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

 
Date: November 15th 2020

  • 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) : 14262 1813 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 4 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


320/00:49:49 100 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 222 2

320/09:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 222 2

323/04:57:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 222 1

328/12:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 222 0

Coasting Arc #1 (Orbit 1515)
---------------------------------------

Vector Time (GMT): 2020/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -536789
14                 A    =         6794463
04  meter
 Y    =        4781635
73  meter          E    =           
0009258
 Z    =        4792352
75                 I    =           51
43016
 XDOT =      -6988
162115                 Wp   =           57
94225
 YDOT =       1804
962373  meter/sec      RA   =          328
98749  deg
 ZDOT =      -2575
186256                 TA   =           57
55812
                                          MA   =           57
46862
                                          Ha   =            229
547  n
mi
                                          Hp   =            222
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1761119
23                 X    =         -613498
09
 Y    =       15687781
25  feet           Y    =         4775203
97  meter
 Z    =       15722942
08                 Z    =         4789558
93
 XDOT =     -22927
041060                 XDOT =       -6995
317246
 YDOT =       5921
792563  feet/sec       YDOT =        1726
775766  meter/sec
 ZDOT =      -8448
773806                 ZDOT =       -2609
150292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11242610
87                 X    =        -3426747
79
 Y    =      -11100709
76  feet           Y    =        -3383496
33  meter
 Z    =       15709769
98                 Z    =         4788337
89
 XDOT =       8544
427315                 XDOT =        2604
341445
 YDOT =     -20872
150346  feet/sec       YDOT =       -6361
831425  meter/sec
 ZDOT =      -8605
890066                 ZDOT =       -2623
075292


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   20318
54377416  
00016717  00000-0  10270-3 0  9008
2 25544  51
6432 329
4307 0001849  45
7369 314
3933 15
49048288 15165


Satellite: ISS
Catalog Number: 25544
Epoch time:      20318
54377416   =   yrday
fracday
Element set:     900
Inclination:       51
6432  deg
RA of node:       329
4307  deg
Eccentricity:     
0001849     
Arg of perigee:    45
7369  deg
Mean anomaly:     314
3933  deg
Mean motion:   15
49048288  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1516
Checksum:              317


Coasting Arc #2 (Orbit 1530)
---------------------------------------

Vector Time (GMT): 2020/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         128455
73                 A    =         6794605
01  meter
 Y    =       -4823205
47  meter          E    =           
0012171
 Z    =       -4795360
89                 I    =           51
40123
 XDOT =       6794
871713                 Wp   =          100
65805
 YDOT =      -2383
947641  meter/sec      RA   =          324
02666  deg
 ZDOT =       2583
212935                 TA   =          194
92184
                                          MA   =          194
95778
                                          Ha   =            229
580  n
mi
                                          Hp   =            222
244

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         421442
68                 X    =          205674
54
 Y    =      -15824164
92  feet           Y    =        -4821337
01  meter
 Z    =      -15732811
31                 Z    =        -4794549
55
 XDOT =      22292
886198                 XDOT =        6808
476576
 YDOT =      -7821
350527  feet/sec       YDOT =       -2307
886556  meter/sec
 ZDOT =       8475
108056                 ZDOT =        2616
253692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12344537
69                 X    =         3762615
09
 Y    =        9915657
81  feet           Y    =         3022292
50  meter
 Z    =      -15728804
16                 Z    =        -4794139
51
 XDOT =      -6355
955327                 XDOT =       -1937
295184
 YDOT =      21581
354457  feet/sec       YDOT =        6577
996838  meter/sec
 ZDOT =       8627
976799                 ZDOT =        2629
807328


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   20319
51148530  
00016717  00000-0  10270-3 0  9010
2 25544  51
6426 324
6443 0001771  46
1290 314
0006 15
49004233 15315


Satellite: ISS
Catalog Number: 25544
Epoch time:      20319
51148530   =   yrday
fracday
Element set:     901
Inclination:       51
6426  deg
RA of node:       324
6443  deg
Eccentricity:     
0001771     
Arg of perigee:    46
1290  deg
Mean anomaly:     314
0006  deg
Mean motion:   15
49004233  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1531
Checksum:              259


Coasting Arc #3 (Orbit 1539)
---------------------------------------

Vector Time (GMT): 2020/320/00:49:49
100
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5796589
42                 A    =         6799385
13  meter
 Y    =       -1235326
53  meter          E    =           
0013736
 Z    =        3319193
29                 I    =           51
40084
 XDOT =      -1424
670190                 Wp   =           84
80111
 YDOT =       5906
655055  meter/sec      RA   =          321
41452  deg
 ZDOT =       4670
832178                 TA   =          313
89711
                                          MA   =          314
01045
                                          Ha   =            229
360  n
mi
                                          Hp   =            222
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19017681
83                 X    =         5793849
17
 Y    =       -4052908
58  feet           Y    =        -1170520
44  meter
 Z    =       10889741
77                 Z    =         3347344
97
 XDOT =      -4674
114797                 XDOT =       -1513
303221
 YDOT =      19378
789550  feet/sec       YDOT =        5890
227495  meter/sec
 ZDOT =      15324
252554                 ZDOT =        4663
696575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3961645
71                 X    =         1207509
61
 Y    =      -18961828
50  feet           Y    =        -5779565
33  meter
 Z    =       11019945
06                 Z    =         3358879
25
 XDOT =      14404
012386                 XDOT =        4390
342975
 YDOT =      11925
178939  feet/sec       YDOT =        3634
794540  meter/sec
 ZDOT =      15290
953421                 ZDOT =        4660
682603


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   20320
09211049  
00016717  00000-0  10270-3 0  9022
2 25544  51
6401 321
7681 0001510  52
1461 307
9826 15
49047282 15400


Satellite: ISS
Catalog Number: 25544
Epoch time:      20320
09211049   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:       321
7681  deg
Eccentricity:     
0001510     
Arg of perigee:    52
1461  deg
Mean anomaly:     307
9826  deg
Mean motion:   15
49047282  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1540
Checksum:              266


Coasting Arc #4 (Orbit 1544)
---------------------------------------

Vector Time (GMT): 2020/320/09:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -485043
73                 A    =         6794193
89  meter
 Y    =       -4712400
52  meter          E    =           
0012849
 Z    =       -4882080
66                 I    =           51
37708
 XDOT =       6571
745986                 Wp   =          100
22703
 YDOT =      -3121
950754  meter/sec      RA   =          319
54608  deg
 ZDOT =       2363
627112                 TA   =          193
05203
                                          MA   =          193
08531
                                          Ha   =            229
574  n
mi
                                          Hp   =            222
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1591350
81                 X    =         -408597
14
 Y    =      -15460631
62  feet           Y    =        -4717396
82  meter
 Z    =      -16017324
98                 Z    =        -4884251
55
 XDOT =      21560
846411                 XDOT =        6594
686667
 YDOT =     -10242
620585  feet/sec       YDOT =       -3048
332683  meter/sec
 ZDOT =       7754
682127                 ZDOT =        2395
606512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6442552
92                 X    =         1963690
13
 Y    =       14133061
93  feet           Y    =         4307757
28  meter
 Z    =      -16027111
39                 Z    =        -4885063
55
 XDOT =     -15960
958662                 XDOT =       -4864
900200
 YDOT =      16226
042867  feet/sec       YDOT =        4945
697866  meter/sec
 ZDOT =       7902
677874                 ZDOT =        2408
736216


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   20320
41468041  
00016717  00000-0  10270-3 0  9035
2 25544  51
6439 320
1752 0001769  49
3545 310
7758 15
49018813 15459


Satellite: ISS
Catalog Number: 25544
Epoch time:      20320
41468041   =   yrday
fracday
Element set:     903
Inclination:       51
6439  deg
RA of node:       320
1752  deg
Eccentricity:     
0001769     
Arg of perigee:    49
3545  deg
Mean anomaly:     310
7758  deg
Mean motion:   15
49018813  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1545
Checksum:              298


Coasting Arc #5 (Orbit 1560)
---------------------------------------

Vector Time (GMT): 2020/321/09:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         855958
83                 A    =         6794118
57  meter
 Y    =        4666487
14  meter          E    =           
0008854
 Z    =        4858517
34                 I    =           51
35213
 XDOT =      -6293
857992                 Wp   =           57
93004
 YDOT =       3657
081762  meter/sec      RA   =          314
58107  deg
 ZDOT =      -2395
873700                 TA   =           55
70927
                                          MA   =           55
62548
                                          Ha   =            229
534  n
mi
                                          Hp   =            222
094

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2808263
88                 X    =          780112
64
 Y    =       15309997
17  feet           Y    =         4675634
49  meter
 Z    =       15940017
51                 Z    =         4862491
62
 XDOT =     -20649
140394                 XDOT =       -6322
646727
 YDOT =      11998
299743  feet/sec       YDOT =        3586
538606  meter/sec
 ZDOT =      -7860
478020                 ZDOT =       -2426
517136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7777002
66                 X    =        -2370430
41
 Y    =      -13461884
59  feet           Y    =        -4103182
42  meter
 Z    =       15958145
58                 Z    =         4864042
77
 XDOT =      14261
918978                 XDOT =        4347
032905
 YDOT =     -17755
816513  feet/sec       YDOT =       -5411
972873  meter/sec
 ZDOT =      -8002
322550                 ZDOT =       -2439
107913


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   20321
44689839  
00016717  00000-0  10270-3 0  9040
2 25544  51
6437 315
0691 0001866  52
9740 307
1581 15
49060160 15611


Satellite: ISS
Catalog Number: 25544
Epoch time:      20321
44689839   =   yrday
fracday
Element set:     904
Inclination:       51
6437  deg
RA of node:       315
0691  deg
Eccentricity:     
0001866     
Arg of perigee:    52
9740  deg
Mean anomaly:     307
1581  deg
Mean motion:   15
49060160  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1561
Checksum:              305


Coasting Arc #6 (Orbit 1575)
---------------------------------------

Vector Time (GMT): 2020/322/09:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1247380
23                 A    =         6794244
24  meter
 Y    =       -4593295
94  meter          E    =           
0012924
 Z    =       -4860412
44                 I    =           51
33044
 XDOT =       5948
727317                 Wp   =          100
46297
 YDOT =      -4162
265759  meter/sec      RA   =          309
61436  deg
 ZDOT =       2410
023056                 TA   =          193
31749
                                          MA   =          193
35164
                                          Ha   =            229
625  n
mi
                                          Hp   =            222
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4092454
82                 X    =        -1172314
32
 Y    =      -15069868
58  feet           Y    =        -4606824
74  meter
 Z    =      -15946235
04                 Z    =        -4866290
07
 XDOT =      19516
821906                 XDOT =        5983
122161
 YDOT =     -13655
727555  feet/sec       YDOT =       -4095
550797  meter/sec
 ZDOT =       7906
899791                 ZDOT =        2439
003269

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9120140
56                 X    =         2779818
84
 Y    =       12641692
45  feet           Y    =         3853187
86  meter
 Z    =      -15973170
81                 Z    =        -4868622
46
 XDOT =     -12352
872452                 XDOT =       -3765
155523
 YDOT =      19058
720695  feet/sec       YDOT =        5809
098068  meter/sec
 ZDOT =       8041
078933                 ZDOT =        2450
920859


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   20322
41460168  
00016717  00000-0  10270-3 0  9051
2 25544  51
6449 310
2822 0001888  53
8310 306
3015 15
49024683 15763


Satellite: ISS
Catalog Number: 25544
Epoch time:      20322
41460168   =   yrday
fracday
Element set:     905
Inclination:       51
6449  deg
RA of node:       310
2822  deg
Eccentricity:     
0001888     
Arg of perigee:    53
8310  deg
Mean anomaly:     306
3015  deg
Mean motion:   15
49024683  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1576
Checksum:              288


Coasting Arc #7 (Orbit 1588)
---------------------------------------

Vector Time (GMT): 2020/323/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2758678
17                 A    =         6792419
80  meter
 Y    =        3339516
96  meter          E    =           
0005142
 Z    =        5228618
73                 I    =           51
30834
 XDOT =      -5038
507421                 Wp   =           58
43201
 YDOT =       5691
615692  meter/sec      RA   =          305
62955  deg
 ZDOT =       -973
507222                 TA   =           40
95401
                                          MA   =           40
91541
                                          Ha   =            229
351  n
mi
                                          Hp   =            222
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9050781
41                 X    =         2695731
63
 Y    =       10956420
46  feet           Y    =         3370013
88  meter
 Z    =       17154260
94                 Z    =         5241867
04
 XDOT =     -16530
536159                 XDOT =       -5097
049504
 YDOT =      18673
279830  feet/sec       YDOT =        5634
944276  meter/sec
 ZDOT =      -3193
921333                 ZDOT =        -998
124189

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2367439
67                 X    =          721595
61
 Y    =      -13937568
36  feet           Y    =        -4248170
84  meter
 Z    =       17215338
49                 Z    =         5247235
17
 XDOT =      23907
345725                 XDOT =        7286
958977
 YDOT =        -38
591407  feet/sec       YDOT =         -11
762661  meter/sec
 ZDOT =      -3308
003096                 ZDOT =       -1008
279344


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   20323
25327528  
00016717  00000-0  10270-3 0  9067
2 25544  51
6450 306
1314 0001516  60
9923 299
1379 15
49080479 15893


Satellite: ISS
Catalog Number: 25544
Epoch time:      20323
25327528   =   yrday
fracday
Element set:     906
Inclination:       51
6450  deg
RA of node:       306
1314  deg
Eccentricity:     
0001516     
Arg of perigee:    60
9923  deg
Mean anomaly:     299
1379  deg
Mean motion:   15
49080479  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1589
Checksum:              314


Coasting Arc #8 (Orbit 1603)
---------------------------------------

Vector Time (GMT): 2020/324/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3028954
74                 A    =         6792530
69  meter
 Y    =       -3116561
85  meter          E    =           
0015604
 Z    =       -5233972
04                 I    =           51
28919
 XDOT =       4533
341988                 Wp   =           94
46198
 YDOT =      -6078
953944  meter/sec      RA   =          300
66121  deg
 ZDOT =        997
607721                 TA   =          185
15228
                                          MA   =          185
16836
                                          Ha   =            229
521  n
mi
                                          Hp   =            222
015

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9937515
56                 X    =        -2968455
39
 Y    =      -10224940
47  feet           Y    =        -3150094
94  meter
 Z    =      -17171824
27                 Z    =        -5248539
07
 XDOT =      14873
169251                 XDOT =        4596
135906
 YDOT =     -19944
074619  feet/sec       YDOT =       -6027
907870  meter/sec
 ZDOT =       3272
991212                 ZDOT =        1019
780975

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -990051
47                 X    =         -301767
69
 Y    =       14142533
45  feet           Y    =         4310644
20  meter
 Z    =      -17239017
30                 Z    =        -5254452
47
 XDOT =     -23720
388640                 XDOT =       -7229
974457
 YDOT =       2448
797695  feet/sec       YDOT =         746
393538  meter/sec
 ZDOT =       3375
784890                 ZDOT =        1028
939235


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   20324
22097554  
00016717  00000-0  10270-3 0  9079
2 25544  51
6446 301
3456 0001560  64
1334 295
9976 15
49051616 16049


Satellite: ISS
Catalog Number: 25544
Epoch time:      20324
22097554   =   yrday
fracday
Element set:     907
Inclination:       51
6446  deg
RA of node:       301
3456  deg
Eccentricity:     
0001560     
Arg of perigee:    64
1334  deg
Mean anomaly:     295
9976  deg
Mean motion:   15
49051616  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1604
Checksum:              302


Coasting Arc #9 (Orbit 1619)
---------------------------------------

Vector Time (GMT): 2020/325/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3260121
76                 A    =         6792427
10  meter
 Y    =        2873311
64  meter          E    =           
0005229
 Z    =        5216922
33                 I    =           51
27381
 XDOT =      -4019
014986                 Wp   =           59
07751
 YDOT =       6442
740029  meter/sec      RA   =          295
69028  deg
 ZDOT =      -1033
505252                 TA   =           40
89659
                                          MA   =           40
85738
                                          Ha   =            229
325  n
mi
                                          Hp   =            222
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10695937
52                 X    =         3202408
23
 Y    =        9426875
47  feet           Y    =         2909445
46  meter
 Z    =       17115886
92                 Z    =         5232618
94
 XDOT =     -13185
744705                 XDOT =       -4085
740743
 YDOT =      21137
598520  feet/sec       YDOT =        6397
423531  meter/sec
 ZDOT =      -3390
765263                 ZDOT =       -1053
189629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -354545
71                 X    =         -108065
53
 Y    =      -14165398
85  feet           Y    =        -4317613
57  meter
 Z    =       17188322
16                 Z    =         5239000
59
 XDOT =      23390
645923                 XDOT =        7129
468877
 YDOT =      -4824
107162  feet/sec       YDOT =       -1470
387863  meter/sec
 ZDOT =      -3482
055759                 ZDOT =       -1061
330595


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   20325
25318303  
00016717  00000-0  10270-3 0  9082
2 25544  51
6453 296
2393 0001502  64
5696 295
5610 15
49090390 16201


Satellite: ISS
Catalog Number: 25544
Epoch time:      20325
25318303   =   yrday
fracday
Element set:     908
Inclination:       51
6453  deg
RA of node:       296
2393  deg
Eccentricity:     
0001502     
Arg of perigee:    64
5696  deg
Mean anomaly:     295
5610  deg
Mean motion:   15
49090390  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1620
Checksum:              297


Coasting Arc #10 (Orbit 1634)
---------------------------------------

Vector Time (GMT): 2020/326/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3490614
49                 A    =         6792574
39  meter
 Y    =       -2613741
92  meter          E    =           
0015666
 Z    =       -5221787
88                 I    =           51
25903
 XDOT =       3459
490222                 Wp   =           94
86515
 YDOT =      -6738
234249  meter/sec      RA   =          290
71936  deg
 ZDOT =       1061
688168                 TA   =          185
37774
                                          MA   =          185
39458
                                          Ha   =            229
571  n
mi
                                          Hp   =            221
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11452147
29                 X    =        -3435762
82
 Y    =       -8575268
75  feet           Y    =        -2652469
37  meter
 Z    =      -17131850
01                 Z    =        -5238610
99
 XDOT =      11350
033537                 XDOT =        3529
424980
 YDOT =     -22107
067745  feet/sec       YDOT =       -6699
156799  meter/sec
 ZDOT =       3483
228896                 ZDOT =        1078
662436

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1735858
43                 X    =          529089
65
 Y    =       14106971
73  feet           Y    =         4299804
98  meter
 Z    =      -17209513
08                 Z    =        -5245459
59
 XDOT =     -22725
203133                 XDOT =       -6926
641915
 YDOT =       7135
863045  feet/sec       YDOT =        2175
011056  meter/sec
 ZDOT =       3561
986097                 ZDOT =        1085
693362


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   20326
22087693  
00016717  00000-0  10270-3 0  9096
2 25544  51
6440 291
4532 0001681  66
0233 294
1092 15
49050323 16358


Satellite: ISS
Catalog Number: 25544
Epoch time:      20326
22087693   =   yrday
fracday
Element set:     909
Inclination:       51
6440  deg
RA of node:       291
4532  deg
Eccentricity:     
0001681     
Arg of perigee:    66
0233  deg
Mean anomaly:     294
1092  deg
Mean motion:   15
49050323  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1635
Checksum:              288


Coasting Arc #11 (Orbit 1650)
---------------------------------------

Vector Time (GMT): 2020/327/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3680132
60                 A    =         6792473
41  meter
 Y    =        2339642
39  meter          E    =           
0005419
 Z    =        5204039
67                 I    =           51
24807
 XDOT =      -2894
777672                 Wp   =           60
73464
 YDOT =       7009
965402  meter/sec      RA   =          285
74704  deg
 ZDOT =      -1100
984502                 TA   =           39
90069
                                          MA   =           39
86087
                                          Ha   =            229
362  n
mi
                                          Hp   =            222
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12073925
86                 X    =         3628418
11
 Y    =        7675992
09  feet           Y    =         2380506
79  meter
 Z    =       17073620
96                 Z    =         5221790
96
 XDOT =      -9497
302073                 XDOT =       -2967
602098
 YDOT =      22998
574154  feet/sec       YDOT =        6977
186801  meter/sec
 ZDOT =      -3612
153879                 ZDOT =       -1115
222718

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3053691
93                 X    =         -930765
30
 Y    =      -13876946
23  feet           Y    =        -4229693
21  meter
 Z    =       17155593
90                 Z    =         5229025
02
 XDOT =      21929
421435                 XDOT =        6684
087654
 YDOT =      -9387
002991  feet/sec       YDOT =       -2861
158512  meter/sec
 ZDOT =      -3678
254044                 ZDOT =       -1121
131833


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   20327
25307942  
00016717  00000-0  10270-3 0  9104
2 25544  51
6438 286
3475 0001595  71
2458 288
8865 15
49089483 16510


Satellite: ISS
Catalog Number: 25544
Epoch time:      20327
25307942   =   yrday
fracday
Element set:     910
Inclination:       51
6438  deg
RA of node:       286
3475  deg
Eccentricity:     
0001595     
Arg of perigee:    71
2458  deg
Mean anomaly:     288
8865  deg
Mean motion:   15
49089483  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1651
Checksum:              338


Coasting Arc #12 (Orbit 1665)
---------------------------------------

Vector Time (GMT): 2020/328/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3867109
43                 A    =         6792625
94  meter
 Y    =       -2049217
62  meter          E    =           
0015680
 Z    =       -5208667
44                 I    =           51
23923
 XDOT =       2296
471547                 Wp   =           96
04703
 YDOT =      -7207
182872  meter/sec      RA   =          280
77377  deg
 ZDOT =       1131
832320                 TA   =          184
88513
                                          MA   =          184
90045
                                          Ha   =            229
594  n
mi
                                          Hp   =            221
917

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12687366
88                 X    =        -3818606
12
 Y    =       -6723154
92  feet           Y    =        -2092190
95  meter
 Z    =      -17088803
94                 Z    =        -5227334
79
 XDOT =       7534
355470                 XDOT =        2371
395933
 YDOT =     -23645
613097  feet/sec       YDOT =       -7181
083207  meter/sec
 ZDOT =       3713
360630                 ZDOT =        1143
169375

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4394575
39                 X    =         1339466
58
 Y    =       13561098
18  feet           Y    =         4133422
73  meter
 Z    =      -17175029
37                 Z    =        -5234948
95
 XDOT =     -20817
585876                 XDOT =       -6345
200175
 YDOT =      11510
227996  feet/sec       YDOT =        3508
317493  meter/sec
 ZDOT =       3766
036358                 ZDOT =        1147
887882


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   20328
22076872  
00016717  00000-0  10270-3 0  9118
2 25544  51
6429 281
5606 0001681  73
2093 286
9242 15
49048591 16665


Satellite: ISS
Catalog Number: 25544
Epoch time:      20328
22076872   =   yrday
fracday
Element set:     911
Inclination:       51
6429  deg
RA of node:       281
5606  deg
Eccentricity:     
0001681     
Arg of perigee:    73
2093  deg
Mean anomaly:     286
9242  deg
Mean motion:   15
49048591  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1666
Checksum:              317


Coasting Arc #13 (Orbit 1670)
---------------------------------------

Vector Time (GMT): 2020/328/12:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1073818
80                 A    =         6801364
18  meter
 Y    =       -6213086
04  meter          E    =           
0007016
 Z    =       -2548661
23                 I    =           51
26582
 XDOT =       4731
801301                 Wp   =           54
82019
 YDOT =      -2961
378316  meter/sec      RA   =          279
11352  deg
 ZDOT =       5239
809063                 TA   =          276
46675
                                          MA   =          276
54664
                                          Ha   =            229
619  n
mi
                                          Hp   =            222
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3523027
55                 X    =         -991882
33
 Y    =      -20384140
56  feet           Y    =        -6224636
00  meter
 Z    =       -8361749
44                 Z    =        -2553678
76
 XDOT =      15524
282484                 XDOT =        4739
112437
 YDOT =      -9715
808125  feet/sec       YDOT =       -2908
423292  meter/sec
 ZDOT =      17190
974616                 ZDOT =        5262
812116

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20611860
88                 X    =         6282495
20
 Y    =        1640535
81  feet           Y    =          500035
31  meter
 Z    =       -8384724
00                 Z    =        -2555663
87
 XDOT =       5758
705621                 XDOT =        1755
253473
 YDOT =      15815
440662  feet/sec       YDOT =        4820
546314  meter/sec
 ZDOT =      17297
425000                 ZDOT =        5272
255140


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   20328
54333154  
00016717  00000-0  10270-3 0  9123
2 25544  51
6423 279
9659 0001870  65
9559 294
1787 15
49054186 16711


Satellite: ISS
Catalog Number: 25544
Epoch time:      20328
54333154   =   yrday
fracday
Element set:     912
Inclination:       51
6423  deg
RA of node:       279
9659  deg
Eccentricity:     
0001870     
Arg of perigee:    65
9559  deg
Mean anomaly:     294
1787  deg
Mean motion:   15
49054186  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1671
Checksum:              338


Coasting Arc #14 (Orbit 1686)
---------------------------------------

Vector Time (GMT): 2020/329/12:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1565620
22                 A    =         6801413
22  meter
 Y    =        6122356
05  meter          E    =           
0015282
 Z    =        2497440
82                 I    =           51
26283
 XDOT =      -4476
741293                 Wp   =          100
12771
 YDOT =       3304
167047  meter/sec      RA   =          274
13960  deg
 ZDOT =      -5268
583095                 TA   =           51
76050
                                          MA   =           51
62305
                                          Ha   =            229
617  n
mi
                                          Hp   =            221
939

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5136549
27                 X    =         1484910
53
 Y    =       20086470
00  feet           Y    =         6139412
56  meter
 Z    =        8193703
46                 Z    =         2504850
32
 XDOT =     -14687
471433                 XDOT =       -4487
764699
 YDOT =      10840
443068  feet/sec       YDOT =        3254
043510  meter/sec
 ZDOT =     -17285
377609                 ZDOT =       -5290
356240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20716316
86                 X    =        -6314333
38
 Y    =         354188
20  feet           Y    =          107956
56  meter
 Z    =        8227755
35                 Z    =         2507819
83
 XDOT =      -7196
597306                 XDOT =       -2193
522859
 YDOT =     -15150
068284  feet/sec       YDOT =       -4617
740813  meter/sec
 ZDOT =     -17386
146435                 ZDOT =       -5299
297433


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   20329
57552673  
00016717  00000-0  10270-3 0  9137
2 25544  51
6431 274
8592 0001966  68
0213 292
1146 15
49074535 16871


Satellite: ISS
Catalog Number: 25544
Epoch time:      20329
57552673   =   yrday
fracday
Element set:     913
Inclination:       51
6431  deg
RA of node:       274
8592  deg
Eccentricity:     
0001966     
Arg of perigee:    68
0213  deg
Mean anomaly:     292
1146  deg
Mean motion:   15
49074535  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1687
Checksum:              322


Coasting Arc #15 (Orbit 1701)
---------------------------------------

Vector Time (GMT): 2020/330/12:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2080563
38                 A    =         6801441
58  meter
 Y    =       -5979089
40  meter          E    =           
0007193
 Z    =       -2484594
74                 I    =           51
26096
 XDOT =       4181
997711                 Wp   =           55
08390
 YDOT =      -3642
361626  meter/sec      RA   =          269
16603  deg
 ZDOT =       5278
231798                 TA   =          276
98708
                                          MA   =          277
06889
                                          Ha   =            229
639  n
mi
                                          Hp   =            221
916

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6825995
33                 X    =        -2001479
83
 Y    =      -19616435
03  feet           Y    =        -6001913
45  meter
 Z    =       -8151557
56                 Z    =        -2494509
67
 XDOT =      13720
464930                 XDOT =        4196
777857
 YDOT =     -11950
005334  feet/sec       YDOT =       -3595
513133  meter/sec
 ZDOT =      17317
033457                 ZDOT =        5298
582348

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20605675
70                 X    =         6280609
95
 Y    =       -2461398
42  feet           Y    =         -750234
24  meter
 Z    =       -8197211
31                 Z    =        -2498510
01
 XDOT =       8617
701354                 XDOT =        2626
675373
 YDOT =      14321
189255  feet/sec       YDOT =        4365
098485  meter/sec
 ZDOT =      17411
229574                 ZDOT =        5306
942774


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   20330
54320652  
00016717  00000-0  10270-3 0  9147
2 25544  51
6424 270
0726 0001967  71
0212 289
1151 15
49069266 17029


Satellite: ISS
Catalog Number: 25544
Epoch time:      20330
54320652   =   yrday
fracday
Element set:     914
Inclination:       51
6424  deg
RA of node:       270
0726  deg
Eccentricity:     
0001967     
Arg of perigee:    71
0212  deg
Mean anomaly:     289
1151  deg
Mean motion:   15
49069266  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1702
Checksum:              280


Coasting Arc #16 (Orbit 1717)
---------------------------------------

Vector Time (GMT): 2020/331/12:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2550802
28                 A    =         6801524
62  meter
 Y    =        5809990
36  meter          E    =           
0015402
 Z    =        2430631
35                 I    =           51
26384
 XDOT =      -3880
112936                 Wp   =          101
92265
 YDOT =       3935
002082  meter/sec      RA   =          264
19255  deg
 ZDOT =      -5308
437096                 TA   =           50
78136
                                          MA   =           50
64472
                                          Ha   =            229
607  n
mi
                                          Hp   =            221
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8368773
87                 X    =         2473836
78
 Y    =       19061648
15  feet           Y    =         5838084
78  meter
 Z    =        7974512
31                 Z    =         2442835
78
 XDOT =     -12730
029319                 XDOT =       -3898
041109
 YDOT =      12910
111818  feet/sec       YDOT =        3891
511933  meter/sec
 ZDOT =     -17416
132205                 ZDOT =       -5327
328841

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20317155
67                 X    =        -6192669
05
 Y    =        4437970
75  feet           Y    =         1352693
48  meter
 Z    =        8030769
22                 Z    =         2447778
46
 XDOT =      -9879
359873                 XDOT =       -3011
228889
 YDOT =     -13403
673491  feet/sec       YDOT =       -4085
439680  meter/sec
 ZDOT =     -17503
587258                 ZDOT =       -5335
093396


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   20331
57539598  
00016717  00000-0  10270-3 0  9153
2 25544  51
6432 264
9665 0001925  75
6228 284
5135 15
49079339 17183


Satellite: ISS
Catalog Number: 25544
Epoch time:      20331
57539598   =   yrday
fracday
Element set:     915
Inclination:       51
6432  deg
RA of node:       264
9665  deg
Eccentricity:     
0001925     
Arg of perigee:    75
6228  deg
Mean anomaly:     284
5135  deg
Mean motion:   15
49079339  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1718
Checksum:              340


Coasting Arc #17 (Orbit 1732)
---------------------------------------

Vector Time (GMT): 2020/332/12:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965450
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3035455
14                 A    =         6801511
61  meter
 Y    =       -5586185
37  meter          E    =           
0007144
 Z    =       -2415012
59                 I    =           51
26911
 XDOT =       3540
286763                 Wp   =           55
29380
 YDOT =      -4216
961010  meter/sec      RA   =          259
21880  deg
 ZDOT =       5319
727206                 TA   =          277
62795
                                          MA   =          277
70908
                                          Ha   =            229
578  n
mi
                                          Hp   =            221
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9958842
33                 X    =        -2961032
13
 Y    =      -18327379
82  feet           Y    =        -5619713
71  meter
 Z    =       -7923269
66                 Z    =        -2429577
60
 XDOT =      11615
114052                 XDOT =        3561
338239
 YDOT =     -13835
173918  feet/sec       YDOT =       -4177
253662  meter/sec
 ZDOT =      17453
173247                 ZDOT =        5336
975722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19798465
70                 X    =         6034572
34
 Y    =       -6482507
86  feet           Y    =        -1975868
40  meter
 Z    =       -7990459
41                 Z    =        -2435492
03
 XDOT =      11093
647675                 XDOT =        3381
343811
 YDOT =      12331
184163  feet/sec       YDOT =        3758
544933  meter/sec
 ZDOT =      17533
035055                 ZDOT =        5344
069085


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   20332
54306957  
00016717  00000-0  10270-3 0  9163
2 25544  51
6437 260
1795 0001853  78
3244 281
8114 15
49090067 17333


Satellite: ISS
Catalog Number: 25544
Epoch time:      20332
54306957   =   yrday
fracday
Element set:     916
Inclination:       51
6437  deg
RA of node:       260
1795  deg
Eccentricity:     
0001853     
Arg of perigee:    78
3244  deg
Mean anomaly:     281
8114  deg
Mean motion:   15
49090067  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1733
Checksum:              310
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