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

 
Date: March 30th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19912 1579 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 865 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


093/12:44:33 314 1 5 1 5 1 5
N/A -0 0 0 0 231 0
000/00:07:06 628 -0 2 -0 0 222 0

096/04:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 231 0
000/00:00:00 000 0 0 0 0 221 7

097/14:00:43 000 0 0 0 0 0 0
N/A 0 0 0 0 230 9
000/00:00:00 000 0 0 0 0 222 0

100/06:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 231 0
000/00:00:00 000 0 0 0 0 222 0

100/08:05:06 000 0 0 0 0 0 0
N/A 0 0 0 0 230 8
000/00:00:00 000 0 0 0 0 221 9

100/14:16:50 000 0 0 0 0 0 0
N/A 0 0 0 0 230 9
000/00:00:00 000 0 0 0 0 222 0

Coasting Arc #1 (Orbit 1980)
---------------------------------------

Vector Time (GMT): 2020/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1345338
14                 A    =         6792550
14  meter
 Y    =       -3994561
34  meter          E    =           
0019602
 Z    =       -5343428
42                 I    =           51
74102
 XDOT =       7280
596651                 Wp   =           84
51889
 YDOT =       2332
018574  meter/sec      RA   =           17
21775  deg
 ZDOT =         91
845100                 TA   =          186
34526
                                          MA   =          186
37012
                                          Ha   =            230
996  n
mi
                                          Hp   =            221
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4413839
05                 X    =         1415861
96
 Y    =      -13105516
21  feet           Y    =        -3979122
66  meter
 Z    =      -17530933
15                 Z    =        -5336721
85
 XDOT =      23886
471952                 XDOT =        7253
532089
 YDOT =       7650
979573  feet/sec       YDOT =        2413
284058  meter/sec
 ZDOT =        301
329069                 ZDOT =         127
145747

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2798157
69                 X    =          852878
46
 Y    =      -13582905
27  feet           Y    =        -4140069
53  meter
 Z    =      -17499861
30                 Z    =        -5333957
72
 XDOT =      23682
806164                 XDOT =        7218
519319
 YDOT =       4291
092295  feet/sec       YDOT =        1307
924932  meter/sec
 ZDOT =        463
106528                 ZDOT =         141
154870


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   20090
51591554  
00016717  00000-0  10270-3 0  9003
2 25544  51
6438  17
7469 0005115  67
1240 293
0449 15
48928755 19819


Satellite: ISS
Catalog Number: 25544
Epoch time:      20090
51591554   =   yrday
fracday
Element set:     900
Inclination:       51
6438  deg
RA of node:        17
7469  deg
Eccentricity:     
0005115     
Arg of perigee:    67
1240  deg
Mean anomaly:     293
0449  deg
Mean motion:   15
48928755  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1981
Checksum:              316


Coasting Arc #2 (Orbit 1996)
---------------------------------------

Vector Time (GMT): 2020/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -979844
47                 A    =         6792416
83  meter
 Y    =        4090903
36  meter          E    =           
0007394
 Z    =        5326912
81                 I    =           51
70819
 XDOT =      -7477
138588                 Wp   =           74
06329
 YDOT =      -1689
077594  meter/sec      RA   =           12
28012  deg
 ZDOT =        -76
131974                 TA   =           16
67386
                                          MA   =           16
64956
                                          Ha   =            230
964  n
mi
                                          Hp   =            221
049

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3214712
83                 X    =        -1051392
47
 Y    =       13421598
96  feet           Y    =         4079546
10  meter
 Z    =       17476748
06                 Z    =         5321979
24
 XDOT =     -24531
294580                 XDOT =       -7457
325302
 YDOT =      -5541
593157  feet/sec       YDOT =       -1772
581493  meter/sec
 ZDOT =       -249
776819                 ZDOT =        -112
404886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1331277
69                 X    =         -405773
44
 Y    =       13766007
49  feet           Y    =         4195879
08  meter
 Z    =       17453800
66                 Z    =         5319918
44
 XDOT =     -24072
349479                 XDOT =       -7337
252121
 YDOT =      -1791
842687  feet/sec       YDOT =        -546
153651  meter/sec
 ZDOT =       -416
053909                 ZDOT =        -126
813231


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   20091
54820301  
00016717  00000-0  10270-3 0  9013
2 25544  51
6434  12
6423 0005008  70
1565 290
0125 15
48967147 19977


Satellite: ISS
Catalog Number: 25544
Epoch time:      20091
54820301   =   yrday
fracday
Element set:     901
Inclination:       51
6434  deg
RA of node:        12
6423  deg
Eccentricity:     
0005008     
Arg of perigee:    70
1565  deg
Mean anomaly:     290
0125  deg
Mean motion:   15
48967147  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1997
Checksum:              284


Coasting Arc #3 (Orbit 2011)
---------------------------------------

Vector Time (GMT): 2020/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         601421
69                 A    =         6792508
75  meter
 Y    =       -4177635
57  meter          E    =           
0019771
 Z    =       -5339092
05                 I    =           51
67571
 XDOT =       7576
707071                 Wp   =           86
09752
 YDOT =       1020
701757  meter/sec      RA   =            7
33888  deg
 ZDOT =         56
309393                 TA   =          184
43162
                                          MA   =          184
44916
                                          Ha   =            231
009  n
mi
                                          Hp   =            221
026

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1973168
28                 X    =          674026
75
 Y    =      -13706153
44  feet           Y    =        -4170504
17  meter
 Z    =      -17516706
20                 Z    =        -5335994
17
 XDOT =      24857
962832                 XDOT =        7564
456649
 YDOT =       3348
759045  feet/sec       YDOT =        1105
361387  meter/sec
 ZDOT =        184
742103                 ZDOT =          93
084221

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -176770
96                 X    =          -53879
79
 Y    =      -13864693
90  feet           Y    =        -4225958
70  meter
 Z    =      -17502172
62                 Z    =        -5334662
21
 XDOT =      24058
172882                 XDOT =        7332
931094
 YDOT =       -746
623320  feet/sec       YDOT =        -227
570788  meter/sec
 ZDOT =        353
364828                 ZDOT =         107
705599


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   20092
51597385  
00016717  00000-0  10270-3 0  9025
2 25544  51
6440   7
8556 0005107  74
2499 285
9214 15
48942018 20129


Satellite: ISS
Catalog Number: 25544
Epoch time:      20092
51597385   =   yrday
fracday
Element set:     902
Inclination:       51
6440  deg
RA of node:         7
8556  deg
Eccentricity:     
0005107     
Arg of perigee:    74
2499  deg
Mean anomaly:     285
9214  deg
Mean motion:   15
48942018  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2012
Checksum:              308


Coasting Arc #4 (Orbit 2027)
---------------------------------------

Vector Time (GMT): 2020/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -225054
54                 A    =         6792384
47  meter
 Y    =        4206258
47  meter          E    =           
0007303
 Z    =        5322318
26                 I    =           51
64252
 XDOT =      -7657
706299                 Wp   =           79
54701
 YDOT =       -354
148325  meter/sec      RA   =            2
39606  deg
 ZDOT =        -42
576100                 TA   =           10
86668
                                          MA   =           10
85092
                                          Ha   =            230
908  n
mi
                                          Hp   =            221
020

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -738367
90                 X    =         -297926
07
 Y    =       13800060
61  feet           Y    =         4203334
42  meter
 Z    =       17461674
09                 Z    =         5321047
96
 XDOT =     -25123
708331                 XDOT =       -7652
970164
 YDOT =      -1161
903952  feet/sec       YDOT =        -439
755761  meter/sec
 ZDOT =       -139
685367                 ZDOT =         -79
762521

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1647048
77                 X    =          502020
46
 Y    =       13729124
80  feet           Y    =         4184637
24  meter
 Z    =       17455523
04                 Z    =         5320443
42
 XDOT =     -23918
419924                 XDOT =       -7290
334393
 YDOT =       3269
490990  feet/sec       YDOT =         996
540854  meter/sec
 ZDOT =       -310
239416                 ZDOT =         -94
560974


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   20093
54825725  
00016717  00000-0  10270-3 0  9032
2 25544  51
6442   2
7503 0004895  77
5235 282
6463 15
48977249 20285


Satellite: ISS
Catalog Number: 25544
Epoch time:      20093
54825725   =   yrday
fracday
Element set:     903
Inclination:       51
6442  deg
RA of node:         2
7503  deg
Eccentricity:     
0004895     
Arg of perigee:    77
5235  deg
Mean anomaly:     282
6463  deg
Mean motion:   15
48977249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2028
Checksum:              321


Coasting Arc #5 (Orbit 2027)
---------------------------------------

Vector Time (GMT): 2020/093/12:48:06
628
Vector Time (MET): N/A
Weight (LBS)     : 939584
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         967565
13                 A    =         6793512
62  meter
 Y    =       -4159258
41  meter          E    =           
0018078
 Z    =       -5299285
15                 I    =           51
64299
 XDOT =       7564
668648                 Wp   =           91
22234
 YDOT =        856
675896  meter/sec      RA   =            2
22534  deg
 ZDOT =        710
534727                 TA   =          185
57347
                                          MA   =          185
59362
                                          Ha   =            230
958  n
mi
                                          Hp   =            221
961

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3174426
28                 X    =         1039744
03
 Y    =      -13645860
94  feet           Y    =        -4148034
95  meter
 Z    =      -17386106
15                 Z    =        -5294409
73
 XDOT =      24818
466694                 XDOT =        7551
075474
 YDOT =       2810
616458  feet/sec       YDOT =         941
193411  meter/sec
 ZDOT =       2331
150679                 ZDOT =         747
247683

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2169593
13                 X    =         -661291
99
 Y    =      -13869666
63  feet           Y    =        -4227474
39  meter
 Z    =      -17363421
41                 Z    =        -5292370
84
 XDOT =      22983
815006                 XDOT =        7005
466814
 YDOT =      -6717
304257  feet/sec       YDOT =       -2047
434338  meter/sec
 ZDOT =       2499
493853                 ZDOT =         761
845726


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   20093
54825878  
00016717  00000-0  10270-3 0  9042
2 25544  51
6452   2
7505 0003740  75
3775 284
7790 15
48662792 20281


Satellite: ISS
Catalog Number: 25544
Epoch time:      20093
54825878   =   yrday
fracday
Element set:     904
Inclination:       51
6452  deg
RA of node:         2
7505  deg
Eccentricity:     
0003740     
Arg of perigee:    75
3775  deg
Mean anomaly:     284
7790  deg
Mean motion:   15
48662792  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2028
Checksum:              327


Coasting Arc #6 (Orbit 2043)
---------------------------------------

Vector Time (GMT): 2020/094/12:48:06
628
Vector Time (MET): N/A
Weight (LBS)     : 939584
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -471421
78                 A    =         6793357
92  meter
 Y    =        4222687
51  meter          E    =           
0006608
 Z    =        5295344
34                 I    =           51
60962
 XDOT =      -7640
927822                 Wp   =           71
67245
 YDOT =       -107
088902  meter/sec      RA   =          357
28268  deg
 ZDOT =       -592
202885                 TA   =           24
00020
                                          MA   =           23
96941
                                          Ha   =            230
926  n
mi
                                          Hp   =            221
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1546659
38                 X    =         -544327
63
 Y    =       13853961
65  feet           Y    =         4217008
28  meter
 Z    =       17373176
96                 Z    =         5292877
15
 XDOT =     -25068
660834                 XDOT =       -7636
285876
 YDOT =       -351
341542  feet/sec       YDOT =        -192
509257  meter/sec
 ZDOT =      -1942
922850                 ZDOT =        -629
307941

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3984106
42                 X    =         1214355
64
 Y    =       13373690
09  feet           Y    =         4076300
74  meter
 Z    =       17361537
83                 Z    =         5291796
73
 XDOT =     -22151
838098                 XDOT =       -6751
880252
 YDOT =       9353
636257  feet/sec       YDOT =        2850
988331  meter/sec
 ZDOT =      -2113
112780                 ZDOT =        -644
076775


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   20094
58073311  
00016717  00000-0  10270-3 0  9055
2 25544  51
6456 357
6461 0003687  78
3704 281
7860 15
48691144 20449


Satellite: ISS
Catalog Number: 25544
Epoch time:      20094
58073311   =   yrday
fracday
Element set:     905
Inclination:       51
6456  deg
RA of node:       357
6461  deg
Eccentricity:     
0003687     
Arg of perigee:    78
3704  deg
Mean anomaly:     281
7860  deg
Mean motion:   15
48691144  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2044
Checksum:              318


Coasting Arc #7 (Orbit 2058)
---------------------------------------

Vector Time (GMT): 2020/095/12:48:06
628
Vector Time (MET): N/A
Weight (LBS)     : 939584
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -36845
40                 A    =         6793388
01  meter
 Y    =       -4249914
09  meter          E    =           
0018393
 Z    =       -5315691
95                 I    =           51
57539
 XDOT =       7603
967938                 Wp   =           90
86272
 YDOT =       -648
936610  meter/sec      RA   =          352
33813  deg
 ZDOT =        467
254718                 TA   =          183
60459
                                          MA   =          183
61786
                                          Ha   =            230
977  n
mi
                                          Hp   =            221
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -120883
86                 X    =           36501
50
 Y    =      -13943287
71  feet           Y    =        -4249916
31  meter
 Z    =      -17439934
22                 Z    =        -5315692
55
 XDOT =      24947
401370                 XDOT =        7608
389762
 YDOT =      -2129
057118  feet/sec       YDOT =        -563
878881  meter/sec
 ZDOT =       1532
987920                 ZDOT =         504
202270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5768342
73                 X    =        -1758190
86
 Y    =      -12695163
29  feet           Y    =        -3869485
77  meter
 Z    =      -17439617
02                 Z    =        -5315595
27
 XDOT =      20898
444550                 XDOT =        6369
845899
 YDOT =     -11829
344307  feet/sec       YDOT =       -3605
584145  meter/sec
 ZDOT =       1702
500555                 ZDOT =         518
922169


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   20095
54867848  
00016717  00000-0  10270-3 0  9069
2 25544  51
6450 352
8611 0003782  81
0068 279
1509 15
48670390 20594


Satellite: ISS
Catalog Number: 25544
Epoch time:      20095
54867848   =   yrday
fracday
Element set:     906
Inclination:       51
6450  deg
RA of node:       352
8611  deg
Eccentricity:     
0003782     
Arg of perigee:    81
0068  deg
Mean anomaly:     279
1509  deg
Mean motion:   15
48670390  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2059
Checksum:              327


Coasting Arc #8 (Orbit 2068)
---------------------------------------

Vector Time (GMT): 2020/096/04:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939584
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5153994
43                 A    =         6798828
19  meter
 Y    =       -2156222
18  meter          E    =           
0010367
 Z    =       -3884943
22                 I    =           51
57021
 XDOT =       4864
517199                 Wp   =           78
34575
 YDOT =      -4242
886992  meter/sec      RA   =          349
21640  deg
 ZDOT =      -4105
943998                 TA   =          148
43898
                                          MA   =          148
37676
                                          Ha   =            231
040  n
mi
                                          Hp   =            221
747

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16909430
54                 X    =        -5110629
17
 Y    =       -7074219
76  feet           Y    =        -2213615
62  meter
 Z    =      -12745876
70                 Z    =        -3909873
63
 XDOT =      15959
702096                 XDOT =        4931
545050
 YDOT =     -13920
232915  feet/sec       YDOT =       -4188
114014  meter/sec
 ZDOT =     -13470
944875                 ZDOT =       -4082
151167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11369162
02                 X    =         3465320
58
 Y    =      -14275570
56  feet           Y    =        -4351193
91  meter
 Z    =      -12860055
97                 Z    =        -3919745
06
 XDOT =       8009
076081                 XDOT =        2441
166389
 YDOT =      18393
792643  feet/sec       YDOT =        5606
427998  meter/sec
 ZDOT =     -13361
506101                 ZDOT =       -4072
587060


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   20096
19397380  
00016717  00000-0  10270-3 0  9071
2 25544  51
6427 349
6699 0003924  86
8672 273
2927 15
48654658 20699


Satellite: ISS
Catalog Number: 25544
Epoch time:      20096
19397380   =   yrday
fracday
Element set:     907
Inclination:       51
6427  deg
RA of node:       349
6699  deg
Eccentricity:     
0003924     
Arg of perigee:    86
8672  deg
Mean anomaly:     273
2927  deg
Mean motion:   15
48654658  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2069
Checksum:              364


Coasting Arc #9 (Orbit 2084)
---------------------------------------

Vector Time (GMT): 2020/097/04:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939584
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5403344
53                 A    =         6799116
35  meter
 Y    =        1605501
96  meter          E    =           
0015212
 Z    =        3789822
60                 I    =           51
53761
 XDOT =      -4356
826939                 Wp   =           94
92171
 YDOT =       4698
157156  meter/sec      RA   =          344
26694  deg
 ZDOT =       4205
579247                 TA   =          310
52241
                                          MA   =          310
65482
                                          Ha   =            230
934  n
mi
                                          Hp   =            221
851

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17727508
30                 X    =         5366581
03
 Y    =        5267394
87  feet           Y    =         1665720
79  meter
 Z    =       12433801
18                 Z    =         3815980
38
 XDOT =     -14294
051636                 XDOT =       -4429
467529
 YDOT =      15413
901429  feet/sec       YDOT =        4649
030238  meter/sec
 ZDOT =      13797
832176                 ZDOT =        4184
238722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9583191
48                 X    =        -2920956
76
 Y    =       15721893
73  feet           Y    =         4792033
21  meter
 Z    =       12553641
29                 Z    =         3826349
86
 XDOT =     -10100
648444                 XDOT =       -3078
677646
 YDOT =     -17136
860203  feet/sec       YDOT =       -5223
314990  meter/sec
 ZDOT =      13699
621580                 ZDOT =        4175
644657


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   20097
22644558  
00016717  00000-0  10270-3 0  9089
2 25544  51
6419 344
5656 0003856  89
2997 270
8595 15
48654684 20859


Satellite: ISS
Catalog Number: 25544
Epoch time:      20097
22644558   =   yrday
fracday
Element set:     908
Inclination:       51
6419  deg
RA of node:       344
5656  deg
Eccentricity:     
0003856     
Arg of perigee:    89
2997  deg
Mean anomaly:     270
8595  deg
Mean motion:   15
48654684  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2085
Checksum:              362


Coasting Arc #10 (Orbit 2090)
---------------------------------------

Vector Time (GMT): 2020/097/14:00:43
000
Vector Time (MET): N/A
Weight (LBS)     : 915571
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6598428
29                 A    =         6804620
60  meter
 Y    =        1071935
23  meter          E    =           
0011345
 Z    =       -1253906
85                 I    =           51
54443
 XDOT =        294
340309                 Wp   =          127
29256
 YDOT =      -4956
397693  meter/sec      RA   =          342
20582  deg
 ZDOT =      -5829
146255                 TA   =           66
32396
                                          MA   =           66
20494
                                          Ha   =            230
904  n
mi
                                          Hp   =            222
005

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21648386
77                 X    =        -6603833
83
 Y    =        3516847
86  feet           Y    =          998116
56  meter
 Z    =       -4113867
61                 Z    =        -1285972
59
 XDOT =        965
683427                 XDOT =         378
056943
 YDOT =     -16261
147287  feet/sec       YDOT =       -4952
638642  meter/sec
 ZDOT =     -19124
495587                 ZDOT =       -5827
512660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12925297
61                 X    =        -3939630
71
 Y    =       17684044
07  feet           Y    =         5390096
63  meter
 Z    =       -4260990
80                 Z    =        -1298749
99
 XDOT =      -9348
536933                 XDOT =       -2849
434057
 YDOT =     -11406
117760  feet/sec       YDOT =       -3476
584693  meter/sec
 ZDOT =     -19116
643171                 ZDOT =       -5826
752838


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   20097
61362154  
00016717  00000-0  10270-3 0  9092
2 25544  51
6439 342
6523 0003525  89
2103 270
9450 15
48638395 20914


Satellite: ISS
Catalog Number: 25544
Epoch time:      20097
61362154   =   yrday
fracday
Element set:     909
Inclination:       51
6439  deg
RA of node:       342
6523  deg
Eccentricity:     
0003525     
Arg of perigee:    89
2103  deg
Mean anomaly:     270
9450  deg
Mean motion:   15
48638395  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2091
Checksum:              310


Coasting Arc #11 (Orbit 2106)
---------------------------------------

Vector Time (GMT): 2020/098/14:00:43
000
Vector Time (MET): N/A
Weight (LBS)     : 915571
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6473063
53                 A    =         6804628
16  meter
 Y    =       -1742751
77  meter          E    =           
0016745
 Z    =        1126832
88                 I    =           51
51228
 XDOT =        296
033450                 Wp   =           64
27679
 YDOT =       4927
478376  meter/sec      RA   =          337
25093  deg
 ZDOT =       5859
280533                 TA   =          307
94990
                                          MA   =          308
10109
                                          Ha   =            230
879  n
mi
                                          Hp   =            221
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21237085
07                 X    =         6486596
87
 Y    =       -5717689
52  feet           Y    =        -1670289
58  meter
 Z    =        3696958
26                 Z    =         1158309
65
 XDOT =        971
238353                 XDOT =         212
449776
 YDOT =      16166
267638  feet/sec       YDOT =        4930
322067  meter/sec
 ZDOT =      19223
361328                 ZDOT =        5860
515056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10761305
89                 X    =         3280046
03
 Y    =      -19152313
11  feet           Y    =        -5837625
04  meter
 Z    =        3841413
09                 Z    =         1170862
71
 XDOT =      10739
623600                 XDOT =        3273
437273
 YDOT =       9929
719232  feet/sec       YDOT =        3026
578422  meter/sec
 ZDOT =      19228
667267                 ZDOT =        5860
897783


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   20098
64608809  
00016717  00000-0  10270-3 0  9108
2 25544  51
6429 337
5469 0003593  92
1418 268
0143 15
48684219 21073


Satellite: ISS
Catalog Number: 25544
Epoch time:      20098
64608809   =   yrday
fracday
Element set:     910
Inclination:       51
6429  deg
RA of node:       337
5469  deg
Eccentricity:     
0003593     
Arg of perigee:    92
1418  deg
Mean anomaly:     268
0143  deg
Mean motion:   15
48684219  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2107
Checksum:              325


Coasting Arc #12 (Orbit 2121)
---------------------------------------

Vector Time (GMT): 2020/099/14:00:43
000
Vector Time (MET): N/A
Weight (LBS)     : 915571
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6291590
28                 A    =         6804787
32  meter
 Y    =        2358816
09  meter          E    =           
0012233
 Z    =       -1051088
58                 I    =           51
48059
 XDOT =       -841
978633                 Wp   =          128
78737
 YDOT =      -4839
581867  meter/sec      RA   =          332
29536  deg
 ZDOT =      -5874
703270                 TA   =           62
60544
                                          MA   =           62
48103
                                          Ha   =            230
913  n
mi
                                          Hp   =            221
958

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20641700
39                 X    =        -6312394
02
 Y    =        7738897
94  feet           Y    =         2288342
64  meter
 Z    =       -3448453
34                 Z    =        -1081701
68
 XDOT =      -2762
397091                 XDOT =        -759
262199
 YDOT =     -15877
893263  feet/sec       YDOT =       -4848
535475  meter/sec
 ZDOT =     -19273
960860                 ZDOT =       -5878
591994

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8554298
31                 X    =        -2607350
13
 Y    =       20292988
60  feet           Y    =         6185302
93  meter
 Z    =       -3588977
67                 Z    =        -1093920
40
 XDOT =     -11860
646308                 XDOT =       -3615
124995
 YDOT =      -8381
591348  feet/sec       YDOT =       -2554
709043  meter/sec
 ZDOT =     -19291
444451                 ZDOT =       -5880
032269


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   20099
61402654  
00016717  00000-0  10270-3 0  9117
2 25544  51
6414 332
7616 0003617  95
2323 264
9240 15
48652172 21227


Satellite: ISS
Catalog Number: 25544
Epoch time:      20099
61402654   =   yrday
fracday
Element set:     911
Inclination:       51
6414  deg
RA of node:       332
7616  deg
Eccentricity:     
0003617     
Arg of perigee:    95
2323  deg
Mean anomaly:     264
9240  deg
Mean motion:   15
48652172  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2122
Checksum:              288


Coasting Arc #13 (Orbit 2131)
---------------------------------------

Vector Time (GMT): 2020/100/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915571
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1831520
39                 A    =         6797895
80  meter
 Y    =       -5021436
48  meter          E    =           
0011511
 Z    =       -4211924
46                 I    =           51
43681
 XDOT =       6689
436133                 Wp   =          105
00896
 YDOT =       -623
062209  meter/sec      RA   =          328
95864  deg
 ZDOT =       3657
144308                 TA   =          202
65979
                                          MA   =          202
71065
                                          Ha   =            231
010  n
mi
                                          Hp   =            221
957

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6008925
17                 X    =         1907994
82
 Y    =      -16474529
13  feet           Y    =        -5000527
81  meter
 Z    =      -13818649
82                 Z    =        -4202841
46
 XDOT =      21946
968939                 XDOT =        6678
141698
 YDOT =      -2044
167353  feet/sec       YDOT =        -548
319074  meter/sec
 ZDOT =      11998
504946                 ZDOT =        3689
611962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17540432
52                 X    =         5346323
83
 Y    =        1004734
27  feet           Y    =          306243
01  meter
 Z    =      -13776650
91                 Z    =        -4199123
20
 XDOT =       8436
819737                 XDOT =        2571
542656
 YDOT =      19026
197643  feet/sec       YDOT =        5799
185042  meter/sec
 ZDOT =      12147
400023                 ZDOT =        3702
527527


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   20100
25931909  
00016717  00000-0  10270-3 0  9121
2 25544  51
6404 329
5715 0003752  96
6487 263
5090 15
48648513 21329


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
25931909   =   yrday
fracday
Element set:     912
Inclination:       51
6404  deg
RA of node:       329
5715  deg
Eccentricity:     
0003752     
Arg of perigee:    96
6487  deg
Mean anomaly:     263
5090  deg
Mean motion:   15
48648513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2132
Checksum:              304


Coasting Arc #14 (Orbit 2133)
---------------------------------------

Vector Time (GMT): 2020/100/08:05:06
000
Vector Time (MET): N/A
Weight (LBS)     : 915571
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3860339
91                 A    =         6794247
94  meter
 Y    =        2368983
32  meter          E    =           
0008759
 Z    =        5058325
91                 I    =           51
42450
 XDOT =      -5478
950318                 Wp   =          113
57195
 YDOT =       5043
578312  meter/sec      RA   =          328
56810  deg
 ZDOT =       1813
335169                 TA   =          318
77965
                                          MA   =          318
84576
                                          Ha   =            230
756  n
mi
                                          Hp   =            221
896

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12665157
18                 X    =         3808991
58
 Y    =        7772254
99  feet           Y    =         2411865
62  meter
 Z    =       16595557
45                 Z    =         5076953
28
 XDOT =     -17975
558785                 XDOT =       -5543
750146
 YDOT =      16547
172939  feet/sec       YDOT =        4981
946592  meter/sec
 ZDOT =       5949
262364                 ZDOT =        1786
562533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4227539
93                 X    =         1288554
17
 Y    =       14145879
94  feet           Y    =         4311664
21  meter
 Z    =       16680787
39                 Z    =         5084304
00
 XDOT =     -23426
712551                 XDOT =       -7140
461986
 YDOT =        108
107192  feet/sec       YDOT =          32
951072  meter/sec
 ZDOT =       5826
163020                 ZDOT =        1775
814488


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   20100
38837628  
00016717  00000-0  10270-3 0  9139
2 25544  51
6421 328
9342 0003633  98
4814 261
6748 15
48698498 21347


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
38837628   =   yrday
fracday
Element set:     913
Inclination:       51
6421  deg
RA of node:       328
9342  deg
Eccentricity:     
0003633     
Arg of perigee:    98
4814  deg
Mean anomaly:     261
6748  deg
Mean motion:   15
48698498  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2134
Checksum:              330


Coasting Arc #15 (Orbit 2137)
---------------------------------------

Vector Time (GMT): 2020/100/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931488
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3897042
88                 A    =         6794430
78  meter
 Y    =        2298045
06  meter          E    =           
0008751
 Z    =        5063156
67                 I    =           51
41517
 XDOT =      -5379
201238                 Wp   =          113
77190
 YDOT =       5156
443062  meter/sec      RA   =          327
28592  deg
 ZDOT =       1793
988097                 TA   =          318
77113
                                          MA   =          318
83720
                                          Ha   =            230
873  n
mi
                                          Hp   =            221
998

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12785573
74                 X    =         3846461
59
 Y    =        7539517
91  feet           Y    =         2341342
04  meter
 Z    =       16611406
40                 Z    =         5081964
23
 XDOT =     -17648
298024                 XDOT =       -5445
176592
 YDOT =      16917
464113  feet/sec       YDOT =        5095
920219  meter/sec
 ZDOT =       5885
787720                 ZDOT =        1767
697173

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13781259
09                 X    =         4200527
77
 Y    =       -5246481
74  feet           Y    =        -1599127
64  meter
 Z    =       16697466
15                 Z    =         5089387
68
 XDOT =       1886
977863                 XDOT =         575
150853
 YDOT =      23365
541979  feet/sec       YDOT =        7121
817195  meter/sec
 ZDOT =       5764
891357                 ZDOT =        1757
138886


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   20100
64649349  
00016717  00000-0  10270-3 0  9140
2 25544  51
6402 327
6559 0003660  99
1383 261
0181 15
48628813 21384


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
64649349   =   yrday
fracday
Element set:     914
Inclination:       51
6402  deg
RA of node:       327
6559  deg
Eccentricity:     
0003660     
Arg of perigee:    99
1383  deg
Mean anomaly:     261
0181  deg
Mean motion:   15
48628813  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2138
Checksum:              308


Coasting Arc #16 (Orbit 2152)
---------------------------------------

Vector Time (GMT): 2020/101/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931488
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4166546
86                 A    =         6794442
29  meter
 Y    =       -1872723
92  meter          E    =           
0016398
 Z    =       -5044441
29                 I    =           51
38756
 XDOT =       4817
479875                 Wp   =           81
69726
 YDOT =      -5629
197251  meter/sec      RA   =          322
32612  deg
 ZDOT =      -1892
256393                 TA   =          169
85691
                                          MA   =          169
82378
                                          Ha   =            230
925  n
mi
                                          Hp   =            221
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13669773
17                 X    =        -4120792
53
 Y    =       -6144107
34  feet           Y    =        -1919061
52  meter
 Z    =      -16550004
24                 Z    =        -5064569
81
 XDOT =      15805
380168                 XDOT =        4889
260792
 YDOT =     -18468
494919  feet/sec       YDOT =       -5574
923465  meter/sec
 ZDOT =      -6208
190265                 ZDOT =       -1868
680169

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13118237
12                 X    =        -3998438
67
 Y    =        7033222
92  feet           Y    =         2143726
35  meter
 Z    =      -16642146
02                 Z    =        -5072526
11
 XDOT =      -4525
892922                 XDOT =       -1379
492163
 YDOT =     -22851
832790  feet/sec       YDOT =       -6965
238634  meter/sec
 ZDOT =      -6099
713704                 ZDOT =       -1859
192737


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   20101
61442714  
00016717  00000-0  10270-3 0  9156
2 25544  51
6398 322
8691 0003696 103
7424 256
4137 15
48670366 21535


Satellite: ISS
Catalog Number: 25544
Epoch time:      20101
61442714   =   yrday
fracday
Element set:     915
Inclination:       51
6398  deg
RA of node:       322
8691  deg
Eccentricity:     
0003696     
Arg of perigee:   103
7424  deg
Mean anomaly:     256
4137  deg
Mean motion:   15
48670366  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2153
Checksum:              305


Coasting Arc #17 (Orbit 2168)
---------------------------------------

Vector Time (GMT): 2020/102/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931488
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4382800
05                 A    =         6794672
24  meter
 Y    =        1393057
18  meter          E    =           
0009440
 Z    =        4995732
71                 I    =           51
36228
 XDOT =      -4225
467242                 Wp   =          116
27205
 YDOT =       6071
078999  meter/sec      RA   =          317
36506  deg
 ZDOT =       2007
065447                 TA   =          314
10090
                                          MA   =          314
17854
                                          Ha   =            230
839  n
mi
                                          Hp   =            221
988

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14379265
25                 X    =         4342630
08
 Y    =        4570397
57  feet           Y    =         1441844
18  meter
 Z    =       16390199
19                 Z    =         5016925
28
 XDOT =     -13863
081503                 XDOT =       -4302
791069
 YDOT =      19918
238185  feet/sec       YDOT =        6023
394479  meter/sec
 ZDOT =       6584
860390                 ZDOT =        1986
351755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12151180
29                 X    =         3703679
75
 Y    =       -8764120
92  feet           Y    =        -2671304
06  meter
 Z    =       16487250
67                 Z    =         5025314
00
 XDOT =       7126
832212                 XDOT =        2172
258458
 YDOT =      22132
581912  feet/sec       YDOT =        6746
010967  meter/sec
 ZDOT =       6489
481961                 ZDOT =        1977
994102


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   20102
64688949  
00016717  00000-0  10270-3 0  9163
2 25544  51
6398 317
7637 0003707 105
7018 254
4541 15
48640196 21694


Satellite: ISS
Catalog Number: 25544
Epoch time:      20102
64688949   =   yrday
fracday
Element set:     916
Inclination:       51
6398  deg
RA of node:       317
7637  deg
Eccentricity:     
0003707     
Arg of perigee:   105
7018  deg
Mean anomaly:     254
4541  deg
Mean motion:   15
48640196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2169
Checksum:              331


Coasting Arc #18 (Orbit 2183)
---------------------------------------

Vector Time (GMT): 2020/103/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931488
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4551658
46                 A    =         6794702
83  meter
 Y    =        -918208
83  meter          E    =           
0015928
 Z    =       -4974993
62                 I    =           51
33851
 XDOT =       3586
513003                 Wp   =           82
63408
 YDOT =      -6419
283038  meter/sec      RA   =          312
40269  deg
 ZDOT =      -2100
365852                 TA   =          166
79327
                                          MA   =          166
75152
                                          Ha   =            230
961  n
mi
                                          Hp   =            221
733

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14933262
65                 X    =        -4516886
66
 Y    =       -3012496
16  feet           Y    =         -968914
23  meter
 Z    =      -16322157
56                 Z    =        -4997019
49
 XDOT =      11766
774943                 XDOT =        3668
231204
 YDOT =     -21060
639887  feet/sec       YDOT =       -6378
719158  meter/sec
 ZDOT =      -6890
964080                 ZDOT =       -2082
745467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11051047
63                 X    =        -3368359
32
 Y    =       10327036
34  feet           Y    =         3147680
68  meter
 Z    =      -16423061
85                 Z    =        -5005749
25
 XDOT =      -9552
873033                 XDOT =       -2911
715701
 YDOT =     -21032
368302  feet/sec       YDOT =       -6410
665858  meter/sec
 ZDOT =      -6809
749327                 ZDOT =       -2075
611595


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   20103
61482054  
00016717  00000-0  10270-3 0  9171
2 25544  51
6395 312
9780 0003914 110
6729 249
4840 15
48677293 21842


Satellite: ISS
Catalog Number: 25544
Epoch time:      20103
61482054   =   yrday
fracday
Element set:     917
Inclination:       51
6395  deg
RA of node:       312
9780  deg
Eccentricity:     
0003914     
Arg of perigee:   110
6729  deg
Mean anomaly:     249
4840  deg
Mean motion:   15
48677293  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2184
Checksum:              317


Coasting Arc #19 (Orbit 2199)
---------------------------------------

Vector Time (GMT): 2020/104/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931488
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4660266
36                 A    =         6794906
57  meter
 Y    =         397162
88  meter          E    =           
0010113
 Z    =        4923018
13                 I    =           51
31678
 XDOT =      -2920
954288                 Wp   =          119
22301
 YDOT =       6730
812289  meter/sec      RA   =          307
43862  deg
 ZDOT =       2213
749294                 TA   =          309
01445
                                          MA   =          309
10445
                                          Ha   =            230
771  n
mi
                                          Hp   =            222
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15289587
80                 X    =         4631565
56
 Y    =        1303027
81  feet           Y    =          449116
74  meter
 Z    =       16151634
29                 Z    =         4945586
22
 XDOT =      -9583
183359                 XDOT =       -3006
756278
 YDOT =      22082
717482  feet/sec       YDOT =        6697
668318  meter/sec
 ZDOT =       7262
957002                 ZDOT =        2199
352117

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9664590
80                 X    =         2945767
28
 Y    =      -11777663
81  feet           Y    =        -3589831
93  meter
 Z    =       16255060
34                 Z    =         4954542
39
 XDOT =      11898
087195                 XDOT =        3626
536977
 YDOT =      19733
090123  feet/sec       YDOT =        6014
645869  meter/sec
 ZDOT =       7196
506921                 ZDOT =        2193
495310


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   20104
64728047  
00016717  00000-0  10270-3 0  9181
2 25544  51
6389 307
8729 0003751 115
0572 245
0968 15
48662581 22001


Satellite: ISS
Catalog Number: 25544
Epoch time:      20104
64728047   =   yrday
fracday
Element set:     918
Inclination:       51
6389  deg
RA of node:       307
8729  deg
Eccentricity:     
0003751     
Arg of perigee:   115
0572  deg
Mean anomaly:     245
0968  deg
Mean motion:   15
48662581  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2200
Checksum:              316
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