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

 
Date: April 25th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16491 3871 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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


116/01:51:40 000 0 0 0 0 0 0
N/A 0 0 0 0 228 4
000/00:00:00 000 0 0 0 0 222 4

116/05:12:17 000 0 0 0 0 0 0
N/A 0 0 0 0 228 2
000/00:00:00 000 0 0 0 0 222 4

117/03:08:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 222 5

130/00:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 1
000/00:00:00 000 0 0 0 0 222 8

Coasting Arc #1 (Orbit 2368)
---------------------------------------

Vector Time (GMT): 2020/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921051
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3653715
34                 A    =         6791767
41  meter
 Y    =       -2368311
27  meter          E    =           
0004802
 Z    =        5210624
80                 I    =           51
24875
 XDOT =       2995
877081                 Wp   =          144
40616
 YDOT =       6971
807754  meter/sec      RA   =          253
20640  deg
 ZDOT =       1063
739277                 TA   =          295
31508
                                          MA   =          295
36481
                                          Ha   =            228
431  n
mi
                                          Hp   =            222
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11987255
04                 X    =         3654616
25
 Y    =       -7770050
11  feet           Y    =        -2327447
83  meter
 Z    =       17095225
72                 Z    =         5228375
61
 XDOT =       9828
993047                 XDOT =        2912
526472
 YDOT =      22873
385020  feet/sec       YDOT =        7004
843732  meter/sec
 ZDOT =       3489
958259                 ZDOT =        1078
089948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5932587
07                 X    =         1808252
54
 Y    =      -12887203
69  feet           Y    =        -3928019
68  meter
 Z    =       17176702
14                 Z    =         5235458
81
 XDOT =      19515
738850                 XDOT =        5948
397201
 YDOT =      13741
748068  feet/sec       YDOT =        4188
484811  meter/sec
 ZDOT =       3555
444399                 ZDOT =        1083
699453


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   20115
55025535  
00016717  00000-0  10270-3 0  9006
2 25544  51
6412 253
9365 0001875 191
5864 168
5243 15
49322413 23692


Satellite: ISS
Catalog Number: 25544
Epoch time:      20115
55025535   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:       253
9365  deg
Eccentricity:     
0001875     
Arg of perigee:   191
5864  deg
Mean anomaly:     168
5243  deg
Mean motion:   15
49322413  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2369
Checksum:              302


Coasting Arc #2 (Orbit 2377)
---------------------------------------

Vector Time (GMT): 2020/116/01:51:40
000
Vector Time (MET): N/A
Weight (LBS)     : 921051
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2537183
66                 A    =         6793817
89  meter
 Y    =       -4166677
62  meter          E    =           
0008114
 Z    =        4725005
93                 I    =           51
26221
 XDOT =       4337
836317                 Wp   =          128
05006
 YDOT =       5710
734757  meter/sec      RA   =          250
35017  deg
 ZDOT =       2698
551473                 TA   =          295
06743
                                          MA   =          295
15162
                                          Ha   =            228
383  n
mi
                                          Hp   =            222
370

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8324093
38                 X    =         2560636
33
 Y    =      -13670202
16  feet           Y    =        -4138173
99  meter
 Z    =       15501987
96                 Z    =         4737387
68
 XDOT =      14231
746447                 XDOT =        4260
546536
 YDOT =      18736
006420  feet/sec       YDOT =        5758
811320  meter/sec
 ZDOT =       8853
515332                 ZDOT =        2719
435755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7865553
34                 X    =         2397420
66
 Y    =       13875497
36  feet           Y    =         4229251
60  meter
 Z    =       15558927
73                 Z    =         4742361
17
 XDOT =     -22270
398271                 XDOT =       -6788
017393
 YDOT =       2559
936638  feet/sec       YDOT =         780
268687  meter/sec
 ZDOT =       8949
015818                 ZDOT =        2727
660021


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   20116
13077586  
00016717  00000-0  10270-3 0  9015
2 25544  51
6418 251
0687 0001497 198
2885 161
8211 15
49332646 23781


Satellite: ISS
Catalog Number: 25544
Epoch time:      20116
13077586   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:       251
0687  deg
Eccentricity:     
0001497     
Arg of perigee:   198
2885  deg
Mean anomaly:     161
8211  deg
Mean motion:   15
49332646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2378
Checksum:              320


Coasting Arc #3 (Orbit 2379)
---------------------------------------

Vector Time (GMT): 2020/116/05:12:17
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4632325
57                 A    =         6794379
56  meter
 Y    =        1987561
90  meter          E    =           
0007606
 Z    =        4550526
93                 I    =           51
26751
 XDOT =         -5
098477                 Wp   =           73
28856
 YDOT =       7026
925617  meter/sec      RA   =          249
61502  deg
 ZDOT =      -3057
593195                 TA   =           47
50578
                                          MA   =           47
44154
                                          Ha   =            228
217  n
mi
                                          Hp   =            222
376

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15197918
54                 X    =         4587651
52
 Y    =        6520872
38  feet           Y    =         2039113
97  meter
 Z    =       14929550
30                 Z    =         4572920
90
 XDOT =        -16
727288                 XDOT =         -68
822955
 YDOT =      23054
217902  feet/sec       YDOT =        7026
512366  meter/sec
 ZDOT =     -10031
473736                 ZDOT =       -3057
772576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -720167
07                 X    =         -219506
92
 Y    =       16428827
43  feet           Y    =         5007506
60  meter
 Z    =       15032131
10                 Z    =         4581793
56
 XDOT =     -20327
001662                 XDOT =       -6195
670107
 YDOT =       8307
738841  feet/sec       YDOT =        2532
198799  meter/sec
 ZDOT =     -10032
592375                 ZDOT =       -3057
934156


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   20116
25977917  
00016717  00000-0  10270-3 0  9026
2 25544  51
6434 250
4312 0001358 205
3896 154
7188 15
49355547 23807


Satellite: ISS
Catalog Number: 25544
Epoch time:      20116
25977917   =   yrday
fracday
Element set:     902
Inclination:       51
6434  deg
RA of node:       250
4312  deg
Eccentricity:     
0001358     
Arg of perigee:   205
3896  deg
Mean anomaly:     154
7188  deg
Mean motion:   15
49355547  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2380
Checksum:              317


Coasting Arc #4 (Orbit 2393)
---------------------------------------

Vector Time (GMT): 2020/117/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2837183
85                 A    =         6803434
79  meter
 Y    =        6176144
41  meter          E    =           
0012721
 Z    =         -34657
84                 I    =           51
30871
 XDOT =      -4362
540946                 Wp   =          141
08129
 YDOT =       1977
282372  meter/sec      RA   =          245
09300  deg
 ZDOT =      -5980
157682                 TA   =           39
29303
                                          MA   =           39
20078
                                          Ha   =            228
485  n
mi
                                          Hp   =            222
466

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9308345
95                 X    =         2768077
85
 Y    =       20262940
96  feet           Y    =         6207485
42  meter
 Z    =        -113706
81                 Z    =          -21043
27
 XDOT =     -14312
798379                 XDOT =       -4355
278591
 YDOT =       6487
146889  feet/sec       YDOT =        1928
538189  meter/sec
 ZDOT =     -19619
939900                 ZDOT =       -6001
331838

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21502541
99                 X    =        -6553974
80
 Y    =        5906186
75  feet           Y    =         1800205
72  meter
 Z    =         -51538
97                 Z    =          -15709
08
 XDOT =      -3674
691374                 XDOT =       -1120
045931
 YDOT =     -13474
055499  feet/sec       YDOT =       -4106
892116  meter/sec
 ZDOT =     -19717
100562                 ZDOT =       -6009
772251


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   20117
16281290  
00016717  00000-0  10270-3 0  9030
2 25544  51
6435 245
9620 0001532 201
5992 158
5093 15
49288840 23941


Satellite: ISS
Catalog Number: 25544
Epoch time:      20117
16281290   =   yrday
fracday
Element set:     903
Inclination:       51
6435  deg
RA of node:       245
9620  deg
Eccentricity:     
0001532     
Arg of perigee:   201
5992  deg
Mean anomaly:     158
5093  deg
Mean motion:   15
49288840  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2394
Checksum:              305


Coasting Arc #5 (Orbit 2409)
---------------------------------------

Vector Time (GMT): 2020/118/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3292443
06                 A    =         6803344
91  meter
 Y    =       -5946272
27  meter          E    =           
0011030
 Z    =         134231
87                 I    =           51
32445
 XDOT =       4248
768904                 Wp   =           48
84779
 YDOT =      -2210
481401  meter/sec      RA   =          240
12099  deg
 ZDOT =       5978
150524                 TA   =          312
60146
                                          MA   =          312
69444
                                          Ha   =            228
375  n
mi
                                          Hp   =            222
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10801978
55                 X    =        -3226357
41
 Y    =      -19508767
29  feet           Y    =        -5982721
21  meter
 Z    =         440393
27                 Z    =          118398
41
 XDOT =      13939
530525                 XDOT =        4244
132532
 YDOT =      -7252
235567  feet/sec       YDOT =       -2162
994913  meter/sec
 ZDOT =      19613
354736                 ZDOT =        5998
778289

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20868232
73                 X    =         6360637
33
 Y    =       -7864483
92  feet           Y    =        -2397094
70  meter
 Z    =         368026
56                 Z    =          112174
50
 XDOT =       4601
109463                 XDOT =        1402
418164
 YDOT =      13189
021131  feet/sec       YDOT =        4020
013641  meter/sec
 ZDOT =      19708
026353                 ZDOT =        6007
006432


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   20118
19484432  
00016717  00000-0  10270-3 0  9048
2 25544  51
6440 240
8544 0001314 210
2721 149
8353 15
49317595 24102


Satellite: ISS
Catalog Number: 25544
Epoch time:      20118
19484432   =   yrday
fracday
Element set:     904
Inclination:       51
6440  deg
RA of node:       240
8544  deg
Eccentricity:     
0001314     
Arg of perigee:   210
2721  deg
Mean anomaly:     149
8353  deg
Mean motion:   15
49317595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2410
Checksum:              284


Coasting Arc #6 (Orbit 2424)
---------------------------------------

Vector Time (GMT): 2020/119/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3702594
05                 A    =         6803418
18  meter
 Y    =        5693775
31  meter          E    =           
0012094
 Z    =        -268595
05                 I    =           51
34155
 XDOT =      -4140
916038                 Wp   =          143
13821
 YDOT =       2417
983305  meter/sec      RA   =          235
15161  deg
 ZDOT =      -5975
246116                 TA   =           39
76245
                                          MA   =           39
67388
                                          Ha   =            228
439  n
mi
                                          Hp   =            222
517

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12147618
27                 X    =         3639954
08
 Y    =       18680365
18  feet           Y    =         5734830
12  meter
 Z    =        -881217
34                 Z    =         -250760
86
 XDOT =     -13585
682539                 XDOT =       -4138
622248
 YDOT =       7933
016091  feet/sec       YDOT =        2371
689865  meter/sec
 ZDOT =     -19603
825840                 ZDOT =       -5995
355545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20080628
31                 X    =        -6120575
51
 Y    =        9665720
20  feet           Y    =         2946111
52  meter
 Z    =        -799647
75                 Z    =         -243732
63
 XDOT =      -5442
458398                 XDOT =       -1658
861320
 YDOT =     -12891
410973  feet/sec       YDOT =       -3929
302065  meter/sec
 ZDOT =     -19696
135912                 ZDOT =       -6003
382226


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   20119
16237318  
00016717  00000-0  10270-3 0  9056
2 25544  51
6434 236
0672 0001420 208
5245 151
5828 15
49285752 24255


Satellite: ISS
Catalog Number: 25544
Epoch time:      20119
16237318   =   yrday
fracday
Element set:     905
Inclination:       51
6434  deg
RA of node:       236
0672  deg
Eccentricity:     
0001420     
Arg of perigee:   208
5245  deg
Mean anomaly:     151
5828  deg
Mean motion:   15
49285752  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2425
Checksum:              295


Coasting Arc #7 (Orbit 2440)
---------------------------------------

Vector Time (GMT): 2020/120/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4115362
14                 A    =         6803269
03  meter
 Y    =       -5397998
47  meter          E    =           
0011374
 Z    =         369826
49                 I    =           51
36109
 XDOT =       4010
474388                 Wp   =           50
04665
 YDOT =      -2640
714436  meter/sec      RA   =          230
18231  deg
 ZDOT =       5968
663783                 TA   =          313
94721
                                          MA   =          314
04100
                                          Ha   =            228
271  n
mi
                                          Hp   =            222
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13501844
30                 X    =        -4056490
68
 Y    =      -17709968
74  feet           Y    =        -5443690
23  meter
 Z    =        1213341
50                 Z    =          349978
15
 XDOT =      13157
724371                 XDOT =        4010
713032
 YDOT =      -8663
761273  feet/sec       YDOT =       -2595
865537  meter/sec
 ZDOT =      19582
230258                 ZDOT =        5988
145622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19097177
95                 X    =         5820819
84
 Y    =      -11465285
54  feet           Y    =        -3494619
03  meter
 Z    =        1122502
52                 Z    =          342138
77
 XDOT =       6330
890925                 XDOT =        1929
655554
 YDOT =      12511
012421  feet/sec       YDOT =        3813
356586  meter/sec
 ZDOT =      19671
677352                 ZDOT =        5995
927257


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   20120
19440042  
00016717  00000-0  10270-3 0  9062
2 25544  51
6429 230
9598 0001314 221
4015 138
7035 15
49328715 24412


Satellite: ISS
Catalog Number: 25544
Epoch time:      20120
19440042   =   yrday
fracday
Element set:     906
Inclination:       51
6429  deg
RA of node:       230
9598  deg
Eccentricity:     
0001314     
Arg of perigee:   221
4015  deg
Mean anomaly:     138
7035  deg
Mean motion:   15
49328715  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2441
Checksum:              278


Coasting Arc #8 (Orbit 2455)
---------------------------------------

Vector Time (GMT): 2020/121/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4480396
09                 A    =         6803341
76  meter
 Y    =        5086801
35  meter          E    =           
0011332
 Z    =        -505004
98                 I    =           51
38376
 XDOT =      -3887
678776                 Wp   =          145
93146
 YDOT =       2839
985853  meter/sec      RA   =          225
21526  deg
 ZDOT =      -5959
191403                 TA   =           39
52475
                                          MA   =           39
44216
                                          Ha   =            228
328  n
mi
                                          Hp   =            222
626

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14699462
23                 X    =         4425634
01
 Y    =       16688980
82  feet           Y    =         5136598
17  meter
 Z    =       -1656840
48                 Z    =         -483373
59
 XDOT =     -12754
851626                 XDOT =       -3890
200970
 YDOT =       9317
538888  feet/sec       YDOT =        2796
497331  meter/sec
 ZDOT =     -19551
152898                 ZDOT =       -5978
082233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17993032
21                 X    =        -5484276
22
 Y    =       13083022
45  feet           Y    =         3987705
24  meter
 Z    =       -1557789
01                 Z    =         -474814
09
 XDOT =      -7139
636623                 XDOT =       -2176
161243
 YDOT =     -12126
518235  feet/sec       YDOT =       -3696
162758  meter/sec
 ZDOT =     -19637
902179                 ZDOT =       -5985
632584


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   20121
16192583  
00016717  00000-0  10270-3 0  9075
2 25544  51
6432 226
1722 0001465 221
3273 138
7767 15
49287733 24566


Satellite: ISS
Catalog Number: 25544
Epoch time:      20121
16192583   =   yrday
fracday
Element set:     907
Inclination:       51
6432  deg
RA of node:       226
1722  deg
Eccentricity:     
0001465     
Arg of perigee:   221
3273  deg
Mean anomaly:     138
7767  deg
Mean motion:   15
49287733  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2456
Checksum:              305


Coasting Arc #9 (Orbit 2471)
---------------------------------------

Vector Time (GMT): 2020/122/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4839926
80                 A    =         6803113
69  meter
 Y    =       -4733871
83  meter          E    =           
0011699
 Z    =         609065
59                 I    =           51
40807
 XDOT =       3741
887380                 Wp   =           51
31451
 YDOT =      -3051
426313  meter/sec      RA   =          220
24815  deg
 ZDOT =       5947
733947                 TA   =          315
26823
                                          MA   =          315
36252
                                          Ha   =            228
150  n
mi
                                          Hp   =            222
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15879024
93                 X    =        -4789590
02
 Y    =      -15531075
56  feet           Y    =        -4787713
91  meter
 Z    =        1998246
70                 Z    =          585677
13
 XDOT =      12276
533399                 XDOT =        3746
840510
 YDOT =     -10011
241183  feet/sec       YDOT =       -3009
554455  meter/sec
 ZDOT =      19513
562817                 ZDOT =        5965
922475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16701205
85                 X    =         5090527
54
 Y    =      -14657564
48  feet           Y    =        -4467625
65  meter
 Z    =        1891099
43                 Z    =          576407
11
 XDOT =       7983
028878                 XDOT =        2433
227202
 YDOT =      11655
920151  feet/sec       YDOT =        3552
724462  meter/sec
 ZDOT =      19597
101977                 ZDOT =        5973
196682


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   20122
19394651  
00016717  00000-0  10270-3 0  9080
2 25544  51
6432 221
0638 0001324 234
0031 126
0996 15
49351059 24728


Satellite: ISS
Catalog Number: 25544
Epoch time:      20122
19394651   =   yrday
fracday
Element set:     908
Inclination:       51
6432  deg
RA of node:       221
0638  deg
Eccentricity:     
0001324     
Arg of perigee:   234
0031  deg
Mean anomaly:     126
0996  deg
Mean motion:   15
49351059  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2472
Checksum:              282


Coasting Arc #10 (Orbit 2486)
---------------------------------------

Vector Time (GMT): 2020/123/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5150705
21                 A    =         6803193
30  meter
 Y    =        4373081
12  meter          E    =           
0010495
 Z    =        -745661
50                 I    =           51
43344
 XDOT =      -3604
663907                 Wp   =          147
50716
 YDOT =       3242
464511  meter/sec      RA   =          215
28400  deg
 ZDOT =      -5930
987826                 TA   =           40
55758
                                          MA   =           40
47943
                                          Ha   =            228
260  n
mi
                                          Hp   =            222
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16898639
13                 X    =         5105043
31
 Y    =       14347379
01  feet           Y    =         4430424
68  meter
 Z    =       -2446395
99                 Z    =         -720752
14
 XDOT =     -11826
325155                 XDOT =       -3611
844823
 YDOT =      10638
006927  feet/sec       YDOT =        3202
114618  meter/sec
 ZDOT =     -19458
621475                 ZDOT =       -5948
515237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15325651
18                 X    =        -4671258
48
 Y    =       16033752
83  feet           Y    =         4887087
86  meter
 Z    =       -2332236
81                 Z    =         -710865
78
 XDOT =      -8755
142096                 XDOT =       -2668
567311
 YDOT =     -11186
772028  feet/sec       YDOT =       -3409
728114  meter/sec
 ZDOT =     -19539
136598                 ZDOT =       -5955
528835


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   20123
16146762  
00016717  00000-0  10270-3 0  9097
2 25544  51
6424 216
2757 0001341 233
1038 126
9989 15
49297913 24878


Satellite: ISS
Catalog Number: 25544
Epoch time:      20123
16146762   =   yrday
fracday
Element set:     909
Inclination:       51
6424  deg
RA of node:       216
2757  deg
Eccentricity:     
0001341     
Arg of perigee:   233
1038  deg
Mean anomaly:     126
9989  deg
Mean motion:   15
49297913  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2487
Checksum:              319


Coasting Arc #11 (Orbit 2502)
---------------------------------------

Vector Time (GMT): 2020/124/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5449839
10                 A    =         6802951
25  meter
 Y    =       -3971997
60  meter          E    =           
0011984
 Z    =         850333
34                 I    =           51
46087
 XDOT =       3441
582290                 Wp   =           53
39114
 YDOT =      -3444
950910  meter/sec      RA   =          210
32115  deg
 ZDOT =       5914
473935                 TA   =          315
81228
                                          MA   =          315
90793
                                          Ha   =            228
095  n
mi
                                          Hp   =            222
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17880049
54                 X    =        -5409148
45
 Y    =      -13031488
19  feet           Y    =        -4032714
08  meter
 Z    =        2789807
55                 Z    =          823958
85
 XDOT =      11291
280479                 XDOT =        3451
119741
 YDOT =     -11302
332382  feet/sec       YDOT =       -3406
411429  meter/sec
 ZDOT =      19404
442045                 ZDOT =        5931
214974

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13774314
08                 X    =         4198410
93
 Y    =      -17333325
21  feet           Y    =        -5283197
52  meter
 Z    =        2668893
22                 Z    =          813478
65
 XDOT =       9556
839374                 XDOT =        2912
924641
 YDOT =      10621
179234  feet/sec       YDOT =        3237
335430  meter/sec
 ZDOT =      19481
357188                 ZDOT =        5937
917671


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   20124
19348550  
00016717  00000-0  10270-3 0  9102
2 25544  51
6419 211
1680 0001345 241
1336 118
9679 15
49359305 25035


Satellite: ISS
Catalog Number: 25544
Epoch time:      20124
19348550   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:       211
1680  deg
Eccentricity:     
0001345     
Arg of perigee:   241
1336  deg
Mean anomaly:     118
9679  deg
Mean motion:   15
49359305  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2503
Checksum:              291


Coasting Arc #12 (Orbit 2517)
---------------------------------------

Vector Time (GMT): 2020/125/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5699973
11                 A    =         6802977
30  meter
 Y    =        3570708
26  meter          E    =           
0009582
 Z    =        -986795
98                 I    =           51
49074
 XDOT =      -3287
417336                 Wp   =          149
82147
 YDOT =       3628
931375  meter/sec      RA   =          205
36084  deg
 ZDOT =      -5890
742939                 TA   =           40
86909
                                          MA   =           40
79728
                                          Ha   =            228
138  n
mi
                                          Hp   =            222
732

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18700699
19                 X    =         5664414
09
 Y    =       11714922
13  feet           Y    =         3634250
60  meter
 Z    =       -3237519
61                 Z    =         -959193
90
 XDOT =     -10785
489947                 XDOT =       -3299
138721
 YDOT =      11905
942831  feet/sec       YDOT =        3592
103600  meter/sec
 ZDOT =     -19326
584447                 ZDOT =       -5906
740512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12178503
60                 X    =        -3712007
90
 Y    =       18423983
52  feet           Y    =         5615630
18  meter
 Z    =       -3110942
81                 Z    =         -948215
37
 XDOT =     -10291
724156                 XDOT =       -3136
917523
 YDOT =     -10059
670386  feet/sec       YDOT =       -3066
187534  meter/sec
 ZDOT =     -19400
095543                 ZDOT =       -5913
149122


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   20125
16100337  
00016717  00000-0  10270-3 0  9110
2 25544  51
6425 206
3799 0001440 246
5006 113
5993 15
49314835 25183


Satellite: ISS
Catalog Number: 25544
Epoch time:      20125
16100337   =   yrday
fracday
Element set:     911
Inclination:       51
6425  deg
RA of node:       206
3799  deg
Eccentricity:     
0001440     
Arg of perigee:   246
5006  deg
Mean anomaly:     113
5993  deg
Mean motion:   15
49314835  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2518
Checksum:              287


Coasting Arc #13 (Orbit 2533)
---------------------------------------

Vector Time (GMT): 2020/126/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5931692
64                 A    =         6802760
80  meter
 Y    =       -3132973
64  meter          E    =           
0012255
 Z    =        1092941
74                 I    =           51
52072
 XDOT =       3107
058212                 Wp   =           55
18799
 YDOT =      -3821
343417  meter/sec      RA   =          200
40118  deg
 ZDOT =       5868
740272                 TA   =          316
66574
                                          MA   =          316
76205
                                          Ha   =            228
046  n
mi
                                          Hp   =            222
680

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19460933
85                 X    =        -5901526
89
 Y    =      -10278784
90  feet           Y    =        -3199137
38  meter
 Z    =        3585766
86                 Z    =         1064200
80
 XDOT =      10193
760537                 XDOT =        3121
051338
 YDOT =     -12537
215936  feet/sec       YDOT =       -3786
519849  meter/sec
 ZDOT =      19254
397218                 ZDOT =        5883
867317

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10429593
92                 X    =         3178940
23
 Y    =      -19404457
91  feet           Y    =        -5914478
77  meter
 Z    =        3453935
93                 Z    =         1052759
67
 XDOT =      11042
669510                 XDOT =        3365
805667
 YDOT =       9399
135161  feet/sec       YDOT =        2864
856397  meter/sec
 ZDOT =      19323
922363                 ZDOT =        5889
931536


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   20126
19301729  
00016717  00000-0  10270-3 0  9123
2 25544  51
6419 201
2712 0001358 252
4641 107
6361 15
49360244 25340


Satellite: ISS
Catalog Number: 25544
Epoch time:      20126
19301729   =   yrday
fracday
Element set:     912
Inclination:       51
6419  deg
RA of node:       201
2712  deg
Eccentricity:     
0001358     
Arg of perigee:   252
4641  deg
Mean anomaly:     107
6361  deg
Mean motion:   15
49360244  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2534
Checksum:              277


Coasting Arc #14 (Orbit 2548)
---------------------------------------

Vector Time (GMT): 2020/127/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6115726
77                 A    =         6802712
90  meter
 Y    =        2702595
01  meter          E    =           
0008721
 Z    =       -1229538
35                 I    =           51
55093
 XDOT =      -2935
036372                 Wp   =          150
31196
 YDOT =       3997
489017  meter/sec      RA   =          195
44552  deg
 ZDOT =      -5837
361461                 TA   =           43
04004
                                          MA   =           42
97187
                                          Ha   =            228
119  n
mi
                                          Hp   =            222
704

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20064720
37                 X    =         6091023
51
 Y    =        8866781
54  feet           Y    =         2770847
32  meter
 Z    =       -4033918
48                 Z    =        -1199889
98
 XDOT =      -9629
384422                 XDOT =       -2951
164283
 YDOT =      13115
121448  feet/sec       YDOT =        3964
577273  meter/sec
 ZDOT =     -19151
448364                 ZDOT =       -5851
658073

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8676577
02                 X    =        -2644620
68
 Y    =       20174457
45  feet           Y    =         6149174
63  meter
 Z    =       -3897896
16                 Z    =        -1188078
75
 XDOT =     -11732
000277                 XDOT =       -3575
913684
 YDOT =      -8742
081801  feet/sec       YDOT =       -2664
586533  meter/sec
 ZDOT =     -19217
173229                 ZDOT =       -5857
394400


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   20127
16053142  
00016717  00000-0  10270-3 0  9135
2 25544  51
6406 196
4835 0001321 256
8643 103
2360 15
49331209 25493


Satellite: ISS
Catalog Number: 25544
Epoch time:      20127
16053142   =   yrday
fracday
Element set:     913
Inclination:       51
6406  deg
RA of node:       196
4835  deg
Eccentricity:     
0001321     
Arg of perigee:   256
8643  deg
Mean anomaly:     103
2360  deg
Mean motion:   15
49331209  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2549
Checksum:              282


Coasting Arc #15 (Orbit 2564)
---------------------------------------

Vector Time (GMT): 2020/128/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6276604
20                 A    =         6802557
53  meter
 Y    =       -2238992
62  meter          E    =           
0012431
 Z    =        1334960
78                 I    =           51
58225
 XDOT =       2733
855802                 Wp   =           57
77309
 YDOT =      -4179
968243  meter/sec      RA   =          190
49068  deg
 ZDOT =       5809
981359                 TA   =          316
74572
                                          MA   =          316
84326
                                          Ha   =            228
049  n
mi
                                          Hp   =            222
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20592533
46                 X    =        -6257585
23
 Y    =       -7345776
33  feet           Y    =        -2309075
80  meter
 Z    =        4379792
57                 Z    =         1304516
97
 XDOT =       8969
343183                 XDOT =        2752
172128
 YDOT =     -13713
806572  feet/sec       YDOT =       -4149
294163  meter/sec
 ZDOT =      19061
618631                 ZDOT =        5823
305932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6793659
65                 X    =         2070707
46
 Y    =      -20810172
28  feet           Y    =        -6342940
51  meter
 Z    =        4240090
21                 Z    =         1292379
50
 XDOT =      12425
857341                 XDOT =        3787
401318
 YDOT =       7975
756020  feet/sec       YDOT =        2431
010435  meter/sec
 ZDOT =      19122
895732                 ZDOT =        5828
658619


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   20128
19254445  
00016717  00000-0  10270-3 0  9149
2 25544  51
6396 191
3753 0001381 257
5814 102
5182 15
49348869 25650


Satellite: ISS
Catalog Number: 25544
Epoch time:      20128
19254445   =   yrday
fracday
Element set:     914
Inclination:       51
6396  deg
RA of node:       191
3753  deg
Eccentricity:     
0001381     
Arg of perigee:   257
5814  deg
Mean anomaly:     102
5182  deg
Mean motion:   15
49348869  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2565
Checksum:              323


Coasting Arc #16 (Orbit 2579)
---------------------------------------

Vector Time (GMT): 2020/129/03:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6391686
89                 A    =         6802373
36  meter
 Y    =        1790209
87  meter          E    =           
0007810
 Z    =       -1470616
55                 I    =           51
61478
 XDOT =      -2540
927152                 Wp   =          150
94349
 YDOT =       4347
005961  meter/sec      RA   =          185
53835  deg
 ZDOT =      -5771
414775                 TA   =           45
07565
                                          MA   =           45
01231
                                          Ha   =            228
059  n
mi
                                          Hp   =            222
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20970101
34                 X    =         6378336
74
 Y    =        5873391
96  feet           Y    =         1861611
73  meter
 Z    =       -4824857
44                 Z    =        -1439599
91
 XDOT =      -8336
375169                 XDOT =       -2561
313034
 YDOT =      14261
830581  feet/sec       YDOT =        4318
477956  meter/sec
 ZDOT =     -18935
087845                 ZDOT =       -5783
807034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4947017
03                 X    =        -1507850
79
 Y    =       21239642
36  feet           Y    =         6473842
99  meter
 Z    =       -4682493
76                 Z    =        -1427224
10
 XDOT =     -13057
988044                 XDOT =       -3980
074756
 YDOT =      -7213
807633  feet/sec       YDOT =       -2198
768567  meter/sec
 ZDOT =     -18992
100782                 ZDOT =       -5788
792318


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   20129
16005532  
00016717  00000-0  10270-3 0  9159
2 25544  51
6394 186
5865 0001343 266
8276  93
2720 15
49357056 25800


Satellite: ISS
Catalog Number: 25544
Epoch time:      20129
16005532   =   yrday
fracday
Element set:     915
Inclination:       51
6394  deg
RA of node:       186
5865  deg
Eccentricity:     
0001343     
Arg of perigee:   266
8276  deg
Mean anomaly:      93
2720  deg
Mean motion:   15
49357056  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2580
Checksum:              313


Coasting Arc #17 (Orbit 2593)
---------------------------------------

Vector Time (GMT): 2020/130/00:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 935485
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6611001
79                 A    =         6802787
12  meter
 Y    =        1058203
28  meter          E    =           
0008547
 Z    =       -1181127
61                 I    =           51
64864
 XDOT =      -1778
759860                 Wp   =          149
62820
 YDOT =       4602
639356  meter/sec      RA   =          181
07040  deg
 ZDOT =      -5858
206881                 TA   =           43
17102
                                          MA   =           43
10404
                                          Ha   =            228
092  n
mi
                                          Hp   =            222
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21689638
42                 X    =         6604414
64
 Y    =        3471795
55  feet           Y    =         1132095
50  meter
 Z    =       -3875090
59                 Z    =        -1149029
31
 XDOT =      -5835
826311                 XDOT =       -1801
639445
 YDOT =      15100
522821  feet/sec       YDOT =        4582
620659  meter/sec
 ZDOT =     -19219
838849                 ZDOT =       -5866
902654

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14371408
33                 X    =        -4380405
26
 Y    =       16645625
13  feet           Y    =         5073586
54  meter
 Z    =       -3727719
56                 Z    =        -1136208
92
 XDOT =      -8629
883143                 XDOT =       -2630
388382
 YDOT =     -11744
316035  feet/sec       YDOT =       -3579
667527  meter/sec
 ZDOT =     -19259
895630                 ZDOT =       -5870
416188


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   20130
06306405  
00016717  00000-0  10270-3 0  9164
2 25544  51
6419 182
1197 0001394 270
1544  89
9447 15
49323178 25941


Satellite: ISS
Catalog Number: 25544
Epoch time:      20130
06306405   =   yrday
fracday
Element set:     916
Inclination:       51
6419  deg
RA of node:       182
1197  deg
Eccentricity:     
0001394     
Arg of perigee:   270
1544  deg
Mean anomaly:      89
9447  deg
Mean motion:   15
49323178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2594
Checksum:              309
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