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

 
Date: March 25th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 ET - UTC (sec) : 67 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


090/14:15:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 1
000/00:00:00 000 0 0 0 0 214 2

091/16:23:58 000 0 0 0 0 0 0
N/A 0 0 0 0 221 2
000/00:00:00 000 0 0 0 0 214 2

093/17:58:46 000 0 0 0 0 0 0
N/A 0 0 0 0 221 2
000/00:00:00 000 0 0 0 0 214 0

094/19:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 2
000/00:00:00 000 0 0 0 0 214 1

098/16:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 2
000/00:00:00 000 0 0 0 0 213 8

Coasting Arc #1 (Orbit 3195)
---------------------------------------

Vector Time (GMT): 2016/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904106
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1973076
71                 A    =         6788439
48  meter
 Y    =        6397638
58  meter          E    =           
0010995
 Z    =       -1088633
30                 I    =           51
99232
 XDOT =      -4853
685725                 Wp   =           30
54353
 YDOT =       -496
104856  meter/sec      RA   =          114
44076  deg
 ZDOT =       5916
826075                 TA   =          317
70340
                                          MA   =          317
78814
                                          Ha   =            220
839  n
mi
                                          Hp   =            214
550

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6473348
79                 X    =        -2039181
91
 Y    =       20989627
88  feet           Y    =         6375204
54  meter
 Z    =       -3571631
56                 Z    =        -1098379
57
 XDOT =     -15924
165764                 XDOT =       -4876
518970
 YDOT =      -1627
640604  feet/sec       YDOT =        -550
508795  meter/sec
 ZDOT =      19412
159039                 ZDOT =        5893
192577

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5517613
18                 X    =        -1681768
50
 Y    =       21253533
66  feet           Y    =         6478077
06  meter
 Z    =       -3615041
75                 Z    =        -1101864
73
 XDOT =     -14554
910531                 XDOT =       -4436
336730
 YDOT =       -513
681360  feet/sec       YDOT =        -156
570078  meter/sec
 ZDOT =      19309
540033                 ZDOT =        5885
547802


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   16085
50213813  
00016717  00000-0  10270-3 0  9000
2 25544  51
6409 115
4128 0002081 351
6731   8
4387 15
54256639 31961


Satellite: ISS
Catalog Number: 25544
Epoch time:      16085
50213813   =   yrday
fracday
Element set:     900
Inclination:       51
6409  deg
RA of node:       115
4128  deg
Eccentricity:     
0002081     
Arg of perigee:   351
6731  deg
Mean anomaly:       8
4387  deg
Mean motion:   15
54256639  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3196
Checksum:              295


Coasting Arc #2 (Orbit 3211)
---------------------------------------

Vector Time (GMT): 2016/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2753650
75                 A    =         6788775
25  meter
 Y    =       -6162899
28  meter          E    =           
0009014
 Z    =        -690205
99                 I    =           52
00573
 XDOT =       4083
667004                 Wp   =          131
97114
 YDOT =       2489
404760  meter/sec      RA   =          109
49447  deg
 ZDOT =      -5991
771270                 TA   =           55
44502
                                          MA   =           55
35999
                                          Ha   =            220
908  n
mi
                                          Hp   =            214
512

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9034287
22                 X    =         2825713
91
 Y    =      -20219485
81  feet           Y    =        -6131703
29  meter
 Z    =       -2264455
35                 Z    =         -676653
49
 XDOT =      13397
857624                 XDOT =        4084
632016
 YDOT =       8167
338451  feet/sec       YDOT =        2535
075631  meter/sec
 ZDOT =     -19658
042224                 ZDOT =       -5971
931685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7791907
81                 X    =         2374973
50
 Y    =      -20736439
91  feet           Y    =        -6320466
88  meter
 Z    =       -2204527
81                 Z    =         -671940
08
 XDOT =      12487
033250                 XDOT =        3806
047735
 YDOT =       6752
841542  feet/sec       YDOT =        2058
266102  meter/sec
 ZDOT =     -19572
241111                 ZDOT =       -5965
619091


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   16086
53088950  
00016717  00000-0  10270-3 0  9017
2 25544  51
6409 110
2832 0002081 355
8086   4
3049 15
54252156 32124


Satellite: ISS
Catalog Number: 25544
Epoch time:      16086
53088950   =   yrday
fracday
Element set:     901
Inclination:       51
6409  deg
RA of node:       110
2832  deg
Eccentricity:     
0002081     
Arg of perigee:   355
8086  deg
Mean anomaly:       4
3049  deg
Mean motion:   15
54252156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3212
Checksum:              285


Coasting Arc #3 (Orbit 3227)
---------------------------------------

Vector Time (GMT): 2016/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3313940
24                 A    =         6786616
61  meter
 Y    =        5420520
04  meter          E    =           
0014705
 Z    =        2363852
80                 I    =           52
00821
 XDOT =      -3243
520054                 Wp   =           64
69128
 YDOT =      -4355
457937  meter/sec      RA   =          104
54614  deg
 ZDOT =       5420
190844                 TA   =          321
57053
                                          MA   =          321
67517
                                          Ha   =            221
047  n
mi
                                          Hp   =            214
413

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10872507
36                 X    =        -3385790
22
 Y    =       17783858
40  feet           Y    =         5383059
90  meter
 Z    =        7755422
57                 Z    =         2347579
21
 XDOT =     -10641
469992                 XDOT =       -3220
904348
 YDOT =     -14289
560161  feet/sec       YDOT =       -4391
602033  meter/sec
 ZDOT =      17782
778360                 ZDOT =        5404
489961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9492855
27                 X    =        -2893422
29
 Y    =       18586792
62  feet           Y    =         5665254
39  meter
 Z    =        7683778
62                 Z    =         2342015
72
 XDOT =     -10488
242129                 XDOT =       -3196
816201
 YDOT =     -12707
666739  feet/sec       YDOT =       -3873
296822  meter/sec
 ZDOT =      17715
282459                 ZDOT =        5399
618094


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   16087
55963353  
00016717  00000-0  10270-3 0  9020
2 25544  51
6407 105
1539 0002296   1
8673 358
2488 15
54262542 32282


Satellite: ISS
Catalog Number: 25544
Epoch time:      16087
55963353   =   yrday
fracday
Element set:     902
Inclination:       51
6407  deg
RA of node:       105
1539  deg
Eccentricity:     
0002296     
Arg of perigee:     1
8673  deg
Mean anomaly:     358
2488  deg
Mean motion:   15
54262542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3228
Checksum:              316


Coasting Arc #4 (Orbit 3242)
---------------------------------------

Vector Time (GMT): 2016/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3729295
02                 A    =         6782831
86  meter
 Y    =       -4199414
21  meter          E    =           
0006976
 Z    =       -3811365
64                 I    =           52
00207
 XDOT =       2353
846405                 Wp   =           58
99744
 YDOT =       5933
027028  meter/sec      RA   =           99
59032  deg
 ZDOT =      -4236
160446                 TA   =          166
44739
                                          MA   =          166
42865
                                          Ha   =            220
985  n
mi
                                          Hp   =            214
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12235219
89                 X    =         3794490
87
 Y    =      -13777605
69  feet           Y    =        -4157346
63  meter
 Z    =      -12504480
43                 Z    =        -3793090
71
 XDOT =       7722
593192                 XDOT =        2307
904488
 YDOT =      19465
311773  feet/sec       YDOT =        5959
091977  meter/sec
 ZDOT =     -13898
164194                 ZDOT =       -4224
838178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10941560
48                 X    =         3334987
63
 Y    =      -14893061
07  feet           Y    =        -4539405
01  meter
 Z    =      -12424332
64                 Z    =        -3786936
59
 XDOT =       8550
920172                 XDOT =        2606
320469
 YDOT =      17830
153911  feet/sec       YDOT =        5434
630912  meter/sec
 ZDOT =     -13849
976792                 ZDOT =       -4221
472926


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   16088
52407486  
00016717  00000-0  10270-3 0  9039
2 25544  51
6400 100
3456 0002230   3
3619 356
7548 15
54274182 32435


Satellite: ISS
Catalog Number: 25544
Epoch time:      16088
52407486   =   yrday
fracday
Element set:     903
Inclination:       51
6400  deg
RA of node:       100
3456  deg
Eccentricity:     
0002230     
Arg of perigee:     3
3619  deg
Mean anomaly:     356
7548  deg
Mean motion:   15
54274182  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3243
Checksum:              288


Coasting Arc #5 (Orbit 3258)
---------------------------------------

Vector Time (GMT): 2016/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3987562
78                 A    =         6779149
97  meter
 Y    =        2607793
53  meter          E    =           
0006878
 Z    =        4817128
91                 I    =           51
99373
 XDOT =      -1470
030115                 Wp   =          100
84445
 YDOT =      -7065
600199  meter/sec      RA   =           94
62302  deg
 ZDOT =       2603
748753                 TA   =          323
61974
                                          MA   =          323
66647
                                          Ha   =            221
181  n
mi
                                          Hp   =            214
299

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13082555
06                 X    =        -4039827
11
 Y    =        8555753
04  feet           Y    =         2562910
18  meter
 Z    =       15804228
70                 Z    =         4797631
01
 XDOT =      -4822
933447                 XDOT =       -1403
559534
 YDOT =     -23181
103016  feet/sec       YDOT =       -7081
667147  meter/sec
 ZDOT =       8542
482785                 ZDOT =        2596
769788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12135321
70                 X    =        -3698846
05
 Y    =        9988687
44  feet           Y    =         3044551
93  meter
 Z    =       15719029
62                 Z    =         4791160
23
 XDOT =      -6731
114519                 XDOT =       -2051
643705
 YDOT =     -21597
881049  feet/sec       YDOT =       -6583
034144  meter/sec
 ZDOT =       8513
381410                 ZDOT =        2594
878654


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   16089
55280654  
00016717  00000-0  10270-3 0  9040
2 25544  51
6395  95
2157 0002303   7
1164 353
0021 15
54275217 32599


Satellite: ISS
Catalog Number: 25544
Epoch time:      16089
55280654   =   yrday
fracday
Element set:     904
Inclination:       51
6395  deg
RA of node:        95
2157  deg
Eccentricity:     
0002303     
Arg of perigee:     7
1164  deg
Mean anomaly:     353
0021  deg
Mean motion:   15
54275217  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3259
Checksum:              293


Coasting Arc #6 (Orbit 3273)
---------------------------------------

Vector Time (GMT): 2016/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4149108
68                 A    =         6777057
50  meter
 Y    =        -781091
68  meter          E    =           
0015481
 Z    =       -5314558
12                 I    =           51
98905
 XDOT =        570
749953                 Wp   =           76
52893
 YDOT =       7606
603298  meter/sec      RA   =           89
64839  deg
 ZDOT =       -670
501494                 TA   =          187
07937
                                          MA   =          187
10126
                                          Ha   =            221
095  n
mi
                                          Hp   =            214
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13612561
30                 X    =         4183350
62
 Y    =       -2562636
75  feet           Y    =         -734502
59  meter
 Z    =      -17436214
31                 Z    =        -5294319
47
 XDOT =       1872
539215                 XDOT =         488
905625
 YDOT =      24956
047567  feet/sec       YDOT =        7612
528127  meter/sec
 ZDOT =      -2199
808051                 ZDOT =        -667
928375

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13275471
07                 X    =         4046363
58
 Y    =       -4323830
10  feet           Y    =        -1317903
41  meter
 Z    =      -17348108
34                 Z    =        -5287703
42
 XDOT =       4794
474724                 XDOT =        1461
355896
 YDOT =      23531
817648  feet/sec       YDOT =        7172
498019  meter/sec
 ZDOT =      -2189
965902                 ZDOT =        -667
501607


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   16090
51723465  
00016717  00000-0  10270-3 0  9051
2 25544  51
6401  90
4076 0002334  11
6898 348
4309 15
54282699 32748


Satellite: ISS
Catalog Number: 25544
Epoch time:      16090
51723465   =   yrday
fracday
Element set:     905
Inclination:       51
6401  deg
RA of node:        90
4076  deg
Eccentricity:     
0002334     
Arg of perigee:    11
6898  deg
Mean anomaly:     348
4309  deg
Mean motion:   15
54282699  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3274
Checksum:              313


Coasting Arc #7 (Orbit 3275)
---------------------------------------

Vector Time (GMT): 2016/090/14:15:30
000
Vector Time (MET): N/A
Weight (LBS)     : 901911
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3899386
99                 A    =         6778116
22  meter
 Y    =        2320289
56  meter          E    =           
0005230
 Z    =        5031092
34                 I    =           51
99294
 XDOT =      -1680
095062                 Wp   =           99
52313
 YDOT =      -7208
281447  meter/sec      RA   =           89
19202  deg
 ZDOT =       2019
593759                 TA   =          330
94525
                                          MA   =          330
97434
                                          Ha   =            221
111  n
mi
                                          Hp   =            214
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12793264
39                 X    =        -3949482
21
 Y    =        7612498
57  feet           Y    =         2276404
36  meter
 Z    =       16506208
47                 Z    =         5012028
14
 XDOT =      -5512
122906                 XDOT =       -1609
175754
 YDOT =     -23649
217346  feet/sec       YDOT =       -7226
672679  meter/sec
 ZDOT =       6625
963775                 ZDOT =        2011
605124

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4634256
35                 X    =        -1412521
34
 Y    =       14243719
37  feet           Y    =         4341485
66  meter
 Z    =       16422934
97                 Z    =         5005710
58
 XDOT =     -18773
244693                 XDOT =       -5722
084982
 YDOT =     -13719
064267  feet/sec       YDOT =       -4181
570789  meter/sec
 ZDOT =       6592
513767                 ZDOT =        2009
398196


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   16090
64582433  
00016717  00000-0  10270-3 0  9064
2 25544  51
6400  89
7664 0002428   5
5181 354
5998 15
54323075 32760


Satellite: ISS
Catalog Number: 25544
Epoch time:      16090
64582433   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:        89
7664  deg
Eccentricity:     
0002428     
Arg of perigee:     5
5181  deg
Mean anomaly:     354
5998  deg
Mean motion:   15
54323075  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3276
Checksum:              318


Coasting Arc #8 (Orbit 3290)
---------------------------------------

Vector Time (GMT): 2016/091/14:15:30
000
Vector Time (MET): N/A
Weight (LBS)     : 901911
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4154099
20                 A    =         6776858
48  meter
 Y    =        -465084
66  meter          E    =           
0015566
 Z    =       -5347363
92                 I    =           51
98668
 XDOT =        801
114879                 Wp   =           80
66324
 YDOT =       7615
386704  meter/sec      RA   =           84
21488  deg
 ZDOT =        -37
637559                 TA   =          188
96540
                                          MA   =          188
99323
                                          Ha   =            221
099  n
mi
                                          Hp   =            214
310

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13628934
40                 X    =         4184966
39
 Y    =       -1525868
32  feet           Y    =         -418458
63  meter
 Z    =      -17543844
87                 Z    =        -5327109
30
 XDOT =       2628
329656                 XDOT =         716
081017
 YDOT =      24984
864515  feet/sec       YDOT =        7623
869848  meter/sec
 ZDOT =       -123
482806                 ZDOT =         -33
953118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9115500
39                 X    =         2778404
52
 Y    =      -10395580
89  feet           Y    =        -3168573
06  meter
 Z    =      -17455720
27                 Z    =        -5320503
54
 XDOT =      18033
933499                 XDOT =        5496
742930
 YDOT =      16009
100277  feet/sec       YDOT =        4879
573765  meter/sec
 ZDOT =       -108
826879                 ZDOT =         -33
170433


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   16091
61024665  
00016717  00000-0  10270-3 0  9071
2 25544  51
6397  84
9573 0002493  11
2875 348
8333 15
54300291 32918


Satellite: ISS
Catalog Number: 25544
Epoch time:      16091
61024665   =   yrday
fracday
Element set:     907
Inclination:       51
6397  deg
RA of node:        84
9573  deg
Eccentricity:     
0002493     
Arg of perigee:    11
2875  deg
Mean anomaly:     348
8333  deg
Mean motion:   15
54300291  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3291
Checksum:              313


Coasting Arc #9 (Orbit 3292)
---------------------------------------

Vector Time (GMT): 2016/091/16:23:58
000
Vector Time (MET): N/A
Weight (LBS)     : 901911
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2656074
33                 A    =         6781931
21  meter
 Y    =        4749932
33  meter          E    =           
0011106
 Z    =        4037232
63                 I    =           52
00494
 XDOT =      -3698
118671                 Wp   =           88
69388
 YDOT =      -5436
889954  meter/sec      RA   =           83
79815  deg
 ZDOT =       3954
595623                 TA   =          320
42189
                                          MA   =          320
50292
                                          Ha   =            221
171  n
mi
                                          Hp   =            214
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8714154
62                 X    =        -2728603
01
 Y    =       15583767
48  feet           Y    =         4719825
15  meter
 Z    =       13245513
88                 Z    =         4024153
51
 XDOT =     -12132
935272                 XDOT =       -3656
256911
 YDOT =     -17837
565465  feet/sec       YDOT =       -5478
010378  meter/sec
 ZDOT =      12974
395087                 ZDOT =        3936
733204

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12692146
45                 X    =         3868566
24
 Y    =       12618436
18  feet           Y    =         3846099
35  meter
 Z    =       13187813
48                 Z    =         4019645
55
 XDOT =     -19517
993198                 XDOT =       -5949
084327
 YDOT =       6120
948453  feet/sec       YDOT =        1865
665088  meter/sec
 ZDOT =      12897
722770                 ZDOT =        3931
225900


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   16091
73883597  
00016717  00000-0  10270-3 0  9082
2 25544  51
6410  84
3171 0002467  12
2758 347
8454 15
54312984 32931


Satellite: ISS
Catalog Number: 25544
Epoch time:      16091
73883597   =   yrday
fracday
Element set:     908
Inclination:       51
6410  deg
RA of node:        84
3171  deg
Eccentricity:     
0002467     
Arg of perigee:    12
2758  deg
Mean anomaly:     347
8454  deg
Mean motion:   15
54312984  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3293
Checksum:              327


Coasting Arc #10 (Orbit 3307)
---------------------------------------

Vector Time (GMT): 2016/092/16:23:58
000
Vector Time (MET): N/A
Weight (LBS)     : 901911
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3328220
37                 A    =         6778356
94  meter
 Y    =       -3205220
12  meter          E    =           
0013837
 Z    =       -4972184
70                 I    =           51
98969
 XDOT =       3082
766161                 Wp   =           64
75992
 YDOT =       6648
629547  meter/sec      RA   =           78
82893  deg
 ZDOT =      -2221
485104                 TA   =          183
63137
                                          MA   =          183
64142
                                          Ha   =            221
093  n
mi
                                          Hp   =            214
159

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10919358
17                 X    =         3387967
29
 Y    =      -10515814
04  feet           Y    =        -3167668
12  meter
 Z    =      -16312941
94                 Z    =        -4955871
66
 XDOT =      10114
062209                 XDOT =        3018
981423
 YDOT =      21813
089066  feet/sec       YDOT =        6682
746249  meter/sec
 ZDOT =      -7288
336955                 ZDOT =       -2206
665329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7445565
37                 X    =        -2269408
32
 Y    =      -13293064
47  feet           Y    =        -4051726
05  meter
 Z    =      -16241453
00                 Z    =        -4950394
88
 XDOT =      22684
592652                 XDOT =        6914
263840
 YDOT =      -3874
512192  feet/sec       YDOT =       -1180
951316  meter/sec
 ZDOT =      -7225
115530                 ZDOT =       -2202
215214


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   16092
70325044  
00016717  00000-0  10270-3 0  9099
2 25544  51
6419  79
5083 0002537  15
1055 345
0173 15
54337254 33080


Satellite: ISS
Catalog Number: 25544
Epoch time:      16092
70325044   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:        79
5083  deg
Eccentricity:     
0002537     
Arg of perigee:    15
1055  deg
Mean anomaly:     345
0173  deg
Mean motion:   15
54337254  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3308
Checksum:              293


Coasting Arc #11 (Orbit 3323)
---------------------------------------

Vector Time (GMT): 2016/093/16:23:58
000
Vector Time (MET): N/A
Weight (LBS)     : 901911
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3928334
35                 A    =         6776654
37  meter
 Y    =        1424287
16  meter          E    =           
0003654
 Z    =        5332312
75                 I    =           51
97725
 XDOT =      -2317
353237                 Wp   =           57
71999
 YDOT =      -7309
298653  meter/sec      RA   =           73
85207  deg
 ZDOT =        246
924867                 TA   =           29
94886
                                          MA   =           29
92796
                                          Ha   =            221
182  n
mi
                                          Hp   =            214
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12888236
05                 X    =        -3969871
14
 Y    =        4672858
15  feet           Y    =         1380126
20  meter
 Z    =       17494464
41                 Z    =         5313128
90
 XDOT =      -7602
864952                 XDOT =       -2236
646062
 YDOT =     -23980
638626  feet/sec       YDOT =       -7334
761553  meter/sec
 ZDOT =        810
120954                 ZDOT =         235
864524

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1531169
74                 X    =          466700
54
 Y    =       13730170
86  feet           Y    =         4184956
08  meter
 Z    =       17410814
00                 Z    =         5306816
11
 XDOT =     -24090
043378                 XDOT =       -7342
645222
 YDOT =       1725
913153  feet/sec       YDOT =         526
058329  meter/sec
 ZDOT =        763
369856                 ZDOT =         232
675132


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   16093
73194929  
00016717  00000-0  10270-3 0  9101
2 25544  51
6420  74
3791 0002499  15
3607 344
7621 15
54371440 33240


Satellite: ISS
Catalog Number: 25544
Epoch time:      16093
73194929   =   yrday
fracday
Element set:     910
Inclination:       51
6420  deg
RA of node:        74
3791  deg
Eccentricity:     
0002499     
Arg of perigee:    15
3607  deg
Mean anomaly:     344
7621  deg
Mean motion:   15
54371440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3324
Checksum:              305


Coasting Arc #12 (Orbit 3324)
---------------------------------------

Vector Time (GMT): 2016/093/17:58:46
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4188533
31                 A    =         6776778
80  meter
 Y    =         462773
50  meter          E    =           
0005004
 Z    =        5304733
39                 I    =           51
97850
 XDOT =      -1667
274539                 Wp   =           41
59875
 YDOT =      -7458
881368  meter/sec      RA   =           73
51804  deg
 ZDOT =       -661
756043                 TA   =           54
71108
                                          MA   =           54
66428
                                          Ha   =            221
170  n
mi
                                          Hp   =            214
006

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13741907
18                 X    =        -4219164
91
 Y    =        1518285
75  feet           Y    =          415763
79  meter
 Z    =       17403980
93                 Z    =         5284312
14
 XDOT =      -5470
060822                 XDOT =       -1580
529036
 YDOT =     -24471
395565  feet/sec       YDOT =       -7477
040984  meter/sec
 ZDOT =      -2171
115628                 ZDOT =        -669
643786

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3984435
81                 X    =         1214456
03
 Y    =       13354940
41  feet           Y    =         4070585
84  meter
 Z    =       17315126
18                 Z    =         5277650
46
 XDOT =     -22119
036171                 XDOT =       -6741
882225
 YDOT =       9473
923655  feet/sec       YDOT =        2887
651930  meter/sec
 ZDOT =      -2204
047710                 ZDOT =        -671
793742


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   16093
79624228  
00016717  00000-0  10270-3 0  9118
2 25544  51
6434  74
0588 0002488  14
8517 345
2709 15
54374328 33250


Satellite: ISS
Catalog Number: 25544
Epoch time:      16093
79624228   =   yrday
fracday
Element set:     911
Inclination:       51
6434  deg
RA of node:        74
0588  deg
Eccentricity:     
0002488     
Arg of perigee:    14
8517  deg
Mean anomaly:     345
2709  deg
Mean motion:   15
54374328  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3325
Checksum:              322


Coasting Arc #13 (Orbit 3339)
---------------------------------------

Vector Time (GMT): 2016/094/17:58:46
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4580576
53                 A    =         6778937
70  meter
 Y    =        1339705
44  meter          E    =           
0011682
 Z    =       -4824775
53                 I    =           51
97474
 XDOT =        635
786753                 Wp   =           95
54521
 YDOT =       7176
581582  meter/sec      RA   =           68
54133  deg
 ZDOT =       2600
645474                 TA   =          199
96359
                                          MA   =          200
00933
                                          Ha   =            221
155  n
mi
                                          Hp   =            214
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15028138
23                 X    =         4588691
81
 Y    =        4395359
05  feet           Y    =         1390973
31  meter
 Z    =      -15829316
05                 Z    =        -4802504
73
 XDOT =       2085
914543                 XDOT =         542
856387
 YDOT =      23545
215163  feet/sec       YDOT =        7183
172067  meter/sec
 ZDOT =       8532
301424                 ZDOT =        2603
507418

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1333965
69                 X    =          406592
74
 Y    =      -15698167
31  feet           Y    =        -4784801
39  meter
 Z    =      -15732750
73                 Z    =        -4795342
42
 XDOT =      21542
532746                 XDOT =        6566
163981
 YDOT =      -6717
422886  feet/sec       YDOT =       -2047
470496  meter/sec
 ZDOT =       8543
428885                 ZDOT =        2604
037124


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   16094
76064250  
00016717  00000-0  10270-3 0  9120
2 25544  51
6426  69
2499 0002559  19
2327 340
8922 15
54354545 33409


Satellite: ISS
Catalog Number: 25544
Epoch time:      16094
76064250   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:        69
2499  deg
Eccentricity:     
0002559     
Arg of perigee:    19
2327  deg
Mean anomaly:     340
8922  deg
Mean motion:   15
54354545  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3340
Checksum:              313


Coasting Arc #14 (Orbit 3340)
---------------------------------------

Vector Time (GMT): 2016/094/19:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1550588
15                 A    =         6788149
23  meter
 Y    =       -6492346
77  meter          E    =           
0008036
 Z    =       -1222178
29                 I    =           52
00406
 XDOT =       4914
947420                 Wp   =          127
37615
 YDOT =        -72
461430  meter/sec      RA   =           68
34416  deg
 ZDOT =      -5881
906615                 TA   =           65
83522
                                          MA   =           65
75123
                                          Ha   =            221
155  n
mi
                                          Hp   =            214
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5087231
47                 X    =        -1471937
07
 Y    =      -21300350
29  feet           Y    =        -6509246
85  meter
 Z    =       -4009771
28                 Z    =        -1229518
85
 XDOT =      16125
155579                 XDOT =        4943
964129
 YDOT =       -237
734351  feet/sec       YDOT =         -17
337659  meter/sec
 ZDOT =     -19297
593882                 ZDOT =       -5857
960595

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16446156
72                 X    =        -5012788
57
 Y    =       14452040
17  feet           Y    =         4404981
85  meter
 Z    =       -4040492
07                 Z    =        -1231541
98
 XDOT =      -6771
292693                 XDOT =       -2063
890013
 YDOT =     -13043
315037  feet/sec       YDOT =       -3975
602423  meter/sec
 ZDOT =     -19193
487938                 ZDOT =       -5850
175124


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   16094
82493577  
00016717  00000-0  10270-3 0  9136
2 25544  51
6420  68
9292 0002411  19
3074 340
8169 15
54311691 33416


Satellite: ISS
Catalog Number: 25544
Epoch time:      16094
82493577   =   yrday
fracday
Element set:     913
Inclination:       51
6420  deg
RA of node:        68
9292  deg
Eccentricity:     
0002411     
Arg of perigee:    19
3074  deg
Mean anomaly:     340
8169  deg
Mean motion:   15
54311691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3341
Checksum:              306


Coasting Arc #15 (Orbit 3356)
---------------------------------------

Vector Time (GMT): 2016/095/19:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         565373
53                 A    =         6785193
33  meter
 Y    =        6118919
45  meter          E    =           
0014757
 Z    =        2858893
86                 I    =           51
98176
 XDOT =      -5409
556155                 Wp   =           71
95121
 YDOT =      -1892
171866  meter/sec      RA   =           63
39191  deg
 ZDOT =       5102
542214                 TA   =          320
42217
                                          MA   =          320
52982
                                          Ha   =            221
156  n
mi
                                          Hp   =            213
941

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1854900
04                 X    =          483020
95
 Y    =       20075195
05  feet           Y    =         6124781
75  meter
 Z    =        9379573
03                 Z    =         2861439
48
 XDOT =     -17747
887648                 XDOT =       -5412
781326
 YDOT =      -6207
912945  feet/sec       YDOT =       -1952
682485  meter/sec
 ZDOT =      16740
624063                 ZDOT =        5076
256362

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16703352
17                 X    =         5091181
74
 Y    =      -11281206
10  feet           Y    =        -3438511
62  meter
 Z    =        9389510
95                 Z    =         2861922
94
 XDOT =       2381
582700                 XDOT =         725
906407
 YDOT =      17411
508715  feet/sec       YDOT =        5307
027856  meter/sec
 ZDOT =      16626
711439                 ZDOT =        5067
821647


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   16095
85362020  
00016717  00000-0  10270-3 0  9149
2 25544  51
6418  63
7991 0002570  20
3097 339
8158 15
54356481 33574


Satellite: ISS
Catalog Number: 25544
Epoch time:      16095
85362020   =   yrday
fracday
Element set:     914
Inclination:       51
6418  deg
RA of node:        63
7991  deg
Eccentricity:     
0002570     
Arg of perigee:    20
3097  deg
Mean anomaly:     339
8158  deg
Mean motion:   15
54356481  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3357
Checksum:              317


Coasting Arc #16 (Orbit 3371)
---------------------------------------

Vector Time (GMT): 2016/096/19:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         610989
42                 A    =         6781154
10  meter
 Y    =       -5292505
32  meter          E    =           
0009790
 Z    =       -4205894
51                 I    =           51
95315
 XDOT =       5637
600586                 Wp   =           58
83000
 YDOT =       3608
501264  meter/sec      RA   =           58
42801  deg
 ZDOT =      -3723
263605                 TA   =          173
05984
                                          MA   =          173
04627
                                          Ha   =            221
130  n
mi
                                          Hp   =            213
926

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2004558
45                 X    =          690556
62
 Y    =      -17363862
61  feet           Y    =        -5285228
54  meter
 Z    =      -13798866
50                 Z    =        -4202732
46
 XDOT =      18496
064916                 XDOT =        5614
916511
 YDOT =      11838
914908  feet/sec       YDOT =        3671
417305  meter/sec
 ZDOT =     -12215
431774                 ZDOT =       -3695
933056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16095746
58                 X    =        -4905983
56
 Y    =        6845081
22  feet           Y    =         2086380
75  meter
 Z    =      -13784139
47                 Z    =        -4201405
71
 XDOT =       1497
625781                 XDOT =         456
476338
 YDOT =     -20829
447137  feet/sec       YDOT =       -6348
815488  meter/sec
 ZDOT =     -12097
304037                 ZDOT =       -3687
258270


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   16096
81800383  
00016717  00000-0  10270-3 0  9156
2 25544  51
6418  58
9891 0002538  22
2071 337
9191 15
54370305 33720


Satellite: ISS
Catalog Number: 25544
Epoch time:      16096
81800383   =   yrday
fracday
Element set:     915
Inclination:       51
6418  deg
RA of node:        58
9891  deg
Eccentricity:     
0002538     
Arg of perigee:    22
2071  deg
Mean anomaly:     337
9191  deg
Mean motion:   15
54370305  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3372
Checksum:              310


Coasting Arc #17 (Orbit 3387)
---------------------------------------

Vector Time (GMT): 2016/097/19:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1883513
60                 A    =         6777882
59  meter
 Y    =        4103194
79  meter          E    =           
0006066
 Z    =        5050368
66                 I    =           51
92426
 XDOT =      -5547
015923                 Wp   =           98
30468
 YDOT =      -4934
507017  meter/sec      RA   =           53
45279  deg
 ZDOT =       1937
490803                 TA   =          332
96976
                                          MA   =          333
00133
                                          Ha   =            221
357  n
mi
                                          Hp   =            213
789

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6179506
57                 X    =        -1953789
29
 Y    =       13461925
16  feet           Y    =         4081739
86  meter
 Z    =       16569450
98                 Z    =         5041047
67
 XDOT =     -18198
871139                 XDOT =       -5500
836348
 YDOT =     -16189
327484  feet/sec       YDOT =       -4996
278962  meter/sec
 ZDOT =       6356
597123                 ZDOT =        1910
657418

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14780613
45                 X    =         4505130
98
 Y    =       -1519713
74  feet           Y    =         -463208
75  meter
 Z    =       16528169
05                 Z    =         5037785
93
 XDOT =      -4636
087487                 XDOT =       -1413
079466
 YDOT =      22886
170139  feet/sec       YDOT =        6975
704658  meter/sec
 ZDOT =       6240
890754                 ZDOT =        1902
223502


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   16097
84667362  
00016717  00000-0  10270-3 0  9169
2 25544  51
6416  53
8590 0002632  30
2171 329
9133 15
54355251 33880


Satellite: ISS
Catalog Number: 25544
Epoch time:      16097
84667362   =   yrday
fracday
Element set:     916
Inclination:       51
6416  deg
RA of node:        53
8590  deg
Eccentricity:     
0002632     
Arg of perigee:    30
2171  deg
Mean anomaly:     329
9133  deg
Mean motion:   15
54355251  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3388
Checksum:              313


Coasting Arc #18 (Orbit 3400)
---------------------------------------

Vector Time (GMT): 2016/098/16:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4318784
15                 A    =         6777595
87  meter
 Y    =       -1134388
40  meter          E    =           
0014261
 Z    =       -5111211
95                 I    =           51
90845
 XDOT =       3760
995031                 Wp   =           93
27028
 YDOT =       6436
732304  meter/sec      RA   =           49
08218  deg
 ZDOT =       1752
744013                 TA   =          193
61655
                                          MA   =          193
65506
                                          Ha   =            221
205  n
mi
                                          Hp   =            213
832

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14169239
32                 X    =         4355976
56
 Y    =       -3721746
71  feet           Y    =        -1085885
59  meter
 Z    =      -16769068
07                 Z    =        -5090141
63
 XDOT =      12339
222542                 XDOT =        3680
224178
 YDOT =      21117
888135  feet/sec       YDOT =        6478
338864  meter/sec
 ZDOT =       5750
472485                 ZDOT =        1770
817188

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -289971
18                 X    =          -88383
22
 Y    =      -14751432
22  feet           Y    =        -4496236
54  meter
 Z    =      -16677276
44                 Z    =        -5083233
86
 XDOT =      22329
888848                 XDOT =        6806
150121
 YDOT =      -7014
835697  feet/sec       YDOT =       -2138
121920  meter/sec
 ZDOT =       5827
806908                 ZDOT =        1776
315545


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   16098
68246153  
00016717  00000-0  10270-3 0  9174
2 25544  51
6436  49
6928 0002549  31
9769 328
1538 15
54404101 34013


Satellite: ISS
Catalog Number: 25544
Epoch time:      16098
68246153   =   yrday
fracday
Element set:     917
Inclination:       51
6436  deg
RA of node:        49
6928  deg
Eccentricity:     
0002549     
Arg of perigee:    31
9769  deg
Mean anomaly:     328
1538  deg
Mean motion:   15
54404101  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3401
Checksum:              321


Coasting Arc #19 (Orbit 3416)
---------------------------------------

Vector Time (GMT): 2016/099/16:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917037
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5236297
94                 A    =         6780739
03  meter
 Y    =        -397494
57  meter          E    =           
0012099
 Z    =        4283478
12                 I    =           51
89852
 XDOT =      -2468
653779                 Wp   =           65
20266
 YDOT =      -6313
829928  meter/sec      RA   =           44
10424  deg
 ZDOT =      -3590
808293                 TA   =           61
35733
                                          MA   =           61
23571
                                          Ha   =            221
270  n
mi
                                          Hp   =            213
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17179455
17                 X    =        -5252271
49
 Y    =       -1304116
03  feet           Y    =         -456139
18  meter
 Z    =       14053405
89                 Z    =         4258002
35
 XDOT =      -8099
257805                 XDOT =       -2380
424617
 YDOT =     -20714
665119  feet/sec       YDOT =       -6340
943132  meter/sec
 ZDOT =     -11780
867104                 ZDOT =       -3602
585584

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5011186
32                 X    =        -1527409
59
 Y    =       16577695
78  feet           Y    =         5052881
67  meter
 Z    =       13942762
63                 Z    =         4249754
05
 XDOT =     -20752
668816                 XDOT =       -6325
413455
 YDOT =       3713
003044  feet/sec       YDOT =        1131
723328  meter/sec
 ZDOT =     -11830
845384                 ZDOT =       -3606
041673


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   16099
71111428  
00016717  00000-0  10270-3 0  9186
2 25544  51
6445  44
5635 0002611  33
1754 326
9562 15
54445781 34179


Satellite: ISS
Catalog Number: 25544
Epoch time:      16099
71111428   =   yrday
fracday
Element set:     918
Inclination:       51
6445  deg
RA of node:        44
5635  deg
Eccentricity:     
0002611     
Arg of perigee:    33
1754  deg
Mean anomaly:     326
9562  deg
Mean motion:   15
54445781  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3417
Checksum:              309
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