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

 
Date: April 5th 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


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 0 221 9

100/08:05:06 000 0 0 0 0 0 0
N/A 0 0 0 0 230 7
000/00:00:00 000 0 0 0 0 221 8

100/14:16:50 000 0 0 0 0 0 0
N/A 0 0 0 0 230 8
000/00:00:00 000 0 0 0 0 222 0

108/01:53:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 5
000/00:00:00 000 0 0 0 0 222 0

Coasting Arc #1 (Orbit 2042)
---------------------------------------

Vector Time (GMT): 2020/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -263400
11                 A    =         6793237
22  meter
 Y    =       -4218726
76  meter          E    =           
0018641
 Z    =       -5334144
33                 I    =           51
61007
 XDOT =       7635
429343                 Wp   =           87
00530
 YDOT =       -392
150125  meter/sec      RA   =          357
45263  deg
 ZDOT =        -66
140044                 TA   =          182
35793
                                          MA   =          182
36673
                                          Ha   =            230
970  n
mi
                                          Hp   =            221
811

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -864173
59                 X    =         -190295
47
 Y    =      -13840967
05  feet           Y    =        -4221263
71  meter
 Z    =      -17500473
53                 Z    =        -5335246
11
 XDOT =      25050
621204                 XDOT =        7639
568271
 YDOT =      -1286
581776  feet/sec       YDOT =        -306
742184  meter/sec
 ZDOT =       -216
994895                 ZDOT =         -29
040350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3461773
28                 X    =        -1055148
49
 Y    =      -13422729
08  feet           Y    =        -4091247
82  meter
 Z    =      -17505205
17                 Z    =        -5335586
54
 XDOT =      23326
385060                 XDOT =        7109
882166
 YDOT =      -5951
735502  feet/sec       YDOT =       -1814
088981  meter/sec
 ZDOT =        -46
791071                 ZDOT =         -14
261919


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
51618408  
00016717  00000-0  10270-3 0  9005
2 25544  51
6453 357
9645 0003874  78
4001 281
7583 15
48691575 20431


Satellite: ISS
Catalog Number: 25544
Epoch time:      20094
51618408   =   yrday
fracday
Element set:     900
Inclination:       51
6453  deg
RA of node:       357
9645  deg
Eccentricity:     
0003874     
Arg of perigee:    78
4001  deg
Mean anomaly:     281
7583  deg
Mean motion:   15
48691575  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2043
Checksum:              320


Coasting Arc #2 (Orbit 2058)
---------------------------------------

Vector Time (GMT): 2020/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         749873
33                 A    =         6793166
53  meter
 Y    =        4155007
14  meter          E    =           
0006172
 Z    =        5316369
69                 I    =           51
57613
 XDOT =      -7577
546697                 Wp   =           87
07430
 YDOT =       1139
336704  meter/sec      RA   =          352
50801  deg
 ZDOT =        178
492684                 TA   =            1
22310
                                          MA   =            1
22159
                                          Ha   =            230
895  n
mi
                                          Hp   =            221
826

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2460214
32                 X    =          677531
42
 Y    =       13631913
20  feet           Y    =         4162988
56  meter
 Z    =       17442157
77                 Z    =         5319836
32
 XDOT =     -24860
717509                 XDOT =       -7590
590928
 YDOT =       3737
981312  feet/sec       YDOT =        1054
526261  meter/sec
 ZDOT =        585
605917                 ZDOT =         141
652506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5206744
53                 X    =         1587015
73
 Y    =       12815129
11  feet           Y    =         3906051
35  meter
 Z    =       17457744
89                 Z    =         5321120
64
 XDOT =     -22552
373964                 XDOT =       -6873
963584
 YDOT =       8596
076418  feet/sec       YDOT =        2620
084092  meter/sec
 ZDOT =        416
548351                 ZDOT =         126
963937


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
54864104  
00016717  00000-0  10270-3 0  9016
2 25544  51
6448 352
8604 0003780  82
3162 277
8417 15
48711190 20597


Satellite: ISS
Catalog Number: 25544
Epoch time:      20095
54864104   =   yrday
fracday
Element set:     901
Inclination:       51
6448  deg
RA of node:       352
8604  deg
Eccentricity:     
0003780     
Arg of perigee:    82
3162  deg
Mean anomaly:     277
8417  deg
Mean motion:   15
48711190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2059
Checksum:              307


Coasting Arc #3 (Orbit 2068)
---------------------------------------

Vector Time (GMT): 2020/096/04:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5134216
25                 A    =         6798701
67  meter
 Y    =       -2173308
86  meter          E    =           
0010455
 Z    =       -3901488
90                 I    =           51
56999
 XDOT =       4890
806426                 Wp   =           78
19937
 YDOT =      -4231
885054  meter/sec      RA   =          349
21557  deg
 ZDOT =      -4085
990142                 TA   =          148
84634
                                          MA   =          148
78432
                                          Ha   =            231
009  n
mi
                                          Hp   =            221
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16844541
51                 X    =        -5090581
03
 Y    =       -7130278
41  feet           Y    =        -2230479
61  meter
 Z    =      -12800160
42                 Z    =        -3926322
58
 XDOT =      16045
952842                 XDOT =        4957
612373
 YDOT =     -13884
137315  feet/sec       YDOT =       -4176
819329  meter/sec
 ZDOT =     -13405
479467                 ZDOT =       -4062
070149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11405440
53                 X    =         3476378
27
 Y    =      -14197563
29  feet           Y    =        -4327417
29  meter
 Z    =      -12913894
78                 Z    =        -3936155
13
 XDOT =       7956
762692                 XDOT =        2425
221268
 YDOT =      18463
957106  feet/sec       YDOT =        5627
814126  meter/sec
 ZDOT =     -13295
458305                 ZDOT =       -4052
455691


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
19392664  
00016717  00000-0  10270-3 0  9026
2 25544  51
6426 349
6695 0003946  87
0422 273
1179 15
48679384 20695


Satellite: ISS
Catalog Number: 25544
Epoch time:      20096
19392664   =   yrday
fracday
Element set:     902
Inclination:       51
6426  deg
RA of node:       349
6695  deg
Eccentricity:     
0003946     
Arg of perigee:    87
0422  deg
Mean anomaly:     273
1179  deg
Mean motion:   15
48679384  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2069
Checksum:              345


Coasting Arc #4 (Orbit 2084)
---------------------------------------

Vector Time (GMT): 2020/097/04:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5379605
87                 A    =         6798972
00  meter
 Y    =        1630836
71  meter          E    =           
0015168
 Z    =        3812485
33                 I    =           51
53733
 XDOT =      -4393
922854                 Wp   =           95
27432
 YDOT =       4687
098388  meter/sec      RA   =          344
26592  deg
 ZDOT =       4179
351194                 TA   =          310
52018
                                          MA   =          310
65221
                                          Ha   =            230
904  n
mi
                                          Hp   =            221
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17649625
57                 X    =         5342450
76
 Y    =        5350514
14  feet           Y    =         1690787
89  meter
 Z    =       12508153
97                 Z    =         3838526
85
 XDOT =     -14415
757394                 XDOT =       -4466
309625
 YDOT =      15377
619383  feet/sec       YDOT =        4637
558055  meter/sec
 ZDOT =      13711
782133                 ZDOT =        4157
831090

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9643637
36                 X    =        -2939380
67
 Y    =       15624939
58  feet           Y    =         4762481
59  meter
 Z    =       12627459
03                 Z    =         3848849
51
 XDOT =     -10041
811984                 XDOT =       -3060
744293
 YDOT =     -17240
353988  feet/sec       YDOT =       -5254
859895  meter/sec
 ZDOT =      13612
748813                 ZDOT =        4149
165838


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
22638200  
00016717  00000-0  10270-3 0  9031
2 25544  51
6418 344
5650 0003878  89
4772 270
6822 15
48679022 20853


Satellite: ISS
Catalog Number: 25544
Epoch time:      20097
22638200   =   yrday
fracday
Element set:     903
Inclination:       51
6418  deg
RA of node:       344
5650  deg
Eccentricity:     
0003878     
Arg of perigee:    89
4772  deg
Mean anomaly:     270
6822  deg
Mean motion:   15
48679022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2085
Checksum:              318


Coasting Arc #5 (Orbit 2090)
---------------------------------------

Vector Time (GMT): 2020/097/14:00:43
000
Vector Time (MET): N/A
Weight (LBS)     : 915727
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6596423
51                 A    =         6804508
78  meter
 Y    =        1042255
95  meter          E    =           
0011266
 Z    =       -1288824
30                 I    =           51
54427
 XDOT =        344
448389                 Wp   =          127
19281
 YDOT =      -4964
474721  meter/sec      RA   =          342
20504  deg
 ZDOT =      -5819
481861                 TA   =           66
81060
                                          MA   =           66
69197
                                          Ha   =            230
871  n
mi
                                          Hp   =            221
958

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21641809
42                 X    =        -6601327
71
 Y    =        3419474
89  feet           Y    =          968462
50  meter
 Z    =       -4228426
18                 Z    =        -1320879
09
 XDOT =       1130
080018                 XDOT =         428
204675
 YDOT =     -16287
646723  feet/sec       YDOT =       -4960
155103  meter/sec
 ZDOT =     -19092
788259                 ZDOT =       -5817
604764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12988433
12                 X    =        -3958874
42
 Y    =       17609541
24  feet           Y    =         5367388
17  meter
 Z    =       -4375496
94                 Z    =        -1333651
47
 XDOT =      -9255
672493                 XDOT =       -2821
128976
 YDOT =     -11535
655596  feet/sec       YDOT =       -3516
067826  meter/sec
 ZDOT =     -19083
818620                 ZDOT =       -5816
747915


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
61355172  
00016717  00000-0  10270-3 0  9049
2 25544  51
6438 342
6517 0003544  89
4148 270
7408 15
48663378 20918


Satellite: ISS
Catalog Number: 25544
Epoch time:      20097
61355172   =   yrday
fracday
Element set:     904
Inclination:       51
6438  deg
RA of node:       342
6517  deg
Eccentricity:     
0003544     
Arg of perigee:    89
4148  deg
Mean anomaly:     270
7408  deg
Mean motion:   15
48663378  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2091
Checksum:              321


Coasting Arc #6 (Orbit 2106)
---------------------------------------

Vector Time (GMT): 2020/098/14:00:43
000
Vector Time (MET): N/A
Weight (LBS)     : 915727
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6474937
08                 A    =         6804508
87  meter
 Y    =       -1706373
89  meter          E    =           
0016799
 Z    =        1170059
53                 I    =           51
51210
 XDOT =        235
335368                 Wp   =           64
75363
 YDOT =       4943
687906  meter/sec      RA   =          337
25005  deg
 ZDOT =       5848
489724                 TA   =          307
95007
                                          MA   =          308
10175
                                          Ha   =            230
843  n
mi
                                          Hp   =            221
841

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21243231
87                 X    =         6487853
52
 Y    =       -5598339
53  feet           Y    =        -1633894
20  meter
 Z    =        3838777
98                 Z    =         1201543
90
 XDOT =        772
097663                 XDOT =         151
627361
 YDOT =      16219
448512  feet/sec       YDOT =        4945
852132  meter/sec
 ZDOT =      19187
958411                 ZDOT =        5849
429094

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10850187
67                 X    =         3307137
20
 Y    =      -19072481
47  feet           Y    =        -5813292
35  meter
 Z    =        3983265
03                 Z    =         1214099
18
 XDOT =      10644
229418                 XDOT =        3244
361127
 YDOT =      10102
522226  feet/sec       YDOT =        3079
248774  meter/sec
 ZDOT =      19191
909833                 ZDOT =        5849
694117


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
64600154  
00016717  00000-0  10270-3 0  9057
2 25544  51
6428 337
5461 0003610  92
4119 267
7445 15
48710185 21078


Satellite: ISS
Catalog Number: 25544
Epoch time:      20098
64600154   =   yrday
fracday
Element set:     905
Inclination:       51
6428  deg
RA of node:       337
5461  deg
Eccentricity:     
0003610     
Arg of perigee:    92
4119  deg
Mean anomaly:     267
7445  deg
Mean motion:   15
48710185  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2107
Checksum:              299


Coasting Arc #7 (Orbit 2121)
---------------------------------------

Vector Time (GMT): 2020/099/14:00:43
000
Vector Time (MET): N/A
Weight (LBS)     : 915727
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6298579
65                 A    =         6804663
17  meter
 Y    =        2316164
06  meter          E    =           
0012106
 Z    =       -1102748
80                 I    =           51
48038
 XDOT =       -771
757096                 Wp   =          128
77285
 YDOT =      -4865
712925  meter/sec      RA   =          332
29436  deg
 ZDOT =      -5862
674038                 TA   =           63
18804
                                          MA   =           63
06427
                                          Ha   =            230
878  n
mi
                                          Hp   =            221
910

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20664631
40                 X    =        -6318654
98
 Y    =        7598963
44  feet           Y    =         2245616
51  meter
 Z    =       -3617942
25                 Z    =        -1133394
08
 XDOT =      -2532
011471                 XDOT =        -688
812107
 YDOT =     -15963
625083  feet/sec       YDOT =       -4873
879988  meter/sec
 ZDOT =     -19234
494876                 ZDOT =       -5866
221093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8670899
13                 X    =        -2642890
06
 Y    =       20212597
40  feet           Y    =         6160799
69  meter
 Z    =       -3758611
07                 Z    =        -1145624
65
 XDOT =     -11770
569816                 XDOT =       -3587
669680
 YDOT =      -8599
135113  feet/sec       YDOT =       -2621
016382  meter/sec
 ZDOT =     -19250
410107                 ZDOT =       -5867
525001


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
61392420  
00016717  00000-0  10270-3 0  9060
2 25544  51
6414 332
7608 0003635  95
4393 264
7171 15
48677905 21229


Satellite: ISS
Catalog Number: 25544
Epoch time:      20099
61392420   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:       332
7608  deg
Eccentricity:     
0003635     
Arg of perigee:    95
4393  deg
Mean anomaly:     264
7171  deg
Mean motion:   15
48677905  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2122
Checksum:              313


Coasting Arc #8 (Orbit 2131)
---------------------------------------

Vector Time (GMT): 2020/100/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915727
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1896527
97                 A    =         6797948
48  meter
 Y    =       -5027203
10  meter          E    =           
0011351
 Z    =       -4175973
04                 I    =           51
43719
 XDOT =       6666
489243                 Wp   =          104
79687
 YDOT =       -561
295663  meter/sec      RA   =          328
95692  deg
 ZDOT =       3708
959641                 TA   =          203
50030
                                          MA   =          203
55220
                                          Ha   =            230
976  n
mi
                                          Hp   =            221
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6222204
63                 X    =         1972887
42
 Y    =      -16493448
51  feet           Y    =        -5005568
11  meter
 Z    =      -13700698
94                 Z    =        -4166574
53
 XDOT =      21871
683868                 XDOT =        6654
254130
 YDOT =      -1841
521204  feet/sec       YDOT =        -486
814393  meter/sec
 ZDOT =      12168
502759                 ZDOT =        3741
313538

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17620802
15                 X    =         5370820
50
 Y    =        1202328
25  feet           Y    =          366469
65  meter
 Z    =      -13657253
16                 Z    =        -4162730
76
 XDOT =       8235
068951                 XDOT =        2510
049016
 YDOT =      19006
666511  feet/sec       YDOT =        5793
231953  meter/sec
 ZDOT =      12316
871907                 ZDOT =        3754
182557


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
25920612  
00016717  00000-0  10270-3 0  9074
2 25544  51
6404 329
5705 0003770  96
8759 263
2819 15
48674013 21322


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
25920612   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:       329
5705  deg
Eccentricity:     
0003770     
Arg of perigee:    96
8759  deg
Mean anomaly:     263
2819  deg
Mean motion:   15
48674013  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2132
Checksum:              300


Coasting Arc #9 (Orbit 2133)
---------------------------------------

Vector Time (GMT): 2020/100/08:05:06
000
Vector Time (MET): N/A
Weight (LBS)     : 915727
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3806020
90                 A    =         6794097
67  meter
 Y    =        2418523
75  meter          E    =           
0008623
 Z    =        5075846
73                 I    =           51
42421
 XDOT =      -5526
960996                 Wp   =          113
54908
 YDOT =       5013
695042  meter/sec      RA   =          328
56603  deg
 ZDOT =       1749
625180                 TA   =          319
44159
                                          MA   =          319
50581
                                          Ha   =            230
721  n
mi
                                          Hp   =            221
850

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12486945
21                 X    =         3754037
52
 Y    =        7934789
21  feet           Y    =         2460795
06  meter
 Z    =       16653040
45                 Z    =         5094208
69
 XDOT =     -18133
074135                 XDOT =       -5591
113622
 YDOT =      16449
130714  feet/sec       YDOT =        4951
530046  meter/sec
 ZDOT =       5740
240093                 ZDOT =        1722
620898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3986072
16                 X    =         1214954
79
 Y    =       14148880
52  feet           Y    =         4312578
78  meter
 Z    =       16737050
08                 Z    =         5101452
86
 XDOT =     -23478
142124                 XDOT =       -7156
137719
 YDOT =        -51
235583  feet/sec       YDOT =         -15
616606  meter/sec
 ZDOT =       5616
080885                 ZDOT =        1711
781454


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
38826116  
00016717  00000-0  10270-3 0  9083
2 25544  51
6420 328
9333 0003649  98
6797 261
4766 15
48724471 21344


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
38826116   =   yrday
fracday
Element set:     908
Inclination:       51
6420  deg
RA of node:       328
9333  deg
Eccentricity:     
0003649     
Arg of perigee:    98
6797  deg
Mean anomaly:     261
4766  deg
Mean motion:   15
48724471  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2134
Checksum:              321


Coasting Arc #10 (Orbit 2137)
---------------------------------------

Vector Time (GMT): 2020/100/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3841696
27                 A    =         6794279
09  meter
 Y    =        2350598
99  meter          E    =           
0008615
 Z    =        5081126
45                 I    =           51
41488
 XDOT =      -5429
477765                 Wp   =          113
76429
 YDOT =       5126
340957  meter/sec      RA   =          327
28378  deg
 ZDOT =       1727
825697                 TA   =          319
44174
                                          MA   =          319
50590
                                          Ha   =            230
839  n
mi
                                          Hp   =            221
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12603990
37                 X    =         3790444
13
 Y    =        7711938
96  feet           Y    =         2393273
30  meter
 Z    =       16670362
37                 Z    =         5099663
52
 XDOT =     -17813
247261                 XDOT =       -5494
791389
 YDOT =      16818
703928  feet/sec       YDOT =        5065
259583  meter/sec
 ZDOT =       5668
719477                 ZDOT =        1701
292154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13803329
93                 X    =         4207254
96
 Y    =       -4996762
85  feet           Y    =        -1523013
32  meter
 Z    =       16755178
34                 Z    =         5106978
36
 XDOT =       1726
235722                 XDOT =         526
156648
 YDOT =      23430
677217  feet/sec       YDOT =        7141
670416  meter/sec
 ZDOT =       5546
712982                 ZDOT =        1690
638117


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
64637408  
00016717  00000-0  10270-3 0  9097
2 25544  51
6402 327
6550 0003679  99
4114 260
7452 15
48654593 21381


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
64637408   =   yrday
fracday
Element set:     909
Inclination:       51
6402  deg
RA of node:       327
6550  deg
Eccentricity:     
0003679     
Arg of perigee:    99
4114  deg
Mean anomaly:     260
7452  deg
Mean motion:   15
48654593  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2138
Checksum:              312


Coasting Arc #11 (Orbit 2152)
---------------------------------------

Vector Time (GMT): 2020/101/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4109873
91                 A    =         6794276
00  meter
 Y    =       -1938261
48  meter          E    =           
0016564
 Z    =       -5066069
98                 I    =           51
38722
 XDOT =       4878
398955                 Wp   =           82
12130
 YDOT =      -5601
231882  meter/sec      RA   =          322
32371  deg
 ZDOT =      -1817
517057                 TA   =          170
18622
                                          MA   =          170
15383
                                          Ha   =            230
891  n
mi
                                          Hp   =            221
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13483838
28                 X    =        -4063285
86
 Y    =       -6359125
60  feet           Y    =        -1983960
67  meter
 Z    =      -16620964
49                 Z    =        -5085921
18
 XDOT =      16005
245915                 XDOT =        4949
499581
 YDOT =     -18376
745021  feet/sec       YDOT =       -5546
280657  meter/sec
 ZDOT =      -5962
982471                 ZDOT =       -1793
646561

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13175738
27                 X    =        -4015965
02
 Y    =        6754515
71  feet           Y    =         2058776
39  meter
 Z    =      -16711830
32                 Z    =        -5093765
88
 XDOT =      -4352
905599                 XDOT =       -1326
765627
 YDOT =     -22949
290168  feet/sec       YDOT =       -6994
943643  meter/sec
 ZDOT =      -5853
158881                 ZDOT =       -1784
042827


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
61429158  
00016717  00000-0  10270-3 0  9108
2 25544  51
6397 322
8681 0003715 103
9691 256
1872 15
48696257 21533


Satellite: ISS
Catalog Number: 25544
Epoch time:      20101
61429158   =   yrday
fracday
Element set:     910
Inclination:       51
6397  deg
RA of node:       322
8681  deg
Eccentricity:     
0003715     
Arg of perigee:   103
9691  deg
Mean anomaly:     256
1872  deg
Mean motion:   15
48696257  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2153
Checksum:              315


Coasting Arc #12 (Orbit 2168)
---------------------------------------

Vector Time (GMT): 2020/102/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4326798
73                 A    =         6794491
37  meter
 Y    =        1472540
47  meter          E    =           
0009256
 Z    =        5021485
63                 I    =           51
36187
 XDOT =      -4298
025373                 Wp   =          116
43232
 YDOT =       6047
307831  meter/sec      RA   =          317
36241  deg
 ZDOT =       1923
259687                 TA   =          314
79102
                                          MA   =          314
86626
                                          Ha   =            230
809  n
mi
                                          Hp   =            221
942

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14195533
91                 X    =         4285619
03
 Y    =        4831169
54  feet           Y    =         1520695
58  meter
 Z    =       16474690
38                 Z    =         5042403
71
 XDOT =     -14101
133115                 XDOT =       -4374
670907
 YDOT =      19840
248790  feet/sec       YDOT =        5998
815707  meter/sec
 ZDOT =       6309
907110                 ZDOT =        1902
195180

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12251532
69                 X    =         3734267
16
 Y    =       -8460969
82  feet           Y    =        -2578903
60  meter
 Z    =       16570478
02                 Z    =         5050681
70
 XDOT =       6945
916516                 XDOT =        2117
115354
 YDOT =      22268
954912  feet/sec       YDOT =        6787
577457  meter/sec
 ZDOT =       6212
922181                 ZDOT =        1893
698681


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
64673660  
00016717  00000-0  10270-3 0  9112
2 25544  51
6398 317
7625 0003732 105
9199 254
2362 15
48664922 21693


Satellite: ISS
Catalog Number: 25544
Epoch time:      20102
64673660   =   yrday
fracday
Element set:     911
Inclination:       51
6398  deg
RA of node:       317
7625  deg
Eccentricity:     
0003732     
Arg of perigee:   105
9199  deg
Mean anomaly:     254
2362  deg
Mean motion:   15
48664922  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2169
Checksum:              319


Coasting Arc #13 (Orbit 2183)
---------------------------------------

Vector Time (GMT): 2020/103/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4498626
74                 A    =         6794502
45  meter
 Y    =       -1011748
69  meter          E    =           
0016147
 Z    =       -5004948
91                 I    =           51
33804
 XDOT =       3669
776456                 Wp   =           83
08643
 YDOT =      -6401
623272  meter/sec      RA   =          312
39979  deg
 ZDOT =      -2008
142009                 TA   =          167
28253
                                          MA   =          167
24175
                                          Ha   =            230
925  n
mi
                                          Hp   =            221
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14759274
08                 X    =        -4462667
39
 Y    =       -3319385
46  feet           Y    =        -1061854
41  meter
 Z    =      -16420436
07                 Z    =        -5026714
29
 XDOT =      12039
949001                 XDOT =        3750
843018
 YDOT =     -21002
701023  feet/sec       YDOT =       -6360
131926  meter/sec
 ZDOT =      -6588
392419                 ZDOT =       -1990
118744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11199765
54                 X    =        -3413688
54
 Y    =       10006769
92  feet           Y    =         3050063
47  meter
 Z    =      -16520139
81                 Z    =        -5035338
61
 XDOT =      -9371
779553                 XDOT =       -2856
518408
 YDOT =     -21208
771765  feet/sec       YDOT =       -6464
433634  meter/sec
 ZDOT =      -6505
332068                 ZDOT =       -1982
825214


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
61465117  
00016717  00000-0  10270-3 0  9127
2 25544  51
6394 312
9767 0003931 110
9237 249
2334 15
48703233 21842


Satellite: ISS
Catalog Number: 25544
Epoch time:      20103
61465117   =   yrday
fracday
Element set:     912
Inclination:       51
6394  deg
RA of node:       312
9767  deg
Eccentricity:     
0003931     
Arg of perigee:   110
9237  deg
Mean anomaly:     249
2334  deg
Mean motion:   15
48703233  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2184
Checksum:              293


Coasting Arc #14 (Orbit 2199)
---------------------------------------

Vector Time (GMT): 2020/104/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4612488
88                 A    =         6794691
36  meter
 Y    =         505214
65  meter          E    =           
0009881
 Z    =        4957748
78                 I    =           51
31625
 XDOT =      -3015
503506                 Wp   =          119
62158
 YDOT =       6721
718847  meter/sec      RA   =          307
43547  deg
 ZDOT =       2112
551701                 TA   =          309
65690
                                          MA   =          309
74403
                                          Ha   =            230
741  n
mi
                                          Hp   =            221
955

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15132837
52                 X    =         4582414
65
 Y    =        1657528
36  feet           Y    =          556626
55  meter
 Z    =       16265579
99                 Z    =         4980081
45
 XDOT =      -9893
384206                 XDOT =       -3100
705223
 YDOT =      22052
883357  feet/sec       YDOT =        6687
520918  meter/sec
 ZDOT =       6930
943902                 ZDOT =        2097
696698

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9867745
90                 X    =         3007688
95
 Y    =      -11447185
81  feet           Y    =        -3489102
23  meter
 Z    =       16367919
60                 Z    =         4988941
89
 XDOT =      11723
322151                 XDOT =        3573
268592
 YDOT =      19955
278405  feet/sec       YDOT =        6082
368858  meter/sec
 ZDOT =       6862
395756                 ZDOT =        2091
658227


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
64709351  
00016717  00000-0  10270-3 0  9133
2 25544  51
6389 307
8715 0003776 115
1631 244
9910 15
48686543 22009


Satellite: ISS
Catalog Number: 25544
Epoch time:      20104
64709351   =   yrday
fracday
Element set:     913
Inclination:       51
6389  deg
RA of node:       307
8715  deg
Eccentricity:     
0003776     
Arg of perigee:   115
1631  deg
Mean anomaly:     244
9910  deg
Mean motion:   15
48686543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2200
Checksum:              306


Coasting Arc #15 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2020/105/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4680067
02                 A    =         6794724
38  meter
 Y    =         -17265
04  meter          E    =           
0015422
 Z    =       -4939862
65                 I    =           51
29909
 XDOT =       2336
047479                 Wp   =           83
98925
 YDOT =      -6944
178856  meter/sec      RA   =          302
47020  deg
 ZDOT =      -2193
275877                 TA   =          164
47451
                                          MA   =          164
42715
                                          Ha   =            230
849  n
mi
                                          Hp   =            221
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15354550
60                 X    =        -4655531
14
 Y    =         -56643
82  feet           Y    =          -69463
65  meter
 Z    =      -16206898
46                 Z    =        -4962536
96
 XDOT =       7664
197766                 XDOT =        2424
179384
 YDOT =     -22782
739028  feet/sec       YDOT =       -6917
562716  meter/sec
 ZDOT =      -7195
786999                 ZDOT =       -2181
714295

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8456571
39                 X    =        -2577562
96
 Y    =       12683532
14  feet           Y    =         3865940
60  meter
 Z    =      -16310836
98                 Z    =        -4971543
11
 XDOT =     -13824
326623                 XDOT =       -4213
654755
 YDOT =     -18383
860877  feet/sec       YDOT =       -5603
400795  meter/sec
 ZDOT =      -7142
335101                 ZDOT =       -2176
983739


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   20105
61500556  
00016717  00000-0  10270-3 0  9148
2 25544  51
6408 303
0862 0003919 118
3617 241
7928 15
48718153 22153


Satellite: ISS
Catalog Number: 25544
Epoch time:      20105
61500556   =   yrday
fracday
Element set:     914
Inclination:       51
6408  deg
RA of node:       303
0862  deg
Eccentricity:     
0003919     
Arg of perigee:   118
3617  deg
Mean anomaly:     241
7928  deg
Mean motion:   15
48718153  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              295


Coasting Arc #16 (Orbit 2230)
---------------------------------------

Vector Time (GMT): 2020/106/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4683646
77                 A    =         6794871
11  meter
 Y    =        -505361
96  meter          E    =           
0010415
 Z    =        4891031
91                 I    =           51
28197
 XDOT =      -1636
535978                 Wp   =          121
70561
 YDOT =       7126
734391  meter/sec      RA   =          297
50245  deg
 ZDOT =       2294
513262                 TA   =          305
68116
                                          MA   =          305
77805
                                          Ha   =            230
651  n
mi
                                          Hp   =            221
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15366295
19                 X    =         4665192
04
 Y    =       -1658011
69  feet           Y    =         -453089
26  meter
 Z    =       16046692
63                 Z    =         4913738
33
 XDOT =      -5369
212525                 XDOT =       -1727
252990
 YDOT =      23381
674512  feet/sec       YDOT =        7107
926259  meter/sec
 ZDOT =       7527
930651                 ZDOT =        2286
343283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6797758
83                 X    =         2071956
89
 Y    =      -13759002
54  feet           Y    =        -4193743
97  meter
 Z    =       16150811
09                 Z    =         4922767
22
 XDOT =      15807
306867                 XDOT =        4818
067133
 YDOT =      16636
230810  feet/sec       YDOT =        5070
723151  meter/sec
 ZDOT =       7490
031090                 ZDOT =        2282
961476


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   20106
64744239  
00016717  00000-0  10270-3 0  9151
2 25544  51
6401 297
9804 0003808 122
7566 237
3952 15
48720240 22318


Satellite: ISS
Catalog Number: 25544
Epoch time:      20106
64744239   =   yrday
fracday
Element set:     915
Inclination:       51
6401  deg
RA of node:       297
9804  deg
Eccentricity:     
0003808     
Arg of perigee:   122
7566  deg
Mean anomaly:     237
3952  deg
Mean motion:   15
48720240  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2231
Checksum:              303


Coasting Arc #17 (Orbit 2245)
---------------------------------------

Vector Time (GMT): 2020/107/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4644419
53                 A    =         6794998
59  meter
 Y    =         997136
26  meter          E    =           
0014689
 Z    =       -4871953
12                 I    =           51
26814
 XDOT =        933
550371                 Wp   =           84
93452
 YDOT =      -7211
456238  meter/sec      RA   =          292
53557  deg
 ZDOT =      -2370
849629                 TA   =          161
67813
                                          MA   =          161
62516
                                          Ha   =            230
798  n
mi
                                          Hp   =            221
800

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15237596
87                 X    =        -4631559
56
 Y    =        3271444
41  feet           Y    =          945270
87  meter
 Z    =      -15984098
15                 Z    =        -4894482
57
 XDOT =       3062
829301                 XDOT =        1025
637806
 YDOT =     -23659
633327  feet/sec       YDOT =       -7200
501763  meter/sec
 ZDOT =      -7778
378049                 ZDOT =       -2366
091035

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5117444
19                 X    =        -1559796
99
 Y    =       14607681
51  feet           Y    =         4452421
32  meter
 Z    =      -16087433
19                 Z    =        -4903449
64
 XDOT =     -17478
971679                 XDOT =       -5327
590568
 YDOT =     -14647
420942  feet/sec       YDOT =       -4464
533903  meter/sec
 ZDOT =      -7756
129975                 ZDOT =       -2364
068417


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   20107
61535168  
00016717  00000-0  10270-3 0  9169
2 25544  51
6403 293
1959 0003939 124
9821 235
1699 15
48720166 22469


Satellite: ISS
Catalog Number: 25544
Epoch time:      20107
61535168   =   yrday
fracday
Element set:     916
Inclination:       51
6403  deg
RA of node:       293
1959  deg
Eccentricity:     
0003939     
Arg of perigee:   124
9821  deg
Mean anomaly:     235
1699  deg
Mean motion:   15
48720166  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2246
Checksum:              322


Coasting Arc #18 (Orbit 2253)
---------------------------------------

Vector Time (GMT): 2020/108/01:53:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916536
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4613037
86                 A    =         6795435
54  meter
 Y    =       -1518047
68  meter          E    =           
0011054
 Z    =        4747264
24                 I    =           51
26268
 XDOT =       -371
507076                 Wp   =          119
86536
 YDOT =       7182
045048  meter/sec      RA   =          290
13862  deg
 ZDOT =       2647
563476                 TA   =          303
79262
                                          MA   =          303
89784
                                          Ha   =            230
543  n
mi
                                          Hp   =            222
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15134638
64                 X    =         4606610
86
 Y    =       -4980471
38  feet           Y    =        -1466497
22  meter
 Z    =       15575013
90                 Z    =         4769656
90
 XDOT =      -1218
855236                 XDOT =        -464
651515
 YDOT =      23563
139921  feet/sec       YDOT =        7177
369854  meter/sec
 ZDOT =       8686
231875                 ZDOT =        2645
532438

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5064108
14                 X    =        -1543540
16
 Y    =       15000212
51  feet           Y    =         4572064
77  meter
 Z    =       15677750
89                 Z    =         4778578
47
 XDOT =     -16959
245295                 XDOT =       -5169
177966
 YDOT =     -14828
171450  feet/sec       YDOT =       -4519
626658  meter/sec
 ZDOT =       8676
498080                 ZDOT =        2644
596615


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   20108
13156822  
00016717  00000-0  10270-3 0  9174
2 25544  51
6393 290
6472 0003542 124
0542 236
0945 15
48729767 22549


Satellite: ISS
Catalog Number: 25544
Epoch time:      20108
13156822   =   yrday
fracday
Element set:     917
Inclination:       51
6393  deg
RA of node:       290
6472  deg
Eccentricity:     
0003542     
Arg of perigee:   124
0542  deg
Mean anomaly:     236
0945  deg
Mean motion:   15
48729767  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2254
Checksum:              307


Coasting Arc #19 (Orbit 2268)
---------------------------------------

Vector Time (GMT): 2020/109/01:53:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916536
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4470030
10                 A    =         6795644
54  meter
 Y    =        1999104
37  meter          E    =           
0013382
 Z    =       -4724274
81                 I    =           51
25295
 XDOT =       -325
185370                 Wp   =           83
72425
 YDOT =      -7141
873108  meter/sec      RA   =          285
16817  deg
 ZDOT =      -2719
686305                 TA   =          159
18083
                                          MA   =          159
12627
                                          Ha   =            230
692  n
mi
                                          Hp   =            221
961

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14665453
09                 X    =        -4469104
68
 Y    =        6558741
37  feet           Y    =         1949122
31  meter
 Z    =      -15499589
27                 Z    =        -4745986
24
 XDOT =      -1066
881135                 XDOT =        -232
088011
 YDOT =     -23431
342218  feet/sec       YDOT =       -7144
989124  meter/sec
 ZDOT =      -8922
855331                 ZDOT =       -2721
039541

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3253024
77                 X    =          991521
95
 Y    =      -15633677
38  feet           Y    =        -4765144
86  meter
 Z    =      -15599225
36                 Z    =        -4754643
89
 XDOT =      18407
782137                 XDOT =        5610
691995
 YDOT =      12722
171412  feet/sec       YDOT =        3877
717846  meter/sec
 ZDOT =      -8928
656617                 ZDOT =       -2721
454537


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   20109
09947626  
00016717  00000-0  10270-3 0  9181
2 25544  51
6396 285
8606 0003602 126
3247 233
8235 15
48704720 22696


Satellite: ISS
Catalog Number: 25544
Epoch time:      20109
09947626   =   yrday
fracday
Element set:     918
Inclination:       51
6396  deg
RA of node:       285
8606  deg
Eccentricity:     
0003602     
Arg of perigee:   126
3247  deg
Mean anomaly:     233
8235  deg
Mean motion:   15
48704720  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2269
Checksum:              321
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