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

 
Date: April 2nd 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 8
000/00:00:00 000 0 0 0 0 221 9

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

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 2028)
---------------------------------------

Vector Time (GMT): 2020/093/13:27:27
745
Vector Time (MET): N/A
Weight (LBS)     : 939587
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2256404
89                 A    =         6794694
71  meter
 Y    =        4026213
35  meter          E    =           
0009132
 Z    =        4979747
54                 I    =           51
64677
 XDOT =      -7227
197412                 Wp   =          105
24856
 YDOT =       1415
623336  meter/sec      RA   =            2
11289  deg
 ZDOT =       2124
602482                 TA   =          324
02136
                                          MA   =          324
08280
                                          Ha   =            230
904  n
mi
                                          Hp   =            221
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7402903
18                 X    =         2187026
26
 Y    =       13209361
40  feet           Y    =         4051058
26  meter
 Z    =       16337754
39                 Z    =         4990539
61
 XDOT =     -23711
277597                 XDOT =       -7252
810236
 YDOT =       4644
433516  feet/sec       YDOT =        1334
660511  meter/sec
 ZDOT =       6970
480584                 ZDOT =        2089
433550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13224852
26                 X    =         4030934
97
 Y    =        7265231
46  feet           Y    =         2214442
55  meter
 Z    =       16386949
60                 Z    =         4994742
24
 XDOT =     -17064
391834                 XDOT =       -5201
226631
 YDOT =      15662
857674  feet/sec       YDOT =        4774
039019  meter/sec
 ZDOT =       6809
045327                 ZDOT =        2075
397016


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
61278098  
00016717  00000-0  10270-3 0  9002
2 25544  51
6456   2
4313 0003790  77
2921 282
8652 15
48675836 20298


Satellite: ISS
Catalog Number: 25544
Epoch time:      20093
61278098   =   yrday
fracday
Element set:     900
Inclination:       51
6456  deg
RA of node:         2
4313  deg
Eccentricity:     
0003790     
Arg of perigee:    77
2921  deg
Mean anomaly:     282
8652  deg
Mean motion:   15
48675836  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2029
Checksum:              314


Coasting Arc #2 (Orbit 2043)
---------------------------------------

Vector Time (GMT): 2020/094/13:27:27
745
Vector Time (MET): N/A
Weight (LBS)     : 939587
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2708935
14                 A    =         6794768
28  meter
 Y    =       -3796993
98  meter          E    =           
0016117
 Z    =       -4955951
07                 I    =           51
61356
 XDOT =       7008
244401                 Wp   =           74
48918
 YDOT =      -2106
358385  meter/sec      RA   =          357
16959  deg
 ZDOT =      -2218
772976                 TA   =          173
79481
                                          MA   =          173
77482
                                          Ha   =            230
904  n
mi
                                          Hp   =            221
780

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8887582
46                 X    =        -2642201
71
 Y    =      -12457329
32  feet           Y    =        -3826914
26  meter
 Z    =      -16259681
98                 Z    =        -4968947
69
 XDOT =      22992
927824                 XDOT =        7042
054901
 YDOT =      -6910
624623  feet/sec       YDOT =       -2027
798244  meter/sec
 ZDOT =      -7279
438899                 ZDOT =       -2184
647753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14176168
86                 X    =        -4320896
27
 Y    =       -5592646
23  feet           Y    =        -1704638
57  meter
 Z    =      -16319006
67                 Z    =        -4974033
23
 XDOT =      15054
780114                 XDOT =        4588
696979
 YDOT =     -17394
390189  feet/sec       YDOT =       -5301
810129  meter/sec
 ZDOT =      -7122
748515                 ZDOT =       -2171
013747


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
58070763  
00016717  00000-0  10270-3 0  9019
2 25544  51
6455 357
6459 0003742  78
0658 282
0911 15
48700919 20444


Satellite: ISS
Catalog Number: 25544
Epoch time:      20094
58070763   =   yrday
fracday
Element set:     901
Inclination:       51
6455  deg
RA of node:       357
6459  deg
Eccentricity:     
0003742     
Arg of perigee:    78
0658  deg
Mean anomaly:     282
0911  deg
Mean motion:   15
48700919  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2044
Checksum:              317


Coasting Arc #3 (Orbit 2059)
---------------------------------------

Vector Time (GMT): 2020/095/13:27:27
745
Vector Time (MET): N/A
Weight (LBS)     : 939587
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3139246
13                 A    =         6795006
77  meter
 Y    =        3495422
60  meter          E    =           
0009891
 Z    =        4901933
24                 I    =           51
58004
 XDOT =      -6749
937961                 Wp   =          106
80900
 YDOT =       2786
280028  meter/sec      RA   =          352
22437  deg
 ZDOT =       2329
214880                 TA   =          320
33326
                                          MA   =          320
40557
                                          Ha   =            230
917  n
mi
                                          Hp   =            221
855

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10299363
94                 X    =         3076115
38
 Y    =       11467921
93  feet           Y    =         3530175
18  meter
 Z    =       16082458
13                 Z    =         4917028
80
 XDOT =     -22145
465752                 XDOT =       -6791
907197
 YDOT =       9141
338673  feet/sec       YDOT =        2710
562886  meter/sec
 ZDOT =       7641
781104                 ZDOT =        2296
324519

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14880205
08                 X    =         4535486
51
 Y    =        3734477
24  feet           Y    =         1138268
66  meter
 Z    =       16151432
34                 Z    =         4922956
58
 XDOT =     -12916
113631                 XDOT =       -3936
831435
 YDOT =      18973
254848  feet/sec       YDOT =        5783
048078  meter/sec
 ZDOT =       7490
716621                 ZDOT =        2283
170426


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
61316164  
00016717  00000-0  10270-3 0  9023
2 25544  51
6449 352
5415 0003857  82
4607 277
6981 15
48672184 20600


Satellite: ISS
Catalog Number: 25544
Epoch time:      20095
61316164   =   yrday
fracday
Element set:     902
Inclination:       51
6449  deg
RA of node:       352
5415  deg
Eccentricity:     
0003857     
Arg of perigee:    82
4607  deg
Mean anomaly:     277
6981  deg
Mean motion:   15
48672184  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2060
Checksum:              317


Coasting Arc #4 (Orbit 2068)
---------------------------------------

Vector Time (GMT): 2020/096/04:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939587
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5129106
43                 A    =         6798661
99  meter
 Y    =       -2177653
78  meter          E    =           
0010447
 Z    =       -3905691
67                 I    =           51
57016
 XDOT =       4897
535668                 Wp   =           78
40722
 YDOT =      -4229
058852  meter/sec      RA   =          349
21552  deg
 ZDOT =      -4080
923615                 TA   =          148
70516
                                          MA   =          148
64294
                                          Ha   =            230
989  n
mi
                                          Hp   =            221
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16827777
00                 X    =        -5085402
59
 Y    =       -7144533
41  feet           Y    =        -2234767
01  meter
 Z    =      -12813949
03                 Z    =        -3930500
36
 XDOT =      16068
030406                 XDOT =        4964
284901
 YDOT =     -13874
865001  feet/sec       YDOT =       -4173
918194  meter/sec
 ZDOT =     -13388
857006                 ZDOT =       -4056
971073

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11414594
17                 X    =         3479168
30
 Y    =      -14177472
97  feet           Y    =        -4321293
76  meter
 Z    =      -12927568
45                 Z    =        -3940322
86
 XDOT =       7943
349067                 XDOT =        2421
132795
 YDOT =      18481
918694  feet/sec       YDOT =        5633
288818  meter/sec
 ZDOT =     -13278
686768                 ZDOT =       -4047
343727


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
19391456  
00016717  00000-0  10270-3 0  9035
2 25544  51
6428 349
6695 0003928  87
7948 272
3651 15
48688203 20693


Satellite: ISS
Catalog Number: 25544
Epoch time:      20096
19391456   =   yrday
fracday
Element set:     903
Inclination:       51
6428  deg
RA of node:       349
6695  deg
Eccentricity:     
0003928     
Arg of perigee:    87
7948  deg
Mean anomaly:     272
3651  deg
Mean motion:   15
48688203  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2069
Checksum:              352


Coasting Arc #5 (Orbit 2084)
---------------------------------------

Vector Time (GMT): 2020/097/04:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939587
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5372800
52                 A    =         6798922
26  meter
 Y    =        1638072
90  meter          E    =           
0015134
 Z    =        3818959
71                 I    =           51
53748
 XDOT =      -4404
499394                 Wp   =           95
56871
 YDOT =       4683
851526  meter/sec      RA   =          344
26583  deg
 ZDOT =       4171
817065                 TA   =          310
32586
                                          MA   =          310
45798
                                          Ha   =            230
881  n
mi
                                          Hp   =            221
796

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17627298
28                 X    =         5335533
54
 Y    =        5374254
92  feet           Y    =         1697947
35  meter
 Z    =       12529395
37                 Z    =         3844967
90
 XDOT =     -14450
457328                 XDOT =       -4476
812475
 YDOT =      15366
966948  feet/sec       YDOT =        4634
193329  meter/sec
 ZDOT =      13687
063863                 ZDOT =        4150
245764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9660881
19                 X    =        -2944636
59
 Y    =       15597167
73  feet           Y    =         4754016
72  meter
 Z    =       12648547
05                 Z    =         3855277
14
 XDOT =     -10024
748829                 XDOT =       -3055
543443
 YDOT =     -17269
781168  feet/sec       YDOT =       -5263
829300  meter/sec
 ZDOT =      13587
795994                 ZDOT =        4141
560219


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
22636365  
00016717  00000-0  10270-3 0  9042
2 25544  51
6420 344
5650 0003857  90
2466 269
9125 15
48688873 20854


Satellite: ISS
Catalog Number: 25544
Epoch time:      20097
22636365   =   yrday
fracday
Element set:     904
Inclination:       51
6420  deg
RA of node:       344
5650  deg
Eccentricity:     
0003857     
Arg of perigee:    90
2466  deg
Mean anomaly:     269
9125  deg
Mean motion:   15
48688873  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2085
Checksum:              330


Coasting Arc #6 (Orbit 2090)
---------------------------------------

Vector Time (GMT): 2020/097/14:00:43
000
Vector Time (MET): N/A
Weight (LBS)     : 915574
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6595727
05                 A    =         6804466
43  meter
 Y    =        1033386
27  meter          E    =           
0011249
 Z    =       -1299201
31                 I    =           51
54444
 XDOT =        359
399098                 Wp   =          127
44422
 YDOT =      -4966
843904  meter/sec      RA   =          342
20502  deg
 ZDOT =      -5816
604907                 TA   =           66
67435
                                          MA   =           66
55602
                                          Ha   =            230
846  n
mi
                                          Hp   =            221
949

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21639524
44                 X    =        -6600481
71
 Y    =        3390374
90  feet           Y    =          959601
45  meter
 Z    =       -4262471
48                 Z    =        -1331252
35
 XDOT =       1179
130900                 XDOT =         443
166791
 YDOT =     -16295
419634  feet/sec       YDOT =       -4962
357033  meter/sec
 ZDOT =     -19083
349431                 ZDOT =       -5814
655157

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13007074
77                 X    =        -3964556
39
 Y    =       17587052
73  feet           Y    =         5360533
67  meter
 Z    =       -4409524
41                 Z    =        -1344023
04
 XDOT =      -9227
889520                 XDOT =       -2812
660726
 YDOT =     -11574
224894  feet/sec       YDOT =       -3527
823748  meter/sec
 ZDOT =     -19074
046453                 ZDOT =       -5813
769359


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
61353079  
00016717  00000-0  10270-3 0  9054
2 25544  51
6441 342
6517 0003520  90
2535 269
9018 15
48673862 20912


Satellite: ISS
Catalog Number: 25544
Epoch time:      20097
61353079   =   yrday
fracday
Element set:     905
Inclination:       51
6441  deg
RA of node:       342
6517  deg
Eccentricity:     
0003520     
Arg of perigee:    90
2535  deg
Mean anomaly:     269
9018  deg
Mean motion:   15
48673862  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2091
Checksum:              310


Coasting Arc #7 (Orbit 2106)
---------------------------------------

Vector Time (GMT): 2020/098/14:00:43
000
Vector Time (MET): N/A
Weight (LBS)     : 915574
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6475480
78                 A    =         6804459
41  meter
 Y    =       -1694477
70  meter          E    =           
0016766
 Z    =        1184135
33                 I    =           51
51227
 XDOT =        215
538142                 Wp   =           65
00520
 YDOT =       4948
849178  meter/sec      RA   =          337
25001  deg
 ZDOT =       5844
880500                 TA   =          307
85394
                                          MA   =          308
00552
                                          Ha   =            230
814  n
mi
                                          Hp   =            221
832

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21245015
68                 X    =         6488195
78
 Y    =       -5559310
04  feet           Y    =        -1621993
05  meter
 Z    =        3884958
43                 Z    =         1215621
85
 XDOT =        707
146136                 XDOT =         131
791424
 YDOT =      16236
381819  feet/sec       YDOT =        4950
791801  meter/sec
 ZDOT =      19176
117125                 ZDOT =        5845
723608

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10879096
09                 X    =         3315948
49
 Y    =      -19046214
48  feet           Y    =        -5805286
17  meter
 Z    =        4029454
48                 Z    =         1228177
73
 XDOT =      10612
839486                 XDOT =        3234
793475
 YDOT =      10158
599534  feet/sec       YDOT =        3096
341138  meter/sec
 ZDOT =      19179
626787                 ZDOT =        5845
950245


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
64597318  
00016717  00000-0  10270-3 0  9065
2 25544  51
6431 337
5461 0003584  93
2598 266
8962 15
48722143 21073


Satellite: ISS
Catalog Number: 25544
Epoch time:      20098
64597318   =   yrday
fracday
Element set:     906
Inclination:       51
6431  deg
RA of node:       337
5461  deg
Eccentricity:     
0003584     
Arg of perigee:    93
2598  deg
Mean anomaly:     266
8962  deg
Mean motion:   15
48722143  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2107
Checksum:              332


Coasting Arc #8 (Orbit 2121)
---------------------------------------

Vector Time (GMT): 2020/099/14:00:43
000
Vector Time (MET): N/A
Weight (LBS)     : 915574
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6300848
92                 A    =         6804607
51  meter
 Y    =        2301120
04  meter          E    =           
0012060
 Z    =       -1120823
75                 I    =           51
48053
 XDOT =       -747
079701                 Wp   =          129
04057
 YDOT =      -4874
777569  meter/sec      RA   =          332
29429  deg
 ZDOT =      -5858
371472                 TA   =           63
11940
                                          MA   =           62
99619
                                          Ha   =            230
846  n
mi
                                          Hp   =            221
901

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20672076
52                 X    =        -6320668
06
 Y    =        7549606
43  feet           Y    =         2230548
55  meter
 Z    =       -3677243
27                 Z    =        -1151479
43
 XDOT =      -2451
048889                 XDOT =        -664
056082
 YDOT =     -15993
364729  feet/sec       YDOT =       -4882
668232  meter/sec
 ZDOT =     -19220
378845                 ZDOT =       -5861
798461

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8711586
19                 X    =        -2655291
47
 Y    =       20183777
65  feet           Y    =         6152015
43  meter
 Z    =       -3817958
70                 Z    =        -1163713
81
 XDOT =     -11738
675488                 XDOT =       -3577
948289
 YDOT =      -8675
337617  feet/sec       YDOT =       -2644
242906  meter/sec
 ZDOT =     -19235
742946                 ZDOT =       -5863
054450


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
61388812  
00016717  00000-0  10270-3 0  9071
2 25544  51
6416 332
7607 0003607  96
2642 263
8919 15
48690918 21224


Satellite: ISS
Catalog Number: 25544
Epoch time:      20099
61388812   =   yrday
fracday
Element set:     907
Inclination:       51
6416  deg
RA of node:       332
7607  deg
Eccentricity:     
0003607     
Arg of perigee:    96
2642  deg
Mean anomaly:     263
8919  deg
Mean motion:   15
48690918  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2122
Checksum:              329


Coasting Arc #9 (Orbit 2131)
---------------------------------------

Vector Time (GMT): 2020/100/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915574
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1920465
93                 A    =         6797955
52  meter
 Y    =       -5029140
70  meter          E    =           
0011262
 Z    =       -4162595
49                 I    =           51
43756
 XDOT =       6657
845968                 Wp   =          104
97252
 YDOT =       -538
518575  meter/sec      RA   =          328
95659  deg
 ZDOT =       3727
939912                 TA   =          203
55632
                                          MA   =          203
60794
                                          Ha   =            230
942  n
mi
                                          Hp   =            221
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6300741
24                 X    =         1996780
28
 Y    =      -16499805
43  feet           Y    =        -5007238
26  meter
 Z    =      -13656809
35                 Z    =        -4153080
81
 XDOT =      21843
326666                 XDOT =        6645
264600
 YDOT =      -1766
793225  feet/sec       YDOT =        -464
135895  meter/sec
 ZDOT =      12230
773988                 ZDOT =        3760
250980

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17649812
96                 X    =         5379662
99
 Y    =        1275264
75  feet           Y    =          388700
70  meter
 Z    =      -13612830
83                 Z    =        -4149190
84
 XDOT =       8160
502792                 XDOT =        2487
321251
 YDOT =      18998
943716  feet/sec       YDOT =        5790
878045  meter/sec
 ZDOT =      12378
945163                 ZDOT =        3773
102486


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
25916448  
00016717  00000-0  10270-3 0  9087
2 25544  51
6406 329
5704 0003741  97
6744 262
4831 15
48687688 21321


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
25916448   =   yrday
fracday
Element set:     908
Inclination:       51
6406  deg
RA of node:       329
5704  deg
Eccentricity:     
0003741     
Arg of perigee:    97
6744  deg
Mean anomaly:     262
4831  deg
Mean motion:   15
48687688  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2132
Checksum:              322


Coasting Arc #10 (Orbit 2133)
---------------------------------------

Vector Time (GMT): 2020/100/08:05:06
000
Vector Time (MET): N/A
Weight (LBS)     : 915574
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3785837
13                 A    =         6794030
09  meter
 Y    =        2436749
76  meter          E    =           
0008552
 Z    =        5082189
36                 I    =           51
42433
 XDOT =      -5544
532330                 Wp   =          113
90239
 YDOT =       5002
441252  meter/sec      RA   =          328
56556  deg
 ZDOT =       1726
030073                 TA   =          319
32422
                                          MA   =          319
38806
                                          Ha   =            230
687  n
mi
                                          Hp   =            221
841

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12420725
50                 X    =         3733620
64
 Y    =        7994585
83  feet           Y    =         2478794
06  meter
 Z    =       16673849
59                 Z    =         5100452
70
 XDOT =     -18190
722866                 XDOT =       -5608
443193
 YDOT =      16412
208833  feet/sec       YDOT =        4940
081112  meter/sec
 ZDOT =       5662
828325                 ZDOT =        1698
941024

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3896747
47                 X    =         1187728
63
 Y    =       14149551
01  feet           Y    =         4312783
15  meter
 Z    =       16757405
83                 Z    =         5107657
30
 XDOT =     -23496
301137                 XDOT =       -7161
672587
 YDOT =       -110
257253  feet/sec       YDOT =         -33
606411  meter/sec
 ZDOT =       5538
281296                 ZDOT =        1688
068139


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
38821837  
00016717  00000-0  10270-3 0  9099
2 25544  51
6422 328
9332 0003619  99
5058 260
6501 15
48738398 21343


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
38821837   =   yrday
fracday
Element set:     909
Inclination:       51
6422  deg
RA of node:       328
9332  deg
Eccentricity:     
0003619     
Arg of perigee:    99
5058  deg
Mean anomaly:     260
6501  deg
Mean motion:   15
48738398  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2134
Checksum:              316


Coasting Arc #11 (Orbit 2137)
---------------------------------------

Vector Time (GMT): 2020/100/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3820772
02                 A    =         6794209
80  meter
 Y    =        2370263
58  meter          E    =           
0008541
 Z    =        5087731
98                 I    =           51
41501
 XDOT =      -5448
189063                 Wp   =          114
12184
 YDOT =       5114
797218  meter/sec      RA   =          327
28328  deg
 ZDOT =       1702
904951                 TA   =          319
33314
                                          MA   =          319
39689
                                          Ha   =            230
805  n
mi
                                          Hp   =            221
943

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12535341
29                 X    =         3769269
46
 Y    =        7776455
33  feet           Y    =         2412702
50  meter
 Z    =       16692034
05                 Z    =         5106166
79
 XDOT =     -17874
636033                 XDOT =       -5513
251159
 YDOT =      16780
830768  feet/sec       YDOT =        5053
508006  meter/sec
 ZDOT =       5586
958500                 ZDOT =        1676
281127

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13811152
44                 X    =         4209639
26
 Y    =       -4902773
36  feet           Y    =        -1494365
32  meter
 Z    =       16776379
85                 Z    =         5113440
58
 XDOT =       1665
617532                 XDOT =         507
680224
 YDOT =      23454
247376  feet/sec       YDOT =        7148
854600  meter/sec
 ZDOT =       5464
538931                 ZDOT =        1665
591466


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
64632896  
00016717  00000-0  10270-3 0  9105
2 25544  51
6404 327
6548 0003650 100
2581 259
8981 15
48668712 21382


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
64632896   =   yrday
fracday
Element set:     910
Inclination:       51
6404  deg
RA of node:       327
6548  deg
Eccentricity:     
0003650     
Arg of perigee:   100
2581  deg
Mean anomaly:     259
8981  deg
Mean motion:   15
48668712  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2138
Checksum:              311


Coasting Arc #12 (Orbit 2152)
---------------------------------------

Vector Time (GMT): 2020/101/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4086971
36                 A    =         6794196
35  meter
 Y    =       -1964354
44  meter          E    =           
0016576
 Z    =       -5074446
12                 I    =           51
38731
 XDOT =       4902
570971                 Wp   =           82
40099
 YDOT =      -5589
793388  meter/sec      RA   =          322
32309  deg
 ZDOT =      -1787
589624                 TA   =          170
20761
                                          MA   =          170
17526
                                          Ha   =            230
854  n
mi
                                          Hp   =            221
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13408698
68                 X    =        -4040052
55
 Y    =       -6444732
42  feet           Y    =        -2009795
67  meter
 Z    =      -16648445
27                 Z    =        -5094185
26
 XDOT =      16084
550431                 XDOT =        4973
396520
 YDOT =     -18339
217153  feet/sec       YDOT =       -5534
573391  meter/sec
 ZDOT =      -5864
795355                 ZDOT =       -1763
602377

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13197959
12                 X    =        -4022737
94
 Y    =        6642673
00  feet           Y    =         2024686
73  meter
 Z    =      -16738795
56                 Z    =        -5101984
89
 XDOT =      -4283
469763                 XDOT =       -1305
601584
 YDOT =     -22987
316634  feet/sec       YDOT =       -7006
534110  meter/sec
 ZDOT =      -5754
437359                 ZDOT =       -1753
952507


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
61423730  
00016717  00000-0  10270-3 0  9119
2 25544  51
6400 322
8679 0003685 104
8038 255
3520 15
48711396 21539


Satellite: ISS
Catalog Number: 25544
Epoch time:      20101
61423730   =   yrday
fracday
Element set:     911
Inclination:       51
6400  deg
RA of node:       322
8679  deg
Eccentricity:     
0003685     
Arg of perigee:   104
8038  deg
Mean anomaly:     255
3520  deg
Mean motion:   15
48711396  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2153
Checksum:              282


Coasting Arc #13 (Orbit 2168)
---------------------------------------

Vector Time (GMT): 2020/102/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4302910
97                 A    =         6794401
22  meter
 Y    =        1505955
69  meter          E    =           
0009149
 Z    =        5032041
53                 I    =           51
36193
 XDOT =      -4328
349581                 Wp   =          116
81959
 YDOT =       6036
829307  meter/sec      RA   =          317
36167  deg
 ZDOT =       1887
806556                 TA   =          314
76209
                                          MA   =          314
83649
                                          Ha   =            230
771  n
mi
                                          Hp   =            221
933

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14117161
97                 X    =         4261308
10
 Y    =        4940799
51  feet           Y    =         1553841
30  meter
 Z    =       16509322
60                 Z    =         5052842
54
 XDOT =     -14200
621985                 XDOT =       -4404
703474
 YDOT =      19805
870429  feet/sec       YDOT =        5987
999707  meter/sec
 ZDOT =       6193
591062                 ZDOT =        1866
595452

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12293053
69                 X    =         3746922
76
 Y    =       -8332618
97  feet           Y    =        -2539782
26  meter
 Z    =       16604571
25                 Z    =         5061073
32
 XDOT =       6868
997212                 XDOT =        2093
670350
 YDOT =      22324
912451  feet/sec       YDOT =        6804
633315  meter/sec
 ZDOT =       6095
934857                 ZDOT =        1858
040944


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
64667188  
00016717  00000-0  10270-3 0  9121
2 25544  51
6400 317
7623 0003702 106
7343 253
4213 15
48680522 21692


Satellite: ISS
Catalog Number: 25544
Epoch time:      20102
64667188   =   yrday
fracday
Element set:     912
Inclination:       51
6400  deg
RA of node:       317
7623  deg
Eccentricity:     
0003702     
Arg of perigee:   106
7343  deg
Mean anomaly:     253
4213  deg
Mean motion:   15
48680522  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2169
Checksum:              287


Coasting Arc #14 (Orbit 2183)
---------------------------------------

Vector Time (GMT): 2020/103/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4474678
68                 A    =         6794398
85  meter
 Y    =       -1053124
89  meter          E    =           
0016183
 Z    =       -5017764
86                 I    =           51
33806
 XDOT =       3706
432555                 Wp   =           83
37524
 YDOT =      -6393
264112  meter/sec      RA   =          312
39891  deg
 ZDOT =      -1967
125748                 TA   =          167
41100
                                          MA   =          167
37053
                                          Ha   =            230
882  n
mi
                                          Hp   =            221
679

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14680704
32                 X    =        -4438196
18
 Y    =       -3455134
16  feet           Y    =        -1102959
89  meter
 Z    =      -16462483
14                 Z    =        -5039412
63
 XDOT =      12160
211795                 XDOT =        3787
203684
 YDOT =     -20975
275957  feet/sec       YDOT =       -6351
364504  meter/sec
 ZDOT =      -6453
824632                 ZDOT =       -1948
925137

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11264622
05                 X    =        -3433456
80
 Y    =        9863801
98  feet           Y    =         3006486
84  meter
 Z    =      -16561644
94                 Z    =        -5047989
38
 XDOT =      -9290
641297                 XDOT =       -2831
787467
 YDOT =     -21285
357013  feet/sec       YDOT =       -6487
776818  meter/sec
 ZDOT =      -6369
951904                 ZDOT =       -1941
561340


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
61457596  
00016717  00000-0  10270-3 0  9130
2 25544  51
6396 312
9765 0003897 111
7286 248
4279 15
48720298 21845


Satellite: ISS
Catalog Number: 25544
Epoch time:      20103
61457596   =   yrday
fracday
Element set:     913
Inclination:       51
6396  deg
RA of node:       312
9765  deg
Eccentricity:     
0003897     
Arg of perigee:   111
7286  deg
Mean anomaly:     248
4279  deg
Mean motion:   15
48720298  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2184
Checksum:              339


Coasting Arc #15 (Orbit 2199)
---------------------------------------

Vector Time (GMT): 2020/104/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4589814
10                 A    =         6794576
14  meter
 Y    =         555299
87  meter          E    =           
0009736
 Z    =        4973337
65                 I    =           51
31625
 XDOT =      -3059
065361                 Wp   =          120
08456
 YDOT =       6716
690542  meter/sec      RA   =          307
43444  deg
 ZDOT =       2065
372048                 TA   =          309
67675
                                          MA   =          309
76258
                                          Ha   =            230
699  n
mi
                                          Hp   =            221
946

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15058445
20                 X    =         4559105
77
 Y    =        1821849
96  feet           Y    =          606454
66  meter
 Z    =       16316724
58                 Z    =         4995558
64
 XDOT =     -10036
303679                 XDOT =       -3143
978441
 YDOT =      22036
386293  feet/sec       YDOT =        6682
007088  meter/sec
 ZDOT =       6776
155013                 ZDOT =        2050
306138

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9960939
60                 X    =         3036094
39
 Y    =      -11292579
25  feet           Y    =        -3441978
16  meter
 Z    =       16418548
85                 Z    =         5004373
69
 XDOT =      11640
711560                 XDOT =        3548
088883
 YDOT =      20056
110065  feet/sec       YDOT =        6113
102348  meter/sec
 ZDOT =       6706
640411                 ZDOT =        2044
183997


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
64700648  
00016717  00000-0  10270-3 0  9144
2 25544  51
6391 307
8712 0003745 115
9400 244
2136 15
48703601 22005


Satellite: ISS
Catalog Number: 25544
Epoch time:      20104
64700648   =   yrday
fracday
Element set:     914
Inclination:       51
6391  deg
RA of node:       307
8712  deg
Eccentricity:     
0003745     
Arg of perigee:   115
9400  deg
Mean anomaly:     244
2136  deg
Mean motion:   15
48703601  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2200
Checksum:              273


Coasting Arc #16 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2020/105/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4659883
87                 A    =         6794591
90  meter
 Y    =         -76338
21  meter          E    =           
0015492
 Z    =       -4958247
96                 I    =           51
29905
 XDOT =       2386
203775                 Wp   =           84
26941
 YDOT =      -6943
758976  meter/sec      RA   =          302
46902  deg
 ZDOT =      -2139
990979                 TA   =          164
74304
                                          MA   =          164
69627
                                          Ha   =            230
801  n
mi
                                          Hp   =            221
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15288332
89                 X    =        -4634599
60
 Y    =        -250453
45  feet           Y    =         -128306
93  meter
 Z    =      -16267217
72                 Z    =        -4980822
41
 XDOT =       7828
752542                 XDOT =        2474
068430
 YDOT =     -22781
361470  feet/sec       YDOT =       -6916
583448  meter/sec
 ZDOT =      -7020
967779                 ZDOT =       -2128
186406

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8581482
03                 X    =        -2615635
72
 Y    =       12521052
09  feet           Y    =         3816416
68  meter
 Z    =      -16370694
63                 Z    =        -4989787
72
 XDOT =     -13744
907245                 XDOT =       -4189
447728
 YDOT =     -18510
250267  feet/sec       YDOT =       -5641
924281  meter/sec
 ZDOT =      -6966
402039                 ZDOT =       -2123
359341


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
61490669  
00016717  00000-0  10270-3 0  9152
2 25544  51
6410 303
0859 0003883 119
1684 240
9855 15
48737339 22152


Satellite: ISS
Catalog Number: 25544
Epoch time:      20105
61490669   =   yrday
fracday
Element set:     915
Inclination:       51
6410  deg
RA of node:       303
0859  deg
Eccentricity:     
0003883     
Arg of perigee:   119
1684  deg
Mean anomaly:     240
9855  deg
Mean motion:   15
48737339  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              318


Coasting Arc #17 (Orbit 2230)
---------------------------------------

Vector Time (GMT): 2020/106/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4667599
41                 A    =         6794724
12  meter
 Y    =        -436813
27  meter          E    =           
0010227
 Z    =        4912819
64                 I    =           51
28187
 XDOT =      -1693
612568                 Wp   =          122
28159
 YDOT =       7132
483389  meter/sec      RA   =          297
50111  deg
 ZDOT =       2234
457749                 TA   =          305
72783
                                          MA   =          305
82292
                                          Ha   =            230
602  n
mi
                                          Hp   =            221
954

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15313646
34                 X    =         4648273
50
 Y    =       -1433114
40  feet           Y    =         -384724
89  meter
 Z    =       16118174
66                 Z    =         4935445
98
 XDOT =      -5556
471679                 XDOT =       -1784
097911
 YDOT =      23400
536053  feet/sec       YDOT =        7113
038281  meter/sec
 ZDOT =       7330
898126                 ZDOT =        2226
011077

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6958915
87                 X    =         2121077
56
 Y    =      -13593376
31  feet           Y    =        -4143261
10  meter
 Z    =       16221921
77                 Z    =         4944441
76
 XDOT =      15735
416673                 XDOT =        4796
155002
 YDOT =      16791
420903  feet/sec       YDOT =        5118
025091  meter/sec
 ZDOT =       7291
729846                 ZDOT =        2222
519257


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
64733029  
00016717  00000-0  10270-3 0  9167
2 25544  51
6403 297
9800 0003772 123
4978 236
6533 15
48739524 22313


Satellite: ISS
Catalog Number: 25544
Epoch time:      20106
64733029   =   yrday
fracday
Element set:     916
Inclination:       51
6403  deg
RA of node:       297
9800  deg
Eccentricity:     
0003772     
Arg of perigee:   123
4978  deg
Mean anomaly:     236
6533  deg
Mean motion:   15
48739524  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2231
Checksum:              314


Coasting Arc #18 (Orbit 2245)
---------------------------------------

Vector Time (GMT): 2020/107/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4633911
44                 A    =         6794831
82  meter
 Y    =         919304
42  meter          E    =           
0014800
 Z    =       -4897104
04                 I    =           51
26800
 XDOT =        996
684437                 Wp   =           85
17617
 YDOT =      -7224
589219  meter/sec      RA   =          292
53408  deg
 ZDOT =      -2304
180283                 TA   =          162
13182
                                          MA   =          162
07973
                                          Ha   =            230
744  n
mi
                                          Hp   =            221
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15203121
53                 X    =        -4620059
75
 Y    =        3016090
61  feet           Y    =          867562
09  meter
 Z    =      -16066614
31                 Z    =        -4919580
04
 XDOT =       3269
962063                 XDOT =        1088
590197
 YDOT =     -23702
720535  feet/sec       YDOT =       -7212
929748  meter/sec
 ZDOT =      -7559
646599                 ZDOT =       -2299
115451

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5316851
51                 X    =        -1620576
34
 Y    =       14444365
91  feet           Y    =         4402642
73  meter
 Z    =      -16169699
62                 Z    =        -4928524
44
 XDOT =     -17420
142417                 XDOT =       -5309
659409
 YDOT =     -14830
718601  feet/sec       YDOT =       -4520
403029  meter/sec
 ZDOT =      -7535
993944                 ZDOT =       -2296
970954


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
61522642  
00016717  00000-0  10270-3 0  9173
2 25544  51
6405 293
1955 0003900 125
7671 234
3842 15
48741800 22466


Satellite: ISS
Catalog Number: 25544
Epoch time:      20107
61522642   =   yrday
fracday
Element set:     917
Inclination:       51
6405  deg
RA of node:       293
1955  deg
Eccentricity:     
0003900     
Arg of perigee:   125
7671  deg
Mean anomaly:     234
3842  deg
Mean motion:   15
48741800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2246
Checksum:              293


Coasting Arc #19 (Orbit 2253)
---------------------------------------

Vector Time (GMT): 2020/108/01:53:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916383
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4608391
04                 A    =         6795254
54  meter
 Y    =       -1436261
91  meter          E    =           
0010833
 Z    =        4776992
06                 I    =           51
26248
 XDOT =       -438
056863                 Wp   =          120
59194
 YDOT =       7203
371547  meter/sec      RA   =          290
13706  deg
 ZDOT =       2578
577604                 TA   =          303
80224
                                          MA   =          303
90535
                                          Ha   =            230
488  n
mi
                                          Hp   =            222
037

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15119393
18                 X    =         4600905
44
 Y    =       -4712145
37  feet           Y    =        -1384769
34  meter
 Z    =       15672546
13                 Z    =         4799359
58
 XDOT =      -1437
194434                 XDOT =        -531
099743
 YDOT =      23633
108749  feet/sec       YDOT =        7197
952712  meter/sec
 ZDOT =       8459
900275                 ZDOT =        2576
223541

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5268872
09                 X    =        -1605952
21
 Y    =       14826067
73  feet           Y    =         4518985
45  meter
 Z    =       15775163
04                 Z    =         4808269
69
 XDOT =     -16897
390569                 XDOT =       -5150
324645
 YDOT =     -15028
498667  feet/sec       YDOT =       -4580
686394  meter/sec
 ZDOT =       8448
684487                 ZDOT =        2575
159032


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
13143575  
00016717  00000-0  10270-3 0  9186
2 25544  51
6395 290
6467 0003498 124
7902 235
3577 15
48750448 22545


Satellite: ISS
Catalog Number: 25544
Epoch time:      20108
13143575   =   yrday
fracday
Element set:     918
Inclination:       51
6395  deg
RA of node:       290
6467  deg
Eccentricity:     
0003498     
Arg of perigee:   124
7902  deg
Mean anomaly:     235
3577  deg
Mean motion:   15
48750448  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2254
Checksum:              325
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