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

 
Date: November 13th 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) : 16464 4774 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


316/09:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 221 5

317/19:38:04 567 1 8 2 1 2 1
N/A -1 1 -0 2 229 1
000/00:06:09 133 0 2 0 1 222 6

320/00:49:49 100 0 0 0 0 0 0
N/A 0 0 0 0 228 9
000/00:00:00 000 0 0 0 0 222 6

320/09:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 222 6

323/04:57:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 8
000/00:00:00 000 0 0 0 0 222 7

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

Coasting Arc #1 (Orbit 1453)
---------------------------------------

Vector Time (GMT): 2020/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1523973
77                 A    =         6792561
41  meter
 Y    =        4340889
94  meter          E    =           
0007888
 Z    =        4992222
36                 I    =           51
55488
 XDOT =      -7378
804707                 Wp   =           64
35907
 YDOT =       -211
428340  meter/sec      RA   =          348
82406  deg
 ZDOT =      -2062
793616                 TA   =           45
77141
                                          MA   =           45
70667
                                          Ha   =            229
171  n
mi
                                          Hp   =            221
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4999913
95                 X    =        -1596651
30
 Y    =       14241764
90  feet           Y    =         4323441
26  meter
 Z    =       16378682
27                 Z    =         4984643
00
 XDOT =     -24208
676860                 XDOT =       -7365
872053
 YDOT =       -693
662533  feet/sec       YDOT =        -293
871061  meter/sec
 ZDOT =      -6767
695591                 ZDOT =       -2098
605979

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7213499
95                 X    =        -2198674
78
 Y    =      -13302162
18  feet           Y    =        -4054499
03  meter
 Z    =       16343382
14                 Z    =         4981462
88
 XDOT =      15647
553464                 XDOT =        4769
374296
 YDOT =     -17027
581695  feet/sec       YDOT =       -5190
006900  meter/sec
 ZDOT =      -6933
304231                 ZDOT =       -2113
271129


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
54471209  
00016717  00000-0  10270-3 0  9009
2 25544  51
6443 349
2217 0001951  90
2203 269
9171 15
49423190 14542


Satellite: ISS
Catalog Number: 25544
Epoch time:      20314
54471209   =   yrday
fracday
Element set:     900
Inclination:       51
6443  deg
RA of node:       349
2217  deg
Eccentricity:     
0001951     
Arg of perigee:    90
2203  deg
Mean anomaly:     269
9171  deg
Mean motion:   15
49423190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1454
Checksum:              285


Coasting Arc #2 (Orbit 1468)
---------------------------------------

Vector Time (GMT): 2020/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1310700
45                 A    =         6792877
28  meter
 Y    =       -4475993
47  meter          E    =           
0014109
 Z    =       -4951756
85                 I    =           51
52304
 XDOT =       7319
161152                 Wp   =          104
04931
 YDOT =       -293
243191  meter/sec      RA   =          343
86772  deg
 ZDOT =       2204
354481                 TA   =          187
53844
                                          MA   =          187
55967
                                          Ha   =            229
185  n
mi
                                          Hp   =            221
436

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4300198
33                 X    =         1384708
09
 Y    =      -14685017
95  feet           Y    =        -4460922
42  meter
 Z    =      -16245921
41                 Z    =        -4945210
19
 XDOT =      24012
995904                 XDOT =        7311
188667
 YDOT =       -962
083960  feet/sec       YDOT =        -211
439679  meter/sec
 ZDOT =       7232
134123                 ZDOT =        2239
889226

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8234571
92                 X    =         2509897
52
 Y    =       12935383
58  feet           Y    =         3942704
92  meter
 Z    =      -16215396
92                 Z    =        -4942452
98
 XDOT =     -13986
582119                 XDOT =       -4263
110230
 YDOT =      18167
722918  feet/sec       YDOT =        5537
521945  meter/sec
 ZDOT =       7396
474263                 ZDOT =        2254
445355


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   20315
51218874  
00016717  00000-0  10270-3 0  9015
2 25544  51
6447 344
4334 0001960  92
7037 267
4338 15
49387908 14695


Satellite: ISS
Catalog Number: 25544
Epoch time:      20315
51218874   =   yrday
fracday
Element set:     901
Inclination:       51
6447  deg
RA of node:       344
4334  deg
Eccentricity:     
0001960     
Arg of perigee:    92
7037  deg
Mean anomaly:     267
4338  deg
Mean motion:   15
49387908  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1469
Checksum:              324


Coasting Arc #3 (Orbit 1482)
---------------------------------------

Vector Time (GMT): 2020/316/09:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4702427
16                 A    =         6800008
65  meter
 Y    =       -4087370
11  meter          E    =           
0006316
 Z    =       -2725562
86                 I    =           51
51677
 XDOT =       5107
468474                 Wp   =           67
10199
 YDOT =       2450
123271  meter/sec      RA   =          339
35288  deg
 ZDOT =       5149
582490                 TA   =          262
10136
                                          MA   =          262
17305
                                          Ha   =            229
110  n
mi
                                          Hp   =            221
480

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15427910
62                 X    =         4761023
33
 Y    =      -13410006
93  feet           Y    =        -4034456
56  meter
 Z    =       -8942135
36                 Z    =        -2702577
60
 XDOT =      16756
786333                 XDOT =        5054
676695
 YDOT =       8038
462174  feet/sec       YDOT =        2506
943465  meter/sec
 ZDOT =      16894
955675                 ZDOT =        5174
264783

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10709912
72                 X    =        -3264381
40
 Y    =       17465392
79  feet           Y    =         5323451
72  meter
 Z    =       -8835627
94                 Z    =        -2693099
40
 XDOT =     -17018
815677                 XDOT =       -5187
335018
 YDOT =      -1851
426288  feet/sec       YDOT =        -564
314733  meter/sec
 ZDOT =      17008
950171                 ZDOT =        5184
328012


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   20316
41516364  
00016717  00000-0  10270-3 0  9021
2 25544  51
6438 339
9641 0001825 101
3494 258
7861 15
49413876 14833


Satellite: ISS
Catalog Number: 25544
Epoch time:      20316
41516364   =   yrday
fracday
Element set:     902
Inclination:       51
6438  deg
RA of node:       339
9641  deg
Eccentricity:     
0001825     
Arg of perigee:   101
3494  deg
Mean anomaly:     258
7861  deg
Mean motion:   15
49413876  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1483
Checksum:              318


Coasting Arc #4 (Orbit 1498)
---------------------------------------

Vector Time (GMT): 2020/317/09:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4470998
30                 A    =         6800234
76  meter
 Y    =        4417472
37  meter          E    =           
0015421
 Z    =        2577655
17                 I    =           51
48712
 XDOT =      -5161
050609                 Wp   =          102
71872
 YDOT =      -2151
740929  meter/sec      RA   =          334
39363  deg
 ZDOT =      -5241
172284                 TA   =           48
27327
                                          MA   =           48
14149
                                          Ha   =            229
064  n
mi
                                          Hp   =            221
405

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14668629
58                 X    =        -4532584
57
 Y    =       14493019
60  feet           Y    =         4367130
11  meter
 Z    =        8456873
92                 Z    =         2555786
75
 XDOT =     -16932
580737                 XDOT =       -5111
146423
 YDOT =      -7059
517484  feet/sec       YDOT =       -2209
176464  meter/sec
 ZDOT =     -17195
447125                 ZDOT =       -5266
122000

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9339959
00                 X    =         2846819
50
 Y    =      -18430555
80  feet           Y    =        -5617633
41  meter
 Z    =        8355525
49                 Z    =         2546764
17
 XDOT =      16843
732588                 XDOT =        5133
969693
 YDOT =        653
023833  feet/sec       YDOT =         199
041664  meter/sec
 ZDOT =     -17310
686063                 ZDOT =       -5276
297112


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   20317
44713090  
00016717  00000-0  10270-3 0  9031
2 25544  51
6443 334
8561 0001802  97
0739 263
0616 15
49448878 14996


Satellite: ISS
Catalog Number: 25544
Epoch time:      20317
44713090   =   yrday
fracday
Element set:     903
Inclination:       51
6443  deg
RA of node:       334
8561  deg
Eccentricity:     
0001802     
Arg of perigee:    97
0739  deg
Mean anomaly:     263
0616  deg
Mean motion:   15
49448878  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1499
Checksum:              321


Coasting Arc #5 (Orbit 1504)
---------------------------------------

Vector Time (GMT): 2020/317/19:41:09
133
Vector Time (MET): N/A
Weight (LBS)     : 938215
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -645441
73                 A    =         6792825
84  meter
 Y    =       -4338882
67  meter          E    =           
0014103
 Z    =       -5199048
32                 I    =           51
44692
 XDOT =       7091
625053                 Wp   =           99
71011
 YDOT =      -2572
507519  meter/sec      RA   =          332
36879  deg
 ZDOT =       1267
117021                 TA   =          182
51520
                                          MA   =          182
52230
                                          Ha   =            229
094  n
mi
                                          Hp   =            222
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2117590
98                 X    =         -571620
44
 Y    =      -14235179
38  feet           Y    =        -4345687
68  meter
 Z    =      -17057245
15                 Z    =        -5202004
42
 XDOT =      23266
486395                 XDOT =        7113
709463
 YDOT =      -8439
985300  feet/sec       YDOT =       -2493
080401  meter/sec
 ZDOT =       4157
208075                 ZDOT =        1301
619827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1309232
31                 X    =          399054
01
 Y    =      -14316144
12  feet           Y    =        -4363560
73  meter
 Z    =      -17070678
49                 Z    =        -5203142
80
 XDOT =      23508
064679                 XDOT =        7165
258114
 YDOT =      -2995
191492  feet/sec       YDOT =        -912
934367  meter/sec
 ZDOT =       4316
865618                 ZDOT =        1315
780640


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   20317
83412046  
00016717  00000-0  10270-3 0  9042
2 25544  51
6454 332
9419 0000171 109
0196 251
0973 15
49026549 15056


Satellite: ISS
Catalog Number: 25544
Epoch time:      20317
83412046   =   yrday
fracday
Element set:     904
Inclination:       51
6454  deg
RA of node:       332
9419  deg
Eccentricity:     
0000171     
Arg of perigee:   109
0196  deg
Mean anomaly:     251
0973  deg
Mean motion:   15
49026549  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1505
Checksum:              292


Coasting Arc #6 (Orbit 1520)
---------------------------------------

Vector Time (GMT): 2020/318/19:41:09
133
Vector Time (MET): N/A
Weight (LBS)     : 938215
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         995202
07                 A    =         6792733
46  meter
 Y    =        4272289
60  meter          E    =           
0004367
 Z    =        5183701
64                 I    =           51
41671
 XDOT =      -6858
579461                 Wp   =           55
61616
 YDOT =       3164
738555  meter/sec      RA   =          327
40916  deg
 ZDOT =      -1288
353817                 TA   =           46
82280
                                          MA   =           46
78631
                                          Ha   =            228
964  n
mi
                                          Hp   =            222
626

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3265098
67                 X    =          922173
90
 Y    =       14016698
16  feet           Y    =         4283010
20  meter
 Z    =       17006895
14                 Z    =         5188358
81
 XDOT =     -22501
901118                 XDOT =       -6887
200512
 YDOT =      10383
000508  feet/sec       YDOT =        3087
880998  meter/sec
 ZDOT =      -4226
882602                 ZDOT =       -1321
740501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         105268
49                 X    =           32085
84
 Y    =       14366370
40  feet           Y    =         4378869
70  meter
 Z    =       17028197
18                 Z    =         5190194
50
 XDOT =     -23115
151783                 XDOT =       -7045
498263
 YDOT =       5374
978096  feet/sec       YDOT =        1638
293324  meter/sec
 ZDOT =      -4381
398737                 ZDOT =       -1335
450335


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
86634965  
00016717  00000-0  10270-3 0  9053
2 25544  51
6445 327
8362 0000067 107
6085 252
5072 15
49060490 15218


Satellite: ISS
Catalog Number: 25544
Epoch time:      20318
86634965   =   yrday
fracday
Element set:     905
Inclination:       51
6445  deg
RA of node:       327
8362  deg
Eccentricity:     
0000067     
Arg of perigee:   107
6085  deg
Mean anomaly:     252
5072  deg
Mean motion:   15
49060490  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1521
Checksum:              305


Coasting Arc #7 (Orbit 1535)
---------------------------------------

Vector Time (GMT): 2020/319/19:41:09
133
Vector Time (MET): N/A
Weight (LBS)     : 938215
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1350711
77                 A    =         6792825
70  meter
 Y    =       -4187371
46  meter          E    =           
0013936
 Z    =       -5187730
85                 I    =           51
38887
 XDOT =       6552
685047                 Wp   =          100
03001
 YDOT =      -3726
046430  meter/sec      RA   =          322
44712  deg
 ZDOT =       1302
068361                 TA   =          182
54816
                                          MA   =          182
55527
                                          Ha   =            229
033  n
mi
                                          Hp   =            222
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4431469
07                 X    =        -1278587
14
 Y    =      -13738095
36  feet           Y    =        -4202072
53  meter
 Z    =      -17020114
35                 Z    =        -5194117
33
 XDOT =      21498
310522                 XDOT =        6587
538918
 YDOT =     -12224
561779  feet/sec       YDOT =       -3652
574796  meter/sec
 ZDOT =       4271
877825                 ZDOT =        1333
984150

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1550567
30                 X    =         -472612
91
 Y    =      -14316796
08  feet           Y    =        -4363759
44  meter
 Z    =      -17049415
40                 Z    =        -5196661
81
 XDOT =      22397
423204                 XDOT =        6826
734593
 YDOT =      -7686
483169  feet/sec       YDOT =       -2342
840070  meter/sec
 ZDOT =       4419
614980                 ZDOT =        1347
098646


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
83406511  
00016717  00000-0  10270-3 0  9066
2 25544  51
6445 323
0493 0000059 139
7076 220
4079 15
49036081 15364


Satellite: ISS
Catalog Number: 25544
Epoch time:      20319
83406511   =   yrday
fracday
Element set:     906
Inclination:       51
6445  deg
RA of node:       323
0493  deg
Eccentricity:     
0000059     
Arg of perigee:   139
7076  deg
Mean anomaly:     220
4079  deg
Mean motion:   15
49036081  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1536
Checksum:              294


Coasting Arc #8 (Orbit 1539)
---------------------------------------

Vector Time (GMT): 2020/320/00:49:49
100
Vector Time (MET): N/A
Weight (LBS)     : 938215
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5799189
92                 A    =         6799422
03  meter
 Y    =       -1241975
14  meter          E    =           
0012563
 Z    =        3314709
00                 I    =           51
40072
 XDOT =      -1416
373403                 Wp   =           90
52671
 YDOT =       5903
893298  meter/sec      RA   =          321
41444  deg
 ZDOT =       4674
582846                 TA   =          308
10123
                                          MA   =          308
21444
                                          Ha   =            228
947  n
mi
                                          Hp   =            222
627

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19026213
65                 X    =         5796545
61
 Y    =       -4074721
57  feet           Y    =        -1177139
43  meter
 Z    =       10875029
54                 Z    =         3342873
55
 XDOT =      -4646
894366                 XDOT =       -1504
994386
 YDOT =      19369
728669  feet/sec       YDOT =        5887
558586  meter/sec
 ZDOT =      15336
557893                 ZDOT =        4667
487575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3945192
83                 X    =         1202494
77
 Y    =      -18978551
48  feet           Y    =        -5784662
49  meter
 Z    =       11005292
66                 Z    =         3354413
20
 XDOT =      14405
491381                 XDOT =        4390
793773
 YDOT =      11897
898134  feet/sec       YDOT =        3626
479351  meter/sec
 ZDOT =      15303
445355                 ZDOT =        4664
490144


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
09212107  
00016717  00000-0  10270-3 0  9073
2 25544  51
6399 321
7679 0000444 173
5347 186
5809 15
49039489 15401


Satellite: ISS
Catalog Number: 25544
Epoch time:      20320
09212107   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:       321
7679  deg
Eccentricity:     
0000444     
Arg of perigee:   173
5347  deg
Mean anomaly:     186
5809  deg
Mean motion:   15
49039489  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1540
Checksum:              318


Coasting Arc #9 (Orbit 1544)
---------------------------------------

Vector Time (GMT): 2020/320/09:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965221
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -491289
97                 A    =         6794207
65  meter
 Y    =       -4709203
55  meter          E    =           
0012062
 Z    =       -4884072
93                 I    =           51
37689
 XDOT =       6571
401297                 Wp   =          107
52020
 YDOT =      -3128
682939  meter/sec      RA   =          319
54606  deg
 ZDOT =       2356
922306                 TA   =          185
69750
                                          MA   =          185
71124
                                          Ha   =            229
124  n
mi
                                          Hp   =            222
627

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1611843
73                 X    =         -414868
98
 Y    =      -15450142
88  feet           Y    =        -4714269
84  meter
 Z    =      -16023861
32                 Z    =        -4886274
23
 XDOT =      21559
715542                 XDOT =        6594
449854
 YDOT =     -10264
707805  feet/sec       YDOT =       -3055
068119  meter/sec
 ZDOT =       7732
684730                 ZDOT =        2388
900293

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6458462
55                 X    =         1968539
39
 Y    =       14116478
90  feet           Y    =         4302702
77  meter
 Z    =      -16033788
45                 Z    =        -4887098
72
 XDOT =     -15954
038369                 XDOT =       -4862
790895
 YDOT =      16245
443917  feet/sec       YDOT =        4951
611306  meter/sec
 ZDOT =       7880
674302                 ZDOT =        2402
029527


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
41469259  
00016717  00000-0  10270-3 0  9082
2 25544  51
6436 320
1750 0000259 137
7585 222
3585 15
49010999 15456


Satellite: ISS
Catalog Number: 25544
Epoch time:      20320
41469259   =   yrday
fracday
Element set:     908
Inclination:       51
6436  deg
RA of node:       320
1750  deg
Eccentricity:     
0000259     
Arg of perigee:   137
7585  deg
Mean anomaly:     222
3585  deg
Mean motion:   15
49010999  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1545
Checksum:              312


Coasting Arc #10 (Orbit 1560)
---------------------------------------

Vector Time (GMT): 2020/321/09:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965221
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         868643
97                 A    =         6794123
52  meter
 Y    =        4659467
49  meter          E    =           
0007104
 Z    =        4863621
93                 I    =           51
35191
 XDOT =      -6291
415813                 Wp   =           61
19619
 YDOT =       3667
840197  meter/sec      RA   =          314
58118  deg
 ZDOT =      -2384
218440                 TA   =           52
31344
                                          MA   =           52
24903
                                          Ha   =            229
045  n
mi
                                          Hp   =            222
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2849881
81                 X    =          792850
54
 Y    =       15286966
82  feet           Y    =         4668756
99  meter
 Z    =       15956764
85                 Z    =         4867657
96
 XDOT =     -20641
127995                 XDOT =       -6320
381650
 YDOT =      12033
596447  feet/sec       YDOT =        3597
323360  meter/sec
 ZDOT =      -7822
238975                 ZDOT =       -2414
850441

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7808114
31                 X    =        -2379913
24
 Y    =      -13426039
66  feet           Y    =        -4092256
89  meter
 Z    =       15975178
73                 Z    =         4869234
48
 XDOT =      14245
167684                 XDOT =        4341
927110
 YDOT =     -17784
060841  feet/sec       YDOT =       -5420
581744  meter/sec
 ZDOT =      -7964
031210                 ZDOT =       -2427
436713


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
44691585  
00016717  00000-0  10270-3 0  9096
2 25544  51
6435 315
0690 0000273 120
8494 239
2683 15
49051579 15612


Satellite: ISS
Catalog Number: 25544
Epoch time:      20321
44691585   =   yrday
fracday
Element set:     909
Inclination:       51
6435  deg
RA of node:       315
0690  deg
Eccentricity:     
0000273     
Arg of perigee:   120
8494  deg
Mean anomaly:     239
2683  deg
Mean motion:   15
49051579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1561
Checksum:              312


Coasting Arc #11 (Orbit 1575)
---------------------------------------

Vector Time (GMT): 2020/322/09:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965221
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1258561
92                 A    =         6794250
13  meter
 Y    =       -4585097
65  meter          E    =           
0011952
 Z    =       -4864611
37                 I    =           51
33021
 XDOT =       5945
928021                 Wp   =          107
19416
 YDOT =      -4174
375170  meter/sec      RA   =          309
61446  deg
 ZDOT =       2397
644791                 TA   =          186
46429
                                          MA   =          186
47972
                                          Ha   =            229
120  n
mi
                                          Hp   =            222
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4129140
16                 X    =        -1183566
46
 Y    =      -15042971
30  feet           Y    =        -4598751
89  meter
 Z    =      -15960011
04                 Z    =        -4870543
49
 XDOT =      19507
637865                 XDOT =        5980
518612
 YDOT =     -13695
456593  feet/sec       YDOT =       -4107
690415  meter/sec
 ZDOT =       7866
288686                 ZDOT =        2426
611880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9144659
21                 X    =         2787292
13
 Y    =       12603468
14  feet           Y    =         3841537
09  meter
 Z    =      -15987199
11                 Z    =        -4872898
29
 XDOT =     -12333
105387                 XDOT =       -3759
130522
 YDOT =      19090
832030  feet/sec       YDOT =        5818
885603  meter/sec
 ZDOT =       8000
407778                 ZDOT =        2438
524291


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
41462426  
00016717  00000-0  10270-3 0  9106
2 25544  51
6446 310
2820 0000204 109
3445 250
7728 15
49016272 15763


Satellite: ISS
Catalog Number: 25544
Epoch time:      20322
41462426   =   yrday
fracday
Element set:     910
Inclination:       51
6446  deg
RA of node:       310
2820  deg
Eccentricity:     
0000204     
Arg of perigee:   109
3445  deg
Mean anomaly:     250
7728  deg
Mean motion:   15
49016272  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1576
Checksum:              273


Coasting Arc #12 (Orbit 1588)
---------------------------------------

Vector Time (GMT): 2020/323/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965221
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2773159
31                 A    =         6792434
93  meter
 Y    =        3323941
21  meter          E    =           
0003349
 Z    =        5231955
60                 I    =           51
30814
 XDOT =      -5028
456628                 Wp   =           62
62098
 YDOT =       5702
305070  meter/sec      RA   =          305
62983  deg
 ZDOT =       -955
480661                 TA   =           36
58336
                                          MA   =           36
56049
                                          Ha   =            228
838  n
mi
                                          Hp   =            222
655

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9098291
71                 X    =         2710369
66
 Y    =       10905318
92  feet           Y    =         3354600
95  meter
 Z    =       17165208
65                 Z    =         5245274
62
 XDOT =     -16497
561116                 XDOT =       -5087
206553
 YDOT =      18708
349967  feet/sec       YDOT =        5645
744885  meter/sec
 ZDOT =      -3134
779071                 ZDOT =        -980
049308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2297747
17                 X    =          700353
34
 Y    =      -13939634
56  feet           Y    =        -4248800
61  meter
 Z    =       17226613
92                 Z    =         5250671
92
 XDOT =      23912
155989                 XDOT =        7288
425146
 YDOT =        -81
114486  feet/sec       YDOT =         -24
723695  meter/sec
 ZDOT =      -3248
637995                 ZDOT =        -990
184861


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
25330247  
00016717  00000-0  10270-3 0  9115
2 25544  51
6448 306
1313 0000379 190
2422 169
8720 15
49071328 15892


Satellite: ISS
Catalog Number: 25544
Epoch time:      20323
25330247   =   yrday
fracday
Element set:     911
Inclination:       51
6448  deg
RA of node:       306
1313  deg
Eccentricity:     
0000379     
Arg of perigee:   190
2422  deg
Mean anomaly:     169
8720  deg
Mean motion:   15
49071328  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1589
Checksum:              291


Coasting Arc #13 (Orbit 1603)
---------------------------------------

Vector Time (GMT): 2020/324/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965221
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3041512
52                 A    =         6792543
77  meter
 Y    =       -3098831
76  meter          E    =           
0014299
 Z    =       -5236136
87                 I    =           51
28898
 XDOT =       4522
546089                 Wp   =           98
87719
 YDOT =      -6091
341704  meter/sec      RA   =          300
66149  deg
 ZDOT =        978
084038                 TA   =          180
55313
                                          MA   =          180
55471
                                          Ha   =            228
994  n
mi
                                          Hp   =            222
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9978715
61                 X    =        -2981199
98
 Y    =      -10166770
87  feet           Y    =        -3132506
32  meter
 Z    =      -17178926
72                 Z    =        -5250765
35
 XDOT =      14837
749635                 XDOT =        4585
574169
 YDOT =     -19984
716875  feet/sec       YDOT =       -6040
415046  meter/sec
 ZDOT =       3208
937134                 ZDOT =        1000
205417

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -919311
31                 X    =         -280206
09
 Y    =       14133998
39  feet           Y    =         4308042
71  meter
 Z    =      -17246404
69                 Z    =        -5256704
15
 XDOT =     -23727
665197                 XDOT =       -7232
192352
 YDOT =       2496
849773  feet/sec       YDOT =         761
039811  meter/sec
 ZDOT =       3311
491590                 ZDOT =        1009
342637


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
22100823  
00016717  00000-0  10270-3 0  9129
2 25544  51
6443 301
3454 0000342 189
3937 170
7207 15
49042540 16043


Satellite: ISS
Catalog Number: 25544
Epoch time:      20324
22100823   =   yrday
fracday
Element set:     912
Inclination:       51
6443  deg
RA of node:       301
3454  deg
Eccentricity:     
0000342     
Arg of perigee:   189
3937  deg
Mean anomaly:     170
7207  deg
Mean motion:   15
49042540  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1604
Checksum:              266


Coasting Arc #14 (Orbit 1619)
---------------------------------------

Vector Time (GMT): 2020/325/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965221
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3275851
15                 A    =         6792439
88  meter
 Y    =        2849168
31  meter          E    =           
0003400
 Z    =        5221517
44                 I    =           51
27360
 XDOT =      -4003
116078                 Wp   =           59
72338
 YDOT =       6455
309590  meter/sec      RA   =          295
69072  deg
 ZDOT =      -1008
764348                 TA   =           40
00436
                                          MA   =           39
97931
                                          Ha   =            228
767  n
mi
                                          Hp   =            222
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10747543
14                 X    =         3218384
11
 Y    =        9347665
05  feet           Y    =         2885479
40  meter
 Z    =       17130962
72                 Z    =         5237291
04
 XDOT =     -13133
582932                 XDOT =       -4070
103750
 YDOT =      21178
837238  feet/sec       YDOT =        6410
169418  meter/sec
 ZDOT =      -3309
594317                 ZDOT =       -1028
372128

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -447558
88                 X    =         -136415
95
 Y    =      -14148813
13  feet           Y    =        -4312558
24  meter
 Z    =       17203755
03                 Z    =         5243704
53
 XDOT =      23386
661168                 XDOT =        7128
254324
 YDOT =      -4883
180320  feet/sec       YDOT =       -1488
393362  meter/sec
 ZDOT =      -3400
531280                 ZDOT =       -1036
481934


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
25322186  
00016717  00000-0  10270-3 0  9132
2 25544  51
6451 296
2392 0000320 211
1433 148
9698 15
49080290 16209


Satellite: ISS
Catalog Number: 25544
Epoch time:      20325
25322186   =   yrday
fracday
Element set:     913
Inclination:       51
6451  deg
RA of node:       296
2392  deg
Eccentricity:     
0000320     
Arg of perigee:   211
1433  deg
Mean anomaly:     148
9698  deg
Mean motion:   15
49080290  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1620
Checksum:              285


Coasting Arc #15 (Orbit 1634)
---------------------------------------

Vector Time (GMT): 2020/326/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965221
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3503768
29                 A    =         6792583
77  meter
 Y    =       -2586777
44  meter          E    =           
0014229
 Z    =       -5225202
09                 I    =           51
25880
 XDOT =       3442
118908                 Wp   =           98
53477
 YDOT =      -6752
439854  meter/sec      RA   =          290
71982  deg
 ZDOT =       1035
089707                 TA   =          181
45363
                                          MA   =          181
45777
                                          Ha   =            228
998  n
mi
                                          Hp   =            222
550

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11495302
77                 X    =        -3449200
58
 Y    =       -8486802
63  feet           Y    =        -2625653
58  meter
 Z    =      -17143051
48                 Z    =        -5242089
78
 XDOT =      11293
041036                 XDOT =        3512
343009
 YDOT =     -22153
674062  feet/sec       YDOT =       -6713
555043  meter/sec
 ZDOT =       3395
963607                 ZDOT =        1051
980294

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1829351
51                 X    =          557586
34
 Y    =       14076297
80  feet           Y    =         4290455
57  meter
 Z    =      -17221014
26                 Z    =        -5248965
15
 XDOT =     -22721
632441                 XDOT =       -6925
553568
 YDOT =       7201
976923  feet/sec       YDOT =        2195
162566  meter/sec
 ZDOT =       3474
334548                 ZDOT =        1058
977170


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
22092171  
00016717  00000-0  10270-3 0  9149
2 25544  51
6438 291
4531 0000145 197
1841 162
9305 15
49040496 16358


Satellite: ISS
Catalog Number: 25544
Epoch time:      20326
22092171   =   yrday
fracday
Element set:     914
Inclination:       51
6438  deg
RA of node:       291
4531  deg
Eccentricity:     
0000145     
Arg of perigee:   197
1841  deg
Mean anomaly:     162
9305  deg
Mean motion:   15
49040496  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1635
Checksum:              291


Coasting Arc #16 (Orbit 1650)
---------------------------------------

Vector Time (GMT): 2020/327/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965221
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3694772
23                 A    =         6792482
48  meter
 Y    =        2305760
85  meter          E    =           
0003587
 Z    =        5210111
00                 I    =           51
24784
 XDOT =      -2871
930036                 Wp   =           58
54043
 YDOT =       7023
045196  meter/sec      RA   =          285
74765  deg
 ZDOT =      -1069
056358                 TA   =           41
77901
                                          MA   =           41
75162
                                          Ha   =            228
772  n
mi
                                          Hp   =            222
662

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12121956
14                 X    =         3643406
03
 Y    =        7564832
18  feet           Y    =         2346790
91  meter
 Z    =       17093540
02                 Z    =         5227934
24
 XDOT =      -9422
342639                 XDOT =       -2945
057512
 YDOT =      23041
486863  feet/sec       YDOT =        6990
520397  meter/sec
 ZDOT =      -3507
402748                 ZDOT =       -1083
184323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3166069
85                 X    =         -965018
09
 Y    =      -13831988
29  feet           Y    =        -4215990
03  meter
 Z    =       17175846
96                 Z    =         5235198
15
 XDOT =      21910
388281                 XDOT =        6678
286348
 YDOT =      -9461
607298  feet/sec       YDOT =       -2883
897904  meter/sec
 ZDOT =      -3572
993738                 ZDOT =       -1089
048491


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
25313083  
00016717  00000-0  10270-3 0  9152
2 25544  51
6436 286
3474 0000232 209
9649 150
1488 15
49078583 16517


Satellite: ISS
Catalog Number: 25544
Epoch time:      20327
25313083   =   yrday
fracday
Element set:     915
Inclination:       51
6436  deg
RA of node:       286
3474  deg
Eccentricity:     
0000232     
Arg of perigee:   209
9649  deg
Mean anomaly:     150
1488  deg
Mean motion:   15
49078583  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1651
Checksum:              313


Coasting Arc #17 (Orbit 1665)
---------------------------------------

Vector Time (GMT): 2020/328/04:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965221
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3878246
17                 A    =         6792630
24  meter
 Y    =       -2011978
90  meter          E    =           
0014148
 Z    =       -5213594
85                 I    =           51
23898
 XDOT =       2271
385782                 Wp   =           98
99176
 YDOT =      -7221
601583  meter/sec      RA   =          280
77442  deg
 ZDOT =       1097
666465                 TA   =          181
61011
                                          MA   =          181
61467
                                          Ha   =            228
994  n
mi
                                          Hp   =            222
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12723904
75                 X    =        -3830134
51
 Y    =       -6600980
63  feet           Y    =        -2055078
95  meter
 Z    =      -17104969
98                 Z    =        -5232317
25
 XDOT =       7452
053090                 XDOT =        2346
639226
 YDOT =     -23692
918580  feet/sec       YDOT =       -7195
780604  meter/sec
 ZDOT =       3601
267931                 ZDOT =        1108
882462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4505539
09                 X    =         1373288
31
 Y    =       13498326
42  feet           Y    =         4114289
89  meter
 Z    =      -17191451
26                 Z    =        -5239954
34
 XDOT =     -20796
222577                 XDOT =       -6338
688642
 YDOT =      11592
761495  feet/sec       YDOT =        3533
473704  meter/sec
 ZDOT =       3653
384524                 ZDOT =        1113
551603


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
22082655  
00016717  00000-0  10270-3 0  9169
2 25544  51
6427 281
5606 0000140 205
6833 154
4310 15
49038139 16667


Satellite: ISS
Catalog Number: 25544
Epoch time:      20328
22082655   =   yrday
fracday
Element set:     916
Inclination:       51
6427  deg
RA of node:       281
5606  deg
Eccentricity:     
0000140     
Arg of perigee:   205
6833  deg
Mean anomaly:     154
4310  deg
Mean motion:   15
49038139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1666
Checksum:              290


Coasting Arc #18 (Orbit 1670)
---------------------------------------

Vector Time (GMT): 2020/328/12:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965221
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1098235
23                 A    =         6801337
08  meter
 Y    =       -6197509
66  meter          E    =           
0005268
 Z    =       -2575636
45                 I    =           51
26546
 XDOT =       4724
619780                 Wp   =           50
29750
 YDOT =      -3003
351610  meter/sec      RA   =          279
11374  deg
 ZDOT =       5222
596544                 TA   =          280
65586
                                          MA   =          280
71518
                                          Ha   =            229
006  n
mi
                                          Hp   =            222
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3603133
96                 X    =        -1016340
10
 Y    =      -20333036
95  feet           Y    =        -6209332
89  meter
 Z    =       -8450250
81                 Z    =        -2580772
68
 XDOT =      15500
721063                 XDOT =        4732
484417
 YDOT =      -9853
515780  feet/sec       YDOT =       -2950
473799  meter/sec
 ZDOT =      17134
503098                 ZDOT =        5245
566054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20581823
45                 X    =         6273339
79
 Y    =        1550932
05  feet           Y    =          472724
09  meter
 Z    =       -8473774
71                 Z    =        -2582806
53
 XDOT =       5891
359103                 XDOT =        1795
686255
 YDOT =      15828
945296  feet/sec       YDOT =        4824
662526  meter/sec
 ZDOT =      17240
799911                 ZDOT =        5254
995813


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
54339156  
00016717  00000-0  10270-3 0  9176
2 25544  51
6420 279
9658 0000188   7
7488 352
3665 15
49043585 16716


Satellite: ISS
Catalog Number: 25544
Epoch time:      20328
54339156   =   yrday
fracday
Element set:     917
Inclination:       51
6420  deg
RA of node:       279
9658  deg
Eccentricity:     
0000188     
Arg of perigee:     7
7488  deg
Mean anomaly:     352
3665  deg
Mean motion:   15
49043585  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1671
Checksum:              336
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