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

 
Date: February 6th 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) : 14538 8138 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 0 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


036/13:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 9
000/00:00:00 000 0 0 0 0 223 2

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

040/13:27:30 000 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

046/21:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 5
000/00:00:00 000 0 0 0 0 222 4

048/06:18:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 7
000/00:00:00 000 0 0 0 0 222 3

050/19:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 222 2

Coasting Arc #1 (Orbit 2817)
---------------------------------------

Vector Time (GMT): 2021/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         858497
65                 A    =         6803551
85  meter
 Y    =        6570398
19  meter          E    =           
0012102
 Z    =        1521106
66                 I    =           51
26744
 XDOT =      -4704
659113                 Wp   =          110
27608
 YDOT =       1947
192155  meter/sec      RA   =          273
16593  deg
 ZDOT =      -5722
514152                 TA   =           53
05647
                                          MA   =           52
94569
                                          Ha   =            229
089  n
mi
                                          Hp   =            223
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2816593
35                 X    =          777573
11
 Y    =       21556424
52  feet           Y    =         6579546
00  meter
 Z    =        4990507
43                 Z    =         1525080
52
 XDOT =     -15435
233312                 XDOT =       -4698
287311
 YDOT =       6388
425706  feet/sec       YDOT =        1894
617091  meter/sec
 ZDOT =     -18774
652731                 ZDOT =       -5745
351626

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13291086
70                 X    =        -4051123
22
 Y    =       17198156
60  feet           Y    =         5241998
13  meter
 Z    =        5008814
68                 Z    =         1526686
71
 XDOT =     -14079
693961                 XDOT =       -4291
490719
 YDOT =      -5350
747229  feet/sec       YDOT =       -1630
907755  meter/sec
 ZDOT =     -18880
644073                 ZDOT =       -5754
820313


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   21036
53527748  
00016717  00000-0  10270-3 0  9000
2 25544  51
6442 273
8970 0002442 338
7265  21
3783 15
48913095 28184


Satellite: ISS
Catalog Number: 25544
Epoch time:      21036
53527748   =   yrday
fracday
Element set:     900
Inclination:       51
6442  deg
RA of node:       273
8970  deg
Eccentricity:     
0002442     
Arg of perigee:   338
7265  deg
Mean anomaly:      21
3783  deg
Mean motion:   15
48913095  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2818
Checksum:              318


Coasting Arc #2 (Orbit 2818)
---------------------------------------

Vector Time (GMT): 2021/036/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4185593
12                 A    =         6793414
85  meter
 Y    =       -1603870
42  meter          E    =           
0003096
 Z    =        5102220
05                 I    =           51
23278
 XDOT =        901
416264                 Wp   =           97
76109
 YDOT =       7439
251643  meter/sec      RA   =          272
95056  deg
 ZDOT =       1597
788503                 TA   =          336
71921
                                          MA   =          336
73323
                                          Ha   =            228
925  n
mi
                                          Hp   =            223
198

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13732260
88                 X    =         4178433
75
 Y    =       -5262042
05  feet           Y    =        -1557104
31  meter
 Z    =       16739567
10                 Z    =         5122534
24
 XDOT =       2957
402442                 XDOT =         810
400274
 YDOT =      24406
993578  feet/sec       YDOT =        7448
822969  meter/sec
 ZDOT =       5242
088264                 ZDOT =        1601
946365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14507547
80                 X    =         4421900
57
 Y    =        1621693
98  feet           Y    =          494292
33  meter
 Z    =       16833845
30                 Z    =         5130956
05
 XDOT =      -8562
098803                 XDOT =       -2609
727715
 YDOT =      21939
873825  feet/sec       YDOT =        6687
273542  meter/sec
 ZDOT =       5261
232853                 ZDOT =        1603
623774


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   21036
59979446  
00016717  00000-0  10270-3 0  9013
2 25544  51
6434 273
5771 0002604 338
0787  22
0251 15
48916724 28194


Satellite: ISS
Catalog Number: 25544
Epoch time:      21036
59979446   =   yrday
fracday
Element set:     901
Inclination:       51
6434  deg
RA of node:       273
5771  deg
Eccentricity:     
0002604     
Arg of perigee:   338
0787  deg
Mean anomaly:      22
0251  deg
Mean motion:   15
48916724  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2819
Checksum:              321


Coasting Arc #3 (Orbit 2833)
---------------------------------------

Vector Time (GMT): 2021/037/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4034840
03                 A    =         6793344
97  meter
 Y    =        1975439
51  meter          E    =           
0013318
 Z    =       -5107739
28                 I    =           51
23167
 XDOT =      -1548
389915                 Wp   =           66
24463
 YDOT =      -7317
581892  meter/sec      RA   =          267
97633  deg
 ZDOT =      -1605
038221                 TA   =          188
13390
                                          MA   =          188
15552
                                          Ha   =            229
051  n
mi
                                          Hp   =            222
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13237664
13                 X    =        -4031820
13
 Y    =        6481100
76  feet           Y    =         1930336
18  meter
 Z    =      -16757674
80                 Z    =        -5127331
13
 XDOT =      -5080
019405                 XDOT =       -1458
651198
 YDOT =     -24007
814606  feet/sec       YDOT =       -7334
395255  meter/sec
 ZDOT =      -5265
873430                 ZDOT =       -1612
341990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14634916
95                 X    =        -4460722
69
 Y    =         -60220
09  feet           Y    =          -18355
08  meter
 Z    =      -16848610
11                 Z    =        -5135456
36
 XDOT =       6201
753213                 XDOT =        1890
294379
 YDOT =     -22666
933117  feet/sec       YDOT =       -6908
881214  meter/sec
 ZDOT =      -5299
633485                 ZDOT =       -1615
328286


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   21037
56755943  
00016717  00000-0  10270-3 0  9026
2 25544  51
6427 268
7894 0002701 338
7839  21
3199 15
48949420 28340


Satellite: ISS
Catalog Number: 25544
Epoch time:      21037
56755943   =   yrday
fracday
Element set:     902
Inclination:       51
6427  deg
RA of node:       268
7894  deg
Eccentricity:     
0002701     
Arg of perigee:   338
7839  deg
Mean anomaly:      21
3199  deg
Mean motion:   15
48949420  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2834
Checksum:              340


Coasting Arc #4 (Orbit 2849)
---------------------------------------

Vector Time (GMT): 2021/038/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3839318
70                 A    =         6793455
90  meter
 Y    =       -2322652
18  meter          E    =           
0003448
 Z    =        5097657
01                 I    =           51
23392
 XDOT =       2186
612487                 Wp   =           94
56851
 YDOT =       7163
767955  meter/sec      RA   =          263
00329  deg
 ZDOT =       1615
962956                 TA   =          339
73183
                                          MA   =          339
74551
                                          Ha   =            229
077  n
mi
                                          Hp   =            223
078

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12596189
96                 X    =         3840245
06
 Y    =       -7620249
95  feet           Y    =        -2279713
30  meter
 Z    =       16724596
50                 Z    =         5116308
57
 XDOT =       7173
925482                 XDOT =        2098
493303
 YDOT =      23503
175706  feet/sec       YDOT =        7187
727423  meter/sec
 ZDOT =       5301
715735                 ZDOT =        1626
370841

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14546175
00                 X    =         4433674
14
 Y    =       -1495820
47  feet           Y    =         -455926
08  meter
 Z    =       16811176
42                 Z    =         5124046
57
 XDOT =      -3799
388077                 XDOT =       -1158
053486
 YDOT =      23223
691260  feet/sec       YDOT =        7078
581096  meter/sec
 ZDOT =       5349
902088                 ZDOT =        1630
650156


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   21038
59984320  
00016717  00000-0  10270-3 0  9034
2 25544  51
6425 263
6837 0002679 345
8440  14
2634 15
48912579 28508


Satellite: ISS
Catalog Number: 25544
Epoch time:      21038
59984320   =   yrday
fracday
Element set:     903
Inclination:       51
6425  deg
RA of node:       263
6837  deg
Eccentricity:     
0002679     
Arg of perigee:   345
8440  deg
Mean anomaly:      14
2634  deg
Mean motion:   15
48912579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2850
Checksum:              326


Coasting Arc #5 (Orbit 2864)
---------------------------------------

Vector Time (GMT): 2021/039/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3625212
21                 A    =         6793397
69  meter
 Y    =        2661243
61  meter          E    =           
0013691
 Z    =       -5104038
75                 I    =           51
23707
 XDOT =      -2801
070766                 Wp   =           66
59482
 YDOT =      -6930
904062  meter/sec      RA   =          258
03026  deg
 ZDOT =      -1622
420849                 TA   =          187
61120
                                          MA   =          187
63201
                                          Ha   =            229
213  n
mi
                                          Hp   =            222
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11893740
86                 X    =        -3629909
85
 Y    =        8731114
22  feet           Y    =         2620677
92  meter
 Z    =      -16745533
95                 Z    =        -5121659
34
 XDOT =      -9189
864719                 XDOT =       -2715
478542
 YDOT =     -22739
186556  feet/sec       YDOT =       -6961
748978  meter/sec
 ZDOT =      -5322
903049                 ZDOT =       -1635
819496

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14340705
63                 X    =        -4371047
07
 Y    =        3048160
56  feet           Y    =          929079
34  meter
 Z    =      -16827335
31                 Z    =        -5128971
80
 XDOT =       1343
363536                 XDOT =         409
457206
 YDOT =     -23441
041365  feet/sec       YDOT =       -7144
829408  meter/sec
 ZDOT =      -5384
995618                 ZDOT =       -1641
346664


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
56760700  
00016717  00000-0  10270-3 0  9047
2 25544  51
6402 258
8969 0002638 347
8335  12
2751 15
48941399 28651


Satellite: ISS
Catalog Number: 25544
Epoch time:      21039
56760700   =   yrday
fracday
Element set:     904
Inclination:       51
6402  deg
RA of node:       258
8969  deg
Eccentricity:     
0002638     
Arg of perigee:   347
8335  deg
Mean anomaly:      12
2751  deg
Mean motion:   15
48941399  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2865
Checksum:              332


Coasting Arc #6 (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    =        2569953
25                 A    =         6795642
78  meter
 Y    =       -4364308
38  meter          E    =           
0007669
 Z    =        4524711
35                 I    =           51
25098
 XDOT =       4132
549835                 Wp   =           96
57107
 YDOT =       5657
752253  meter/sec      RA   =          254
68625  deg
 ZDOT =       3104
555086                 TA   =          322
10637
                                          MA   =          322
16032
                                          Ha   =            229
077  n
mi
                                          Hp   =            222
902

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8431605
14                 X    =         2596587
53
 Y    =      -14318597
04  feet           Y    =        -4335420
63  meter
 Z    =       14844853
51                 Z    =         4537259
23
 XDOT =      13558
234368                 XDOT =        4053
896326
 YDOT =      18562
179309  feet/sec       YDOT =        5703
525459  meter/sec
 ZDOT =      10185
548181                 ZDOT =        3124
438014

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2535475
00                 X    =          772812
78
 Y    =       16369237
63  feet           Y    =         4989343
63  meter
 Z    =       14903130
15                 Z    =         4542474
07
 XDOT =     -20969
465686                 XDOT =       -6391
493141
 YDOT =      -6125
332648  feet/sec       YDOT =       -1867
001391  meter/sec
 ZDOT =      10277
764720                 ZDOT =        3132
662687


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
27730115  
00016717  00000-0  10270-3 0  9055
2 25544  51
6410 255
3880 0002566 349
7276  10
3822 15
48976074 28767


Satellite: ISS
Catalog Number: 25544
Epoch time:      21040
27730115   =   yrday
fracday
Element set:     905
Inclination:       51
6410  deg
RA of node:       255
3880  deg
Eccentricity:     
0002566     
Arg of perigee:   349
7276  deg
Mean anomaly:      10
3822  deg
Mean motion:   15
48976074  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2876
Checksum:              306


Coasting Arc #7 (Orbit 2880)
---------------------------------------

Vector Time (GMT): 2021/040/13:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4070863
78                 A    =         6799822
30  meter
 Y    =        4356669
29  meter          E    =           
0012189
 Z    =        3260680
13                 I    =           51
26750
 XDOT =      -2227
554125                 Wp   =           80
06535
 YDOT =       5617
838795  meter/sec      RA   =          252
95846  deg
 ZDOT =      -4707
916286                 TA   =           61
97778
                                          MA   =           61
85453
                                          Ha   =            229
110  n
mi
                                          Hp   =            222
945

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13355852
30                 X    =         4006005
64
 Y    =       14293534
43  feet           Y    =         4401829
83  meter
 Z    =       10697769
44                 Z    =         3280296
80
 XDOT =      -7308
248440                 XDOT =       -2267
341372
 YDOT =      18431
229641  feet/sec       YDOT =        5592
706438  meter/sec
 ZDOT =     -15445
919575                 ZDOT =       -4718
832871

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7850295
86                 X    =         2392770
18
 Y    =       17863411
07  feet           Y    =         5444767
69  meter
 Z    =       10788771
38                 Z    =         3288417
52
 XDOT =     -11553
096858                 XDOT =       -3521
383922
 YDOT =      14470
221081  feet/sec       YDOT =        4410
523385  meter/sec
 ZDOT =     -15496
633573                 ZDOT =       -4723
373913


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
59988798  
00016717  00000-0  10270-3 0  9063
2 25544  51
6404 253
7904 0002702 346
6981  13
4097 15
48966443 28813


Satellite: ISS
Catalog Number: 25544
Epoch time:      21040
59988798   =   yrday
fracday
Element set:     906
Inclination:       51
6404  deg
RA of node:       253
7904  deg
Eccentricity:     
0002702     
Arg of perigee:   346
6981  deg
Mean anomaly:      13
4097  deg
Mean motion:   15
48966443  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2881
Checksum:              340


Coasting Arc #8 (Orbit 2895)
---------------------------------------

Vector Time (GMT): 2021/041/13:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4442501
96                 A    =         6799813
28  meter
 Y    =       -3966280
66  meter          E    =           
0005297
 Z    =       -3282477
72                 I    =           51
27746
 XDOT =       1715
249511                 Wp   =           56
96781
 YDOT =      -5799
423435  meter/sec      RA   =          247
98563  deg
 ZDOT =       4694
504582                 TA   =          264
81022
                                          MA   =          264
87067
                                          Ha   =            229
240  n
mi
                                          Hp   =            222
789

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14575137
66                 X    =        -4381875
82
 Y    =      -13012731
81  feet           Y    =        -4015620
85  meter
 Z    =      -10769283
84                 Z    =        -3303909
71
 XDOT =       5627
459027                 XDOT =        1757
170579
 YDOT =     -19026
979773  feet/sec       YDOT =       -5780
008004  meter/sec
 ZDOT =      15401
917921                 ZDOT =        4702
937950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9714073
56                 X    =        -2960849
62
 Y    =      -16889364
32  feet           Y    =        -5147878
24  meter
 Z    =      -10868737
26                 Z    =        -3312791
12
 XDOT =       9952
949463                 XDOT =        3033
658996
 YDOT =     -15643
764270  feet/sec       YDOT =       -4768
219350  meter/sec
 ZDOT =      15441
092894                 ZDOT =        4706
445114


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
56765254  
00016717  00000-0  10270-3 0  9072
2 25544  51
6394 249
0028 0002505 354
7360   5
3763 15
48945437 28964


Satellite: ISS
Catalog Number: 25544
Epoch time:      21041
56765254   =   yrday
fracday
Element set:     907
Inclination:       51
6394  deg
RA of node:       249
0028  deg
Eccentricity:     
0002505     
Arg of perigee:   354
7360  deg
Mean anomaly:       5
3763  deg
Mean motion:   15
48945437  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2896
Checksum:              320


Coasting Arc #9 (Orbit 2911)
---------------------------------------

Vector Time (GMT): 2021/042/13:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4763462
86                 A    =         6799812
79  meter
 Y    =        3575356
22  meter          E    =           
0012628
 Z    =        3272304
66                 I    =           51
29121
 XDOT =      -1208
389956                 Wp   =           80
34465
 YDOT =       5927
812014  meter/sec      RA   =          243
01431  deg
 ZDOT =      -4700
096362                 TA   =           61
55251
                                          MA   =           61
42533
                                          Ha   =            229
267  n
mi
                                          Hp   =            222
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15628158
98                 X    =         4707233
72
 Y    =       11730171
34  feet           Y    =         3628310
30  meter
 Z    =       10735907
67                 Z    =         3295306
26
 XDOT =      -3964
533977                 XDOT =       -1251
757234
 YDOT =      19448
202146  feet/sec       YDOT =        5914
056443  meter/sec
 ZDOT =     -15420
263655                 ZDOT =       -4706
071353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11388593
24                 X    =         3471243
22
 Y    =       15806088
32  feet           Y    =         4817695
72  meter
 Z    =       10842670
44                 Z    =         3304845
95
 XDOT =      -8284
977133                 XDOT =       -2525
261030
 YDOT =      16605
865276  feet/sec       YDOT =        5061
467736  meter/sec
 ZDOT =     -15448
010731                 ZDOT =       -4708
553671


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
59993063  
00016717  00000-0  10270-3 0  9088
2 25544  51
6392 243
8965 0002604 356
6304   3
4828 15
48954070 29126


Satellite: ISS
Catalog Number: 25544
Epoch time:      21042
59993063   =   yrday
fracday
Element set:     908
Inclination:       51
6392  deg
RA of node:       243
8965  deg
Eccentricity:     
0002604     
Arg of perigee:   356
6304  deg
Mean anomaly:       3
4828  deg
Mean motion:   15
48954070  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2912
Checksum:              318


Coasting Arc #10 (Orbit 2926)
---------------------------------------

Vector Time (GMT): 2021/043/13:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5060891
07                 A    =         6799763
49  meter
 Y    =       -3126823
69  meter          E    =           
0005691
 Z    =       -3294835
80                 I    =           51
30699
 XDOT =        671
487651                 Wp   =           61
29028
 YDOT =      -6016
021548  meter/sec      RA   =          238
04391  deg
 ZDOT =       4686
705513                 TA   =          260
33824
                                          MA   =          260
40254
                                          Ha   =            229
397  n
mi
                                          Hp   =            222
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16603973
32                 X    =        -5009545
99
 Y    =      -10258607
92  feet           Y    =        -3183131
22  meter
 Z    =      -10809828
73                 Z    =        -3319293
94
 XDOT =       2203
043475                 XDOT =         715
946233
 YDOT =     -19737
603505  feet/sec       YDOT =       -6008
263784  meter/sec
 ZDOT =      15376
330422                 ZDOT =        4690
075350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13006253
69                 X    =        -3964306
12
 Y    =      -14467226
57  feet           Y    =        -4409610
66  meter
 Z    =      -10923373
29                 Z    =        -3329444
18
 XDOT =       6471
042227                 XDOT =        1972
373671
 YDOT =     -17417
420516  feet/sec       YDOT =       -5308
829773  meter/sec
 ZDOT =      15391
965957                 ZDOT =        4691
471224


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
56769366  
00016717  00000-0  10270-3 0  9094
2 25544  51
6386 239
1094 0002429   6
8161 353
3022 15
48946622 29273


Satellite: ISS
Catalog Number: 25544
Epoch time:      21043
56769366   =   yrday
fracday
Element set:     909
Inclination:       51
6386  deg
RA of node:       239
1094  deg
Eccentricity:     
0002429     
Arg of perigee:     6
8161  deg
Mean anomaly:     353
3022  deg
Mean motion:   15
48946622  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2927
Checksum:              321


Coasting Arc #11 (Orbit 2942)
---------------------------------------

Vector Time (GMT): 2021/044/13:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5307662
68                 A    =         6799812
84  meter
 Y    =        2686918
79  meter          E    =           
0013005
 Z    =        3284404
53                 I    =           51
32590
 XDOT =       -149
441786                 Wp   =           81
25403
 YDOT =       6053
737102  meter/sec      RA   =          233
07521  deg
 ZDOT =      -4693
034624                 TA   =           60
49695
                                          MA   =           60
36731
                                          Ha   =            229
396  n
mi
                                          Hp   =            222
656

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17413591
47                 X    =         5261269
04
 Y    =        8815350
36  feet           Y    =         2746013
65  meter
 Z    =       10775605
43                 Z    =         3310073
41
 XDOT =       -490
294574                 XDOT =        -194
330104
 YDOT =      19861
342199  feet/sec       YDOT =        6051
814733  meter/sec
 ZDOT =     -15397
095222                 ZDOT =       -4693
869830

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14413754
16                 X    =         4393312
27
 Y    =       13061567
40  feet           Y    =         3981165
74  meter
 Z    =       10894787
28                 Z    =         3320731
16
 XDOT =      -4636
344249                 XDOT =       -1413
157727
 YDOT =      18010
934495  feet/sec       YDOT =        5489
732834  meter/sec
 ZDOT =     -15400
946022                 ZDOT =       -4694
208348


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
59997182  
00016717  00000-0  10270-3 0  9109
2 25544  51
6384 234
0034 0002431   6
5571 353
5610 15
48938828 29436


Satellite: ISS
Catalog Number: 25544
Epoch time:      21044
59997182   =   yrday
fracday
Element set:     910
Inclination:       51
6384  deg
RA of node:       234
0034  deg
Eccentricity:     
0002431     
Arg of perigee:     6
5571  deg
Mean anomaly:     353
5610  deg
Mean motion:   15
48938828  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2943
Checksum:              309


Coasting Arc #12 (Orbit 2957)
---------------------------------------

Vector Time (GMT): 2021/045/13:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5521966
77                 A    =         6799701
11  meter
 Y    =       -2194813
52  meter          E    =           
0005967
 Z    =       -3307319
99                 I    =           51
34939
 XDOT =       -394
752241                 Wp   =           63
81523
 YDOT =      -6045
351221  meter/sec      RA   =          228
10743  deg
 ZDOT =       4680
098062                 TA   =          257
66926
                                          MA   =          257
73607
                                          Ha   =            229
494  n
mi
                                          Hp   =            222
453

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18116688
89                 X    =        -5480948
70
 Y    =       -7200831
76  feet           Y    =        -2256334
98  meter
 Z    =      -10850787
38                 Z    =        -3334043
00
 XDOT =      -1295
118902                 XDOT =        -349
854507
 YDOT =     -19833
829464  feet/sec       YDOT =       -6049
514314  meter/sec
 ZDOT =      15354
652433                 ZDOT =        4678
289962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15714574
73                 X    =        -4789802
38
 Y    =      -11419729
20  feet           Y    =        -3480733
46  meter
 Z    =      -10974876
19                 Z    =        -3345142
26
 XDOT =       2690
398354                 XDOT =         820
033418
 YDOT =     -18422
025137  feet/sec       YDOT =       -5615
033262  meter/sec
 ZDOT =      15346
214680                 ZDOT =        4677
526235


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
56773220  
00016717  00000-0  10270-3 0  9113
2 25544  51
6407 229
2162 0002459  14
6024 345
5197 15
48952918 29586


Satellite: ISS
Catalog Number: 25544
Epoch time:      21045
56773220   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       229
2162  deg
Eccentricity:     
0002459     
Arg of perigee:    14
6024  deg
Mean anomaly:     345
5197  deg
Mean motion:   15
48952918  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2958
Checksum:              313


Coasting Arc #13 (Orbit 2973)
---------------------------------------

Vector Time (GMT): 2021/046/13:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5687798
35                 A    =         6799778
85  meter
 Y    =        1721147
66  meter          E    =           
0013492
 Z    =        3295610
06                 I    =           51
37233
 XDOT =        914
171896                 Wp   =           81
65641
 YDOT =       5990
565244  meter/sec      RA   =          223
14142  deg
 ZDOT =      -4687
904018                 TA   =           59
96792
                                          MA   =           59
83414
                                          Ha   =            229
561  n
mi
                                          Hp   =            222
468

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18660755
74                 X    =         5652121
44
 Y    =        5646809
89  feet           Y    =         1784553
44  meter
 Z    =       10812368
96                 Z    =         3323151
70
 XDOT =       2999
251626                 XDOT =         869
886206
 YDOT =      19654
085447  feet/sec       YDOT =        6000
540273  meter/sec
 ZDOT =     -15380
262525                 ZDOT =       -4683
571362

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16794956
13                 X    =         5119102
63
 Y    =        9759997
23  feet           Y    =         2974847
16  meter
 Z    =       10940269
28                 Z    =         3334594
08
 XDOT =       -774
254923                 XDOT =        -235
992900
 YDOT =      18616
931425  feet/sec       YDOT =        5674
440698  meter/sec
 ZDOT =     -15360
088904                 ZDOT =       -4681
755098


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
60000804  
00016717  00000-0  10270-3 0  9121
2 25544  51
6399 224
1099 0002489  18
6484 341
4757 15
48937105 29742


Satellite: ISS
Catalog Number: 25544
Epoch time:      21046
60000804   =   yrday
fracday
Element set:     912
Inclination:       51
6399  deg
RA of node:       224
1099  deg
Eccentricity:     
0002489     
Arg of perigee:    18
6484  deg
Mean anomaly:     341
4757  deg
Mean motion:   15
48937105  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2974
Checksum:              317


Coasting Arc #14 (Orbit 2978)
---------------------------------------

Vector Time (GMT): 2021/046/21:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4010202
36                 A    =         6793132
32  meter
 Y    =       -1925333
86  meter          E    =           
0007060
 Z    =        5131158
09                 I    =           51
36061
 XDOT =       4741
639561                 Wp   =           41
30466
 YDOT =       5825
868216  meter/sec      RA   =          221
58964  deg
 ZDOT =      -1513
373887                 TA   =           63
37805
                                          MA   =           63
30575
                                          Ha   =            229
498  n
mi
                                          Hp   =            222
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13156831
87                 X    =         4006510
34
 Y    =       -6316712
13  feet           Y    =        -1880509
22  meter
 Z    =       16834508
17                 Z    =         5150628
76
 XDOT =      15556
560239                 XDOT =        4683
491446
 YDOT =      19113
740867  feet/sec       YDOT =        5878
567434  meter/sec
 ZDOT =      -4965
137426                 ZDOT =       -1490
482985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8647839
07                 X    =        -2635861
35
 Y    =      -11626107
96  feet           Y    =        -3543637
71  meter
 Z    =       16924899
86                 Z    =         5158709
48
 XDOT =      15005
641683                 XDOT =        4573
719585
 YDOT =     -18265
292897  feet/sec       YDOT =       -5567
261275  meter/sec
 ZDOT =      -4858
787419                 ZDOT =       -1480
958405


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
92259244  
00016717  00000-0  10270-3 0  9131
2 25544  51
6422 222
5187 0002784  17
0121 343
1122 15
48971730 29790


Satellite: ISS
Catalog Number: 25544
Epoch time:      21046
92259244   =   yrday
fracday
Element set:     913
Inclination:       51
6422  deg
RA of node:       222
5187  deg
Eccentricity:     
0002784     
Arg of perigee:    17
0121  deg
Mean anomaly:     343
1122  deg
Mean motion:   15
48971730  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2979
Checksum:              295


Coasting Arc #15 (Orbit 2993)
---------------------------------------

Vector Time (GMT): 2021/047/21:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3819278
06                 A    =         6793240
53  meter
 Y    =        2281987
72  meter          E    =           
0014421
 Z    =       -5146160
13                 I    =           51
38756
 XDOT =      -5228
520570                 Wp   =           90
45553
 YDOT =      -5378
462919  meter/sec      RA   =          216
62648  deg
 ZDOT =       1498
948474                 TA   =          194
04825
                                          MA   =          194
08841
                                          Ha   =            229
728  n
mi
                                          Hp   =            222
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12530439
84                 X    =        -3819515
49
 Y    =        7486836
34  feet           Y    =         2239276
19  meter
 Z    =      -16883727
47                 Z    =        -5164713
01
 XDOT =     -17153
938878                 XDOT =       -5175
269250
 YDOT =     -17645
875720  feet/sec       YDOT =       -5436
634183  meter/sec
 ZDOT =       4917
809954                 ZDOT =        1473
680498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9863982
50                 X    =         3006541
86
 Y    =       10623119
14  feet           Y    =         3237926
71  meter
 Z    =      -16969858
08                 Z    =        -5172412
74
 XDOT =     -12988
277430                 XDOT =       -3958
826961
 YDOT =      19710
032105  feet/sec       YDOT =        6007
617786  meter/sec
 ZDOT =       4800
407002                 ZDOT =        1463
164054


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
89035180  
00016717  00000-0  10270-3 0  9140
2 25544  51
6429 217
7320 0002799  20
0298 340
0961 15
48930799 29941


Satellite: ISS
Catalog Number: 25544
Epoch time:      21047
89035180   =   yrday
fracday
Element set:     914
Inclination:       51
6429  deg
RA of node:       217
7320  deg
Eccentricity:     
0002799     
Arg of perigee:    20
0298  deg
Mean anomaly:     340
0961  deg
Mean motion:   15
48930799  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2994
Checksum:              325


Coasting Arc #16 (Orbit 2999)
---------------------------------------

Vector Time (GMT): 2021/048/06:18:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957811
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3085139
68                 A    =         6792582
91  meter
 Y    =        2987047
85  meter          E    =           
0015480
 Z    =       -5276219
01                 I    =           51
39711
 XDOT =      -5904
870041                 Wp   =           85
08976
 YDOT =      -4805
869907  meter/sec      RA   =          214
72030  deg
 ZDOT =        735
128248                 TA   =          191
95615
                                          MA   =          191
99294
                                          Ha   =            229
681  n
mi
                                          Hp   =            222
269

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10121849
34                 X    =        -3092684
10
 Y    =        9800025
77  feet           Y    =         2952505
16  meter
 Z    =      -17310429
82                 Z    =        -5291223
60
 XDOT =     -19372
933205                 XDOT =       -5854
261240
 YDOT =     -15767
289720  feet/sec       YDOT =       -4871
619416  meter/sec
 ZDOT =       2411
838083                 ZDOT =         706
568395

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3731115
49                 X    =        -1137244
00
 Y    =      -13496483
52  feet           Y    =        -4113728
18  meter
 Z    =      -17380075
65                 Z    =        -5297447
06
 XDOT =      22199
379877                 XDOT =        6766
370987
 YDOT =      -9058
678889  feet/sec       YDOT =       -2761
085326  meter/sec
 ZDOT =       2279
147073                 ZDOT =         694
684028


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
27745511  
00016717  00000-0  10270-3 0  9150
2 25544  51
6438 215
8192 0002939  17
7841 342
3411 15
48968438 30005


Satellite: ISS
Catalog Number: 25544
Epoch time:      21048
27745511   =   yrday
fracday
Element set:     915
Inclination:       51
6438  deg
RA of node:       215
8192  deg
Eccentricity:     
0002939     
Arg of perigee:    17
7841  deg
Mean anomaly:     342
3411  deg
Mean motion:   15
48968438  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3000
Checksum:              309


Coasting Arc #17 (Orbit 3015)
---------------------------------------

Vector Time (GMT): 2021/049/06:18:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957811
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2811495
28                 A    =         6792506
60  meter
 Y    =       -3232468
34  meter          E    =           
0005507
 Z    =        5268344
80                 I    =           51
42649
 XDOT =       6310
987674                 Wp   =           42
31135
 YDOT =       4283
784022  meter/sec      RA   =          209
75979  deg
 ZDOT =       -735
092416                 TA   =           54
76244
                                          MA   =           54
71092
                                          Ha   =            229
557  n
mi
                                          Hp   =            222
349

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9224065
88                 X    =         2821842
59
 Y    =      -10605211
10  feet           Y    =        -3200970
13  meter
 Z    =       17284595
78                 Z    =         5282026
96
 XDOT =      20705
340139                 XDOT =        6266
186648
 YDOT =      14054
409521  feet/sec       YDOT =        4354
107514  meter/sec
 ZDOT =      -2411
720524                 ZDOT =        -704
545583

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5094853
32                 X    =         1552911
29
 Y    =       13015261
04  feet           Y    =         3967051
56  meter
 Z    =       17348100
62                 Z    =         5287701
07
 XDOT =     -21182
732616                 XDOT =       -6456
496901
 YDOT =      11336
787361  feet/sec       YDOT =        3455
452787  meter/sec
 ZDOT =      -2269
787617                 ZDOT =        -691
831266


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
30972786  
00016717  00000-0  10270-3 0  9162
2 25544  51
6445 210
7135 0002899  19
3013 340
8246 15
48990258 30169


Satellite: ISS
Catalog Number: 25544
Epoch time:      21049
30972786   =   yrday
fracday
Element set:     916
Inclination:       51
6445  deg
RA of node:       210
7135  deg
Eccentricity:     
0002899     
Arg of perigee:    19
3013  deg
Mean anomaly:     340
8246  deg
Mean motion:   15
48990258  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3016
Checksum:              315


Coasting Arc #18 (Orbit 3030)
---------------------------------------

Vector Time (GMT): 2021/050/06:18:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957811
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2510601
10                 A    =         6792557
52  meter
 Y    =        3475501
54  meter          E    =           
0015809
 Z    =       -5281997
91                 I    =           51
45628
 XDOT =      -6650
143018                 Wp   =           85
11284
 YDOT =      -3708
374597  meter/sec      RA   =          204
80112  deg
 ZDOT =        724
019869                 TA   =          191
82007
                                          MA   =          191
85722
                                          Ha   =            229
780  n
mi
                                          Hp   =            222
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8236880
26                 X    =        -2523622
11
 Y    =       11402564
10  feet           Y    =         3447353
27  meter
 Z    =      -17329389
47                 Z    =        -5294224
94
 XDOT =     -21818
054521                 XDOT =       -6611
697409
 YDOT =     -12166
583325  feet/sec       YDOT =       -3782
526315  meter/sec
 ZDOT =       2375
393272                 ZDOT =         691
810038

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6476612
64                 X    =        -1974071
53
 Y    =      -12407584
08  feet           Y    =        -3781831
63  meter
 Z    =      -17386136
72                 Z    =        -5299294
47
 XDOT =      19844
935320                 XDOT =        6048
736285
 YDOT =     -13462
975977  feet/sec       YDOT =       -4103
515078  meter/sec
 ZDOT =       2225
721955                 ZDOT =         678
400052


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
27748372  
00016717  00000-0  10270-3 0  9173
2 25544  51
6442 205
9267 0003054  23
3477 336
7811 15
48974633 30319


Satellite: ISS
Catalog Number: 25544
Epoch time:      21050
27748372   =   yrday
fracday
Element set:     917
Inclination:       51
6442  deg
RA of node:       205
9267  deg
Eccentricity:     
0003054     
Arg of perigee:    23
3477  deg
Mean anomaly:     336
7811  deg
Mean motion:   15
48974633  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3031
Checksum:              306


Coasting Arc #19 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2021/050/19:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 957811
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         122948
84                 A    =         6793081
47  meter
 Y    =       -4395934
17  meter          E    =           
0005200
 Z    =        5173009
28                 I    =           51
47304
 XDOT =       7322
688886                 Wp   =           90
78791
 YDOT =       1806
896053  meter/sec      RA   =          202
11644  deg
 ZDOT =       1360
171416                 TA   =          346
09269
                                          MA   =          346
10700
                                          Ha   =            229
847  n
mi
                                          Hp   =            222
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         403375
44                 X    =          146969
25
 Y    =      -14422356
19  feet           Y    =        -4394424
89  meter
 Z    =       16971815
21                 Z    =         5173664
90
 XDOT =      24024
569836                 XDOT =        7295
332557
 YDOT =       5928
136656  feet/sec       YDOT =        1888
630701  meter/sec
 ZDOT =       4462
504645                 ZDOT =        1395
675146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14136727
38                 X    =        -4308874
51
 Y    =       -2866841
48  feet           Y    =         -873813
28  meter
 Z    =       16974797
20                 Z    =         5173918
19
 XDOT =       9923
774324                 XDOT =        3024
766414
 YDOT =     -21511
296236  feet/sec       YDOT =       -6556
643093  meter/sec
 ZDOT =       4627
462842                 ZDOT =        1410
450674


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
85813658  
00016717  00000-0  10270-3 0  9188
2 25544  51
6424 203
0531 0002957  31
0095 329
1229 15
48964210 30404


Satellite: ISS
Catalog Number: 25544
Epoch time:      21050
85813658   =   yrday
fracday
Element set:     918
Inclination:       51
6424  deg
RA of node:       203
0531  deg
Eccentricity:     
0002957     
Arg of perigee:    31
0095  deg
Mean anomaly:     329
1229  deg
Mean motion:   15
48964210  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3040
Checksum:              286
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