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

 
Date: October 28th 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) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 453 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


311/18:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 2
000/00:00:00 000 0 0 0 0 221 3

Coasting Arc #1 (Orbit 1236)
---------------------------------------

Vector Time (GMT): 2020/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3577675
88                 A    =         6791277
87  meter
 Y    =        2168936
92  meter          E    =           
0003828
 Z    =        5346306
74                 I    =           51
95750
 XDOT =      -4029
614388                 Wp   =           77
56436
 YDOT =      -6518
928943  meter/sec      RA   =           57
97933  deg
 ZDOT =        -51
073679                 TA   =           12
92537
                                          MA   =           12
91556
                                          Ha   =            229
158  n
mi
                                          Hp   =            221
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11737781
74                 X    =        -3627633
25
 Y    =        7115934
77  feet           Y    =         2128649
62  meter
 Z    =       17540376
44                 Z    =         5328806
20
 XDOT =     -13220
519647                 XDOT =       -3956
170177
 YDOT =     -21387
562148  feet/sec       YDOT =       -6563
580332  meter/sec
 ZDOT =       -167
564563                 ZDOT =         -70
469581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5759665
78                 X    =         1755546
13
 Y    =      -12572844
38  feet           Y    =        -3832202
97  meter
 Z    =       17459286
58                 Z    =         5321590
55
 XDOT =      22076
471593                 XDOT =        6728
908542
 YDOT =       9752
520358  feet/sec       YDOT =        2972
568205  meter/sec
 ZDOT =       -257
069251                 ZDOT =         -78
354708


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   20300
54826550  
00016717  00000-0  10270-3 0  9007
2 25544  51
6437  58
4861 0001477  64
0789 296
0513 15
49355937 12373


Satellite: ISS
Catalog Number: 25544
Epoch time:      20300
54826550   =   yrday
fracday
Element set:     900
Inclination:       51
6437  deg
RA of node:        58
4861  deg
Eccentricity:     
0001477     
Arg of perigee:    64
0789  deg
Mean anomaly:     296
0513  deg
Mean motion:   15
49355937  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1237
Checksum:              314


Coasting Arc #2 (Orbit 1251)
---------------------------------------

Vector Time (GMT): 2020/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3474235
57                 A    =         6791294
91  meter
 Y    =       -2354204
56  meter          E    =           
0016278
 Z    =       -5353429
32                 I    =           51
93973
 XDOT =       4480
486314                 Wp   =           89
05213
 YDOT =       6196
276805  meter/sec      RA   =           53
05226  deg
 ZDOT =        183
610162                 TA   =          182
69061
                                          MA   =          182
69938
                                          Ha   =            229
060  n
mi
                                          Hp   =            221
754

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11398410
68                 X    =         3526307
04
 Y    =       -7723768
25  feet           Y    =        -2315062
23  meter
 Z    =      -17563744
48                 Z    =        -5336426
04
 XDOT =      14699
758248                 XDOT =        4409
972789
 YDOT =      20328
992143  feet/sec       YDOT =        6245
986560  meter/sec
 ZDOT =        602
395544                 ZDOT =         205
203389

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4913937
84                 X    =        -1497768
25
 Y    =       12969011
99  feet           Y    =         3952954
85  meter
 Z    =      -17484948
53                 Z    =        -5329412
31
 XDOT =     -22809
236882                 XDOT =       -6952
255402
 YDOT =      -7699
153634  feet/sec       YDOT =       -2346
702028  meter/sec
 ZDOT =        702
067871                 ZDOT =         213
990287


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   20301
51578119  
00016717  00000-0  10270-3 0  9011
2 25544  51
6448  53
6989 0001594  67
4236 292
7082 15
49359494 12520


Satellite: ISS
Catalog Number: 25544
Epoch time:      20301
51578119   =   yrday
fracday
Element set:     901
Inclination:       51
6448  deg
RA of node:        53
6989  deg
Eccentricity:     
0001594     
Arg of perigee:    67
4236  deg
Mean anomaly:     292
7082  deg
Mean motion:   15
49359494  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1252
Checksum:              325


Coasting Arc #3 (Orbit 1267)
---------------------------------------

Vector Time (GMT): 2020/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3355568
69                 A    =         6791244
66  meter
 Y    =        2520585
99  meter          E    =           
0004189
 Z    =        5335915
16                 I    =           51
91884
 XDOT =      -4921
084885                 Wp   =           71
04763
 YDOT =      -5866
707860  meter/sec      RA   =           48
12225  deg
 ZDOT =       -321
843234                 TA   =           22
01952
                                          MA   =           22
00153
                                          Ha   =            229
163  n
mi
                                          Hp   =            221
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11009083
64                 X    =        -3409424
54
 Y    =        8269639
07  feet           Y    =         2482760
71  meter
 Z    =       17506283
34                 Z    =         5319483
92
 XDOT =     -16145
291618                 XDOT =       -4853
552480
 YDOT =     -19247
729200  feet/sec       YDOT =       -5921
361380  meter/sec
 ZDOT =      -1055
916123                 ZDOT =        -345
584082

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4052570
06                 X    =         1235223
35
 Y    =      -13259868
91  feet           Y    =        -4041608
04  meter
 Z    =       17430127
98                 Z    =         5312703
01
 XDOT =      23442
850063                 XDOT =        7145
380699
 YDOT =       5626
045792  feet/sec       YDOT =        1714
818757  meter/sec
 ZDOT =      -1165
524264                 ZDOT =        -355
251796


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   20302
54779199  
00016717  00000-0  10270-3 0  9027
2 25544  51
6452  48
5909 0001604  67
1519 292
9800 15
49380731 12688


Satellite: ISS
Catalog Number: 25544
Epoch time:      20302
54779199   =   yrday
fracday
Element set:     902
Inclination:       51
6452  deg
RA of node:        48
5909  deg
Eccentricity:     
0001604     
Arg of perigee:    67
1519  deg
Mean anomaly:     292
9800  deg
Mean motion:   15
49380731  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1268
Checksum:              319


Coasting Arc #4 (Orbit 1282)
---------------------------------------

Vector Time (GMT): 2020/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3241624
65                 A    =         6791341
23  meter
 Y    =       -2697798
67  meter          E    =           
0016250
 Z    =       -5337213
91                 I    =           51
89547
 XDOT =       5314
409722                 Wp   =           91
16892
 YDOT =       5481
770871  meter/sec      RA   =           43
19297  deg
 ZDOT =        457
788861                 TA   =          183
18813
                                          MA   =          183
19850
                                          Ha   =            229
083  n
mi
                                          Hp   =            221
698

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10635251
49                 X    =         3297477
03
 Y    =       -8851045
51  feet           Y    =        -2661236
41  meter
 Z    =      -17510544
32                 Z    =        -5321331
26
 XDOT =      17435
727434                 XDOT =        5250
492198
 YDOT =      17984
812569  feet/sec       YDOT =        5540
843047  meter/sec
 ZDOT =       1501
931959                 ZDOT =         483
449293

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3173915
57                 X    =         -967409
46
 Y    =       13562773
67  feet           Y    =         4133933
41  meter
 Z    =      -17436919
84                 Z    =        -5314773
17
 XDOT =     -23775
502535                 XDOT =       -7246
773173
 YDOT =      -3484
314752  feet/sec       YDOT =       -1062
019136  meter/sec
 ZDOT =       1620
421488                 ZDOT =         493
904469


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   20303
51530073  
00016717  00000-0  10270-3 0  9032
2 25544  51
6452  43
8044 0001660  70
7995 289
3335 15
49365996 12832


Satellite: ISS
Catalog Number: 25544
Epoch time:      20303
51530073   =   yrday
fracday
Element set:     903
Inclination:       51
6452  deg
RA of node:        43
8044  deg
Eccentricity:     
0001660     
Arg of perigee:    70
7995  deg
Mean anomaly:     289
3335  deg
Mean motion:   15
49365996  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1283
Checksum:              308


Coasting Arc #5 (Orbit 1298)
---------------------------------------

Vector Time (GMT): 2020/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3114836
90                 A    =         6791285
90  meter
 Y    =        2855033
79  meter          E    =           
0004500
 Z    =        5313352
17                 I    =           51
87061
 XDOT =      -5696
036997                 Wp   =           67
08524
 YDOT =      -5092
510432  meter/sec      RA   =           38
26013  deg
 ZDOT =       -600
697489                 TA   =           28
64547
                                          MA   =           28
62076
                                          Ha   =            229
119  n
mi
                                          Hp   =            221
573

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10219281
17                 X    =        -3172341
13
 Y    =        9366908
77  feet           Y    =         2819880
06  meter
 Z    =       17432257
79                 Z    =         5298081
38
 XDOT =     -18687
785423                 XDOT =       -5635
749743
 YDOT =     -16707
711392  feet/sec       YDOT =       -5155
870535  meter/sec
 ZDOT =      -1970
792287                 ZDOT =        -628
220752

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2293423
43                 X    =          699035
46
 Y    =      -13761407
26  feet           Y    =        -4194476
93  meter
 Z    =       17361456
69                 Z    =         5291772
00
 XDOT =      24008
002565                 XDOT =        7317
639182
 YDOT =       1345
585269  feet/sec       YDOT =         410
134390  meter/sec
 ZDOT =      -2097
900151                 ZDOT =        -639
439966


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   20304
54730444  
00016717  00000-0  10270-3 0  9041
2 25544  51
6457  38
6967 0001550  72
8040 287
3279 15
49398675 12997


Satellite: ISS
Catalog Number: 25544
Epoch time:      20304
54730444   =   yrday
fracday
Element set:     904
Inclination:       51
6457  deg
RA of node:        38
6967  deg
Eccentricity:     
0001550     
Arg of perigee:    72
8040  deg
Mean anomaly:     287
3279  deg
Mean motion:   15
49398675  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1299
Checksum:              332


Coasting Arc #6 (Orbit 1313)
---------------------------------------

Vector Time (GMT): 2020/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2990759
83                 A    =         6791433
80  meter
 Y    =       -3024860
95  meter          E    =           
0016039
 Z    =       -5308192
16                 I    =           51
84367
 XDOT =       6022
562408                 Wp   =           93
32233
 YDOT =       4656
628976  meter/sec      RA   =           33
32680  deg
 ZDOT =        740
712318                 TA   =          183
74588
                                          MA   =          183
75791
                                          Ha   =            229
066  n
mi
                                          Hp   =            221
672

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9812204
16                 X    =         3050147
35
 Y    =       -9924084
48  feet           Y    =        -2991084
12  meter
 Z    =      -17415328
61                 Z    =        -5293519
54
 XDOT =      19759
063018                 XDOT =        5966
444904
 YDOT =      15277
654120  feet/sec       YDOT =        4723
663825  meter/sec
 ZDOT =       2430
158525                 ZDOT =         769
832052

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1388237
93                 X    =         -423134
92
 Y    =       13971576
64  feet           Y    =         4258536
56  meter
 Z    =      -17347285
54                 Z    =        -5287452
63
 XDOT =     -23934
423051                 XDOT =       -7295
212146
 YDOT =        801
938922  feet/sec       YDOT =         244
430983  meter/sec
 ZDOT =       2564
655080                 ZDOT =         781
706868


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   20305
51480459  
00016717  00000-0  10270-3 0  9058
2 25544  51
6459  33
9097 0001639  72
9671 287
1659 15
49375732 13147


Satellite: ISS
Catalog Number: 25544
Epoch time:      20305
51480459   =   yrday
fracday
Element set:     905
Inclination:       51
6459  deg
RA of node:        33
9097  deg
Eccentricity:     
0001639     
Arg of perigee:    72
9671  deg
Mean anomaly:     287
1659  deg
Mean motion:   15
49375732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1314
Checksum:              329


Coasting Arc #7 (Orbit 1329)
---------------------------------------

Vector Time (GMT): 2020/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2857931
52                 A    =         6791393
08  meter
 Y    =        3173178
54  meter          E    =           
0005062
 Z    =        5277135
69                 I    =           51
81529
 XDOT =      -6335
370948                 Wp   =           63
03695
 YDOT =      -4220
258209  meter/sec      RA   =           28
39048  deg
 ZDOT =       -890
472318                 TA   =           35
48017
                                          MA   =           35
44652
                                          Ha   =            229
108  n
mi
                                          Hp   =            221
521

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9376415
73                 X    =        -2918836
62
 Y    =       10410690
73  feet           Y    =         3140878
50  meter
 Z    =       17313437
29                 Z    =         5263104
66
 XDOT =     -20785
337755                 XDOT =       -6283
382350
 YDOT =     -13845
991499  feet/sec       YDOT =       -4290
814178  meter/sec
 ZDOT =      -2921
497105                 ZDOT =        -921
121752

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         500041
98                 X    =          152412
80
 Y    =      -14081869
20  feet           Y    =        -4292153
73  meter
 Z    =       17248353
03                 Z    =         5257298
00
 XDOT =      23763
888837                 XDOT =        7243
233317
 YDOT =      -2919
678926  feet/sec       YDOT =        -889
918137  meter/sec
 ZDOT =      -3063
075242                 ZDOT =        -933
625334


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   20306
54679756  
00016717  00000-0  10270-3 0  9063
2 25544  51
6462  28
8022 0001619  73
6629 286
4699 15
49414526 13300


Satellite: ISS
Catalog Number: 25544
Epoch time:      20306
54679756   =   yrday
fracday
Element set:     906
Inclination:       51
6462  deg
RA of node:        28
8022  deg
Eccentricity:     
0001619     
Arg of perigee:    73
6629  deg
Mean anomaly:     286
4699  deg
Mean motion:   15
49414526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1330
Checksum:              327


Coasting Arc #8 (Orbit 1344)
---------------------------------------

Vector Time (GMT): 2020/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2722474
13                 A    =         6791606
27  meter
 Y    =       -3337697
61  meter          E    =           
0015843
 Z    =       -5264946
40                 I    =           51
78388
 XDOT =       6588
468066                 Wp   =           95
49720
 YDOT =       3745
504306  meter/sec      RA   =           23
45335  deg
 ZDOT =       1033
610996                 TA   =          184
39960
                                          MA   =          184
41354
                                          Ha   =            229
098  n
mi
                                          Hp   =            221
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8932001
75                 X    =         2785169
79
 Y    =      -10950451
49  feet           Y    =        -3306902
24  meter
 Z    =      -17273446
19                 Z    =        -5251569
11
 XDOT =      21615
708877                 XDOT =        6541
074193
 YDOT =      12288
399955  feet/sec       YDOT =        3818
916257  meter/sec
 ZDOT =       3391
112192                 ZDOT =        1065
501141

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         432599
64                 X    =          131856
37
 Y    =       14200225
80  feet           Y    =         4328228
82  meter
 Z    =      -17211375
05                 Z    =        -5246027
11
 XDOT =     -23294
944497                 XDOT =       -7100
299083
 YDOT =       4993
626557  feet/sec       YDOT =        1522
057374  meter/sec
 ZDOT =       3538
439667                 ZDOT =        1078
516410


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   20307
51428984  
00016717  00000-0  10270-3 0  9077
2 25544  51
6448  24
0153 0001723  76
3768 283
7574 15
49379299 13452


Satellite: ISS
Catalog Number: 25544
Epoch time:      20307
51428984   =   yrday
fracday
Element set:     907
Inclination:       51
6448  deg
RA of node:        24
0153  deg
Eccentricity:     
0001723     
Arg of perigee:    76
3768  deg
Mean anomaly:     283
7574  deg
Mean motion:   15
49379299  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1345
Checksum:              333


Coasting Arc #9 (Orbit 1360)
---------------------------------------

Vector Time (GMT): 2020/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2580874
40                 A    =         6791588
52  meter
 Y    =        3480168
82  meter          E    =           
0005594
 Z    =        5226211
03                 I    =           51
75312
 XDOT =      -6827
341399                 Wp   =           62
04829
 YDOT =      -3273
693621  meter/sec      RA   =           18
51287  deg
 ZDOT =      -1188
060597                 TA   =           39
35583
                                          MA   =           39
31520
                                          Ha   =            229
084  n
mi
                                          Hp   =            221
505

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8467435
70                 X    =        -2644985
53
 Y    =       11417876
70  feet           Y    =         3450948
90  meter
 Z    =       17146361
64                 Z    =         5213518
25
 XDOT =     -22399
414038                 XDOT =       -6784
455462
 YDOT =     -10740
464637  feet/sec       YDOT =       -3349
802003  meter/sec
 ZDOT =      -3897
836603                 ZDOT =       -1221
122071

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1335619
16                 X    =         -407096
72
 Y    =      -14223163
49  feet           Y    =        -4335220
23  meter
 Z    =       17087446
71                 Z    =         5208253
76
 XDOT =      22738
522784                 XDOT =        6930
701745
 YDOT =      -7015
522518  feet/sec       YDOT =       -2138
331263  meter/sec
 ZDOT =      -4050
595561                 ZDOT =       -1234
621527


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   20308
54627477  
00016717  00000-0  10270-3 0  9080
2 25544  51
6452  18
9078 0001594  80
1633 279
9697 15
49421891 13612


Satellite: ISS
Catalog Number: 25544
Epoch time:      20308
54627477   =   yrday
fracday
Element set:     908
Inclination:       51
6452  deg
RA of node:        18
9078  deg
Eccentricity:     
0001594     
Arg of perigee:    80
1633  deg
Mean anomaly:     279
9697  deg
Mean motion:   15
49421891  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1361
Checksum:              336


Coasting Arc #10 (Orbit 1375)
---------------------------------------

Vector Time (GMT): 2020/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2432905
38                 A    =         6791830
64  meter
 Y    =       -3639491
99  meter          E    =           
0015488
 Z    =       -5206386
01                 I    =           51
72044
 XDOT =       7002
351380                 Wp   =           97
68741
 YDOT =       2773
693258  meter/sec      RA   =           13
57034  deg
 ZDOT =       1334
604184                 TA   =          185
14694
                                          MA   =          185
16288
                                          Ha   =            229
102  n
mi
                                          Hp   =            221
572

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7981973
03                 X    =         2498712
73
 Y    =      -11940590
50  feet           Y    =        -3611917
21  meter
 Z    =      -17081318
92                 Z    =        -5194408
00
 XDOT =      22973
593768                 XDOT =        6964
331767
 YDOT =       9100
043498  feet/sec       YDOT =        2851
785909  meter/sec
 ZDOT =       4378
622652                 ZDOT =        1368
527548

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2292171
76                 X    =          698653
95
 Y    =       14245439
91  feet           Y    =         4342010
08  meter
 Z    =      -17025699
44                 Z    =        -5189433
19
 XDOT =     -21901
860212                 XDOT =       -6675
686993
 YDOT =       8939
212513  feet/sec       YDOT =        2724
671974  meter/sec
 ZDOT =       4535
386439                 ZDOT =        1382
385787


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   20309
51375782  
00016717  00000-0  10270-3 0  9098
2 25544  51
6446  14
1198 0001752  79
2269 280
9079 15
49387131 13766


Satellite: ISS
Catalog Number: 25544
Epoch time:      20309
51375782   =   yrday
fracday
Element set:     909
Inclination:       51
6446  deg
RA of node:        14
1198  deg
Eccentricity:     
0001752     
Arg of perigee:    79
2269  deg
Mean anomaly:     280
9079  deg
Mean motion:   15
49387131  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1376
Checksum:              328


Coasting Arc #11 (Orbit 1391)
---------------------------------------

Vector Time (GMT): 2020/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2282426
91                 A    =         6791849
09  meter
 Y    =        3776467
43  meter          E    =           
0006401
 Z    =        5158954
34                 I    =           51
68794
 XDOT =      -7162
788166                 Wp   =           61
45740
 YDOT =      -2281
052549  meter/sec      RA   =            8
62542  deg
 ZDOT =      -1494
786173                 TA   =           42
95975
                                          MA   =           42
90978
                                          Ha   =            229
110  n
mi
                                          Hp   =            221
438

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7488277
26                 X    =        -2349546
65
 Y    =       12389985
01  feet           Y    =         3750568
04  meter
 Z    =       16925703
20                 Z    =         5147704
21
 XDOT =     -23499
961174                 XDOT =       -7129
487422
 YDOT =      -7483
768206  feet/sec       YDOT =       -2360
965682  meter/sec
 ZDOT =      -4904
154110                 ZDOT =       -1529
500209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3204828
54                 X    =         -976831
74
 Y    =      -14180320
26  feet           Y    =        -4322161
62  meter
 Z    =       16873442
01                 Z    =         5143025
12
 XDOT =      20992
638561                 XDOT =        6398
556233
 YDOT =     -10788
131321  feet/sec       YDOT =       -3288
222427  meter/sec
 ZDOT =      -5064
595462                 ZDOT =       -1543
688697


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   20310
54573258  
00016717  00000-0  10270-3 0  9103
2 25544  51
6448   9
0124 0001736  81
7332 278
4015 15
49430316 13925


Satellite: ISS
Catalog Number: 25544
Epoch time:      20310
54573258   =   yrday
fracday
Element set:     910
Inclination:       51
6448  deg
RA of node:         9
0124  deg
Eccentricity:     
0001736     
Arg of perigee:    81
7332  deg
Mean anomaly:     278
4015  deg
Mean motion:   15
49430316  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1392
Checksum:              282


Coasting Arc #12 (Orbit 1406)
---------------------------------------

Vector Time (GMT): 2020/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2118533
49                 A    =         6792130
62  meter
 Y    =       -3931283
98  meter          E    =           
0015166
 Z    =       -5131192
44                 I    =           51
65374
 XDOT =       7258
113842                 Wp   =           99
91235
 YDOT =       1768
991638  meter/sec      RA   =            3
67843  deg
 ZDOT =       1642
965750                 TA   =          185
97344
                                          MA   =          185
99155
                                          Ha   =            229
157  n
mi
                                          Hp   =            221
484

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6950569
19                 X    =         2187261
66
 Y    =      -12897913
31  feet           Y    =        -3907208
37  meter
 Z    =      -16834620
86                 Z    =        -5120734
60
 XDOT =      23812
709455                 XDOT =        7229
812280
 YDOT =       5803
778340  feet/sec       YDOT =        1849
998714  meter/sec
 ZDOT =       5390
307578                 ZDOT =        1678
154812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4187971
52                 X    =         1276493
72
 Y    =       14098283
15  feet           Y    =         4297156
71  meter
 Z    =      -16786016
38                 Z    =        -5116377
79
 XDOT =     -19830
329822                 XDOT =       -6044
284530
 YDOT =      12496
029028  feet/sec       YDOT =        3808
789648  meter/sec
 ZDOT =       5552
969002                 ZDOT =        1692
544952


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   20311
51320825  
00016717  00000-0  10270-3 0  9112
2 25544  51
6437   4
2244 0001909  83
8943 276
2425 15
49392513 14070


Satellite: ISS
Catalog Number: 25544
Epoch time:      20311
51320825   =   yrday
fracday
Element set:     911
Inclination:       51
6437  deg
RA of node:         4
2244  deg
Eccentricity:     
0001909     
Arg of perigee:    83
8943  deg
Mean anomaly:     276
2425  deg
Mean motion:   15
49392513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1407
Checksum:              286


Coasting Arc #13 (Orbit 1410)
---------------------------------------

Vector Time (GMT): 2020/311/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6792618
80                 A    =         6803041
40  meter
 Y    =          92143
70  meter          E    =           
0013347
 Z    =        -236005
81                 I    =           51
67966
 XDOT =        136
160688                 Wp   =           48
64409
 YDOT =       4755
363379  meter/sec      RA   =            2
35055  deg
 ZDOT =       6004
812091                 TA   =          308
81947
                                          MA   =          308
93856
                                          Ha   =            229
168  n
mi
                                          Hp   =            221
349

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22285494
76                 X    =         6792229
98
 Y    =         302308
71  feet           Y    =          168101
47  meter
 Z    =        -774297
28                 Z    =         -203010
34
 XDOT =        446
721416                 XDOT =          53
806252
 YDOT =      15601
585888  feet/sec       YDOT =        4756
425139  meter/sec
 ZDOT =      19700
827071                 ZDOT =        6005
273818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17625707
64                 X    =         5372315
69
 Y    =       13648521
59  feet           Y    =         4160069
38  meter
 Z    =        -621685
01                 Z    =         -189489
59
 XDOT =      -8140
159009                 XDOT =       -2481
120466
 YDOT =      11366
984329  feet/sec       YDOT =        3464
656824  meter/sec
 ZDOT =      19702
681896                 ZDOT =        6005
377442


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   20311
77120129  
00016717  00000-0  10270-3 0  9126
2 25544  51
6420   2
9480 0001996  80
8108 279
3268 15
49417454 14111


Satellite: ISS
Catalog Number: 25544
Epoch time:      20311
77120129   =   yrday
fracday
Element set:     912
Inclination:       51
6420  deg
RA of node:         2
9480  deg
Eccentricity:     
0001996     
Arg of perigee:    80
8108  deg
Mean anomaly:     279
3268  deg
Mean motion:   15
49417454  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1411
Checksum:              291


Coasting Arc #14 (Orbit 1426)
---------------------------------------

Vector Time (GMT): 2020/312/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6787551
94                 A    =         6803075
30  meter
 Y    =         361277
72  meter          E    =           
0013367
 Z    =          67378
32                 I    =           51
64728
 XDOT =       -320
203233                 Wp   =          127
07821
 YDOT =      -4743
433797  meter/sec      RA   =          357
40262  deg
 ZDOT =      -6007
059831                 TA   =           52
19757
                                          MA   =           52
07661
                                          Ha   =            229
112  n
mi
                                          Hp   =            221
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22268871
20                 X    =        -6791414
68
 Y    =        1185294
34  feet           Y    =          285352
84  meter
 Z    =         221057
49                 Z    =           34397
26
 XDOT =      -1050
535542                 XDOT =        -237
957689
 YDOT =     -15562
446840  feet/sec       YDOT =       -4746
554326  meter/sec
 ZDOT =     -19708
201545                 ZDOT =       -6008
415788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18715522
01                 X    =        -5704491
11
 Y    =      -12127693
87  feet           Y    =        -3696521
09  meter
 Z    =          68492
70                 Z    =           20876
58
 XDOT =       7520
571942                 XDOT =        2292
270328
 YDOT =     -11765
899164  feet/sec       YDOT =       -3586
246065  meter/sec
 ZDOT =     -19714
194652                 ZDOT =       -6008
886530


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   20312
80316873  
00016717  00000-0  10270-3 0  9135
2 25544  51
6435 357
8400 0001928  81
4336 278
7033 15
49411399 14278


Satellite: ISS
Catalog Number: 25544
Epoch time:      20312
80316873   =   yrday
fracday
Element set:     913
Inclination:       51
6435  deg
RA of node:       357
8400  deg
Eccentricity:     
0001928     
Arg of perigee:    81
4336  deg
Mean anomaly:     278
7033  deg
Mean motion:   15
49411399  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1427
Checksum:              307


Coasting Arc #15 (Orbit 1442)
---------------------------------------

Vector Time (GMT): 2020/313/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6743830
64                 A    =         6803027
29  meter
 Y    =        -846369
43  meter          E    =           
0013888
 Z    =          59007
76                 I    =           51
61335
 XDOT =        532
595218                 Wp   =           50
97942
 YDOT =       4728
066120  meter/sec      RA   =          352
45255  deg
 ZDOT =       6004
787538                 TA   =          309
65518
                                          MA   =          309
77762
                                          Ha   =            229
136  n
mi
                                          Hp   =            221
335

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22125428
60                 X    =         6752507
15
 Y    =       -2776802
60  feet           Y    =         -770906
57  meter
 Z    =         193595
00                 Z    =           91788
06
 XDOT =       1747
359640                 XDOT =         450
516812
 YDOT =      15512
027953  feet/sec       YDOT =        4733
562800  meter/sec
 ZDOT =      19700
746516                 ZDOT =        6007
175551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19714486
55                 X    =         6008975
50
 Y    =       10416454
53  feet           Y    =         3174935
34  meter
 Z    =         345250
15                 Z    =          105232
25
 XDOT =      -6818
527592                 XDOT =       -2078
287210
 YDOT =      12194
127409  feet/sec       YDOT =        3716
770034  meter/sec
 ZDOT =      19711
516992                 ZDOT =        6008
070379


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   20313
83513096  
00016717  00000-0  10270-3 0  9146
2 25544  51
6433 352
7325 0001962  83
9105 276
2269 15
49426897 14436


Satellite: ISS
Catalog Number: 25544
Epoch time:      20313
83513096   =   yrday
fracday
Element set:     914
Inclination:       51
6433  deg
RA of node:       352
7325  deg
Eccentricity:     
0001962     
Arg of perigee:    83
9105  deg
Mean anomaly:     276
2269  deg
Mean motion:   15
49426897  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1443
Checksum:              316


Coasting Arc #16 (Orbit 1457)
---------------------------------------

Vector Time (GMT): 2020/314/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6670217
43                 A    =         6803024
92  meter
 Y    =        1290131
83  meter          E    =           
0012843
 Z    =        -232112
15                 I    =           51
58006
 XDOT =       -711
112439                 Wp   =          129
14593
 YDOT =      -4713
838368  meter/sec      RA   =          347
50040  deg
 ZDOT =      -5996
311620                 TA   =           53
35190
                                          MA   =           53
23389
                                          Ha   =            229
129  n
mi
                                          Hp   =            221
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21883915
44                 X    =        -6683020
84
 Y    =        4232715
99  feet           Y    =         1215469
09  meter
 Z    =        -761522
79                 Z    =         -264544
91
 XDOT =      -2333
046059                 XDOT =        -629
221016
 YDOT =     -15465
348975  feet/sec       YDOT =       -4721
332511  meter/sec
 ZDOT =     -19672
938387                 ZDOT =       -5999
567179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20501864
27                 X    =        -6248968
23
 Y    =       -8731788
61  feet           Y    =        -2661449
17  meter
 Z    =        -911584
28                 Z    =         -277850
89
 XDOT =       6194
061332                 XDOT =        1887
949894
 YDOT =     -12554
120580  feet/sec       YDOT =       -3826
495953  meter/sec
 ZDOT =     -19687
725887                 ZDOT =       -6000
818850


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   20314
80259338  
00016717  00000-0  10270-3 0  9151
2 25544  51
6435 347
9442 0002011  84
8868 275
2512 15
49417269 14585


Satellite: ISS
Catalog Number: 25544
Epoch time:      20314
80259338   =   yrday
fracday
Element set:     915
Inclination:       51
6435  deg
RA of node:       347
9442  deg
Eccentricity:     
0002011     
Arg of perigee:    84
8868  deg
Mean anomaly:     275
2512  deg
Mean motion:   15
49417269  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1458
Checksum:              320
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