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

 
Date: September 11th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14325 6884 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 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


254/16:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 218 5

260/17:57:24 363 -1 0 2 2 2 2
N/A -2 0 -0 2 229 7
000/00:00:44 725 -0 5 -0 0 219 0

264/20:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 218 9

268/13:57:43 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 218 7

268/17:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 7

Coasting Arc #1 (Orbit 2863)
---------------------------------------

Vector Time (GMT): 2019/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3881207
33                 A    =         6788186
71  meter
 Y    =       -1747772
16  meter          E    =           
0019978
 Z    =       -5303969
37                 I    =           51
26666
 XDOT =       3005
487787                 Wp   =           69
38945
 YDOT =      -7032
330821  meter/sec      RA   =          292
38795  deg
 ZDOT =        125
303624                 TA   =          201
77139
                                          MA   =          201
85642
                                          Ha   =            229
226  n
mi
                                          Hp   =            218
473

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12733619
84                 X    =        -3835611
35
 Y    =       -5734160
63  feet           Y    =        -1790919
93  meter
 Z    =      -17401474
32                 Z    =        -5322711
74
 XDOT =       9860
524234                 XDOT =        3083
293321
 YDOT =     -23071
951512  feet/sec       YDOT =       -6998
286292  meter/sec
 ZDOT =        411
101129                 ZDOT =         140
092376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11335909
34                 X    =         3455185
17
 Y    =        7972119
81  feet           Y    =         2429902
12  meter
 Z    =      -17486550
43                 Z    =        -5329900
57
 XDOT =     -13377
898233                 XDOT =       -4077
583381
 YDOT =      20021
016986  feet/sec       YDOT =        6102
405977  meter/sec
 ZDOT =        478
937312                 ZDOT =         145
980093


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   19254
51588503  
00016717  00000-0  10270-3 0  9003
2 25544  51
6425 293
0838 0008236  28
2688 331
8908 15
50419999 28645


Satellite: ISS
Catalog Number: 25544
Epoch time:      19254
51588503   =   yrday
fracday
Element set:     900
Inclination:       51
6425  deg
RA of node:       293
0838  deg
Eccentricity:     
0008236     
Arg of perigee:    28
2688  deg
Mean anomaly:     331
8908  deg
Mean motion:   15
50419999  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2864
Checksum:              342


Coasting Arc #2 (Orbit 2866)
---------------------------------------

Vector Time (GMT): 2019/254/16:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2435454
76                 A    =         6790576
38  meter
 Y    =       -4216092
75  meter          E    =           
0014992
 Z    =       -4744305
34                 I    =           51
26985
 XDOT =       4491
285401                 Wp   =           74
95776
 YDOT =      -5590
194779  meter/sec      RA   =          291
38317  deg
 ZDOT =       2673
159651                 TA   =          221
58519
                                          MA   =          221
69931
                                          Ha   =            229
278  n
mi
                                          Hp   =            218
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7990337
14                 X    =        -2365083
26
 Y    =      -13832325
28  feet           Y    =        -4242934
55  meter
 Z    =      -15565306
22                 Z    =        -4755964
53
 XDOT =      14735
188322                 XDOT =        4540
478205
 YDOT =     -18340
534052  feet/sec       YDOT =       -5539
694834  meter/sec
 ZDOT =       8770
208828                 ZDOT =        2695
096204

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15922320
12                 X    =         4853123
17
 Y    =        -127341
25  feet           Y    =          -38813
61  meter
 Z    =      -15617969
60                 Z    =        -4760357
13
 XDOT =       8830
589018                 XDOT =        2691
563533
 YDOT =      20601
043529  feet/sec       YDOT =        6279
198067  meter/sec
 ZDOT =       8870
421824                 ZDOT =        2703
704572


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   19254
70925063  
00016717  00000-0  10270-3 0  9011
2 25544  51
6402 292
1258 0008432  28
4904 331
6707 15
50422909 28670


Satellite: ISS
Catalog Number: 25544
Epoch time:      19254
70925063   =   yrday
fracday
Element set:     901
Inclination:       51
6402  deg
RA of node:       292
1258  deg
Eccentricity:     
0008432     
Arg of perigee:    28
4904  deg
Mean anomaly:     331
6707  deg
Mean motion:   15
50422909  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2867
Checksum:              305


Coasting Arc #3 (Orbit 2882)
---------------------------------------

Vector Time (GMT): 2019/255/16:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2429294
53                 A    =         6791491
77  meter
 Y    =        4481748
52  meter          E    =           
0016581
 Z    =        4482097
43                 I    =           51
26214
 XDOT =      -4276
979027                 Wp   =           50
21898
 YDOT =       5511
740365  meter/sec      RA   =          286
39782  deg
 ZDOT =      -3174
899667                 TA   =           71
94606
                                          MA   =           71
76547
                                          Ha   =            229
311  n
mi
                                          Hp   =            218
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7970126
40                 X    =         2357226
45
 Y    =       14703899
33  feet           Y    =         4508512
01  meter
 Z    =       14705044
05                 Z    =         4493722
50
 XDOT =     -14032
083421                 XDOT =       -4322
873287
 YDOT =      18083
137680  feet/sec       YDOT =        5463
655301  meter/sec
 ZDOT =     -10416
337491                 ZDOT =       -3195
787326

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16678736
86                 X    =        -5083678
99
 Y    =         -23867
08  feet           Y    =           -7274
69  meter
 Z    =       14757542
41                 Z    =         4498098
93
 XDOT =      -9325
730852                 XDOT =       -2842
482764
 YDOT =     -19639
593691  feet/sec       YDOT =       -5986
148157  meter/sec
 ZDOT =     -10511
756669                 ZDOT =       -3203
983433


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   19255
74053171  
00016717  00000-0  10270-3 0  9029
2 25544  51
6403 287
0131 0008508  31
6097 328
5563 15
50451745 28830


Satellite: ISS
Catalog Number: 25544
Epoch time:      19255
74053171   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:       287
0131  deg
Eccentricity:     
0008508     
Arg of perigee:    31
6097  deg
Mean anomaly:     328
5563  deg
Mean motion:   15
50451745  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2883
Checksum:              303


Coasting Arc #4 (Orbit 2897)
---------------------------------------

Vector Time (GMT): 2019/256/16:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2508790
88                 A    =         6792528
09  meter
 Y    =       -4698367
09  meter          E    =           
0013190
 Z    =       -4223472
07                 I    =           51
25636
 XDOT =       4048
399775                 Wp   =           71
18549
 YDOT =      -5398
503277  meter/sec      RA   =          281
41342  deg
 ZDOT =       3614
207785                 TA   =          236
00625
                                          MA   =          236
13163
                                          Ha   =            229
430  n
mi
                                          Hp   =            218
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8230941
21                 X    =        -2435550
79
 Y    =      -15414590
19  feet           Y    =        -4726013
05  meter
 Z    =      -13856535
68                 Z    =        -4235480
42
 XDOT =      13282
151493                 XDOT =        4090
910827
 YDOT =     -17711
624923  feet/sec       YDOT =       -5352
993179  meter/sec
 ZDOT =      11857
637089                 ZDOT =        3633
977010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17430477
00                 X    =         5312809
39
 Y    =        -174536
73  feet           Y    =          -53198
80  meter
 Z    =      -13910771
85                 Z    =        -4240003
26
 XDOT =       9686
158076                 XDOT =        2952
340982
 YDOT =      18575
838648  feet/sec       YDOT =        5661
915620  meter/sec
 ZDOT =      11947
944433                 ZDOT =        3641
733463


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   19256
70735784  
00016717  00000-0  10270-3 0  9034
2 25544  51
6396 282
2206 0008542  35
1259 325
0453 15
50427690 28986


Satellite: ISS
Catalog Number: 25544
Epoch time:      19256
70735784   =   yrday
fracday
Element set:     903
Inclination:       51
6396  deg
RA of node:       282
2206  deg
Eccentricity:     
0008542     
Arg of perigee:    35
1259  deg
Mean anomaly:     325
0453  deg
Mean motion:   15
50427690  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2898
Checksum:              324


Coasting Arc #5 (Orbit 2913)
---------------------------------------

Vector Time (GMT): 2019/257/16:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2578688
26                 A    =         6793611
70  meter
 Y    =        4936996
87  meter          E    =           
0018392
 Z    =        3882242
93                 I    =           51
25522
 XDOT =      -3865
851367                 Wp   =           62
65382
 YDOT =       5228
342430  meter/sec      RA   =          276
42864  deg
 ZDOT =      -4057
833303                 TA   =           70
19518
                                          MA   =           69
99698
                                          Ha   =            229
445  n
mi
                                          Hp   =            218
122

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8460263
34                 X    =         2504431
97
 Y    =       16197496
31  feet           Y    =         4965418
79  meter
 Z    =       12737017
50                 Z    =         3894588
32
 XDOT =     -12683
239392                 XDOT =       -3904
318249
 YDOT =      17153
354429  feet/sec       YDOT =        5184
896251  meter/sec
 ZDOT =     -13313
101387                 ZDOT =       -4076
706065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18231718
27                 X    =        -5557027
73
 Y    =         340265
57  feet           Y    =          103712
94  meter
 Z    =       12792780
20                 Z    =         3899239
40
 XDOT =      -9782
744592                 XDOT =       -2981
780552
 YDOT =     -17554
676351  feet/sec       YDOT =       -5350
665352  meter/sec
 ZDOT =     -13399
303697                 ZDOT =       -4084
107767


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   19257
73863830  
00016717  00000-0  10270-3 0  9043
2 25544  51
6401 277
1079 0008531  38
5490 321
6268 15
50454810 29145


Satellite: ISS
Catalog Number: 25544
Epoch time:      19257
73863830   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       277
1079  deg
Eccentricity:     
0008531     
Arg of perigee:    38
5490  deg
Mean anomaly:     321
6268  deg
Mean motion:   15
50454810  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2914
Checksum:              312


Coasting Arc #6 (Orbit 2928)
---------------------------------------

Vector Time (GMT): 2019/258/16:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2725954
90                 A    =         6794688
51  meter
 Y    =       -5110235
90  meter          E    =           
0012324
 Z    =       -3556741
89                 I    =           51
25653
 XDOT =       3685
353695                 Wp   =           62
15146
 YDOT =      -5039
194667  meter/sec      RA   =          271
44462  deg
 ZDOT =       4433
140478                 TA   =          255
70916
                                          MA   =          255
84605
                                          Ha   =            229
512  n
mi
                                          Hp   =            218
026

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8943421
60                 X    =        -2651331
47
 Y    =      -16765865
82  feet           Y    =        -5140302
59  meter
 Z    =      -11669100
69                 Z    =        -3569801
78
 XDOT =      12091
055430                 XDOT =        3719
895766
 YDOT =     -16532
790902  feet/sec       YDOT =       -4997
788832  meter/sec
 ZDOT =      14544
424142                 ZDOT =        4451
126996

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18946456
99                 X    =         5774880
09
 Y    =        -854477
22  feet           Y    =         -260444
66  meter
 Z    =      -11728111
25                 Z    =        -3574728
31
 XDOT =       9763
904141                 XDOT =        2976
037982
 YDOT =      16523
040805  feet/sec       YDOT =        5036
222837  meter/sec
 ZDOT =      14626
569141                 ZDOT =        4458
178274


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   19258
70546219  
00016717  00000-0  10270-3 0  9051
2 25544  51
6405 272
3150 0008507  41
8273 318
3527 15
50436346 29296


Satellite: ISS
Catalog Number: 25544
Epoch time:      19258
70546219   =   yrday
fracday
Element set:     905
Inclination:       51
6405  deg
RA of node:       272
3150  deg
Eccentricity:     
0008507     
Arg of perigee:    41
8273  deg
Mean anomaly:     318
3527  deg
Mean motion:   15
50436346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2929
Checksum:              311


Coasting Arc #7 (Orbit 2944)
---------------------------------------

Vector Time (GMT): 2019/259/16:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2856422
08                 A    =         6795801
28  meter
 Y    =        5297126
18  meter          E    =           
0019659
 Z    =        3146080
33                 I    =           51
26111
 XDOT =      -3564
154715                 Wp   =           74
91535
 YDOT =       4792
446851  meter/sec      RA   =          266
46099  deg
 ZDOT =      -4802
877716                 TA   =           68
64744
                                          MA   =           68
43774
                                          Ha   =            229
600  n
mi
                                          Hp   =            217
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9371463
51                 X    =         2781693
79
 Y    =       17379022
89  feet           Y    =         5328651
20  meter
 Z    =       10321785
87                 Z    =         3159773
78
 XDOT =     -11693
420980                 XDOT =       -3594
150510
 YDOT =      15723
250825  feet/sec       YDOT =        4752
421745  meter/sec
 ZDOT =     -15757
472822                 ZDOT =       -4820
264483

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19667588
30                 X    =        -5994680
91
 Y    =        1326379
67  feet           Y    =          404280
52  meter
 Z    =       10383675
44                 Z    =         3164944
27
 XDOT =      -9465
104642                 XDOT =       -2884
963895
 YDOT =     -15595
788805  feet/sec       YDOT =       -4753
596428  meter/sec
 ZDOT =     -15836
862136                 ZDOT =       -4827
075579


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   19259
73673934  
00016717  00000-0  10270-3 0  9061
2 25544  51
6409 267
2019 0008652  45
4335 314
7520 15
50456190 29457


Satellite: ISS
Catalog Number: 25544
Epoch time:      19259
73673934   =   yrday
fracday
Element set:     906
Inclination:       51
6409  deg
RA of node:       267
2019  deg
Eccentricity:     
0008652     
Arg of perigee:    45
4335  deg
Mean anomaly:     314
7520  deg
Mean motion:   15
50456190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2945
Checksum:              322


Coasting Arc #8 (Orbit 2959)
---------------------------------------

Vector Time (GMT): 2019/260/16:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3052681
99                 A    =         6796793
84  meter
 Y    =       -5405332
38  meter          E    =           
0013300
 Z    =       -2765366
84                 I    =           51
26700
 XDOT =       3455
992359                 Wp   =           52
71579
 YDOT =      -4548
942992  meter/sec      RA   =          261
47925  deg
 ZDOT =       5101
442024                 TA   =          275
84160
                                          MA   =          275
99319
                                          Ha   =            229
642  n
mi
                                          Hp   =            217
807

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10015360
86                 X    =        -2978578
38
 Y    =      -17734030
12  feet           Y    =        -5439055
54  meter
 Z    =       -9072725
84                 Z    =        -2780015
26
 XDOT =      11338
557607                 XDOT =        3481
822907
 YDOT =     -14924
353647  feet/sec       YDOT =       -4510
150742  meter/sec
 ZDOT =      16737
014516                 ZDOT =        5118
293249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20225962
24                 X    =         6164873
29
 Y    =       -2123078
92  feet           Y    =         -647114
45  meter
 Z    =       -9138961
60                 Z    =        -2785555
50
 XDOT =       9107
843738                 XDOT =        2776
070771
 YDOT =      14739
947161  feet/sec       YDOT =        4492
735895  meter/sec
 ZDOT =      16813
943662                 ZDOT =        5124
890028


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   19260
70356175  
00016717  00000-0  10270-3 0  9076
2 25544  51
6404 262
4096 0008603  48
9646 311
2247 15
50439286 29605


Satellite: ISS
Catalog Number: 25544
Epoch time:      19260
70356175   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:       262
4096  deg
Eccentricity:     
0008603     
Arg of perigee:    48
9646  deg
Mean anomaly:     311
2247  deg
Mean motion:   15
50439286  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2960
Checksum:              315


Coasting Arc #9 (Orbit 2960)
---------------------------------------

Vector Time (GMT): 2019/260/17:57:46
725
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3644142
13                 A    =         6790572
02  meter
 Y    =        2800255
14  meter          E    =           
0019140
 Z    =       -5016599
85                 I    =           51
24399
 XDOT =      -2637
154118                 Wp   =           64
68724
 YDOT =      -6910
795068  meter/sec      RA   =          261
26556  deg
 ZDOT =      -1939
729303                 TA   =          186
31811
                                          MA   =          186
34228
                                          Ha   =            229
679  n
mi
                                          Hp   =            218
974

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11955846
88                 X    =        -3650816
47
 Y    =        9187188
78  feet           Y    =         2759465
99  meter
 Z    =      -16458660
92                 Z    =        -5034318
35
 XDOT =      -8652
080441                 XDOT =       -2550
257398
 YDOT =     -22673
212166  feet/sec       YDOT =       -6939
799896  meter/sec
 ZDOT =      -6363
941284                 ZDOT =       -1952
328021

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8104031
55                 X    =        -2470108
82
 Y    =      -12609785
00  feet           Y    =        -3843462
47  meter
 Z    =      -16539414
33                 Z    =        -5041213
49
 XDOT =      22425
896121                 XDOT =        6835
413138
 YDOT =      -5981
581242  feet/sec       YDOT =       -1823
185963  meter/sec
 ZDOT =      -6420
755562                 ZDOT =       -1957
046295


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   19260
76801850  
00016717  00000-0  10270-3 0  9088
2 25544  51
6419 262
0898 0006956  44
4188 315
7520 15
50037247 29613


Satellite: ISS
Catalog Number: 25544
Epoch time:      19260
76801850   =   yrday
fracday
Element set:     908
Inclination:       51
6419  deg
RA of node:       262
0898  deg
Eccentricity:     
0006956     
Arg of perigee:    44
4188  deg
Mean anomaly:     315
7520  deg
Mean motion:   15
50037247  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2961
Checksum:              325


Coasting Arc #10 (Orbit 2976)
---------------------------------------

Vector Time (GMT): 2019/261/17:57:46
725
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3560547
21                 A    =         6790079
36  meter
 Y    =       -2696258
82  meter          E    =           
0009152
 Z    =        5106245
86                 I    =           51
24884
 XDOT =       2975
077685                 Wp   =           79
06530
 YDOT =       6892
892319  meter/sec      RA   =          256
28253  deg
 ZDOT =       1564
477266                 TA   =          355
76651
                                          MA   =          355
77425
                                          Ha   =            229
497  n
mi
                                          Hp   =            219
100

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11681585
32                 X    =         3565629
34
 Y    =       -8845993
51  feet           Y    =        -2656413
46  meter
 Z    =       16752775
12                 Z    =         5123554
41
 XDOT =       9760
753559                 XDOT =        2890
178807
 YDOT =      22614
476111  feet/sec       YDOT =        6925
687156  meter/sec
 ZDOT =       5132
799430                 ZDOT =        1578
722502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7999052
74                 X    =         2438111
27
 Y    =       12168691
41  feet           Y    =         3709017
14  meter
 Z    =       16831655
17                 Z    =         5130288
50
 XDOT =     -22362
400970                 XDOT =       -6816
059816
 YDOT =       7508
133903  feet/sec       YDOT =        2288
479214  meter/sec
 ZDOT =       5197
115817                 ZDOT =        1584
080901


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   19261
79957917  
00016717  00000-0  10270-3 0  9099
2 25544  51
6421 256
9793 0006752  47
6937 312
4785 15
50047608 29779


Satellite: ISS
Catalog Number: 25544
Epoch time:      19261
79957917   =   yrday
fracday
Element set:     909
Inclination:       51
6421  deg
RA of node:       256
9793  deg
Eccentricity:     
0006752     
Arg of perigee:    47
6937  deg
Mean anomaly:     312
4785  deg
Mean motion:   15
50047608  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2977
Checksum:              362


Coasting Arc #11 (Orbit 2991)
---------------------------------------

Vector Time (GMT): 2019/262/17:57:46
725
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3523791
41                 A    =         6789753
54  meter
 Y    =        2608682
51  meter          E    =           
0020359
 Z    =       -5202376
55                 I    =           51
25799
 XDOT =      -3295
999809                 Wp   =           71
14983
 YDOT =      -6799
075298  meter/sec      RA   =          251
29967  deg
 ZDOT =      -1174
154801                 TA   =          187
48092
                                          MA   =          187
51134
                                          Ha   =            229
727  n
mi
                                          Hp   =            218
831

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11560995
43                 X    =        -3527430
00
 Y    =        8558669
64  feet           Y    =         2569256
34  meter
 Z    =      -17068164
52                 Z    =        -5219503
00
 XDOT =     -10813
647667                 XDOT =       -3214
022156
 YDOT =     -22306
677486  feet/sec       YDOT =       -6835
475194  meter/sec
 ZDOT =      -3852
213915                 ZDOT =       -1189
966214

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7926890
26                 X    =        -2416116
15
 Y    =      -11891238
65  feet           Y    =        -3624449
54  meter
 Z    =      -17146210
53                 Z    =        -5226164
97
 XDOT =      21989
923698                 XDOT =        6702
528743
 YDOT =      -8988
706654  feet/sec       YDOT =       -2739
757788  meter/sec
 ZDOT =      -3923
673085                 ZDOT =       -1195
935556


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   19262
76666667  
00016717  00000-0  10270-3 0  9108
2 25544  51
6433 252
1882 0006905  50
6883 309
4879 15
50045061 29921


Satellite: ISS
Catalog Number: 25544
Epoch time:      19262
76666667   =   yrday
fracday
Element set:     910
Inclination:       51
6433  deg
RA of node:       252
1882  deg
Eccentricity:     
0006905     
Arg of perigee:    50
6883  deg
Mean anomaly:     309
4879  deg
Mean motion:   15
50045061  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2992
Checksum:              333


Coasting Arc #12 (Orbit 3007)
---------------------------------------

Vector Time (GMT): 2019/263/17:57:46
725
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3498073
89                 A    =         6789447
40  meter
 Y    =       -2500842
33  meter          E    =           
0008751
 Z    =        5246532
02                 I    =           51
26854
 XDOT =       3627
872810                 Wp   =           74
01829
 YDOT =       6711
077887  meter/sec      RA   =          246
31731  deg
 ZDOT =        781
371637                 TA   =            8
48407
                                          MA   =            8
46929
                                          Ha   =            229
610  n
mi
                                          Hp   =            218
913

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11476620
36                 X    =         3500294
03
 Y    =       -8204863
29  feet           Y    =        -2461711
78  meter
 Z    =       17213031
56                 Z    =         5263530
03
 XDOT =      11902
469849                 XDOT =        3548
762454
 YDOT =      22017
972070  feet/sec       YDOT =        6751
205016  meter/sec
 ZDOT =       2563
555241                 ZDOT =         798
802252

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7779829
45                 X    =         2371292
01
 Y    =       11654798
39  feet           Y    =         3552382
55  meter
 Z    =       17290488
15                 Z    =         5270140
79
 XDOT =     -21591
059646                 XDOT =       -6580
954980
 YDOT =      10498
560854  feet/sec       YDOT =        3199
961348  meter/sec
 ZDOT =       2642
399988                 ZDOT =         805
403516


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   19263
79822417  
00016717  00000-0  10270-3 0  9110
2 25544  51
6430 247
0776 0006866  54
4856 305
6934 15
50052810 30080


Satellite: ISS
Catalog Number: 25544
Epoch time:      19263
79822417   =   yrday
fracday
Element set:     911
Inclination:       51
6430  deg
RA of node:       247
0776  deg
Eccentricity:     
0006866     
Arg of perigee:    54
4856  deg
Mean anomaly:     305
6934  deg
Mean motion:   15
50052810  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3008
Checksum:              314


Coasting Arc #13 (Orbit 3022)
---------------------------------------

Vector Time (GMT): 2019/264/17:57:46
725
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3514171
72                 A    =         6789333
70  meter
 Y    =        2424523
04  meter          E    =           
0021010
 Z    =       -5297081
98                 I    =           51
28214
 XDOT =      -3931
202239                 Wp   =           77
74404
 YDOT =      -6547
013723  meter/sec      RA   =          241
33650  deg
 ZDOT =       -385
535806                 TA   =          188
53287
                                          MA   =          188
56864
                                          Ha   =            229
787  n
mi
                                          Hp   =            218
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11529434
77                 X    =        -3515291
77
 Y    =        7954471
91  feet           Y    =         2385218
68  meter
 Z    =      -17378877
89                 Z    =        -5314155
43
 XDOT =     -12897
645142                 XDOT =       -3855
826729
 YDOT =     -21479
703814  feet/sec       YDOT =       -6590
553757  meter/sec
 ZDOT =      -1264
881252                 ZDOT =        -404
449008

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7727787
06                 X    =        -2355429
49
 Y    =      -11566013
28  feet           Y    =        -3525320
85  meter
 Z    =      -17456675
80                 Z    =        -5320794
78
 XDOT =      20885
338034                 XDOT =        6365
851033
 YDOT =     -11901
016351  feet/sec       YDOT =       -3627
429784  meter/sec
 ZDOT =      -1350
498029                 ZDOT =        -411
631799


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   19264
76531037  
00016717  00000-0  10270-3 0  9124
2 25544  51
6426 242
2872 0006878  57
3435 302
8379 15
50045585 30237


Satellite: ISS
Catalog Number: 25544
Epoch time:      19264
76531037   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:       242
2872  deg
Eccentricity:     
0006878     
Arg of perigee:    57
3435  deg
Mean anomaly:     302
8379  deg
Mean motion:   15
50045585  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3023
Checksum:              315


Coasting Arc #14 (Orbit 3024)
---------------------------------------

Vector Time (GMT): 2019/264/20:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -520503
96                 A    =         6797274
62  meter
 Y    =       -6022243
34  meter          E    =           
0019303
 Z    =        3086578
22                 I    =           51
30839
 XDOT =       5577
710637                 Wp   =           75
15359
 YDOT =       2019
752587  meter/sec      RA   =          240
92031  deg
 ZDOT =       4860
665631                 TA   =          320
48331
                                          MA   =          320
62390
                                          Ha   =            229
783  n
mi
                                          Hp   =            218
925

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1707690
15                 X    =         -468115
80
 Y    =      -19758016
21  feet           Y    =        -6027770
98  meter
 Z    =       10126568
95                 Z    =         3084177
19
 XDOT =      18299
575582                 XDOT =        5531
100037
 YDOT =       6626
484866  feet/sec       YDOT =        2081
865994  meter/sec
 ZDOT =      15947
065719                 ZDOT =        4887
647002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16118887
82                 X    =         4913037
01
 Y    =      -11562460
08  feet           Y    =        -3524237
83  meter
 Z    =       10116016
09                 Z    =         3083361
70
 XDOT =       2684
897783                 XDOT =         818
356844
 YDOT =      17861
734143  feet/sec       YDOT =        5444
256567  meter/sec
 ZDOT =      16069
654359                 ZDOT =        4898
030649


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   19264
89425447  
00016717  00000-0  10270-3 0  9136
2 25544  51
6412 241
6477 0006832  56
8890 303
2915 15
50024037 30257


Satellite: ISS
Catalog Number: 25544
Epoch time:      19264
89425447   =   yrday
fracday
Element set:     913
Inclination:       51
6412  deg
RA of node:       241
6477  deg
Eccentricity:     
0006832     
Arg of perigee:    56
8890  deg
Mean anomaly:     303
2915  deg
Mean motion:   15
50024037  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3025
Checksum:              307


Coasting Arc #15 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2019/265/20:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         682770
62                 A    =         6796452
20  meter
 Y    =        5857557
69  meter          E    =           
0011071
 Z    =       -3391105
78                 I    =           51
32257
 XDOT =      -5784
139324                 Wp   =           73
48261
 YDOT =      -1982
902062  meter/sec      RA   =          235
94383  deg
 ZDOT =      -4599
174542                 TA   =          146
20050
                                          MA   =          146
12988
                                          Ha   =            229
782  n
mi
                                          Hp   =            218
906

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2240061
08                 X    =          633691
14
 Y    =       19217708
94  feet           Y    =         5864918
41  meter
 Z    =      -11125675
14                 Z    =        -3387908
46
 XDOT =     -18976
835053                 XDOT =       -5739
195726
 YDOT =      -6505
584192  feet/sec       YDOT =       -2047
333194  meter/sec
 ZDOT =     -15089
155323                 ZDOT =       -4627
162629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15175190
50                 X    =        -4625398
06
 Y    =       12015303
46  feet           Y    =         3662264
49  meter
 Z    =      -11111477
58                 Z    =        -3386778
37
 XDOT =      -3438
843566                 XDOT =       -1048
159519
 YDOT =     -18386
203137  feet/sec       YDOT =       -5604
114716  meter/sec
 ZDOT =     -15216
342732                 ZDOT =       -4637
941265


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   19265
86133828  
00016717  00000-0  10270-3 0  9144
2 25544  51
6409 236
8562 0006688  60
2622 299
9193 15
50024731 30402


Satellite: ISS
Catalog Number: 25544
Epoch time:      19265
86133828   =   yrday
fracday
Element set:     914
Inclination:       51
6409  deg
RA of node:       236
8562  deg
Eccentricity:     
0006688     
Arg of perigee:    60
2622  deg
Mean anomaly:     299
9193  deg
Mean motion:   15
50024731  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3040
Checksum:              320


Coasting Arc #16 (Orbit 3055)
---------------------------------------

Vector Time (GMT): 2019/266/20:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -849626
55                 A    =         6795706
38  meter
 Y    =       -5666788
70  meter          E    =           
0018062
 Z    =        3635824
15                 I    =           51
33944
 XDOT =       6022
366605                 Wp   =           83
20753
 YDOT =       1899
889891  meter/sec      RA   =          230
96756  deg
 ZDOT =       4351
926879                 TA   =          320
11592
                                          MA   =          320
24850
                                          Ha   =            229
827  n
mi
                                          Hp   =            218
832

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2787488
69                 X    =         -803856
55
 Y    =      -18591826
43  feet           Y    =        -5676033
80  meter
 Z    =       11928556
92                 Z    =         3631808
31
 XDOT =      19758
420621                 XDOT =        5979
534644
 YDOT =       6233
234551  feet/sec       YDOT =        1966
996876  meter/sec
 ZDOT =      14277
975326                 ZDOT =        4381
077199

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14141354
21                 X    =         4310284
76
 Y    =      -12404677
97  feet           Y    =        -3780945
85  meter
 Z    =       11910610
35                 Z    =         3630354
03
 XDOT =       4397
613346                 XDOT =        1340
392548
 YDOT =      18902
038185  feet/sec       YDOT =        5761
341239  meter/sec
 ZDOT =      14410
474047                 ZDOT =        4392
312489


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   19266
89289282  
00016717  00000-0  10270-3 0  9155
2 25544  51
6406 231
7447 0006773  63
5202 296
6643 15
50028410 30569


Satellite: ISS
Catalog Number: 25544
Epoch time:      19266
89289282   =   yrday
fracday
Element set:     915
Inclination:       51
6406  deg
RA of node:       231
7447  deg
Eccentricity:     
0006773     
Arg of perigee:    63
5202  deg
Mean anomaly:     296
6643  deg
Mean motion:   15
50028410  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3056
Checksum:              318


Coasting Arc #17 (Orbit 3070)
---------------------------------------

Vector Time (GMT): 2019/267/20:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         953355
43                 A    =         6794844
94  meter
 Y    =        5485612
41  meter          E    =           
0013258
 Z    =       -3909090
90                 I    =           51
35677
 XDOT =      -6236
630302                 Wp   =           71
34168
 YDOT =      -1796
585407  meter/sec      RA   =          225
99281  deg
 ZDOT =      -4049
322424                 TA   =          156
02347
                                          MA   =          155
96167
                                          Ha   =            229
883  n
mi
                                          Hp   =            218
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3127806
54                 X    =          910931
01
 Y    =       17997416
03  feet           Y    =         5496036
11  meter
 Z    =      -12825101
38                 Z    =        -3904563
15
 XDOT =     -20461
385504                 XDOT =       -6196
407540
 YDOT =      -5894
309079  feet/sec       YDOT =       -1866
103086  meter/sec
 ZDOT =     -13285
178558                 ZDOT =       -4079
519777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13238985
76                 X    =        -4035242
86
 Y    =       12607130
33  feet           Y    =         3842653
32  meter
 Z    =      -12804800
03                 Z    =        -3902903
05
 XDOT =      -5399
107471                 XDOT =       -1645
647957
 YDOT =     -19278
656776  feet/sec       YDOT =       -5876
134585  meter/sec
 ZDOT =     -13422
466952                 ZDOT =       -4091
167927


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   19267
85997390  
00016717  00000-0  10270-3 0  9169
2 25544  51
6388 226
9531 0006843  67
9430 292
2446 15
50034527 30713


Satellite: ISS
Catalog Number: 25544
Epoch time:      19267
85997390   =   yrday
fracday
Element set:     916
Inclination:       51
6388  deg
RA of node:       226
9531  deg
Eccentricity:     
0006843     
Arg of perigee:    67
9430  deg
Mean anomaly:     292
2446  deg
Mean motion:   15
50034527  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3071
Checksum:              336


Coasting Arc #18 (Orbit 3082)
---------------------------------------

Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1035358
41                 A    =         6790538
79  meter
 Y    =       -4463141
75  meter          E    =           
0011419
 Z    =        5002434
45                 I    =           51
36228
 XDOT =       6418
904863                 Wp   =           95
68600
 YDOT =       3705
254455  meter/sec      RA   =          222
27700  deg
 ZDOT =       1972
277385                 TA   =          335
06486
                                          MA   =          335
11998
                                          Ha   =            229
784  n
mi
                                          Hp   =            218
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3396845
17                 X    =         1060890
65
 Y    =      -14642853
51  feet           Y    =        -4451420
57  meter
 Z    =       16412186
53                 Z    =         5007526
11
 XDOT =      21059
399157                 XDOT =        6367
414379
 YDOT =      12156
346638  feet/sec       YDOT =        3776
747397  meter/sec
 ZDOT =       6470
726330                 ZDOT =        2003
332604

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5129422
62                 X    =         1563448
01
 Y    =       14102200
69  feet           Y    =         4298350
77  meter
 Z    =       16435587
67                 Z    =         5009567
12
 XDOT =     -23225
023781                 XDOT =       -7078
987249
 YDOT =        722
744285  feet/sec       YDOT =         220
292458  meter/sec
 ZDOT =       6611
832961                 ZDOT =        2015
286687


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   19268
63363911  
00016717  00000-0  10270-3 0  9173
2 25544  51
6406 223
1217 0006795  71
1486 289
0400 15
50067426 30839


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
63363911   =   yrday
fracday
Element set:     917
Inclination:       51
6406  deg
RA of node:       223
1217  deg
Eccentricity:     
0006795     
Arg of perigee:    71
1486  deg
Mean anomaly:     289
0400  deg
Mean motion:   15
50067426  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3083
Checksum:              306


Coasting Arc #19 (Orbit 3084)
---------------------------------------

Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916741
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1219050
09                 A    =         6790349
79  meter
 Y    =       -4338334
09  meter          E    =           
0011002
 Z    =        5070241
92                 I    =           51
36610
 XDOT =       6408
799750                 Wp   =           94
75015
 YDOT =       3837
475679  meter/sec      RA   =          221
63265  deg
 ZDOT =       1738
480285                 TA   =          338
35790
                                          MA   =          338
40436
                                          Ha   =            229
883  n
mi
                                          Hp   =            218
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3999508
16                 X    =         1242843
67
 Y    =      -14233379
57  feet           Y    =        -4324568
44  meter
 Z    =       16634651
98                 Z    =         5076221
66
 XDOT =      21026
245900                 XDOT =        6356
967134
 YDOT =      12590
143305  feet/sec       YDOT =        3908
853697  meter/sec
 ZDOT =       5703
675475                 ZDOT =        1769
485562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13267217
97                 X    =         4043848
04
 Y    =        6453883
55  feet           Y    =         1967143
71  meter
 Z    =       16662086
32                 Z    =         5078603
91
 XDOT =     -15786
186874                 XDOT =       -4811
629759
 YDOT =      17327
454889  feet/sec       YDOT =        5281
408250  meter/sec
 ZDOT =       5844
551186                 ZDOT =        1781
419202


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   19268
76258386  
00016717  00000-0  10270-3 0  9187
2 25544  51
6422 222
4834 0006918  71
6009 288
5893 15
50031022 30852


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
76258386   =   yrday
fracday
Element set:     918
Inclination:       51
6422  deg
RA of node:       222
4834  deg
Eccentricity:     
0006918     
Arg of perigee:    71
6009  deg
Mean anomaly:     288
5893  deg
Mean motion:   15
50031022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3085
Checksum:              323
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