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

 
Date: September 14th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


257/13:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 214 1

257/20:59:14 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 214 3

261/11:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 214 6

270/15:15:09 148 -0 4 0 9 0 9
N/A -0 7 -0 1 221 3
000/00:00:18 297 0 3 -0 0 216 0

271/01:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 216 1

Coasting Arc #1 (Orbit 1240)
---------------------------------------

Vector Time (GMT): 2018/257/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4329473
71                 A    =         6778548
64  meter
 Y    =         441692
30  meter          E    =           
0008280
 Z    =        5193550
72                 I    =           51
27000
 XDOT =      -2084
114790                 Wp   =          140
80137
 YDOT =       7299
012988  meter/sec      RA   =          292
66687  deg
 ZDOT =       1109
334565                 TA   =          298
47427
                                          MA   =          298
55764
                                          Ha   =            222
496  n
mi
                                          Hp   =            214
190

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14204310
09                 X    =         4298985
13
 Y    =        1449121
72  feet           Y    =          489937
41  meter
 Z    =       17039208
40                 Z    =         5214507
84
 XDOT =      -6837
646950                 XDOT =       -2170
968078
 YDOT =      23946
893005  feet/sec       YDOT =        7275
221432  meter/sec
 ZDOT =       3639
549097                 ZDOT =        1098
999069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14158947
25                 X    =        -4315647
12
 Y    =         420658
33  feet           Y    =          128216
66  meter
 Z    =       17133133
43                 Z    =         5222179
07
 XDOT =       3674
159634                 XDOT =        1119
883857
 YDOT =     -23610
441737  feet/sec       YDOT =       -7196
462642  meter/sec
 ZDOT =       3592
285229                 ZDOT =        1094
928538


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   18257
59179460  
00016717  00000-0  10270-3 0  9001
2 25544  51
6387 293
1683 0004796 155
2233 204
9150 15
53852726 12414


Satellite: ISS
Catalog Number: 25544
Epoch time:      18257
59179460   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:       293
1683  deg
Eccentricity:     
0004796     
Arg of perigee:   155
2233  deg
Mean anomaly:     204
9150  deg
Mean motion:   15
53852726  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1241
Checksum:              319


Coasting Arc #2 (Orbit 1240)
---------------------------------------

Vector Time (GMT): 2018/257/13:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3746807
63                 A    =         6778292
29  meter
 Y    =       -2031967
06  meter          E    =           
0017375
 Z    =       -5285190
16                 I    =           51
26822
 XDOT =       3209
269289                 Wp   =          107
12980
 YDOT =      -6939
479050  meter/sec      RA   =          292
48081  deg
 ZDOT =        388
889370                 TA   =          166
62697
                                          MA   =          166
58086
                                          Ha   =            222
606  n
mi
                                          Hp   =            214
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12292675
96                 X    =        -3698134
32
 Y    =       -6666558
60  feet           Y    =        -2073594
73  meter
 Z    =      -17339862
73                 Z    =        -5303272
58
 XDOT =      10529
098718                 XDOT =        3284
740919
 YDOT =     -22767
319719  feet/sec       YDOT =       -6903
168757  meter/sec
 ZDOT =       1275
883760                 ZDOT =         404
662832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13727422
48                 X    =         4184118
37
 Y    =        2073863
48  feet           Y    =          632113
59  meter
 Z    =      -17420697
10                 Z    =        -5309828
48
 XDOT =      -1898
670595                 XDOT =        -578
714797
 YDOT =      23995
437006  feet/sec       YDOT =        7313
809199  meter/sec
 ZDOT =       1347
488213                 ZDOT =         410
714407


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   18257
59179432  
00016717  00000-0  10270-3 0  9011
2 25544  51
6386 293
1689 0004716 157
2593 202
8770 15
53827821 12415


Satellite: ISS
Catalog Number: 25544
Epoch time:      18257
59179432   =   yrday
fracday
Element set:     901
Inclination:       51
6386  deg
RA of node:       293
1689  deg
Eccentricity:     
0004716     
Arg of perigee:   157
2593  deg
Mean anomaly:     202
8770  deg
Mean motion:   15
53827821  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1241
Checksum:              330


Coasting Arc #3 (Orbit 1245)
---------------------------------------

Vector Time (GMT): 2018/257/20:59:14
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         500926
43                 A    =         6785747
58  meter
 Y    =        5934778
49  meter          E    =           
0015302
 Z    =        3233675
86                 I    =           51
29082
 XDOT =      -5224
601944                 Wp   =          108
57431
 YDOT =       3028
497841  meter/sec      RA   =          290
96820  deg
 ZDOT =      -4735
227041                 TA   =           33
72998
                                          MA   =           33
63270
                                          Ha   =            222
528  n
mi
                                          Hp   =            214
331

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1643459
41                 X    =          418817
27
 Y    =       19471058
02  feet           Y    =         5939921
33  meter
 Z    =       10609172
76                 Z    =         3235909
33
 XDOT =     -17141
082495                 XDOT =       -5235
077770
 YDOT =       9936
016539  feet/sec       YDOT =        2970
013796  meter/sec
 ZDOT =     -15535
521788                 ZDOT =       -4760
632161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14441279
71                 X    =        -4401702
06
 Y    =       13155820
76  feet           Y    =         4009894
17  meter
 Z    =       10618447
46                 Z    =         3236502
78
 XDOT =     -17322
154302                 XDOT =       -5279
792631
 YDOT =      -6347
165129  feet/sec       YDOT =       -1934
615931  meter/sec
 ZDOT =     -15649
826666                 ZDOT =       -4770
067168


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   18257
91336497  
00016717  00000-0  10270-3 0  9024
2 25544  51
6400 291
5678 0004604 157
7321 202
4032 15
53831849 12469


Satellite: ISS
Catalog Number: 25544
Epoch time:      18257
91336497   =   yrday
fracday
Element set:     902
Inclination:       51
6400  deg
RA of node:       291
5678  deg
Eccentricity:     
0004604     
Arg of perigee:   157
7321  deg
Mean anomaly:     202
4032  deg
Mean motion:   15
53831849  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1246
Checksum:              307


Coasting Arc #4 (Orbit 1260)
---------------------------------------

Vector Time (GMT): 2018/258/20:59:14
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         339985
33                 A    =         6788660
44  meter
 Y    =       -6528146
41  meter          E    =           
0006034
 Z    =       -1833033
81                 I    =           51
29142
 XDOT =       5051
216589                 Wp   =           76
38724
 YDOT =      -1307
652282  meter/sec      RA   =          285
96763  deg
 ZDOT =       5610
951180                 TA   =          263
37000
                                          MA   =          263
43868
                                          Ha   =            222
379  n
mi
                                          Hp   =            214
421

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1115437
44                 X    =          421863
56
 Y    =      -21417803
18  feet           Y    =        -6523886
76  meter
 Z    =       -6013890
46                 Z    =        -1831183
00
 XDOT =      16572
232903                 XDOT =        5038
208528
 YDOT =      -4290
197776  feet/sec       YDOT =       -1251
238464  meter/sec
 ZDOT =      18408
632480                 ZDOT =        5635
456840

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17437737
66                 X    =         5315022
44
 Y    =      -12490044
81  feet           Y    =        -3806965
66  meter
 Z    =       -6004786
26                 Z    =        -1830258
85
 XDOT =      12721
382176                 XDOT =        3877
477287
 YDOT =       8884
432878  feet/sec       YDOT =        2707
975141  meter/sec
 ZDOT =      18518
687277                 ZDOT =        5644
495882


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   18258
87806760  
00016717  00000-0  10270-3 0  9036
2 25544  51
6413 286
7600 0004466 162
8037 197
3268 15
53868139 12613


Satellite: ISS
Catalog Number: 25544
Epoch time:      18258
87806760   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:       286
7600  deg
Eccentricity:     
0004466     
Arg of perigee:   162
8037  deg
Mean anomaly:     197
3268  deg
Mean motion:   15
53868139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1261
Checksum:              333


Coasting Arc #5 (Orbit 1276)
---------------------------------------

Vector Time (GMT): 2018/259/20:59:14
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1113621
46                 A    =         6790213
30  meter
 Y    =        6685377
55  meter          E    =           
0016522
 Z    =         223826
22                 I    =           51
28780
 XDOT =      -4769
147110                 Wp   =          141
07271
 YDOT =       -586
549910  meter/sec      RA   =          280
97402  deg
 ZDOT =      -5980
774374                 TA   =           36
50293
                                          MA   =           36
39042
                                          Ha   =            222
398  n
mi
                                          Hp   =            214
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3653613
73                 X    =        -1189383
68
 Y    =       21933653
38  feet           Y    =         6672500
66  meter
 Z    =         734338
00                 Z    =          218232
24
 XDOT =     -15646
808104                 XDOT =       -4733
182164
 YDOT =      -1924
376344  feet/sec       YDOT =        -639
681052  meter/sec
 ZDOT =     -19621
963168                 ZDOT =       -6003
853914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19215377
70                 X    =        -5856847
12
 Y    =       11191097
71  feet           Y    =         3411046
58  meter
 Z    =         708440
51                 Z    =          215932
67
 XDOT =      -7610
161447                 XDOT =       -2319
577209
 YDOT =     -11769
017389  feet/sec       YDOT =       -3587
196500  meter/sec
 ZDOT =     -19725
392412                 ZDOT =       -6012
299607


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   18259
90708340  
00016717  00000-0  10270-3 0  9047
2 25544  51
6411 281
6329 0004577 165
8229 194
3053 15
53819089 12778


Satellite: ISS
Catalog Number: 25544
Epoch time:      18259
90708340   =   yrday
fracday
Element set:     904
Inclination:       51
6411  deg
RA of node:       281
6329  deg
Eccentricity:     
0004577     
Arg of perigee:   165
8229  deg
Mean anomaly:     194
3053  deg
Mean motion:   15
53819089  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1277
Checksum:              329


Coasting Arc #6 (Orbit 1292)
---------------------------------------

Vector Time (GMT): 2018/260/20:59:14
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1773710
83                 A    =         6789314
74  meter
 Y    =       -6404967
83  meter          E    =           
0013015
 Z    =        1368011
98                 I    =           51
27932
 XDOT =       4398
889294                 Wp   =           78
46156
 YDOT =       2461
435787  meter/sec      RA   =          275
97987  deg
 ZDOT =       5776
636294                 TA   =          296
51415
                                          MA   =          296
64755
                                          Ha   =            222
215  n
mi
                                          Hp   =            214
642

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5819261
26                 X    =         1838556
05
 Y    =      -21013674
00  feet           Y    =        -6384770
33  meter
 Z    =        4488228
28                 Z    =         1376785
89
 XDOT =      14432
051490                 XDOT =        4342
978038
 YDOT =       8075
576729  feet/sec       YDOT =        2510
314903  meter/sec
 ZDOT =      18952
218813                 ZDOT =        5797
868650

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19710728
07                 X    =         6007829
92
 Y    =       -9303968
35  feet           Y    =        -2835849
55  meter
 Z    =        4528339
81                 Z    =         1380237
98
 XDOT =       2518
921829                 XDOT =         767
767373
 YDOT =      14676
909631  feet/sec       YDOT =        4473
522056  meter/sec
 ZDOT =      19047
145085                 ZDOT =        5805
569822


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   18260
93609583  
00016717  00000-0  10270-3 0  9052
2 25544  51
6404 276
5053 0004319 170
3496 189
7740 15
53856495 12939


Satellite: ISS
Catalog Number: 25544
Epoch time:      18260
93609583   =   yrday
fracday
Element set:     905
Inclination:       51
6404  deg
RA of node:       276
5053  deg
Eccentricity:     
0004319     
Arg of perigee:   170
3496  deg
Mean anomaly:     189
7740  deg
Mean motion:   15
53856495  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1293
Checksum:              335


Coasting Arc #7 (Orbit 1301)
---------------------------------------

Vector Time (GMT): 2018/261/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1118212
66                 A    =         6788717
17  meter
 Y    =        6438833
98  meter          E    =           
0017045
 Z    =        1801688
87                 I    =           51
27394
 XDOT =      -4639
521604                 Wp   =          126
99198
 YDOT =       2387
619298  meter/sec      RA   =          272
92005  deg
 ZDOT =      -5626
483561                 TA   =           33
09016
                                          MA   =           32
98364
                                          Ha   =            222
269  n
mi
                                          Hp   =            214
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3668676
70                 X    =         1037377
08
 Y    =       21124783
40  feet           Y    =         6450886
73  meter
 Z    =        5911052
71                 Z    =         1806924
06
 XDOT =     -15221
527571                 XDOT =       -4638
545344
 YDOT =       7833
396646  feet/sec       YDOT =        2335
742103  meter/sec
 ZDOT =     -18459
591737                 ZDOT =       -5649
018482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         483456
22                 X    =          147357
46
 Y    =      -21429251
43  feet           Y    =        -6531635
84  meter
 Z    =        5933772
82                 Z    =         1808613
96
 XDOT =      14756
266327                 XDOT =        4497
709976
 YDOT =      -4830
905862  feet/sec       YDOT =       -1472
460107  meter/sec
 ZDOT =     -18560
936596                 ZDOT =       -5657
373474


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   18261
51491501  
00016717  00000-0  10270-3 0  9067
2 25544  51
6388 273
6197 0004620 169
0366 191
0888 15
53863611 13021


Satellite: ISS
Catalog Number: 25544
Epoch time:      18261
51491501   =   yrday
fracday
Element set:     906
Inclination:       51
6388  deg
RA of node:       273
6197  deg
Eccentricity:     
0004620     
Arg of perigee:   169
0366  deg
Mean anomaly:     191
0888  deg
Mean motion:   15
53863611  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1302
Checksum:              312


Coasting Arc #8 (Orbit 1316)
---------------------------------------

Vector Time (GMT): 2018/262/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -427333
56                 A    =         6789994
84  meter
 Y    =       -6770338
19  meter          E    =           
0009358
 Z    =        -226907
52                 I    =           51
27884
 XDOT =       4775
399917                 Wp   =           65
50009
 YDOT =       -494
992055  meter/sec      RA   =          267
92508  deg
 ZDOT =       5974
612436                 TA   =          292
04417
                                          MA   =          292
14354
                                          Ha   =            222
156  n
mi
                                          Hp   =            214
669

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1402012
99                 X    =         -350491
80
 Y    =      -22212395
64  feet           Y    =        -6774687
30  meter
 Z    =        -744447
24                 Z    =         -228796
30
 XDOT =      15667
322562                 XDOT =        4751
558706
 YDOT =      -1623
989683  feet/sec       YDOT =        -441
723163  meter/sec
 ZDOT =      19601
746838                 ZDOT =        5997
751726

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2502580
67                 X    =         -762786
59
 Y    =       22115192
54  feet           Y    =         6740710
69  meter
 Z    =        -752137
73                 Z    =         -229251
58
 XDOT =     -13968
659657                 XDOT =       -4257
647463
 YDOT =       -932
478444  feet/sec       YDOT =        -284
219430  meter/sec
 ZDOT =      19705
582288                 ZDOT =        6006
261481


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   18262
47961105  
00016717  00000-0  10270-3 0  9076
2 25544  51
6397 268
8130 0004573 173
9289 186
1920 15
53890048 13171


Satellite: ISS
Catalog Number: 25544
Epoch time:      18262
47961105   =   yrday
fracday
Element set:     907
Inclination:       51
6397  deg
RA of node:       268
8130  deg
Eccentricity:     
0004573     
Arg of perigee:   173
9289  deg
Mean anomaly:     186
1920  deg
Mean motion:   15
53890048  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1317
Checksum:              331


Coasting Arc #9 (Orbit 1332)
---------------------------------------

Vector Time (GMT): 2018/263/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -314816
95                 A    =         6789283
54  meter
 Y    =        6627897
28  meter          E    =           
0012562
 Z    =       -1406921
01                 I    =           51
27643
 XDOT =      -4841
157176                 Wp   =          153
95878
 YDOT =      -1448
133304  meter/sec      RA   =          262
93079  deg
 ZDOT =      -5769
497517                 TA   =           41
45968
                                          MA   =           41
36444
                                          Ha   =            222
116  n
mi
                                          Hp   =            214
799

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1032864
01                 X    =         -382074
49
 Y    =       21745069
82  feet           Y    =         6624000
62  meter
 Z    =       -4615882
56                 Z    =        -1408614
10
 XDOT =     -15883
061600                 XDOT =       -4796
578881
 YDOT =      -4751
093516  feet/sec       YDOT =       -1502
021644  meter/sec
 ZDOT =     -18928
797629                 ZDOT =       -5792
905703

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4417267
45                 X    =         1346383
12
 Y    =      -21314913
86  feet           Y    =        -6496785
74  meter
 Z    =       -4624222
83                 Z    =        -1409463
12
 XDOT =      13256
439316                 XDOT =        4040
562704
 YDOT =       6854
715243  feet/sec       YDOT =        2089
317206  meter/sec
 ZDOT =     -19033
623528                 ZDOT =       -5801
448451


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   18263
50861887  
00016717  00000-0  10270-3 0  9088
2 25544  51
6378 263
6851 0004513 176
2802 183
8385 15
53854175 13332


Satellite: ISS
Catalog Number: 25544
Epoch time:      18263
50861887   =   yrday
fracday
Element set:     908
Inclination:       51
6378  deg
RA of node:       263
6851  deg
Eccentricity:     
0004513     
Arg of perigee:   176
2802  deg
Mean anomaly:     183
8385  deg
Mean motion:   15
53854175  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1333
Checksum:              334


Coasting Arc #10 (Orbit 1348)
---------------------------------------

Vector Time (GMT): 2018/264/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1060793
55                 A    =         6786536
84  meter
 Y    =       -6053098
39  meter          E    =           
0013172
 Z    =        2871539
30                 I    =           51
27156
 XDOT =       4808
770924                 Wp   =          100
61734
 YDOT =       3234
832314  meter/sec      RA   =          257
93208  deg
 ZDOT =       5020
397679                 TA   =          292
24711
                                          MA   =          292
38676
                                          Ha   =            221
944  n
mi
                                          Hp   =            214
938

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3480293
79                 X    =         1114453
77
 Y    =      -19859246
69  feet           Y    =        -6040935
58  meter
 Z    =        9421060
68                 Z    =         2876823
10
 XDOT =      15776
807492                 XDOT =        4747
854391
 YDOT =      10612
966908  feet/sec       YDOT =        3288
267159  meter/sec
 ZDOT =      16471
120994                 ZDOT =        5043
608681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6176162
08                 X    =        -1882494
20
 Y    =       19180653
53  feet           Y    =         5846263
20  meter
 Z    =        9445425
37                 Z    =         2878965
65
 XDOT =     -12620
030265                 XDOT =       -3846
585225
 YDOT =     -12261
431404  feet/sec       YDOT =       -3737
284292  meter/sec
 ZDOT =      16574
874773                 ZDOT =        5052
021831


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   18264
53762390  
00016717  00000-0  10270-3 0  9092
2 25544  51
6367 258
5577 0004462 182
8076 177
3052 15
53881888 13494


Satellite: ISS
Catalog Number: 25544
Epoch time:      18264
53762390   =   yrday
fracday
Element set:     909
Inclination:       51
6367  deg
RA of node:       258
5577  deg
Eccentricity:     
0004462     
Arg of perigee:   182
8076  deg
Mean anomaly:     177
3052  deg
Mean motion:   15
53881888  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1349
Checksum:              350


Coasting Arc #11 (Orbit 1363)
---------------------------------------

Vector Time (GMT): 2018/265/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1882810
61                 A    =         6782943
66  meter
 Y    =        5068846
00  meter          E    =           
0006995
 Z    =       -4099602
83                 I    =           51
26750
 XDOT =      -4643
140120                 Wp   =          106
08350
 YDOT =      -4779
223911  meter/sec      RA   =          252
92404  deg
 ZDOT =      -3784
005362                 TA   =          124
67506
                                          MA   =          124
60913
                                          Ha   =            221
878  n
mi
                                          Hp   =            214
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6177200
16                 X    =        -1919438
27
 Y    =       16630072
18  feet           Y    =         5047585
88  meter
 Z    =      -13450140
53                 Z    =        -4108838
33
 XDOT =     -15233
399345                 XDOT =       -4570
971776
 YDOT =     -15679
868474  feet/sec       YDOT =       -4830
743600  meter/sec
 ZDOT =     -12414
715755                 ZDOT =       -3806
384274

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8095846
32                 X    =         2467613
96
 Y    =      -15749401
05  feet           Y    =        -4800417
44  meter
 Z    =      -13492109
61                 Z    =        -4112395
01
 XDOT =      11948
273878                 XDOT =        3641
833878
 YDOT =      16842
383877  feet/sec       YDOT =        5133
558606  meter/sec
 ZDOT =     -12514
585035                 ZDOT =       -3814
445519


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   18265
50231549  
00016717  00000-0  10270-3 0  9109
2 25544  51
6368 253
7496 0004367 184
4340 175
6775 15
53860339 13646


Satellite: ISS
Catalog Number: 25544
Epoch time:      18265
50231549   =   yrday
fracday
Element set:     910
Inclination:       51
6368  deg
RA of node:       253
7496  deg
Eccentricity:     
0004367     
Arg of perigee:   184
4340  deg
Mean anomaly:     175
6775  deg
Mean motion:   15
53860339  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1364
Checksum:              329


Coasting Arc #12 (Orbit 1379)
---------------------------------------

Vector Time (GMT): 2018/266/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2707809
36                 A    =         6779785
11  meter
 Y    =       -3805868
33  meter          E    =           
0009023
 Z    =        4912592
93                 I    =           51
26714
 XDOT =       4321
806689                 Wp   =          147
88028
 YDOT =       5937
707201  meter/sec      RA   =          247
90836  deg
 ZDOT =       2208
482500                 TA   =          280
40440
                                          MA   =          280
50608
                                          Ha   =            221
708  n
mi
                                          Hp   =            215
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8883888
97                 X    =         2726303
61
 Y    =      -12486444
65  feet           Y    =        -3775483
74  meter
 Z    =       16117430
87                 Z    =         4925791
89
 XDOT =      14179
155803                 XDOT =        4244
360754
 YDOT =      19480
666670  feet/sec       YDOT =        5985
603876  meter/sec
 ZDOT =       7245
677492                 ZDOT =        2229
287518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10056102
57                 X    =        -3065100
06
 Y    =       11479751
33  feet           Y    =         3499028
20  meter
 Z    =       16177035
32                 Z    =         4930760
37
 XDOT =     -11138
814891                 XDOT =       -3395
110779
 YDOT =     -20141
799426  feet/sec       YDOT =       -6139
220465  meter/sec
 ZDOT =       7338
382293                 ZDOT =        2236
738923


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   18266
53131633  
00016717  00000-0  10270-3 0  9117
2 25544  51
6362 248
6218 0004236 189
5939 170
5133 15
53863579 13809


Satellite: ISS
Catalog Number: 25544
Epoch time:      18266
53131633   =   yrday
fracday
Element set:     911
Inclination:       51
6362  deg
RA of node:       248
6218  deg
Eccentricity:     
0004236     
Arg of perigee:   189
5939  deg
Mean anomaly:     170
5133  deg
Mean motion:   15
53863579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1380
Checksum:              320


Coasting Arc #13 (Orbit 1394)
---------------------------------------

Vector Time (GMT): 2018/267/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3562036
45                 A    =         6778196
73  meter
 Y    =        2338497
88  meter          E    =           
0014197
 Z    =       -5283159
02                 I    =           51
27518
 XDOT =      -3771
788338                 Wp   =          103
61787
 YDOT =      -6652
534243  meter/sec      RA   =          242
88671  deg
 ZDOT =       -405
798093                 TA   =          162
51203
                                          MA   =          162
46309
                                          Ha   =            221
669  n
mi
                                          Hp   =            215
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11686471
30                 X    =        -3562258
57
 Y    =        7672237
14  feet           Y    =         2298662
80  meter
 Z    =      -17333198
89                 Z    =        -5300463
04
 XDOT =     -12374
633656                 XDOT =       -3695
146366
 YDOT =     -21825
899747  feet/sec       YDOT =       -6694
284517  meter/sec
 ZDOT =      -1331
358572                 ZDOT =        -423
933190

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12210185
22                 X    =         3721664
45
 Y    =       -6606279
18  feet           Y    =        -2013593
89  meter
 Z    =      -17411061
72                 Z    =        -5306891
61
 XDOT =       9883
862660                 XDOT =        3012
601339
 YDOT =      21953
315841  feet/sec       YDOT =        6691
370668  meter/sec
 ZDOT =      -1412
031348                 ZDOT =        -430
387155


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   18267
49600302  
00016717  00000-0  10270-3 0  9128
2 25544  51
6361 243
8145 0004254 192
8362 167
2683 15
53861264 13959


Satellite: ISS
Catalog Number: 25544
Epoch time:      18267
49600302   =   yrday
fracday
Element set:     912
Inclination:       51
6361  deg
RA of node:       243
8145  deg
Eccentricity:     
0004254     
Arg of perigee:   192
8362  deg
Mean anomaly:     167
2683  deg
Mean motion:   15
53861264  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1395
Checksum:              311


Coasting Arc #14 (Orbit 1410)
---------------------------------------

Vector Time (GMT): 2018/268/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4343669
75                 A    =         6778723
90  meter
 Y    =        -822911
86  meter          E    =           
0002777
 Z    =        5136364
70                 I    =           51
29376
 XDOT =       2995
075198                 Wp   =          122
21153
 YDOT =       6915
891759  meter/sec      RA   =          237
86485  deg
 ZDOT =      -1425
718730                 TA   =          341
56333
                                          MA   =          341
57339
                                          Ha   =            221
396  n
mi
                                          Hp   =            215
413

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14250884
99                 X    =         4327599
01
 Y    =       -2699842
07  feet           Y    =         -774427
13  meter
 Z    =       16851590
21                 Z    =         5157425
96
 XDOT =       9826
362199                 XDOT =        2924
442615
 YDOT =      22689
933594  feet/sec       YDOT =        6948
989654  meter/sec
 ZDOT =      -4677
554887                 ZDOT =       -1411
342035

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14296506
59                 X    =        -4357575
21
 Y    =        1670533
66  feet           Y    =          509178
66  meter
 Z    =       16946155
30                 Z    =         5165188
14
 XDOT =      -8071
107403                 XDOT =       -2460
073536
 YDOT =     -22299
703279  feet/sec       YDOT =       -6796
949559  meter/sec
 ZDOT =      -4613
751711                 ZDOT =       -1406
271522


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   18268
52499979  
00016717  00000-0  10270-3 0  9130
2 25544  51
6366 238
6864 0004248 198
2495 161
8506 15
53879985 14116


Satellite: ISS
Catalog Number: 25544
Epoch time:      18268
52499979   =   yrday
fracday
Element set:     913
Inclination:       51
6366  deg
RA of node:       238
6864  deg
Eccentricity:     
0004248     
Arg of perigee:   198
2495  deg
Mean anomaly:     161
8506  deg
Mean motion:   15
53879985  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1411
Checksum:              370


Coasting Arc #15 (Orbit 1425)
---------------------------------------

Vector Time (GMT): 2018/269/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5026180
61                 A    =         6781333
39  meter
 Y    =        -646173
04  meter          E    =           
0010585
 Z    =       -4516832
83                 I    =           51
32183
 XDOT =      -1948
215663                 Wp   =          133
36539
 YDOT =      -6714
894233  meter/sec      RA   =          232
84860  deg
 ZDOT =       3126
034161                 TA   =          168
16973
                                          MA   =          168
14484
                                          Ha   =            221
448  n
mi
                                          Hp   =            215
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16490093
85                 X    =        -4996640
72
 Y    =       -2119990
29  feet           Y    =         -702214
67  meter
 Z    =      -14819005
36                 Z    =        -4541176
73
 XDOT =      -6391
783670                 XDOT =       -1888
167855
 YDOT =     -22030
492890  feet/sec       YDOT =       -6736
344400  meter/sec
 ZDOT =      10256
017587                 ZDOT =        3116
716971

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16249588
09                 X    =         4952874
45
 Y    =        3020183
67  feet           Y    =          920551
98  meter
 Z    =      -14928156
34                 Z    =        -4550102
05
 XDOT =       5457
525871                 XDOT =        1663
453886
 YDOT =      21167
029083  feet/sec       YDOT =        6451
710464  meter/sec
 ZDOT =      10214
878206                 ZDOT =        3113
494877


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   18269
48968136  
00016717  00000-0  10270-3 0  9143
2 25544  51
6375 233
8792 0004103 201
5484 158
5496 15
53866619 14266


Satellite: ISS
Catalog Number: 25544
Epoch time:      18269
48968136   =   yrday
fracday
Element set:     914
Inclination:       51
6375  deg
RA of node:       233
8792  deg
Eccentricity:     
0004103     
Arg of perigee:   201
5484  deg
Mean anomaly:     158
5496  deg
Mean motion:   15
53866619  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1426
Checksum:              343


Coasting Arc #16 (Orbit 1441)
---------------------------------------

Vector Time (GMT): 2018/270/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5495627
34                 A    =         6784853
32  meter
 Y    =        1958136
64  meter          E    =           
0010953
 Z    =        3451349
19                 I    =           51
35442
 XDOT =        667
156556                 Wp   =          108
06516
 YDOT =       6147
270498  meter/sec      RA   =          227
84245  deg
 ZDOT =      -4541
446549                 TA   =           31
24868
                                          MA   =           31
18361
                                          Ha   =            221
143  n
mi
                                          Hp   =            215
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18030273
42                 X    =         5456557
37
 Y    =        6424332
80  feet           Y    =         2019374
49  meter
 Z    =       11323324
12                 Z    =         3477950
33
 XDOT =       2188
833845                 XDOT =         620
426773
 YDOT =      20168
210296  feet/sec       YDOT =        6154
469319  meter/sec
 ZDOT =     -14899
759019                 ZDOT =       -4538
319869

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17698417
21                 X    =        -5394477
57
 Y    =       -7100428
98  feet           Y    =        -2164210
75  meter
 Z    =       11442482
99                 Z    =         3487668
82
 XDOT =      -2040
310766                 XDOT =        -621
886722
 YDOT =     -18948
720522  feet/sec       YDOT =       -5775
570015  meter/sec
 ZDOT =     -14886
327439                 ZDOT =       -4537
352604


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   18270
51867306  
00016717  00000-0  10270-3 0  9157
2 25544  51
6372 228
7515 0004061 206
6457 153
4488 15
53892791 14421


Satellite: ISS
Catalog Number: 25544
Epoch time:      18270
51867306   =   yrday
fracday
Element set:     915
Inclination:       51
6372  deg
RA of node:       228
7515  deg
Eccentricity:     
0004061     
Arg of perigee:   206
6457  deg
Mean anomaly:     153
4488  deg
Mean motion:   15
53892791  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1442
Checksum:              322


Coasting Arc #17 (Orbit 1443)
---------------------------------------

Vector Time (GMT): 2018/270/15:15:18
297
Vector Time (MET): N/A
Weight (LBS)     : 943647
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4773114
00                 A    =         6780615
80  meter
 Y    =         505631
01  meter          E    =           
0010966
 Z    =       -4799615
58                 I    =           51
34528
 XDOT =      -3238
544059                 Wp   =          129
22074
 YDOT =      -6460
257775  meter/sec      RA   =          227
06596  deg
 ZDOT =       2537
187614                 TA   =          165
89464
                                          MA   =          165
86400
                                          Ha   =            221
261  n
mi
                                          Hp   =            215
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15659822
82                 X    =        -4755098
99
 Y    =        1658894
38  feet           Y    =          452354
94  meter
 Z    =      -15746770
27                 Z    =        -4822758
37
 XDOT =     -10625
144552                 XDOT =       -3178
387479
 YDOT =     -21195
071440  feet/sec       YDOT =       -6496
136790  meter/sec
 ZDOT =       8324
106345                 ZDOT =        2521
602462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7728173
13                 X    =         2355547
17
 Y    =      -13600547
43  feet           Y    =        -4145446
86  meter
 Z    =      -15850653
14                 Z    =        -4831279
08
 XDOT =      22452
950931                 XDOT =        6843
659444
 YDOT =       3126
822972  feet/sec       YDOT =         953
055642  meter/sec
 ZDOT =       8254
806958                 ZDOT =        2516
065161


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   18270
64729731  
00016717  00000-0  10270-3 0  9161
2 25544  51
6404 228
1111 0004148 216
7943 143
2925 15
53730034 14447


Satellite: ISS
Catalog Number: 25544
Epoch time:      18270
64729731   =   yrday
fracday
Element set:     916
Inclination:       51
6404  deg
RA of node:       228
1111  deg
Eccentricity:     
0004148     
Arg of perigee:   216
7943  deg
Mean anomaly:     143
2925  deg
Mean motion:   15
53730034  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1444
Checksum:              292


Coasting Arc #18 (Orbit 1450)
---------------------------------------

Vector Time (GMT): 2018/271/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943647
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -55509
72                 A    =         6781983
08  meter
 Y    =       -5106224
93  meter          E    =           
0009216
 Z    =        4462001
57                 I    =           51
35868
 XDOT =       6388
241349                 Wp   =          141
20343
 YDOT =       2755
552595  meter/sec      RA   =          225
06518  deg
 ZDOT =       3222
196850                 TA   =          276
19266
                                          MA   =          276
29764
                                          Ha   =            221
348  n
mi
                                          Hp   =            216
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -182118
49                 X    =          -20080
78
 Y    =      -16752706
46  feet           Y    =        -5106647
13  meter
 Z    =       14639112
76                 Z    =         4461818
49
 XDOT =      20958
797078                 XDOT =        6341
301210
 YDOT =       9040
526888  feet/sec       YDOT =        2826
728213  meter/sec
 ZDOT =      10571
511976                 ZDOT =        3253
114932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6402469
20                 X    =        -1951472
61
 Y    =      -15482388
54  feet           Y    =        -4719032
03  meter
 Z    =       14638783
98                 Z    =         4461901
36
 XDOT =      21619
407110                 XDOT =        6589
595287
 YDOT =       1219
195804  feet/sec       YDOT =         371
610881  meter/sec
 ZDOT =      10709
969470                 ZDOT =        3264
398694


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   18271
09752655  
00016717  00000-0  10270-3 0  9173
2 25544  51
6399 225
8637 0004721 215
1135 144
9707 15
53752954 14519


Satellite: ISS
Catalog Number: 25544
Epoch time:      18271
09752655   =   yrday
fracday
Element set:     917
Inclination:       51
6399  deg
RA of node:       225
8637  deg
Eccentricity:     
0004721     
Arg of perigee:   215
1135  deg
Mean anomaly:     144
9707  deg
Mean motion:   15
53752954  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1451
Checksum:              326


Coasting Arc #19 (Orbit 1465)
---------------------------------------

Vector Time (GMT): 2018/272/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943647
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1259375
26                 A    =         6779377
27  meter
 Y    =        4279324
22  meter          E    =           
0010291
 Z    =       -5113743
14                 I    =           51
37486
 XDOT =      -6467
972618                 Wp   =           94
46671
 YDOT =      -3788
049834  meter/sec      RA   =          220
05580  deg
 ZDOT =      -1580
601971                 TA   =          160
23932
                                          MA   =          160
19942
                                          Ha   =            221
203  n
mi
                                          Hp   =            216
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4131808
59                 X    =        -1282293
93
 Y    =       14039777
63  feet           Y    =         4265112
44  meter
 Z    =      -16777372
51                 Z    =        -5119916
88
 XDOT =     -21220
382604                 XDOT =       -6417
455006
 YDOT =     -12427
985019  feet/sec       YDOT =       -3860
096860  meter/sec
 ZDOT =      -5185
702004                 ZDOT =       -1611
898690

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1657312
22                 X    =          505148
76
 Y    =       14508495
02  feet           Y    =         4422189
28  meter
 Z    =      -16805484
66                 Z    =        -5122311
73
 XDOT =     -23270
746032                 XDOT =       -7092
923391
 YDOT =      -3497
293863  feet/sec       YDOT =       -1065
975169  meter/sec
 ZDOT =      -5325
774969                 ZDOT =       -1623
296210


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   18272
06230445  
00016717  00000-0  10270-3 0  9180
2 25544  51
6408 221
0580 0004647 219
2362 140
8454 15
53732422 14667


Satellite: ISS
Catalog Number: 25544
Epoch time:      18272
06230445   =   yrday
fracday
Element set:     918
Inclination:       51
6408  deg
RA of node:       221
0580  deg
Eccentricity:     
0004647     
Arg of perigee:   219
2362  deg
Mean anomaly:     140
8454  deg
Mean motion:   15
53732422  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1466
Checksum:              291
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