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

 
Date: January 14th 2021

  • 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) : 16464 4774 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


021/16:17:19 647 2 1 2 2 2 2
N/A -0 8 -0 2 228 4
000/00:06:39 293 -0 0 0 0 223 7

026/07:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 223 5

Coasting Arc #1 (Orbit 2460)
---------------------------------------

Vector Time (GMT): 2021/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6316181
33                 A    =         6801544
09  meter
 Y    =        1389538
20  meter          E    =           
0006234
 Z    =       -2100192
28                 I    =           51
83987
 XDOT =        683
310003                 Wp   =           40
95677
 YDOT =       5243
741695  meter/sec      RA   =           27
19164  deg
 ZDOT =       5538
291346                 TA   =          295
91341
                                          MA   =          295
97765
                                          Ha   =            228
549  n
mi
                                          Hp   =            222
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20722379
69                 X    =         6310374
91
 Y    =        4558852
37  feet           Y    =         1460138
10  meter
 Z    =       -6890394
62                 Z    =        -2069525
51
 XDOT =       2241
830718                 XDOT =         597
721001
 YDOT =      17203
876951  feet/sec       YDOT =        5250
903656  meter/sec
 ZDOT =      18170
247197                 ZDOT =        5541
403338

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3655779
68                 X    =         1114281
65
 Y    =       20946996
73  feet           Y    =         6384644
60  meter
 Z    =       -6748058
65                 Z    =        -2056808
28
 XDOT =     -13590
316149                 XDOT =       -4142
328362
 YDOT =       8214
949746  feet/sec       YDOT =        2503
916682  meter/sec
 ZDOT =      18184
414411                 ZDOT =        5542
609513


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   21013
50407040  
00016717  00000-0  10270-3 0  9004
2 25544  51
6444  27
8241 0000339 209
5978 150
5153 15
49324000 24616


Satellite: ISS
Catalog Number: 25544
Epoch time:      21013
50407040   =   yrday
fracday
Element set:     900
Inclination:       51
6444  deg
RA of node:        27
8241  deg
Eccentricity:     
0000339     
Arg of perigee:   209
5978  deg
Mean anomaly:     150
5153  deg
Mean motion:   15
49324000  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2461
Checksum:              264


Coasting Arc #2 (Orbit 2476)
---------------------------------------

Vector Time (GMT): 2021/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6429669
72                 A    =         6801790
54  meter
 Y    =        -942453
56  meter          E    =           
0013770
 Z    =        1986630
37                 I    =           51
80882
 XDOT =       -979
604783                 Wp   =          112
30632
 YDOT =      -5150
640065  meter/sec      RA   =           22
25475  deg
 ZDOT =      -5588
042037                 TA   =           45
85615
                                          MA   =           45
74301
                                          Ha   =            228
581  n
mi
                                          Hp   =            222
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21094716
92                 X    =        -6428302
67
 Y    =       -3092039
23  feet           Y    =        -1014347
32  meter
 Z    =        6517816
17                 Z    =         1955401
73
 XDOT =      -3213
926452                 XDOT =        -894
793281
 YDOT =     -16898
425410  feet/sec       YDOT =       -5161
119884  meter/sec
 ZDOT =     -18333
471250                 ZDOT =       -5592
595010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5509135
50                 X    =        -1679184
50
 Y    =      -20641364
03  feet           Y    =        -6291487
76  meter
 Z    =        6372851
26                 Z    =         1942445
06
 XDOT =      12800
356909                 XDOT =        3901
548786
 YDOT =      -9109
941254  feet/sec       YDOT =       -2776
710094  meter/sec
 ZDOT =     -18354
334759                 ZDOT =       -5594
401235


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   21014
53611874  
00016717  00000-0  10270-3 0  9011
2 25544  51
6435  22
7163 0000153 267
5718  92
5415 15
49308010 24779


Satellite: ISS
Catalog Number: 25544
Epoch time:      21014
53611874   =   yrday
fracday
Element set:     901
Inclination:       51
6435  deg
RA of node:        22
7163  deg
Eccentricity:     
0000153     
Arg of perigee:   267
5718  deg
Mean anomaly:      92
5415  deg
Mean motion:   15
49308010  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2477
Checksum:              284


Coasting Arc #3 (Orbit 2491)
---------------------------------------

Vector Time (GMT): 2021/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6511155
91                 A    =         6801884
20  meter
 Y    =         459085
09  meter          E    =           
0007033
 Z    =       -1904327
16                 I    =           51
77673
 XDOT =       1284
219247                 Wp   =           38
40899
 YDOT =       5038
491610  meter/sec      RA   =           17
31689  deg
 ZDOT =       5622
102173                 TA   =          300
70539
                                          MA   =          300
77466
                                          Ha   =            228
581  n
mi
                                          Hp   =            222
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21362060
07                 X    =         6514788
20
 Y    =        1506184
69  feet           Y    =          531917
99  meter
 Z    =       -6247792
53                 Z    =        -1872690
66
 XDOT =       4213
317740                 XDOT =        1200
473766
 YDOT =      16530
484286  feet/sec       YDOT =        5052
383960  meter/sec
 ZDOT =      18445
217103                 ZDOT =        5628
137231

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7418324
58                 X    =         2261105
33
 Y    =       20134259
67  feet           Y    =         6136922
35  meter
 Z    =       -6100914
90                 Z    =        -1859558
86
 XDOT =     -11925
984760                 XDOT =       -3635
040155
 YDOT =       9974
742670  feet/sec       YDOT =        3040
301566  meter/sec
 ZDOT =      18472
969339                 ZDOT =        5630
561055


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   21015
50366183  
00016717  00000-0  10270-3 0  9020
2 25544  51
6429  17
9291 0000138 224
5815 135
5324 15
49318972 24926


Satellite: ISS
Catalog Number: 25544
Epoch time:      21015
50366183   =   yrday
fracday
Element set:     902
Inclination:       51
6429  deg
RA of node:        17
9291  deg
Eccentricity:     
0000138     
Arg of perigee:   224
5815  deg
Mean anomaly:     135
5324  deg
Mean motion:   15
49318972  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2492
Checksum:              300


Coasting Arc #4 (Orbit 2507)
---------------------------------------

Vector Time (GMT): 2021/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6556557
20                 A    =         6802073
25  meter
 Y    =           3688
66  meter          E    =           
0013587
 Z    =        1786661
92                 I    =           51
74370
 XDOT =      -1554
921557                 Wp   =          114
56262
 YDOT =      -4916
468318  meter/sec      RA   =           12
37568  deg
 ZDOT =      -5667
584819                 TA   =           45
87608
                                          MA   =           45
76439
                                          Ha   =            228
509  n
mi
                                          Hp   =            222
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21511014
45                 X    =        -6564789
48
 Y    =          12101
89  feet           Y    =          -69677
62  meter
 Z    =        5861751
69                 Z    =         1754793
70
 XDOT =      -5101
448677                 XDOT =       -1472
299499
 YDOT =     -16130
145400  feet/sec       YDOT =       -4933
394272  meter/sec
 ZDOT =     -18594
438383                 ZDOT =       -5674
937408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9199300
44                 X    =        -2803946
77
 Y    =      -19488703
65  feet           Y    =        -5940156
87  meter
 Z    =        5713783
65                 Z    =         1741561
26
 XDOT =      11049
860961                 XDOT =        3367
997621
 YDOT =     -10705
447972  feet/sec       YDOT =       -3263
020542  meter/sec
 ZDOT =     -18628
315027                 ZDOT =       -5677
910420


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   21016
53570568  
00016717  00000-0  10270-3 0  9039
2 25544  51
6421  12
8212 0000319 299
0089  61
1029 15
49317968 25084


Satellite: ISS
Catalog Number: 25544
Epoch time:      21016
53570568   =   yrday
fracday
Element set:     903
Inclination:       51
6421  deg
RA of node:        12
8212  deg
Eccentricity:     
0000319     
Arg of perigee:   299
0089  deg
Mean anomaly:      61
1029  deg
Mean motion:   15
49317968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2508
Checksum:              297


Coasting Arc #5 (Orbit 2522)
---------------------------------------

Vector Time (GMT): 2021/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6564387
13                 A    =         6802188
97  meter
 Y    =        -497122
63  meter          E    =           
0007711
 Z    =       -1700197
49                 I    =           51
71105
 XDOT =       1832
754290                 Wp   =           36
57976
 YDOT =       4776
276550  meter/sec      RA   =            7
43339  deg
 ZDOT =       5699
014828                 TA   =          304
84265
                                          MA   =          304
91515
                                          Ha   =            228
560  n
mi
                                          Hp   =            222
331

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21536703
18                 X    =         6577716
59
 Y    =       -1630979
75  feet           Y    =         -423640
33  meter
 Z    =       -5578075
76                 Z    =        -1668278
79
 XDOT =       6012
973394                 XDOT =        1751
526509
 YDOT =      15670
198656  feet/sec       YDOT =        4796
317322  meter/sec
 ZDOT =      18697
555210                 ZDOT =        5707
720300

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10995929
83                 X    =         3351559
41
 Y    =       18633592
20  feet           Y    =         5679518
90  meter
 Z    =       -5429859
75                 Z    =        -1655021
25
 XDOT =     -10099
643073                 XDOT =       -3078
371209
 YDOT =      11401
109443  feet/sec       YDOT =        3475
058158  meter/sec
 ZDOT =      18737
719807                 ZDOT =        5711
256997


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   21017
50324443  
00016717  00000-0  10270-3 0  9047
2 25544  51
6425   8
0340 0000155 272
4021  87
7111 15
49318368 25234


Satellite: ISS
Catalog Number: 25544
Epoch time:      21017
50324443   =   yrday
fracday
Element set:     904
Inclination:       51
6425  deg
RA of node:         8
0340  deg
Eccentricity:     
0000155     
Arg of perigee:   272
4021  deg
Mean anomaly:      87
7111  deg
Mean motion:   15
49318368  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2523
Checksum:              265


Coasting Arc #6 (Orbit 2538)
---------------------------------------

Vector Time (GMT): 2021/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6539917
55                 A    =         6802331
98  meter
 Y    =         963406
53  meter          E    =           
0013460
 Z    =        1576924
66                 I    =           51
67820
 XDOT =      -2074
176405                 Wp   =          116
65556
 YDOT =      -4631
541939  meter/sec      RA   =            2
48762  deg
 ZDOT =      -5740
537374                 TA   =           46
14117
                                          MA   =           46
03003
                                          Ha   =            228
485  n
mi
                                          Hp   =            222
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21456422
41                 X    =        -6557864
21
 Y    =        3160782
58  feet           Y    =          890172
07  meter
 Z    =        5173637
34                 Z    =         1545113
51
 XDOT =      -6805
040700                 XDOT =       -1994
347362
 YDOT =     -15195
347570  feet/sec       YDOT =       -4654
290332  meter/sec
 ZDOT =     -18833
784035                 ZDOT =       -5750
418936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12637377
59                 X    =        -3851872
69
 Y    =      -17668391
23  feet           Y    =        -5385325
65  meter
 Z    =        5025910
00                 Z    =         1531897
37
 XDOT =       9174
411346                 XDOT =        2796
360578
 YDOT =     -11963
183511  feet/sec       YDOT =       -3646
378334  meter/sec
 ZDOT =     -18879
414222                 ZDOT =       -5754
445455


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   21018
53528102  
00016717  00000-0  10270-3 0  9050
2 25544  51
6429   2
9261 0000423 318
9511  41
1608 15
49328353 25398


Satellite: ISS
Catalog Number: 25544
Epoch time:      21018
53528102   =   yrday
fracday
Element set:     905
Inclination:       51
6429  deg
RA of node:         2
9261  deg
Eccentricity:     
0000423     
Arg of perigee:   318
9511  deg
Mean anomaly:      41
1608  deg
Mean motion:   15
49328353  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2539
Checksum:              282


Coasting Arc #7 (Orbit 2553)
---------------------------------------

Vector Time (GMT): 2021/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6473079
87                 A    =         6802455
84  meter
 Y    =       -1454778
01  meter          E    =           
0008504
 Z    =       -1485707
46                 I    =           51
64375
 XDOT =       2323
309902                 Wp   =           35
40008
 YDOT =       4469
764687  meter/sec      RA   =          357
54097  deg
 ZDOT =       5769
058144                 TA   =          308
41914
                                          MA   =          308
49546
                                          Ha   =            228
542  n
mi
                                          Hp   =            222
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21237138
69                 X    =         6496083
12
 Y    =       -4772893
74  feet           Y    =        -1382262
70  meter
 Z    =       -4874368
31                 Z    =        -1454208
60
 XDOT =       7622
407814                 XDOT =        2245
132750
 YDOT =      14664
582306  feet/sec       YDOT =        4495
308306  meter/sec
 ZDOT =      18927
356117                 ZDOT =        5780
153917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14255702
92                 X    =         4345138
25
 Y    =       16491702
24  feet           Y    =         5026670
84  meter
 Z    =       -4728079
13                 Z    =        -1441118
52
 XDOT =      -8183
397448                 XDOT =       -2494
299542
 YDOT =      12492
298833  feet/sec       YDOT =        3807
652684  meter/sec
 ZDOT =      18978
628166                 ZDOT =        5784
685865


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   21019
50281374  
00016717  00000-0  10270-3 0  9066
2 25544  51
6421 358
1391 0000274 318
3319  41
7810 15
49322637 25541


Satellite: ISS
Catalog Number: 25544
Epoch time:      21019
50281374   =   yrday
fracday
Element set:     906
Inclination:       51
6421  deg
RA of node:       358
1391  deg
Eccentricity:     
0000274     
Arg of perigee:   318
3319  deg
Mean anomaly:      41
7810  deg
Mean motion:   15
49322637  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2554
Checksum:              291


Coasting Arc #8 (Orbit 2569)
---------------------------------------

Vector Time (GMT): 2021/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6378029
67                 A    =         6802603
28  meter
 Y    =        1914601
97  meter          E    =           
0013283
 Z    =        1358285
97                 I    =           51
61060
 XDOT =      -2537
446615                 Wp   =          119
26867
 YDOT =      -4308
352013  meter/sec      RA   =          352
59095  deg
 ZDOT =      -5805
445610                 TA   =           45
95887
                                          MA   =           45
84953
                                          Ha   =            228
467  n
mi
                                          Hp   =            222
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20925294
20                 X    =        -6405562
97
 Y    =        6281502
51  feet           Y    =         1843124
24  meter
 Z    =        4456318
79                 Z    =         1327237
74
 XDOT =      -8324
956085                 XDOT =       -2460
881681
 YDOT =     -14135
013165  feet/sec       YDOT =       -4336
299240  meter/sec
 ZDOT =     -19046
737566                 ZDOT =       -5817
585527

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15701000
97                 X    =        -4785665
10
 Y    =      -15233786
67  feet           Y    =        -4643258
18  meter
 Z    =        4312110
93                 Z    =         1314331
41
 XDOT =       7236
502045                 XDOT =        2205
685823
 YDOT =     -12900
842420  feet/sec       YDOT =       -3932
176770  meter/sec
 ZDOT =     -19102
860953                 ZDOT =       -5822
552019


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   21020
53484601  
00016717  00000-0  10270-3 0  9070
2 25544  51
6423 353
0314 0000495 319
8466  40
2647 15
49324734 25706


Satellite: ISS
Catalog Number: 25544
Epoch time:      21020
53484601   =   yrday
fracday
Element set:     907
Inclination:       51
6423  deg
RA of node:       353
0314  deg
Eccentricity:     
0000495     
Arg of perigee:   319
8466  deg
Mean anomaly:      40
2647  deg
Mean motion:   15
49324734  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2570
Checksum:              290


Coasting Arc #9 (Orbit 2584)
---------------------------------------

Vector Time (GMT): 2021/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6237295
71                 A    =         6802678
59  meter
 Y    =       -2392161
93  meter          E    =           
0009196
 Z    =       -1262574
89                 I    =           51
57778
 XDOT =       2758
553338                 Wp   =           35
12940
 YDOT =       4130
261879  meter/sec      RA   =          347
63914  deg
 ZDOT =       5830
695278                 TA   =          311
15850
                                          MA   =          311
23780
                                          Ha   =            228
501  n
mi
                                          Hp   =            222
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20463568
60                 X    =         6269714
80
 Y    =       -7848300
31  feet           Y    =        -2322230
67  meter
 Z    =       -4142306
08                 Z    =        -1232198
39
 XDOT =       9050
371843                 XDOT =        2683
840722
 YDOT =      13550
727951  feet/sec       YDOT =        4160
691974  meter/sec
 ZDOT =      19129
577683                 ZDOT =        5843
913792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17082260
68                 X    =         5206673
05
 Y    =       13773122
31  feet           Y    =         4198047
68  meter
 Z    =       -4001203
43                 Z    =        -1219566
81
 XDOT =      -6230
802567                 XDOT =       -1899
148623
 YDOT =      13274
716656  feet/sec       YDOT =        4046
133637  meter/sec
 ZDOT =      19190
712767                 ZDOT =        5849
329252


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   21021
50237294  
00016717  00000-0  10270-3 0  9083
2 25544  51
6427 348
2439 0000391 320
6671  39
4450 15
49331542 25850


Satellite: ISS
Catalog Number: 25544
Epoch time:      21021
50237294   =   yrday
fracday
Element set:     908
Inclination:       51
6427  deg
RA of node:       348
2439  deg
Eccentricity:     
0000391     
Arg of perigee:   320
6671  deg
Mean anomaly:      39
4450  deg
Mean motion:   15
49331542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2585
Checksum:              297


Coasting Arc #10 (Orbit 2587)
---------------------------------------

Vector Time (GMT): 2021/021/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -199093
49                 A    =         6792751
54  meter
 Y    =       -4270044
26  meter          E    =           
0012333
 Z    =       -5289838
59                 I    =           51
53814
 XDOT =       7523
289358                 Wp   =           95
05280
 YDOT =      -1207
254554  meter/sec      RA   =          346
74831  deg
 ZDOT =        691
695750                 TA   =          181
57539
                                          MA   =          181
57928
                                          Ha   =            228
403  n
mi
                                          Hp   =            223
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -653193
85                 X    =         -125635
13
 Y    =      -14009331
56  feet           Y    =        -4271859
66  meter
 Z    =      -17355113
49                 Z    =        -5290627
50
 XDOT =      24682
707869                 XDOT =        7532
870291
 YDOT =      -3960
808905  feet/sec       YDOT =       -1123
070182  meter/sec
 ZDOT =       2269
343013                 ZDOT =         728
263606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1875737
74                 X    =         -571724
86
 Y    =      -13894249
50  feet           Y    =        -4234967
25  meter
 Z    =      -17358555
12                 Z    =        -5290887
60
 XDOT =      23159
490340                 XDOT =        7059
012656
 YDOT =      -6172
457105  feet/sec       YDOT =       -1881
364926  meter/sec
 ZDOT =       2439
116744                 ZDOT =         743
442784


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   21021
69587876  
00016717  00000-0  10270-3 0  9098
2 25544  51
6462 347
2868 0002215 276
9241  83
1657 15
48918060 25880


Satellite: ISS
Catalog Number: 25544
Epoch time:      21021
69587876   =   yrday
fracday
Element set:     909
Inclination:       51
6462  deg
RA of node:       347
2868  deg
Eccentricity:     
0002215     
Arg of perigee:   276
9241  deg
Mean anomaly:      83
1657  deg
Mean motion:   15
48918060  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2588
Checksum:              342


Coasting Arc #11 (Orbit 2603)
---------------------------------------

Vector Time (GMT): 2021/022/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         592460
06                 A    =         6792651
90  meter
 Y    =        4228024
99  meter          E    =           
0001929
 Z    =        5283016
00                 I    =           51
50534
 XDOT =      -7397
823952                 Wp   =           14
98308
 YDOT =       1873
641430  meter/sec      RA   =          341
79591  deg
 ZDOT =       -667
982649                 TA   =           81
42449
                                          MA   =           81
40263
                                          Ha   =            228
333  n
mi
                                          Hp   =            223
654

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1943766
59                 X    =          519475
46
 Y    =       13871473
07  feet           Y    =         4234241
87  meter
 Z    =       17332729
65                 Z    =         5285716
91
 XDOT =     -24271
075959                 XDOT =       -7414
981132
 YDOT =       6147
117551  feet/sec       YDOT =        1790
817749  meter/sec
 ZDOT =      -2191
544125                 ZDOT =        -703
959414

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3381289
21                 X    =         1030616
95
 Y    =       13577028
56  feet           Y    =         4138278
31  meter
 Z    =       17345047
98                 Z    =         5286770
62
 XDOT =     -22414
881404                 XDOT =       -6832
055852
 YDOT =       8603
355359  feet/sec       YDOT =        2622
302713  meter/sec
 ZDOT =      -2358
596974                 ZDOT =        -718
900358


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   21022
72818342  
00016717  00000-0  10270-3 0  9100
2 25544  51
6462 342
1814 0002280 281
5264  78
5630 15
48945206 26044


Satellite: ISS
Catalog Number: 25544
Epoch time:      21022
72818342   =   yrday
fracday
Element set:     910
Inclination:       51
6462  deg
RA of node:       342
1814  deg
Eccentricity:     
0002280     
Arg of perigee:   281
5264  deg
Mean anomaly:      78
5630  deg
Mean motion:   15
48945206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2604
Checksum:              288


Coasting Arc #12 (Orbit 2618)
---------------------------------------

Vector Time (GMT): 2021/023/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -986830
20                 A    =         6792699
47  meter
 Y    =       -4158994
44  meter          E    =           
0012406
 Z    =       -5289996
31                 I    =           51
47276
 XDOT =       7194
682698                 Wp   =           92
87161
 YDOT =      -2522
048164  meter/sec      RA   =          336
84144  deg
 ZDOT =        641
389385                 TA   =          183
27594
                                          MA   =          183
28407
                                          Ha   =            228
426  n
mi
                                          Hp   =            223
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3237631
89                 X    =         -914554
33
 Y    =      -13644994
88  feet           Y    =        -4169625
33  meter
 Z    =      -17355630
92                 Z    =        -5294614
67
 XDOT =      23604
602026                 XDOT =        7219
234833
 YDOT =      -8274
436233  feet/sec       YDOT =       -2441
454816  meter/sec
 ZDOT =       2104
295882                 ZDOT =         676
397229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4867530
10                 X    =        -1483623
18
 Y    =      -13123955
83  feet           Y    =        -4000181
74  meter
 Z    =      -17376852
54                 Z    =        -5296464
65
 XDOT =      21355
191400                 XDOT =        6509
062339
 YDOT =     -10918
844986  feet/sec       YDOT =       -3328
063952  meter/sec
 ZDOT =       2266
875263                 ZDOT =         690
943580


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   21023
69596900  
00016717  00000-0  10270-3 0  9111
2 25544  51
6455 337
3953 0002231 286
6246  73
4659 15
48927366 26196


Satellite: ISS
Catalog Number: 25544
Epoch time:      21023
69596900   =   yrday
fracday
Element set:     911
Inclination:       51
6455  deg
RA of node:       337
3953  deg
Eccentricity:     
0002231     
Arg of perigee:   286
6246  deg
Mean anomaly:      73
4659  deg
Mean motion:   15
48927366  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2619
Checksum:              331


Coasting Arc #13 (Orbit 2634)
---------------------------------------

Vector Time (GMT): 2021/024/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1361807
31                 A    =         6792633
66  meter
 Y    =        4046587
30  meter          E    =           
0002086
 Z    =        5282816
12                 I    =           51
44224
 XDOT =      -6953
555870                 Wp   =           12
92907
 YDOT =       3153
791435  meter/sec      RA   =          331
88481  deg
 ZDOT =       -621
243626                 TA   =           83
03543
                                          MA   =           83
01171
                                          Ha   =            228
330  n
mi
                                          Hp   =            223
651

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4467871
75                 X    =         1290795
49
 Y    =       13276205
06  feet           Y    =         4061418
46  meter
 Z    =       17332073
87                 Z    =         5289259
04
 XDOT =     -22813
503512                 XDOT =       -6985
288136
 YDOT =      10347
084762  feet/sec       YDOT =        3075
854401  meter/sec
 ZDOT =      -2038
200873                 ZDOT =        -655
097450

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6255253
00                 X    =         1906601
12
 Y    =       12492438
28  feet           Y    =         3807695
19  meter
 Z    =       17361770
63                 Z    =         5291867
69
 XDOT =     -20116
966662                 XDOT =       -6131
651439
 YDOT =      13133
508432  feet/sec       YDOT =        4003
093370  meter/sec
 ZDOT =      -2195
447978                 ZDOT =        -669
172544


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   21024
72826931  
00016717  00000-0  10270-3 0  9127
2 25544  51
6458 332
2902 0002334 287
9363  72
1533 15
48943694 26352


Satellite: ISS
Catalog Number: 25544
Epoch time:      21024
72826931   =   yrday
fracday
Element set:     912
Inclination:       51
6458  deg
RA of node:       332
2902  deg
Eccentricity:     
0002334     
Arg of perigee:   287
9363  deg
Mean anomaly:      72
1533  deg
Mean motion:   15
48943694  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2635
Checksum:              313


Coasting Arc #14 (Orbit 2649)
---------------------------------------

Vector Time (GMT): 2021/025/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1733456
63                 A    =         6792643
08  meter
 Y    =       -3907774
20  meter          E    =           
0012389
 Z    =       -5289463
62                 I    =           51
41299
 XDOT =       6639
623364                 Wp   =           90
95748
 YDOT =      -3754
144900  meter/sec      RA   =          326
92534  deg
 ZDOT =        598
592098                 TA   =          184
78106
                                          MA   =          184
79290
                                          Ha   =            228
419  n
mi
                                          Hp   =            223
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5687193
66                 X    =        -1663937
24
 Y    =      -12820781
50  feet           Y    =        -3926769
72  meter
 Z    =      -17353883
28                 Z    =        -5297715
44
 XDOT =      21783
541222                 XDOT =        6678
202335
 YDOT =     -12316
748360  feet/sec       YDOT =       -3679
680204  meter/sec
 ZDOT =       1963
884836                 ZDOT =         630
937414

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7597046
40                 X    =        -2315579
74
 Y    =      -11733610
55  feet           Y    =        -3576404
50  meter
 Z    =      -17391985
05                 Z    =        -5301077
04
 XDOT =      18596
622150                 XDOT =        5668
250431
 YDOT =     -15169
312901  feet/sec       YDOT =       -4623
606572  meter/sec
 ZDOT =       2114
152847                 ZDOT =         644
393788


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   21025
69604874  
00016717  00000-0  10270-3 0  9135
2 25544  51
6459 327
5034 0002385 294
0900  66
0000 15
48939505 26502


Satellite: ISS
Catalog Number: 25544
Epoch time:      21025
69604874   =   yrday
fracday
Element set:     913
Inclination:       51
6459  deg
RA of node:       327
5034  deg
Eccentricity:     
0002385     
Arg of perigee:   294
0900  deg
Mean anomaly:      66
0000  deg
Mean motion:   15
48939505  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2650
Checksum:              301


Coasting Arc #15 (Orbit 2659)
---------------------------------------

Vector Time (GMT): 2021/026/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6008978
18                 A    =         6803134
23  meter
 Y    =        2648481
21  meter          E    =           
0005597
 Z    =       -1768367
64                 I    =           51
42771
 XDOT =       -605
831453                 Wp   =          149
32466
 YDOT =      -5136
292909  meter/sec      RA   =          323
81294  deg
 ZDOT =      -5646
618563                 TA   =           50
10151
                                          MA   =           50
05232
                                          Ha   =            228
572  n
mi
                                          Hp   =            223
480

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19714495
34                 X    =        -6029558
20
 Y    =        8689242
81  feet           Y    =         2581169
60  meter
 Z    =       -5801731
10                 Z    =        -1797605
91
 XDOT =      -1987
636000                 XDOT =        -520
923467
 YDOT =     -16851
354687  feet/sec       YDOT =       -5142
592437  meter/sec
 ZDOT =     -18525
651455                 ZDOT =       -5649
355676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3277108
36                 X    =          998862
63
 Y    =      -21256310
03  feet           Y    =        -6478923
30  meter
 Z    =       -5937524
35                 Z    =        -1809757
42
 XDOT =      13650
331721                 XDOT =        4160
621108
 YDOT =       7271
418305  feet/sec       YDOT =        2216
328299  meter/sec
 ZDOT =     -18538
110391                 ZDOT =       -5650
416047


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   21026
34123314  
00016717  00000-0  10270-3 0  9144
2 25544  51
6435 324
3114 0001964 296
7814  63
3134 15
48918267 26606


Satellite: ISS
Catalog Number: 25544
Epoch time:      21026
34123314   =   yrday
fracday
Element set:     914
Inclination:       51
6435  deg
RA of node:       324
3114  deg
Eccentricity:     
0001964     
Arg of perigee:   296
7814  deg
Mean anomaly:      63
3134  deg
Mean motion:   15
48918267  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2660
Checksum:              294


Coasting Arc #16 (Orbit 2675)
---------------------------------------

Vector Time (GMT): 2021/027/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5749333
42                 A    =         6803064
81  meter
 Y    =       -3178870
46  meter          E    =           
0012694
 Z    =        1740561
33                 I    =           51
40024
 XDOT =       1075
977238                 Wp   =           57
53619
 YDOT =       5055
776718  meter/sec      RA   =          318
85119  deg
 ZDOT =       5655
924285                 TA   =          321
59300
                                          MA   =          321
68329
                                          Ha   =            228
448  n
mi
                                          Hp   =            223
460

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18862642
45                 X    =         5775998
81
 Y    =      -10429365
04  feet           Y    =        -3114428
34  meter
 Z    =        5710503
06                 Z    =         1768553
01
 XDOT =       3530
109050                 XDOT =         991
889589
 YDOT =      16587
193957  feet/sec       YDOT =        5067
338393  meter/sec
 ZDOT =      18556
182036                 ZDOT =        5660
947042

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -982875
11                 X    =         -299580
33
 Y    =       21496580
31  feet           Y    =         6552157
68  meter
 Z    =        5840528
40                 Z    =         1780193
06
 XDOT =     -14343
037361                 XDOT =       -4371
757788
 YDOT =      -5724
245257  feet/sec       YDOT =       -1744
749954  meter/sec
 ZDOT =      18579
261074                 ZDOT =        5662
958775


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   21027
37352357  
00016717  00000-0  10270-3 0  9150
2 25544  51
6425 319
2068 0002108 296
8380  63
2554 15
48959458 26765


Satellite: ISS
Catalog Number: 25544
Epoch time:      21027
37352357   =   yrday
fracday
Element set:     915
Inclination:       51
6425  deg
RA of node:       319
2068  deg
Eccentricity:     
0002108     
Arg of perigee:   296
8380  deg
Mean anomaly:      63
2554  deg
Mean motion:   15
48959458  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2676
Checksum:              329


Coasting Arc #17 (Orbit 2690)
---------------------------------------

Vector Time (GMT): 2021/028/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5456851
58                 A    =         6803145
85  meter
 Y    =        3666588
25  meter          E    =           
0005413
 Z    =       -1740946
17                 I    =           51
37495
 XDOT =      -1517
937071                 Wp   =          147
03902
 YDOT =      -4936
961007  meter/sec      RA   =          313
88659  deg
 ZDOT =      -5652
603865                 TA   =           52
08816
                                          MA   =           52
03923
                                          Ha   =            228
616  n
mi
                                          Hp   =            223
438

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17903056
36                 X    =        -5488990
68
 Y    =       12029489
00  feet           Y    =         3605386
23  meter
 Z    =       -5711765
65                 Z    =        -1767530
34
 XDOT =      -4980
108502                 XDOT =       -1435
161438
 YDOT =     -16197
378631  feet/sec       YDOT =       -4953
472427  meter/sec
 ZDOT =     -18545
288271                 ZDOT =       -5659
776493

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1252802
96                 X    =         -381854
34
 Y    =      -21499590
67  feet           Y    =        -6553075
24  meter
 Z    =       -5835270
78                 Z    =        -1778590
53
 XDOT =      14843
295707                 XDOT =        4524
236531
 YDOT =       4166
345630  feet/sec       YDOT =        1269
902148  meter/sec
 ZDOT =     -18578
360846                 ZDOT =       -5662
684386


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   21028
34129669  
00016717  00000-0  10270-3 0  9167
2 25544  51
6420 314
4201 0002108 306
2916  53
8039 15
48930364 26912


Satellite: ISS
Catalog Number: 25544
Epoch time:      21028
34129669   =   yrday
fracday
Element set:     916
Inclination:       51
6420  deg
RA of node:       314
4201  deg
Eccentricity:     
0002108     
Arg of perigee:   306
2916  deg
Mean anomaly:      53
8039  deg
Mean motion:   15
48930364  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2691
Checksum:              293
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