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

 
Date: February 1st 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) : 16490 3108 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


033/03:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 9
000/00:00:00 000 0 0 0 0 223 1

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

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

040/13:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 222 9

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

Coasting Arc #1 (Orbit 2756)
---------------------------------------

Vector Time (GMT): 2021/032/13:47:11
137
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4512850
53                 A    =         6799730
79  meter
 Y    =        3836711
19  meter          E    =           
0003660
 Z    =       -3343922
96                 I    =           51
28550
 XDOT =      -1566
610689                 Wp   =           59
81585
 YDOT =      -5883
327833  meter/sec      RA   =          292
72484  deg
 ZDOT =      -4638
117531                 TA   =          159
23740
                                          MA   =          159
22253
                                          Ha   =            228
802  n
mi
                                          Hp   =            223
357

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14805940
06                 X    =        -4539175
97
 Y    =       12587635
15  feet           Y    =         3786098
00  meter
 Z    =      -10970875
86                 Z    =        -3365908
03
 XDOT =      -5139
798850                 XDOT =       -1478
176372
 YDOT =     -19302
256670  feet/sec       YDOT =       -5900
352410  meter/sec
 ZDOT =     -15216
921034                 ZDOT =       -4645
512429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18386106
38                 X    =        -5604085
23
 Y    =        6112661
66  feet           Y    =         1863139
28  meter
 Z    =      -11072984
97                 Z    =        -3375045
82
 XDOT =       3051
317793                 XDOT =         930
041663
 YDOT =     -18437
167473  feet/sec       YDOT =       -5619
648646  meter/sec
 ZDOT =     -15251
060269                 ZDOT =       -4648
523170


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
59968327  
00016717  00000-0  10270-3 0  9004
2 25544  51
6443 293
3630 0002566 321
3854  38
7112 15
48915271 27572


Satellite: ISS
Catalog Number: 25544
Epoch time:      21032
59968327   =   yrday
fracday
Element set:     900
Inclination:       51
6443  deg
RA of node:       293
3630  deg
Eccentricity:     
0002566     
Arg of perigee:   321
3854  deg
Mean anomaly:      38
7112  deg
Mean motion:   15
48915271  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2757
Checksum:              310


Coasting Arc #2 (Orbit 2765)
---------------------------------------

Vector Time (GMT): 2021/033/03:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4604140
14                 A    =         6796364
00  meter
 Y    =        2468899
20  meter          E    =           
0008652
 Z    =       -4356254
45                 I    =           51
26654
 XDOT =       -441
495700                 Wp   =           54
76991
 YDOT =      -6836
580054  meter/sec      RA   =          289
82125  deg
 ZDOT =      -3407
926358                 TA   =          180
41266
                                          MA   =          180
41337
                                          Ha   =            228
885  n
mi
                                          Hp   =            223
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15105446
66                 X    =        -4610246
25
 Y    =        8100063
00  feet           Y    =         2417378
16  meter
 Z    =      -14292173
40                 Z    =        -4378633
91
 XDOT =      -1448
476707                 XDOT =        -348
460802
 YDOT =     -22429
724587  feet/sec       YDOT =       -6840
997051  meter/sec
 ZDOT =     -11180
860754                 ZDOT =       -3409
844830

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13639568
14                 X    =         4157340
37
 Y    =      -10235584
70  feet           Y    =        -3119806
22  meter
 Z    =      -14396067
06                 Z    =        -4387921
24
 XDOT =       3936
724228                 XDOT =        1199
913545
 YDOT =      20984
106316  feet/sec       YDOT =        6395
955605  meter/sec
 ZDOT =     -11189
575906                 ZDOT =       -3410
582736


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
18034602  
00016717  00000-0  10270-3 0  9011
2 25544  51
6436 290
4895 0002225 327
4178  32
6834 15
48937842 27665


Satellite: ISS
Catalog Number: 25544
Epoch time:      21033
18034602   =   yrday
fracday
Element set:     901
Inclination:       51
6436  deg
RA of node:       290
4895  deg
Eccentricity:     
0002225     
Arg of perigee:   327
4178  deg
Mean anomaly:      32
6834  deg
Mean motion:   15
48937842  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2766
Checksum:              310


Coasting Arc #3 (Orbit 2781)
---------------------------------------

Vector Time (GMT): 2021/034/03:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4364447
82                 A    =         6796450
09  meter
 Y    =       -2872553
05  meter          E    =           
0008112
 Z    =        4340015
97                 I    =           51
25534
 XDOT =       1046
925234                 Wp   =           96
63467
 YDOT =       6774
597138  meter/sec      RA   =          284
84859  deg
 ZDOT =       3424
666878                 TA   =          318
37391
                                          MA   =          318
43563
                                          Ha   =            228
887  n
mi
                                          Hp   =            223
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14319054
54                 X    =         4375164
31
 Y    =       -9424386
65  feet           Y    =        -2823686
67  meter
 Z    =       14238897
52                 Z    =         4361242
40
 XDOT =       3434
794075                 XDOT =         954
457061
 YDOT =      22226
368562  feet/sec       YDOT =        6785
787634  meter/sec
 ZDOT =      11235
783721                 ZDOT =        3429
527657

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12467372
78                 X    =        -3800055
22
 Y    =       11644866
53  feet           Y    =         3549355
32  meter
 Z    =       14337443
59                 Z    =         4370052
81
 XDOT =      -6136
283958                 XDOT =       -1870
339350
 YDOT =     -20456
945062  feet/sec       YDOT =       -6235
276855  meter/sec
 ZDOT =      11258
167449                 ZDOT =        3431
489438


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
21263364  
00016717  00000-0  10270-3 0  9026
2 25544  51
6426 285
3829 0002324 335
6125  24
4915 15
48922530 27822


Satellite: ISS
Catalog Number: 25544
Epoch time:      21034
21263364   =   yrday
fracday
Element set:     902
Inclination:       51
6426  deg
RA of node:       285
3829  deg
Eccentricity:     
0002324     
Arg of perigee:   335
6125  deg
Mean anomaly:      24
4915  deg
Mean motion:   15
48922530  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2782
Checksum:              292


Coasting Arc #4 (Orbit 2796)
---------------------------------------

Vector Time (GMT): 2021/035/03:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4104746
91                 A    =         6796427
09  meter
 Y    =        3249308
79  meter          E    =           
0009027
 Z    =       -4343719
22                 I    =           51
24716
 XDOT =      -1634
125415                 Wp   =           54
31664
 YDOT =      -6643
693954  meter/sec      RA   =          279
87677  deg
 ZDOT =      -3425
453947                 TA   =          180
64791
                                          MA   =          180
64908
                                          Ha   =            229
054  n
mi
                                          Hp   =            223
002

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13467017
41                 X    =        -4119677
64
 Y    =       10660461
91  feet           Y    =         3203323
08  meter
 Z    =      -14251047
29                 Z    =        -4363694
39
 XDOT =      -5361
303854                 XDOT =       -1543
073528
 YDOT =     -21796
896175  feet/sec       YDOT =       -6661
458807  meter/sec
 ZDOT =     -11238
365969                 ZDOT =       -3433
170638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11202120
71                 X    =         3414406
39
 Y    =      -12917682
58  feet           Y    =        -3937309
65  meter
 Z    =      -14343790
42                 Z    =        -4371987
32
 XDOT =       8225
874698                 XDOT =        2507
246608
 YDOT =      19652
526550  feet/sec       YDOT =        5990
090092  meter/sec
 ZDOT =     -11274
016807                 ZDOT =       -3436
320323


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
18040081  
00016717  00000-0  10270-3 0  9033
2 25544  51
6419 280
5971 0002356 338
6743  21
4308 15
48936609 27974


Satellite: ISS
Catalog Number: 25544
Epoch time:      21035
18040081   =   yrday
fracday
Element set:     903
Inclination:       51
6419  deg
RA of node:       280
5971  deg
Eccentricity:     
0002356     
Arg of perigee:   338
6743  deg
Mean anomaly:      21
4308  deg
Mean motion:   15
48936609  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2797
Checksum:              311


Coasting Arc #5 (Orbit 2812)
---------------------------------------

Vector Time (GMT): 2021/036/03:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3796748
78                 A    =         6796486
92  meter
 Y    =       -3603485
70  meter          E    =           
0008266
 Z    =        4328211
41                 I    =           51
24153
 XDOT =       2217
373182                 Wp   =           94
91544
 YDOT =       6477
732682  meter/sec      RA   =          274
90387  deg
 ZDOT =       3441
584906                 TA   =          319
88847
                                          MA   =          319
94947
                                          Ha   =            228
956  n
mi
                                          Hp   =            223
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12456524
87                 X    =         3815738
24
 Y    =      -11822459
65  feet           Y    =        -3560921
66  meter
 Z    =       14200168
66                 Z    =         4346700
26
 XDOT =       7274
846399                 XDOT =        2128
055417
 YDOT =      21252
403812  feet/sec       YDOT =        6502
029448  meter/sec
 ZDOT =      11291
289061                 ZDOT =        3452
139104

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9756979
97                 X    =        -2973927
49
 Y    =       14046044
30  feet           Y    =         4281234
30  meter
 Z    =       14286018
88                 Z    =         4354378
56
 XDOT =     -10260
729711                 XDOT =       -3127
470416
 YDOT =     -18682
633877  feet/sec       YDOT =       -5694
466806  meter/sec
 ZDOT =      11340
121966                 ZDOT =        3456
469175


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
21268579  
00016717  00000-0  10270-3 0  9043
2 25544  51
6407 275
4913 0002477 339
7158  20
3893 15
48929522 28138


Satellite: ISS
Catalog Number: 25544
Epoch time:      21036
21268579   =   yrday
fracday
Element set:     904
Inclination:       51
6407  deg
RA of node:       275
4913  deg
Eccentricity:     
0002477     
Arg of perigee:   339
7158  deg
Mean anomaly:      20
3893  deg
Mean motion:   15
48929522  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2813
Checksum:              325


Coasting Arc #6 (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    =        4185744
95                 A    =         6793404
52  meter
 Y    =       -1602376
14  meter          E    =           
0003126
 Z    =        5102494
64                 I    =           51
23290
 XDOT =        900
328573                 Wp   =           96
08053
 YDOT =       7439
693248  meter/sec      RA   =          272
95138  deg
 ZDOT =       1596
603080                 TA   =          338
41213
                                          MA   =          338
42531
                                          Ha   =            228
950  n
mi
                                          Hp   =            223
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13732759
03                 X    =         4178567
53
 Y    =       -5257139
57  feet           Y    =        -1555608
44  meter
 Z    =       16740467
98                 Z    =         5122809
53
 XDOT =       2953
833901                 XDOT =         809
313483
 YDOT =      24408
442416  feet/sec       YDOT =        7449
252417  meter/sec
 ZDOT =       5238
199080                 ZDOT =        1600
755660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14505720
12                 X    =         4421343
49
 Y    =        1626269
60  feet           Y    =          495686
97  meter
 Z    =       16834749
37                 Z    =         5131231
61
 XDOT =      -8565
575574                 XDOT =       -2610
787435
 YDOT =      21939
656446  feet/sec       YDOT =        6687
207285  meter/sec
 ZDOT =       5257
319155                 ZDOT =        1602
430879


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
59979236  
00016717  00000-0  10270-3 0  9054
2 25544  51
6435 273
5777 0002668 339
6273  20
4771 15
48919771 28192


Satellite: ISS
Catalog Number: 25544
Epoch time:      21036
59979236   =   yrday
fracday
Element set:     905
Inclination:       51
6435  deg
RA of node:       273
5777  deg
Eccentricity:     
0002668     
Arg of perigee:   339
6273  deg
Mean anomaly:      20
4771  deg
Mean motion:   15
48919771  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2819
Checksum:              350


Coasting Arc #7 (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    =       -4035469
44                 A    =         6793328
36  meter
 Y    =        1972585
64  meter          E    =           
0013397
 Z    =       -5108386
75                 I    =           51
23179
 XDOT =      -1546
287441                 Wp   =           66
02456
 YDOT =      -7318
532725  meter/sec      RA   =          267
97713  deg
 ZDOT =      -1602
514687                 TA   =          188
37868
                                          MA   =          188
40107
                                          Ha   =            229
074  n
mi
                                          Hp   =            222
948

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13239729
15                 X    =        -4032414
44
 Y    =        6471737
65  feet           Y    =         1927475
47  meter
 Z    =      -16759799
06                 Z    =        -5127981
57
 XDOT =      -5073
121525                 XDOT =       -1456
550505
 YDOT =     -24010
934136  feet/sec       YDOT =       -7335
322586  meter/sec
 ZDOT =      -5257
594116                 ZDOT =       -1609
808246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14632571
09                 X    =        -4460007
67
 Y    =         -69513
65  feet           Y    =          -21187
76  meter
 Z    =      -16850748
11                 Z    =        -5136108
02
 XDOT =       6208
589238                 XDOT =        1892
378000
 YDOT =     -22666
840893  feet/sec       YDOT =       -6908
853104  meter/sec
 ZDOT =      -5291
306787                 ZDOT =       -1612
790309


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
56755488  
00016717  00000-0  10270-3 0  9064
2 25544  51
6428 268
7901 0002762 340
3151  19
7892 15
48954194 28348


Satellite: ISS
Catalog Number: 25544
Epoch time:      21037
56755488   =   yrday
fracday
Element set:     906
Inclination:       51
6428  deg
RA of node:       268
7901  deg
Eccentricity:     
0002762     
Arg of perigee:   340
3151  deg
Mean anomaly:      19
7892  deg
Mean motion:   15
48954194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2834
Checksum:              336


Coasting Arc #8 (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    =        3840874
99                 A    =         6793431
65  meter
 Y    =       -2317419
09  meter          E    =           
0003484
 Z    =        5098776
46                 I    =           51
23402
 XDOT =       2183
044756                 Wp   =           93
12794
 YDOT =       7165
962012  meter/sec      RA   =          263
00404  deg
 ZDOT =       1611
347446                 TA   =          341
21894
                                          MA   =          341
23179
                                          Ha   =            229
098  n
mi
                                          Hp   =            223
046

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12601295
91                 X    =         3841737
28
 Y    =       -7603080
99  feet           Y    =        -2274463
16  meter
 Z    =       16728269
23                 Z    =         5117435
43
 XDOT =       7162
220329                 XDOT =        2094
923721
 YDOT =      23510
374054  feet/sec       YDOT =        7189
881572  meter/sec
 ZDOT =       5286
572984                 ZDOT =        1621
737996

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14543359
07                 X    =         4432815
85
 Y    =       -1478138
24  feet           Y    =         -450536
54  meter
 Z    =       16814883
44                 Z    =         5125176
47
 XDOT =      -3811
668841                 XDOT =       -1161
796663
 YDOT =      23225
391146  feet/sec       YDOT =        7079
099221  meter/sec
 ZDOT =       5334
678867                 ZDOT =        1626
010119


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
59983488  
00016717  00000-0  10270-3 0  9072
2 25544  51
6425 263
6843 0002743 347
2756  12
8325 15
48919104 28505


Satellite: ISS
Catalog Number: 25544
Epoch time:      21038
59983488   =   yrday
fracday
Element set:     907
Inclination:       51
6425  deg
RA of node:       263
6843  deg
Eccentricity:     
0002743     
Arg of perigee:   347
2756  deg
Mean anomaly:      12
8325  deg
Mean motion:   15
48919104  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2850
Checksum:              331


Coasting Arc #9 (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    =       -3628353
84                 A    =         6793365
74  meter
 Y    =        2653516
65  meter          E    =           
0013781
 Z    =       -5105860
61                 I    =           51
23716
 XDOT =      -2795
853930                 Wp   =           66
45341
 YDOT =      -6934
642920  meter/sec      RA   =          258
03095  deg
 ZDOT =      -1615
215942                 TA   =          187
82410
                                          MA   =          187
84561
                                          Ha   =            229
231  n
mi
                                          Hp   =            222
806

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11904048
04                 X    =        -3632955
99
 Y    =        8705763
29  feet           Y    =         2612916
36  meter
 Z    =      -16751511
19                 Z    =        -5123496
23
 XDOT =      -9172
749114                 XDOT =       -2710
255281
 YDOT =     -22751
453151  feet/sec       YDOT =       -6965
429462  meter/sec
 ZDOT =      -5299
264902                 ZDOT =       -1628
589233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14339511
72                 X    =        -4370683
17
 Y    =        3020835
76  feet           Y    =          920750
74  meter
 Z    =      -16833382
20                 Z    =        -5130814
90
 XDOT =       1361
887016                 XDOT =         415
103162
 YDOT =     -23445
242632  feet/sec       YDOT =       -7146
109954  meter/sec
 ZDOT =      -5361
239757                 ZDOT =       -1634
105878


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
56759404  
00016717  00000-0  10270-3 0  9080
2 25544  51
6403 258
8975 0002701 349
2936  10
8156 15
48949652 28656


Satellite: ISS
Catalog Number: 25544
Epoch time:      21039
56759404   =   yrday
fracday
Element set:     908
Inclination:       51
6403  deg
RA of node:       258
8975  deg
Eccentricity:     
0002701     
Arg of perigee:   349
2936  deg
Mean anomaly:      10
8156  deg
Mean motion:   15
48949652  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2865
Checksum:              340


Coasting Arc #10 (Orbit 2875)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2575988
00                 A    =         6795597
39  meter
 Y    =       -4355967
29  meter          E    =           
0007691
 Z    =        4529177
95                 I    =           51
25104
 XDOT =       4127
757724                 Wp   =           96
04813
 YDOT =       5665
922265  meter/sec      RA   =          254
68692  deg
 ZDOT =       3096
210700                 TA   =          322
72357
                                          MA   =          322
77692
                                          Ha   =            229
092  n
mi
                                          Hp   =            222
864

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8451404
20                 X    =         2602506
87
 Y    =      -14291231
27  feet           Y    =        -4327012
70  meter
 Z    =       14859507
70                 Z    =         4541754
86
 XDOT =      13542
512219                 XDOT =        4049
053742
 YDOT =      18588
983809  feet/sec       YDOT =        5711
641600  meter/sec
 ZDOT =      10158
171587                 ZDOT =        3116
070229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2502945
80                 X    =          762897
88
 Y    =       16360362
11  feet           Y    =         4986638
37  meter
 Z    =       14917919
00                 Z    =         4546981
71
 XDOT =     -20974
905209                 XDOT =       -6393
151108
 YDOT =      -6153
566768  feet/sec       YDOT =       -1875
607151  meter/sec
 ZDOT =      10250
279448                 ZDOT =        3124
285176


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
27728412  
00016717  00000-0  10270-3 0  9096
2 25544  51
6411 255
3886 0002630 351
2109   8
8994 15
48985577 28769


Satellite: ISS
Catalog Number: 25544
Epoch time:      21040
27728412   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:       255
3886  deg
Eccentricity:     
0002630     
Arg of perigee:   351
2109  deg
Mean anomaly:       8
8994  deg
Mean motion:   15
48985577  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2876
Checksum:              329


Coasting Arc #11 (Orbit 2880)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4067106
64                 A    =         6799814
02  meter
 Y    =        4365978
32  meter          E    =           
0012266
 Z    =        3252906
45                 I    =           51
26769
 XDOT =      -2236
102857                 Wp   =           79
92204
 YDOT =       5608
713740  meter/sec      RA   =          252
95918  deg
 ZDOT =      -4714
732464                 TA   =           62
22768
                                          MA   =           62
10337
                                          Ha   =            229
127  n
mi
                                          Hp   =            222
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13343525
72                 X    =         4002182
44
 Y    =       14324075
85  feet           Y    =         4411096
47  meter
 Z    =       10672265
26                 Z    =         3272504
72
 XDOT =      -7336
295462                 XDOT =       -2275
754321
 YDOT =      18401
291798  feet/sec       YDOT =        5583
486545  meter/sec
 ZDOT =     -15468
282363                 ZDOT =       -4725
690245

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7828788
29                 X    =         2386214
67
 Y    =       17888266
20  feet           Y    =         5452343
54  meter
 Z    =       10763181
66                 Z    =         3280617
77
 XDOT =     -11567
796238                 XDOT =       -3525
864293
 YDOT =      14434
350355  feet/sec       YDOT =        4399
589988  meter/sec
 ZDOT =     -15519
187469                 ZDOT =       -4730
248341


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
59986891  
00016717  00000-0  10270-3 0  9100
2 25544  51
6405 253
7910 0002762 348
1981  11
9104 15
48976673 28812


Satellite: ISS
Catalog Number: 25544
Epoch time:      21040
59986891   =   yrday
fracday
Element set:     910
Inclination:       51
6405  deg
RA of node:       253
7910  deg
Eccentricity:     
0002762     
Arg of perigee:   348
1981  deg
Mean anomaly:      11
9104  deg
Mean motion:   15
48976673  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2881
Checksum:              326


Coasting Arc #12 (Orbit 2895)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4438581
70                 A    =         6799808
18  meter
 Y    =       -3979208
24  meter          E    =           
0005393
 Z    =       -3272003
38                 I    =           51
27768
 XDOT =       1727
892652                 Wp   =           56
23111
 YDOT =      -5788
177238  meter/sec      RA   =          247
98629  deg
 ZDOT =       4703
835607                 TA   =          265
69054
                                          MA   =          265
75216
                                          Ha   =            229
253  n
mi
                                          Hp   =            222
746

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14562275
92                 X    =        -4377862
16
 Y    =      -13055145
15  feet           Y    =        -4028504
07  meter
 Z    =      -10734919
21                 Z    =        -3293416
11
 XDOT =       5668
939147                 XDOT =        1769
641699
 YDOT =     -18990
082803  feet/sec       YDOT =       -5768
621385  meter/sec
 ZDOT =      15432
531519                 ZDOT =        4712
329971

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9688840
51                 X    =        -2953158
59
 Y    =      -16925716
06  feet           Y    =        -5158958
25  meter
 Z    =      -10834283
12                 Z    =        -3302289
49
 XDOT =       9977
987302                 XDOT =        3041
290530
 YDOT =     -15597
667718  feet/sec       YDOT =       -4754
169120  meter/sec
 ZDOT =      15471
989539                 ZDOT =        4715
862411


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21041
56762665  
00016717  00000-0  10270-3 0  9110
2 25544  51
6395 249
0033 0002570 356
2123   3
9007 15
48957144 28960


Satellite: ISS
Catalog Number: 25544
Epoch time:      21041
56762665   =   yrday
fracday
Element set:     911
Inclination:       51
6395  deg
RA of node:       249
0033  deg
Eccentricity:     
0002570     
Arg of perigee:   356
2123  deg
Mean anomaly:       3
9007  deg
Mean motion:   15
48957144  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2896
Checksum:              304


Coasting Arc #13 (Orbit 2911)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4759783
94                 A    =         6799811
27  meter
 Y    =        3592945
72  meter          E    =           
0012716
 Z    =        3258351
63                 I    =           51
29146
 XDOT =      -1226
321815                 Wp   =           80
34822
 YDOT =       5914
354158  meter/sec      RA   =          243
01490  deg
 ZDOT =      -4712
397895                 TA   =           61
74040
                                          MA   =           61
61211
                                          Ha   =            229
279  n
mi
                                          Hp   =            222
739

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15616089
05                 X    =         4703426
16
 Y    =       11787879
66  feet           Y    =         3645857
94  meter
 Z    =       10690130
03                 Z    =         3281335
05
 XDOT =      -4023
365536                 XDOT =       -1269
477519
 YDOT =      19404
049074  feet/sec       YDOT =        5900
399243  meter/sec
 ZDOT =     -15460
623016                 ZDOT =       -4718
459476

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11360297
08                 X    =         3462618
55
 Y    =       15857736
39  feet           Y    =         4833438
05  meter
 Z    =       10796808
36                 Z    =         3290867
19
 XDOT =      -8324
084533                 XDOT =       -2537
180966
 YDOT =      16548
431652  feet/sec       YDOT =        5043
961967  meter/sec
 ZDOT =     -15488
771997                 ZDOT =       -4720
977705


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21042
59989628  
00016717  00000-0  10270-3 0  9125
2 25544  51
6393 243
8970 0002669 358
0552   2
0587 15
48967889 29124


Satellite: ISS
Catalog Number: 25544
Epoch time:      21042
59989628   =   yrday
fracday
Element set:     912
Inclination:       51
6393  deg
RA of node:       243
8970  deg
Eccentricity:     
0002669     
Arg of perigee:   358
0552  deg
Mean anomaly:       2
0587  deg
Mean motion:   15
48967889  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2912
Checksum:              353


Coasting Arc #14 (Orbit 2926)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5058258
16                 A    =         6799767
75  meter
 Y    =       -3149301
84  meter          E    =           
0005785
 Z    =       -3277284
57                 I    =           51
30727
 XDOT =        695
546704                 Wp   =           60
31865
 YDOT =      -6001
151989  meter/sec      RA   =          238
04441  deg
 ZDOT =       4702
361814                 TA   =          261
55086
                                          MA   =          261
61644
                                          Ha   =            229
405  n
mi
                                          Hp   =            222
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16595335
18                 X    =        -5006747
18
 Y    =      -10332355
11  feet           Y    =        -3205579
00  meter
 Z    =      -10752245
98                 Z    =        -3301729
53
 XDOT =       2281
977376                 XDOT =         739
761175
 YDOT =     -19688
818860  feet/sec       YDOT =       -5993
126543  meter/sec
 ZDOT =      15427
696239                 ZDOT =        4705
847923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12977743
99                 X    =        -3955616
37
 Y    =      -14535735
02  feet           Y    =        -4430492
04  meter
 Z    =      -10865729
32                 Z    =        -3311874
30
 XDOT =       6527
872817                 XDOT =        1989
695635
 YDOT =     -17350
708006  feet/sec       YDOT =       -5288
495800  meter/sec
 ZDOT =      15443
871555                 ZDOT =        4707
292050


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21043
56765029  
00016717  00000-0  10270-3 0  9131
2 25544  51
6387 239
1098 0002501   8
1271 351
9919 15
48961907 29278


Satellite: ISS
Catalog Number: 25544
Epoch time:      21043
56765029   =   yrday
fracday
Element set:     913
Inclination:       51
6387  deg
RA of node:       239
1098  deg
Eccentricity:     
0002501     
Arg of perigee:     8
1271  deg
Mean anomaly:     351
9919  deg
Mean motion:   15
48961907  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2927
Checksum:              323


Coasting Arc #15 (Orbit 2942)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5306820
56                 A    =         6799822
79  meter
 Y    =        2715207
21  meter          E    =           
0013106
 Z    =        3262415
98                 I    =           51
32623
 XDOT =       -180
932210                 Wp   =           81
41919
 YDOT =       6037
749533  meter/sec      RA   =          233
07561  deg
 ZDOT =      -4712
501058                 TA   =           60
63372
                                          MA   =           60
50290
                                          Ha   =            229
402  n
mi
                                          Hp   =            222
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17410828
62                 X    =         5260217
46
 Y    =        8908160
14  feet           Y    =         2774291
48  meter
 Z    =       10703464
51                 Z    =         3288080
26
 XDOT =       -593
609614                 XDOT =        -225
544856
 YDOT =      19808
889544  feet/sec       YDOT =        6035
476555  meter/sec
 ZDOT =     -15460
961476                 ZDOT =       -4713
488557

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14387184
40                 X    =         4385213
81
 Y    =       13150518
36  feet           Y    =         4008278
00  meter
 Z    =       10822625
13                 Z    =         3298736
14
 XDOT =      -4715
335556                 XDOT =       -1437
234277
 YDOT =      17935
231675  feet/sec       YDOT =        5466
658614  meter/sec
 ZDOT =     -15465
519379                 ZDOT =       -4713
890307


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21044
59991760  
00016717  00000-0  10270-3 0  9149
2 25544  51
6386 234
0038 0002501   7
9141 352
2048 15
48956423 29430


Satellite: ISS
Catalog Number: 25544
Epoch time:      21044
59991760   =   yrday
fracday
Element set:     914
Inclination:       51
6386  deg
RA of node:       234
0038  deg
Eccentricity:     
0002501     
Arg of perigee:     7
9141  deg
Mean anomaly:     352
2048  deg
Mean motion:   15
48956423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2943
Checksum:              303


Coasting Arc #16 (Orbit 2957)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5524012
13                 A    =         6799719
53  meter
 Y    =       -2228946
64  meter          E    =           
0006061
 Z    =       -3280801
63                 I    =           51
34976
 XDOT =       -355
128357                 Wp   =           62
56299
 YDOT =      -6029
524346  meter/sec      RA   =          228
10772  deg
 ZDOT =       4703
797659                 TA   =          259
28589
                                          MA   =          259
35413
                                          Ha   =            229
496  n
mi
                                          Hp   =            222
395

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18123399
37                 X    =        -5482741
03
 Y    =       -7312817
05  feet           Y    =        -2290489
55  meter
 Z    =      -10763784
88                 Z    =        -3307533
96
 XDOT =      -1165
119281                 XDOT =        -310
525664
 YDOT =     -19781
904023  feet/sec       YDOT =       -6033
245985  meter/sec
 ZDOT =      15432
407017                 ZDOT =        4702
181313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15694101
06                 X    =        -4783562
00
 Y    =      -11530065
66  feet           Y    =        -3514364
01  meter
 Z    =      -10887917
19                 Z    =        -3318637
16
 XDOT =       2795
053376                 XDOT =         851
932269
 YDOT =     -18341
326839  feet/sec       YDOT =       -5590
436420  meter/sec
 ZDOT =      15424
859678                 ZDOT =        4701
497230


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21045
56766669  
00016717  00000-0  10270-3 0  9156
2 25544  51
6408 229
2165 0002534  15
8267 344
2962 15
48971971 29582


Satellite: ISS
Catalog Number: 25544
Epoch time:      21045
56766669   =   yrday
fracday
Element set:     915
Inclination:       51
6408  deg
RA of node:       229
2165  deg
Eccentricity:     
0002534     
Arg of perigee:    15
8267  deg
Mean anomaly:     344
2962  deg
Mean motion:   15
48971971  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2958
Checksum:              342


Coasting Arc #17 (Orbit 2973)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5693769
56                 A    =         6799806
64  meter
 Y    =        1761819
49  meter          E    =           
0013611
 Z    =        3263649
22                 I    =           51
37274
 XDOT =        865
103518                 Wp   =           82
01266
 YDOT =       5975
589898  meter/sec      RA   =          223
14159  deg
 ZDOT =      -4716
270914                 TA   =           60
05062
                                          MA   =           59
91555
                                          Ha   =            229
562  n
mi
                                          Hp   =            222
405

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18680346
34                 X    =         5657792
65
 Y    =        5780247
66  feet           Y    =         1825290
36  meter
 Z    =       10707510
56                 Z    =         3291219
14
 XDOT =       2838
266135                 XDOT =         821
126720
 YDOT =      19604
953734  feet/sec       YDOT =        5985
017934  meter/sec
 ZDOT =     -15473
329771                 ZDOT =       -4712
175856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16784118
72                 X    =         5115799
39
 Y    =        9894531
89  feet           Y    =         3015853
32  meter
 Z    =       10835542
54                 Z    =         3302673
37
 XDOT =       -909
239596                 XDOT =        -277
136229
 YDOT =      18533
116502  feet/sec       YDOT =        5648
893910  meter/sec
 ZDOT =     -15454
259527                 ZDOT =       -4710
458304


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21046
59992922  
00016717  00000-0  10270-3 0  9164
2 25544  51
6400 224
1102 0002566  19
7889 340
3360 15
48958151 29749


Satellite: ISS
Catalog Number: 25544
Epoch time:      21046
59992922   =   yrday
fracday
Element set:     916
Inclination:       51
6400  deg
RA of node:       224
1102  deg
Eccentricity:     
0002566     
Arg of perigee:    19
7889  deg
Mean anomaly:     340
3360  deg
Mean motion:   15
48958151  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2974
Checksum:              317


Coasting Arc #18 (Orbit 2978)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4043975
14                 A    =         6793115
93  meter
 Y    =       -1883483
16  meter          E    =           
0007256
 Z    =        5120084
37                 I    =           51
36089
 XDOT =       4705
069952                 Wp   =           41
64596
 YDOT =       5843
259339  meter/sec      RA   =          221
58932  deg
 ZDOT =      -1560
076650                 TA   =           63
50021
                                          MA   =           63
42581
                                          Ha   =            229
497  n
mi
                                          Hp   =            222
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13267634
98                 X    =         4039866
42
 Y    =       -6179406
70  feet           Y    =        -1838283
18  meter
 Z    =       16798177
08                 Z    =         5139718
09
 XDOT =      15436
581207                 XDOT =        4646
956932
 YDOT =      19170
798356  feet/sec       YDOT =        5895
549802  meter/sec
 ZDOT =      -5118
361714                 ZDOT =       -1537
363300

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8533777
45                 X    =        -2601095
37
 Y    =      -11760920
88  feet           Y    =        -3584728
68  meter
 Z    =       16889326
24                 Z    =         5147866
64
 XDOT =      15074
136391                 XDOT =        4594
596772
 YDOT =     -18167
486064  feet/sec       YDOT =       -5537
449752  meter/sec
 ZDOT =      -5012
835986                 ZDOT =       -1527
912409


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   21046
92250919  
00016717  00000-0  10270-3 0  9175
2 25544  51
6423 222
5189 0002859  18
0947 342
0304 15
48993364 29790


Satellite: ISS
Catalog Number: 25544
Epoch time:      21046
92250919   =   yrday
fracday
Element set:     917
Inclination:       51
6423  deg
RA of node:       222
5189  deg
Eccentricity:     
0002859     
Arg of perigee:    18
0947  deg
Mean anomaly:     342
0304  deg
Mean motion:   15
48993364  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2979
Checksum:              329
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