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

 
Date: November 23rd 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) : 75 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 497 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


328/13:07:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 222 1

335/15:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 221 8

337/17:50:56 000 0 0 0 0 0 0
N/A 0 0 0 0 229 7
000/00:00:00 000 0 0 0 0 221 9

338/19:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 221 9

Coasting Arc #1 (Orbit 1599)
---------------------------------------

Vector Time (GMT): 2020/323/21:45:59
942
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5093721
52                 A    =         6797699
43  meter
 Y    =       -2223961
22  meter          E    =           
0012173
 Z    =        3903727
48                 I    =           51
30903
 XDOT =       -267
630139                 Wp   =           93
81926
 YDOT =       6505
036025  meter/sec      RA   =          302
18393  deg
 ZDOT =       4043
400851                 TA   =          313
60349
                                          MA   =          313
70444
                                          Ha   =            229
419  n
mi
                                          Hp   =            222
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16711684
77                 X    =         5099249
66
 Y    =       -7296460
69  feet           Y    =        -2166969
11  meter
 Z    =       12807504
86                 Z    =         3928484
24
 XDOT =       -878
051636                 XDOT =        -359
992277
 YDOT =      21341
981710  feet/sec       YDOT =        6501
526292  meter/sec
 ZDOT =      13265
750823                 ZDOT =        4041
877219

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12222231
06                 X    =         3725336
03
 Y    =      -13423426
88  feet           Y    =        -4091460
51  meter
 Z    =       12922058
90                 Z    =         3938643
55
 XDOT =       6811
847220                 XDOT =        2076
251033
 YDOT =      19002
240621  feet/sec       YDOT =        5791
882941  meter/sec
 ZDOT =      13258
392771                 ZDOT =        4041
158117


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
96292059  
00016717  00000-0  10270-3 0  9009
2 25544  51
6421 302
6218 0001595  51
2603 308
8689 15
49012552 16003


Satellite: ISS
Catalog Number: 25544
Epoch time:      20323
96292059   =   yrday
fracday
Element set:     900
Inclination:       51
6421  deg
RA of node:       302
6218  deg
Eccentricity:     
0001595     
Arg of perigee:    51
2603  deg
Mean anomaly:     308
8689  deg
Mean motion:   15
49012552  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1600
Checksum:              286


Coasting Arc #2 (Orbit 1614)
---------------------------------------

Vector Time (GMT): 2020/324/21:45:59
942
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4892174
61                 A    =         6797591
25  meter
 Y    =        2628894
80  meter          E    =           
0008414
 Z    =       -3928717
94                 I    =           51
29147
 XDOT =       -273
976185                 Wp   =           69
88638
 YDOT =      -6506
634473  meter/sec      RA   =          297
21329  deg
 ZDOT =      -4016
944807                 TA   =          157
85133
                                          MA   =          157
81496
                                          Ha   =            229
593  n
mi
                                          Hp   =            222
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16050441
62                 X    =        -4902124
50
 Y    =        8624982
95  feet           Y    =         2574131
76  meter
 Z    =      -12889494
54                 Z    =        -3952506
28
 XDOT =       -898
871998                 XDOT =        -181
684505
 YDOT =     -21347
225961  feet/sec       YDOT =       -6509
181827  meter/sec
 ZDOT =     -13178
952779                 ZDOT =       -4018
052187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10828738
05                 X    =        -3300599
36
 Y    =       14556621
93  feet           Y    =         4436858
36  meter
 Z    =      -12999587
18                 Z    =        -3962274
17
 XDOT =      -8683
778665                 XDOT =       -2646
815737
 YDOT =     -18221
267670  feet/sec       YDOT =       -5553
842386  meter/sec
 ZDOT =     -13183
773470                 ZDOT =       -4018
414154


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
93063844  
00016717  00000-0  10270-3 0  9016
2 25544  51
6417 297
8343 0001767  58
2646 301
8676 15
49028315 16156


Satellite: ISS
Catalog Number: 25544
Epoch time:      20324
93063844   =   yrday
fracday
Element set:     901
Inclination:       51
6417  deg
RA of node:       297
8343  deg
Eccentricity:     
0001767     
Arg of perigee:    58
2646  deg
Mean anomaly:     301
8676  deg
Mean motion:   15
49028315  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1615
Checksum:              316


Coasting Arc #3 (Orbit 1630)
---------------------------------------

Vector Time (GMT): 2020/325/21:45:59
942
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4640117
38                 A    =         6797568
61  meter
 Y    =       -3031946
25  meter          E    =           
0012328
 Z    =        3925111
73                 I    =           51
27674
 XDOT =        827
484690                 Wp   =           95
26946
 YDOT =       6476
847224  meter/sec      RA   =          292
24184  deg
 ZDOT =       4012
770728                 TA   =          312
52534
                                          MA   =          312
62939
                                          Ha   =            229
449  n
mi
                                          Hp   =            222
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15223482
21                 X    =         4654610
61
 Y    =       -9947330
22  feet           Y    =        -2979976
42  meter
 Z    =       12877663
15                 Z    =         3947686
67
 XDOT =       2714
844782                 XDOT =         735
505275
 YDOT =      21249
498766  feet/sec       YDOT =        6485
586126  meter/sec
 ZDOT =      13165
258295                 ZDOT =        4016
567488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9254503
77                 X    =         2820772
75
 Y    =      -15567778
60  feet           Y    =        -4745058
92  meter
 Z    =       12982158
01                 Z    =         3956961
76
 XDOT =      10525
664748                 XDOT =        3208
222615
 YDOT =      17282
885589  feet/sec       YDOT =        5267
823528  meter/sec
 ZDOT =      13182
531273                 ZDOT =        4018
035532


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
96286668  
00016717  00000-0  10270-3 0  9022
2 25544  51
6414 292
7278 0001625  62
4493 297
6822 15
49036388 16316


Satellite: ISS
Catalog Number: 25544
Epoch time:      20325
96286668   =   yrday
fracday
Element set:     902
Inclination:       51
6414  deg
RA of node:       292
7278  deg
Eccentricity:     
0001625     
Arg of perigee:    62
4493  deg
Mean anomaly:     297
6822  deg
Mean motion:   15
49036388  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1631
Checksum:              332


Coasting Arc #4 (Orbit 1645)
---------------------------------------

Vector Time (GMT): 2020/326/21:45:59
942
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4375301
50                 A    =         6797492
94  meter
 Y    =        3393005
97  meter          E    =           
0008704
 Z    =       -3952680
56                 I    =           51
26412
 XDOT =      -1360
188245                 Wp   =           72
10030
 YDOT =      -6389
473514  meter/sec      RA   =          287
26985  deg
 ZDOT =      -3983
801831                 TA   =          156
04779
                                          MA   =          156
00727
                                          Ha   =            229
673  n
mi
                                          Hp   =            221
908

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14354663
70                 X    =        -4393717
97
 Y    =       11131909
34  feet           Y    =         3343975
50  meter
 Z    =      -12968112
07                 Z    =        -3973978
68
 XDOT =      -4462
559859                 XDOT =       -1269
286993
 YDOT =     -20962
839612  feet/sec       YDOT =       -6404
175587  meter/sec
 ZDOT =     -13070
215982                 ZDOT =       -3990
188775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7673564
27                 X    =        -2338902
39
 Y    =       16386738
10  feet           Y    =         4994677
77  meter
 Z    =      -13066710
84                 Z    =        -3982733
46
 XDOT =     -12201
791254                 XDOT =       -3719
105974
 YDOT =     -16147
220921  feet/sec       YDOT =       -4921
672937  meter/sec
 ZDOT =     -13099
485757                 ZDOT =       -3992
723259


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
93058046  
00016717  00000-0  10270-3 0  9038
2 25544  51
6407 287
9410 0001919  70
0338 290
1018 15
49038568 16464


Satellite: ISS
Catalog Number: 25544
Epoch time:      20326
93058046   =   yrday
fracday
Element set:     903
Inclination:       51
6407  deg
RA of node:       287
9410  deg
Eccentricity:     
0001919     
Arg of perigee:    70
0338  deg
Mean anomaly:     290
1018  deg
Mean motion:   15
49038568  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1646
Checksum:              306


Coasting Arc #5 (Orbit 1661)
---------------------------------------

Vector Time (GMT): 2020/327/21:45:59
942
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4060919
20                 A    =         6797462
22  meter
 Y    =       -3746260
44  meter          E    =           
0012448
 Z    =        3950274
16                 I    =           51
25470
 XDOT =       1900
929595                 Wp   =           97
36857
 YDOT =       6268
583480  meter/sec      RA   =          282
29668  deg
 ZDOT =       3978
269375                 TA   =          310
85239
                                          MA   =          310
96022
                                          Ha   =            229
484  n
mi
                                          Hp   =            222
066

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13323225
71                 X    =         4083320
89
 Y    =      -12290880
72  feet           Y    =        -3700723
29  meter
 Z    =       12960217
07                 Z    =         3970054
86
 XDOT =       6236
645653                 XDOT =        1811
366824
 YDOT =      20566
218767  feet/sec       YDOT =        6289
340047  meter/sec
 ZDOT =      13052
064880                 ZDOT =        3987
286220

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5936488
25                 X    =         1809441
62
 Y    =      -17057251
23  feet           Y    =        -5199050
17  meter
 Z    =       13051804
72                 Z    =         3978190
08
 XDOT =      13820
068608                 XDOT =        4212
356912
 YDOT =      14859
592005  feet/sec       YDOT =        4529
203643  meter/sec
 ZDOT =      13093
515618                 ZDOT =        3990
903560


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
96280431  
00016717  00000-0  10270-3 0  9048
2 25544  51
6402 282
8345 0001631  76
8127 283
3205 15
49048524 16624


Satellite: ISS
Catalog Number: 25544
Epoch time:      20327
96280431   =   yrday
fracday
Element set:     904
Inclination:       51
6402  deg
RA of node:       282
8345  deg
Eccentricity:     
0001631     
Arg of perigee:    76
8127  deg
Mean anomaly:     283
3205  deg
Mean motion:   15
49048524  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1662
Checksum:              296


Coasting Arc #6 (Orbit 1671)
---------------------------------------

Vector Time (GMT): 2020/328/13:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2393643
03                 A    =         6802889
42  meter
 Y    =       -6117434
67  meter          E    =           
0015711
 Z    =        1739537
53                 I    =           51
27103
 XDOT =       4070
560920                 Wp   =           65
31930
 YDOT =       3207
498374  meter/sec      RA   =          279
10819  deg
 ZDOT =       5644
744034                 TA   =          313
83646
                                          MA   =          313
96621
                                          Ha   =            229
625  n
mi
                                          Hp   =            222
055

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7853159
54                 X    =         2453422
38
 Y    =      -20070323
72  feet           Y    =        -6090333
07  meter
 Z    =        5707144
14                 Z    =         1751309
91
 XDOT =      13354
858662                 XDOT =        4006
971994
 YDOT =      10523
288627  feet/sec       YDOT =        3252
662486  meter/sec
 ZDOT =      18519
501424                 ZDOT =        5664
363108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18197109
95                 X    =         5546479
11
 Y    =       11520785
69  feet           Y    =         3511535
48  meter
 Z    =        5761787
01                 Z    =         1756192
68
 XDOT =     -12027
277083                 XDOT =       -3665
914055
 YDOT =       9634
743498  feet/sec       YDOT =        2936
669818  meter/sec
 ZDOT =      18610
087216                 ZDOT =        5672
354583


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
60794448  
00016717  00000-0  10270-3 0  9059
2 25544  51
6428 279
6468 0001807  68
3174 291
8168 15
49032069 16725


Satellite: ISS
Catalog Number: 25544
Epoch time:      20328
60794448   =   yrday
fracday
Element set:     905
Inclination:       51
6428  deg
RA of node:       279
6468  deg
Eccentricity:     
0001807     
Arg of perigee:    68
3174  deg
Mean anomaly:     291
8168  deg
Mean motion:   15
49032069  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1672
Checksum:              338


Coasting Arc #7 (Orbit 1686)
---------------------------------------

Vector Time (GMT): 2020/329/13:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1887667
58                 A    =         6802803
59  meter
 Y    =        6286013
92  meter          E    =           
0008134
 Z    =       -1782298
07                 I    =           51
26754
 XDOT =      -4316
665739                 Wp   =          128
41049
 YDOT =      -2885
399205  meter/sec      RA   =          274
13448  deg
 ZDOT =      -5627
185652                 TA   =           71
21958
                                          MA   =           71
13135
                                          Ha   =            229
666  n
mi
                                          Hp   =            222
007

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6193135
09                 X    =        -1949161
90
 Y    =       20623405
25  feet           Y    =         6264560
91  meter
 Z    =       -5847434
61                 Z    =        -1791616
81
 XDOT =     -14162
289170                 XDOT =       -4256
745530
 YDOT =      -9466
532825  feet/sec       YDOT =       -2933
335975  meter/sec
 ZDOT =     -18461
895185                 ZDOT =       -5648
009171

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19227841
01                 X    =        -5860645
94
 Y    =       -9667561
96  feet           Y    =        -2946672
89  meter
 Z    =       -5890724
38                 Z    =        -1795492
79
 XDOT =      11072
898862                 XDOT =        3375
019573
 YDOT =     -10759
592141  feet/sec       YDOT =       -3279
523685  meter/sec
 ZDOT =     -18558
068613                 ZDOT =       -5656
499313


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20329
57564948  
00016717  00000-0  10270-3 0  9067
2 25544  51
6436 274
8595 0001906  68
6032 291
5321 15
49038318 16875


Satellite: ISS
Catalog Number: 25544
Epoch time:      20329
57564948   =   yrday
fracday
Element set:     906
Inclination:       51
6436  deg
RA of node:       274
8595  deg
Eccentricity:     
0001906     
Arg of perigee:    68
6032  deg
Mean anomaly:     291
5321  deg
Mean motion:   15
49038318  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1687
Checksum:              336


Coasting Arc #8 (Orbit 1702)
---------------------------------------

Vector Time (GMT): 2020/330/13:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1338198
80                 A    =         6802821
20  meter
 Y    =       -6418710
31  meter          E    =           
0015834
 Z    =        1785258
04                 I    =           51
26570
 XDOT =       4550
235769                 Wp   =           66
36319
 YDOT =       2522
769632  meter/sec      RA   =          269
16123  deg
 ZDOT =       5626
012212                 TA   =          313
31822
                                          MA   =          313
45012
                                          Ha   =            229
683  n
mi
                                          Hp   =            221
995

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4390416
01                 X    =         1401203
41
 Y    =      -21058760
85  feet           Y    =        -6403393
41  meter
 Z    =        5857145
79                 Z    =         1791911
31
 XDOT =      14928
595042                 XDOT =        4494
358837
 YDOT =       8276
803254  feet/sec       YDOT =        2573
340941  meter/sec
 ZDOT =      18458
045315                 ZDOT =        5647
980225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20106126
81                 X    =         6128347
45
 Y    =        7624121
35  feet           Y    =         2323832
19  meter
 Z    =        5888102
92                 Z    =         1794693
77
 XDOT =      -9957
324810                 XDOT =       -3034
992602
 YDOT =      11841
076372  feet/sec       YDOT =        3609
160078  meter/sec
 ZDOT =      18559
528997                 ZDOT =        5656
944438


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20330
60786565  
00016717  00000-0  10270-3 0  9075
2 25544  51
6430 269
7538 0001936  72
3863 287
7498 15
49035713 17033


Satellite: ISS
Catalog Number: 25544
Epoch time:      20330
60786565   =   yrday
fracday
Element set:     907
Inclination:       51
6430  deg
RA of node:       269
7538  deg
Eccentricity:     
0001936     
Arg of perigee:    72
3863  deg
Mean anomaly:     287
7498  deg
Mean motion:   15
49035713  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1703
Checksum:              332


Coasting Arc #9 (Orbit 1717)
---------------------------------------

Vector Time (GMT): 2020/331/13:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -814247
26                 A    =         6802734
26  meter
 Y    =        6499106
39  meter          E    =           
0008203
 Z    =       -1830526
39                 I    =           51
26821
 XDOT =      -4741
564952                 Wp   =          129
35553
 YDOT =      -2167
297928  meter/sec      RA   =          264
18796  deg
 ZDOT =      -5607
691919                 TA   =           70
82867
                                          MA   =           70
73990
                                          Ha   =            229
670  n
mi
                                          Hp   =            221
999

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2671414
91                 X    =         -877969
91
 Y    =       21322527
53  feet           Y    =         6489644
70  meter
 Z    =       -6005664
00                 Z    =        -1834636
16
 XDOT =     -15556
315458                 XDOT =       -4689
737695
 YDOT =      -7110
557506  feet/sec       YDOT =       -2220
031407  meter/sec
 ZDOT =     -18397
939367                 ZDOT =       -5630
599263

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20738036
09                 X    =        -6320953
40
 Y    =       -5611564
54  feet           Y    =        -1710404
87  meter
 Z    =       -6024851
90                 Z    =        -1836374
86
 XDOT =       8807
640179                 XDOT =        2684
568727
 YDOT =     -12760
213249  feet/sec       YDOT =       -3889
312998  meter/sec
 ZDOT =     -18503
783742                 ZDOT =       -5639
953285


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20331
57556590  
00016717  00000-0  10270-3 0  9086
2 25544  51
6440 264
9671 0001858  76
3199 283
8158 15
49040660 17181


Satellite: ISS
Catalog Number: 25544
Epoch time:      20331
57556590   =   yrday
fracday
Element set:     908
Inclination:       51
6440  deg
RA of node:       264
9671  deg
Eccentricity:     
0001858     
Arg of perigee:    76
3199  deg
Mean anomaly:     283
8158  deg
Mean motion:   15
49040660  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1718
Checksum:              331


Coasting Arc #10 (Orbit 1733)
---------------------------------------

Vector Time (GMT): 2020/332/13:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         253463
13                 A    =         6802737
72  meter
 Y    =       -6537812
10  meter          E    =           
0015726
 Z    =        1836102
97                 I    =           51
27299
 XDOT =       4914
120478                 Wp   =           67
58505
 YDOT =       1774
031233  meter/sec      RA   =          259
21456  deg
 ZDOT =       5605
675612                 TA   =          312
67878
                                          MA   =          312
81115
                                          Ha   =            229
662  n
mi
                                          Hp   =            222
007

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         831571
96                 X    =          317633
17
 Y    =      -21449514
77  feet           Y    =        -6534619
03  meter
 Z    =        6023959
88                 Z    =         1837489
61
 XDOT =      16122
442514                 XDOT =        4866
687755
 YDOT =       5820
312443  feet/sec       YDOT =        1828
718835  meter/sec
 ZDOT =      18391
324187                 ZDOT =        5629
431914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21185665
06                 X    =         6457390
71
 Y    =        3444035
34  feet           Y    =         1049741
97  meter
 Z    =        6030547
66                 Z    =         1838110
93
 XDOT =      -7508
754663                 XDOT =       -2288
668421
 YDOT =      13605
787419  feet/sec       YDOT =        4147
044005  meter/sec
 ZDOT =      18501
112559                 ZDOT =        5639
139108


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20332
60777643  
00016717  00000-0  10270-3 0  9096
2 25544  51
6441 259
8611 0001849  78
1086 282
0271 15
49041513 17347


Satellite: ISS
Catalog Number: 25544
Epoch time:      20332
60777643   =   yrday
fracday
Element set:     909
Inclination:       51
6441  deg
RA of node:       259
8611  deg
Eccentricity:     
0001849     
Arg of perigee:    78
1086  deg
Mean anomaly:     282
0271  deg
Mean motion:   15
49041513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1734
Checksum:              307


Coasting Arc #11 (Orbit 1748)
---------------------------------------

Vector Time (GMT): 2020/333/13:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         272066
10                 A    =         6802662
86  meter
 Y    =        6528676
63  meter          E    =           
0008199
 Z    =       -1885030
82                 I    =           51
28160
 XDOT =      -5047
101801                 Wp   =          130
19594
 YDOT =      -1396
366223  meter/sec      RA   =          254
24195  deg
 ZDOT =      -5586
026785                 TA   =           70
61290
                                          MA   =           70
52429
                                          Ha   =            229
669  n
mi
                                          Hp   =            222
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         892605
31                 X    =          208196
84
 Y    =       21419542
74  feet           Y    =         6531362
12  meter
 Z    =       -6184484
33                 Z    =        -1883863
73
 XDOT =     -16558
732942                 XDOT =       -5003
977774
 YDOT =      -4581
254013  feet/sec       YDOT =       -1452
564903  meter/sec
 ZDOT =     -18326
859530                 ZDOT =       -5610
439563

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21396427
89                 X    =        -6521631
22
 Y    =       -1360549
93  feet           Y    =         -414695
62  meter
 Z    =       -6179253
95                 Z    =        -1883436
60
 XDOT =       6213
664470                 XDOT =        1893
924931
 YDOT =     -14288
352259  feet/sec       YDOT =       -4355
089769  meter/sec
 ZDOT =     -18439
702354                 ZDOT =       -5620
421278


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   20333
57546928  
00016717  00000-0  10270-3 0  9105
2 25544  51
6454 255
0744 0001807  82
9920 277
1435 15
49039882 17499


Satellite: ISS
Catalog Number: 25544
Epoch time:      20333
57546928   =   yrday
fracday
Element set:     910
Inclination:       51
6454  deg
RA of node:       255
0744  deg
Eccentricity:     
0001807     
Arg of perigee:    82
9920  deg
Mean anomaly:     277
1435  deg
Mean motion:   15
49039882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1749
Checksum:              328


Coasting Arc #12 (Orbit 1764)
---------------------------------------

Vector Time (GMT): 2020/334/13:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -827527
97                 A    =         6802637
28  meter
 Y    =       -6473600
89  meter          E    =           
0015770
 Z    =        1893558
31                 I    =           51
29136
 XDOT =       5155
970744                 Wp   =           68
78130
 YDOT =        983
315384  meter/sec      RA   =          249
26980  deg
 ZDOT =       5582
862924                 TA   =          312
14041
                                          MA   =          312
27430
                                          Ha   =            229
689  n
mi
                                          Hp   =            221
969

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2714986
79                 X    =         -764274
72
 Y    =      -21238848
07  feet           Y    =        -6482501
45  meter
 Z    =        6212461
63                 Z    =         1889691
32
 XDOT =      16915
914516                 XDOT =        5117
472869
 YDOT =       3226
100341  feet/sec       YDOT =        1040
757268  meter/sec
 ZDOT =      18316
479411                 ZDOT =        5607
815764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21400366
36                 X    =         6522831
67
 Y    =        -839094
08  feet           Y    =         -255755
88  meter
 Z    =        6194734
93                 Z    =         1888155
21
 XDOT =      -4782
920042                 XDOT =       -1457
834029
 YDOT =      14871
800651  feet/sec       YDOT =        4532
924838  meter/sec
 ZDOT =      18431
840682                 ZDOT =        5618
025040


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   20334
60767322  
00016717  00000-0  10270-3 0  9114
2 25544  51
6448 249
9686 0001918  82
1920 277
9448 15
49048989 17652


Satellite: ISS
Catalog Number: 25544
Epoch time:      20334
60767322   =   yrday
fracday
Element set:     911
Inclination:       51
6448  deg
RA of node:       249
9686  deg
Eccentricity:     
0001918     
Arg of perigee:    82
1920  deg
Mean anomaly:     277
9448  deg
Mean motion:   15
49048989  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1765
Checksum:              350


Coasting Arc #13 (Orbit 1779)
---------------------------------------

Vector Time (GMT): 2020/335/13:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1340842
36                 A    =         6802588
33  meter
 Y    =        6377373
64  meter          E    =           
0008163
 Z    =       -1944333
58                 I    =           51
30445
 XDOT =      -5228
800908                 Wp   =          131
59440
 YDOT =       -590
234633  meter/sec      RA   =          244
29952  deg
 ZDOT =      -5562
343556                 TA   =           69
89428
                                          MA   =           69
80645
                                          Ha   =            229
647  n
mi
                                          Hp   =            222
056

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4399089
11                 X    =         1278873
63
 Y    =       20923141
87  feet           Y    =         6392021
67  meter
 Z    =       -6379047
18                 Z    =        -1937969
84
 XDOT =     -17154
858623                 XDOT =       -5194
792898
 YDOT =      -1936
465333  feet/sec       YDOT =        -648
515961  meter/sec
 ZDOT =     -18249
158648                 ZDOT =       -5587
661004

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21190328
40                 X    =        -6458812
10
 Y    =        2910776
74  feet           Y    =          887204
75  meter
 Z    =       -6349760
21                 Z    =        -1935406
91
 XDOT =       3381
800382                 XDOT =        1030
772756
 YDOT =     -15298
366881  feet/sec       YDOT =       -4662
942225  meter/sec
 ZDOT =     -18366
228102                 ZDOT =       -5598
026325


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   20335
57536183  
00016717  00000-0  10270-3 0  9121
2 25544  51
6450 245
1828 0001707  91
8106 268
3240 15
49036816 17807


Satellite: ISS
Catalog Number: 25544
Epoch time:      20335
57536183   =   yrday
fracday
Element set:     912
Inclination:       51
6450  deg
RA of node:       245
1828  deg
Eccentricity:     
0001707     
Arg of perigee:    91
8106  deg
Mean anomaly:     268
3240  deg
Mean motion:   15
49036816  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1780
Checksum:              302


Coasting Arc #14 (Orbit 1780)
---------------------------------------

Vector Time (GMT): 2020/335/15:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4530619
28                 A    =         6793097
94  meter
 Y    =           4952
24  meter          E    =           
0014899
 Z    =       -5075092
45                 I    =           51
27350
 XDOT =      -1963
140933                 Wp   =          101
30053
 YDOT =      -7183
140316  meter/sec      RA   =          243
87037  deg
 ZDOT =       1747
042763                 TA   =          185
71533
                                          MA   =          185
73235
                                          Ha   =            229
570  n
mi
                                          Hp   =            221
829

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14864236
47                 X    =        -4505685
56
 Y    =          16247
51  feet           Y    =          -45572
31  meter
 Z    =      -16650565
78                 Z    =        -5097040
29
 XDOT =      -6440
751093                 XDOT =       -1891
157276
 YDOT =     -23566
733320  feet/sec       YDOT =       -7204
691311  meter/sec
 ZDOT =       5731
767594                 ZDOT =        1737
680297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6168592
92                 X    =        -1880187
12
 Y    =      -13397904
92  feet           Y    =        -4083681
42  meter
 Z    =      -16752066
61                 Z    =        -5106029
90
 XDOT =      17736
001576                 XDOT =        5405
933280
 YDOT =     -15272
480808  feet/sec       YDOT =       -4655
052150  meter/sec
 ZDOT =       5688
629413                 ZDOT =        1733
894245


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   20335
63987267  
00016717  00000-0  10270-3 0  9132
2 25544  51
6441 244
8631 0001696  85
6739 274
4605 15
49078028 17810


Satellite: ISS
Catalog Number: 25544
Epoch time:      20335
63987267   =   yrday
fracday
Element set:     913
Inclination:       51
6441  deg
RA of node:       244
8631  deg
Eccentricity:     
0001696     
Arg of perigee:    85
6739  deg
Mean anomaly:     274
4605  deg
Mean motion:   15
49078028  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1781
Checksum:              336


Coasting Arc #15 (Orbit 1796)
---------------------------------------

Vector Time (GMT): 2020/336/15:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4520237
19                 A    =         6793079
19  meter
 Y    =        -349044
41  meter          E    =           
0006706
 Z    =        5054464
00                 I    =           51
29014
 XDOT =       2548
284283                 Wp   =           62
67009
 YDOT =       7002
403342  meter/sec      RA   =          238
89983  deg
 ZDOT =      -1790
522579                 TA   =           44
77900
                                          MA   =           44
72489
                                          Ha   =            229
336  n
mi
                                          Hp   =            222
022

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14830174
52                 X    =         4499252
28
 Y    =       -1145158
84  feet           Y    =         -298613
95  meter
 Z    =       16582887
13                 Z    =         5076370
88
 XDOT =       8360
512739                 XDOT =        2478
489366
 YDOT =      22973
764246  feet/sec       YDOT =        7030
510098  meter/sec
 ZDOT =      -5874
417910                 ZDOT =       -1778
312315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7401279
93                 X    =         2255910
12
 Y    =       12770886
40  feet           Y    =         3892566
18  meter
 Z    =       16684217
89                 Z    =         5085349
61
 XDOT =     -16142
611876                 XDOT =       -4920
268100
 YDOT =      16976
947825  feet/sec       YDOT =        5174
573697  meter/sec
 ZDOT =      -5818
087419                 ZDOT =       -1773
353045


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   20336
67206973  
00016717  00000-0  10270-3 0  9146
2 25544  51
6445 239
7573 0001545  87
5930 272
5397 15
49096526 17976


Satellite: ISS
Catalog Number: 25544
Epoch time:      20336
67206973   =   yrday
fracday
Element set:     914
Inclination:       51
6445  deg
RA of node:       239
7573  deg
Eccentricity:     
0001545     
Arg of perigee:    87
5930  deg
Mean anomaly:     272
5397  deg
Mean motion:   15
49096526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1797
Checksum:              346


Coasting Arc #16 (Orbit 1811)
---------------------------------------

Vector Time (GMT): 2020/337/15:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4495514
12                 A    =         6793154
08  meter
 Y    =         707565
14  meter          E    =           
0014755
 Z    =       -5056907
07                 I    =           51
30743
 XDOT =      -3109
436479                 Wp   =          102
33008
 YDOT =      -6746
671256  meter/sec      RA   =          233
92884  deg
 ZDOT =       1821
682708                 TA   =          185
42845
                                          MA   =          185
44447
                                          Ha   =            229
541  n
mi
                                          Hp   =            221
839

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14749062
06                 X    =        -4478528
36
 Y    =        2321407
94  feet           Y    =          657388
82  meter
 Z    =      -16590902
44                 Z    =        -5078703
41
 XDOT =     -10201
563250                 XDOT =       -3042
610852
 YDOT =     -22134
748215  feet/sec       YDOT =       -6781
069837  meter/sec
 ZDOT =       5976
649305                 ZDOT =        1806
739385

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8634912
96                 X    =        -2631921
47
 Y    =      -12041837
29  feet           Y    =        -3670352
01  meter
 Z    =      -16691741
77                 Z    =        -5087642
89
 XDOT =      14316
343297                 XDOT =        4363
621437
 YDOT =     -18448
270215  feet/sec       YDOT =       -5623
032762  meter/sec
 ZDOT =       5907
651082                 ZDOT =        1800
652050


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   20337
63975290  
00016717  00000-0  10270-3 0  9159
2 25544  51
6432 234
9691 0001645  90
3615 269
7723 15
49085646 18123


Satellite: ISS
Catalog Number: 25544
Epoch time:      20337
63975290   =   yrday
fracday
Element set:     915
Inclination:       51
6432  deg
RA of node:       234
9691  deg
Eccentricity:     
0001645     
Arg of perigee:    90
3615  deg
Mean anomaly:     269
7723  deg
Mean motion:   15
49085646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1812
Checksum:              326


Coasting Arc #17 (Orbit 1813)
---------------------------------------

Vector Time (GMT): 2020/337/17:50:56
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         861054
46                 A    =         6798999
73  meter
 Y    =        5795401
19  meter          E    =           
0006881
 Z    =       -3455202
96                 I    =           51
32703
 XDOT =      -5884
578325                 Wp   =           91
47353
 YDOT =      -1827
390966  meter/sec      RA   =          233
38478  deg
 ZDOT =      -4539
592108                 TA   =          129
11648
                                          MA   =          129
05528
                                          Ha   =            229
651  n
mi
                                          Hp   =            221
882

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2824981
83                 X    =          812968
12
 Y    =       19013783
43  feet           Y    =         5804761
78  meter
 Z    =      -11335967
72                 Z    =        -3451136
16
 XDOT =     -19306
359333                 XDOT =       -5841
655544
 YDOT =      -5995
377186  feet/sec       YDOT =       -1892
955856  meter/sec
 ZDOT =     -14893
674896                 ZDOT =       -4568
073439

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4150797
95                 X    =        -1265163
22
 Y    =       18780284
44  feet           Y    =         5724230
70  meter
 Z    =      -11317262
89                 Z    =        -3449501
73
 XDOT =     -14378
784384                 XDOT =       -4382
653480
 YDOT =     -12216
558621  feet/sec       YDOT =       -3723
607068  meter/sec
 ZDOT =     -15025
392518                 ZDOT =       -4579
739640


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   20337
76877822  
00016717  00000-0  10270-3 0  9166
2 25544  51
6410 234
3280 0001969  97
4162 262
7212 15
49091621 18149


Satellite: ISS
Catalog Number: 25544
Epoch time:      20337
76877822   =   yrday
fracday
Element set:     916
Inclination:       51
6410  deg
RA of node:       234
3280  deg
Eccentricity:     
0001969     
Arg of perigee:    97
4162  deg
Mean anomaly:     262
7212  deg
Mean motion:   15
49091621  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1814
Checksum:              309


Coasting Arc #18 (Orbit 1829)
---------------------------------------

Vector Time (GMT): 2020/338/17:50:56
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1340605
93                 A    =         6798982
13  meter
 Y    =       -5686876
01  meter          E    =           
0014121
 Z    =        3465395
26                 I    =           51
34656
 XDOT =       6035
074048                 Wp   =           93
36538
 YDOT =       1346
134968  meter/sec      RA   =          228
41648  deg
 ZDOT =       4526
937321                 TA   =          307
42013
                                          MA   =          307
54855
                                          Ha   =            229
618  n
mi
                                          Hp   =            221
946

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4398313
40                 X    =        -1293746
94
 Y    =      -18657729
69  feet           Y    =        -5701606
14  meter
 Z    =       11369407
02                 Z    =         3458996
03
 XDOT =      19800
111707                 XDOT =        5997
583203
 YDOT =       4416
453306  feet/sec       YDOT =        1413
413192  meter/sec
 ZDOT =      14852
156564                 ZDOT =        4556
162694

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2227291
57                 X    =          678878
47
 Y    =      -19056899
33  feet           Y    =        -5808542
92  meter
 Z    =       11339894
81                 Z    =         3456399
94
 XDOT =      15579
489617                 XDOT =        4748
628435
 YDOT =      10772
103085  feet/sec       YDOT =        3283
337020  meter/sec
 ZDOT =      14987
347367                 ZDOT =        4568
143478


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   20338
80097072  
00016717  00000-0  10270-3 0  9174
2 25544  51
6394 229
2214 0001897 108
5953 251
5404 15
49089496 18306


Satellite: ISS
Catalog Number: 25544
Epoch time:      20338
80097072   =   yrday
fracday
Element set:     917
Inclination:       51
6394  deg
RA of node:       229
2214  deg
Eccentricity:     
0001897     
Arg of perigee:   108
5953  deg
Mean anomaly:     251
5404  deg
Mean motion:   15
49089496  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1830
Checksum:              324


Coasting Arc #19 (Orbit 1830)
---------------------------------------

Vector Time (GMT): 2020/338/19:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -13967
18                 A    =         6796021
58  meter
 Y    =       -5219210
90  meter          E    =           
0011508
 Z    =        4345507
68                 I    =           51
34033
 XDOT =       6237
182149                 Wp   =          109
30793
 YDOT =       2844
850239  meter/sec      RA   =          228
08196  deg
 ZDOT =       3425
697337                 TA   =          305
71744
                                          MA   =          305
82445
                                          Ha   =            229
563  n
mi
                                          Hp   =            221
946

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -45824
07                 X    =           23288
54
 Y    =      -17123395
34  feet           Y    =        -5219159
43  meter
 Z    =       14256914
95                 Z    =         4345529
53
 XDOT =      20463
196026                 XDOT =        6188
266428
 YDOT =       9333
498161  feet/sec       YDOT =        2914
324868  meter/sec
 ZDOT =      11239
164492                 ZDOT =        3455
876946

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1352631
34                 X    =         -412282
03
 Y    =      -17069792
83  feet           Y    =        -5202872
86  meter
 Z    =       14257101
83                 Z    =         4345564
64
 XDOT =      19749
277967                 XDOT =        6019
579924
 YDOT =       7969
489655  feet/sec       YDOT =        2429
100447  meter/sec
 ZDOT =      11378
747105                 ZDOT =        3468
242118


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   20338
86548272  
00016717  00000-0  10270-3 0  9184
2 25544  51
6415 228
9020 0001883 112
8765 247
2584 15
49099520 18316


Satellite: ISS
Catalog Number: 25544
Epoch time:      20338
86548272   =   yrday
fracday
Element set:     918
Inclination:       51
6415  deg
RA of node:       228
9020  deg
Eccentricity:     
0001883     
Arg of perigee:   112
8765  deg
Mean anomaly:     247
2584  deg
Mean motion:   15
49099520  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1831
Checksum:              324
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