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

 
Date: August 3rd 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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


219/03:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 0
000/00:00:00 000 0 0 0 0 222 5

223/13:37:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 0
000/00:00:00 000 0 0 0 0 222 5

Coasting Arc #1 (Orbit 3934)
---------------------------------------

Vector Time (GMT): 2020/216/12:38:59
863
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3891404
66                 A    =         6802409
85  meter
 Y    =       -5225099
14  meter          E    =           
0006140
 Z    =       -1950320
12                 I    =           52
01810
 XDOT =       2942
167937                 Wp   =          136
66916
 YDOT =       4284
404724  meter/sec      RA   =          113
15999  deg
 ZDOT =      -5622
751432                 TA   =           64
66744
                                          MA   =           64
60386
                                          Ha   =            228
893  n
mi
                                          Hp   =            222
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12767075
66                 X    =         3959017
35
 Y    =      -17142713
73  feet           Y    =        -5181204
46  meter
 Z    =       -6398688
06                 Z    =        -1931253
96
 XDOT =       9652
781946                 XDOT =        2921
351147
 YDOT =      14056
445945  feet/sec       YDOT =        4317
190259  meter/sec
 ZDOT =     -18447
347219                 ZDOT =       -5608
510089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20706789
85                 X    =        -6311429
55
 Y    =        5405604
71  feet           Y    =         1647628
31  meter
 Z    =       -6310495
64                 Z    =        -1923439
07
 XDOT =       1520
893436                 XDOT =         463
568319
 YDOT =     -15575
321374  feet/sec       YDOT =       -4747
357955  meter/sec
 ZDOT =     -18381
732072                 ZDOT =       -5602
751936


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
55558371  
00016717  00000-0  10270-3 0  9007
2 25544  51
6449 114
0295 0000952 347
7131  12
3996 15
49104665 39356


Satellite: ISS
Catalog Number: 25544
Epoch time:      20216
55558371   =   yrday
fracday
Element set:     900
Inclination:       51
6449  deg
RA of node:       114
0295  deg
Eccentricity:     
0000952     
Arg of perigee:   347
7131  deg
Mean anomaly:      12
3996  deg
Mean motion:   15
49104665  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3935
Checksum:              307


Coasting Arc #2 (Orbit 3950)
---------------------------------------

Vector Time (GMT): 2020/217/12:38:59
863
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3443456
52                 A    =         6802299
33  meter
 Y    =        5513265
17  meter          E    =           
0014264
 Z    =        1979684
73                 I    =           52
02952
 XDOT =      -3270
905071                 Wp   =           63
35682
 YDOT =      -4066
738040  meter/sec      RA   =          108
23761  deg
 ZDOT =       5611
226709                 TA   =          318
33229
                                          MA   =          318
44086
                                          Ha   =            228
922  n
mi
                                          Hp   =            222
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11297429
52                 X    =        -3514467
49
 Y    =       18088140
31  feet           Y    =         5474360
80  meter
 Z    =        6495028
64                 Z    =         1962786
12
 XDOT =     -10731
315851                 XDOT =       -3252
441873
 YDOT =     -13342
316404  feet/sec       YDOT =       -4103
212772  meter/sec
 ZDOT =      18409
536448                 ZDOT =        5595
382942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20024157
08                 X    =         6103363
08
 Y    =       -7406460
68  feet           Y    =        -2257489
22  meter
 Z    =        6416821
97                 Z    =         1955847
34
 XDOT =        -82
755546                 XDOT =         -25
223890
 YDOT =      15734
368411  feet/sec       YDOT =        4795
835492  meter/sec
 ZDOT =      18336
514761                 ZDOT =        5588
969699


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
58773727  
00016717  00000-0  10270-3 0  9016
2 25544  51
6444 108
9230 0001159 353
6538   6
4597 15
49126840 39517


Satellite: ISS
Catalog Number: 25544
Epoch time:      20217
58773727   =   yrday
fracday
Element set:     901
Inclination:       51
6444  deg
RA of node:       108
9230  deg
Eccentricity:     
0001159     
Arg of perigee:   353
6538  deg
Mean anomaly:       6
4597  deg
Mean motion:   15
49126840  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3951
Checksum:              317


Coasting Arc #3 (Orbit 3965)
---------------------------------------

Vector Time (GMT): 2020/218/12:38:59
863
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2999243
96                 A    =         6802226
29  meter
 Y    =       -5751598
92  meter          E    =           
0005777
 Z    =       -2042869
21                 I    =           52
03903
 XDOT =       3567
369268                 Wp   =          135
04935
 YDOT =       3838
289361  meter/sec      RA   =          103
31661  deg
 ZDOT =      -5582
659031                 TA   =           67
34619
                                          MA   =           67
28511
                                          Ha   =            228
871  n
mi
                                          Hp   =            222
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9840039
25                 X    =         3073259
99
 Y    =      -18870075
21  feet           Y    =        -5717645
30  meter
 Z    =       -6702326
81                 Z    =        -2028120
92
 XDOT =      11703
967414                 XDOT =        3551
299894
 YDOT =      12592
812864  feet/sec       YDOT =        3878
092625  meter/sec
 ZDOT =     -18315
810469                 ZDOT =       -5565
369459

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19191894
02                 X    =        -5849689
30
 Y    =        9245980
00  feet           Y    =         2818174
70  meter
 Z    =       -6634029
92                 Z    =        -2022052
32
 XDOT =      -1306
015977                 XDOT =        -398
073670
 YDOT =     -15763
074377  feet/sec       YDOT =       -4804
585070  meter/sec
 ZDOT =     -18236
105668                 ZDOT =       -5558
365008


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
55537890  
00016717  00000-0  10270-3 0  9024
2 25544  51
6448 104
1363 0001027 346
9162  13
1961 15
49111412 39663


Satellite: ISS
Catalog Number: 25544
Epoch time:      20218
55537890   =   yrday
fracday
Element set:     902
Inclination:       51
6448  deg
RA of node:       104
1363  deg
Eccentricity:     
0001027     
Arg of perigee:   346
9162  deg
Mean anomaly:      13
1961  deg
Mean motion:   15
49111412  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3966
Checksum:              291


Coasting Arc #4 (Orbit 3975)
---------------------------------------

Vector Time (GMT): 2020/219/03:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2786439
47                 A    =         6795399
97  meter
 Y    =       -4277494
64  meter          E    =           
0009654
 Z    =        4480059
85                 I    =           52
01879
 XDOT =       3670
471922                 Wp   =           63
70393
 YDOT =      -5859
816734  meter/sec      RA   =          100
16856  deg
 ZDOT =      -3302
304455                 TA   =           59
48892
                                          MA   =           59
39365
                                          Ha   =            228
976  n
mi
                                          Hp   =            222
450

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9141861
78                 X    =        -2760161
19
 Y    =      -14033775
06  feet           Y    =        -4308507
81  meter
 Z    =       14698359
10                 Z    =         4466588
44
 XDOT =      12042
230715                 XDOT =        3751
765668
 YDOT =     -19225
120520  feet/sec       YDOT =       -5818
316247  meter/sec
 ZDOT =     -10834
332203                 ZDOT =       -3284
277916

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11774772
86                 X    =        -3588950
77
 Y    =      -11987310
96  feet           Y    =        -3653732
38  meter
 Z    =       14636302
11                 Z    =         4461144
88
 XDOT =       7306
727068                 XDOT =        2227
090410
 YDOT =     -20342
675852  feet/sec       YDOT =       -6200
447600  meter/sec
 ZDOT =     -10750
886760                 ZDOT =       -3276
870284


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
20047024  
00016717  00000-0  10270-3 0  9033
2 25544  51
6423 100
9426 0001046   5
8970 354
2192 15
49165556 39763


Satellite: ISS
Catalog Number: 25544
Epoch time:      20219
20047024   =   yrday
fracday
Element set:     903
Inclination:       51
6423  deg
RA of node:       100
9426  deg
Eccentricity:     
0001046     
Arg of perigee:     5
8970  deg
Mean anomaly:     354
2192  deg
Mean motion:   15
49165556  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3976
Checksum:              290


Coasting Arc #5 (Orbit 3990)
---------------------------------------

Vector Time (GMT): 2020/220/03:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3126120
50                 A    =         6795622
79  meter
 Y    =        4068731
20  meter          E    =           
0009061
 Z    =       -4464514
79                 I    =           52
02324
 XDOT =      -3180
062887                 Wp   =          103
49841
 YDOT =       6105
640367  meter/sec      RA   =           95
24762  deg
 ZDOT =       3341
278300                 TA   =          200
12104
                                          MA   =          200
15678
                                          Ha   =            229
037  n
mi
                                          Hp   =            222
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10256300
86                 X    =         3102076
00
 Y    =       13348855
63  feet           Y    =         4103555
35  meter
 Z    =      -14647358
24                 Z    =        -4449387
96
 XDOT =     -10433
277188                 XDOT =       -3264
331320
 YDOT =      20031
628502  feet/sec       YDOT =        6069
607394  meter/sec
 ZDOT =      10962
199148                 ZDOT =        3325
626567

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12924899
69                 X    =         3939509
43
 Y    =       10879692
78  feet           Y    =         3316130
36  meter
 Z    =      -14577654
49                 Z    =        -4443269
09
 XDOT =      -5280
181655                 XDOT =       -1609
399368
 YDOT =      20847
769102  feet/sec       YDOT =        6354
400022  meter/sec
 ZDOT =      10889
699421                 ZDOT =        3319
180383


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   20220
16810910  
00016717  00000-0  10270-3 0  9043
2 25544  51
6416  96
1558 0001126  12
1280 347
9897 15
49119782 39919


Satellite: ISS
Catalog Number: 25544
Epoch time:      20220
16810910   =   yrday
fracday
Element set:     904
Inclination:       51
6416  deg
RA of node:        96
1558  deg
Eccentricity:     
0001126     
Arg of perigee:    12
1280  deg
Mean anomaly:     347
9897  deg
Mean motion:   15
49119782  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3991
Checksum:              306


Coasting Arc #6 (Orbit 4006)
---------------------------------------

Vector Time (GMT): 2020/221/03:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3430273
53                 A    =         6795656
30  meter
 Y    =       -3848440
25  meter          E    =           
0009967
 Z    =        4422324
65                 I    =           52
02409
 XDOT =       2690
537532                 Wp   =           64
77245
 YDOT =      -6317
539029  meter/sec      RA   =           90
32586  deg
 ZDOT =      -3400
632696                 TA   =           59
54059
                                          MA   =           59
44218
                                          Ha   =            229
020  n
mi
                                          Hp   =            222
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11254178
24                 X    =        -3408464
94
 Y    =      -12626116
30  feet           Y    =        -3886678
14  meter
 Z    =       14508939
16                 Z    =         4405714
93
 XDOT =       8827
222873                 XDOT =        2777
500232
 YDOT =     -20726
834084  feet/sec       YDOT =       -6286
965232  meter/sec
 ZDOT =     -11156
931417                 ZDOT =       -3387
352205

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13917449
08                 X    =        -4242038
48
 Y    =       -9726021
95  feet           Y    =        -2964491
49  meter
 Z    =       14432385
95                 Z    =         4398991
24
 XDOT =       3268
144474                 XDOT =         996
130436
 YDOT =     -21190
349707  feet/sec       YDOT =       -6458
818591  meter/sec
 ZDOT =     -11095
361062                 ZDOT =       -3381
866052


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   20221
20025503  
00016717  00000-0  10270-3 0  9056
2 25544  51
6401  91
0487 0001128   7
3517 352
7649 15
49157503 40070


Satellite: ISS
Catalog Number: 25544
Epoch time:      20221
20025503   =   yrday
fracday
Element set:     905
Inclination:       51
6401  deg
RA of node:        91
0487  deg
Eccentricity:     
0001128     
Arg of perigee:     7
3517  deg
Mean anomaly:     352
7649  deg
Mean motion:   15
49157503  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4007
Checksum:              270


Coasting Arc #7 (Orbit 4021)
---------------------------------------

Vector Time (GMT): 2020/222/03:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3738390
06                 A    =         6795848
23  meter
 Y    =        3588317
23  meter          E    =           
0008779
 Z    =       -4405358
02                 I    =           52
02386
 XDOT =      -2172
628413                 Wp   =          102
75267
 YDOT =       6481
346489  meter/sec      RA   =           85
40474  deg
 ZDOT =       3439
475064                 TA   =          201
99246
                                          MA   =          202
03015
                                          Ha   =            229
067  n
mi
                                          Hp   =            222
530

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12265059
26                 X    =         3719385
02
 Y    =       11772694
33  feet           Y    =         3630016
38  meter
 Z    =      -14453274
36                 Z    =        -4387244
73
 XDOT =      -7128
045976                 XDOT =       -2261
650086
 YDOT =      21264
260133  feet/sec       YDOT =        6456
552806  meter/sec
 ZDOT =      11284
367009                 ZDOT =        3428
705294

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14855271
61                 X    =         4527886
79
 Y    =        8411635
48  feet           Y    =         2563866
49  meter
 Z    =      -14369775
37                 Z    =        -4379907
53
 XDOT =      -1203
461112                 XDOT =        -366
814947
 YDOT =      21295
358637  feet/sec       YDOT =        6490
825313  meter/sec
 ZDOT =      11234
370210                 ZDOT =        3424
236040


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   20222
16789177  
00016717  00000-0  10270-3 0  9067
2 25544  51
6406  86
2615 0001180  15
5127 344
6058 15
49122882 40223


Satellite: ISS
Catalog Number: 25544
Epoch time:      20222
16789177   =   yrday
fracday
Element set:     906
Inclination:       51
6406  deg
RA of node:        86
2615  deg
Eccentricity:     
0001180     
Arg of perigee:    15
5127  deg
Mean anomaly:     344
6058  deg
Mean motion:   15
49122882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4022
Checksum:              294


Coasting Arc #8 (Orbit 4037)
---------------------------------------

Vector Time (GMT): 2020/223/03:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4009004
45                 A    =         6795893
28  meter
 Y    =       -3324108
06  meter          E    =           
0010377
 Z    =        4360433
71                 I    =           52
02074
 XDOT =       1662
535335                 Wp   =           66
15007
 YDOT =      -6610
560858  meter/sec      RA   =           80
48278  deg
 ZDOT =      -3500
266918                 TA   =           59
31799
                                          MA   =           59
21576
                                          Ha   =            229
087  n
mi
                                          Hp   =            222
397

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13152901
72                 X    =        -3992715
61
 Y    =      -10905866
35  feet           Y    =        -3368848
63  meter
 Z    =       14305884
86                 Z    =         4340999
21
 XDOT =       5454
512253                 XDOT =        1753
335178
 YDOT =     -21688
191790  feet/sec       YDOT =       -6591
461435  meter/sec
 ZDOT =     -11483
815348                 ZDOT =       -3491
970647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15628869
20                 X    =        -4763679
33
 Y    =       -7087373
27  feet           Y    =        -2160231
37  meter
 Z    =       14216282
01                 Z    =         4333122
76
 XDOT =       -810
036404                 XDOT =        -246
899096
 YDOT =     -21241
753550  feet/sec       YDOT =       -6474
486482  meter/sec
 ZDOT =     -11445
219774                 ZDOT =       -3488
502987


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   20223
20003363  
00016717  00000-0  10270-3 0  9070
2 25544  51
6409  81
1543 0001231  13
6653 346
4530 15
49159525 40386


Satellite: ISS
Catalog Number: 25544
Epoch time:      20223
20003363   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:        81
1543  deg
Eccentricity:     
0001231     
Arg of perigee:    13
6653  deg
Mean anomaly:     346
4530  deg
Mean motion:   15
49159525  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4038
Checksum:              270


Coasting Arc #9 (Orbit 4043)
---------------------------------------

Vector Time (GMT): 2020/223/13:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3478545
57                 A    =         6793021
02  meter
 Y    =       -2864844
69  meter          E    =           
0013615
 Z    =       -5095415
00                 I    =           52
00859
 XDOT =       2883
176473                 Wp   =           71
43719
 YDOT =       6833
396348  meter/sec      RA   =           78
50341  deg
 ZDOT =      -1873
604754                 TA   =          180
45613
                                          MA   =          180
45737
                                          Ha   =            228
973  n
mi
                                          Hp   =            222
521

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11412551
07                 X    =         3535072
99
 Y    =       -9399096
76  feet           Y    =        -2825628
92  meter
 Z    =      -16717240
82                 Z    =        -5078380
51
 XDOT =       9459
240396                 XDOT =        2815
649930
 YDOT =      22419
279358  feet/sec       YDOT =        6865
260569  meter/sec
 ZDOT =      -6146
997224                 ZDOT =       -1859
763368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13774457
38                 X    =        -4198454
61
 Y    =        5610858
42  feet           Y    =         1710189
65  meter
 Z    =      -16638451
67                 Z    =        -5071400
07
 XDOT =      -2107
370452                 XDOT =        -642
326514
 YDOT =     -23214
272695  feet/sec       YDOT =       -7075
710317  meter/sec
 ZDOT =      -6083
380595                 ZDOT =       -1854
214405


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   20223
58708611  
00016717  00000-0  10270-3 0  9080
2 25544  51
6408  79
2377 0001213  11
9334 348
1844 15
49153738 40449


Satellite: ISS
Catalog Number: 25544
Epoch time:      20223
58708611   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:        79
2377  deg
Eccentricity:     
0001213     
Arg of perigee:    11
9334  deg
Mean anomaly:     348
1844  deg
Mean motion:   15
49153738  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4044
Checksum:              303


Coasting Arc #10 (Orbit 4059)
---------------------------------------

Vector Time (GMT): 2020/224/13:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3244817
94                 A    =         6793055
01  meter
 Y    =        3090360
39  meter          E    =           
0005145
 Z    =        5101888
84                 I    =           52
00015
 XDOT =      -3428
485817                 Wp   =          110
96321
 YDOT =      -6607
773681  meter/sec      RA   =           73
58110  deg
 ZDOT =       1818
724001                 TA   =          321
49010
                                          MA   =          321
52680
                                          Ha   =            229
206  n
mi
                                          Hp   =            222
429

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10645728
14                 X    =        -3303916
01
 Y    =       10138977
65  feet           Y    =         3053743
88  meter
 Z    =       16738480
45                 Z    =         5085983
47
 XDOT =     -11248
313048                 XDOT =       -3363
175164
 YDOT =     -21679
047510  feet/sec       YDOT =       -6645
748355  meter/sec
 ZDOT =       5966
942260                 ZDOT =        1802
228241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13143676
58                 X    =         4006192
62
 Y    =       -6769963
73  feet           Y    =        -2063484
95  meter
 Z    =       16664887
64                 Z    =         5079457
75
 XDOT =       4361
834735                 XDOT =        1329
487227
 YDOT =      22996
282774  feet/sec       YDOT =        7009
266990  meter/sec
 ZDOT =       5891
075199                 ZDOT =        1795
599721


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   20224
61922780  
00016717  00000-0  10270-3 0  9091
2 25544  51
6405  74
1309 0001258  16
3824 343
7366 15
49114044 40602


Satellite: ISS
Catalog Number: 25544
Epoch time:      20224
61922780   =   yrday
fracday
Element set:     909
Inclination:       51
6405  deg
RA of node:        74
1309  deg
Eccentricity:     
0001258     
Arg of perigee:    16
3824  deg
Mean anomaly:     343
7366  deg
Mean motion:   15
49114044  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4060
Checksum:              287


Coasting Arc #11 (Orbit 4074)
---------------------------------------

Vector Time (GMT): 2020/225/13:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3012826
34                 A    =         6792861
11  meter
 Y    =       -3301723
30  meter          E    =           
0013998
 Z    =       -5127741
57                 I    =           51
98889
 XDOT =       3939
922129                 Wp   =           73
16581
 YDOT =       6318
093241  meter/sec      RA   =           68
65795  deg
 ZDOT =      -1753
285239                 TA   =          179
92214
                                          MA   =          179
92192
                                          Ha   =            229
036  n
mi
                                          Hp   =            222
423

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9884600
85                 X    =         3074430
75
 Y    =      -10832425
51  feet           Y    =        -3267686
99  meter
 Z    =      -16823299
10                 Z    =        -5112957
09
 XDOT =      12926
253704                 XDOT =        3877
494897
 YDOT =      20728
652365  feet/sec       YDOT =        6361
803309  meter/sec
 ZDOT =      -5752
248161                 ZDOT =       -1734
298040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12471106
56                 X    =        -3801193
28
 Y    =        7862328
06  feet           Y    =         2396437
59  meter
 Z    =      -16754864
01                 Z    =        -5106882
55
 XDOT =      -6559
339280                 XDOT =       -1999
286612
 YDOT =     -22476
220683  feet/sec       YDOT =       -6850
752064  meter/sec
 ZDOT =      -5664
878474                 ZDOT =       -1726
654959


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   20225
58685782  
00016717  00000-0  10270-3 0  9108
2 25544  51
6402  69
3433 0001128  24
6229 335
4975 15
49156779 40751


Satellite: ISS
Catalog Number: 25544
Epoch time:      20225
58685782   =   yrday
fracday
Element set:     910
Inclination:       51
6402  deg
RA of node:        69
3433  deg
Eccentricity:     
0001128     
Arg of perigee:    24
6229  deg
Mean anomaly:     335
4975  deg
Mean motion:   15
49156779  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4075
Checksum:              323


Coasting Arc #12 (Orbit 4090)
---------------------------------------

Vector Time (GMT): 2020/226/13:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2754270
02                 A    =         6792869
16  meter
 Y    =        3488884
12  meter          E    =           
0004993
 Z    =        5133039
47                 I    =           51
97575
 XDOT =      -4444
091085                 Wp   =          110
95688
 YDOT =      -6008
261957  meter/sec      RA   =           63
73364  deg
 ZDOT =       1696
103646                 TA   =          322
70811
                                          MA   =          322
74277
                                          Ha   =            229
210  n
mi
                                          Hp   =            222
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9036318
95                 X    =        -2818012
23
 Y    =       11446470
23  feet           Y    =         3457727
14  meter
 Z    =       16840680
66                 Z    =         5119505
84
 XDOT =     -14580
351329                 XDOT =       -4384
813242
 YDOT =     -19712
145529  feet/sec       YDOT =       -6057
627635  meter/sec
 ZDOT =       5564
644509                 ZDOT =        1674
659718

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11660714
11                 X    =         3554185
66
 Y    =       -8877589
60  feet           Y    =        -2705889
31  meter
 Z    =       16778003
91                 Z    =         5113935
59
 XDOT =       8736
906726                 XDOT =        2663
009170
 YDOT =      21825
217717  feet/sec       YDOT =        6652
326360  meter/sec
 ZDOT =       5465
928735                 ZDOT =        1666
015079


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   20226
61899640  
00016717  00000-0  10270-3 0  9114
2 25544  51
6407  64
2360 0001207  23
6783 336
4422 15
49126670 40914


Satellite: ISS
Catalog Number: 25544
Epoch time:      20226
61899640   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:        64
2360  deg
Eccentricity:     
0001207     
Arg of perigee:    23
6783  deg
Mean anomaly:     336
4422  deg
Mean motion:   15
49126670  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4091
Checksum:              292


Coasting Arc #13 (Orbit 4105)
---------------------------------------

Vector Time (GMT): 2020/227/13:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2500650
89                 A    =         6792679
81  meter
 Y    =       -3662341
24  meter          E    =           
0014468
 Z    =       -5158305
02                 I    =           51
96029
 XDOT =       4903
583993                 Wp   =           74
51997
 YDOT =       5640
645062  meter/sec      RA   =           58
80900  deg
 ZDOT =      -1627
680301                 TA   =          179
80537
                                          MA   =          179
80481
                                          Ha   =            229
114  n
mi
                                          Hp   =            222
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8204235
20                 X    =         2566474
24
 Y    =      -12015555
25  feet           Y    =        -3634008
73  meter
 Z    =      -16923572
90                 Z    =        -5145998
39
 XDOT =      16087
873993                 XDOT =        4848
050418
 YDOT =      18506
053353  feet/sec       YDOT =        5695
170063  meter/sec
 ZDOT =      -5340
158468                 ZDOT =       -1603
995307

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10825313
34                 X    =        -3299555
51
 Y    =        9819501
39  feet           Y    =         2992984
02  meter
 Z    =      -16866545
18                 Z    =        -5140922
97
 XDOT =     -10796
894100                 XDOT =       -3290
893322
 YDOT =     -20887
756449  feet/sec       YDOT =       -6366
588166  meter/sec
 ZDOT =      -5231
086002                 ZDOT =       -1594
435013


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   20227
58662261  
00016717  00000-0  10270-3 0  9129
2 25544  51
6415  59
4488 0001229  37
5565 322
5671 15
49168969 41062


Satellite: ISS
Catalog Number: 25544
Epoch time:      20227
58662261   =   yrday
fracday
Element set:     912
Inclination:       51
6415  deg
RA of node:        59
4488  deg
Eccentricity:     
0001229     
Arg of perigee:    37
5565  deg
Mean anomaly:     322
5671  deg
Mean motion:   15
49168969  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4106
Checksum:              325


Coasting Arc #14 (Orbit 4121)
---------------------------------------

Vector Time (GMT): 2020/228/13:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2224075
61                 A    =         6792679
40  meter
 Y    =        3808995
21  meter          E    =           
0004984
 Z    =        5162183
11                 I    =           51
94024
 XDOT =      -5353
587468                 Wp   =          110
51693
 YDOT =      -5254
524743  meter/sec      RA   =           53
88246  deg
 ZDOT =       1567
667747                 TA   =          324
40781
                                          MA   =          324
44104
                                          Ha   =            229
254  n
mi
                                          Hp   =            222
240

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7296835
98                 X    =        -2291578
18
 Y    =       12496703
46  feet           Y    =         3783746
17  meter
 Z    =       16936296
28                 Z    =         5151215
94
 XDOT =     -17564
263345                 XDOT =       -5302
046627
 YDOT =     -17239
254405  feet/sec       YDOT =       -5314
104325  meter/sec
 ZDOT =       5143
266887                 ZDOT =        1541
787275

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9868609
64                 X    =         3007952
22
 Y    =      -10664990
67  feet           Y    =        -3250689
16  meter
 Z    =       16885439
35                 Z    =         5146681
91
 XDOT =      12814
304234                 XDOT =        3905
799931
 YDOT =      19827
017721  feet/sec       YDOT =        6043
275001  meter/sec
 ZDOT =       5024
043584                 ZDOT =        1531
328484


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   20228
61875758  
00016717  00000-0  10270-3 0  9132
2 25544  51
6402  54
3414 0001224  37
9582 322
1654 15
49142721 41222


Satellite: ISS
Catalog Number: 25544
Epoch time:      20228
61875758   =   yrday
fracday
Element set:     913
Inclination:       51
6402  deg
RA of node:        54
3414  deg
Eccentricity:     
0001224     
Arg of perigee:    37
9582  deg
Mean anomaly:     322
1654  deg
Mean motion:   15
49142721  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4122
Checksum:              288


Coasting Arc #15 (Orbit 4136)
---------------------------------------

Vector Time (GMT): 2020/229/13:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1953953
60                 A    =         6792521
19  meter
 Y    =       -3944323
52  meter          E    =           
0014723
 Z    =       -5186393
68                 I    =           51
92038
 XDOT =       5749
840510                 Wp   =           76
04254
 YDOT =       4817
314105  meter/sec      RA   =           48
95612  deg
 ZDOT =      -1497
517893                 TA   =          179
55677
                                          MA   =          179
55546
                                          Ha   =            229
127  n
mi
                                          Hp   =            222
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6410608
91                 X    =         2023107
02
 Y    =      -12940693
98  feet           Y    =        -3922086
00  meter
 Z    =      -17015727
29                 Z    =        -5176734
64
 XDOT =      18864
306134                 XDOT =        5702
818465
 YDOT =      15804
836301  feet/sec       YDOT =        4881
350118  meter/sec
 ZDOT =      -4913
116447                 ZDOT =       -1469
701835

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8900309
40                 X    =        -2712814
31
 Y    =       11439647
20  feet           Y    =         3486804
47  meter
 Z    =      -16970898
82                 Z    =        -5172729
96
 XDOT =     -14659
964743                 XDOT =       -4468
357254
 YDOT =     -18503
762017  feet/sec       YDOT =       -5639
946663  meter/sec
 ZDOT =      -4784
936659                 ZDOT =       -1458
448694


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   20229
58638192  
00016717  00000-0  10270-3 0  9149
2 25544  51
6414  49
5550 0001180  45
3749 314
7497 15
49176210 41379


Satellite: ISS
Catalog Number: 25544
Epoch time:      20229
58638192   =   yrday
fracday
Element set:     914
Inclination:       51
6414  deg
RA of node:        49
5550  deg
Eccentricity:     
0001180     
Arg of perigee:    45
3749  deg
Mean anomaly:     314
7497  deg
Mean motion:   15
49176210  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4137
Checksum:              312


Coasting Arc #16 (Orbit 4152)
---------------------------------------

Vector Time (GMT): 2020/230/13:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 958140
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1665301
42                 A    =         6792463
58  meter
 Y    =        4049755
97  meter          E    =           
0004728
 Z    =        5189196
56                 I    =           51
89733
 XDOT =      -6133
918252                 Wp   =          110
50378
 YDOT =      -4364
101066  meter/sec      RA   =           44
02571  deg
 ZDOT =       1434
686375                 TA   =          325
71787
                                          MA   =          325
74837
                                          Ha   =            229
188  n
mi
                                          Hp   =            222
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5463587
34                 X    =        -1735668
80
 Y    =       13286600
94  feet           Y    =         4030739
66  meter
 Z    =       17024923
09                 Z    =         5180936
66
 XDOT =     -20124
403715                 XDOT =       -6091
630409
 YDOT =     -14317
916883  feet/sec       YDOT =       -4432
458551  meter/sec
 ZDOT =       4706
976296                 ZDOT =        1404
993376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7830932
62                 X    =         2386868
26
 Y    =      -12098192
65  feet           Y    =        -3687529
12  meter
 Z    =       16986547
21                 Z    =         5177499
59
 XDOT =      16439
781843                 XDOT =        5010
845506
 YDOT =      17070
176961  feet/sec       YDOT =        5202
989938  meter/sec
 ZDOT =       4570
108527                 ZDOT =        1392
969079


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   20230
61851296  
00016717  00000-0  10270-3 0  9158
2 25544  51
6417  44
4466 0001149  41
6830 318
4407 15
49170440 41536


Satellite: ISS
Catalog Number: 25544
Epoch time:      20230
61851296   =   yrday
fracday
Element set:     915
Inclination:       51
6417  deg
RA of node:        44
4466  deg
Eccentricity:     
0001149     
Arg of perigee:    41
6830  deg
Mean anomaly:     318
4407  deg
Mean motion:   15
49170440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4153
Checksum:              288
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