166
0555  deg
Eccentricity:     
0001395     
Arg of perigee:   145
4889  deg
Mean anomaly:     214
6352  deg
Mean motion:   15
49514560  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3772
Checksum:              307


Coasting Arc #6 (Orbit 3787)
---------------------------------------

Vector Time (GMT): 2020/207/00:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 983050
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3242513
97                 A    =         6791802
95  meter
 Y    =       -3096746
61  meter          E    =           
0006616
 Z    =        5098240
34                 I    =           51
75598
 XDOT =       6413
393382                 Wp   =          130
48880
 YDOT =      -3807
881019  meter/sec      RA   =          160
02099  deg
 ZDOT =       1760
301968                 TA   =          302
47357
                                          MA   =          302
53752
                                          Ha   =            228
589  n
mi
                                          Hp   =            221
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10638169
18                 X    =        -3232408
09
 Y    =      -10159929
82  feet           Y    =        -3132950
52  meter
 Z    =       16726510
30                 Z    =         5082514
14
 XDOT =      21041
316869                 XDOT =        6446
947217
 YDOT =     -12493
047963  feet/sec       YDOT =       -3735
974368  meter/sec
 ZDOT =       5775
268923                 ZDOT =        1791
536392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         798079
85                 X    =          243254
74
 Y    =      -14770806
80  feet           Y    =        -4502141
91  meter
 Z    =       16654047
55                 Z    =         5076153
69
 XDOT =      22031
845374                 XDOT =        6715
306470
 YDOT =       7885
635080  feet/sec       YDOT =        2403
541572  meter/sec
 ZDOT =       5919
372883                 ZDOT =        1804
224855


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   20207
07374062  
00016717  00000-0  10270-3 0  9052
2 25544  51
6424 160
9466 0001325 153
3990 206
7229 15
49546021 37888


Satellite: ISS
Catalog Number: 25544
Epoch time:      20207
07374062   =   yrday
fracday
Element set:     905
Inclination:       51
6424  deg
RA of node:       160
9466  deg
Eccentricity:     
0001325     
Arg of perigee:   153
3990  deg
Mean anomaly:     206
7229  deg
Mean motion:   15
49546021  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3788
Checksum:              304


Coasting Arc #7 (Orbit 3802)
---------------------------------------

Vector Time (GMT): 2020/208/00:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 983050
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3311467
49                 A    =         6791673
52  meter
 Y    =        2941748
67  meter          E    =           
0013986
 Z    =       -5160894
35                 I    =           51
78675
 XDOT =      -6182
864587                 Wp   =           83
43974
 YDOT =       4226
839016  meter/sec      RA   =          155
08007  deg
 ZDOT =      -1559
960152                 TA   =          171
53055
                                          MA   =          171
50692
                                          Ha   =            228
559  n
mi
                                          Hp   =            221
775

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10864394
65                 X    =         3303394
18
 Y    =        9651406
41  feet           Y    =         2978735
01  meter
 Z    =      -16932068
09                 Z    =        -5144828
22
 XDOT =     -20284
988804                 XDOT =       -6222
093558
 YDOT =      13867
582073  feet/sec       YDOT =        4157
478549  meter/sec
 ZDOT =      -5117
979501                 ZDOT =       -1590
088712

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -11519
24                 X    =           -3511
06
 Y    =       14618016
42  feet           Y    =         4455571
41  meter
 Z    =      -16858028
05                 Z    =        -5138326
95
 XDOT =     -22713
479569                 XDOT =       -6923
068573
 YDOT =      -6072
569649  feet/sec       YDOT =       -1850
919229  meter/sec
 ZDOT =      -5257
008979                 ZDOT =       -1602
336337


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   20208
04114781  
00016717  00000-0  10270-3 0  9061
2 25544  51
6426 156
1586 0001315 149
0037 211
1191 15
49514785 38031


Satellite: ISS
Catalog Number: 25544
Epoch time:      20208
04114781   =   yrday
fracday
Element set:     906
Inclination:       51
6426  deg
RA of node:       156
1586  deg
Eccentricity:     
0001315     
Arg of perigee:   149
0037  deg
Mean anomaly:     211
1191  deg
Mean motion:   15
49514785  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3803
Checksum:              286


Coasting Arc #8 (Orbit 3818)
---------------------------------------

Vector Time (GMT): 2020/209/00:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 983050
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3378117
18                 A    =         6791385
19  meter
 Y    =       -2772412
59  meter          E    =           
0005690
 Z    =        5195666
16                 I    =           51
81586
 XDOT =       5934
333153                 Wp   =          131
94470
 YDOT =      -4651
001005  meter/sec      RA   =          150
14026  deg
 ZDOT =       1371
931072                 TA   =          304
86377
                                          MA   =          304
91726
                                          Ha   =            228
591  n
mi
                                          Hp   =            221
669

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11083061
60                 X    =        -3372101
48
 Y    =       -9095841
84  feet           Y    =        -2810155
80  meter
 Z    =       17046148
81                 Z    =         5179271
19
 XDOT =      19469
596959                 XDOT =        5979
236997
 YDOT =     -15259
189649  feet/sec       YDOT =       -4584
388065  meter/sec
 ZDOT =       4501
086194                 ZDOT =        1400
866228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -798705
72                 X    =         -243445
50
 Y    =      -14404900
10  feet           Y    =        -4390613
55  meter
 Z    =       16970583
52                 Z    =         5172633
86
 XDOT =      23314
579573                 XDOT =        7106
283854
 YDOT =       4185
550301  feet/sec       YDOT =        1275
755732  meter/sec
 ZDOT =       4634
639705                 ZDOT =        1412
638182


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   20209
07304659  
00016717  00000-0  10270-3 0  9071
2 25544  51
6422 151
0501 0001324 154
8065 205
3150 15
49545786 38195


Satellite: ISS
Catalog Number: 25544
Epoch time:      20209
07304659   =   yrday
fracday
Element set:     907
Inclination:       51
6422  deg
RA of node:       151
0501  deg
Eccentricity:     
0001324     
Arg of perigee:   154
8065  deg
Mean anomaly:     205
3150  deg
Mean motion:   15
49545786  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3819
Checksum:              290


Coasting Arc #9 (Orbit 3833)
---------------------------------------

Vector Time (GMT): 2020/210/00:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 983050
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3437307
78                 A    =         6791319
13  meter
 Y    =        2630395
70  meter          E    =           
0014413
 Z    =       -5245940
46                 I    =           51
84428
 XDOT =      -5637
613976                 Wp   =           86
16640
 YDOT =       5037
203241  meter/sec      RA   =          145
20338  deg
 ZDOT =      -1170
049790                 TA   =          172
62853
                                          MA   =          172
60732
                                          Ha   =            228
497  n
mi
                                          Hp   =            221
863

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11277256
49                 X    =         3433120
03
 Y    =        8629907
16  feet           Y    =         2668811
14  meter
 Z    =      -17211090
75                 Z    =        -5229253
45
 XDOT =     -18496
108845                 XDOT =       -5687
839101
 YDOT =      16526
257354  feet/sec       YDOT =        4973
878685  meter/sec
 ZDOT =      -3838
746030                 ZDOT =       -1197
556488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1519612
60                 X    =          463177
92
 Y    =       14212122
84  feet           Y    =         4331855
04  meter
 Z    =      -17134170
49                 Z    =        -5222495
17
 XDOT =     -23655
324145                 XDOT =       -7210
142799
 YDOT =      -2244
496075  feet/sec       YDOT =        -684
122404  meter/sec
 ZDOT =      -3965
741562                 ZDOT =       -1208
758028


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   20210
04045380  
00016717  00000-0  10270-3 0  9084
2 25544  51
6426 146
2621 0001290 158
2875 201
8331 15
49510888 38341


Satellite: ISS
Catalog Number: 25544
Epoch time:      20210
04045380   =   yrday
fracday
Element set:     908
Inclination:       51
6426  deg
RA of node:       146
2621  deg
Eccentricity:     
0001290     
Arg of perigee:   158
2875  deg
Mean anomaly:     201
8331  deg
Mean motion:   15
49510888  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3834
Checksum:              289


Coasting Arc #10 (Orbit 3849)
---------------------------------------

Vector Time (GMT): 2020/211/00:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 983050
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3492303
70                 A    =         6791053
07  meter
 Y    =       -2475469
43  meter          E    =           
0004680
 Z    =        5269488
69                 I    =           51
87154
 XDOT =       5325
017777                 Wp   =          132
36064
 YDOT =      -5423
807424  meter/sec      RA   =          140
26688  deg
 ZDOT =        977
514468                 TA   =          308
28638
                                          MA   =          308
32847
                                          Ha   =            228
534  n
mi
                                          Hp   =            221
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11457689
30                 X    =        -3489958
67
 Y    =       -8121618
86  feet           Y    =        -2514510
30  meter
 Z    =       17288348
71                 Z    =         5252530
01
 XDOT =      17470
530766                 XDOT =        5380
524479
 YDOT =     -17794
643779  feet/sec       YDOT =       -5363
949016  meter/sec
 ZDOT =       3207
068466                 ZDOT =        1003
515382

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2254316
76                 X    =         -687115
75
 Y    =      -13959031
82  feet           Y    =        -4254712
90  meter
 Z    =       17210166
32                 Z    =         5245658
69
 XDOT =      23903
480870                 XDOT =        7285
780969
 YDOT =        256
500521  feet/sec       YDOT =          78
181359  meter/sec
 ZDOT =       3327
151787                 ZDOT =        1014
115865


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   20211
07235134  
00016717  00000-0  10270-3 0  9097
2 25544  51
6433 141
1531 0001254 161
5907 198
5289 15
49549352 38506


Satellite: ISS
Catalog Number: 25544
Epoch time:      20211
07235134   =   yrday
fracday
Element set:     909
Inclination:       51
6433  deg
RA of node:       141
1531  deg
Eccentricity:     
0001254     
Arg of perigee:   161
5907  deg
Mean anomaly:     198
5289  deg
Mean motion:   15
49549352  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3850
Checksum:              297


Coasting Arc #11 (Orbit 3857)
---------------------------------------

Vector Time (GMT): 2020/211/13:47:46
146
Vector Time (MET): N/A
Weight (LBS)     : 982807
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1407411
37                 A    =         6792769
34  meter
 Y    =        4200329
50  meter          E    =           
0012508
 Z    =       -5160778
90                 I    =           51
88762
 XDOT =      -6285
118271                 Wp   =          105
79312
 YDOT =       4061
702596  meter/sec      RA   =          137
52318  deg
 ZDOT =       1591
662573                 TA   =          179
53955
                                          MA   =          179
53840
                                          Ha   =            228
442  n
mi
                                          Hp   =            223
058

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4617491
38                 X    =         1385405
32
 Y    =       13780608
61  feet           Y    =         4215945
73  meter
 Z    =      -16931689
31                 Z    =        -5153995
27
 XDOT =     -20620
466769                 XDOT =       -6337
801642
 YDOT =      13325
795920  feet/sec       YDOT =        3991
123163  meter/sec
 ZDOT =       5221
990069                 ZDOT =        1561
004696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1859279
31                 X    =          566708
33
 Y    =      -14450776
37  feet           Y    =        -4404596
64  meter
 Z    =      -16900492
47                 Z    =        -5151270
11
 XDOT =      23367
515587                 XDOT =        7122
418751
 YDOT =      -2935
538046  feet/sec       YDOT =        -894
751996  meter/sec
 ZDOT =       5080
438049                 ZDOT =        1548
517517


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   20211
58830232  
00016717  00000-0  10270-3 0  9105
2 25544  51
6436 138
6025 0001368 245
7139 114
3868 15
49121246 38581


Satellite: ISS
Catalog Number: 25544
Epoch time:      20211
58830232   =   yrday
fracday
Element set:     910
Inclination:       51
6436  deg
RA of node:       138
6025  deg
Eccentricity:     
0001368     
Arg of perigee:   245
7139  deg
Mean anomaly:     114
3868  deg
Mean motion:   15
49121246  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3858
Checksum:              300


Coasting Arc #12 (Orbit 3869)
---------------------------------------

Vector Time (GMT): 2020/212/08:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 982807
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5415589
20                 A    =         6802829
05  meter
 Y    =       -3757005
97  meter          E    =           
0007697
 Z    =       -1669176
88                 I    =           51
93578
 XDOT =       1587
794932                 Wp   =          151
20305
 YDOT =       4826
813345  meter/sec      RA   =          133
81110  deg
 ZDOT =      -5730
250025                 TA   =           46
96528
                                          MA   =           46
90084
                                          Ha   =            228
559  n
mi
                                          Hp   =            223
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17767681
10                 X    =         5465306
48
 Y    =      -12326135
06  feet           Y    =        -3696166
78  meter
 Z    =       -5476302
10                 Z    =        -1642750
08
 XDOT =       5209
300959                 XDOT =        1561
536019
 YDOT =      15836
001789  feet/sec       YDOT =        4844
423102  meter/sec
 ZDOT =     -18800
032892                 ZDOT =       -5722
600391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4581078
39                 X    =        -1396312
69
 Y    =      -21165055
96  feet           Y    =        -6451109
06  meter
 Z    =       -5354260
78                 Z    =        -1631978
68
 XDOT =      15129
198843                 XDOT =        4611
379807
 YDOT =       1457
531672  feet/sec       YDOT =         444
255654  meter/sec
 ZDOT =     -18764
858593                 ZDOT =       -5719
528899


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   20212
36242748  
00016717  00000-0  10270-3 0  9112
2 25544  51
6399 134
7714 0001206 244
7643 115
3382 15
49110851 38707


Satellite: ISS
Catalog Number: 25544
Epoch time:      20212
36242748   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:       134
7714  deg
Eccentricity:     
0001206     
Arg of perigee:   244
7643  deg
Mean anomaly:     115
3382  deg
Mean motion:   15
49110851  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3870
Checksum:              293


Coasting Arc #13 (Orbit 3885)
---------------------------------------

Vector Time (GMT): 2020/213/08:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 982807
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5079378
02                 A    =         6802662
45  meter
 Y    =        4186236
51  meter          E    =           
0012438
 Z    =        1694508
88                 I    =           51
95793
 XDOT =      -1958
453223                 Wp   =           64
32192
 YDOT =      -4703
446958  meter/sec      RA   =          128
88479  deg
 ZDOT =       5721
759054                 TA   =          314
13322
                                          MA   =          314
23545
                                          Ha   =            228
409  n
mi
                                          Hp   =            223
006

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16664626
04                 X    =        -5134043
08
 Y    =       13734371
75  feet           Y    =         4129129
40  meter
 Z    =        5559412
34                 Z    =         1669703
42
 XDOT =      -6425
371468                 XDOT =       -1933
504916
 YDOT =     -15431
256423  feet/sec       YDOT =       -4725
209046  meter/sec
 ZDOT =      18772
175375                 ZDOT =        5712
305769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6658744
39                 X    =         2029585
29
 Y    =       20573402
22  feet           Y    =         6270773
00  meter
 Z    =        5444817
55                 Z    =         1659580
39
 XDOT =     -15258
163946                 XDOT =       -4650
688371
 YDOT =        -42
479700  feet/sec       YDOT =         -12
947813  meter/sec
 ZDOT =      18728
677042                 ZDOT =        5708
500763


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   20213
39459359  
00016717  00000-0  10270-3 0  9125
2 25544  51
6397 129
6658 0001453 242
3007 117
7996 15
49156757 38866


Satellite: ISS
Catalog Number: 25544
Epoch time:      20213
39459359   =   yrday
fracday
Element set:     912
Inclination:       51
6397  deg
RA of node:       129
6658  deg
Eccentricity:     
0001453     
Arg of perigee:   242
3007  deg
Mean anomaly:     117
7996  deg
Mean motion:   15
49156757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3886
Checksum:              345


Coasting Arc #14 (Orbit 3900)
---------------------------------------

Vector Time (GMT): 2020/214/08:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 982807
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4724669
42                 A    =         6802701
63  meter
 Y    =       -4565762
30  meter          E    =           
0007169
 Z    =       -1750189
05                 I    =           51
97897
 XDOT =       2302
912909                 Wp   =          151
64444
 YDOT =       4563
202143  meter/sec      RA   =          123
95858  deg
 ZDOT =      -5703
081114                 TA   =           47
42679
                                          MA   =           47
36632
                                          Ha   =            228
477  n
mi
                                          Hp   =            223
069

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15500883
93                 X    =         4783875
24
 Y    =      -14979535
12  feet           Y    =        -4512596
41  meter
 Z    =       -5742090
07                 Z    =        -1727095
71
 XDOT =       7555
488546                 XDOT =        2279
416406
 YDOT =      14971
135641  feet/sec       YDOT =        4588
824318  meter/sec
 ZDOT =     -18710
896042                 ZDOT =       -5691
951167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8585198
90                 X    =        -2616768
63
 Y    =      -19803345
66  feet           Y    =        -6036059
76  meter
 Z    =       -5635364
55                 Z    =        -1717659
11
 XDOT =      15269
099815                 XDOT =        4654
021623
 YDOT =      -1324
525999  feet/sec       YDOT =        -403
715524  meter/sec
 ZDOT =     -18659
655687                 ZDOT =       -5687
463053


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   20214
36225280  
00016717  00000-0  10270-3 0  9138
2 25544  51
6408 124
8780 0001310 256
1079 103
9926 15
49113050 39013


Satellite: ISS
Catalog Number: 25544
Epoch time:      20214
36225280   =   yrday
fracday
Element set:     913
Inclination:       51
6408  deg
RA of node:       124
8780  deg
Eccentricity:     
0001310     
Arg of perigee:   256
1079  deg
Mean anomaly:     103
9926  deg
Mean motion:   15
49113050  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3901
Checksum:              275


Coasting Arc #15 (Orbit 3912)
---------------------------------------

Vector Time (GMT): 2020/215/02:37:45
000
Vector Time (MET): N/A
Weight (LBS)     : 955249
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4784887
55                 A    =         6800841
80  meter
 Y    =       -3982676
62  meter          E    =           
0004198
 Z    =       -2735476
12                 I    =           51
98949
 XDOT =       1545
091964                 Wp   =          138
30579
 YDOT =       5414
685914  meter/sec      RA   =          120
14215  deg
 ZDOT =      -5188
376925                 TA   =           72
39603
                                          MA   =           72
35019
                                          Ha   =            228
476  n
mi
                                          Hp   =            223
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15698449
97                 X    =         4842354
48
 Y    =      -13066524
36  feet           Y    =        -3928846
95  meter
 Z    =       -8974659
19                 Z    =        -2712094
45
 XDOT =       5069
199356                 XDOT =        1509
630069
 YDOT =      17764
717564  feet/sec       YDOT =        5431
766573  meter/sec
 ZDOT =     -17022
234006                 ZDOT =       -5180
957130

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17843308
76                 X    =         5438640
51
 Y    =      -10035912
89  feet           Y    =        -3058946
25  meter
 Z    =       -8866604
91                 Z    =        -2702541
18
 XDOT =       1190
913240                 XDOT =         362
990355
 YDOT =      17103
855252  feet/sec       YDOT =        5213
255081  meter/sec
 ZDOT =     -16988
145619                 ZDOT =       -5177
986785


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   20215
13637723  
00016717  00000-0  10270-3 0  9144
2 25544  51
6434 121
0479 0001304 252
6736 107
4271 15
49122163 39130


Satellite: ISS
Catalog Number: 25544
Epoch time:      20215
13637723   =   yrday
fracday
Element set:     914
Inclination:       51
6434  deg
RA of node:       121
0479  deg
Eccentricity:     
0001304     
Arg of perigee:   252
6736  deg
Mean anomaly:     107
4271  deg
Mean motion:   15
49122163  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3913
Checksum:              278


Coasting Arc #16 (Orbit 3928)
---------------------------------------

Vector Time (GMT): 2020/216/02:37:45
000
Vector Time (MET): N/A
Weight (LBS)     : 955249
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4431390
90                 A    =         6800864
73  meter
 Y    =        4350082
81  meter          E    =           
0012302
 Z    =        2759437
84                 I    =           52
00473
 XDOT =      -1970
231138                 Wp   =           78
59018
 YDOT =      -5298
723518  meter/sec      RA   =          115
21894  deg
 ZDOT =       5171
989145                 TA   =          312
42710
                                          MA   =          312
53109
                                          Ha   =            228
573  n
mi
                                          Hp   =            223
049

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14538684
07                 X    =        -4493108
90
 Y    =       14271925
22  feet           Y    =         4300182
47  meter
 Z    =        9053273
74                 Z    =         2737762
97
 XDOT =      -6464
012921                 XDOT =       -1935
954700
 YDOT =     -17384
263510  feet/sec       YDOT =       -5320
564913  meter/sec
 ZDOT =      16968
468322                 ZDOT =        5162
501503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16719426
89                 X    =        -5096081
32
 Y    =       11718627
61  feet           Y    =         3571837
70  meter
 Z    =        8953071
01                 Z    =         2728896
05
 XDOT =      -2822
147853                 XDOT =        -860
190666
 YDOT =     -17000
488749  feet/sec       YDOT =       -5181
748971  meter/sec
 ZDOT =      16924
832116                 ZDOT =        5158
688829


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   20216
16854338  
00016717  00000-0  10270-3 0  9152
2 25544  51
6429 115
9420 0001156 262
8247  97
2772 15
49095072 39294


Satellite: ISS
Catalog Number: 25544
Epoch time:      20216
16854338   =   yrday
fracday
Element set:     915
Inclination:       51
6429  deg
RA of node:       115
9420  deg
Eccentricity:     
0001156     
Arg of perigee:   262
8247  deg
Mean anomaly:      97
2772  deg
Mean motion:   15
49095072  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3929
Checksum:              320


Coasting Arc #17 (Orbit 3943)
---------------------------------------

Vector Time (GMT): 2020/217/02:37:45
000
Vector Time (MET): N/A
Weight (LBS)     : 955249
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4066559
32                 A    =         6800644
61  meter
 Y    =       -4669895
81  meter          E    =           
0003843
 Z    =       -2810233
89                 I    =           52
01826
 XDOT =       2372
387266                 Wp   =          132
16974
 YDOT =       5154
825083  meter/sec      RA   =          110
29677  deg
 ZDOT =      -5140
039606                 TA   =           79
45163
                                          MA   =           79
40834
                                          Ha   =            228
462  n
mi
                                          Hp   =            223
058

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13341730
04                 X    =         4132127
39
 Y    =      -15321180
48  feet           Y    =        -4624053
81  meter
 Z    =       -9219927
46                 Z    =        -2790321
78
 XDOT =       7783
422789                 XDOT =        2339
534836
 YDOT =      16912
155785  feet/sec       YDOT =        5181
171513  meter/sec
 ZDOT =     -16863
647002                 ZDOT =       -5128
595192

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15484374
83                 X    =         4719637
45
 Y    =      -13216053
81  feet           Y    =        -4028253
20  meter
 Z    =       -9127839
40                 Z    =        -2782165
45
 XDOT =       4399
000092                 XDOT =        1340
815228
 YDOT =      16748
713149  feet/sec       YDOT =        5105
007768  meter/sec
 ZDOT =     -16810
973313                 ZDOT =       -5123
984666


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   20217
13619820  
00016717  00000-0  10270-3 0  9166
2 25544  51
6435 111
1553 0001231 263
7124  96
3885 15
49126790 39448


Satellite: ISS
Catalog Number: 25544
Epoch time:      20217
13619820   =   yrday
fracday
Element set:     916
Inclination:       51
6435  deg
RA of node:       111
1553  deg
Eccentricity:     
0001231     
Arg of perigee:   263
7124  deg
Mean anomaly:      96
3885  deg
Mean motion:   15
49126790  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3944
Checksum:              298


Coasting Arc #18 (Orbit 3959)
---------------------------------------

Vector Time (GMT): 2020/218/02:37:45
000
Vector Time (MET): N/A
Weight (LBS)     : 955249
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3661284
39                 A    =         6800678
96  meter
 Y    =        4973737
14  meter          E    =           
0012291
 Z    =        2833462
60                 I    =           52
02736
 XDOT =      -2779
378529                 Wp   =           78
88121
 YDOT =      -4973
894963  meter/sec      RA   =          105
37472  deg
 ZDOT =       5123
070887                 TA   =          313
05509
                                          MA   =          313
15795
                                          Ha   =            228
584  n
mi
                                          Hp   =            223
029

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12012087
88                 X    =        -3730393
06
 Y    =       16318035
22  feet           Y    =         4932407
48  meter
 Z    =        9296137
13                 Z    =         2815510
40
 XDOT =      -9118
695962                 XDOT =       -2748
436660
 YDOT =     -16318
553028  feet/sec       YDOT =       -5004
803220  meter/sec
 ZDOT =      16807
975351                 ZDOT =        5109
645005

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14064146
57                 X    =        -4286751
87
 Y    =       14639183
30  feet           Y    =         4462023
07  meter
 Z    =        9213077
01                 Z    =         2808145
87
 XDOT =      -6001
802488                 XDOT =       -1829
349398
 YDOT =     -16339
483204  feet/sec       YDOT =       -4980
274481  meter/sec
 ZDOT =      16746
148721                 ZDOT =        5104
226130


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   20218
16836470  
00016717  00000-0  10270-3 0  9173
2 25544  51
6423 106
0488 0001109 273
7600  86
3423 15
49095271 39603


Satellite: ISS
Catalog Number: 25544
Epoch time:      20218
16836470   =   yrday
fracday
Element set:     917
Inclination:       51
6423  deg
RA of node:       106
0488  deg
Eccentricity:     
0001109     
Arg of perigee:   273
7600  deg
Mean anomaly:      86
3423  deg
Mean motion:   15
49095271  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3960
Checksum:              300


Coasting Arc #19 (Orbit 3974)
---------------------------------------

Vector Time (GMT): 2020/219/02:37:45
000
Vector Time (MET): N/A
Weight (LBS)     : 955249
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3253302
82                 A    =         6800460
12  meter
 Y    =       -5228895
20  meter          E    =           
0003469
 Z    =       -2884352
80                 I    =           52
03617
 XDOT =       3158
144952                 Wp   =          125
10310
 YDOT =       4768
792329  meter/sec      RA   =          100
45366  deg
 ZDOT =      -5089
238005                 TA   =           87
44351
                                          MA   =           87
40380
                                          Ha   =            228
435  n
mi
                                          Hp   =            223
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10673565
69                 X    =         3325542
30
 Y    =      -17155168
00  feet           Y    =        -5192110
44  meter
 Z    =       -9463099
75                 Z    =        -2868374
63
 XDOT =      10361
367953                 XDOT =        3129
304173
 YDOT =      15645
644124  feet/sec       YDOT =        4803
947869  meter/sec
 ZDOT =     -16696
975082                 ZDOT =       -5073
967240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12573973
43                 X    =         3832547
10
 Y    =      -15859204
71  feet           Y    =        -4833885
60  meter
 Z    =       -9389135
65                 Z    =        -2861808
55
 XDOT =       7519
335562                 XDOT =        2291
893479
 YDOT =      15792
932190  feet/sec       YDOT =        4813
685732  meter/sec
 ZDOT =     -16626
626092                 ZDOT =       -5067
795633


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   20219
13601697  
00016717  00000-0  10270-3 0  9183
2 25544  51
6437 101
2618 0001290 276
5105  83
5898 15
49125267 39752


Satellite: ISS
Catalog Number: 25544
Epoch time:      20219
13601697   =   yrday
fracday
Element set:     918
Inclination:       51
6437  deg
RA of node:       101
2618  deg
Eccentricity:     
0001290     
Arg of perigee:   276
5105  deg
Mean anomaly:      83
5898  deg
Mean motion:   15
49125267  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3975
Checksum:              319


Coasting Arc #20 (Orbit 3975)
---------------------------------------

Vector Time (GMT): 2020/219/03:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 955249
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3487671
76                 A    =         6793236
05  meter
 Y    =       -2903630
33  meter          E    =           
0004947
 Z    =        5052948
54                 I    =           52
01060
 XDOT =       2809
124730                 Wp   =           46
40538
 YDOT =      -6844
842831  meter/sec      RA   =          100
18852  deg
 ZDOT =      -1989
864900                 TA   =           62
86032
                                          MA   =           62
80988
                                          Ha   =            228
539  n
mi
                                          Hp   =            223
015

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11442492
65                 X    =        -3479487
02
 Y    =       -9526346
22  feet           Y    =        -2942586
36  meter
 Z    =       16577915
15                 Z    =         5036026
99
 XDOT =       9216
288483                 XDOT =        2895
122423
 YDOT =     -22456
833434  feet/sec       YDOT =       -6812
948283  meter/sec
 ZDOT =      -6528
428150                 ZDOT =       -1976
010953

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13064943
51                 X    =        -3982194
78
 Y    =       -7319182
91  feet           Y    =        -2230886
95  meter
 Z    =       16499878
60                 Z    =         5029163
00
 XDOT =       4586
481058                 XDOT =        1397
959427
 YDOT =     -22793
175970  feet/sec       YDOT =       -6947
360036  meter/sec
 ZDOT =      -6464
215990                 ZDOT =       -1970
293034


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   20219
20052674  
00016717  00000-0  10270-3 0  9197
2 25544  51
6419 100
9425 0001282 278
3099  81
7906 15
49127399 39766


Satellite: ISS
Catalog Number: 25544
Epoch time:      20219
20052674   =   yrday
fracday
Element set:     919
Inclination:       51
6419  deg
RA of node:       100
9425  deg
Eccentricity:     
0001282     
Arg of perigee:   278
3099  deg
Mean anomaly:      81
7906  deg
Mean motion:   15
49127399  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3976
Checksum:              327
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