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

 
Date: March 17th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14706 8384 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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


073/19:14:08 000 0 0 0 0 0 0
N/A 0 0 0 0 224 5
000/00:00:00 000 0 0 0 0 215 4

074/01:07:11 000 0 0 0 0 0 0
N/A 0 0 0 0 224 4
000/00:00:00 000 0 0 0 0 215 5

074/14:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 5
000/00:00:00 000 0 0 0 0 215 6

082/14:09:43 786 0 6 2 1 2 1
N/A 2 0 0 0 224 1
000/00:05:27 573 0 3 -0 0 217 1

082/22:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 1
000/00:00:00 000 0 0 0 0 217 1

087/06:36:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 9
000/00:00:00 000 0 0 0 0 217 1

Coasting Arc #1 (Orbit 38)
---------------------------------------

Vector Time (GMT): 2019/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900065
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3032882
76                 A    =         6793300
80  meter
 Y    =        6071878
82  meter          E    =           
0014871
 Z    =          92194
84                 I    =           52
00212
 XDOT =      -4181
578740                 Wp   =           58
24698
 YDOT =      -2191
108601  meter/sec      RA   =          115
93394  deg
 ZDOT =       6040
168000                 TA   =          302
74060
                                          MA   =          302
88385
                                          Ha   =            224
538  n
mi
                                          Hp   =            215
447

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9950402
77                 X    =        -3101002
65
 Y    =       19920862
28  feet           Y    =         6037582
13  meter
 Z    =         302476
50                 Z    =           77296
44
 XDOT =     -13719
090355                 XDOT =       -4186
106061
 YDOT =      -7188
676512  feet/sec       YDOT =       -2237
894873  meter/sec
 ZDOT =      19816
824146                 ZDOT =        6019
844659

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13276568
14                 X    =        -4046697
97
 Y    =       17877932
95  feet           Y    =         5449193
96  meter
 Z    =         234549
23                 Z    =           71490
61
 XDOT =     -11080
544084                 XDOT =       -3377
349837
 YDOT =      -8526
608295  feet/sec       YDOT =       -2598
910208  meter/sec
 ZDOT =      19725
053649                 ZDOT =        6012
196352


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   19072
56422397  
00016717  00000-0  10270-3 0  9004
2 25544  51
6391 116
6350 0003823  99
1163 261
0421 15
52762846   398


Satellite: ISS
Catalog Number: 25544
Epoch time:      19072
56422397   =   yrday
fracday
Element set:     900
Inclination:       51
6391  deg
RA of node:       116
6350  deg
Eccentricity:     
0003823     
Arg of perigee:    99
1163  deg
Mean anomaly:     261
0421  deg
Mean motion:   15
52762846  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              39
Checksum:              296


Coasting Arc #2 (Orbit 53)
---------------------------------------

Vector Time (GMT): 2019/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900065
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3359698
60                 A    =         6792364
47  meter
 Y    =       -5734006
89  meter          E    =           
0012011
 Z    =       -1385946
57                 I    =           52
01357
 XDOT =       3546
669112                 Wp   =          131
17336
 YDOT =       3479
002148  meter/sec      RA   =          110
99452  deg
 ZDOT =      -5836
406387                 TA   =           63
83892
                                          MA   =           63
71544
                                          Ha   =            224
492  n
mi
                                          Hp   =            215
374

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11022633
19                 X    =         3430300
31
 Y    =      -18812358
57  feet           Y    =        -5696041
70  meter
 Z    =       -4547068
79                 Z    =        -1369454
74
 XDOT =      11636
053516                 XDOT =        3535
852191
 YDOT =      11414
049042  feet/sec       YDOT =        3518
602712  meter/sec
 ZDOT =     -19148
314917                 ZDOT =       -5819
204541

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13879302
09                 X    =         4230411
28
 Y    =      -16835849
60  feet           Y    =        -5131566
96  meter
 Z    =       -4471940
67                 Z    =        -1363047
52
 XDOT =       8590
787816                 XDOT =        2618
472126
 YDOT =      12111
895913  feet/sec       YDOT =        3691
705874  meter/sec
 ZDOT =     -19070
778542                 ZDOT =       -5812
773300


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   19073
52957901  
00016717  00000-0  10270-3 0  9016
2 25544  51
6396 111
8322 0003881 105
0061 255
1521 15
52813382   541


Satellite: ISS
Catalog Number: 25544
Epoch time:      19073
52957901   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:       111
8322  deg
Eccentricity:     
0003881     
Arg of perigee:   105
0061  deg
Mean anomaly:     255
1521  deg
Mean motion:   15
52813382  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              54
Checksum:              281


Coasting Arc #3 (Orbit 58)
---------------------------------------

Vector Time (GMT): 2019/073/19:14:08
000
Vector Time (MET): N/A
Weight (LBS)     : 900065
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4233392
61                 A    =         6781393
48  meter
 Y    =        -405212
31  meter          E    =           
0006949
 Z    =        5277033
26                 I    =           51
97986
 XDOT =       1854
877061                 Wp   =          112
88578
 YDOT =      -7386
901108  meter/sec      RA   =          109
49863  deg
 ZDOT =        917
224041                 TA   =          328
36363
                                          MA   =          328
40538
                                          Ha   =            224
465  n
mi
                                          Hp   =            215
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13889083
37                 X    =        -4254179
50
 Y    =       -1329436
71  feet           Y    =         -452669
04  meter
 Z    =       17313101
23                 Z    =         5256418
69
 XDOT =       6085
554661                 XDOT =        1932
886288
 YDOT =     -24235
239857  feet/sec       YDOT =       -7365
722357  meter/sec
 ZDOT =       3009
265228                 ZDOT =         926
424091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1065947
48                 X    =          324900
79
 Y    =       14027044
99  feet           Y    =         4275443
31  meter
 Z    =       17219851
27                 Z    =         5248610
67
 XDOT =     -23889
718869                 XDOT =       -7281
586311
 YDOT =      -1945
231888  feet/sec       YDOT =        -592
906679  meter/sec
 ZDOT =       3051
547598                 ZDOT =         930
111708


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   19073
85136387  
00016717  00000-0  10270-3 0  9020
2 25544  51
6387 110
2329 0003551 104
6138 255
5407 15
52837301   594


Satellite: ISS
Catalog Number: 25544
Epoch time:      19073
85136387   =   yrday
fracday
Element set:     902
Inclination:       51
6387  deg
RA of node:       110
2329  deg
Eccentricity:     
0003551     
Arg of perigee:   104
6138  deg
Mean anomaly:     255
5407  deg
Mean motion:   15
52837301  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              59
Checksum:              298


Coasting Arc #4 (Orbit 62)
---------------------------------------

Vector Time (GMT): 2019/074/01:07:11
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2942531
67                 A    =         6792628
62  meter
 Y    =        6002897
02  meter          E    =           
0016204
 Z    =        1166088
83                 I    =           52
01830
 XDOT =      -3843
793339                 Wp   =           67
17519
 YDOT =      -3041
036147  meter/sec      RA   =          108
28617  deg
 ZDOT =       5896
543334                 TA   =          305
41657
                                          MA   =          305
56778
                                          Ha   =            224
360  n
mi
                                          Hp   =            215
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9653975
30                 X    =        -3015103
24
 Y    =       19694544
01  feet           Y    =         5969585
85  meter
 Z    =        3825750
75                 Z    =         1151618
69
 XDOT =     -12610
870536                 XDOT =       -3838
143849
 YDOT =      -9977
152712  feet/sec       YDOT =       -3083
988276  meter/sec
 ZDOT =      19345
614612                 ZDOT =        5877
885630

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6746614
05                 X    =         2056367
96
 Y    =      -20882007
72  feet           Y    =        -6364835
95  meter
 Z    =        3759737
28                 Z    =         1145967
92
 XDOT =      12519
451433                 XDOT =        3815
928797
 YDOT =       7548
165216  feet/sec       YDOT =        2300
680758  meter/sec
 ZDOT =      19261
451317                 ZDOT =        5870
890361


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   19074
10879143  
00016717  00000-0  10270-3 0  9034
2 25544  51
6373 108
9503 0003536 106
8449 253
3091 15
52804550   639


Satellite: ISS
Catalog Number: 25544
Epoch time:      19074
10879143   =   yrday
fracday
Element set:     903
Inclination:       51
6373  deg
RA of node:       108
9503  deg
Eccentricity:     
0003536     
Arg of perigee:   106
8449  deg
Mean anomaly:     253
3091  deg
Mean motion:   15
52804550  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              63
Checksum:              297


Coasting Arc #5 (Orbit 70)
---------------------------------------

Vector Time (GMT): 2019/074/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3872464
09                 A    =         6781360
92  meter
 Y    =        1642183
95  meter          E    =           
0018479
 Z    =       -5335177
71                 I    =           51
98598
 XDOT =      -2403
522147                 Wp   =           96
62971
 YDOT =       7249
065498  meter/sec      RA   =          105
49182  deg
 ZDOT =        486
091399                 TA   =          177
99839
                                          MA   =          177
99098
                                          Ha   =            224
479  n
mi
                                          Hp   =            215
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12704934
67                 X    =         3879727
99
 Y    =        5387742
63  feet           Y    =         1685528
94  meter
 Z    =      -17503863
86                 Z    =        -5316349
34
 XDOT =      -7885
571347                 XDOT =       -2486
765755
 YDOT =      23783
023286  feet/sec       YDOT =        7221
722210  meter/sec
 ZDOT =       1594
788054                 ZDOT =         474
213608

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13763827
17                 X    =         4195214
52
 Y    =       -1992681
61  feet           Y    =         -607369
36  meter
 Z    =      -17418802
12                 Z    =        -5309250
89
 XDOT =       5346
607252                 XDOT =        1629
645890
 YDOT =      23446
762586  feet/sec       YDOT =        7146
573236  meter/sec
 ZDOT =       1540
384848                 ZDOT =         469
509302


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   19074
62364840  
00016717  00000-0  10270-3 0  9045
2 25544  51
6372 106
3898 0003823 107
6075 252
5494 15
52781170   719


Satellite: ISS
Catalog Number: 25544
Epoch time:      19074
62364840   =   yrday
fracday
Element set:     904
Inclination:       51
6372  deg
RA of node:       106
3898  deg
Eccentricity:     
0003823     
Arg of perigee:   107
6075  deg
Mean anomaly:     252
5494  deg
Mean motion:   15
52781170  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              71
Checksum:              308


Coasting Arc #6 (Orbit 86)
---------------------------------------

Vector Time (GMT): 2019/075/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3500741
73                 A    =         6782377
58  meter
 Y    =       -2829772
70  meter          E    =           
0008368
 Z    =        5066768
88                 I    =           51
99746
 XDOT =       2796
346710                 Wp   =           77
00774
 YDOT =      -6884
250343  meter/sec      RA   =          100
53073  deg
 ZDOT =      -1908
299288                 TA   =           31
41885
                                          MA   =           31
36889
                                          Ha   =            224
526  n
mi
                                          Hp   =            215
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11485373
12                 X    =        -3493449
44
 Y    =       -9284031
18  feet           Y    =        -2868879
42  meter
 Z    =       16623257
49                 Z    =         5049781
68
 XDOT =       9174
365848                 XDOT =        2882
389850
 YDOT =     -22586
123173  feet/sec       YDOT =       -6852
498637  meter/sec
 ZDOT =      -6260
824436                 ZDOT =       -1894
506551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14753825
85                 X    =        -4496966
12
 Y    =       -1724321
20  feet           Y    =         -525573
10  meter
 Z    =       16546632
88                 Z    =         5043413
70
 XDOT =      -4283
844849                 XDOT =       -1305
715910
 YDOT =     -22961
556266  feet/sec       YDOT =       -6998
682350  meter/sec
 ZDOT =      -6197
770841                 ZDOT =       -1889
080552


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   19075
65335803  
00016717  00000-0  10270-3 0  9057
2 25544  51
6372 101
2666 0003720 110
1329 250
0223 15
52807253   874


Satellite: ISS
Catalog Number: 25544
Epoch time:      19075
65335803   =   yrday
fracday
Element set:     905
Inclination:       51
6372  deg
RA of node:       101
2666  deg
Eccentricity:     
0003720     
Arg of perigee:   110
1329  deg
Mean anomaly:     250
0223  deg
Mean motion:   15
52807253  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              87
Checksum:              275


Coasting Arc #7 (Orbit 101)
---------------------------------------

Vector Time (GMT): 2019/076/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3174400
17                 A    =         6784640
57  meter
 Y    =        3938171
36  meter          E    =           
0013338
 Z    =       -4534961
25                 I    =           52
00931
 XDOT =      -3123
520714                 Wp   =          110
92999
 YDOT =       6208
699031  meter/sec      RA   =           95
57407  deg
 ZDOT =       3208
204740                 TA   =          191
18143
                                          MA   =          191
21110
                                          Ha   =            224
427  n
mi
                                          Hp   =            215
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10414698
71                 X    =         3152154
45
 Y    =       12920509
70  feet           Y    =         3973545
03  meter
 Z    =      -14878481
80                 Z    =        -4519595
76
 XDOT =     -10247
771371                 XDOT =       -3208
299416
 YDOT =      20369
747476  feet/sec       YDOT =        6173
295824  meter/sec
 ZDOT =      10525
606104                 ZDOT =        3192
825784

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15854026
06                 X    =         4832307
14
 Y    =        5109722
12  feet           Y    =         1557443
30  meter
 Z    =      -14809299
05                 Z    =        -4513874
35
 XDOT =       2812
514241                 XDOT =         857
254341
 YDOT =      21547
712492  feet/sec       YDOT =        6567
742768  meter/sec
 ZDOT =      10455
421760                 ZDOT =        3186
812552


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   19076
61871035  
00016717  00000-0  10270-3 0  9067
2 25544  51
6367  96
4642 0003732 112
1212 248
0336 15
52783128  1027


Satellite: ISS
Catalog Number: 25544
Epoch time:      19076
61871035   =   yrday
fracday
Element set:     906
Inclination:       51
6367  deg
RA of node:        96
4642  deg
Eccentricity:     
0003732     
Arg of perigee:   112
1212  deg
Mean anomaly:     248
0336  deg
Mean motion:   15
52783128  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             102
Checksum:              288


Coasting Arc #8 (Orbit 117)
---------------------------------------

Vector Time (GMT): 2019/077/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2843550
28                 A    =         6787369
57  meter
 Y    =       -4910867
06  meter          E    =           
0014966
 Z    =        3710343
15                 I    =           52
02059
 XDOT =       3452
017981                 Wp   =           92
09673
 YDOT =      -5294
722644  meter/sec      RA   =           90
62197  deg
 ZDOT =      -4347
775770                 TA   =           43
93433
                                          MA   =           43
81544
                                          Ha   =            224
387  n
mi
                                          Hp   =            215
533

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9329233
20                 X    =        -2806446
70
 Y    =      -16111768
57  feet           Y    =        -4942457
83  meter
 Z    =       12173041
84                 Z    =         3696621
06
 XDOT =      11325
518310                 XDOT =        3532
087216
 YDOT =     -17371
137284  feet/sec       YDOT =       -5255
672466  meter/sec
 ZDOT =     -14264
356200                 ZDOT =       -4330
812509

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16808327
43                 X    =        -5123178
20
 Y    =       -8099442
00  feet           Y    =        -2468709
92  meter
 Z    =       12111391
10                 Z    =         3691552
01
 XDOT =       -830
387008                 XDOT =        -253
101960
 YDOT =     -19562
896537  feet/sec       YDOT =       -5962
770865  meter/sec
 ZDOT =     -14187
075924                 ZDOT =       -4324
220742


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   19077
64841816  
00016717  00000-0  10270-3 0  9076
2 25544  51
6364  91
3407 0003616 116
2420 243
9104 15
52816703  1184


Satellite: ISS
Catalog Number: 25544
Epoch time:      19077
64841816   =   yrday
fracday
Element set:     907
Inclination:       51
6364  deg
RA of node:        91
3407  deg
Eccentricity:     
0003616     
Arg of perigee:   116
2420  deg
Mean anomaly:     243
9104  deg
Mean motion:   15
52816703  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             118
Checksum:              294


Coasting Arc #9 (Orbit 132)
---------------------------------------

Vector Time (GMT): 2019/078/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2548740
75                 A    =         6790118
86  meter
 Y    =        5683838
20  meter          E    =           
0007359
 Z    =       -2707312
79                 I    =           52
02967
 XDOT =      -3764
182220                 Wp   =           82
12125
 YDOT =       4164
103222  meter/sec      RA   =           85
67583  deg
 ZDOT =       5211
643275                 TA   =          247
50569
                                          MA   =          247
58363
                                          Ha   =            224
354  n
mi
                                          Hp   =            215
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8362010
34                 X    =         2498143
45
 Y    =       18647763
14  feet           Y    =         5712056
78  meter
 Z    =       -8882259
82                 Z    =        -2695055
72
 XDOT =     -12349
679200                 XDOT =       -3835
781507
 YDOT =      13661
755979  feet/sec       YDOT =        4121
609778  meter/sec
 ZDOT =      17098
567176                 ZDOT =        5193
184200

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17588074
97                 X    =         5360845
25
 Y    =       10454419
14  feet           Y    =         3186506
95  meter
 Z    =       -8827319
30                 Z    =        -2690566
92
 XDOT =      -1620
946518                 XDOT =        -494
064499
 YDOT =      17057
083905  feet/sec       YDOT =        5198
999174  meter/sec
 ZDOT =      17014
615921                 ZDOT =        5186
054933


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   19078
61376724  
00016717  00000-0  10270-3 0  9086
2 25544  51
6372  86
5377 0003695 118
6256 241
5267 15
52802621  1330


Satellite: ISS
Catalog Number: 25544
Epoch time:      19078
61376724   =   yrday
fracday
Element set:     908
Inclination:       51
6372  deg
RA of node:        86
5377  deg
Eccentricity:     
0003695     
Arg of perigee:   118
6256  deg
Mean anomaly:     241
5267  deg
Mean motion:   15
52802621  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             133
Checksum:              320


Coasting Arc #10 (Orbit 148)
---------------------------------------

Vector Time (GMT): 2019/079/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2207569
61                 A    =         6792210
78  meter
 Y    =       -6235397
26  meter          E    =           
0017448
 Z    =        1505419
30                 I    =           52
03333
 XDOT =       4118
087490                 Wp   =          118
84947
 YDOT =      -2868
576150  meter/sec      RA   =           80
73401  deg
 ZDOT =      -5800
280370                 TA   =           44
80167
                                          MA   =           44
66091
                                          Ha   =            224
290  n
mi
                                          Hp   =            215
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7242682
44                 X    =        -2144991
96
 Y    =      -20457340
11  feet           Y    =        -6259733
75  meter
 Z    =        4939039
70                 Z    =         1494848
72
 XDOT =      13510
785727                 XDOT =        4178
032870
 YDOT =      -9411
339076  feet/sec       YDOT =       -2822
190432  meter/sec
 ZDOT =     -19029
791240                 ZDOT =       -5780
130498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17900483
33                 X    =        -5456067
32
 Y    =      -12288057
65  feet           Y    =        -3745399
97  meter
 Z    =        4891795
38                 Z    =         1491019
23
 XDOT =       4617
248466                 XDOT =        1407
337333
 YDOT =     -14321
306408  feet/sec       YDOT =       -4365
134193  meter/sec
 ZDOT =     -18938
306490                 ZDOT =       -5772
395818


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   19079
64347090  
00016717  00000-0  10270-3 0  9095
2 25544  51
6374  81
4137 0003582 121
4268 238
7234 15
52815993  1495


Satellite: ISS
Catalog Number: 25544
Epoch time:      19079
64347090   =   yrday
fracday
Element set:     909
Inclination:       51
6374  deg
RA of node:        81
4137  deg
Eccentricity:     
0003582     
Arg of perigee:   121
4268  deg
Mean anomaly:     238
7234  deg
Mean motion:   15
52815993  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             149
Checksum:              324


Coasting Arc #11 (Orbit 163)
---------------------------------------

Vector Time (GMT): 2019/080/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1862009
01                 A    =         6793090
70  meter
 Y    =        6523594
69  meter          E    =           
0012557
 Z    =        -261818
26                 I    =           52
02957
 XDOT =      -4476
337548                 Wp   =           59
94443
 YDOT =       1510
986754  meter/sec      RA   =           75
79584  deg
 ZDOT =       6035
258610                 TA   =          297
25161
                                          MA   =          297
37947
                                          Ha   =            224
230  n
mi
                                          Hp   =            215
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6108953
45                 X    =         1790193
70
 Y    =       21402869
71  feet           Y    =         6544015
39  meter
 Z    =        -858983
78                 Z    =         -252948
73
 XDOT =     -14686
146810                 XDOT =       -4522
216897
 YDOT =       4957
305624  feet/sec       YDOT =        1460
673552  meter/sec
 ZDOT =      19800
717226                 ZDOT =        6013
402733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17749634
33                 X    =         5410088
54
 Y    =       13432011
40  feet           Y    =         4094077
08  meter
 Z    =        -819480
40                 Z    =         -249777
62
 XDOT =      -7884
459748                 XDOT =       -2403
183331
 YDOT =      11574
325375  feet/sec       YDOT =        3527
854374  meter/sec
 ZDOT =      19701
641332                 ZDOT =        6005
060278


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   19080
60881729  
00016717  00000-0  10270-3 0  9107
2 25544  51
6370  76
6111 0003614 126
4413 233
7072 15
52825043  1641


Satellite: ISS
Catalog Number: 25544
Epoch time:      19080
60881729   =   yrday
fracday
Element set:     910
Inclination:       51
6370  deg
RA of node:        76
6111  deg
Eccentricity:     
0003614     
Arg of perigee:   126
4413  deg
Mean anomaly:     233
7072  deg
Mean motion:   15
52825043  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             164
Checksum:              282


Coasting Arc #12 (Orbit 179)
---------------------------------------

Vector Time (GMT): 2019/081/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1411944
44                 A    =         6792659
02  meter
 Y    =       -6556055
27  meter          E    =           
0013000
 Z    =       -1045225
82                 I    =           52
02064
 XDOT =       4860
452040                 Wp   =          138
26950
 YDOT =       -109
964566  meter/sec      RA   =           70
85722  deg
 ZDOT =      -5927
649416                 TA   =           52
99680
                                          MA   =           52
87790
                                          Ha   =            224
152  n
mi
                                          Hp   =            215
713

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4632363
65                 X    =        -1333450
71
 Y    =      -21509367
70  feet           Y    =        -6571405
88  meter
 Z    =       -3429218
58                 Z    =        -1051892
98
 XDOT =      15946
364961                 XDOT =        4890
113657
 YDOT =       -360
776134  feet/sec       YDOT =         -55
446541  meter/sec
 ZDOT =     -19447
668689                 ZDOT =       -5903
967136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16856311
59                 X    =        -5137803
77
 Y    =      -14134112
96  feet           Y    =        -4308077
63  meter
 Z    =       -3458734
19                 Z    =        -1054222
18
 XDOT =      11427
960287                 XDOT =        3483
242296
 YDOT =      -8937
294920  feet/sec       YDOT =       -2724
087492  meter/sec
 ZDOT =     -19340
467252                 ZDOT =       -5894
974418


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   19081
63851840  
00016717  00000-0  10270-3 0  9113
2 25544  51
6388  71
4873 0003466 129
8518 230
2940 15
52821383  1803


Satellite: ISS
Catalog Number: 25544
Epoch time:      19081
63851840   =   yrday
fracday
Element set:     911
Inclination:       51
6388  deg
RA of node:        71
4873  deg
Eccentricity:     
0003466     
Arg of perigee:   129
8518  deg
Mean anomaly:     230
2940  deg
Mean motion:   15
52821383  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             180
Checksum:              310


Coasting Arc #13 (Orbit 194)
---------------------------------------

Vector Time (GMT): 2019/082/14:12:27
573
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4608236
40                 A    =         6784273
72  meter
 Y    =         910977
42  meter          E    =           
0013350
 Z    =       -4907506
42                 I    =           51
97685
 XDOT =       1142
449180                 Wp   =          113
98539
 YDOT =       7176
920085  meter/sec      RA   =           65
95880  deg
 ZDOT =       2404
908622                 TA   =          179
51906
                                          MA   =          179
51777
                                          Ha   =            224
126  n
mi
                                          Hp   =            217
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15118885
84                 X    =         4621545
10
 Y    =        2988771
06  feet           Y    =          962583
79  meter
 Z    =      -16100742
86                 Z    =        -4885089
07
 XDOT =       3748
192848                 XDOT =        1050
428178
 YDOT =      23546
325737  feet/sec       YDOT =        7189
181508  meter/sec
 ZDOT =       7890
120151                 ZDOT =        2410
233889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14396153
04                 X    =         4387947
45
 Y    =       -5789486
32  feet           Y    =        -1764635
43  meter
 Z    =      -15999375
23                 Z    =        -4876609
57
 XDOT =      15504
379705                 XDOT =        4725
734934
 YDOT =      16683
068160  feet/sec       YDOT =        5084
999175  meter/sec
 ZDOT =       7913
480694                 ZDOT =        2412
028916


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   19082
60386100  
00016717  00000-0  10270-3 0  9124
2 25544  51
6388  66
6845 0002132 155
5541 204
5712 15
52416939  1953


Satellite: ISS
Catalog Number: 25544
Epoch time:      19082
60386100   =   yrday
fracday
Element set:     912
Inclination:       51
6388  deg
RA of node:        66
6845  deg
Eccentricity:     
0002132     
Arg of perigee:   155
5541  deg
Mean anomaly:     204
5712  deg
Mean motion:   15
52416939  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             195
Checksum:              301


Coasting Arc #14 (Orbit 200)
---------------------------------------

Vector Time (GMT): 2019/082/22:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1627890
19                 A    =         6785663
48  meter
 Y    =        4780613
10  meter          E    =           
0010466
 Z    =        4527375
93                 I    =           51
97535
 XDOT =      -5076
466475                 Wp   =          120
93820
 YDOT =      -4771
787067  meter/sec      RA   =           64
29521  deg
 ZDOT =       3202
663017                 TA   =          296
98893
                                          MA   =          297
09576
                                          Ha   =            224
137  n
mi
                                          Hp   =            217
057

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5340847
08                 X    =        -1703218
92
 Y    =       15684426
18  feet           Y    =         4761988
19  meter
 Z    =       14853595
57                 Z    =         4519284
75
 XDOT =     -16655
073738                 XDOT =       -5038
286510
 YDOT =     -15655
469379  feet/sec       YDOT =       -4828
341844  meter/sec
 ZDOT =      10507
424595                 ZDOT =        3178
096627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11086167
89                 X    =         3379063
97
 Y    =      -12358158
38  feet           Y    =        -3766766
68  meter
 Z    =       14816476
52                 Z    =         4516062
04
 XDOT =       8462
821538                 XDOT =        2579
468005
 YDOT =      20098
872652  feet/sec       YDOT =        6126
136384  meter/sec
 ZDOT =      10396
734648                 ZDOT =        3168
924721


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   19082
99009525  
00016717  00000-0  10270-3 0  9130
2 25544  51
6372  64
7618 0002182 160
2996 199
8241 15
52419604  2018


Satellite: ISS
Catalog Number: 25544
Epoch time:      19082
99009525   =   yrday
fracday
Element set:     913
Inclination:       51
6372  deg
RA of node:        64
7618  deg
Eccentricity:     
0002182     
Arg of perigee:   160
2996  deg
Mean anomaly:     199
8241  deg
Mean motion:   15
52419604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             201
Checksum:              312


Coasting Arc #15 (Orbit 215)
---------------------------------------

Vector Time (GMT): 2019/083/22:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2236586
99                 A    =         6783598
97  meter
 Y    =       -3964339
50  meter          E    =           
0013260
 Z    =       -5041513
46                 I    =           51
95281
 XDOT =       5036
680054                 Wp   =           85
46028
 YDOT =       5401
391730  meter/sec      RA   =           59
33907  deg
 ZDOT =      -2016
422880                 TA   =          165
01957
                                          MA   =          164
98026
                                          Ha   =            224
135  n
mi
                                          Hp   =            217
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7337883
84                 X    =         2305240
09
 Y    =      -13006363
19  feet           Y    =        -3938944
98  meter
 Z    =      -16540398
50                 Z    =        -5030481
85
 XDOT =      16524
540859                 XDOT =        4985
700518
 YDOT =      17721
101475  feet/sec       YDOT =        5457
430195  meter/sec
 ZDOT =      -6615
560629                 ZDOT =       -1992
080775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11743196
73                 X    =        -3579326
36
 Y    =        9315067
81  feet           Y    =         2839232
67  meter
 Z    =      -16490046
92                 Z    =        -5026166
30
 XDOT =      -8131
012253                 XDOT =       -2478
332535
 YDOT =     -21747
099650  feet/sec       YDOT =       -6628
515973  meter/sec
 ZDOT =      -6505
968131                 ZDOT =       -1983
019086


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   19083
95568255  
00016717  00000-0  10270-3 0  9148
2 25544  51
6369  59
9606 0002409 160
0303 200
0943 15
52432913  2167


Satellite: ISS
Catalog Number: 25544
Epoch time:      19083
95568255   =   yrday
fracday
Element set:     914
Inclination:       51
6369  deg
RA of node:        59
9606  deg
Eccentricity:     
0002409     
Arg of perigee:   160
0303  deg
Mean anomaly:     200
0943  deg
Mean motion:   15
52432913  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             216
Checksum:              299


Coasting Arc #16 (Orbit 231)
---------------------------------------

Vector Time (GMT): 2019/084/22:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2877616
85                 A    =         6782579
98  meter
 Y    =        3105804
07  meter          E    =           
0004996
 Z    =        5296208
81                 I    =           51
93143
 XDOT =      -4910
830238                 Wp   =          137
05928
 YDOT =      -5841
156907  meter/sec      RA   =           54
37863  deg
 ZDOT =        753
166425                 TA   =          305
75074
                                          MA   =          305
79719
                                          Ha   =            224
221  n
mi
                                          Hp   =            217
125

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9441000
18                 X    =        -2937859
05
 Y    =       10189645
90  feet           Y    =         3073288
05  meter
 Z    =       17376013
15                 Z    =         5282083
88
 XDOT =     -16111
647762                 XDOT =       -4848
806254
 YDOT =     -19163
900613  feet/sec       YDOT =       -5895
726399  meter/sec
 ZDOT =       2471
018455                 ZDOT =         729
462435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12552534
28                 X    =         3826012
45
 Y    =       -6133881
62  feet           Y    =        -1869607
12  meter
 Z    =       17311746
89                 Z    =         5276620
45
 XDOT =       7826
239608                 XDOT =        2385
437833
 YDOT =      22725
818965  feet/sec       YDOT =        6926
829621  meter/sec
 ZDOT =       2364
377192                 ZDOT =         720
662168


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   19084
98564162  
00016717  00000-0  10270-3 0  9156
2 25544  51
6372  54
8388 0002343 164
4609 195
6615 15
52392167  2325


Satellite: ISS
Catalog Number: 25544
Epoch time:      19084
98564162   =   yrday
fracday
Element set:     915
Inclination:       51
6372  deg
RA of node:        54
8388  deg
Eccentricity:     
0002343     
Arg of perigee:   164
4609  deg
Mean anomaly:     195
6615  deg
Mean motion:   15
52392167  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             232
Checksum:              325


Coasting Arc #17 (Orbit 246)
---------------------------------------

Vector Time (GMT): 2019/085/22:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3577633
46                 A    =         6782387
53  meter
 Y    =       -2237003
30  meter          E    =           
0015648
 Z    =       -5323531
93                 I    =           51
91219
 XDOT =       4627
219855                 Wp   =          102
74903
 YDOT =       6071
844474  meter/sec      RA   =           49
41594  deg
 ZDOT =        556
249034                 TA   =          172
56040
                                          MA   =          172
53715
                                          Ha   =            224
051  n
mi
                                          Hp   =            217
166

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11737642
59                 X    =         3628241
11
 Y    =       -7339249
69  feet           Y    =        -2196713
02  meter
 Z    =      -17465655
94                 Z    =        -5306030
11
 XDOT =      15181
167503                 XDOT =        4556
276918
 YDOT =      19920
749586  feet/sec       YDOT =        6123
192645  meter/sec
 ZDOT =       1824
964022                 ZDOT =         578
553684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13640442
66                 X    =        -4157606
92
 Y    =        2888671
19  feet           Y    =          880466
98  meter
 Z    =      -17386197
97                 Z    =        -5299313
14
 XDOT =      -7309
274683                 XDOT =       -2227
866924
 YDOT =     -22887
929639  feet/sec       YDOT =       -6976
240954  meter/sec
 ZDOT =       1925
232302                 ZDOT =         586
810806


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   19085
95122369  
00016717  00000-0  10270-3 0  9164
2 25544  51
6385  50
0375 0002449 165
6433 194
4789 15
52442457  2471


Satellite: ISS
Catalog Number: 25544
Epoch time:      19085
95122369   =   yrday
fracday
Element set:     916
Inclination:       51
6385  deg
RA of node:        50
0375  deg
Eccentricity:     
0002449     
Arg of perigee:   165
6433  deg
Mean anomaly:     194
4789  deg
Mean motion:   15
52442457  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             247
Checksum:              329


Coasting Arc #18 (Orbit 262)
---------------------------------------

Vector Time (GMT): 2019/086/22:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4266900
04                 A    =         6783528
95  meter
 Y    =        1396682
12  meter          E    =           
0005139
 Z    =        5080999
92                 I    =           51
89187
 XDOT =      -4203
936213                 Wp   =           81
87336
 YDOT =      -6144
888576  meter/sec      RA   =           44
45240  deg
 ZDOT =      -1838
941093                 TA   =           25
88226
                                          MA   =           25
85656
                                          Ha   =            224
225  n
mi
                                          Hp   =            217
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13999015
87                 X    =        -4306881
59
 Y    =        4582290
41  feet           Y    =         1348743
36  meter
 Z    =       16669947
24                 Z    =         5060175
82
 XDOT =     -13792
441644                 XDOT =       -4125
977361
 YDOT =     -20160
395589  feet/sec       YDOT =       -6191
464128  meter/sec
 ZDOT =      -6033
271301                 ZDOT =       -1859
172505

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14834492
78                 X    =         4521553
40
 Y    =         214598
52  feet           Y    =           65409
63  meter
 Z    =       16575546
54                 Z    =         5052226
58
 XDOT =       6526
766380                 XDOT =        1989
358393
 YDOT =      22437
895962  feet/sec       YDOT =        6839
070689  meter/sec
 ZDOT =      -6124
135933                 ZDOT =       -1866
636632


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   19086
98117836  
00016717  00000-0  10270-3 0  9172
2 25544  51
6372  44
9157 0002494 168
8636 191
2571 15
52402962  2636


Satellite: ISS
Catalog Number: 25544
Epoch time:      19086
98117836   =   yrday
fracday
Element set:     917
Inclination:       51
6372  deg
RA of node:        44
9157  deg
Eccentricity:     
0002494     
Arg of perigee:   168
8636  deg
Mean anomaly:     191
2571  deg
Mean motion:   15
52402962  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             263
Checksum:              332


Coasting Arc #19 (Orbit 267)
---------------------------------------

Vector Time (GMT): 2019/087/06:36:30
000
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3311054
03                 A    =         6792004
78  meter
 Y    =       -5479973
03  meter          E    =           
0007867
 Z    =       -2258830
40                 I    =           51
91647
 XDOT =       5285
135754                 Wp   =          144
55060
 YDOT =       -945
693713  meter/sec      RA   =           42
80979  deg
 ZDOT =      -5468
578986                 TA   =           60
45367
                                          MA   =           60
37527
                                          Ha   =            223
921  n
mi
                                          Hp   =            217
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10863038
16                 X    =        -3238557
24
 Y    =      -17978914
14  feet           Y    =        -5516594
31  meter
 Z    =       -7410860
88                 Z    =        -2274737
82
 XDOT =      17339
684231                 XDOT =        5321
881163
 YDOT =      -3102
669663  feet/sec       YDOT =        -886
386451  meter/sec
 ZDOT =     -17941
532107                 ZDOT =       -5442
816606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14923537
63                 X    =         4548694
27
 Y    =      -14746934
94  feet           Y    =        -4494865
77  meter
 Z    =       -7482228
63                 Z    =        -2280583
29
 XDOT =       6056
945467                 XDOT =        1846
156978
 YDOT =      15147
375212  feet/sec       YDOT =        4616
919965  meter/sec
 ZDOT =     -17824
833805                 ZDOT =       -5433
009344


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   19087
30303696  
00016717  00000-0  10270-3 0  9181
2 25544  51
6410  43
3190 0002238 169
5666 190
5533 15
52451331  2685


Satellite: ISS
Catalog Number: 25544
Epoch time:      19087
30303696   =   yrday
fracday
Element set:     918
Inclination:       51
6410  deg
RA of node:        43
3190  deg
Eccentricity:     
0002238     
Arg of perigee:   169
5666  deg
Mean anomaly:     190
5533  deg
Mean motion:   15
52451331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             268
Checksum:              300
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