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

 
Date: February 10th 2021

  • *
  • !!! The status of spaceflight nasa gov has been updated !!! *
  • *
  • spaceflight nasa gov will be taken offline by February 20, 2021 *
  • *
  • 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 are provided in xml and txt formats at the following links: *
  • https://nasa-public-data s3 amazonaws com/iss-coords/current/ISS_OEM/ISS OEM_J2K_EPH xml *
  • https://nasa-public-data s3 amazonaws com/iss-coords/current/ISS_OEM/ISS OEM_J2K_EPH txt *
  • *
  • The above links are permanent links to the most current posted ISS ephemeris data *
  • Older archived ephemeris data can be found by searching on data nasa gov *
  • *

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15144 822 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 84 1 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


040/05:21:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 222 9

040/09:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 8

040/14:00:36 808 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 7

046/21:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 7
000/00:00:00 000 0 0 0 0 222 4

050/19:24:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 222 2

053/09:36:25 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 222 1

054/01:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 1
000/00:00:00 000 0 0 0 0 222 0

Coasting Arc #1 (Orbit 2865)
---------------------------------------

Vector Time (GMT): 2021/039/14:00:36
808
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4164993
95                 A    =         6792603
13  meter
 Y    =        -857743
60  meter          E    =           
0003289
 Z    =        5295113
10                 I    =           51
23391
 XDOT =       1588
214814                 Wp   =           37
48003
 YDOT =       7495
426455  meter/sec      RA   =          257
84129  deg
 ZDOT =        -32
504051                 TA   =           52
84673
                                          MA   =           52
81670
                                          Ha   =            229
160  n
mi
                                          Hp   =            223
003

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13664678
31                 X    =         4148556
08
 Y    =       -2814119
44  feet           Y    =         -811259
87  meter
 Z    =       17372418
32                 Z    =         5315304
44
 XDOT =       5210
678525                 XDOT =        1504
438511
 YDOT =      24591
294143  feet/sec       YDOT =        7512
718596  meter/sec
 ZDOT =       -106
640587                 ZDOT =         -24
992369

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13833910
95                 X    =         4216576
06
 Y    =          30223
65  feet           Y    =            9212
17  meter
 Z    =       17466127
61                 Z    =         5323675
70
 XDOT =         48
640210                 XDOT =          14
825536
 YDOT =      24128
577289  feet/sec       YDOT =        7354
390358  meter/sec
 ZDOT =        -71
872593                 ZDOT =         -21
906766


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   21039
63213375  
00016717  00000-0  10270-3 0  9002
2 25544  51
6398 258
5773 0002602 350
9235   9
1867 15
48903546 28666


Satellite: ISS
Catalog Number: 25544
Epoch time:      21039
63213375   =   yrday
fracday
Element set:     900
Inclination:       51
6398  deg
RA of node:       258
5773  deg
Eccentricity:     
0002602     
Arg of perigee:   350
9235  deg
Mean anomaly:       9
1867  deg
Mean motion:   15
48903546  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2866
Checksum:              322


Coasting Arc #2 (Orbit 2875)
---------------------------------------

Vector Time (GMT): 2021/040/05:21:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2566946
77                 A    =         6795658
44  meter
 Y    =       -4368362
71  meter          E    =           
0007760
 Z    =        4522399
40                 I    =           51
25094
 XDOT =       4134
949986                 Wp   =           95
86032
 YDOT =       5653
790844  meter/sec      RA   =          254
68661  deg
 ZDOT =       3108
790661                 TA   =          322
77006
                                          MA   =          322
82384
                                          Ha   =            229
124  n
mi
                                          Hp   =            222
870

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8421741
36                 X    =         2593637
84
 Y    =      -14331898
65  feet           Y    =        -4339508
26  meter
 Z    =       14837268
39                 Z    =         4534932
82
 XDOT =      13566
108878                 XDOT =        4056
320022
 YDOT =      18549
182558  feet/sec       YDOT =        5699
591021  meter/sec
 ZDOT =      10199
444427                 ZDOT =        3128
685306

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2551470
54                 X    =          777688
22
 Y    =       16373402
67  feet           Y    =         4990613
13  meter
 Z    =       14895477
93                 Z    =         4540141
67
 XDOT =     -20967
030297                 XDOT =       -6390
750834
 YDOT =      -6111
503585  feet/sec       YDOT =       -1862
786293  meter/sec
 ZDOT =      10291
715375                 ZDOT =        3136
914846


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   21040
27730988  
00016717  00000-0  10270-3 0  9019
2 25544  51
6409 255
3885 0002633 351
9254   8
1853 15
48973703 28761


Satellite: ISS
Catalog Number: 25544
Epoch time:      21040
27730988   =   yrday
fracday
Element set:     901
Inclination:       51
6409  deg
RA of node:       255
3885  deg
Eccentricity:     
0002633     
Arg of perigee:   351
9254  deg
Mean anomaly:       8
1853  deg
Mean motion:   15
48973703  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2876
Checksum:              324


Coasting Arc #3 (Orbit 2877)
---------------------------------------

Vector Time (GMT): 2021/040/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4477015
84                 A    =         6795728
75  meter
 Y    =       -2400923
95  meter          E    =           
0008821
 Z    =       -4521750
90                 I    =           51
25500
 XDOT =        584
662725                 Wp   =           94
21425
 YDOT =      -6962
116045  meter/sec      RA   =          253
78432  deg
 ZDOT =       3122
472870                 TA   =          207
30642
                                          MA   =          207
35282
                                          Ha   =            229
255  n
mi
                                          Hp   =            222
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14688372
18                 X    =        -4427871
89
 Y    =       -7877047
08  feet           Y    =        -2450714
16  meter
 Z    =      -14835140
74                 Z    =        -4543378
53
 XDOT =       1918
184794                 XDOT =         647
305098
 YDOT =     -22841
588073  feet/sec       YDOT =       -6955
227826  meter/sec
 ZDOT =      10244
333564                 ZDOT =        3125
464629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4870245
98                 X    =         1484450
97
 Y    =      -15845800
36  feet           Y    =        -4829799
95  meter
 Z    =      -14935490
07                 Z    =        -4552337
37
 XDOT =      21605
464144                 XDOT =        6585
345471
 YDOT =      -3014
154980  feet/sec       YDOT =        -918
714438  meter/sec
 ZDOT =      10258
284119                 ZDOT =        3126
724999


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   21040
40634637  
00016717  00000-0  10270-3 0  9029
2 25544  51
6434 254
7516 0002790 352
1639   7
9467 15
48942294 28788


Satellite: ISS
Catalog Number: 25544
Epoch time:      21040
40634637   =   yrday
fracday
Element set:     902
Inclination:       51
6434  deg
RA of node:       254
7516  deg
Eccentricity:     
0002790     
Arg of perigee:   352
1639  deg
Mean anomaly:       7
9467  deg
Mean motion:   15
48942294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2878
Checksum:              321


Coasting Arc #4 (Orbit 2880)
---------------------------------------

Vector Time (GMT): 2021/040/14:00:36
808
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4075601
38                 A    =         6792503
80  meter
 Y    =        1235039
92  meter          E    =           
0014841
 Z    =       -5304464
83                 I    =           51
24153
 XDOT =      -2238
405680                 Wp   =           80
48153
 YDOT =      -7314
380184  meter/sec      RA   =          252
86843  deg
 ZDOT =         19
288333                 TA   =          189
68942
                                          MA   =          189
71807
                                          Ha   =            229
309  n
mi
                                          Hp   =            222
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13371395
61                 X    =        -4063343
90
 Y    =        4051968
25  feet           Y    =         1189532
40  meter
 Z    =      -17403099
84                 Z    =        -5324232
01
 XDOT =      -7343
850656                 XDOT =       -2156
541375
 YDOT =     -23997
310314  feet/sec       YDOT =       -7338
953917  meter/sec
 ZDOT =         63
281931                 ZDOT =           8
613885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13777666
84                 X    =        -4199432
85
 Y    =        1478734
69  feet           Y    =          450718
33  meter
 Z    =      -17494850
43                 Z    =        -5332430
41
 XDOT =      -2577
574436                 XDOT =        -785
644688
 YDOT =     -23947
179449  feet/sec       YDOT =       -7299
100296  meter/sec
 ZDOT =         13
806676                 ZDOT =           4
208275


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   21040
59989920  
00016717  00000-0  10270-3 0  9038
2 25544  51
6390 253
7901 0002505 355
5322   4
5805 15
48941640 28813


Satellite: ISS
Catalog Number: 25544
Epoch time:      21040
59989920   =   yrday
fracday
Element set:     903
Inclination:       51
6390  deg
RA of node:       253
7901  deg
Eccentricity:     
0002505     
Arg of perigee:   355
5322  deg
Mean anomaly:       4
5805  deg
Mean motion:   15
48941640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2881
Checksum:              305


Coasting Arc #5 (Orbit 2896)
---------------------------------------

Vector Time (GMT): 2021/041/14:00:36
808
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3944362
20                 A    =         6792608
18  meter
 Y    =       -1583602
98  meter          E    =           
0003507
 Z    =        5296379
17                 I    =           51
25290
 XDOT =       2873
200047                 Wp   =           43
20659
 YDOT =       7103
111370  meter/sec      RA   =          247
89617  deg
 ZDOT =        -13
424906                 TA   =           46
93681
                                          MA   =           46
90745
                                          Ha   =            229
300  n
mi
                                          Hp   =            222
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12940820
87                 X    =         3936051
55
 Y    =       -5195547
85  feet           Y    =        -1539540
88  meter
 Z    =       17376572
08                 Z    =         5315518
41
 XDOT =       9426
509340                 XDOT =        2793
622555
 YDOT =      23304
171163  feet/sec       YDOT =        7134
796618  meter/sec
 ZDOT =        -44
044966                 ZDOT =            
338369

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13522572
51                 X    =         4121680
10
 Y    =       -2916015
38  feet           Y    =         -888801
49  meter
 Z    =       17465414
59                 Z    =         5323458
37
 XDOT =       5072
143205                 XDOT =        1545
989249
 YDOT =      23590
657340  feet/sec       YDOT =        7190
432357  meter/sec
 ZDOT =         19
797830                 ZDOT =           6
034379


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   21041
63218235  
00016717  00000-0  10270-3 0  9049
2 25544  51
6391 248
6837 0002575 359
6846    
4302 15
48901723 28970


Satellite: ISS
Catalog Number: 25544
Epoch time:      21041
63218235   =   yrday
fracday
Element set:     904
Inclination:       51
6391  deg
RA of node:       248
6837  deg
Eccentricity:     
0002575     
Arg of perigee:   359
6846  deg
Mean anomaly:        
4302  deg
Mean motion:   15
48901723  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2897
Checksum:              313


Coasting Arc #6 (Orbit 2911)
---------------------------------------

Vector Time (GMT): 2021/042/14:00:36
808
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3790204
77                 A    =         6792486
79  meter
 Y    =        1936883
94  meter          E    =           
0015345
 Z    =       -5306648
25                 I    =           51
26713
 XDOT =      -3480
024764                 Wp   =           80
65140
 YDOT =      -6811
356784  meter/sec      RA   =          242
92528  deg
 ZDOT =          1
920994                 TA   =          189
35273
                                          MA   =          189
38134
                                          Ha   =            229
470  n
mi
                                          Hp   =            222
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12435055
03                 X    =        -3785806
22
 Y    =        6354606
09  feet           Y    =         1894523
72  meter
 Z    =      -17410263
30                 Z    =        -5325048
21
 XDOT =     -11417
404081                 XDOT =       -3403
608783
 YDOT =     -22346
971077  feet/sec       YDOT =       -6849
845661  meter/sec
 ZDOT =          6
302474                 ZDOT =         -14
797368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13149879
90                 X    =        -4008083
39
 Y    =        4371592
06  feet           Y    =         1332461
26  meter
 Z    =      -17495677
23                 Z    =        -5332682
42
 XDOT =      -7502
705572                 XDOT =       -2286
824658
 YDOT =     -22885
665847  feet/sec       YDOT =       -6975
550950  meter/sec
 ZDOT =        -71
288456                 ZDOT =         -21
728721


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   21042
59994461  
00016717  00000-0  10270-3 0  9058
2 25544  51
6394 243
8970 0002524   6
9426 353
1758 15
48947609 29122


Satellite: ISS
Catalog Number: 25544
Epoch time:      21042
59994461   =   yrday
fracday
Element set:     905
Inclination:       51
6394  deg
RA of node:       243
8970  deg
Eccentricity:     
0002524     
Arg of perigee:     6
9426  deg
Mean anomaly:     353
1758  deg
Mean motion:   15
48947609  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2912
Checksum:              334


Coasting Arc #7 (Orbit 2927)
---------------------------------------

Vector Time (GMT): 2021/043/14:00:36
808
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3598970
05                 A    =         6792612
11  meter
 Y    =       -2255626
71  meter          E    =           
0003793
 Z    =        5298314
81                 I    =           51
28253
 XDOT =       4068
095386                 Wp   =           50
45699
 YDOT =       6493
569177  meter/sec      RA   =          237
95478  deg
 ZDOT =          3
524112                 TA   =           39
52306
                                          MA   =           39
49541
                                          Ha   =            229
474  n
mi
                                          Hp   =            222
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11807644
51                 X    =         3598190
43
 Y    =       -7400350
09  feet           Y    =        -2215384
65  meter
 Z    =       17382922
61                 Z    =         5315794
73
 XDOT =      13346
769638                 XDOT =        3995
162848
 YDOT =      21304
360816  feet/sec       YDOT =        6538
653761  meter/sec
 ZDOT =         11
562047                 ZDOT =          23
107301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12595536
32                 X    =         3839119
47
 Y    =       -5719311
99  feet           Y    =        -1743246
29  meter
 Z    =       17464065
50                 Z    =         5323047
17
 XDOT =       9867
840348                 XDOT =        3007
717738
 YDOT =      22021
059744  feet/sec       YDOT =        6712
019010  meter/sec
 ZDOT =        102
480979                 ZDOT =          31
236202


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   21043
63222641  
00016717  00000-0  10270-3 0  9069
2 25544  51
6382 238
7904 0002539  11
4932 348
6276 15
48900439 29289


Satellite: ISS
Catalog Number: 25544
Epoch time:      21043
63222641   =   yrday
fracday
Element set:     906
Inclination:       51
6382  deg
RA of node:       238
7904  deg
Eccentricity:     
0002539     
Arg of perigee:    11
4932  deg
Mean anomaly:     348
6276  deg
Mean motion:   15
48900439  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2928
Checksum:              312


Coasting Arc #8 (Orbit 2942)
---------------------------------------

Vector Time (GMT): 2021/044/14:00:36
808
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3384962
85                 A    =         6792471
74  meter
 Y    =        2575233
96  meter          E    =           
0015613
 Z    =       -5309460
30                 I    =           51
30335
 XDOT =      -4613
962258                 Wp   =           81
10003
 YDOT =      -6100
246853  meter/sec      RA   =          232
98712  deg
 ZDOT =        -14
898659                 TA   =          188
74335
                                          MA   =          188
77058
                                          Ha   =            229
544  n
mi
                                          Hp   =            222
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11105521
15                 X    =        -3387718
87
 Y    =        8448930
33  feet           Y    =         2537365
21  meter
 Z    =      -17419489
16                 Z    =        -5325909
38
 XDOT =     -15137
671450                 XDOT =       -4545
332151
 YDOT =     -20013
933245  feet/sec       YDOT =       -6151
459772  meter/sec
 ZDOT =        -48
880116                 ZDOT =         -37
143762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11924601
57                 X    =        -3634618
56
 Y    =        7060803
10  feet           Y    =         2152132
79  meter
 Z    =      -17495844
17                 Z    =        -5332733
30
 XDOT =     -12096
323841                 XDOT =       -3686
959507
 YDOT =     -20824
760182  feet/sec       YDOT =       -6347
386903  meter/sec
 ZDOT =       -152
182341                 ZDOT =         -46
385178


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   21044
59998751  
00016717  00000-0  10270-3 0  9078
2 25544  51
6399 234
0045 0002471  13
7496 346
3721 15
48952972 29433


Satellite: ISS
Catalog Number: 25544
Epoch time:      21044
59998751   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:       234
0045  deg
Eccentricity:     
0002471     
Arg of perigee:    13
7496  deg
Mean anomaly:     346
3721  deg
Mean motion:   15
48952972  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2943
Checksum:              335


Coasting Arc #9 (Orbit 2958)
---------------------------------------

Vector Time (GMT): 2021/045/14:00:36
808
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3140243
25                 A    =         6792560
22  meter
 Y    =       -2853895
49  meter          E    =           
0003958
 Z    =        5301265
64                 I    =           51
32527
 XDOT =       5137
431997                 Wp   =           53
98096
 YDOT =       5685
597516  meter/sec      RA   =          228
01840  deg
 ZDOT =         19
876658                 TA   =           35
84195
                                          MA   =           35
81539
                                          Ha   =            229
550  n
mi
                                          Hp   =            222
543

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10302635
34                 X    =         3146173
24
 Y    =       -9363174
18  feet           Y    =        -2818745
56  meter
 Z    =       17392603
80                 Z    =         5316533
83
 XDOT =      16855
091855                 XDOT =        5073
375541
 YDOT =      18653
535159  feet/sec       YDOT =        5742
689826  meter/sec
 ZDOT =         65
212133                 ZDOT =          44
675649

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11097714
54                 X    =         3382583
39
 Y    =       -8257350
63  feet           Y    =        -2516840
47  meter
 Z    =       17463472
88                 Z    =         5322866
53
 XDOT =      14229
315889                 XDOT =        4337
095483
 YDOT =      19489
713663  feet/sec       YDOT =        5940
464725  meter/sec
 ZDOT =        180
393012                 ZDOT =          54
983790


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   21045
63226694  
00016717  00000-0  10270-3 0  9085
2 25544  51
6403 228
8970 0002574  17
6304 342
4935 15
48918069 29592


Satellite: ISS
Catalog Number: 25544
Epoch time:      21045
63226694   =   yrday
fracday
Element set:     908
Inclination:       51
6403  deg
RA of node:       228
8970  deg
Eccentricity:     
0002574     
Arg of perigee:    17
6304  deg
Mean anomaly:     342
4935  deg
Mean motion:   15
48918069  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2959
Checksum:              331


Coasting Arc #10 (Orbit 2973)
---------------------------------------

Vector Time (GMT): 2021/046/14:00:36
808
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2874789
12                 A    =         6792448
49  meter
 Y    =        3128979
91  meter          E    =           
0015984
 Z    =       -5313041
82                 I    =           51
34988
 XDOT =      -5604
908800                 Wp   =           81
20071
 YDOT =      -5204
015891  meter/sec      RA   =          223
05411  deg
 ZDOT =        -29
741275                 TA   =          188
50044
                                          MA   =          188
52755
                                          Ha   =            229
659  n
mi
                                          Hp   =            222
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9431722
85                 X    =        -2883757
60
 Y    =       10265682
11  feet           Y    =         3096781
47  meter
 Z    =      -17431239
56                 Z    =        -5327028
04
 XDOT =     -18388
808400                 XDOT =       -5546
154876
 YDOT =     -17073
542950  feet/sec       YDOT =       -5266
365513  meter/sec
 ZDOT =        -97
576362                 ZDOT =         -56
824030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10164165
72                 X    =        -3098037
71
 Y    =        9421470
67  feet           Y    =         2871664
26  meter
 Z    =      -17496152
81                 Z    =        -5332827
38
 XDOT =     -16155
717264                 XDOT =       -4924
262622
 YDOT =     -17858
167228  feet/sec       YDOT =       -5443
169371  meter/sec
 ZDOT =       -223
378711                 ZDOT =         -68
085831


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   21046
60002538  
00016717  00000-0  10270-3 0  9093
2 25544  51
6413 224
1115 0002589  21
6782 338
4477 15
48961153 29749


Satellite: ISS
Catalog Number: 25544
Epoch time:      21046
60002538   =   yrday
fracday
Element set:     909
Inclination:       51
6413  deg
RA of node:       224
1115  deg
Eccentricity:     
0002589     
Arg of perigee:    21
6782  deg
Mean anomaly:     338
4477  deg
Mean motion:   15
48961153  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2974
Checksum:              306


Coasting Arc #11 (Orbit 2978)
---------------------------------------

Vector Time (GMT): 2021/046/21:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2902293
64                 A    =         6801248
48  meter
 Y    =        5504133
50  meter          E    =           
0005084
 Z    =       -2750050
76                 I    =           51
38906
 XDOT =      -5672
467476                 Wp   =           89
60967
 YDOT =        437
358873  meter/sec      RA   =          221
52990  deg
 ZDOT =      -5119
342274                 TA   =          121
54324
                                          MA   =          121
49358
                                          Ha   =            229
737  n
mi
                                          Hp   =            222
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9521960
77                 X    =         2853886
89
 Y    =       18058180
77  feet           Y    =         5536318
22  meter
 Z    =       -9022476
23                 Z    =        -2736070
78
 XDOT =     -18610
457598                 XDOT =       -5652
070323
 YDOT =       1434
904439  feet/sec       YDOT =         374
038991  meter/sec
 ZDOT =     -16795
742369                 ZDOT =       -5146
846730

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14290590
96                 X    =         4355772
12
 Y    =      -14618919
09  feet           Y    =        -4455846
54  meter
 Z    =       -8957506
44                 Z    =        -2730247
96
 XDOT =       5921
537564                 XDOT =        1804
884649
 YDOT =      16141
501778  feet/sec       YDOT =        4919
929742  meter/sec
 ZDOT =     -16923
453115                 ZDOT =       -5158
268509


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   21046
92261087  
00016717  00000-0  10270-3 0  9106
2 25544  51
6433 222
5189 0002888  20
8991 339
2276 15
48961858 29792


Satellite: ISS
Catalog Number: 25544
Epoch time:      21046
92261087   =   yrday
fracday
Element set:     910
Inclination:       51
6433  deg
RA of node:       222
5189  deg
Eccentricity:     
0002888     
Arg of perigee:    20
8991  deg
Mean anomaly:     339
2276  deg
Mean motion:   15
48961858  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2979
Checksum:              342


Coasting Arc #12 (Orbit 2994)
---------------------------------------

Vector Time (GMT): 2021/047/21:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3383655
25                 A    =         6801397
59  meter
 Y    =       -5220483
60  meter          E    =           
0015514
 Z    =        2728518
51                 I    =           51
41387
 XDOT =       5610
141526                 Wp   =           69
88105
 YDOT =       -941
705796  meter/sec      RA   =          216
56667  deg
 ZDOT =       5136
815327                 TA   =          321
03900
                                          MA   =          321
15068
                                          Ha   =            229
908  n
mi
                                          Hp   =            222
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11101231
14                 X    =        -3338280
05
 Y    =      -17127570
85  feet           Y    =        -5258068
22  meter
 Z    =        8951832
37                 Z    =         2712192
85
 XDOT =      18405
976135                 XDOT =        5595
303802
 YDOT =      -3089
585945  feet/sec       YDOT =        -879
051839  meter/sec
 ZDOT =      16853
068658                 ZDOT =        5164
030663

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12649781
26                 X    =        -3855653
33
 Y    =       16060097
31  feet           Y    =         4895117
66  meter
 Z    =        8875957
84                 Z    =         2705391
95
 XDOT =      -7612
888553                 XDOT =       -2320
408431
 YDOT =     -15414
366986  feet/sec       YDOT =       -4698
299057  meter/sec
 ZDOT =      16979
441981                 ZDOT =        5175
333916


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   21047
95488880  
00016717  00000-0  10270-3 0  9113
2 25544  51
6417 217
4132 0003032  26
1826 333
9476 15
48931211 29954


Satellite: ISS
Catalog Number: 25544
Epoch time:      21047
95488880   =   yrday
fracday
Element set:     911
Inclination:       51
6417  deg
RA of node:       217
4132  deg
Eccentricity:     
0003032     
Arg of perigee:    26
1826  deg
Mean anomaly:     333
9476  deg
Mean motion:   15
48931211  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2995
Checksum:              311


Coasting Arc #13 (Orbit 3009)
---------------------------------------

Vector Time (GMT): 2021/048/21:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957811
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3820562
97                 A    =         6801318
12  meter
 Y    =        4916418
82  meter          E    =           
0005335
 Z    =       -2741207
56                 I    =           51
44273
 XDOT =      -5499
274528                 Wp   =           91
67723
 YDOT =       1417
767015  meter/sec      RA   =          211
60582  deg
 ZDOT =      -5130
661938                 TA   =          119
33842
                                          MA   =          119
28512
                                          Ha   =            229
827  n
mi
                                          Hp   =            222
335

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12534655
41                 X    =         3778617
11
 Y    =       16129983
02  feet           Y    =         4958908
47  meter
 Z    =       -8993463
12                 Z    =        -2722751
16
 XDOT =     -18042
239265                 XDOT =       -5489
798326
 YDOT =       4651
466585  feet/sec       YDOT =        1356
322934  meter/sec
 ZDOT =     -16832
880373                 ZDOT =       -5157
351840

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10949774
70                 X    =         3337491
33
 Y    =      -17289648
70  feet           Y    =        -5269884
92  meter
 Z    =       -8907682
03                 Z    =        -2715061
48
 XDOT =       9151
363475                 XDOT =        2789
335587
 YDOT =      14516
813747  feet/sec       YDOT =        4424
724830  meter/sec
 ZDOT =     -16956
819410                 ZDOT =       -5168
438556


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   21048
92264620  
00016717  00000-0  10270-3 0  9126
2 25544  51
6426 212
6271 0002874  26
5640 333
5657 15
48949905 30101


Satellite: ISS
Catalog Number: 25544
Epoch time:      21048
92264620   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:       212
6271  deg
Eccentricity:     
0002874     
Arg of perigee:    26
5640  deg
Mean anomaly:     333
5657  deg
Mean motion:   15
48949905  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3010
Checksum:              301


Coasting Arc #14 (Orbit 3025)
---------------------------------------

Vector Time (GMT): 2021/049/21:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957811
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4244743
58                 A    =         6801364
56  meter
 Y    =       -4553026
09  meter          E    =           
0015692
 Z    =        2720022
87                 I    =           51
47216
 XDOT =       5350
640727                 Wp   =           70
22744
 YDOT =      -1901
398837  meter/sec      RA   =          206
64637  deg
 ZDOT =       5148
168555                 TA   =          320
55847
                                          MA   =          320
67260
                                          Ha   =            229
942  n
mi
                                          Hp   =            222
222

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13926324
08                 X    =        -4206726
88
 Y    =      -14937749
65  feet           Y    =        -4600281
24  meter
 Z    =        8923959
53                 Z    =         2699496
35
 XDOT =      17554
595562                 XDOT =        5346
498618
 YDOT =      -6238
185162  feet/sec       YDOT =       -1841
587134  meter/sec
 ZDOT =      16890
316782                 ZDOT =        5174
149453

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9044493
39                 X    =        -2756761
59
 Y    =       18356734
85  feet           Y    =         5595132
78  meter
 Z    =        8828552
86                 Z    =         2690942
91
 XDOT =     -10648
094125                 XDOT =       -3245
539089
 YDOT =     -13458
106627  feet/sec       YDOT =       -4102
030900  meter/sec
 ZDOT =      17010
969429                 ZDOT =        5184
943482


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   21049
95492017  
00016717  00000-0  10270-3 0  9134
2 25544  51
6422 207
5213 0003061  29
9664 330
1661 15
48953766 30263


Satellite: ISS
Catalog Number: 25544
Epoch time:      21049
95492017   =   yrday
fracday
Element set:     913
Inclination:       51
6422  deg
RA of node:       207
5213  deg
Eccentricity:     
0003061     
Arg of perigee:    29
9664  deg
Mean anomaly:     330
1661  deg
Mean motion:   15
48953766  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3026
Checksum:              301


Coasting Arc #15 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2021/050/19:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957811
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         766252
98                 A    =         6792655
08  meter
 Y    =       -4215369
93  meter          E    =           
0004590
 Z    =        5267013
84                 I    =           51
47160
 XDOT =       7272
980342                 Wp   =           78
60972
 YDOT =       2288
955766  meter/sec      RA   =          202
10703  deg
 ZDOT =        774
159032                 TA   =            3
97309
                                          MA   =            3
96945
                                          Ha   =            229
874  n
mi
                                          Hp   =            222
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2513953
36                 X    =          787749
85
 Y    =      -13829953
83  feet           Y    =        -4206680
87  meter
 Z    =       17280229
13                 Z    =         5270788
20
 XDOT =      23861
484062                 XDOT =        7243
083636
 YDOT =       7509
697394  feet/sec       YDOT =        2370
120325  meter/sec
 ZDOT =       2539
891838                 ZDOT =         809
415125

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13207446
66                 X    =        -4025629
74
 Y    =       -4748343
78  feet           Y    =        -1447295
18  meter
 Z    =       17297701
80                 Z    =         5272339
51
 XDOT =      11170
218407                 XDOT =        3404
682571
 YDOT =     -21224
233012  feet/sec       YDOT =       -6469
146222  meter/sec
 ZDOT =       2703
706670                 ZDOT =         824
089793


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   21050
85815918  
00016717  00000-0  10270-3 0  9145
2 25544  51
6423 203
0536 0003027  32
9551 327
1787 15
48961492 30400


Satellite: ISS
Catalog Number: 25544
Epoch time:      21050
85815918   =   yrday
fracday
Element set:     914
Inclination:       51
6423  deg
RA of node:       203
0536  deg
Eccentricity:     
0003027     
Arg of perigee:    32
9551  deg
Mean anomaly:     327
1787  deg
Mean motion:   15
48961492  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3040
Checksum:              299


Coasting Arc #16 (Orbit 3054)
---------------------------------------

Vector Time (GMT): 2021/051/19:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957811
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -388982
17                 A    =         6792733
66  meter
 Y    =        4274277
25  meter          E    =           
0016616
 Z    =       -5279497
84                 I    =           51
50404
 XDOT =      -7428
239193                 Wp   =           76
49079
 YDOT =      -1642
655928  meter/sec      RA   =          197
15205  deg
 ZDOT =       -780
880572                 TA   =          186
00290
                                          MA   =          186
02284
                                          Ha   =            229
966  n
mi
                                          Hp   =            222
109

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1276188
23                 X    =         -411105
20
 Y    =       14023219
31  feet           Y    =         4269803
67  meter
 Z    =      -17321187
15                 Z    =        -5281441
06
 XDOT =     -24370
863495                 XDOT =       -7405
525428
 YDOT =      -5389
291104  feet/sec       YDOT =       -1725
596856  meter/sec
 ZDOT =      -2561
944133                 ZDOT =        -816
908265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13670968
54                 X    =         4166911
21
 Y    =        3327664
55  feet           Y    =         1014272
15  meter
 Z    =      -17330150
84                 Z    =        -5282229
98
 XDOT =      -8875
291565                 XDOT =       -2705
188869
 YDOT =      22218
622405  feet/sec       YDOT =        6772
236109  meter/sec
 ZDOT =      -2729
360062                 ZDOT =        -831
908947


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   21051
82591564  
00016717  00000-0  10270-3 0  9152
2 25544  51
6427 198
2672 0002964  36
1345 324
0005 15
48941852 30559


Satellite: ISS
Catalog Number: 25544
Epoch time:      21051
82591564   =   yrday
fracday
Element set:     915
Inclination:       51
6427  deg
RA of node:       198
2672  deg
Eccentricity:     
0002964     
Arg of perigee:    36
1345  deg
Mean anomaly:     324
0005  deg
Mean motion:   15
48941852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3055
Checksum:              305


Coasting Arc #17 (Orbit 3070)
---------------------------------------

Vector Time (GMT): 2021/052/19:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957811
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          13146
85                 A    =         6792657
25  meter
 Y    =       -4280392
77  meter          E    =           
0004961
 Z    =        5269960
91                 I    =           51
53597
 XDOT =       7558
515289                 Wp   =           81
94719
 YDOT =        993
503186  meter/sec      RA   =          192
19900  deg
 ZDOT =        788
135121                 TA   =             
50641
                                          MA   =             
50591
                                          Ha   =            230
015  n
mi
                                          Hp   =            222
009

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          43132
70                 X    =           35412
59
 Y    =      -14043283
36  feet           Y    =        -4280121
31  meter
 Z    =       17289897
98                 Z    =         5270078
80
 XDOT =      24798
278507                 XDOT =        7543
015639
 YDOT =       3259
524890  feet/sec       YDOT =        1077
941284  meter/sec
 ZDOT =       2585
745148                 ZDOT =         824
813059

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13917166
23                 X    =        -4241952
27
 Y    =       -1873913
46  feet           Y    =         -571168
82  meter
 Z    =       17290378
04                 Z    =         5270107
23
 XDOT =       6530
760940                 XDOT =        1990
575934
 YDOT =     -23072
780374  feet/sec       YDOT =       -7032
583458  meter/sec
 ZDOT =       2756
200392                 ZDOT =         840
089880


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   21052
85818722  
00016717  00000-0  10270-3 0  9165
2 25544  51
6418 193
1613 0003123  40
8627 319
2756 15
48963750 30719


Satellite: ISS
Catalog Number: 25544
Epoch time:      21052
85818722   =   yrday
fracday
Element set:     916
Inclination:       51
6418  deg
RA of node:       193
1613  deg
Eccentricity:     
0003123     
Arg of perigee:    40
8627  deg
Mean anomaly:     319
2756  deg
Mean motion:   15
48963750  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3071
Checksum:              308


Coasting Arc #18 (Orbit 3079)
---------------------------------------

Vector Time (GMT): 2021/053/09:36:25
000
Vector Time (MET): N/A
Weight (LBS)     : 972941
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5919841
31                 A    =         6800473
97  meter
 Y    =       -1451458
66  meter          E    =           
0014733
 Z    =        3003946
29                 I    =           51
57990
 XDOT =       3644
670522                 Wp   =           87
23950
 YDOT =       4571
694012  meter/sec      RA   =          189
23427  deg
 ZDOT =      -4951
804880                 TA   =           58
41100
                                          MA   =           58
26727
                                          Ha   =            229
843  n
mi
                                          Hp   =            222
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19422051
53                 X    =         5921040
86
 Y    =       -4762003
46  feet           Y    =        -1385252
05  meter
 Z    =        9855466
83                 Z    =         3032704
82
 XDOT =      11957
580452                 XDOT =        3617
330066
 YDOT =      14998
996103  feet/sec       YDOT =        4612
298533  meter/sec
 ZDOT =     -16246
079003                 ZDOT =       -4934
167241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12686038
88                 X    =         3866704
65
 Y    =       15372227
74  feet           Y    =         4685455
01  meter
 Z    =        9989095
10                 Z    =         3044676
19
 XDOT =      -7156
918259                 XDOT =       -2181
428685
 YDOT =      16455
637822  feet/sec       YDOT =        5015
678408  meter/sec
 ZDOT =     -16164
035643                 ZDOT =       -4926
798064


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   21053
43883860  
00016717  00000-0  10270-3 0  9176
2 25544  51
6397 190
2862 0002858  37
6291 322
5059 15
48966118 30808


Satellite: ISS
Catalog Number: 25544
Epoch time:      21053
43883860   =   yrday
fracday
Element set:     917
Inclination:       51
6397  deg
RA of node:       190
2862  deg
Eccentricity:     
0002858     
Arg of perigee:    37
6291  deg
Mean anomaly:     322
5059  deg
Mean motion:   15
48966118  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3080
Checksum:              328


Coasting Arc #19 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2021/054/01:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 972941
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         287329
76                 A    =         6792592
89  meter
 Y    =        4256978
01  meter          E    =           
0017030
 Z    =       -5300108
17                 I    =           51
57872
 XDOT =      -7615
243177                 Wp   =           77
29900
 YDOT =       -285
563505  meter/sec      RA   =          185
96882  deg
 ZDOT =       -640
287036                 TA   =          186
55515
                                          MA   =          186
57745
                                          Ha   =            230
055  n
mi
                                          Hp   =            221
974

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         942682
95                 X    =          265449
83
 Y    =       13966463
30  feet           Y    =         4260068
85  meter
 Z    =      -17388806
33                 Z    =        -5298765
57
 XDOT =     -24984
393626                 XDOT =       -7608
373872
 YDOT =       -936
888140  feet/sec       YDOT =        -370
684232  meter/sec
 ZDOT =      -2100
679253                 ZDOT =        -677
261307

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -149620
14                 X    =          -45604
22
 Y    =      -14005278
63  feet           Y    =        -4268808
93  meter
 Z    =      -17382494
58                 Z    =        -5298184
35
 XDOT =      23833
863601                 XDOT =        7264
561625
 YDOT =       2573
701510  feet/sec       YDOT =         784
464220  meter/sec
 ZDOT =      -2272
536985                 ZDOT =        -692
669273


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   21054
08400856  
00016717  00000-0  10270-3 0  9189
2 25544  51
6426 187
0986 0003261  39
3272 320
8115 15
48966004 30908


Satellite: ISS
Catalog Number: 25544
Epoch time:      21054
08400856   =   yrday
fracday
Element set:     918
Inclination:       51
6426  deg
RA of node:       187
0986  deg
Eccentricity:     
0003261     
Arg of perigee:    39
3272  deg
Mean anomaly:     320
8115  deg
Mean motion:   15
48966004  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3090
Checksum:              301
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