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

 
Date: February 24th 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


050/19:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 222 1

051/17:36:48 295 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 222 1

053/09:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 222 0

054/01:32:30 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 221 9

063/11:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 2
000/00:00:00 000 0 0 0 0 221 8

Coasting Arc #1 (Orbit 3005)
---------------------------------------

Vector Time (GMT): 2021/048/14:53:53
651
Vector Time (MET): N/A
Weight (LBS)     : 957236
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4607312
46                 A    =         6794794
36  meter
 Y    =       -1531324
39  meter          E    =           
0009802
 Z    =        4749270
39                 I    =           51
41332
 XDOT =       4597
800926                 Wp   =           53
70439
 YDOT =       5516
878978  meter/sec      RA   =          212
92229  deg
 ZDOT =      -2671
990580                 TA   =           62
83971
                                          MA   =           62
73980
                                          Ha   =            229
642  n
mi
                                          Hp   =            222
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15115854
52                 X    =         4601024
95
 Y    =       -5024030
14  feet           Y    =        -1479837
04  meter
 Z    =       15581595
77                 Z    =         4771635
31
 XDOT =      15084
648708                 XDOT =        4548
746553
 YDOT =      18099
996647  feet/sec       YDOT =        5568
020505  meter/sec
 ZDOT =      -8766
373293                 ZDOT =       -2649
776051

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13859162
15                 X    =         4224272
62
 Y    =       -7642416
65  feet           Y    =        -2329408
60  meter
 Z    =       15685444
07                 Z    =         4780923
35
 XDOT =      17597
454665                 XDOT =        5363
704182
 YDOT =      14067
868629  feet/sec       YDOT =        4287
886358  meter/sec
 ZDOT =      -8663
135182                 ZDOT =       -2640
523603


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
66450415  
00016717  00000-0  10270-3 0  9003
2 25544  51
6426 213
8989 0002614  28
5435 331
5857 15
48946158 30068


Satellite: ISS
Catalog Number: 25544
Epoch time:      21048
66450415   =   yrday
fracday
Element set:     900
Inclination:       51
6426  deg
RA of node:       213
8989  deg
Eccentricity:     
0002614     
Arg of perigee:    28
5435  deg
Mean anomaly:     331
5857  deg
Mean motion:   15
48946158  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3006
Checksum:              315


Coasting Arc #2 (Orbit 3020)
---------------------------------------

Vector Time (GMT): 2021/049/14:57:53
651
Vector Time (MET): N/A
Weight (LBS)     : 957236
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5490393
08                 A    =         6797632
16  meter
 Y    =         659130
13  meter          E    =           
0007812
 Z    =       -3959941
04                 I    =           51
45345
 XDOT =      -3537
444612                 Wp   =           88
20787
 YDOT =      -5483
277113  meter/sec      RA   =          207
94415  deg
 ZDOT =       3999
016471                 TA   =          223
68218
                                          MA   =          223
74403
                                          Ha   =            229
692  n
mi
                                          Hp   =            222
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18013100
65                 X    =        -5478120
80
 Y    =        2162500
42  feet           Y    =          597801
09  meter
 Z    =      -12991932
54                 Z    =        -3986581
00
 XDOT =     -11605
789411                 XDOT =       -3495
290646
 YDOT =     -17989
754308  feet/sec       YDOT =       -5522
599549  meter/sec
 ZDOT =      13120
132779                 ZDOT =        3981
935778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17045447
47                 X    =        -5195452
39
 Y    =        5947327
56  feet           Y    =         1812745
44  meter
 Z    =      -13115659
71                 Z    =        -3997653
08
 XDOT =     -14840
741796                 XDOT =       -4523
458099
 YDOT =     -13826
694517  feet/sec       YDOT =       -4214
376489  meter/sec
 ZDOT =      13040
722736                 ZDOT =        3974
812290


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
63224706  
00016717  00000-0  10270-3 0  9014
2 25544  51
6437 209
1130 0002665  28
2005 331
9289 15
48972457 30213


Satellite: ISS
Catalog Number: 25544
Epoch time:      21049
63224706   =   yrday
fracday
Element set:     901
Inclination:       51
6437  deg
RA of node:       209
1130  deg
Eccentricity:     
0002665     
Arg of perigee:    28
2005  deg
Mean anomaly:     331
9289  deg
Mean motion:   15
48972457  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3021
Checksum:              291


Coasting Arc #3 (Orbit 3036)
---------------------------------------

Vector Time (GMT): 2021/050/14:57:53
651
Vector Time (MET): N/A
Weight (LBS)     : 957236
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5418639
64                 A    =         6797717
89  meter
 Y    =       -1111044
06  meter          E    =           
0013078
 Z    =        3943801
20                 I    =           51
48381
 XDOT =       3991
520497                 Wp   =           71
44124
 YDOT =       5163
812423  meter/sec      RA   =          202
98626  deg
 ZDOT =      -4014
421611                 TA   =           60
65959
                                          MA   =           60
52901
                                          Ha   =            229
773  n
mi
                                          Hp   =            222
144

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17777689
10                 X    =         5411504
52
 Y    =       -3645157
68  feet           Y    =        -1050488
76  meter
 Z    =       12938980
30                 Z    =         3970105
10
 XDOT =      13095
539687                 XDOT =        3952
979970
 YDOT =      16941
641807  feet/sec       YDOT =        5208
232927  meter/sec
 ZDOT =     -13170
674577                 ZDOT =       -3995
126358

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16369778
04                 X    =         4989508
35
 Y    =       -7628053
26  feet           Y    =        -2325030
63  meter
 Z    =       13061155
61                 Z    =         3981040
23
 XDOT =      16183
120476                 XDOT =        4932
615121
 YDOT =      12247
314727  feet/sec       YDOT =        3732
981529  meter/sec
 ZDOT =     -13080
966786                 ZDOT =       -3987
078677


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
66450645  
00016717  00000-0  10270-3 0  9023
2 25544  51
6433 204
0072 0002778  35
7489 324
3846 15
48958996 30376


Satellite: ISS
Catalog Number: 25544
Epoch time:      21050
66450645   =   yrday
fracday
Element set:     902
Inclination:       51
6433  deg
RA of node:       204
0072  deg
Eccentricity:     
0002778     
Arg of perigee:    35
7489  deg
Mean anomaly:     324
3846  deg
Mean motion:   15
48958996  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3037
Checksum:              323


Coasting Arc #4 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2021/050/19:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 957236
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         175255
29                 A    =         6792979
68  meter
 Y    =       -4382758
43  meter          E    =           
0005275
 Z    =        5182436
37                 I    =           51
47281
 XDOT =       7321
530633                 Wp   =           89
15575
 YDOT =       1846
647727  meter/sec      RA   =          202
11439  deg
 ZDOT =       1313
022995                 TA   =          348
18822
                                          MA   =          348
20059
                                          Ha   =            229
879  n
mi
                                          Hp   =            222
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         574984
56                 X    =          199078
70
 Y    =      -14379128
70  feet           Y    =        -4380665
32  meter
 Z    =       17002743
99                 Z    =         5183345
59
 XDOT =      24020
769792                 XDOT =        7293
958890
 YDOT =       6058
555534  feet/sec       YDOT =        1928
368217  meter/sec
 ZDOT =       4307
818224                 ZDOT =        1348
520575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14063478
67                 X    =        -4286548
30
 Y    =       -3027709
92  feet           Y    =         -922845
98  meter
 Z    =       17006904
28                 Z    =         5183704
42
 XDOT =      10039
853730                 XDOT =        3060
147417
 YDOT =     -21490
571568  feet/sec       YDOT =       -6550
326214  meter/sec
 ZDOT =       4472
748436                 ZDOT =        1363
293723


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
85805354  
00016717  00000-0  10270-3 0  9036
2 25544  51
6423 203
0524 0003107  32
7068 327
4273 15
48984120 30403


Satellite: ISS
Catalog Number: 25544
Epoch time:      21050
85805354   =   yrday
fracday
Element set:     903
Inclination:       51
6423  deg
RA of node:       203
0524  deg
Eccentricity:     
0003107     
Arg of perigee:    32
7068  deg
Mean anomaly:     327
4273  deg
Mean motion:   15
48984120  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3040
Checksum:              273


Coasting Arc #5 (Orbit 3053)
---------------------------------------

Vector Time (GMT): 2021/051/17:36:48
295
Vector Time (MET): N/A
Weight (LBS)     : 957236
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5138253
63                 A    =         6801800
83  meter
 Y    =        3698190
94  meter          E    =           
0005913
 Z    =       -2490133
25                 I    =           51
53127
 XDOT =      -4676
814531                 Wp   =          102
43350
 YDOT =       2937
932544  meter/sec      RA   =          197
53241  deg
 ZDOT =      -5299
035025                 TA   =          105
43976
                                          MA   =          105
37445
                                          Ha   =            229
925  n
mi
                                          Hp   =            222
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16857787
51                 X    =         5108612
88
 Y    =       12133172
38  feet           Y    =         3755484
87  meter
 Z    =       -8169728
50                 Z    =        -2465246
04
 XDOT =     -15343
879696                 XDOT =       -4683
580559
 YDOT =       9638
886299  feet/sec       YDOT =        2885
595198  meter/sec
 ZDOT =     -17385
285515                 ZDOT =       -5321
769206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19738385
09                 X    =         6016259
78
 Y    =       -6608469
72  feet           Y    =        -2014261
57  meter
 Z    =       -8054043
53                 Z    =        -2454872
47
 XDOT =      -1581
326624                 XDOT =        -481
988355
 YDOT =      16545
418938  feet/sec       YDOT =        5043
043692  meter/sec
 ZDOT =     -17490
866733                 ZDOT =       -5331
216180


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
76128002  
00016717  00000-0  10270-3 0  9046
2 25544  51
6418 198
5848 0002972  35
9148 324
2202 15
48978061 30546


Satellite: ISS
Catalog Number: 25544
Epoch time:      21051
76128002   =   yrday
fracday
Element set:     904
Inclination:       51
6418  deg
RA of node:       198
5848  deg
Eccentricity:     
0002972     
Arg of perigee:    35
9148  deg
Mean anomaly:     324
2202  deg
Mean motion:   15
48978061  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3054
Checksum:              306


Coasting Arc #6 (Orbit 3069)
---------------------------------------

Vector Time (GMT): 2021/052/17:36:48
295
Vector Time (MET): N/A
Weight (LBS)     : 957236
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5442568
96                 A    =         6801885
95  meter
 Y    =       -3226259
10  meter          E    =           
0016279
 Z    =        2474144
62                 I    =           51
56413
 XDOT =       4403
284433                 Wp   =           68
56677
 YDOT =      -3337
070410  meter/sec      RA   =          192
57899  deg
 ZDOT =       5312
357592                 TA   =          319
13983
                                          MA   =          319
26175
                                          Ha   =            230
033  n
mi
                                          Hp   =            222
087

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17856197
39                 X    =        -5418105
19
 Y    =      -10584839
55  feet           Y    =        -3286985
06  meter
 Z    =        8117272
38                 Z    =         2447766
66
 XDOT =      14446
471237                 XDOT =        4414
469432
 YDOT =     -10948
393733  feet/sec       YDOT =       -3287
767217  meter/sec
 ZDOT =      17428
994725                 ZDOT =        5333
773736

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18921462
07                 X    =        -5767261
64
 Y    =        8650816
33  feet           Y    =         2636768
82  meter
 Z    =        7994646
60                 Z    =         2436768
28
 XDOT =       -166
884079                 XDOT =         -50
866267
 YDOT =     -16632
844850  feet/sec       YDOT =       -5069
691110  meter/sec
 ZDOT =      17528
459807                 ZDOT =        5342
674549


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
79353732  
00016717  00000-0  10270-3 0  9051
2 25544  51
6418 193
4789 0003050  38
6564 321
4804 15
48963704 30707


Satellite: ISS
Catalog Number: 25544
Epoch time:      21052
79353732   =   yrday
fracday
Element set:     905
Inclination:       51
6418  deg
RA of node:       193
4789  deg
Eccentricity:     
0003050     
Arg of perigee:    38
6564  deg
Mean anomaly:     321
4804  deg
Mean motion:   15
48963704  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3070
Checksum:              312


Coasting Arc #7 (Orbit 3079)
---------------------------------------

Vector Time (GMT): 2021/053/09:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6546044
08                 A    =         6802833
93  meter
 Y    =        -376328
28  meter          E    =           
0014853
 Z    =        1792194
82                 I    =           51
58827
 XDOT =       1834
933309                 Wp   =          102
98119
 YDOT =       4836
953120  meter/sec      RA   =          189
22682  deg
 ZDOT =      -5650
165885                 TA   =           57
35582
                                          MA   =           57
21259
                                          Ha   =            229
850  n
mi
                                          Hp   =            221
981

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21476522
57                 X    =         6541060
52
 Y    =       -1234672
83  feet           Y    =         -303153
58  meter
 Z    =        5879904
26                 Z    =         1823980
13
 XDOT =       6020
122404                 XDOT =        1808
153309
 YDOT =      15869
268768  feet/sec       YDOT =        4857
322996  meter/sec
 ZDOT =     -18537
289649                 ZDOT =       -5641
317682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10704252
61                 X    =         3262656
20
 Y    =       18612509
94  feet           Y    =         5673093
03  meter
 Z    =        6027616
67                 Z    =         1837217
56
 XDOT =     -10077
295644                 XDOT =       -3071
559712
 YDOT =      11823
107654  feet/sec       YDOT =        3603
683213  meter/sec
 ZDOT =     -18496
089788                 ZDOT =       -5637
608167


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
43869520  
00016717  00000-0  10270-3 0  9061
2 25544  51
6397 190
2847 0003010  36
4692 323
6663 15
49008608 30809


Satellite: ISS
Catalog Number: 25544
Epoch time:      21053
43869520   =   yrday
fracday
Element set:     906
Inclination:       51
6397  deg
RA of node:       190
2847  deg
Eccentricity:     
0003010     
Arg of perigee:    36
4692  deg
Mean anomaly:     323
6663  deg
Mean motion:   15
49008608  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3080
Checksum:              304


Coasting Arc #8 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2021/054/01:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1767243
70                 A    =         6793655
27  meter
 Y    =        4209025
49  meter          E    =           
0015634
 Z    =       -5045688
54                 I    =           51
58238
 XDOT =      -7359
028341                 Wp   =           68
50841
 YDOT =        770
387831  meter/sec      RA   =          185
98827  deg
 ZDOT =      -1934
094356                 TA   =          182
65668
                                          MA   =          182
66499
                                          Ha   =            230
045  n
mi
                                          Hp   =            221
949

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5798043
65                 X    =         1744554
21
 Y    =       13809138
75  feet           Y    =         4228661
27  meter
 Z    =      -16554096
28                 Z    =        -5037159
25
 XDOT =     -24143
793770                 XDOT =       -7357
701629
 YDOT =       2527
519132  feet/sec       YDOT =         688
101305  meter/sec
 ZDOT =      -6345
453923                 ZDOT =       -1969
837518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4781574
47                 X    =        -1457423
90
 Y    =      -14239362
73  feet           Y    =        -4340157
76  meter
 Z    =      -16514382
26                 Z    =        -5033583
71
 XDOT =      23186
410923                 XDOT =        7067
218049
 YDOT =       -231
212094  feet/sec       YDOT =         -70
473446  meter/sec
 ZDOT =      -6511
571751                 ZDOT =       -1984
727070


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
08385593  
00016717  00000-0  10270-3 0  9077
2 25544  51
6425 187
0972 0003366  39
4349 320
7046 15
48994477 30901


Satellite: ISS
Catalog Number: 25544
Epoch time:      21054
08385593   =   yrday
fracday
Element set:     907
Inclination:       51
6425  deg
RA of node:       187
0972  deg
Eccentricity:     
0003366     
Arg of perigee:    39
4349  deg
Mean anomaly:     320
7046  deg
Mean motion:   15
48994477  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3090
Checksum:              332


Coasting Arc #9 (Orbit 3105)
---------------------------------------

Vector Time (GMT): 2021/055/01:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2118650
46                 A    =         6793589
29  meter
 Y    =       -4029131
16  meter          E    =           
0007103
 Z    =        5037009
34                 I    =           51
61616
 XDOT =       7281
893489                 Wp   =           97
38061
 YDOT =      -1402
745505  meter/sec      RA   =          181
04107  deg
 ZDOT =       1937
583248                 TA   =          333
78764
                                          MA   =          333
82358
                                          Ha   =            230
061  n
mi
                                          Hp   =            221
882

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6950952
95                 X    =        -2097904
23
 Y    =      -13218934
24  feet           Y    =        -4052707
43  meter
 Z    =       16525621
19                 Z    =         5026768
45
 XDOT =      23890
726671                 XDOT =        7287
626817
 YDOT =      -4602
183415  feet/sec       YDOT =       -1321
282059  meter/sec
 ZDOT =       6356
900419                 ZDOT =        1972
968748

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6213546
95                 X    =         1893889
11
 Y    =       13638964
17  feet           Y    =         4157156
28  meter
 Z    =       16477943
31                 Z    =         5022477
12
 XDOT =     -23095
340156                 XDOT =       -7039
459680
 YDOT =       2629
932593  feet/sec       YDOT =         801
603454  meter/sec
 ZDOT =       6521
371819                 ZDOT =        1987
714130


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   21055
11610811  
00016717  00000-0  10270-3 0  9087
2 25544  51
6423 181
9921 0003235  42
3038 317
8361 15
49012929 31068


Satellite: ISS
Catalog Number: 25544
Epoch time:      21055
11610811   =   yrday
fracday
Element set:     908
Inclination:       51
6423  deg
RA of node:       181
9921  deg
Eccentricity:     
0003235     
Arg of perigee:    42
3038  deg
Mean anomaly:     317
8361  deg
Mean motion:   15
49012929  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3106
Checksum:              279


Coasting Arc #10 (Orbit 3120)
---------------------------------------

Vector Time (GMT): 2021/056/01:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2456905
87                 A    =         6793627
86  meter
 Y    =        3838772
05  meter          E    =           
0015826
 Z    =       -5052422
51                 I    =           51
65112
 XDOT =      -7120
163246                 Wp   =           69
79244
 YDOT =       2016
402552  meter/sec      RA   =          176
09538  deg
 ZDOT =      -1929
964548                 TA   =          181
43440
                                          MA   =          181
43895
                                          Ha   =            230
105  n
mi
                                          Hp   =            221
867

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8060714
79                 X    =         2438337
95
 Y    =       12594396
50  feet           Y    =         3866143
02  meter
 Z    =      -16576189
33                 Z    =        -5040533
37
 XDOT =     -23360
115635                 XDOT =       -7132
807728
 YDOT =       6615
493938  feet/sec       YDOT =        1936
709010  meter/sec
 ZDOT =      -6331
904685                 ZDOT =       -1964
581173

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7584953
72                 X    =        -2311893
90
 Y    =      -12957404
16  feet           Y    =        -3949416
79  meter
 Z    =      -16520839
96                 Z    =        -5035552
02
 XDOT =      22651
455948                 XDOT =        6904
163773
 YDOT =      -4979
489647  feet/sec       YDOT =       -1517
748445  meter/sec
 ZDOT =      -6492
815167                 ZDOT =       -1979
010063


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   21056
08384642  
00016717  00000-0  10270-3 0  9095
2 25544  51
6433 177
2054 0003378  46
0062 314
1367 15
49001131 31216


Satellite: ISS
Catalog Number: 25544
Epoch time:      21056
08384642   =   yrday
fracday
Element set:     909
Inclination:       51
6433  deg
RA of node:       177
2054  deg
Eccentricity:     
0003378     
Arg of perigee:    46
0062  deg
Mean anomaly:     314
1367  deg
Mean motion:   15
49001131  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3121
Checksum:              275


Coasting Arc #11 (Orbit 3136)
---------------------------------------

Vector Time (GMT): 2021/057/01:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2771934
70                 A    =         6793589
43  meter
 Y    =       -3601705
29  meter          E    =           
0007367
 Z    =        5043504
11                 I    =           51
68550
 XDOT =       6936
524291                 Wp   =           99
24667
 YDOT =      -2625
935619  meter/sec      RA   =          171
15237  deg
 ZDOT =       1933
526405                 TA   =          331
97949
                                          MA   =          332
01913
                                          Ha   =            230
147  n
mi
                                          Hp   =            221
808

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9094273
94                 X    =        -2755950
97
 Y    =      -11816618
39  feet           Y    =        -3632613
47  meter
 Z    =       16546929
50                 Z    =         5030078
55
 XDOT =      22757
625626                 XDOT =        6955
981114
 YDOT =      -8615
274340  feet/sec       YDOT =       -2548
257523  meter/sec
 ZDOT =       6343
590567                 ZDOT =        1967
267598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8862130
42                 X    =         2701177
35
 Y    =       12077476
15  feet           Y    =         3681214
73  meter
 Z    =       16484428
37                 Z    =         5024453
77
 XDOT =     -22072
532563                 XDOT =       -6727
707925
 YDOT =       7307
809256  feet/sec       YDOT =        2227
420261  meter/sec
 ZDOT =       6500
440380                 ZDOT =        1981
334228


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   21057
11609670  
00016717  00000-0  10270-3 0  9103
2 25544  51
6438 172
0999 0003216  48
8369 311
3058 15
49009914 31373


Satellite: ISS
Catalog Number: 25544
Epoch time:      21057
11609670   =   yrday
fracday
Element set:     910
Inclination:       51
6438  deg
RA of node:       172
0999  deg
Eccentricity:     
0003216     
Arg of perigee:    48
8369  deg
Mean anomaly:     311
3058  deg
Mean motion:   15
49009914  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3137
Checksum:              310


Coasting Arc #12 (Orbit 3151)
---------------------------------------

Vector Time (GMT): 2021/058/01:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3069429
40                 A    =         6793579
80  meter
 Y    =        3358265
94  meter          E    =           
0015997
 Z    =       -5059758
50                 I    =           51
72026
 XDOT =      -6673
692051                 Wp   =           70
84080
 YDOT =       3201
044029  meter/sec      RA   =          166
21146  deg
 ZDOT =      -1923
765316                 TA   =          180
46832
                                          MA   =          180
46982
                                          Ha   =            230
148  n
mi
                                          Hp   =            221
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10070306
42                 X    =         3056224
77
 Y    =       11017932
88  feet           Y    =         3392516
34  meter
 Z    =      -16600257
56                 Z    =        -5044881
18
 XDOT =     -21895
315129                 XDOT =       -6699
646845
 YDOT =      10502
112955  feet/sec       YDOT =        3126
268733  meter/sec
 ZDOT =      -6311
565997                 ZDOT =       -1956
245748

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10054258
51                 X    =        -3064538
00
 Y    =      -11136087
13  feet           Y    =        -3394279
36  meter
 Z    =      -16530998
66                 Z    =        -5038648
39
 XDOT =      21161
108810                 XDOT =        6449
905965
 YDOT =      -9511
362499  feet/sec       YDOT =       -2899
063290  meter/sec
 ZDOT =      -6462
559423                 ZDOT =       -1969
788112


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   21058
08383026  
00016717  00000-0  10270-3 0  9115
2 25544  51
6452 167
3135 0003419  51
3257 308
8198 15
49013166 31525


Satellite: ISS
Catalog Number: 25544
Epoch time:      21058
08383026   =   yrday
fracday
Element set:     911
Inclination:       51
6452  deg
RA of node:       167
3135  deg
Eccentricity:     
0003419     
Arg of perigee:    51
3257  deg
Mean anomaly:     308
8198  deg
Mean motion:   15
49013166  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3152
Checksum:              294


Coasting Arc #13 (Orbit 3167)
---------------------------------------

Vector Time (GMT): 2021/059/01:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3338053
47                 A    =         6793594
31  meter
 Y    =       -3072204
93  meter          E    =           
0007745
 Z    =        5050676
26                 I    =           51
75249
 XDOT =       6389
962712                 Wp   =          100
27136
 YDOT =      -3769
626593  meter/sec      RA   =          161
27292  deg
 ZDOT =       1926
370024                 TA   =          331
04352
                                          MA   =          331
08647
                                          Ha   =            230
295  n
mi
                                          Hp   =            221
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10951619
01                 X    =        -3327983
69
 Y    =      -10079412
49  feet           Y    =        -3109476
70  meter
 Z    =       16570460
17                 Z    =         5034486
47
 XDOT =      20964
444593                 XDOT =        6422
283967
 YDOT =     -12367
541314  feet/sec       YDOT =       -3697
988526  meter/sec
 ZDOT =       6320
111627                 ZDOT =        1957
487953

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11120277
79                 X    =         3389460
67
 Y    =       10018182
44  feet           Y    =         3053542
01  meter
 Z    =       16495093
45                 Z    =         5027704
48
 XDOT =     -20122
079390                 XDOT =       -6133
209798
 YDOT =      11670
399354  feet/sec       YDOT =        3557
137723  meter/sec
 ZDOT =       6464
772177                 ZDOT =        1970
462560


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   21059
11607758  
00016717  00000-0  10270-3 0  9122
2 25544  51
6447 162
2079 0003387  55
6935 304
4535 15
49003296 31681


Satellite: ISS
Catalog Number: 25544
Epoch time:      21059
11607758   =   yrday
fracday
Element set:     912
Inclination:       51
6447  deg
RA of node:       162
2079  deg
Eccentricity:     
0003387     
Arg of perigee:    55
6935  deg
Mean anomaly:     304
4535  deg
Mean motion:   15
49003296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3168
Checksum:              317


Coasting Arc #14 (Orbit 3182)
---------------------------------------

Vector Time (GMT): 2021/060/01:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3588395
19                 A    =         6793554
85  meter
 Y    =        2783509
85  meter          E    =           
0016034
 Z    =       -5067148
15                 I    =           51
78428
 XDOT =      -6033
531130                 Wp   =           72
05354
 YDOT =       4290
857942  meter/sec      RA   =          156
33697  deg
 ZDOT =      -1915
868828                 TA   =          179
35386
                                          MA   =          179
35178
                                          Ha   =            230
157  n
mi
                                          Hp   =            221
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11772950
09                 X    =         3581615
22
 Y    =        9132250
15  feet           Y    =         2823599
46  meter
 Z    =      -16624501
79                 Z    =        -5049734
24
 XDOT =     -19795
049640                 XDOT =       -6071
758399
 YDOT =      14077
617919  feet/sec       YDOT =        4223
172708  meter/sec
 ZDOT =      -6285
658885                 ZDOT =       -1945
269998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12090969
51                 X    =        -3685327
51
 Y    =       -8859879
49  feet           Y    =        -2700491
27  meter
 Z    =      -16543439
74                 Z    =        -5042440
43
 XDOT =      18781
184340                 XDOT =        5724
504987
 YDOT =     -13639
610018  feet/sec       YDOT =       -4157
353133  meter/sec
 ZDOT =      -6422
338524                 ZDOT =       -1957
528782


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   21060
08380858  
00016717  00000-0  10270-3 0  9130
2 25544  51
6448 157
4220 0003336  56
6874 303
4595 15
49016192 31834


Satellite: ISS
Catalog Number: 25544
Epoch time:      21060
08380858   =   yrday
fracday
Element set:     913
Inclination:       51
6448  deg
RA of node:       157
4220  deg
Eccentricity:     
0003336     
Arg of perigee:    56
6874  deg
Mean anomaly:     303
4595  deg
Mean motion:   15
49016192  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3183
Checksum:              308


Coasting Arc #15 (Orbit 3198)
---------------------------------------

Vector Time (GMT): 2021/061/01:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3803791
91                 A    =         6793587
04  meter
 Y    =       -2457159
51  meter          E    =           
0007880
 Z    =        5058048
35                 I    =           51
81532
 XDOT =       5657
892896                 Wp   =          102
16641
 YDOT =      -4802
391492  meter/sec      RA   =          151
40227  deg
 ZDOT =       1917
785692                 TA   =          329
24970
                                          MA   =          329
29585
                                          Ha   =            230
337  n
mi
                                          Hp   =            221
661

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12479632
26                 X    =        -3800601
22
 Y    =       -8061546
95  feet           Y    =        -2499677
93  meter
 Z    =       16594646
81                 Z    =         5039579
29
 XDOT =      18562
640735                 XDOT =        5701
858843
 YDOT =     -15755
877598  feet/sec       YDOT =       -4738
874833  meter/sec
 ZDOT =       6291
947809                 ZDOT =        1945
376333

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12904810
69                 X    =         3933386
30
 Y    =        7552582
97  feet           Y    =         2302027
29  meter
 Z    =       16508676
95                 Z    =         5031844
73
 XDOT =     -17325
526124                 XDOT =       -5280
820362
 YDOT =      15540
100995  feet/sec       YDOT =        4736
622783  meter/sec
 ZDOT =       6420
211707                 ZDOT =        1956
880528


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   21061
11605307  
00016717  00000-0  10270-3 0  9145
2 25544  51
6452 152
3160 0003328  61
0196 299
1287 15
48999787 31999


Satellite: ISS
Catalog Number: 25544
Epoch time:      21061
11605307   =   yrday
fracday
Element set:     914
Inclination:       51
6452  deg
RA of node:       152
3160  deg
Eccentricity:     
0003328     
Arg of perigee:    61
0196  deg
Mean anomaly:     299
1287  deg
Mean motion:   15
48999787  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3199
Checksum:              318


Coasting Arc #16 (Orbit 3213)
---------------------------------------

Vector Time (GMT): 2021/062/01:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3998977
58                 A    =         6793516
05  meter
 Y    =        2133513
23  meter          E    =           
0016144
 Z    =       -5075159
86                 I    =           51
84405
 XDOT =      -5220
024473                 Wp   =           73
04986
 YDOT =       5254
327620  meter/sec      RA   =          146
46935  deg
 ZDOT =      -1904
729329                 TA   =          178
48654
                                          MA   =          178
48165
                                          Ha   =            230
185  n
mi
                                          Hp   =            221
730

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13120005
18                 X    =         3999474
71
 Y    =        6999715
31  feet           Y    =         2178235
05  meter
 Z    =      -16650786
93                 Z    =        -5055733
58
 XDOT =     -17126
064543                 XDOT =       -5269
140031
 YDOT =      17238
607677  feet/sec       YDOT =        5195
678759  meter/sec
 ZDOT =      -6249
111971                 ZDOT =       -1930
205590

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13611956
68                 X    =        -4148924
40
 Y    =       -6232834
57  feet           Y    =        -1899767
98  meter
 Z    =      -16560364
26                 Z    =        -5047599
03
 XDOT =      15617
144246                 XDOT =        4760
105566
 YDOT =     -17191
994391  feet/sec       YDOT =       -5240
119890  meter/sec
 ZDOT =      -6367
550557                 ZDOT =       -1940
829410


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   21062
08377886  
00016717  00000-0  10270-3 0  9151
2 25544  51
6447 147
5291 0003352  61
4044 298
7443 15
49022029 32141


Satellite: ISS
Catalog Number: 25544
Epoch time:      21062
08377886   =   yrday
fracday
Element set:     915
Inclination:       51
6447  deg
RA of node:       147
5291  deg
Eccentricity:     
0003352     
Arg of perigee:    61
4044  deg
Mean anomaly:     298
7443  deg
Mean motion:   15
49022029  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3214
Checksum:              306


Coasting Arc #17 (Orbit 3229)
---------------------------------------

Vector Time (GMT): 2021/063/01:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4155165
94                 A    =         6793585
43  meter
 Y    =       -1777597
60  meter          E    =           
0008132
 Z    =        5065939
41                 I    =           51
87082
 XDOT =       4764
305255                 Wp   =          103
33054
 YDOT =      -5694
352986  meter/sec      RA   =          141
53850  deg
 ZDOT =       1905
262330                 TA   =          328
22451
                                          MA   =          328
27356
                                          Ha   =            230
439  n
mi
                                          Hp   =            221
586

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13632434
19                 X    =        -4159586
68
 Y    =       -5832013
12  feet           Y    =        -1824088
09  meter
 Z    =       16620536
13                 Z    =         5045744
80
 XDOT =      15630
922751                 XDOT =        4818
372575
 YDOT =     -18682
260454  feet/sec       YDOT =       -5640
772666  meter/sec
 ZDOT =       6250
860662                 ZDOT =        1928
536880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14141311
93                 X    =         4310271
88
 Y    =        4795278
57  feet           Y    =         1461600
91  meter
 Z    =       16526538
07                 Z    =         5037288
80
 XDOT =     -13808
678853                 XDOT =       -4208
885314
 YDOT =      18755
891794  feet/sec       YDOT =        5716
795819  meter/sec
 ZDOT =       6359
070867                 ZDOT =        1938
244800


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   21063
11601991  
00016717  00000-0  10270-3 0  9164
2 25544  51
6438 142
4231 0003449  66
5010 293
6503 15
48992308 32309


Satellite: ISS
Catalog Number: 25544
Epoch time:      21063
11601991   =   yrday
fracday
Element set:     916
Inclination:       51
6438  deg
RA of node:       142
4231  deg
Eccentricity:     
0003449     
Arg of perigee:    66
5010  deg
Mean anomaly:     293
6503  deg
Mean motion:   15
48992308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3230
Checksum:              287


Coasting Arc #18 (Orbit 3235)
---------------------------------------

Vector Time (GMT): 2021/063/11:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 972366
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4575004
35                 A    =         6794354
16  meter
 Y    =        1150468
70  meter          E    =           
0014819
 Z    =       -4903560
28                 I    =           51
88356
 XDOT =      -4093
508892                 Wp   =           73
32168
 YDOT =       5991
958305  meter/sec      RA   =          139
47684  deg
 ZDOT =      -2415
314809                 TA   =          173
02297
                                          MA   =          173
00232
                                          Ha   =            230
216  n
mi
                                          Hp   =            221
806

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15009856
80                 X    =         4585617
90
 Y    =        3774503
61  feet           Y    =         1201688
82  meter
 Z    =      -16087796
18                 Z    =        -4881311
19
 XDOT =     -13430
147285                 XDOT =       -4148
476462
 YDOT =      19658
655855  feet/sec       YDOT =        5945
874277  meter/sec
 ZDOT =      -7924
261186                 ZDOT =       -2435
333062

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12158643
56                 X    =         3705954
56
 Y    =        9748394
40  feet           Y    =         2971310
61  meter
 Z    =      -15984244
06                 Z    =        -4871997
59
 XDOT =     -19656
835478                 XDOT =       -5991
403454
 YDOT =      11381
419142  feet/sec       YDOT =        3469
056554  meter/sec
 ZDOT =      -8017
324554                 ZDOT =       -2443
680524


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   21063
50310937  
00016717  00000-0  10270-3 0  9175
2 25544  51
6431 140
5059 0003089  74
7520 285
3971 15
48984602 32367


Satellite: ISS
Catalog Number: 25544
Epoch time:      21063
50310937   =   yrday
fracday
Element set:     917
Inclination:       51
6431  deg
RA of node:       140
5059  deg
Eccentricity:     
0003089     
Arg of perigee:    74
7520  deg
Mean anomaly:     285
3971  deg
Mean motion:   15
48984602  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3236
Checksum:              306
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