[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: December 13th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15140 5164 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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


346/03:16:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 219 4

349/11:36:38 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 219 1

355/13:08:55 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 5

356/04:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 4

359/09:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 3

Coasting Arc #1 (Orbit 274)
---------------------------------------

Vector Time (GMT): 2019/345/11:24:50
319
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6399283
94                 A    =         6798920
68  meter
 Y    =        -602810
93  meter          E    =           
0013218
 Z    =       -2200498
82                 I    =           51
51020
 XDOT =      -1380
382922                 Wp   =           31
27778
 YDOT =      -5193
050920  meter/sec      RA   =          201
17770  deg
 ZDOT =       5462
719944                 TA   =          304
27792
                                          MA   =          304
40301
                                          Ha   =            229
240  n
mi
                                          Hp   =            219
554

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20995026
05                 X    =        -6381378
58
 Y    =       -1977726
16  feet           Y    =         -674271
82  meter
 Z    =       -7219484
33                 Z    =        -2231541
17
 XDOT =      -4528
815362                 XDOT =       -1348
745339
 YDOT =     -17037
568635  feet/sec       YDOT =       -5208
311217  meter/sec
 ZDOT =      17922
309527                 ZDOT =        5456
090572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8954552
79                 X    =         2729347
69
 Y    =      -19038202
55  feet           Y    =        -5802844
14  meter
 Z    =       -7361134
52                 Z    =        -2243673
80
 XDOT =      16216
206503                 XDOT =        4942
699742
 YDOT =        741
273929  feet/sec       YDOT =         225
940294  meter/sec
 ZDOT =      17892
343173                 ZDOT =        5453
586199


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   19345
48004270  
00016717  00000-0  10270-3 0  9004
2 25544  51
6415 202
3564 0007472  20
6419 339
5032 15
50105232  2751


Satellite: ISS
Catalog Number: 25544
Epoch time:      19345
48004270   =   yrday
fracday
Element set:     900
Inclination:       51
6415  deg
RA of node:       202
3564  deg
Eccentricity:     
0007472     
Arg of perigee:    20
6419  deg
Mean anomaly:     339
5032  deg
Mean motion:   15
50105232  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             275
Checksum:              269


Coasting Arc #2 (Orbit 285)
---------------------------------------

Vector Time (GMT): 2019/346/03:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1641370
35                 A    =         6791396
06  meter
 Y    =       -4526873
26  meter          E    =           
0010303
 Z    =        4779377
42                 I    =           51
50241
 XDOT =       7208
116440                 Wp   =           72
73258
 YDOT =        147
996477  meter/sec      RA   =          197
93686  deg
 ZDOT =       2613
976319                 TA   =          351
44008
                                          MA   =          351
45764
                                          Ha   =            229
409  n
mi
                                          Hp   =            219
438

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5385073
33                 X    =        -1613843
36
 Y    =      -14851946
41  feet           Y    =        -4545075
04  meter
 Z    =       15680372
10                 Z    =         4771470
33
 XDOT =      23648
675984                 XDOT =        7193
228391
 YDOT =        485
552747  feet/sec       YDOT =         228
519085  meter/sec
 ZDOT =       8576
037791                 ZDOT =        2648
954909

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8169567
64                 X    =        -2490084
22
 Y    =       13563192
39  feet           Y    =         4134061
04  meter
 Z    =       15644531
72                 Z    =         4768453
27
 XDOT =     -13363
771133                 XDOT =       -4073
277441
 YDOT =     -18132
008758  feet/sec       YDOT =       -5526
636269  meter/sec
 ZDOT =       8735
697525                 ZDOT =        2662
640605


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   19346
18919882  
00016717  00000-0  10270-3 0  9017
2 25544  51
6382 198
8411 0007407  25
3533 334
7979 15
50116406  2865


Satellite: ISS
Catalog Number: 25544
Epoch time:      19346
18919882   =   yrday
fracday
Element set:     901
Inclination:       51
6382  deg
RA of node:       198
8411  deg
Eccentricity:     
0007407     
Arg of perigee:    25
3533  deg
Mean anomaly:     334
7979  deg
Mean motion:   15
50116406  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             286
Checksum:              326


Coasting Arc #3 (Orbit 300)
---------------------------------------

Vector Time (GMT): 2019/347/03:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1571307
75                 A    =         6790802
06  meter
 Y    =        4396333
37  meter          E    =           
0018312
 Z    =       -4948152
08                 I    =           51
53198
 XDOT =      -7319
066685                 Wp   =           57
35471
 YDOT =        119
505889  meter/sec      RA   =          192
97175  deg
 ZDOT =      -2214
369270                 TA   =          190
92112
                                          MA   =          190
96093
                                          Ha   =            229
518  n
mi
                                          Hp   =            219
305

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5155209
15                 X    =         1546065
41
 Y    =       14423665
91  feet           Y    =         4413764
50  meter
 Z    =      -16234094
74                 Z    =        -4940579
81
 XDOT =     -24012
685976                 XDOT =       -7309
102822
 YDOT =        392
079688  feet/sec       YDOT =          37
714983  meter/sec
 ZDOT =      -7264
991043                 ZDOT =       -2249
898571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7749409
31                 X    =         2362019
96
 Y    =      -13254370
80  feet           Y    =        -4039932
22  meter
 Z    =      -16199767
33                 Z    =        -4937689
08
 XDOT =      14620
116096                 XDOT =        4456
211386
 YDOT =      17640
291386  feet/sec       YDOT =        5376
760814  meter/sec
 ZDOT =      -7427
209154                 ZDOT =       -2263
813350


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   19347
15622863  
00016717  00000-0  10270-3 0  9026
2 25544  51
6376 194
0491 0007510  29
3424 330
8147 15
50106213  3019


Satellite: ISS
Catalog Number: 25544
Epoch time:      19347
15622863   =   yrday
fracday
Element set:     902
Inclination:       51
6376  deg
RA of node:       194
0491  deg
Eccentricity:     
0007510     
Arg of perigee:    29
3424  deg
Mean anomaly:     330
8147  deg
Mean motion:   15
50106213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             301
Checksum:              279


Coasting Arc #4 (Orbit 316)
---------------------------------------

Vector Time (GMT): 2019/348/03:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1466564
31                 A    =         6790183
02  meter
 Y    =       -4266788
95  meter          E    =           
0009098
 Z    =        5066213
47                 I    =           51
56256
 XDOT =       7440
388659                 Wp   =           69
80222
 YDOT =       -405
770630  meter/sec      RA   =          188
00938  deg
 ZDOT =       1812
526679                 TA   =            2
63772
                                          MA   =            2
63293
                                          Ha   =            229
547  n
mi
                                          Hp   =            219
198

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4811562
70                 X    =        -1443351
71
 Y    =      -13998651
42  feet           Y    =        -4283060
13  meter
 Z    =       16621435
28                 Z    =         5059145
14
 XDOT =      24410
723946                 XDOT =        7435
568863
 YDOT =      -1331
268470  feet/sec       YDOT =        -322
594188  meter/sec
 ZDOT =       5946
609839                 ZDOT =        1848
657576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7419639
61                 X    =        -2261506
15
 Y    =       12850154
77  feet           Y    =         3916727
18  meter
 Z    =       16589392
94                 Z    =         5056446
97
 XDOT =     -15938
335166                 XDOT =       -4858
004558
 YDOT =     -17090
951018  feet/sec       YDOT =       -5209
321870  meter/sec
 ZDOT =       6111
621333                 ZDOT =        1862
822182


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   19348
18772651  
00016717  00000-0  10270-3 0  9032
2 25544  51
6372 188
9384 0007460  31
9076 328
2525 15
50121158  3177


Satellite: ISS
Catalog Number: 25544
Epoch time:      19348
18772651   =   yrday
fracday
Element set:     903
Inclination:       51
6372  deg
RA of node:       188
9384  deg
Eccentricity:     
0007460     
Arg of perigee:    31
9076  deg
Mean anomaly:     328
2525  deg
Mean motion:   15
50121158  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             317
Checksum:              313


Coasting Arc #5 (Orbit 331)
---------------------------------------

Vector Time (GMT): 2019/349/03:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1365885
39                 A    =         6789787
22  meter
 Y    =        4188106
91  meter          E    =           
0019868
 Z    =       -5184077
05                 I    =           51
59518
 XDOT =      -7485
243238                 Wp   =           64
48786
 YDOT =        709
035394  meter/sec      RA   =          183
04786  deg
 ZDOT =      -1395
213168                 TA   =          192
02504
                                          MA   =          192
07254
                                          Ha   =            229
620  n
mi
                                          Hp   =            219
102

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4481251
29                 X    =         1344132
52
 Y    =       13740508
22  feet           Y    =         4203260
35  meter
 Z    =      -17008126
81                 Z    =        -5177494
32
 XDOT =     -24557
884640                 XDOT =       -7485
838417
 YDOT =       2326
231606  feet/sec       YDOT =         625
326998  meter/sec
 ZDOT =      -4577
471025                 ZDOT =       -1431
574885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7222028
28                 X    =         2201274
22
 Y    =      -12559441
46  feet           Y    =        -3828117
76  meter
 Z    =      -16978288
92                 Z    =        -5174982
46
 XDOT =      17108
239555                 XDOT =        5214
591416
 YDOT =      16268
745917  feet/sec       YDOT =        4958
713755  meter/sec
 ZDOT =      -4743
583557                 ZDOT =       -1445
844268


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   19349
15475490  
00016717  00000-0  10270-3 0  9042
2 25544  51
6380 184
1461 0007489  35
7278 324
4373 15
50109295  3321


Satellite: ISS
Catalog Number: 25544
Epoch time:      19349
15475490   =   yrday
fracday
Element set:     904
Inclination:       51
6380  deg
RA of node:       184
1461  deg
Eccentricity:     
0007489     
Arg of perigee:    35
7278  deg
Mean anomaly:     324
4373  deg
Mean motion:   15
50109295  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             332
Checksum:              317


Coasting Arc #6 (Orbit 337)
---------------------------------------

Vector Time (GMT): 2019/349/11:36:38
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5295817
84                 A    =         6796557
36  meter
 Y    =       -2709512
92  meter          E    =           
0018175
 Z    =        3265254
23                 I    =           51
63075
 XDOT =       4799
397472                 Wp   =           68
68417
 YDOT =      -3645
183114  meter/sec      RA   =          181
33755  deg
 ZDOT =       4744
398089                 TA   =          329
17538
                                          MA   =          329
28197
                                          Ha   =            229
588  n
mi
                                          Hp   =            219
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17374730
45                 X    =        -5280986
39
 Y    =       -8889478
09  feet           Y    =        -2768652
04  meter
 Z    =       10712776
36                 Z    =         3239564
89
 XDOT =      15746
054699                 XDOT =        4816
756743
 YDOT =     -11959
262186  feet/sec       YDOT =       -3591
416485  meter/sec
 ZDOT =      15565
610529                 ZDOT =        4767
753283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12558263
83                 X    =         3827758
82
 Y    =      -15023023
88  feet           Y    =        -4579017
68  meter
 Z    =       10595584
91                 Z    =         3229534
28
 XDOT =       7070
690956                 XDOT =        2155
146603
 YDOT =      16998
953516  feet/sec       YDOT =        5181
281032  meter/sec
 ZDOT =      15672
483503                 ZDOT =        4776
972972


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   19349
54156356  
00016717  00000-0  10270-3 0  9053
2 25544  51
6391 182
2292 0007334  34
6572 325
5055 15
50135080  3384


Satellite: ISS
Catalog Number: 25544
Epoch time:      19349
54156356   =   yrday
fracday
Element set:     905
Inclination:       51
6391  deg
RA of node:       182
2292  deg
Eccentricity:     
0007334     
Arg of perigee:    34
6572  deg
Mean anomaly:     325
5055  deg
Mean motion:   15
50135080  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             338
Checksum:              301


Coasting Arc #7 (Orbit 352)
---------------------------------------

Vector Time (GMT): 2019/350/11:36:38
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5213253
00                 A    =         6795684
90  meter
 Y    =        2507721
74  meter          E    =           
0011744
 Z    =       -3580369
13                 I    =           51
66039
 XDOT =      -4898
733104                 Wp   =           58
00785
 YDOT =       3836
459437  meter/sec      RA   =          176
38285  deg
 ZDOT =      -4450
460625                 TA   =          164
13323
                                          MA   =          164
09641
                                          Ha   =            229
664  n
mi
                                          Hp   =            219
031

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17103848
44                 X    =         5202214
78
 Y    =        8227433
53  feet           Y    =         2565958
74  meter
 Z    =      -11746617
89                 Z    =        -3555071
80
 XDOT =     -16071
959001                 XDOT =       -4919
651735
 YDOT =      12586
809177  feet/sec       YDOT =        3781
561927  meter/sec
 ZDOT =     -14601
248769                 ZDOT =       -4474
306986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11595678
94                 X    =        -3534362
94
 Y    =       15115260
76  feet           Y    =         4607131
48  meter
 Z    =      -11631184
29                 Z    =        -3545184
97
 XDOT =      -7916
413385                 XDOT =       -2412
922800
 YDOT =     -17380
803724  feet/sec       YDOT =       -5297
668975  meter/sec
 ZDOT =     -14710
390893                 ZDOT =       -4483
727144


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   19350
50858993  
00016717  00000-0  10270-3 0  9068
2 25544  51
6382 177
4369 0007538  39
2886 320
8810 15
50130234  3530


Satellite: ISS
Catalog Number: 25544
Epoch time:      19350
50858993   =   yrday
fracday
Element set:     906
Inclination:       51
6382  deg
RA of node:       177
4369  deg
Eccentricity:     
0007538     
Arg of perigee:    39
2886  deg
Mean anomaly:     320
8810  deg
Mean motion:   15
50130234  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             353
Checksum:              322


Coasting Arc #8 (Orbit 368)
---------------------------------------

Vector Time (GMT): 2019/351/11:36:38
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5100785
15                 A    =         6794846
03  meter
 Y    =       -2298305
05  meter          E    =           
0016798
 Z    =        3838790
78                 I    =           51
69063
 XDOT =       4982
703185                 Wp   =           76
79966
 YDOT =      -4079
717037  meter/sec      RA   =          171
43044  deg
 ZDOT =       4166
610988                 TA   =          329
33993
                                          MA   =          329
43798
                                          Ha   =            229
745  n
mi
                                          Hp   =            218
909

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16734859
42                 X    =        -5093352
30
 Y    =       -7540370
88  feet           Y    =        -2355304
45  meter
 Z    =       12594457
96                 Z    =         3814031
10
 XDOT =      16347
451394                 XDOT =        5007
714530
 YDOT =     -13384
898416  feet/sec       YDOT =       -4023
857492  meter/sec
 ZDOT =      13669
983556                 ZDOT =        4190
875245

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10590461
65                 X    =         3227972
71
 Y    =      -15086039
93  feet           Y    =        -4598224
97  meter
 Z    =       12481450
45                 Z    =         3804346
10
 XDOT =       8961
014489                 XDOT =        2731
317216
 YDOT =      17724
206781  feet/sec       YDOT =        5402
338227  meter/sec
 ZDOT =      13781
061921                 ZDOT =        4200
467674


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   19351
54008334  
00016717  00000-0  10270-3 0  9070
2 25544  51
6378 172
3255 0007343  42
7724 317
3997 15
50134307  3696


Satellite: ISS
Catalog Number: 25544
Epoch time:      19351
54008334   =   yrday
fracday
Element set:     907
Inclination:       51
6378  deg
RA of node:       172
3255  deg
Eccentricity:     
0007343     
Arg of perigee:    42
7724  deg
Mean anomaly:     317
3997  deg
Mean motion:   15
50134307  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             369
Checksum:              310


Coasting Arc #9 (Orbit 383)
---------------------------------------

Vector Time (GMT): 2019/352/11:36:38
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4976139
54                 A    =         6793949
85  meter
 Y    =        2143434
30  meter          E    =           
0014427
 Z    =       -4114970
96                 I    =           51
72046
 XDOT =      -5022
327221                 Wp   =           59
74327
 YDOT =       4315
217778  meter/sec      RA   =          166
47945  deg
 ZDOT =      -3828
611715                 TA   =          170
65325
                                          MA   =          170
62638
                                          Ha   =            229
759  n
mi
                                          Hp   =            218
829

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16325917
12                 X    =         4971789
32
 Y    =        7032264
78  feet           Y    =         2199057
01  meter
 Z    =      -13500560
91                 Z    =        -4090809
28
 XDOT =     -16477
451512                 XDOT =       -5051
610820
 YDOT =      14157
538641  feet/sec       YDOT =        4258
891126  meter/sec
 ZDOT =     -12561
062058                 ZDOT =       -3853
078945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9759340
72                 X    =        -2974647
05
 Y    =       14956925
61  feet           Y    =         4558870
93  meter
 Z    =      -13390261
67                 Z    =        -4081351
76
 XDOT =     -10024
490098                 XDOT =       -3055
464582
 YDOT =     -17877
806570  feet/sec       YDOT =       -5449
155443  meter/sec
 ZDOT =     -12673
093973                 ZDOT =       -3862
759043


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   19352
50710908  
00016717  00000-0  10270-3 0  9085
2 25544  51
6377 167
5335 0007504  47
5482 312
6302 15
50137109  3841


Satellite: ISS
Catalog Number: 25544
Epoch time:      19352
50710908   =   yrday
fracday
Element set:     908
Inclination:       51
6377  deg
RA of node:       167
5335  deg
Eccentricity:     
0007504     
Arg of perigee:    47
5482  deg
Mean anomaly:     312
6302  deg
Mean motion:   15
50137109  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             384
Checksum:              300


Coasting Arc #10 (Orbit 399)
---------------------------------------

Vector Time (GMT): 2019/353/11:36:38
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4825879
08                 A    =         6793125
87  meter
 Y    =       -1989642
02  meter          E    =           
0015100
 Z    =        4333284
32                 I    =           51
75044
 XDOT =       5045
930962                 Wp   =           83
79111
 YDOT =      -4595
063920  meter/sec      RA   =          161
53000  deg
 ZDOT =       3500
817611                 TA   =          330
63244
                                          MA   =          330
71721
                                          Ha   =            229
858  n
mi
                                          Hp   =            218
711

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15832936
61                 X    =        -4824320
29
 Y    =       -6527696
90  feet           Y    =        -2043599
98  meter
 Z    =       14216812
08                 Z    =         4309845
72
 XDOT =      16554
891606                 XDOT =        5079
934297
 YDOT =     -15075
669029  feet/sec       YDOT =       -4538
446860  meter/sec
 ZDOT =      11485
622082                 ZDOT =        3525
411080

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8926192
12                 X    =         2720703
36
 Y    =      -14718940
41  feet           Y    =        -4486333
04  meter
 Z    =       14109795
95                 Z    =         4300665
80
 XDOT =      11253
791548                 XDOT =        3430
155664
 YDOT =      17971
185615  feet/sec       YDOT =        5477
617375  meter/sec
 ZDOT =      11598
260153                 ZDOT =        3535
149695


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   19353
53859985  
00016717  00000-0  10270-3 0  9099
2 25544  51
6381 162
4216 0007338  50
5654 309
6145 15
50139283  4003


Satellite: ISS
Catalog Number: 25544
Epoch time:      19353
53859985   =   yrday
fracday
Element set:     909
Inclination:       51
6381  deg
RA of node:       162
4216  deg
Eccentricity:     
0007338     
Arg of perigee:    50
5654  deg
Mean anomaly:     309
6145  deg
Mean motion:   15
50139283  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             400
Checksum:              316


Coasting Arc #11 (Orbit 414)
---------------------------------------

Vector Time (GMT): 2019/354/11:36:38
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4675429
66                 A    =         6792297
01  meter
 Y    =        1893569
82  meter          E    =           
0017189
 Z    =       -4565972
39                 I    =           51
77929
 XDOT =      -5015
766674                 Wp   =           63
99161
 YDOT =       4854
004734  meter/sec      RA   =          156
58267  deg
 ZDOT =      -3124
805665                 TA   =          174
67867
                                          MA   =          174
66037
                                          Ha   =            229
896  n
mi
                                          Hp   =            218
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15339336
15                 X    =         4676086
72
 Y    =        6212499
40  feet           Y    =         1945857
76  meter
 Z    =      -14980224
39                 Z    =        -4543259
15
 XDOT =     -16455
927409                 XDOT =       -5054
494195
 YDOT =      15925
212383  feet/sec       YDOT =        4797
698558  meter/sec
 ZDOT =     -10251
987090                 ZDOT =       -3149
264155

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8291785
24                 X    =        -2527336
14
 Y    =       14430292
25  feet           Y    =         4398353
08  meter
 Z    =      -14876507
26                 Z    =        -4534359
41
 XDOT =     -12447
319935                 XDOT =       -3793
943116
 YDOT =     -17830
668885  feet/sec       YDOT =       -5434
787876  meter/sec
 ZDOT =     -10364
038674                 ZDOT =       -3158
958988


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   19354
50562238  
00016717  00000-0  10270-3 0  9101
2 25544  51
6383 157
6299 0007641  55
8764 304
3110 15
50143100  4152


Satellite: ISS
Catalog Number: 25544
Epoch time:      19354
50562238   =   yrday
fracday
Element set:     910
Inclination:       51
6383  deg
RA of node:       157
6299  deg
Eccentricity:     
0007641     
Arg of perigee:    55
8764  deg
Mean anomaly:     304
3110  deg
Mean motion:   15
50143100  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             415
Checksum:              287


Coasting Arc #12 (Orbit 430)
---------------------------------------

Vector Time (GMT): 2019/355/11:36:38
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4506436
94                 A    =         6791572
11  meter
 Y    =       -1803736
02  meter          E    =           
0013429
 Z    =        4738486
32                 I    =           51
80583
 XDOT =       4969
549615                 Wp   =           89
30081
 YDOT =      -5149
936863  meter/sec      RA   =          151
63659  deg
 ZDOT =       2759
238516                 TA   =          333
42435
                                          MA   =          333
49314
                                          Ha   =            229
999  n
mi
                                          Hp   =            218
504

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14784898
11                 X    =        -4508949
15
 Y    =       -5917769
10  feet           Y    =        -1854144
62  meter
 Z    =       15546214
97                 Z    =         4716589
39
 XDOT =      16304
296637                 XDOT =        5013
365454
 YDOT =     -16896
118317  feet/sec       YDOT =       -5094
119079  meter/sec
 ZDOT =       9052
619802                 ZDOT =        2783
484846

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7682831
34                 X    =         2341726
99
 Y    =      -14060105
49  feet           Y    =        -4285520
15  meter
 Z    =       15446214
41                 Z    =         4708006
15
 XDOT =      13770
652972                 XDOT =        4197
295026
 YDOT =      17615
708580  feet/sec       YDOT =        5369
267975  meter/sec
 ZDOT =       9163
737402                 ZDOT =        2793
107160


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   19355
53711116  
00016717  00000-0  10270-3 0  9117
2 25544  51
6370 152
5181 0007430  59
2814 300
9068 15
50138333  4316


Satellite: ISS
Catalog Number: 25544
Epoch time:      19355
53711116   =   yrday
fracday
Element set:     911
Inclination:       51
6370  deg
RA of node:       152
5181  deg
Eccentricity:     
0007430     
Arg of perigee:    59
2814  deg
Mean anomaly:     300
9068  deg
Mean motion:   15
50138333  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             431
Checksum:              277


Coasting Arc #13 (Orbit 431)
---------------------------------------

Vector Time (GMT): 2019/355/13:08:55
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4676743
18                 A    =         6791893
78  meter
 Y    =       -1605650
83  meter          E    =           
0013993
 Z    =        4644063
01                 I    =           51
81094
 XDOT =       4746
879913                 Wp   =           89
96979
 YDOT =      -5248
717880  meter/sec      RA   =          151
32047  deg
 ZDOT =       2957
892667                 TA   =          330
60770
                                          MA   =          330
68633
                                          Ha   =            229
933  n
mi
                                          Hp   =            218
498

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15343645
60                 X    =        -4680999
12
 Y    =       -5267883
31  feet           Y    =        -1657973
66  meter
 Z    =       15236427
21                 Z    =         4621334
57
 XDOT =      15573
752996                 XDOT =        4790
851942
 YDOT =     -17220
203020  feet/sec       YDOT =       -5195
389292  meter/sec
 ZDOT =       9704
372267                 ZDOT =        2981
057715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         762003
81                 X    =          232258
76
 Y    =      -16301843
76  feet           Y    =        -4968801
98  meter
 Z    =       15132614
09                 Z    =         4612420
78
 XDOT =      19665
239630                 XDOT =        5993
965039
 YDOT =      10049
689929  feet/sec       YDOT =        3063
145490  meter/sec
 ZDOT =       9810
553669                 ZDOT =        2990
256758


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   19355
60157885  
00016717  00000-0  10270-3 0  9123
2 25544  51
6389 152
1983 0007293  60
6799 299
5079 15
50157663  4320


Satellite: ISS
Catalog Number: 25544
Epoch time:      19355
60157885   =   yrday
fracday
Element set:     912
Inclination:       51
6389  deg
RA of node:       152
1983  deg
Eccentricity:     
0007293     
Arg of perigee:    60
6799  deg
Mean anomaly:     299
5079  deg
Mean motion:   15
50157663  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             432
Checksum:              347


Coasting Arc #14 (Orbit 440)
---------------------------------------

Vector Time (GMT): 2019/356/04:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         560224
02                 A    =         6789860
30  meter
 Y    =        4412944
26  meter          E    =           
0019811
 Z    =       -5146605
40                 I    =           51
82393
 XDOT =      -6933
341354                 Wp   =           87
18274
 YDOT =       2781
334781  meter/sec      RA   =          148
22349  deg
 ZDOT =       1636
524654                 TA   =          198
57719
                                          MA   =          198
64962
                                          Ha   =            229
949  n
mi
                                          Hp   =            218
447

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1838005
31                 X    =          535835
04
 Y    =       14478163
58  feet           Y    =         4419073
20  meter
 Z    =      -16885188
31                 Z    =        -5143942
84
 XDOT =     -22747
182919                 XDOT =       -6971
877124
 YDOT =       9125
114112  feet/sec       YDOT =        2703
585635  meter/sec
 ZDOT =       5369
175373                 ZDOT =        1602
751546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5510229
27                 X    =         1679517
88
 Y    =      -13529062
52  feet           Y    =        -4123658
26  meter
 Z    =      -16873260
19                 Z    =        -5142969
71
 XDOT =      23316
434829                 XDOT =        7106
849336
 YDOT =       3019
082744  feet/sec       YDOT =         920
216420  meter/sec
 ZDOT =       5214
619269                 ZDOT =        1589
415953


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   19356
18179226  
00016717  00000-0  10270-3 0  9131
2 25544  51
6408 149
3280 0007638  59
0244 301
1656 15
50130330  4413


Satellite: ISS
Catalog Number: 25544
Epoch time:      19356
18179226   =   yrday
fracday
Element set:     913
Inclination:       51
6408  deg
RA of node:       149
3280  deg
Eccentricity:     
0007638     
Arg of perigee:    59
0244  deg
Mean anomaly:     301
1656  deg
Mean motion:   15
50130330  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             441
Checksum:              288


Coasting Arc #15 (Orbit 456)
---------------------------------------

Vector Time (GMT): 2019/357/04:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -484011
20                 A    =         6790274
64  meter
 Y    =       -4548436
27  meter          E    =           
0013542
 Z    =        5010515
55                 I    =           51
85376
 XDOT =       6745
018515                 Wp   =           59
91502
 YDOT =      -3006
233290  meter/sec      RA   =          143
28028  deg
 ZDOT =      -2066
639255                 TA   =           50
18523
                                          MA   =           50
06611
                                          Ha   =            229
930  n
mi
                                          Hp   =            218
357

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1587963
25                 X    =         -457451
72
 Y    =      -14922691
19  feet           Y    =        -4553700
91  meter
 Z    =       16438699
31                 Z    =         5008228
37
 XDOT =      22129
325837                 XDOT =        6788
172430
 YDOT =      -9862
970112  feet/sec       YDOT =       -2930
564196  meter/sec
 ZDOT =      -6780
312515                 ZDOT =       -2033
769833

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5712866
26                 X    =        -1741281
64
 Y    =       13889083
96  feet           Y    =         4233392
79  meter
 Z    =       16428502
07                 Z    =         5007407
43
 XDOT =     -23168
780674                 XDOT =       -7061
844349
 YDOT =      -1645
873463  feet/sec       YDOT =        -501
662232  meter/sec
 ZDOT =      -6629
849029                 ZDOT =       -2020
777984


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   19357
21327804  
00016717  00000-0  10270-3 0  9144
2 25544  51
6410 144
2171 0007601  61
9986 298
1933 15
50162595  4572


Satellite: ISS
Catalog Number: 25544
Epoch time:      19357
21327804   =   yrday
fracday
Element set:     914
Inclination:       51
6410  deg
RA of node:       144
2171  deg
Eccentricity:     
0007601     
Arg of perigee:    61
9986  deg
Mean anomaly:     298
1933  deg
Mean motion:   15
50162595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             457
Checksum:              310


Coasting Arc #16 (Orbit 471)
---------------------------------------

Vector Time (GMT): 2019/358/04:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         476730
11                 A    =         6790923
71  meter
 Y    =        4707891
01  meter          E    =           
0018287
 Z    =       -4886809
65                 I    =           51
88291
 XDOT =      -6497
424579                 Wp   =           91
43413
 YDOT =       3200
669454  meter/sec      RA   =          138
33873  deg
 ZDOT =       2457
134794                 TA   =          202
62598
                                          MA   =          202
70670
                                          Ha   =            230
011  n
mi
                                          Hp   =            218
313

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1564075
16                 X    =          447787
14
 Y    =       15445836
65  feet           Y    =         4713060
98  meter
 Z    =      -16032840
07                 Z    =        -4884563
52
 XDOT =     -21317
009775                 XDOT =       -6544
667930
 YDOT =      10500
884037  feet/sec       YDOT =        3127
746170  meter/sec
 ZDOT =       8061
465861                 ZDOT =        2425
458328

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5741204
49                 X    =         1749919
13
 Y    =      -14435341
49  feet           Y    =        -4399892
09  meter
 Z    =      -16022847
71                 Z    =        -4883763
98
 XDOT =      22748
657032                 XDOT =        6933
790663
 YDOT =        287
889967  feet/sec       YDOT =          87
748862  meter/sec
 ZDOT =       7916
418039                 ZDOT =        2412
924218


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   19358
18029536  
00016717  00000-0  10270-3 0  9153
2 25544  51
6420 139
4250 0007689  65
5685 294
6267 15
50138599  4724


Satellite: ISS
Catalog Number: 25544
Epoch time:      19358
18029536   =   yrday
fracday
Element set:     915
Inclination:       51
6420  deg
RA of node:       139
4250  deg
Eccentricity:     
0007689     
Arg of perigee:    65
5685  deg
Mean anomaly:     294
6267  deg
Mean motion:   15
50138599  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             472
Checksum:              341


Coasting Arc #17 (Orbit 487)
---------------------------------------

Vector Time (GMT): 2019/359/04:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -454384
58                 A    =         6791552
69  meter
 Y    =       -4876454
46  meter          E    =           
0015646
 Z    =        4695726
46                 I    =           51
90923
 XDOT =       6269
251386                 Wp   =           66
49013
 YDOT =      -3358
397120  meter/sec      RA   =          133
40007  deg
 ZDOT =      -2867
368366                 TA   =           51
94631
                                          MA   =           51
80523
                                          Ha   =            230
004  n
mi
                                          Hp   =            218
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1490763
05                 X    =         -422630
08
 Y    =      -15998866
33  feet           Y    =        -4881358
87  meter
 Z    =       15405926
71                 Z    =         4693595
62
 XDOT =      20568
410060                 XDOT =        6320
268089
 YDOT =     -11018
363255  feet/sec       YDOT =       -3288
004232  meter/sec
 ZDOT =      -9407
376529                 ZDOT =       -2836
791314

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5811295
68                 X    =        -1771282
92
 Y    =       14990194
51  feet           Y    =         4569011
29  meter
 Z    =       15396479
70                 Z    =         4692847
01
 XDOT =     -22291
302340                 XDOT =       -6794
388953
 YDOT =        922
741904  feet/sec       YDOT =         281
251732  meter/sec
 ZDOT =      -9267
318922                 ZDOT =       -2824
678808


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   19359
21177914  
00016717  00000-0  10270-3 0  9163
2 25544  51
6417 134
3145 0007677  68
8854 291
3117 15
50168072  4882


Satellite: ISS
Catalog Number: 25544
Epoch time:      19359
21177914   =   yrday
fracday
Element set:     916
Inclination:       51
6417  deg
RA of node:       134
3145  deg
Eccentricity:     
0007677     
Arg of perigee:    68
8854  deg
Mean anomaly:     291
3117  deg
Mean motion:   15
50168072  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             488
Checksum:              329


Coasting Arc #18 (Orbit 491)
---------------------------------------

Vector Time (GMT): 2019/359/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4880055
21                 A    =         6800830
30  meter
 Y    =        4688061
49  meter          E    =           
0020225
 Z    =         588119
38                 I    =           51
94127
 XDOT =      -2901
048715                 Wp   =           59
39688
 YDOT =      -3790
202009  meter/sec      RA   =          132
24786  deg
 ZDOT =       5997
645778                 TA   =          306
91634
                                          MA   =          307
10147
                                          Ha   =            230
023  n
mi
                                          Hp   =            218
280

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16010679
83                 X    =        -4934972
54
 Y    =       15380779
18  feet           Y    =         4633182
11  meter
 Z    =        1929525
53                 Z    =          564281
28
 XDOT =      -9517
876361                 XDOT =       -2887
583128
 YDOT =     -12435
045962  feet/sec       YDOT =       -3822
569222  meter/sec
 ZDOT =      19677
315544                 ZDOT =        5983
585715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4922276
70                 X    =        -1500309
94
 Y    =      -21658517
03  feet           Y    =        -6601515
99  meter
 Z    =        1820202
65                 Z    =          554797
77
 XDOT =      14049
815265                 XDOT =        4282
383693
 YDOT =      -1502
959077  feet/sec       YDOT =        -458
101927  meter/sec
 ZDOT =      19613
239915                 ZDOT =        5978
115526


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   19359
46965046  
00016717  00000-0  10270-3 0  9172
2 25544  51
6377 133
0319 0007574  73
2246 286
9735 15
50137610  4922


Satellite: ISS
Catalog Number: 25544
Epoch time:      19359
46965046   =   yrday
fracday
Element set:     917
Inclination:       51
6377  deg
RA of node:       133
0319  deg
Eccentricity:     
0007574     
Arg of perigee:    73
2246  deg
Mean anomaly:     286
9735  deg
Mean motion:   15
50137610  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             492
Checksum:              328


Coasting Arc #19 (Orbit 506)
---------------------------------------

Vector Time (GMT): 2019/360/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4673667
80                 A    =         6800422
03  meter
 Y    =       -4833465
40  meter          E    =           
0014625
 Z    =       -1005793
75                 I    =           51
96338
 XDOT =       2821
513278                 Wp   =          112
93547
 YDOT =       3945
990985  meter/sec      RA   =          127
31636  deg
 ZDOT =      -5926
089495                 TA   =           77
89139
                                          MA   =           77
72756
                                          Ha   =            229
998  n
mi
                                          Hp   =            218
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15333555
79                 X    =         4732255
22
 Y    =      -15857826
13  feet           Y    =        -4780873
40  meter
 Z    =       -3299848
28                 Z    =         -982949
45
 XDOT =       9256
933327                 XDOT =        2805
963802
 YDOT =      12946
164650  feet/sec       YDOT =        3977
457140  meter/sec
 ZDOT =     -19442
550837                 ZDOT =       -5912
420873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6041457
64                 X    =         1841436
29
 Y    =       21231347
24  feet           Y    =         6471314
64  meter
 Z    =       -3195037
62                 Z    =         -973847
47
 XDOT =     -14357
698605                 XDOT =       -4376
226535
 YDOT =       1206
794408  feet/sec       YDOT =         367
830936  meter/sec
 ZDOT =     -19380
272653                 ZDOT =       -5907
107105


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   19360
43666493  
00016717  00000-0  10270-3 0  9186
2 25544  51
6391 128
2399 0007622  74
8643 285
3350 15
50181162  5078


Satellite: ISS
Catalog Number: 25544
Epoch time:      19360
43666493   =   yrday
fracday
Element set:     918
Inclination:       51
6391  deg
RA of node:       128
2399  deg
Eccentricity:     
0007622     
Arg of perigee:    74
8643  deg
Mean anomaly:     285
3350  deg
Mean motion:   15
50181162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             507
Checksum:              318
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