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

 
Date: July 24th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14119 0213 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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


205/22:24:29 000 0 0 0 0 0 0
N/A 0 0 0 0 227 2
000/00:00:00 000 0 0 0 0 219 2

207/04:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 1
000/00:00:00 000 0 0 0 0 219 4

210/10:44:30 000 0 0 0 0 0 0
N/A 0 0 0 0 226 6
000/00:00:00 000 0 0 0 0 219 9

212/15:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 2
000/00:00:00 000 0 0 0 0 220 2

213/11:38:30 000 0 0 0 0 0 0
N/A 0 0 0 0 226 2
000/00:00:00 000 0 0 0 0 220 3

216/18:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 8
000/00:00:00 000 0 0 0 0 220 9

Coasting Arc #1 (Orbit 2103)
---------------------------------------

Vector Time (GMT): 2019/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5716236
47                 A    =         6795491
68  meter
 Y    =       -2569747
96  meter          E    =           
0016514
 Z    =        2600478
79                 I    =           51
67773
 XDOT =       4103
075166                 Wp   =          124
94844
 YDOT =       3801
170480  meter/sec      RA   =          174
93815  deg
 ZDOT =      -5248
546184                 TA   =           25
80940
                                          MA   =           25
72710
                                          Ha   =            227
090  n
mi
                                          Hp   =            219
045

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18754056
66                 X    =         5731915
72
 Y    =       -8430931
63  feet           Y    =        -2505737
48  meter
 Z    =        8531754
55                 Z    =         2628283
80
 XDOT =      13461
532696                 XDOT =        4085
758736
 YDOT =      12471
031759  feet/sec       YDOT =        3846
957453  meter/sec
 ZDOT =     -17219
639711                 ZDOT =       -5228
656977

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16862457
14                 X    =        -5139676
94
 Y    =      -11673810
94  feet           Y    =        -3558177
57  meter
 Z    =        8658277
10                 Z    =         2639042
86
 XDOT =       2834
075747                 XDOT =         863
826288
 YDOT =     -16832
865357  feet/sec       YDOT =       -5130
657361  meter/sec
 ZDOT =     -17129
506703                 ZDOT =       -5221
073643


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   19205
53757005  
00016717  00000-0  10270-3 0  9006
2 25544  51
6383 175
9689 0006402 176
6753 183
4441 15
51001776 21045


Satellite: ISS
Catalog Number: 25544
Epoch time:      19205
53757005   =   yrday
fracday
Element set:     900
Inclination:       51
6383  deg
RA of node:       175
9689  deg
Eccentricity:     
0006402     
Arg of perigee:   176
6753  deg
Mean anomaly:     183
4441  deg
Mean motion:   15
51001776  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2104
Checksum:              305


Coasting Arc #2 (Orbit 2110)
---------------------------------------

Vector Time (GMT): 2019/205/22:24:29
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4420723
07                 A    =         6790744
20  meter
 Y    =       -2859251
69  meter          E    =           
0013521
 Z    =        4286928
05                 I    =           51
67543
 XDOT =       5774
056995                 Wp   =          135
21341
 YDOT =      -3563
479776  meter/sec      RA   =          172
83088  deg
 ZDOT =       3561
301586                 TA   =          278
38263
                                          MA   =          278
53588
                                          Ha   =            227
228  n
mi
                                          Hp   =            219
159

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14503684
63                 X    =        -4409244
90
 Y    =       -9380747
02  feet           Y    =        -2908623
43  meter
 Z    =       14064724
58                 Z    =         4265481
68
 XDOT =      18943
756545                 XDOT =        5796
177019
 YDOT =     -11691
206613  feet/sec       YDOT =       -3498
786771  meter/sec
 ZDOT =      11684
060322                 ZDOT =        3589
403067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7371597
14                 X    =         2246862
81
 Y    =      -15708013
48  feet           Y    =        -4787802
51  meter
 Z    =       13967448
87                 Z    =         4257278
41
 XDOT =      12931
991756                 XDOT =        3941
671087
 YDOT =      16619
663720  feet/sec       YDOT =        5065
673502  meter/sec
 ZDOT =      11812
002400                 ZDOT =        3600
298332


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   19205
98859232  
00016717  00000-0  10270-3 0  9011
2 25544  51
6376 173
7281 0006703 179
9583 180
1570 15
51014125 21119


Satellite: ISS
Catalog Number: 25544
Epoch time:      19205
98859232   =   yrday
fracday
Element set:     901
Inclination:       51
6376  deg
RA of node:       173
7281  deg
Eccentricity:     
0006703     
Arg of perigee:   179
9583  deg
Mean anomaly:     180
1570  deg
Mean motion:   15
51014125  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2111
Checksum:              304


Coasting Arc #3 (Orbit 2125)
---------------------------------------

Vector Time (GMT): 2019/206/22:24:29
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3982269
79                 A    =         6789294
30  meter
 Y    =        2915171
94  meter          E    =           
0010169
 Z    =       -4669195
21                 I    =           51
70505
 XDOT =      -6070
498051                 Wp   =          108
40776
 YDOT =       3651
575340  meter/sec      RA   =          167
87074  deg
 ZDOT =      -2905
915104                 TA   =          132
71698
                                          MA   =          132
63132
                                          Ha   =            227
154  n
mi
                                          Hp   =            219
261

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13065189
59                 X    =         3972055
75
 Y    =        9564212
39  feet           Y    =         2959647
75  meter
 Z    =      -15318881
93                 Z    =        -4649875
52
 XDOT =     -19916
332187                 XDOT =       -6096
764607
 YDOT =      11980
234056  feet/sec       YDOT =        3583
544139  meter/sec
 ZDOT =      -9533
842206                 ZDOT =       -2935
466636

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7494691
72                 X    =        -2284382
04
 Y    =       14445748
46  feet           Y    =         4403064
13  meter
 Z    =      -15231264
83                 Z    =        -4642489
52
 XDOT =     -13750
070192                 XDOT =       -4191
021394
 YDOT =     -17298
919145  feet/sec       YDOT =       -5272
710555  meter/sec
 ZDOT =      -9668
399123                 ZDOT =       -2946
928053


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   19206
95507013  
00016717  00000-0  10270-3 0  9027
2 25544  51
6390 168
9328 0006639 180
7328 179
3814 15
51017206 21268


Satellite: ISS
Catalog Number: 25544
Epoch time:      19206
95507013   =   yrday
fracday
Element set:     902
Inclination:       51
6390  deg
RA of node:       168
9328  deg
Eccentricity:     
0006639     
Arg of perigee:   180
7328  deg
Mean anomaly:     179
3814  deg
Mean motion:   15
51017206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2126
Checksum:              309


Coasting Arc #4 (Orbit 2129)
---------------------------------------

Vector Time (GMT): 2019/207/04:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3904511
51                 A    =         6789115
71  meter
 Y    =        2912396
64  meter          E    =           
0010169
 Z    =       -4736035
54                 I    =           51
71464
 XDOT =      -6105
993117                 Wp   =          108
53858
 YDOT =       3700
276826  meter/sec      RA   =          166
59340  deg
 ZDOT =      -2766
504479                 TA   =          134
09672
                                          MA   =          134
01299
                                          Ha   =            227
126  n
mi
                                          Hp   =            219
447

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12810077
15                 X    =         3894658
97
 Y    =        9555107
08  feet           Y    =         2956004
95  meter
 Z    =      -15538174
35                 Z    =        -4717092
67
 XDOT =     -20032
785816                 XDOT =       -6133
478802
 YDOT =      12140
015832  feet/sec       YDOT =        3631
841878  meter/sec
 ZDOT =      -9076
458263                 ZDOT =       -2796
231378

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14583615
34                 X    =         4445085
95
 Y    =        6736364
62  feet           Y    =         2053243
94  meter
 Z    =      -15452267
32                 Z    =        -4709851
08
 XDOT =     -16602
984334                 XDOT =       -5060
589625
 YDOT =      14874
080368  feet/sec       YDOT =        4533
619696  meter/sec
 ZDOT =      -9211
820873                 ZDOT =       -2807
763002


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   19207
21279611  
00016717  00000-0  10270-3 0  9038
2 25544  51
6411 167
6561 0006728 184
3688 175
7405 15
50987495 21301


Satellite: ISS
Catalog Number: 25544
Epoch time:      19207
21279611   =   yrday
fracday
Element set:     903
Inclination:       51
6411  deg
RA of node:       167
6561  deg
Eccentricity:     
0006728     
Arg of perigee:   184
3688  deg
Mean anomaly:     175
7405  deg
Mean motion:   15
50987495  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2130
Checksum:              323


Coasting Arc #5 (Orbit 2145)
---------------------------------------

Vector Time (GMT): 2019/208/04:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3474423
85                 A    =         6787915
46  meter
 Y    =       -3000502
52  meter          E    =           
0010845
 Z    =        4999630
59                 I    =           51
74310
 XDOT =       6308
642842                 Wp   =          157
00292
 YDOT =      -3821
815935  meter/sec      RA   =          161
63501  deg
 ZDOT =       2079
190563                 TA   =          272
72178
                                          MA   =          272
84591
                                          Ha   =            226
989  n
mi
                                          Hp   =            219
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11399028
37                 X    =        -3464898
42
 Y    =       -9844168
37  feet           Y    =        -3039303
23  meter
 Z    =       16402987
51                 Z    =         4982776
07
 XDOT =      20697
647118                 XDOT =        6340
811124
 YDOT =     -12538
766192  feet/sec       YDOT =       -3751
088614  meter/sec
 ZDOT =       6821
491350                 ZDOT =        2109
913137

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13389919
39                 X    =        -4081247
43
 Y    =       -7075073
47  feet           Y    =        -2156482
39  meter
 Z    =       16326570
13                 Z    =         4976338
57
 XDOT =      16877
413022                 XDOT =        5144
235489
 YDOT =     -15791
317668  feet/sec       YDOT =       -4813
193625  meter/sec
 ZDOT =       6961
410909                 ZDOT =        2121
838045


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   19208
24370167  
00016717  00000-0  10270-3 0  9041
2 25544  51
6410 162
5414 0006645 188
0207 172
0839 15
51020022 21460


Satellite: ISS
Catalog Number: 25544
Epoch time:      19208
24370167   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:       162
5414  deg
Eccentricity:     
0006645     
Arg of perigee:   188
0207  deg
Mean anomaly:     172
0839  deg
Mean motion:   15
51020022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2146
Checksum:              275


Coasting Arc #6 (Orbit 2160)
---------------------------------------

Vector Time (GMT): 2019/209/04:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3003755
56                 A    =         6787150
76  meter
 Y    =        3170265
95  meter          E    =           
0012977
 Z    =       -5205241
04                 I    =           51
77068
 XDOT =      -6438
127793                 Wp   =          108
44498
 YDOT =       3920
308129  meter/sec      RA   =          156
67735  deg
 ZDOT =      -1334
265507                 TA   =          148
77376
                                          MA   =          148
69661
                                          Ha   =            226
888  n
mi
                                          Hp   =            219
752

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9854841
07                 X    =         2993365
45
 Y    =       10401135
00  feet           Y    =         3203798
59  meter
 Z    =      -17077562
46                 Z    =        -5190674
88
 XDOT =     -21122
466512                 XDOT =       -6475
006243
 YDOT =      12861
903312  feet/sec       YDOT =        3848
106425  meter/sec
 ZDOT =      -4377
511505                 ZDOT =       -1365
628369

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12145302
59                 X    =         3701888
23
 Y    =        7748764
82  feet           Y    =         2361823
52  meter
 Z    =      -17011552
25                 Z    =        -5185121
13
 XDOT =     -16889
613758                 XDOT =       -5147
954274
 YDOT =      16597
220013  feet/sec       YDOT =        5058
832660  meter/sec
 ZDOT =      -4520
374298                 ZDOT =       -1377
810086


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   19209
21017707  
00016717  00000-0  10270-3 0  9058
2 25544  51
6402 157
7465 0006659 191
2753 168
8250 15
50984109 21611


Satellite: ISS
Catalog Number: 25544
Epoch time:      19209
21017707   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:       157
7465  deg
Eccentricity:     
0006659     
Arg of perigee:   191
2753  deg
Mean anomaly:     168
8250  deg
Mean motion:   15
50984109  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2161
Checksum:              313


Coasting Arc #7 (Orbit 2176)
---------------------------------------

Vector Time (GMT): 2019/210/04:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2566104
97                 A    =         6786538
64  meter
 Y    =       -3361974
19  meter          E    =           
0007648
 Z    =        5307340
28                 I    =           51
80007
 XDOT =       6498
088879                 Wp   =          173
19855
 YDOT =      -4020
655702  meter/sec      RA   =          151
72124  deg
 ZDOT =        587
425403                 TA   =          271
16044
                                          MA   =          271
24806
                                          Ha   =            226
741  n
mi
                                          Hp   =            219
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8418979
56                 X    =        -2554099
50
 Y    =      -11030099
06  feet           Y    =        -3390603
75  meter
 Z    =       17412533
73                 Z    =         5294903
97
 XDOT =      21319
189234                 XDOT =        6539
712704
 YDOT =     -13191
127631  feet/sec       YDOT =       -3947
756853  meter/sec
 ZDOT =       1927
248696                 ZDOT =         619
090886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11049042
25                 X    =        -3367748
08
 Y    =       -8509942
85  feet           Y    =        -2593830
58  meter
 Z    =       17356214
20                 Z    =         5290174
09
 XDOT =      16653
708841                 XDOT =        5076
050455
 YDOT =     -17347
433482  feet/sec       YDOT =       -5287
497725  meter/sec
 ZDOT =       2071
521694                 ZDOT =         631
399812


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   19210
24107961  
00016717  00000-0  10270-3 0  9066
2 25544  51
6410 152
6316 0006562 195
3032 164
7922 15
51023237 21772


Satellite: ISS
Catalog Number: 25544
Epoch time:      19210
24107961   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:       152
6316  deg
Eccentricity:     
0006562     
Arg of perigee:   195
3032  deg
Mean anomaly:     164
7922  deg
Mean motion:   15
51023237  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2177
Checksum:              282


Coasting Arc #8 (Orbit 2180)
---------------------------------------

Vector Time (GMT): 2019/210/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3602864
96                 A    =         6787315
89  meter
 Y    =       -2598636
30  meter          E    =           
0009275
 Z    =        5131859
94                 I    =           51
80920
 XDOT =       5779
810369                 Wp   =          165
46262
 YDOT =      -4757
193581  meter/sec      RA   =          150
46393  deg
 ZDOT =       1639
449799                 TA   =          268
68900
                                          MA   =          268
79527
                                          Ha   =            226
611  n
mi
                                          Hp   =            219
856

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11820423
10                 X    =        -3598465
89
 Y    =       -8525709
66  feet           Y    =        -2638902
15  meter
 Z    =       16836810
82                 Z    =         5114369
13
 XDOT =      18962
632443                 XDOT =        5824
613676
 YDOT =     -15607
590490  feet/sec       YDOT =       -4692
309389  meter/sec
 ZDOT =       5378
772305                 ZDOT =        1667
633781

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4654511
29                 X    =        -1418695
04
 Y    =       13907253
05  feet           Y    =         4238930
73  meter
 Z    =       16757450
98                 Z    =         5107671
06
 XDOT =     -19452
943162                 XDOT =       -5929
257076
 YDOT =     -13183
836653  feet/sec       YDOT =       -4018
433412  meter/sec
 ZDOT =       5507
271190                 ZDOT =        1678
616259


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   19210
49880574  
00016717  00000-0  10270-3 0  9072
2 25544  51
6400 151
3537 0006295 196
9410 163
1532 15
51033446 21810


Satellite: ISS
Catalog Number: 25544
Epoch time:      19210
49880574   =   yrday
fracday
Element set:     907
Inclination:       51
6400  deg
RA of node:       151
3537  deg
Eccentricity:     
0006295     
Arg of perigee:   196
9410  deg
Mean anomaly:     163
1532  deg
Mean motion:   15
51033446  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2181
Checksum:              296


Coasting Arc #9 (Orbit 2195)
---------------------------------------

Vector Time (GMT): 2019/211/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3166429
00                 A    =         6786743
13  meter
 Y    =        2864283
97  meter          E    =           
0012885
 Z    =       -5285376
51                 I    =           51
83565
 XDOT =      -5850
740163                 Wp   =          108
71794
 YDOT =       4857
434954  meter/sec      RA   =          145
50920  deg
 ZDOT =       -878
541434                 TA   =          152
92220
                                          MA   =          152
85493
                                          Ha   =            226
468  n
mi
                                          Hp   =            220
117

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10388546
60                 X    =         3159837
38
 Y    =        9397257
11  feet           Y    =         2899657
02  meter
 Z    =      -17340474
13                 Z    =        -5270011
11
 XDOT =     -19195
341741                 XDOT =       -5900
355172
 YDOT =      15936
466386  feet/sec       YDOT =        4791
730568  meter/sec
 ZDOT =      -2882
353787                 ZDOT =        -907
081502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5685275
44                 X    =         1732871
95
 Y    =      -12896506
95  feet           Y    =        -3930855
32  meter
 Z    =      -17270788
52                 Z    =        -5264136
34
 XDOT =      20146
323021                 XDOT =        6140
599257
 YDOT =      12890
076972  feet/sec       YDOT =        3928
895461  meter/sec
 ZDOT =      -3012
504198                 ZDOT =        -918
211280


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   19211
46527621  
00016717  00000-0  10270-3 0  9082
2 25544  51
6401 146
5576 0006178 199
6609 160
4304 15
51004723 21969


Satellite: ISS
Catalog Number: 25544
Epoch time:      19211
46527621   =   yrday
fracday
Element set:     908
Inclination:       51
6401  deg
RA of node:       146
5576  deg
Eccentricity:     
0006178     
Arg of perigee:   199
6609  deg
Mean anomaly:     160
4304  deg
Mean motion:   15
51004723  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2196
Checksum:              305


Coasting Arc #10 (Orbit 2211)
---------------------------------------

Vector Time (GMT): 2019/212/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2770189
97                 A    =         6786411
30  meter
 Y    =       -3146970
40  meter          E    =           
0005950
 Z    =        5336679
88                 I    =           51
86209
 XDOT =       5857
006674                 Wp   =          181
09840
 YDOT =      -4940
975481  meter/sec      RA   =          140
55857  deg
 ZDOT =        120
861237                 TA   =          267
71862
                                          MA   =          267
78675
                                          Ha   =            226
359  n
mi
                                          Hp   =            220
166

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9088549
76                 X    =        -2760715
78
 Y    =      -10324706
04  feet           Y    =        -3177896
24  meter
 Z    =       17508792
24                 Z    =         5323246
29
 XDOT =      19215
901162                 XDOT =        5911
235718
 YDOT =     -16210
549477  feet/sec       YDOT =       -4875
175119  meter/sec
 ZDOT =        396
526368                 ZDOT =         149
442869

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6762475
22                 X    =        -2061202
45
 Y    =       12066426
31  feet           Y    =         3677846
74  meter
 Z    =       17447904
81                 Z    =         5318121
39
 XDOT =     -20704
029036                 XDOT =       -6310
588050
 YDOT =     -12392
775417  feet/sec       YDOT =       -3777
317947  meter/sec
 ZDOT =        526
894782                 ZDOT =         160
597530


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   19212
49617634  
00016717  00000-0  10270-3 0  9091
2 25544  51
6405 141
4442 0006154 204
1889 155
8974 15
51024014 22120


Satellite: ISS
Catalog Number: 25544
Epoch time:      19212
49617634   =   yrday
fracday
Element set:     909
Inclination:       51
6405  deg
RA of node:       141
4442  deg
Eccentricity:     
0006154     
Arg of perigee:   204
1889  deg
Mean anomaly:     155
8974  deg
Mean motion:   15
51024014  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2212
Checksum:              295


Coasting Arc #11 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2019/212/15:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1832352
12                 A    =         6792456
46  meter
 Y    =       -5382307
10  meter          E    =           
0010020
 Z    =        3704561
63                 I    =           51
89018
 XDOT =       6259
848124                 Wp   =          116
22611
 YDOT =       -861
698868  meter/sec      RA   =          139
53577  deg
 ZDOT =      -4343
427071                 TA   =           19
84162
                                          MA   =           19
80268
                                          Ha   =            226
154  n
mi
                                          Hp   =            220
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6011653
94                 X    =         1874408
18
 Y    =      -17658487
87  feet           Y    =        -5361581
71  meter
 Z    =       12154073
59                 Z    =         3713563
85
 XDOT =      20537
559461                 XDOT =        6290
116093
 YDOT =      -2827
096023  feet/sec       YDOT =        -791
527136  meter/sec
 ZDOT =     -14250
088817                 ZDOT =       -4312
946386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5362646
74                 X    =        -1634534
73
 Y    =       17838098
10  feet           Y    =         5437052
30  meter
 Z    =       12195407
25                 Z    =         3717160
13
 XDOT =     -19231
355437                 XDOT =       -5861
717137
 YDOT =       3876
713573  feet/sec       YDOT =        1181
622297  meter/sec
 ZDOT =     -14111
365556                 ZDOT =       -4301
144222


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   19212
68946894  
00016717  00000-0  10270-3 0  9107
2 25544  51
6429 140
4865 0006085 205
5912 154
4939 15
51047312 22154


Satellite: ISS
Catalog Number: 25544
Epoch time:      19212
68946894   =   yrday
fracday
Element set:     910
Inclination:       51
6429  deg
RA of node:       140
4865  deg
Eccentricity:     
0006085     
Arg of perigee:   205
5912  deg
Mean anomaly:     154
4939  deg
Mean motion:   15
51047312  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              315


Coasting Arc #12 (Orbit 2227)
---------------------------------------

Vector Time (GMT): 2019/213/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         435554
34                 A    =         6790430
86  meter
 Y    =       -5202562
70  meter          E    =           
0006718
 Z    =        4335146
24                 I    =           51
90281
 XDOT =       6371
191637                 Wp   =          111
73170
 YDOT =      -2403
457573  meter/sec      RA   =          135
40450  deg
 ZDOT =      -3522
531742                 TA   =           13
99888
                                          MA   =           13
98027
                                          Ha   =            226
173  n
mi
                                          Hp   =            220
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1428984
04                 X    =          472641
35
 Y    =      -17068775
27  feet           Y    =        -5197485
04  meter
 Z    =       14222920
73                 Z    =         4337351
57
 XDOT =      20902
859701                 XDOT =        6414
704319
 YDOT =      -7885
359493  feet/sec       YDOT =       -2331
966832  meter/sec
 ZDOT =     -11556
862672                 ZDOT =       -3491
478233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14964249
24                 X    =        -4561103
17
 Y    =        8316267
07  feet           Y    =         2534798
20  meter
 Z    =       14233323
77                 Z    =         4338317
08
 XDOT =     -17556
119399                 XDOT =       -5351
105193
 YDOT =     -12041
943194  feet/sec       YDOT =       -3670
384285  meter/sec
 ZDOT =     -11415
407463                 ZDOT =       -3479
416195


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   19213
52707547  
00016717  00000-0  10270-3 0  9112
2 25544  51
6418 136
3300 0006191 208
2432 151
8384 15
51015828 22281


Satellite: ISS
Catalog Number: 25544
Epoch time:      19213
52707547   =   yrday
fracday
Element set:     911
Inclination:       51
6418  deg
RA of node:       136
3300  deg
Eccentricity:     
0006191     
Arg of perigee:   208
2432  deg
Mean anomaly:     151
8384  deg
Mean motion:   15
51015828  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2228
Checksum:              287


Coasting Arc #13 (Orbit 2242)
---------------------------------------

Vector Time (GMT): 2019/214/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -684004
34                 A    =         6791912
39  meter
 Y    =        5518612
74  meter          E    =           
0007606
 Z    =       -3907862
49                 I    =           51
93131
 XDOT =      -6081
713736                 Wp   =          156
79409
 YDOT =       2163
441558  meter/sec      RA   =          130
46023  deg
 ZDOT =       4115
598108                 TA   =          156
29171
                                          MA   =          156
25665
                                          Ha   =            225
980  n
mi
                                          Hp   =            220
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2244108
73                 X    =         -726682
51
 Y    =       18105684
84  feet           Y    =         5510725
32  meter
 Z    =      -12821071
15                 Z    =        -3911288
38
 XDOT =     -19953
129054                 XDOT =       -6125
444707
 YDOT =       7097
905373  feet/sec       YDOT =        2095
186813  meter/sec
 ZDOT =      13502
618464                 ZDOT =        4085
950131

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16140654
09                 X    =         4919671
37
 Y    =       -8480628
49  feet           Y    =        -2584895
56  meter
 Z    =      -12837053
36                 Z    =        -3912733
86
 XDOT =      16587
907117                 XDOT =        5055
994089
 YDOT =      11316
167114  feet/sec       YDOT =        3449
167736  meter/sec
 ZDOT =      13367
558757                 ZDOT =        4074
431909


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   19214
49354001  
00016717  00000-0  10270-3 0  9123
2 25544  51
6423 131
5344 0006106 211
7706 148
3077 15
51024194 22434


Satellite: ISS
Catalog Number: 25544
Epoch time:      19214
49354001   =   yrday
fracday
Element set:     912
Inclination:       51
6423  deg
RA of node:       131
5344  deg
Eccentricity:     
0006106     
Arg of perigee:   211
7706  deg
Mean anomaly:     148
3077  deg
Mean motion:   15
51024194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2243
Checksum:              271


Coasting Arc #14 (Orbit 2258)
---------------------------------------

Vector Time (GMT): 2019/215/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         872082
09                 A    =         6793465
06  meter
 Y    =       -5806439
27  meter          E    =           
0010191
 Z    =        3404135
59                 I    =           51
95701
 XDOT =       5802
250244                 Wp   =          119
39892
 YDOT =      -1860
281369  meter/sec      RA   =          125
52055  deg
 ZDOT =      -4653
935079                 TA   =           21
04219
                                          MA   =           21
00029
                                          Ha   =            225
879  n
mi
                                          Hp   =            220
632

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2861161
70                 X    =          920411
55
 Y    =      -19049997
59  feet           Y    =        -5796416
90  meter
 Z    =       11168423
86                 Z    =         3408488
95
 XDOT =      19036
254081                 XDOT =        5845
226890
 YDOT =      -6103
285331  feet/sec       YDOT =       -1795
156094  meter/sec
 ZDOT =     -15268
815875                 ZDOT =       -4625
646288

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17126031
30                 X    =        -5220014
34
 Y    =        8794058
70  feet           Y    =         2680429
09  meter
 Z    =       11188651
83                 Z    =         3410301
08
 XDOT =     -15442
241604                 XDOT =       -4706
795241
 YDOT =     -10787
274123  feet/sec       YDOT =       -3287
961153  meter/sec
 ZDOT =     -15139
949772                 ZDOT =       -4614
656690


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   19215
52443392  
00016717  00000-0  10270-3 0  9131
2 25544  51
6421 126
4205 0006058 215
4295 144
6455 15
51019330 22593


Satellite: ISS
Catalog Number: 25544
Epoch time:      19215
52443392   =   yrday
fracday
Element set:     913
Inclination:       51
6421  deg
RA of node:       126
4205  deg
Eccentricity:     
0006058     
Arg of perigee:   215
4295  deg
Mean anomaly:     144
6455  deg
Mean motion:   15
51019330  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2259
Checksum:              288


Coasting Arc #15 (Orbit 2273)
---------------------------------------

Vector Time (GMT): 2019/216/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1002817
95                 A    =         6794872
08  meter
 Y    =        6085284
87  meter          E    =           
0002611
 Z    =       -2855764
11                 I    =           51
98048
 XDOT =      -5512
627222                 Wp   =          174
99531
 YDOT =       1487
072121  meter/sec      RA   =          120
58246  deg
 ZDOT =       5102
382548                 TA   =          152
77165
                                          MA   =          152
75796
                                          Ha   =            225
687  n
mi
                                          Hp   =            220
798

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3290085
15                 X    =        -1056919
39
 Y    =       19964845
37  feet           Y    =         6073768
19  meter
 Z    =       -9369304
81                 Z    =        -2860766
65
 XDOT =     -18086
047316                 XDOT =       -5553
630424
 YDOT =       4878
845542  feet/sec       YDOT =        1425
196722  meter/sec
 ZDOT =      16740
100222                 ZDOT =        5075
505242

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17970105
06                 X    =         5477288
02
 Y    =       -9276829
97  feet           Y    =        -2827577
77  meter
 Z    =       -9392514
76                 Z    =        -2862838
50
 XDOT =      14068
200261                 XDOT =        4287
987440
 YDOT =      10419
330360  feet/sec       YDOT =        3175
811894  meter/sec
 ZDOT =      16617
674135                 ZDOT =        5065
067076


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   19216
49089531  
00016717  00000-0  10270-3 0  9140
2 25544  51
6422 121
6250 0006119 219
4255 140
6451 15
51036196 22747


Satellite: ISS
Catalog Number: 25544
Epoch time:      19216
49089531   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:       121
6250  deg
Eccentricity:     
0006119     
Arg of perigee:   219
4255  deg
Mean anomaly:     140
6451  deg
Mean motion:   15
51036196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2274
Checksum:              291


Coasting Arc #16 (Orbit 2278)
---------------------------------------

Vector Time (GMT): 2019/216/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3799862
17                 A    =         6798139
43  meter
 Y    =        5584567
80  meter          E    =           
0007183
 Z    =         743144
55                 I    =           51
99207
 XDOT =      -3550
824411                 Wp   =           65
08208
 YDOT =      -3217
016748  meter/sec      RA   =          119
29983  deg
 ZDOT =       5976
792061                 TA   =          302
89593
                                          MA   =          302
96502
                                          Ha   =            225
769  n
mi
                                          Hp   =            220
855

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12466739
39                 X    =        -3865637
71
 Y    =       18322072
83  feet           Y    =         5541707
29  meter
 Z    =        2438138
29                 Z    =          724526
89
 XDOT =     -11649
686389                 XDOT =       -3543
618290
 YDOT =     -10554
516890  feet/sec       YDOT =       -3256
684329  meter/sec
 ZDOT =      19608
897837                 ZDOT =        5959
561283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3030243
24                 X    =         -923618
14
 Y    =      -21962319
57  feet           Y    =        -6694115
00  meter
 Z    =        2352999
66                 Z    =          717194
30
 XDOT =      14215
166762                 XDOT =        4332
782829
 YDOT =        146
531527  feet/sec       YDOT =          44
662809  meter/sec
 ZDOT =      19530
715502                 ZDOT =        5952
962085


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   19216
81304773  
00016717  00000-0  10270-3 0  9155
2 25544  51
6386 120
0225 0006376 219
2328 140
8362 15
51027541 22797


Satellite: ISS
Catalog Number: 25544
Epoch time:      19216
81304773   =   yrday
fracday
Element set:     915
Inclination:       51
6386  deg
RA of node:       120
0225  deg
Eccentricity:     
0006376     
Arg of perigee:   219
2328  deg
Mean anomaly:     140
8362  deg
Mean motion:   15
51027541  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2279
Checksum:              296


Coasting Arc #17 (Orbit 2293)
---------------------------------------

Vector Time (GMT): 2019/217/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3715499
48                 A    =         6797409
84  meter
 Y    =       -5501413
05  meter          E    =           
0011263
 Z    =       -1427148
92                 I    =           52
00643
 XDOT =       3300
960158                 Wp   =          175
11510
 YDOT =       3736
263094  meter/sec      RA   =          114
36703  deg
 ZDOT =      -5823
063729                 TA   =           20
35258
                                          MA   =           20
30773
                                          Ha   =            225
550  n
mi
                                          Hp   =            220
919

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12189958
91                 X    =         3783673
92
 Y    =      -18049255
41  feet           Y    =        -5459482
52  meter
 Z    =       -4682247
13                 Z    =        -1408935
14
 XDOT =      10829
921777                 XDOT =        3287
219665
 YDOT =      12258
081016  feet/sec       YDOT =        3773
099973  meter/sec
 ZDOT =     -19104
539793                 ZDOT =       -5807
062469

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3412273
85                 X    =         1040061
07
 Y    =       21529057
25  feet           Y    =         6562056
65  meter
 Z    =       -4598938
84                 Z    =        -1401756
56
 XDOT =     -14806
386247                 XDOT =       -4512
986528
 YDOT =      -1708
587848  feet/sec       YDOT =        -520
777576  meter/sec
 ZDOT =     -19031
993302                 ZDOT =       -5800
951558


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   19217
77950529  
00016717  00000-0  10270-3 0  9168
2 25544  51
6397 115
2268 0006134 223
8136 136
2529 15
51068236 22949


Satellite: ISS
Catalog Number: 25544
Epoch time:      19217
77950529   =   yrday
fracday
Element set:     916
Inclination:       51
6397  deg
RA of node:       115
2268  deg
Eccentricity:     
0006134     
Arg of perigee:   223
8136  deg
Mean anomaly:     136
2529  deg
Mean motion:   15
51068236  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2294
Checksum:              321


Coasting Arc #18 (Orbit 2309)
---------------------------------------

Vector Time (GMT): 2019/218/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933877
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3608085
23                 A    =         6796554
18  meter
 Y    =        5372302
82  meter          E    =           
0008521
 Z    =        2068338
85                 I    =           52
01559
 XDOT =      -3113
628944                 Wp   =           86
19573
 YDOT =      -4242
168085  meter/sec      RA   =          109
43384  deg
 ZDOT =       5567
899878                 TA   =          296
52594
                                          MA   =          296
61328
                                          Ha   =            225
488  n
mi
                                          Hp   =            221
089

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11837549
96                 X    =        -3677938
44
 Y    =       17625665
42  feet           Y    =         5331564
06  meter
 Z    =        6785888
61                 Z    =         2050642
74
 XDOT =     -10215
318057                 XDOT =       -3093
005871
 YDOT =     -13917
874296  feet/sec       YDOT =       -4276
871662  meter/sec
 ZDOT =      18267
388052                 ZDOT =        5552
825208

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3730370
28                 X    =        -1137016
86
 Y    =      -20927689
82  feet           Y    =        -6378759
86  meter
 Z    =        6704930
37                 Z    =         2043662
78
 XDOT =      15582
450645                 XDOT =        4749
530956
 YDOT =       3073
554640  feet/sec       YDOT =         936
819454  meter/sec
 ZDOT =      18199
101984                 ZDOT =        5547
086285


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   19218
81039226  
00016717  00000-0  10270-3 0  9177
2 25544  51
6392 110
1111 0006290 225
5154 134
5484 15
51041866 23107


Satellite: ISS
Catalog Number: 25544
Epoch time:      19218
81039226   =   yrday
fracday
Element set:     917
Inclination:       51
6392  deg
RA of node:       110
1111  deg
Eccentricity:     
0006290     
Arg of perigee:   225
5154  deg
Mean anomaly:     134
5484  deg
Mean motion:   15
51041866  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2310
Checksum:              278


Coasting Arc #19 (Orbit 2324)
---------------------------------------

Vector Time (GMT): 2019/219/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933877
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3506417
73                 A    =         6795268
96  meter
 Y    =       -5153372
22  meter          E    =           
0006905
 Z    =       -2695450
02                 I    =           52
02165
 XDOT =       2979
458899                 Wp   =          185
73829
 YDOT =       4754
665463  meter/sec      RA   =          104
50148  deg
 ZDOT =      -5219
991022                 TA   =           24
49645
                                          MA   =           24
46366
                                          Ha   =            225
380  n
mi
                                          Hp   =            221
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11503995
17                 X    =         3576876
50
 Y    =      -16907389
17  feet           Y    =        -5113766
94  meter
 Z    =       -8843339
95                 Z    =        -2678246
34
 XDOT =       9775
127623                 XDOT =        2951
425025
 YDOT =      15599
296137  feet/sec       YDOT =        4787
827290  meter/sec
 ZDOT =     -17125
954797                 ZDOT =       -5205
585983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3807044
90                 X    =         1160387
29
 Y    =       20126951
28  feet           Y    =         6134694
75  meter
 Z    =       -8764622
99                 Z    =        -2671457
09
 XDOT =     -16560
887774                 XDOT =       -5047
758594
 YDOT =      -4288
917263  feet/sec       YDOT =       -1307
261982  meter/sec
 ZDOT =     -17060
763815                 ZDOT =       -5200
120811


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   19219
77684677  
00016717  00000-0  10270-3 0  9180
2 25544  51
6394 105
3162 0006206 229
5741 130
4869 15
51052351 23253


Satellite: ISS
Catalog Number: 25544
Epoch time:      19219
77684677   =   yrday
fracday
Element set:     918
Inclination:       51
6394  deg
RA of node:       105
3162  deg
Eccentricity:     
0006206     
Arg of perigee:   229
5741  deg
Mean anomaly:     130
4869  deg
Mean motion:   15
51052351  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2325
Checksum:              317
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