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

 
Date: December 17th 2020

  • spaceflight nasa gov will be taken offline in the next 30 days *
  • *
  • Current information about the International Space Station can be *
  • found at www nasa gov/station *
  • *
  • Predicted ISS and visiting vehicle sightings opportunities can be *
  • found at spotthestation nasa gov *
  • *
  • Updated ISS trajectory information will be made available as a CCSDS *
  • Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
  • system *
  • Included in the OEM are a sequence of events with ISS maneuver *
  • details (in the comment section), predicted post-maneuver state *
  • vectors, predicted coasting state vectors at 4-minute intervals, *
  • and ISS ballistic details *
  • *
  • OEMs will be provided in xml and txt formats *
  • Links to the OEMs and more details to follow *
  • *

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14570 0291 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 497 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


355/04:48:45 000 0 0 -0 0 0 1
N/A 0 0 -0 1 229 1
000/00:07:30 000 0 1 -0 0 222 1

358/10:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 222 2

361/14:12:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 9
000/00:00:00 000 0 0 0 0 222 3

Coasting Arc #1 (Orbit 1995)
---------------------------------------

Vector Time (GMT): 2020/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4076616
39                 A    =         6796605
23  meter
 Y    =        3598074
52  meter          E    =           
0008896
 Z    =       -4087468
73                 I    =           51
66508
 XDOT =      -6102
125772                 Wp   =          112
70556
 YDOT =      -2533
485347  meter/sec      RA   =          175
04000  deg
 ZDOT =       3859
144696                 TA   =          197
29397
                                          MA   =          197
32430
                                          Ha   =            229
245  n
mi
                                          Hp   =            221
907

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13374725
69                 X    =        -4096693
44
 Y    =       11804706
42  feet           Y    =         3552375
33  meter
 Z    =      -13410330
49                 Z    =        -4107319
62
 XDOT =     -20020
097678                 XDOT =       -6092
087697
 YDOT =      -8311
959799  feet/sec       YDOT =       -2601
668248  meter/sec
 ZDOT =      12661
235879                 ZDOT =        3829
526673

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10023396
35                 X    =        -3055131
21
 Y    =      -14672752
25  feet           Y    =        -4472254
89  meter
 Z    =      -13502340
98                 Z    =        -4115513
53
 XDOT =       9725
303411                 XDOT =        2964
272480
 YDOT =     -18158
537254  feet/sec       YDOT =       -5534
722155  meter/sec
 ZDOT =      12524
008687                 ZDOT =        3817
317848


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   20349
50906283  
00016717  00000-0  10270-3 0  9008
2 25544  51
6387 176
2393 0001553 128
2424 231
8866 15
49187353 19965


Satellite: ISS
Catalog Number: 25544
Epoch time:      20349
50906283   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:       176
2393  deg
Eccentricity:     
0001553     
Arg of perigee:   128
2424  deg
Mean anomaly:     231
8866  deg
Mean motion:   15
49187353  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1996
Checksum:              327


Coasting Arc #2 (Orbit 2011)
---------------------------------------

Vector Time (GMT): 2020/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3830559
70                 A    =         6796791
17  meter
 Y    =       -3899839
19  meter          E    =           
0011525
 Z    =        4030021
76                 I    =           51
69917
 XDOT =       6247
140367                 Wp   =           84
39580
 YDOT =       2061
642430  meter/sec      RA   =          170
09525  deg
 ZDOT =      -3932
114577                 TA   =           46
47830
                                          MA   =           46
38259
                                          Ha   =            229
108  n
mi
                                          Hp   =            222
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12567453
07                 X    =         3854308
64
 Y    =      -12794747
99  feet           Y    =        -3856871
06  meter
 Z    =       13221856
18                 Z    =         4048686
11
 XDOT =      20495
867345                 XDOT =        6242
722127
 YDOT =       6763
918734  feet/sec       YDOT =        2131
478452  meter/sec
 ZDOT =     -12900
638375                 ZDOT =       -3901
778745

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11346862
03                 X    =         3458523
55
 Y    =       13805774
67  feet           Y    =         4208000
12  meter
 Z    =       13308389
89                 Z    =         4056397
24
 XDOT =      -7975
727968                 XDOT =       -2431
001885
 YDOT =      18889
420917  feet/sec       YDOT =        5757
495495  meter/sec
 ZDOT =     -12760
054019                 ZDOT =       -3889
264465


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   20350
54118101  
00016717  00000-0  10270-3 0  9019
2 25544  51
6385 171
1323 0001434 135
3519 224
7746 15
49186604 20128


Satellite: ISS
Catalog Number: 25544
Epoch time:      20350
54118101   =   yrday
fracday
Element set:     901
Inclination:       51
6385  deg
RA of node:       171
1323  deg
Eccentricity:     
0001434     
Arg of perigee:   135
3519  deg
Mean anomaly:     224
7746  deg
Mean motion:   15
49186604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2012
Checksum:              271


Coasting Arc #3 (Orbit 2026)
---------------------------------------

Vector Time (GMT): 2020/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3547855
40                 A    =         6796907
98  meter
 Y    =        4205111
99  meter          E    =           
0008475
 Z    =       -4000292
96                 I    =           51
73256
 XDOT =      -6343
482956                 Wp   =          113
81976
 YDOT =      -1567
567723  meter/sec      RA   =          165
15212  deg
 ZDOT =       3981
549995                 TA   =          197
67531
                                          MA   =          197
70482
                                          Ha   =            229
228  n
mi
                                          Hp   =            221
949

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11639945
52                 X    =        -3575183
53
 Y    =       13796299
18  feet           Y    =         4165285
22  meter
 Z    =      -13124320
72                 Z    =        -4017592
60
 XDOT =     -20811
951957                 XDOT =       -6344
822459
 YDOT =      -5142
938723  feet/sec       YDOT =       -1638
513289  meter/sec
 ZDOT =      13062
828068                 ZDOT =        3950
732478

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12665808
66                 X    =        -3860538
48
 Y    =      -12778544
09  feet           Y    =        -3894900
24  meter
 Z    =      -13204548
44                 Z    =        -4024746
36
 XDOT =       6125
539355                 XDOT =        1867
064395
 YDOT =     -19410
906359  feet/sec       YDOT =       -5916
444258  meter/sec
 ZDOT =      12919
979323                 ZDOT =        3938
009698


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   20351
50879220  
00016717  00000-0  10270-3 0  9023
2 25544  51
6382 166
3439 0001672 137
3771 222
7509 15
49189902 20270


Satellite: ISS
Catalog Number: 25544
Epoch time:      20351
50879220   =   yrday
fracday
Element set:     902
Inclination:       51
6382  deg
RA of node:       166
3439  deg
Eccentricity:     
0001672     
Arg of perigee:   137
3771  deg
Mean anomaly:     222
7509  deg
Mean motion:   15
49189902  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2027
Checksum:              307


Coasting Arc #4 (Orbit 2042)
---------------------------------------

Vector Time (GMT): 2020/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3256655
98                 A    =         6797128
91  meter
 Y    =       -4471147
88  meter          E    =           
0011766
 Z    =        3940497
20                 I    =           51
76647
 XDOT =       6412
382799                 Wp   =           87
05971
 YDOT =       1087
670469  meter/sec      RA   =          160
21172  deg
 ZDOT =      -4054
381150                 TA   =           45
32329
                                          MA   =           45
22748
                                          Ha   =            229
127  n
mi
                                          Hp   =            222
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10684566
86                 X    =         3287271
18
 Y    =      -14669120
35  feet           Y    =        -4434559
05  meter
 Z    =       12928140
42                 Z    =         3956390
26
 XDOT =      21038
001309                 XDOT =        6419
437221
 YDOT =       3568
472668  feet/sec       YDOT =        1159
418414  meter/sec
 ZDOT =     -13301
775426                 ZDOT =       -4023
215309

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13826151
01                 X    =         4214210
83
 Y    =       11673429
96  feet           Y    =         3558061
45  meter
 Z    =       13001863
58                 Z    =         3962968
02
 XDOT =      -4302
524645                 XDOT =       -1311
409512
 YDOT =      19790
660505  feet/sec       YDOT =        6032
193322  meter/sec
 ZDOT =     -13157
281395                 ZDOT =       -4010
339369


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   20352
54090679  
00016717  00000-0  10270-3 0  9032
2 25544  51
6390 161
2367 0001559 143
3731 216
7526 15
49179333 20437


Satellite: ISS
Catalog Number: 25544
Epoch time:      20352
54090679   =   yrday
fracday
Element set:     903
Inclination:       51
6390  deg
RA of node:       161
2367  deg
Eccentricity:     
0001559     
Arg of perigee:   143
3731  deg
Mean anomaly:     216
7526  deg
Mean motion:   15
49179333  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2043
Checksum:              303


Coasting Arc #5 (Orbit 2057)
---------------------------------------

Vector Time (GMT): 2020/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2929350
50                 A    =         6797205
95  meter
 Y    =        4734817
70  meter          E    =           
0008074
 Z    =       -3908036
39                 I    =           51
79942
 XDOT =      -6430
865533                 Wp   =          113
49477
 YDOT =       -594
188600  meter/sec      RA   =          155
27339  deg
 ZDOT =       4104
092715                 TA   =          199
52921
                                          MA   =          199
56016
                                          Ha   =            229
228  n
mi
                                          Hp   =            221
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9610730
00                 X    =        -2963096
19
 Y    =       15534178
80  feet           Y    =         4701871
43  meter
 Z    =      -12821641
69                 Z    =        -3922347
19
 XDOT =     -21098
640200                 XDOT =       -6443
678271
 YDOT =      -1949
437664  feet/sec       YDOT =        -666
175341  meter/sec
 ZDOT =      13464
871113                 ZDOT =        4072
823267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14951141
60                 X    =        -4557107
96
 Y    =      -10413120
49  feet           Y    =        -3173919
13  meter
 Z    =      -12888041
90                 Z    =        -3928275
17
 XDOT =       2423
223985                 XDOT =         738
598671
 YDOT =     -19950
374961  feet/sec       YDOT =       -6080
874288  meter/sec
 ZDOT =      13319
868630                 ZDOT =        4059
895959


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   20353
50851279  
00016717  00000-0  10270-3 0  9041
2 25544  51
6400 156
4487 0001760 139
6352 220
4929 15
49198114 20582


Satellite: ISS
Catalog Number: 25544
Epoch time:      20353
50851279   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       156
4487  deg
Eccentricity:     
0001760     
Arg of perigee:   139
6352  deg
Mean anomaly:     220
4929  deg
Mean motion:   15
49198114  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2058
Checksum:              307


Coasting Arc #6 (Orbit 2073)
---------------------------------------

Vector Time (GMT): 2020/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2598154
35                 A    =         6797462
16  meter
 Y    =       -4958504
59  meter          E    =           
0012155
 Z    =        3845512
42                 I    =           51
82920
 XDOT =       6425
343030                 Wp   =           89
57571
 YDOT =        118
851319  meter/sec      RA   =          150
33784  deg
 ZDOT =      -4176
431010                 TA   =           44
35128
                                          MA   =           44
25398
                                          Ha   =            229
184  n
mi
                                          Hp   =            222
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8524128
45                 X    =         2634729
69
 Y    =      -16268059
69  feet           Y    =        -4929246
08  meter
 Z    =       12616510
58                 Z    =         3858221
38
 XDOT =      21080
521753                 XDOT =        6443
822919
 YDOT =        389
932149  feet/sec       YDOT =         190
807909  meter/sec
 ZDOT =     -13702
201476                 ZDOT =       -4145
174689

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15906027
94                 X    =         4848157
32
 Y    =        9100384
55  feet           Y    =         2773797
21  meter
 Z    =       12675493
97                 Z    =         3863490
56
 XDOT =       -597
683543                 XDOT =        -182
173944
 YDOT =      19980
154101  feet/sec       YDOT =        6089
950970  meter/sec
 ZDOT =     -13557
234855                 ZDOT =       -4132
245184


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   20354
54062415  
00016717  00000-0  10270-3 0  9053
2 25544  51
6389 151
3421 0001745 145
6484 214
4779 15
49177796 20743


Satellite: ISS
Catalog Number: 25544
Epoch time:      20354
54062415   =   yrday
fracday
Element set:     905
Inclination:       51
6389  deg
RA of node:       151
3421  deg
Eccentricity:     
0001745     
Arg of perigee:   145
6484  deg
Mean anomaly:     214
4779  deg
Mean motion:   15
49177796  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2074
Checksum:              320


Coasting Arc #7 (Orbit 2084)
---------------------------------------

Vector Time (GMT): 2020/355/04:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1494652
93                 A    =         6791817
08  meter
 Y    =       -3987107
31  meter          E    =           
0003572
 Z    =        5288293
98                 I    =           51
83541
 XDOT =       6711
865340                 Wp   =           82
10654
 YDOT =      -3606
316088  meter/sec      RA   =          146
89262  deg
 ZDOT =       -821
025322                 TA   =           15
73065
                                          MA   =           15
71955
                                          Ha   =            229
068  n
mi
                                          Hp   =            222
093

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4903716
95                 X    =        -1475644
01
 Y    =      -13081060
74  feet           Y    =        -4003715
83  meter
 Z    =       17350045
85                 Z    =         5281079
39
 XDOT =      22020
555576                 XDOT =        6755
681449
 YDOT =     -11831
745695  feet/sec       YDOT =       -3531
014114  meter/sec
 ZDOT =      -2693
652631                 ZDOT =        -788
316001

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         602147
96                 X    =          183534
70
 Y    =       13998463
31  feet           Y    =         4266731
62  meter
 Z    =       17316614
10                 Z    =         5278103
98
 XDOT =     -23636
353779                 XDOT =       -7204
360632
 YDOT =       4165
024480  feet/sec       YDOT =        1269
499461  meter/sec
 ZDOT =      -2541
902482                 ZDOT =        -774
771877


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   20355
25019835  
00016717  00000-0  10270-3 0  9061
2 25544  51
6429 147
8366 0001236 143
8826 216
2407 15
49239204 20854


Satellite: ISS
Catalog Number: 25544
Epoch time:      20355
25019835   =   yrday
fracday
Element set:     906
Inclination:       51
6429  deg
RA of node:       147
8366  deg
Eccentricity:     
0001236     
Arg of perigee:   143
8826  deg
Mean anomaly:     216
2407  deg
Mean motion:   15
49239204  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2085
Checksum:              309


Coasting Arc #8 (Orbit 2099)
---------------------------------------

Vector Time (GMT): 2020/356/04:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1756237
31                 A    =         6791933
30  meter
 Y    =        3899207
52  meter          E    =           
0015285
 Z    =       -5289917
44                 I    =           51
86435
 XDOT =      -6392
342892                 Wp   =          100
45120
 YDOT =       4102
870285  meter/sec      RA   =          141
95933  deg
 ZDOT =        901
512582                 TA   =          178
16942
                                          MA   =          178
16382
                                          Ha   =            229
017  n
mi
                                          Hp   =            222
195

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5761933
44                 X    =         1738199
83
 Y    =       12792675
58  feet           Y    =         3918746
63  meter
 Z    =      -17355372
18                 Z    =        -5281429
87
 XDOT =     -20972
253584                 XDOT =       -6442
126337
 YDOT =      13460
860515  feet/sec       YDOT =        4031
108077  meter/sec
 ZDOT =       2957
718445                 ZDOT =         870
340790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1748100
67                 X    =         -532821
08
 Y    =      -13969985
53  feet           Y    =        -4258051
59  meter
 Z    =      -17316033
54                 Z    =        -5277927
02
 XDOT =      23056
117616                 XDOT =        7027
504649
 YDOT =      -6373
887131  feet/sec       YDOT =       -1942
760798  meter/sec
 ZDOT =       2813
075426                 ZDOT =         857
425390


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   20356
21779993  
00016717  00000-0  10270-3 0  9077
2 25544  51
6440 143
0488 0001220 145
3255 214
7975 15
49219397 21008


Satellite: ISS
Catalog Number: 25544
Epoch time:      20356
21779993   =   yrday
fracday
Element set:     907
Inclination:       51
6440  deg
RA of node:       143
0488  deg
Eccentricity:     
0001220     
Arg of perigee:   145
3255  deg
Mean anomaly:     214
7975  deg
Mean motion:   15
49219397  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2100
Checksum:              309


Coasting Arc #9 (Orbit 2115)
---------------------------------------

Vector Time (GMT): 2020/357/04:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2003454
52                 A    =         6791885
33  meter
 Y    =       -3783027
12  meter          E    =           
0003654
 Z    =        5270048
64                 I    =           51
89070
 XDOT =       6059
427671                 Wp   =           77
04659
 YDOT =      -4586
479000  meter/sec      RA   =          137
02794  deg
 ZDOT =       -987
419327                 TA   =           22
38636
                                          MA   =           22
37042
                                          Ha   =            229
010  n
mi
                                          Hp   =            222
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6573013
50                 X    =        -1986601
40
 Y    =      -12411506
28  feet           Y    =        -3805337
39  meter
 Z    =       17290185
83                 Z    =         5260357
32
 XDOT =      19880
012044                 XDOT =        6115
061015
 YDOT =     -15047
503282  feet/sec       YDOT =       -4518
406977  meter/sec
 ZDOT =      -3239
564721                 ZDOT =        -957
850415

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2873805
35                 X    =          875935
87
 Y    =       13803720
79  feet           Y    =         4207374
10  meter
 Z    =       17245261
85                 Z    =         5256355
81
 XDOT =     -22360
399488                 XDOT =       -6815
449764
 YDOT =       8536
676004  feet/sec       YDOT =        2601
978846  meter/sec
 ZDOT =      -3102
332624                 ZDOT =        -945
590984


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   20357
24990299  
00016717  00000-0  10270-3 0  9086
2 25544  51
6442 137
9420 0001129 150
1955 209
9260 15
49249091 21161


Satellite: ISS
Catalog Number: 25544
Epoch time:      20357
24990299   =   yrday
fracday
Element set:     908
Inclination:       51
6442  deg
RA of node:       137
9420  deg
Eccentricity:     
0001129     
Arg of perigee:   150
1955  deg
Mean anomaly:     209
9260  deg
Mean motion:   15
49249091  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2116
Checksum:              311


Coasting Arc #10 (Orbit 2130)
---------------------------------------

Vector Time (GMT): 2020/358/04:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2253953
89                 A    =         6792021
09  meter
 Y    =        3664600
03  meter          E    =           
0015018
 Z    =       -5268830
85                 I    =           51
91417
 XDOT =      -5668
231602                 Wp   =          101
57450
 YDOT =       5023
837741  meter/sec      RA   =          132
09824  deg
 ZDOT =       1069
039215                 TA   =          178
65539
                                          MA   =          178
65134
                                          Ha   =            228
963  n
mi
                                          Hp   =            222
244

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7394861
85                 X    =         2238400
61
 Y    =       12022965
97  feet           Y    =         3689718
85  meter
 Z    =      -17286190
47                 Z    =        -5257919
52
 XDOT =     -18596
560373                 XDOT =       -5729
181175
 YDOT =      16482
407286  feet/sec       YDOT =        4960
110619  meter/sec
 ZDOT =       3507
346507                 ZDOT =        1041
357619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4006803
41                 X    =        -1221273
68
 Y    =      -13598804
38  feet           Y    =        -4144915
58  meter
 Z    =      -17235606
15                 Z    =        -5253412
75
 XDOT =      21372
531313                 XDOT =        6514
347544
 YDOT =     -10581
204935  feet/sec       YDOT =       -3225
151264  meter/sec
 ZDOT =       3378
844756                 ZDOT =        1029
871882


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   20358
21750033  
00016717  00000-0  10270-3 0  9095
2 25544  51
6435 133
1544 0001122 148
6515 211
4702 15
49226224 21314


Satellite: ISS
Catalog Number: 25544
Epoch time:      20358
21750033   =   yrday
fracday
Element set:     909
Inclination:       51
6435  deg
RA of node:       133
1544  deg
Eccentricity:     
0001122     
Arg of perigee:   148
6515  deg
Mean anomaly:     211
4702  deg
Mean motion:   15
49226224  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2131
Checksum:              263


Coasting Arc #11 (Orbit 2134)
---------------------------------------

Vector Time (GMT): 2020/358/10:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5376165
62                 A    =         6797549
04  meter
 Y    =       -1613112
79  meter          E    =           
0006603
 Z    =       -3839894
79                 I    =           51
93482
 XDOT =      -1105
758477                 Wp   =           90
46474
 YDOT =       6301
392637  meter/sec      RA   =          130
90395  deg
 ZDOT =      -4201
615925                 TA   =          135
35593
                                          MA   =          135
30274
                                          Ha   =            229
109  n
mi
                                          Hp   =            222
230

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17638338
65                 X    =         5412456
35
 Y    =       -5292364
80  feet           Y    =        -1552789
40  meter
 Z    =      -12598080
03                 Z    =        -3813691
52
 XDOT =      -3627
816525                 XDOT =       -1155
731367
 YDOT =      20673
860356  feet/sec       YDOT =        6288
748198  meter/sec
 ZDOT =     -13784
829149                 ZDOT =       -4207
108086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         213184
49                 X    =           64978
63
 Y    =       18496590
64  feet           Y    =         5637760
83  meter
 Z    =      -12476474
79                 Z    =        -3802829
51
 XDOT =     -17554
992323                 XDOT =       -5350
761660
 YDOT =      -9099
105883  feet/sec       YDOT =       -2773
407473  meter/sec
 ZDOT =     -13810
391571                 ZDOT =       -4209
407351


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   20358
47552650  
00016717  00000-0  10270-3 0  9100
2 25544  51
6402 131
8728 0001594 152
6231 207
5003 15
49218922 21350


Satellite: ISS
Catalog Number: 25544
Epoch time:      20358
47552650   =   yrday
fracday
Element set:     910
Inclination:       51
6402  deg
RA of node:       131
8728  deg
Eccentricity:     
0001594     
Arg of perigee:   152
6231  deg
Mean anomaly:     207
5003  deg
Mean motion:   15
49218922  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2135
Checksum:              284


Coasting Arc #12 (Orbit 2150)
---------------------------------------

Vector Time (GMT): 2020/359/10:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5204759
90                 A    =         6797369
28  meter
 Y    =        2004016
87  meter          E    =           
0012129
 Z    =        3878187
14                 I    =           51
95613
 XDOT =        636
847943                 Wp   =          105
17800
 YDOT =      -6408
399952  meter/sec      RA   =          125
97614  deg
 ZDOT =       4152
264959                 TA   =          301
28415
                                          MA   =          301
40288
                                          Ha   =            229
070  n
mi
                                          Hp   =            222
213

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17075983
93                 X    =        -5245620
63
 Y    =        6574858
49  feet           Y    =         1945584
66  meter
 Z    =       12723711
08                 Z    =         3852805
38
 XDOT =       2089
396137                 XDOT =         688
291940
 YDOT =     -21024
934226  feet/sec       YDOT =       -6400
991021  meter/sec
 ZDOT =      13622
916532                 ZDOT =        4155
482847

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1915370
62                 X    =         -583804
96
 Y    =      -18279319
72  feet           Y    =        -5571536
65  meter
 Z    =       12605897
08                 Z    =         3842277
43
 XDOT =      18460
821661                 XDOT =        5626
858442
 YDOT =       7502
445345  feet/sec       YDOT =        2286
745341  meter/sec
 ZDOT =      13637
942882                 ZDOT =        4156
844990


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   20359
50762666  
00016717  00000-0  10270-3 0  9116
2 25544  51
6407 126
7653 0001640 163
1572 196
9632 15
49234553 21517


Satellite: ISS
Catalog Number: 25544
Epoch time:      20359
50762666   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       126
7653  deg
Eccentricity:     
0001640     
Arg of perigee:   163
1572  deg
Mean anomaly:     196
9632  deg
Mean motion:   15
49234553  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2151
Checksum:              307


Coasting Arc #13 (Orbit 2165)
---------------------------------------

Vector Time (GMT): 2020/360/10:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5015941
56                 A    =         6797190
72  meter
 Y    =       -2347151
38  meter          E    =           
0006710
 Z    =       -3947199
35                 I    =           51
97542
 XDOT =       -175
306318                 Wp   =           87
63755
 YDOT =       6474
396117  meter/sec      RA   =          121
05000  deg
 ZDOT =      -4078
400599                 TA   =          139
82211
                                          MA   =          139
77248
                                          Ha   =            229
015  n
mi
                                          Hp   =            222
326

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16456501
20                 X    =         5060988
61
 Y    =       -7700627
88  feet           Y    =        -2290807
20  meter
 Z    =      -12950129
11                 Z    =        -3922724
66
 XDOT =       -575
151962                 XDOT =        -227
881371
 YDOT =      21241
457077  feet/sec       YDOT =        6472
142206  meter/sec
 ZDOT =     -13380
579392                 ZDOT =       -4079
379140

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3471317
23                 X    =         1058057
49
 Y    =       17916364
21  feet           Y    =         5460907
81  meter
 Z    =      -12836502
46                 Z    =        -3912565
95
 XDOT =     -19186
916882                 XDOT =       -5848
172266
 YDOT =      -5859
056839  feet/sec       YDOT =       -1785
840525  meter/sec
 ZDOT =     -13385
231457                 ZDOT =       -4079
818548


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   20360
47521918  
00016717  00000-0  10270-3 0  9128
2 25544  51
6418 121
9775 0001537 162
4292 197
6912 15
49219789 21666


Satellite: ISS
Catalog Number: 25544
Epoch time:      20360
47521918   =   yrday
fracday
Element set:     912
Inclination:       51
6418  deg
RA of node:       121
9775  deg
Eccentricity:     
0001537     
Arg of perigee:   162
4292  deg
Mean anomaly:     197
6912  deg
Mean motion:   15
49219789  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2166
Checksum:              328


Coasting Arc #14 (Orbit 2181)
---------------------------------------

Vector Time (GMT): 2020/361/10:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4793009
44                 A    =         6796977
66  meter
 Y    =        2698648
63  meter          E    =           
0011731
 Z    =        3985900
90                 I    =           51
99200
 XDOT =       -309
109804                 Wp   =          107
16262
 YDOT =      -6513
061018  meter/sec      RA   =          116
12515  deg
 ZDOT =       4024
830361                 TA   =          300
97178
                                          MA   =          301
08699
                                          Ha   =            229
008  n
mi
                                          Hp   =            222
238

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15725096
58                 X    =        -4842191
59
 Y    =        8853834
07  feet           Y    =         2644774
24  meter
 Z    =       13077102
68                 Z    =         3962499
17
 XDOT =      -1014
139778                 XDOT =        -255
806171
 YDOT =     -21368
310427  feet/sec       YDOT =       -6516
220189  meter/sec
 ZDOT =      13204
824020                 ZDOT =        4023
457442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5067053
23                 X    =        -1544437
82
 Y    =      -17401850
78  feet           Y    =        -5304084
12  meter
 Z    =       12968431
50                 Z    =         3952777
92
 XDOT =      19798
936349                 XDOT =        6034
715799
 YDOT =       4103
345800  feet/sec       YDOT =        1250
699800  meter/sec
 ZDOT =      13198
580431                 ZDOT =        4022
927315


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   20361
50731391  
00016717  00000-0  10270-3 0  9132
2 25544  51
6424 116
8705 0001547 166
4444 193
6748 15
49244034 21825


Satellite: ISS
Catalog Number: 25544
Epoch time:      20361
50731391   =   yrday
fracday
Element set:     913
Inclination:       51
6424  deg
RA of node:       116
8705  deg
Eccentricity:     
0001547     
Arg of perigee:   166
4444  deg
Mean anomaly:     193
6748  deg
Mean motion:   15
49244034  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2182
Checksum:              301


Coasting Arc #15 (Orbit 2183)
---------------------------------------

Vector Time (GMT): 2020/361/14:12:30
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2334738
58                 A    =         6793383
54  meter
 Y    =       -4053738
74  meter          E    =           
0006376
 Z    =        4921714
37                 I    =           51
98420
 XDOT =       4693
088903                 Wp   =           69
98037
 YDOT =      -5578
313113  meter/sec      RA   =          115
39155  deg
 ZDOT =      -2363
654272                 TA   =           43
09162
                                          MA   =           43
04172
                                          Ha   =            228
920  n
mi
                                          Hp   =            222
255

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7659903
46                 X    =        -2313141
84
 Y    =      -13299667
77  feet           Y    =        -4079727
36  meter
 Z    =       16147356
85                 Z    =         4910425
01
 XDOT =      15397
273304                 XDOT =        4766
599798
 YDOT =     -18301
552209  feet/sec       YDOT =       -5525
420282  meter/sec
 ZDOT =      -7754
771232                 ZDOT =       -2340
679224

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5757080
56                 X    =         1754758
16
 Y    =      -14286292
79  feet           Y    =        -4354462
04  meter
 Z    =       16095038
94                 Z    =         4905767
87
 XDOT =      22888
274115                 XDOT =        6976
345950
 YDOT =        590
116985  feet/sec       YDOT =         179
867657  meter/sec
 ZDOT =      -7648
019727                 ZDOT =       -2331
116413


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   20361
63632468  
00016717  00000-0  10270-3 0  9142
2 25544  51
6443 116
2344 0001301 169
8099 190
3077 15
49251775 21841


Satellite: ISS
Catalog Number: 25544
Epoch time:      20361
63632468   =   yrday
fracday
Element set:     914
Inclination:       51
6443  deg
RA of node:       116
2344  deg
Eccentricity:     
0001301     
Arg of perigee:   169
8099  deg
Mean anomaly:     190
3077  deg
Mean motion:   15
49251775  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2184
Checksum:              307


Coasting Arc #16 (Orbit 2198)
---------------------------------------

Vector Time (GMT): 2020/362/14:12:30
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2625729
88                 A    =         6793545
64  meter
 Y    =        3917642
50  meter          E    =           
0012518
 Z    =       -4901580
08                 I    =           51
99715
 XDOT =      -4232
013582                 Wp   =          112
92498
 YDOT =       5887
902277  meter/sec      RA   =          110
46857  deg
 ZDOT =       2439
140565                 TA   =          180
94098
                                          MA   =          180
94334
                                          Ha   =            228
850  n
mi
                                          Hp   =            222
344

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8614599
33                 X    =         2605535
54
 Y    =       12853157
80  feet           Y    =         3946893
12  meter
 Z    =      -16081299
49                 Z    =        -4888873
77
 XDOT =     -13884
558997                 XDOT =       -4309
387314
 YDOT =      19317
264688  feet/sec       YDOT =        5840
143871  meter/sec
 ZDOT =       8002
429675                 ZDOT =        2418
396043

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4565073
81                 X    =        -1391434
50
 Y    =       14848089
71  feet           Y    =         4525697
74  meter
 Z    =      -16022406
61                 Z    =        -4883629
53
 XDOT =     -22707
868207                 XDOT =       -6921
358229
 YDOT =       1548
920018  feet/sec       YDOT =         472
110821  meter/sec
 ZDOT =       7905
998803                 ZDOT =        2409
748435


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   20362
60391366  
00016717  00000-0  10270-3 0  9150
2 25544  51
6434 111
4479 0001346 168
8132 191
3048 15
49241943 21994


Satellite: ISS
Catalog Number: 25544
Epoch time:      20362
60391366   =   yrday
fracday
Element set:     915
Inclination:       51
6434  deg
RA of node:       111
4479  deg
Eccentricity:     
0001346     
Arg of perigee:   168
8132  deg
Mean anomaly:     191
3048  deg
Mean motion:   15
49241943  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2199
Checksum:              308


Coasting Arc #17 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2020/363/14:12:30
000
Vector Time (MET): N/A
Weight (LBS)     : 996846
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2893542
27                 A    =         6793627
25  meter
 Y    =       -3758649
60  meter          E    =           
0006597
 Z    =        4859025
10                 I    =           52
00935
 XDOT =       3767
704577                 Wp   =           69
96730
 YDOT =      -6175
667091  meter/sec      RA   =          105
54524  deg
 ZDOT =      -2528
485410                 TA   =           44
80874
                                          MA   =           44
75548
                                          Ha   =            228
826  n
mi
                                          Hp   =            222
334

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9493248
93                 X    =        -2874899
15
 Y    =      -12331527
57  feet           Y    =        -3790903
82  meter
 Z    =       15941683
39                 Z    =         4845014
11
 XDOT =      12361
235488                 XDOT =        3848
764635
 YDOT =     -20261
374969  feet/sec       YDOT =       -6133
080266  meter/sec
 ZDOT =      -8295
555807                 ZDOT =       -2509
987549

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3346872
22                 X    =         1020126
65
 Y    =      -15266086
32  feet           Y    =        -4653103
11  meter
 Z    =       15876733
66                 Z    =         4839228
42
 XDOT =      22406
846359                 XDOT =        6829
606770
 YDOT =      -3642
573054  feet/sec       YDOT =       -1110
256267  meter/sec
 ZDOT =      -8209
521853                 ZDOT =       -2502
262261


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   20363
63600455  
00016717  00000-0  10270-3 0  9167
2 25544  51
6443 106
3409 0001271 181
2196 178
8951 15
49262295 22151


Satellite: ISS
Catalog Number: 25544
Epoch time:      20363
63600455   =   yrday
fracday
Element set:     916
Inclination:       51
6443  deg
RA of node:       106
3409  deg
Eccentricity:     
0001271     
Arg of perigee:   181
2196  deg
Mean anomaly:     178
8951  deg
Mean motion:   15
49262295  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              302
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