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

 
Date: January 30th 2021

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

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19920 769 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


029/19:22:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 7
000/00:00:00 000 0 0 0 0 223 3

033/03:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 9
000/00:00:00 000 0 0 0 0 223 3

036/13:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 0
000/00:00:00 000 0 0 0 0 223 2

040/05:21:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 2
000/00:00:00 000 0 0 0 0 222 9

Coasting Arc #1 (Orbit 2646)
---------------------------------------

Vector Time (GMT): 2021/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4971659
15                 A    =         6803871
88  meter
 Y    =       -4428107
50  meter          E    =           
0008554
 Z    =       -1379880
45                 I    =           51
45281
 XDOT =       4134
442295                 Wp   =           22
17842
 YDOT =       2845
039201  meter/sec      RA   =          327
81490  deg
 ZDOT =       5785
881322                 TA   =          322
78174
                                          MA   =          322
84100
                                          Ha   =            228
595  n
mi
                                          Hp   =            223
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16311217
69                 X    =         5027508
63
 Y    =      -14527911
75  feet           Y    =        -4372198
42  meter
 Z    =       -4527166
84                 Z    =        -1355595
38
 XDOT =      13564
443224                 XDOT =        4074
217010
 YDOT =       9334
118112  feet/sec       YDOT =        2890
936188  meter/sec
 ZDOT =      18982
550269                 ZDOT =        5805
818420

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21192699
04                 X    =         6459534
67
 Y    =        5384705
10  feet           Y    =         1641258
11  meter
 Z    =       -4414265
55                 Z    =        -1345468
14
 XDOT =        195
986699                 XDOT =          59
736746
 YDOT =      14812
039199  feet/sec       YDOT =        4514
709548  meter/sec
 ZDOT =      19074
924084                 ZDOT =        5814
036861


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21025
50262281  
00016717  00000-0  10270-3 0  9003
2 25544  51
6439 328
4595 0002289 295
7716  64
3197 15
48877081 26472


Satellite: ISS
Catalog Number: 25544
Epoch time:      21025
50262281   =   yrday
fracday
Element set:     900
Inclination:       51
6439  deg
RA of node:       328
4595  deg
Eccentricity:     
0002289     
Arg of perigee:   295
7716  deg
Mean anomaly:      64
3197  deg
Mean motion:   15
48877081  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2647
Checksum:              329


Coasting Arc #2 (Orbit 2662)
---------------------------------------

Vector Time (GMT): 2021/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4560098
18                 A    =         6803834
42  meter
 Y    =        4846443
83  meter          E    =           
0011506
 Z    =        1391115
46                 I    =           51
42561
 XDOT =      -4386
038298                 Wp   =          119
13676
 YDOT =      -2459
347725  meter/sec      RA   =          322
85404  deg
 ZDOT =      -5778
694751                 TA   =           45
69014
                                          MA   =           45
59585
                                          Ha   =            228
630  n
mi
                                          Hp   =            223
651

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14960952
03                 X    =        -4620710
75
 Y    =       15900406
28  feet           Y    =         4795110
49  meter
 Z    =        4564027
09                 Z    =         1368818
11
 XDOT =     -14389
889429                 XDOT =       -4330
142267
 YDOT =      -8068
726132  feet/sec       YDOT =       -2508
082457  meter/sec
 ZDOT =     -18958
972280                 ZDOT =       -5799
864356

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21629112
13                 X    =        -6592553
38
 Y    =       -3125736
87  feet           Y    =         -952724
60  meter
 Z    =        4460339
25                 Z    =         1359511
40
 XDOT =      -1822
661205                 XDOT =        -555
547135
 YDOT =     -14729
226367  feet/sec       YDOT =       -4489
468197  meter/sec
 ZDOT =     -19057
086439                 ZDOT =       -5808
599947


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21026
53493885  
00016717  00000-0  10270-3 0  9014
2 25544  51
6449 323
3540 0002266 302
0302  58
0628 15
48885910 26632


Satellite: ISS
Catalog Number: 25544
Epoch time:      21026
53493885   =   yrday
fracday
Element set:     901
Inclination:       51
6449  deg
RA of node:       323
3540  deg
Eccentricity:     
0002266     
Arg of perigee:   302
0302  deg
Mean anomaly:      58
0628  deg
Mean motion:   15
48885910  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2663
Checksum:              300


Coasting Arc #3 (Orbit 2677)
---------------------------------------

Vector Time (GMT): 2021/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4092928
45                 A    =         6803792
91  meter
 Y    =       -5237524
99  meter          E    =           
0008813
 Z    =       -1429443
50                 I    =           51
39824
 XDOT =       4612
376367                 Wp   =           22
10212
 YDOT =       2036
065498  meter/sec      RA   =          317
89189  deg
 ZDOT =       5766
044832                 TA   =          322
29175
                                          MA   =          322
35349
                                          Ha   =            228
689  n
mi
                                          Hp   =            223
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13428242
95                 X    =         4158135
07
 Y    =      -17183480
92  feet           Y    =        -5191390
19  meter
 Z    =       -4689775
26                 Z    =        -1409404
34
 XDOT =      15132
468395                 XDOT =        4561
258354
 YDOT =       6680
004915  feet/sec       YDOT =        2087
358084  meter/sec
 ZDOT =      18917
469921                 ZDOT =        5788
325313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21814636
07                 X    =         6649101
08
 Y    =         759607
31  feet           Y    =          231528
31  meter
 Z    =       -4596560
34                 Z    =        -1401031
59
 XDOT =       3490
216080                 XDOT =        1063
817861
 YDOT =      14468
433880  feet/sec       YDOT =        4409
978647  meter/sec
 ZDOT =      19020
761772                 ZDOT =        5797
528188


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21027
50273349  
00016717  00000-0  10270-3 0  9024
2 25544  51
6440 318
5686 0002320 306
1407  53
9528 15
48882114 26784


Satellite: ISS
Catalog Number: 25544
Epoch time:      21027
50273349   =   yrday
fracday
Element set:     902
Inclination:       51
6440  deg
RA of node:       318
5686  deg
Eccentricity:     
0002320     
Arg of perigee:   306
1407  deg
Mean anomaly:      53
9528  deg
Mean motion:   15
48882114  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2678
Checksum:              302


Coasting Arc #4 (Orbit 2693)
---------------------------------------

Vector Time (GMT): 2021/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3615360
94                 A    =         6803765
12  meter
 Y    =        5574728
18  meter          E    =           
0011520
 Z    =        1438815
49                 I    =           51
37473
 XDOT =      -4786
995376                 Wp   =          117
15173
 YDOT =      -1610
165569  meter/sec      RA   =          312
92805  deg
 ZDOT =      -5759
282546                 TA   =           47
13044
                                          MA   =           47
03374
                                          Ha   =            228
692  n
mi
                                          Hp   =            223
599

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11861420
41                 X    =        -3684419
26
 Y    =       18289790
61  feet           Y    =         5533912
38  meter
 Z    =        4720523
25                 Z    =         1421086
73
 XDOT =     -15705
365408                 XDOT =       -4740
659871
 YDOT =      -5282
695437  feet/sec       YDOT =       -1663
437717  meter/sec
 ZDOT =     -18895
283943                 ZDOT =       -5782
422700

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21763108
92                 X    =        -6633395
60
 Y    =        1532593
50  feet           Y    =          467134
50  meter
 Z    =        4638029
96                 Z    =         1413671
53
 XDOT =      -5059
175532                 XDOT =       -1542
036702
 YDOT =     -14025
832909  feet/sec       YDOT =       -4275
073871  meter/sec
 ZDOT =     -19002
586697                 ZDOT =       -5791
988425


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21028
53504738  
00016717  00000-0  10270-3 0  9038
2 25544  51
6449 313
4638 0002311 308
2628  51
8314 15
48887973 26948


Satellite: ISS
Catalog Number: 25544
Epoch time:      21028
53504738   =   yrday
fracday
Element set:     903
Inclination:       51
6449  deg
RA of node:       313
4638  deg
Eccentricity:     
0002311     
Arg of perigee:   308
2628  deg
Mean anomaly:      51
8314  deg
Mean motion:   15
48887973  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2694
Checksum:              320


Coasting Arc #5 (Orbit 2708)
---------------------------------------

Vector Time (GMT): 2021/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3087520
20                 A    =         6803696
17  meter
 Y    =       -5875022
60  meter          E    =           
0008922
 Z    =       -1475260
67                 I    =           51
35230
 XDOT =       4930
146031                 Wp   =           21
73428
 YDOT =       1152
567904  meter/sec      RA   =          307
96202  deg
 ZDOT =       5747
501182                 TA   =          322
13501
                                          MA   =          322
19773
                                          Ha   =            228
723  n
mi
                                          Hp   =            223
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10129659
44                 X    =         3160152
74
 Y    =      -19275008
55  feet           Y    =        -5840089
55  meter
 Z    =       -4840094
07                 Z    =        -1460087
10
 XDOT =      16175
019788                 XDOT =        4888
974156
 YDOT =       3781
390761  feet/sec       YDOT =        1207
469872  meter/sec
 ZDOT =      18856
631174                 ZDOT =        5771
349124

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21442563
72                 X    =         6535693
42
 Y    =       -3877001
71  feet           Y    =        -1181710
12  meter
 Z    =       -4769463
72                 Z    =        -1453732
54
 XDOT =       6627
892614                 XDOT =        2020
181669
 YDOT =      13402
681416  feet/sec       YDOT =        4085
137296  meter/sec
 ZDOT =      18967
238743                 ZDOT =        5781
214369


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   21029
50283874  
00016717  00000-0  10270-3 0  9042
2 25544  51
6448 308
6779 0002418 312
0134  48
0810 15
48893527 27090


Satellite: ISS
Catalog Number: 25544
Epoch time:      21029
50283874   =   yrday
fracday
Element set:     904
Inclination:       51
6448  deg
RA of node:       308
6779  deg
Eccentricity:     
0002418     
Arg of perigee:   312
0134  deg
Mean anomaly:      48
0810  deg
Mean motion:   15
48893527  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2709
Checksum:              316


Coasting Arc #6 (Orbit 2713)
---------------------------------------

Vector Time (GMT): 2021/029/19:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4262168
26                 A    =         6793201
71  meter
 Y    =       -1192300
10  meter          E    =           
0012665
 Z    =       -5164936
93                 I    =           51
30932
 XDOT =       3533
282953                 Wp   =           72
35533
 YDOT =      -6643
551424  meter/sec      RA   =          306
45874  deg
 ZDOT =      -1381
126369                 TA   =          184
26615
                                          MA   =          184
27696
                                          Ha   =            228
722  n
mi
                                          Hp   =            223
287

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13983491
66                 X    =        -4223431
40
 Y    =       -3911745
75  feet           Y    =        -1239745
94  meter
 Z    =      -16945331
12                 Z    =        -5185546
11
 XDOT =      11592
135674                 XDOT =        3614
019060
 YDOT =     -21796
428555  feet/sec       YDOT =       -6603
588230  meter/sec
 ZDOT =      -4531
254492                 ZDOT =       -1363
767841

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10521078
02                 X    =        -3206824
58
 Y    =        9843695
04  feet           Y    =         3000358
25  meter
 Z    =      -17040910
36                 Z    =        -5194069
48
 XDOT =     -11924
263864                 XDOT =       -3634
515626
 YDOT =     -20454
605728  feet/sec       YDOT =       -6234
563826  meter/sec
 ZDOT =      -4450
463670                 ZDOT =       -1356
501326


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   21029
82543508  
00016717  00000-0  10270-3 0  9051
2 25544  51
6430 307
0789 0002019 309
4993  50
5978 15
48910777 27141


Satellite: ISS
Catalog Number: 25544
Epoch time:      21029
82543508   =   yrday
fracday
Element set:     905
Inclination:       51
6430  deg
RA of node:       307
0789  deg
Eccentricity:     
0002019     
Arg of perigee:   309
4993  deg
Mean anomaly:      50
5978  deg
Mean motion:   15
48910777  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2714
Checksum:              326


Coasting Arc #7 (Orbit 2729)
---------------------------------------

Vector Time (GMT): 2021/030/19:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4355664
20                 A    =         6793286
12  meter
 Y    =         792668
21  meter          E    =           
0002411
 Z    =        5150882
67                 I    =           51
28901
 XDOT =      -2928
160618                 Wp   =          116
51871
 YDOT =       6938
605530  meter/sec      RA   =          301
49012  deg
 ZDOT =       1406
746758                 TA   =          319
86252
                                          MA   =          319
88032
                                          Ha   =            228
646  n
mi
                                          Hp   =            223
461

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14290236
86                 X    =         4321457
42
 Y    =        2600617
49  feet           Y    =          841185
05  meter
 Z    =       16899221
36                 Z    =         5171957
00
 XDOT =      -9606
826174                 XDOT =       -3012
365537
 YDOT =      22764
453839  feet/sec       YDOT =        6905
389888  meter/sec
 ZDOT =       4615
310887                 ZDOT =        1392
318973

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9370869
64                 X    =         2856241
07
 Y    =      -10947486
04  feet           Y    =        -3336793
74  meter
 Z    =       16996973
71                 Z    =         5180677
59
 XDOT =      14041
129979                 XDOT =        4279
736418
 YDOT =      19088
318786  feet/sec       YDOT =        5818
119566  meter/sec
 ZDOT =       4548
132021                 ZDOT =        1386
270640


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   21030
85774371  
00016717  00000-0  10270-3 0  9061
2 25544  51
6418 301
9726 0002080 314
2926  45
8053 15
48887705 27302


Satellite: ISS
Catalog Number: 25544
Epoch time:      21030
85774371   =   yrday
fracday
Element set:     906
Inclination:       51
6418  deg
RA of node:       301
9726  deg
Eccentricity:     
0002080     
Arg of perigee:   314
2926  deg
Mean anomaly:      45
8053  deg
Mean motion:   15
48887705  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2730
Checksum:              307


Coasting Arc #8 (Orbit 2744)
---------------------------------------

Vector Time (GMT): 2021/031/19:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4423619
23                 A    =         6793237
71  meter
 Y    =        -389150
10  meter          E    =           
0012859
 Z    =       -5152339
43                 I    =           51
27262
 XDOT =       2293
093740                 Wp   =           71
51068
 YDOT =      -7157
579804  meter/sec      RA   =          296
52256  deg
 ZDOT =      -1427
113005                 TA   =          184
64871
                                          MA   =          184
66066
                                          Ha   =            228
812  n
mi
                                          Hp   =            223
188

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14513186
45                 X    =        -4393912
51
 Y    =       -1276739
18  feet           Y    =         -438452
13  meter
 Z    =      -16904000
75                 Z    =        -5173754
83
 XDOT =       7523
273425                 XDOT =        2379
893443
 YDOT =     -23482
873374  feet/sec       YDOT =       -7131
451458  meter/sec
 ZDOT =      -4682
129282                 ZDOT =       -1415
763536

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8133940
93                 X    =        -2479225
20
 Y    =       11947094
65  feet           Y    =         3641474
45  meter
 Z    =      -17003347
30                 Z    =        -5182620
26
 XDOT =     -15948
918708                 XDOT =       -4861
230422
 YDOT =     -17451
838180  feet/sec       YDOT =       -5319
320277  meter/sec
 ZDOT =      -4629
250344                 ZDOT =       -1410
995505


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   21031
82553139  
00016717  00000-0  10270-3 0  9077
2 25544  51
6420 297
1878 0001981 317
4146  42
6850 15
48915752 27457


Satellite: ISS
Catalog Number: 25544
Epoch time:      21031
82553139   =   yrday
fracday
Element set:     907
Inclination:       51
6420  deg
RA of node:       297
1878  deg
Eccentricity:     
0001981     
Arg of perigee:   317
4146  deg
Mean anomaly:      42
6850  deg
Mean motion:   15
48915752  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2745
Checksum:              318


Coasting Arc #9 (Orbit 2760)
---------------------------------------

Vector Time (GMT): 2021/032/19:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4441123
16                 A    =         6793254
45  meter
 Y    =         -20914
66  meter          E    =           
0002509
 Z    =        5138683
29                 I    =           51
25858
 XDOT =      -1646
800328                 Wp   =          114
00440
 YDOT =       7340
309780  meter/sec      RA   =          291
55106  deg
 ZDOT =       1451
561585                 TA   =          321
92865
                                          MA   =          321
94638
                                          Ha   =            228
629  n
mi
                                          Hp   =            223
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14570614
05                 X    =         4416066
82
 Y    =         -68617
64  feet           Y    =           28609
18  meter
 Z    =       16859197
14                 Z    =         5160195
12
 XDOT =      -5402
888215                 XDOT =       -1735
810194
 YDOT =      24082
381167  feet/sec       YDOT =        7321
396411  meter/sec
 ZDOT =       4762
341157                 ZDOT =        1443
345965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6768741
60                 X    =         2063112
44
 Y    =      -12771706
08  feet           Y    =        -3892816
01  meter
 Z    =       16959000
31                 Z    =         5169103
29
 XDOT =      17726
523193                 XDOT =        5403
044269
 YDOT =      15674
298077  feet/sec       YDOT =        4777
526054  meter/sec
 ZDOT =       4724
019395                 ZDOT =        1439
881112


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   21032
85783720  
00016717  00000-0  10270-3 0  9083
2 25544  51
6419 292
0810 0002148 317
6673  42
4311 15
48915616 27615


Satellite: ISS
Catalog Number: 25544
Epoch time:      21032
85783720   =   yrday
fracday
Element set:     908
Inclination:       51
6419  deg
RA of node:       292
0810  deg
Eccentricity:     
0002148     
Arg of perigee:   317
6673  deg
Mean anomaly:      42
4311  deg
Mean motion:   15
48915616  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2761
Checksum:              302


Coasting Arc #10 (Orbit 2765)
---------------------------------------

Vector Time (GMT): 2021/033/03:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3815037
71                 A    =         6802279
92  meter
 Y    =        5139894
95  meter          E    =           
0003592
 Z    =       -2300159
13                 I    =           51
28601
 XDOT =      -2933
955355                 Wp   =          128
25800
 YDOT =      -4583
632558  meter/sec      RA   =          289
84413  deg
 ZDOT =      -5384
189068                 TA   =           77
42548
                                          MA   =           77
38531
                                          Ha   =            228
900  n
mi
                                          Hp   =            223
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12516527
92                 X    =        -3861057
45
 Y    =       16863172
41  feet           Y    =         5096975
09  meter
 Z    =       -7546453
85                 Z    =        -2318802
52
 XDOT =      -9625
837778                 XDOT =       -2856
329035
 YDOT =     -15038
164560  feet/sec       YDOT =       -4616
008228  meter/sec
 ZDOT =     -17664
662296                 ZDOT =       -5398
252110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10427966
85                 X    =         3178444
30
 Y    =      -18192649
94  feet           Y    =        -5545119
70  meter
 Z    =       -7633086
94                 Z    =        -2326564
90
 XDOT =       9854
923135                 XDOT =        3003
780571
 YDOT =      13076
891647  feet/sec       YDOT =        3985
836574  meter/sec
 ZDOT =     -17729
781638                 ZDOT =       -5404
037443


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   21033
18043158  
00016717  00000-0  10270-3 0  9095
2 25544  51
6435 290
4898 0002247 325
4287  34
6717 15
48902714 27662


Satellite: ISS
Catalog Number: 25544
Epoch time:      21033
18043158   =   yrday
fracday
Element set:     909
Inclination:       51
6435  deg
RA of node:       290
4898  deg
Eccentricity:     
0002247     
Arg of perigee:   325
4287  deg
Mean anomaly:      34
6717  deg
Mean motion:   15
48902714  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2766
Checksum:              321


Coasting Arc #11 (Orbit 2781)
---------------------------------------

Vector Time (GMT): 2021/034/03:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3335009
85                 A    =         6802324
99  meter
 Y    =       -5467860
86  meter          E    =           
0013617
 Z    =        2269613
20                 I    =           51
27553
 XDOT =       3342
060755                 Wp   =           62
32070
 YDOT =       4288
005774  meter/sec      RA   =          284
87213  deg
 ZDOT =       5400
838906                 TA   =          323
02864
                                          MA   =          323
12241
                                          Ha   =            228
946  n
mi
                                          Hp   =            223
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10941633
35                 X    =         3384881
00
 Y    =      -17939176
05  feet           Y    =        -5430287
50  meter
 Z    =        7446237
54                 Z    =         2285934
26
 XDOT =      10964
766256                 XDOT =        3267
628900
 YDOT =      14068
260413  feet/sec       YDOT =        4324
963005  meter/sec
 ZDOT =      17719
287749                 ZDOT =        5416
892178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8410316
09                 X    =        -2563464
34
 Y    =       19226663
12  feet           Y    =         5860286
92  meter
 Z    =        7522090
12                 Z    =         2292733
07
 XDOT =     -11213
682130                 XDOT =       -3417
930313
 YDOT =     -11890
499597  feet/sec       YDOT =       -3624
224277  meter/sec
 ZDOT =      17793
657658                 ZDOT =        5423
506854


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   21034
21273458  
00016717  00000-0  10270-3 0  9100
2 25544  51
6432 285
3840 0002365 333
2574  26
8454 15
48911590 27827


Satellite: ISS
Catalog Number: 25544
Epoch time:      21034
21273458   =   yrday
fracday
Element set:     910
Inclination:       51
6432  deg
RA of node:       285
3840  deg
Eccentricity:     
0002365     
Arg of perigee:   333
2574  deg
Mean anomaly:      26
8454  deg
Mean motion:   15
48911590  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2782
Checksum:              301


Coasting Arc #12 (Orbit 2796)
---------------------------------------

Vector Time (GMT): 2021/035/03:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2848626
96                 A    =         6802373
29  meter
 Y    =        5745747
78  meter          E    =           
0003841
 Z    =       -2266996
48                 I    =           51
26689
 XDOT =      -3705
088888                 Wp   =          122
89632
 YDOT =      -3964
095781  meter/sec      RA   =          279
89990  deg
 ZDOT =      -5400
141093                 TA   =           82
39669
                                          MA   =           82
35307
                                          Ha   =            229
087  n
mi
                                          Hp   =            223
166

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9345888
99                 X    =        -2901654
36
 Y    =       18850878
53  feet           Y    =         5713595
89  meter
 Z    =       -7437652
49                 Z    =        -2280962
54
 XDOT =     -12155
803438                 XDOT =       -3634
255426
 YDOT =     -13005
563587  feet/sec       YDOT =       -4005
132682  meter/sec
 ZDOT =     -17716
998336                 ZDOT =       -5417
966644

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6364072
26                 X    =         1939769
23
 Y    =      -20030724
14  feet           Y    =        -6105364
72  meter
 Z    =       -7502573
68                 Z    =        -2286784
46
 XDOT =      12386
547333                 XDOT =        3775
419627
 YDOT =      10591
647910  feet/sec       YDOT =        3228
334283  meter/sec
 ZDOT =     -17799
606874                 ZDOT =       -5425
320175


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   21035
18051809  
00016717  00000-0  10270-3 0  9112
2 25544  51
6420 280
5977 0002305 337
3651  22
7397 15
48897154 27973


Satellite: ISS
Catalog Number: 25544
Epoch time:      21035
18051809   =   yrday
fracday
Element set:     911
Inclination:       51
6420  deg
RA of node:       280
5977  deg
Eccentricity:     
0002305     
Arg of perigee:   337
3651  deg
Mean anomaly:      22
7397  deg
Mean motion:   15
48897154  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2797
Checksum:              319


Coasting Arc #13 (Orbit 2812)
---------------------------------------

Vector Time (GMT): 2021/036/03:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2316846
33                 A    =         6802347
80  meter
 Y    =       -5983226
87  meter          E    =           
0013837
 Z    =        2236650
18                 I    =           51
26175
 XDOT =       4051
519613                 Wp   =           61
75453
 YDOT =       3601
071890  meter/sec      RA   =          274
92755  deg
 ZDOT =       5417
108407                 TA   =          323
20681
                                          MA   =          323
30170
                                          Ha   =            228
992  n
mi
                                          Hp   =            223
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7601201
86                 X    =         2372716
21
 Y    =      -19630009
42  feet           Y    =        -5957005
90  meter
 Z    =        7338091
14                 Z    =         2248039
87
 XDOT =      13292
387182                 XDOT =        3984
637421
 YDOT =      11814
540320  feet/sec       YDOT =        3646
004796  meter/sec
 ZDOT =      17772
665378                 ZDOT =        5436
626443

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4169049
69                 X    =        -1270726
34
 Y    =       20614423
69  feet           Y    =         6283276
34  meter
 Z    =        7391054
17                 Z    =         2252793
31
 XDOT =     -13453
599259                 XDOT =       -4100
657054
 YDOT =      -9147
971760  feet/sec       YDOT =       -2788
301793  meter/sec
 ZDOT =      17863
143407                 ZDOT =        5444
686110


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
21281881  
00016717  00000-0  10270-3 0  9123
2 25544  51
6413 275
4926 0002400 337
4692  22
6352 15
48929986 28132


Satellite: ISS
Catalog Number: 25544
Epoch time:      21036
21281881   =   yrday
fracday
Element set:     912
Inclination:       51
6413  deg
RA of node:       275
4926  deg
Eccentricity:     
0002400     
Arg of perigee:   337
4692  deg
Mean anomaly:      22
6352  deg
Mean motion:   15
48929986  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2813
Checksum:              309


Coasting Arc #14 (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    =        4174550
88                 A    =         6793569
16  meter
 Y    =       -1692090
77  meter          E    =           
0003260
 Z    =        5082812
26                 I    =           51
23339
 XDOT =        964
303781                 Wp   =           97
39240
 YDOT =       7414
374047  meter/sec      RA   =          272
95377  deg
 ZDOT =       1674
948119                 TA   =          336
31816
                                          MA   =          336
33316
                                          Ha   =            228
984  n
mi
                                          Hp   =            223
228

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13696033
06                 X    =         4168473
11
 Y    =       -5551478
91  feet           Y    =        -1645442
10  meter
 Z    =       16675893
25                 Z    =         5103075
44
 XDOT =       3163
726314                 XDOT =         873
186514
 YDOT =      24325
374169  feet/sec       YDOT =        7424
648058  meter/sec
 ZDOT =       5495
236611                 ZDOT =        1679
411212

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14609469
43                 X    =         4452966
28
 Y    =        1348439
23  feet           Y    =          411004
28  meter
 Z    =       16769936
50                 Z    =         5111476
64
 XDOT =      -8362
880983                 XDOT =       -2549
006124
 YDOT =      21954
532647  feet/sec       YDOT =        6691
741551  meter/sec
 ZDOT =       5515
797781                 ZDOT =        1681
215164


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
59993312  
00016717  00000-0  10270-3 0  9134
2 25544  51
6435 273
5786 0002689 339
0188  21
0851 15
48892824 28199


Satellite: ISS
Catalog Number: 25544
Epoch time:      21036
59993312   =   yrday
fracday
Element set:     913
Inclination:       51
6435  deg
RA of node:       273
5786  deg
Eccentricity:     
0002689     
Arg of perigee:   339
0188  deg
Mean anomaly:      21
0851  deg
Mean motion:   15
48892824  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2819
Checksum:              337


Coasting Arc #15 (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    =       -4014022
52                 A    =         6793508
37  meter
 Y    =        2071856
12  meter          E    =           
0013247
 Z    =       -5086044
64                 I    =           51
23232
 XDOT =      -1615
275658                 Wp   =           65
17776
 YDOT =      -7283
800015  meter/sec      RA   =          267
97984  deg
 ZDOT =      -1690
353094                 TA   =          188
34789
                                          MA   =          188
36995
                                          Ha   =            229
109  n
mi
                                          Hp   =            223
009

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13169365
21                 X    =        -4012187
70
 Y    =        6797428
23  feet           Y    =         2026978
97  meter
 Z    =      -16686498
17                 Z    =        -5105538
24
 XDOT =      -5299
460820                 XDOT =       -1525
495327
 YDOT =     -23896
981677  feet/sec       YDOT =       -7301
361105  meter/sec
 ZDOT =      -5545
777868                 ZDOT =       -1697
981658

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14715479
42                 X    =        -4485278
13
 Y    =         253105
05  feet           Y    =           77146
42  meter
 Z    =      -16776979
31                 Z    =        -5113623
29
 XDOT =       5980
494546                 XDOT =        1822
854738
 YDOT =     -22659
012102  feet/sec       YDOT =       -6906
466889  meter/sec
 ZDOT =      -5581
045461                 ZDOT =       -1701
102657


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
56771258  
00016717  00000-0  10270-3 0  9146
2 25544  51
6429 268
7911 0002783 339
6457  20
4581 15
48925811 28341


Satellite: ISS
Catalog Number: 25544
Epoch time:      21037
56771258   =   yrday
fracday
Element set:     914
Inclination:       51
6429  deg
RA of node:       268
7911  deg
Eccentricity:     
0002783     
Arg of perigee:   339
6457  deg
Mean anomaly:      20
4581  deg
Mean motion:   15
48925811  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2834
Checksum:              331


Coasting Arc #16 (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    =        3807304
59                 A    =         6793626
03  meter
 Y    =       -2425700
14  meter          E    =           
0003661
 Z    =        5073684
85                 I    =           51
23460
 XDOT =       2256
475826                 Wp   =           94
62220
 YDOT =       7120
291828  meter/sec      RA   =          263
00703  deg
 ZDOT =       1709
546124                 TA   =          338
74322
                                          MA   =          338
75842
                                          Ha   =            229
137  n
mi
                                          Hp   =            223
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12491156
81                 X    =         3809502
09
 Y    =       -7958333
80  feet           Y    =        -2383112
15  meter
 Z    =       16645947
67                 Z    =         5092183
98
 XDOT =       7403
135913                 XDOT =        2168
383051
 YDOT =      23360
537492  feet/sec       YDOT =        7145
032699  meter/sec
 ZDOT =       5608
747125                 ZDOT =        1720
293431

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14597614
08                 X    =         4449352
77
 Y    =       -1845927
84  feet           Y    =         -562638
80  meter
 Z    =       16731821
86                 Z    =         5099859
30
 XDOT =      -3558
528273                 XDOT =       -1084
639418
 YDOT =      23189
127320  feet/sec       YDOT =        7068
046007  meter/sec
 ZDOT =       5658
509066                 ZDOT =        1724
713563


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
60001135  
00016717  00000-0  10270-3 0  9153
2 25544  51
6426 263
6854 0002765 346
6896  13
4180 15
48890149 28503


Satellite: ISS
Catalog Number: 25544
Epoch time:      21038
60001135   =   yrday
fracday
Element set:     915
Inclination:       51
6426  deg
RA of node:       263
6854  deg
Eccentricity:     
0002765     
Arg of perigee:   346
6896  deg
Mean anomaly:      13
4180  deg
Mean motion:   15
48890149  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2850
Checksum:              310


Coasting Arc #17 (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    =       -3580843
37                 A    =         6793574
78  meter
 Y    =        2769441
91  meter          E    =           
0013606
 Z    =       -5077887
53                 I    =           51
23778
 XDOT =      -2872
106602                 Wp   =           65
46390
 YDOT =      -6877
183641  meter/sec      RA   =          258
03428  deg
 ZDOT =      -1723
523819                 TA   =          187
73032
                                          MA   =          187
75131
                                          Ha   =            229
271  n
mi
                                          Hp   =            222
866

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11748173
78                 X    =        -3586881
24
 Y    =        9086095
52  feet           Y    =         2729364
89  meter
 Z    =      -16659736
00                 Z    =        -5095295
85
 XDOT =      -9422
921921                 XDOT =       -2786
618730
 YDOT =     -22562
938456  feet/sec       YDOT =       -6908
823508  meter/sec
 ZDOT =      -5654
605705                 ZDOT =       -1737
267770

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14356309
95                 X    =        -4375803
27
 Y    =        3431290
08  feet           Y    =         1045857
22  meter
 Z    =      -16740553
63                 Z    =        -5102520
75
 XDOT =       1088
174206                 XDOT =         331
675498
 YDOT =     -23375
469048  feet/sec       YDOT =       -7124
842966  meter/sec
 ZDOT =      -5718
301309                 ZDOT =       -1742
938239


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
56778870  
00016717  00000-0  10270-3 0  9167
2 25544  51
6403 258
8988 0002721 348
7116  11
3972 15
48919824 28656


Satellite: ISS
Catalog Number: 25544
Epoch time:      21039
56778870   =   yrday
fracday
Element set:     916
Inclination:       51
6403  deg
RA of node:       258
8988  deg
Eccentricity:     
0002721     
Arg of perigee:   348
7116  deg
Mean anomaly:      11
3972  deg
Mean motion:   15
48919824  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2865
Checksum:              347


Coasting Arc #18 (Orbit 2875)
---------------------------------------

Vector Time (GMT): 2021/040/05:21:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942685
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2374706
02                 A    =         6796284
74  meter
 Y    =       -4620953
24  meter          E    =           
0008510
 Z    =        4374356
40                 I    =           51
25320
 XDOT =       4278
263337                 Wp   =           93
54889
 YDOT =       5392
745258  meter/sec      RA   =          254
69245  deg
 ZDOT =       3367
999579                 TA   =          322
12270
                                          MA   =          322
18254
                                          Ha   =            229
152  n
mi
                                          Hp   =            222
918

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7791030
24                 X    =         2404955
01
 Y    =      -15160607
74  feet           Y    =        -4594228
67  meter
 Z    =       14351562
98                 Z    =         4385964
64
 XDOT =      14036
297037                 XDOT =        4201
282766
 YDOT =      17692
733787  feet/sec       YDOT =        5440
157277  meter/sec
 ZDOT =      11049
867385                 ZDOT =        3388
594353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3524149
99                 X    =         1074160
92
 Y    =       16630514
40  feet           Y    =         5068980
79  meter
 Z    =       14405481
50                 Z    =         4390790
76
 XDOT =     -20759
372686                 XDOT =       -6327
456795
 YDOT =      -5272
722207  feet/sec       YDOT =       -1607
125729  meter/sec
 ZDOT =      11145
390123                 ZDOT =        3397
114909


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
27749262  
00016717  00000-0  10270-3 0  9171
2 25544  51
6411 255
3900 0002640 351
0563   9
0540 15
48952279 28762


Satellite: ISS
Catalog Number: 25544
Epoch time:      21040
27749262   =   yrday
fracday
Element set:     917
Inclination:       51
6411  deg
RA of node:       255
3900  deg
Eccentricity:     
0002640     
Arg of perigee:   351
0563  deg
Mean anomaly:       9
0540  deg
Mean motion:   15
48952279  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2876
Checksum:              297
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