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

 
Date: September 18th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 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


263/18:05:08 491 0 1 0 8 0 9
N/A -0 8 0 1 222 0
000/00:00:16 983 0 2 -0 0 215 2

267/01:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 215 7

268/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 215 7

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

274/09:07:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 216 3

Coasting Arc #1 (Orbit 1286)
---------------------------------------

Vector Time (GMT): 2018/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4301935
67                 A    =         6778552
45  meter
 Y    =        -722051
28  meter          E    =           
0007970
 Z    =        5185765
58                 I    =           51
24343
 XDOT =       -117
151688                 Wp   =          145
96942
 YDOT =       7583
753222  meter/sec      RA   =          277
85044  deg
 ZDOT =       1145
770630                 TA   =          292
94556
                                          MA   =          293
02965
                                          Ha   =            222
248  n
mi
                                          Hp   =            214
466

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14113962
16                 X    =         4284500
37
 Y    =       -2368934
64  feet           Y    =         -674041
26  meter
 Z    =       17013666
62                 Z    =         5206620
61
 XDOT =       -384
355931                 XDOT =        -207
512170
 YDOT =      24881
080126  feet/sec       YDOT =        7581
937975  meter/sec
 ZDOT =       3759
089995                 ZDOT =        1144
981676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14143292
58                 X    =        -4310875
58
 Y    =        1260509
80  feet           Y    =          384203
39  meter
 Z    =       17107279
76                 Z    =         5214298
87
 XDOT =       2454
628456                 XDOT =         748
170753
 YDOT =     -23740
955904  feet/sec       YDOT =       -7236
243360  meter/sec
 ZDOT =       3754
641495                 ZDOT =        1144
414728


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
55021177  
00016717  00000-0  10270-3 0  9002
2 25544  51
6388 278
4263 0004600 165
1486 194
9802 15
53864325 12879


Satellite: ISS
Catalog Number: 25544
Epoch time:      18260
55021177   =   yrday
fracday
Element set:     900
Inclination:       51
6388  deg
RA of node:       278
4263  deg
Eccentricity:     
0004600     
Arg of perigee:   165
1486  deg
Mean anomaly:     194
9802  deg
Mean motion:   15
53864325  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1287
Checksum:              315


Coasting Arc #2 (Orbit 1301)
---------------------------------------

Vector Time (GMT): 2018/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4177477
93                 A    =         6778350
09  meter
 Y    =        -996995
31  meter          E    =           
0016328
 Z    =       -5257960
55                 I    =           51
23944
 XDOT =        929
975385                 Wp   =          111
06347
 YDOT =      -7568
047931  meter/sec      RA   =          272
82605  deg
 ZDOT =        692
139263                 TA   =          165
61725
                                          MA   =          165
57072
                                          Ha   =            222
261  n
mi
                                          Hp   =            214
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13705636
27                 X    =        -4140478
40
 Y    =       -3270982
00  feet           Y    =        -1043504
18  meter
 Z    =      -17250526
75                 Z    =        -5278163
35
 XDOT =       3051
100343                 XDOT =        1011
172235
 YDOT =     -24829
553580  feet/sec       YDOT =       -7557
194264  meter/sec
 ZDOT =       2270
798108                 ZDOT =         696
854381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13364110
15                 X    =         4073380
77
 Y    =        4100518
26  feet           Y    =         1249837
97  meter
 Z    =      -17341014
15                 Z    =        -5285541
11
 XDOT =      -4255
687428                 XDOT =       -1297
133528
 YDOT =      23621
612913  feet/sec       YDOT =        7199
867616  meter/sec
 ZDOT =       2292
835440                 ZDOT =         698
856242


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
51490912  
00016717  00000-0  10270-3 0  9017
2 25544  51
6392 273
6198 0004548 171
4134 188
7097 15
53844200 13024


Satellite: ISS
Catalog Number: 25544
Epoch time:      18261
51490912   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:       273
6198  deg
Eccentricity:     
0004548     
Arg of perigee:   171
4134  deg
Mean anomaly:     188
7097  deg
Mean motion:   15
53844200  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1302
Checksum:              305


Coasting Arc #3 (Orbit 1317)
---------------------------------------

Vector Time (GMT): 2018/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3969557
69                 A    =         6780086
41  meter
 Y    =        2639454
58  meter          E    =           
0006668
 Z    =        4815267
28                 I    =           51
24431
 XDOT =      -1707
060234                 Wp   =           97
47838
 YDOT =       7063
150952  meter/sec      RA   =          267
80284  deg
 ZDOT =      -2462
284748                 TA   =           16
83440
                                          MA   =           16
81229
                                          Ha   =            221
992  n
mi
                                          Hp   =            214
709

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13023483
24                 X    =         3916357
59
 Y    =        8659627
87  feet           Y    =         2683547
76  meter
 Z    =       15798120
98                 Z    =         4834420
58
 XDOT =      -5600
591320                 XDOT =       -1773
955031
 YDOT =      23173
067428  feet/sec       YDOT =        7043
687239  meter/sec
 ZDOT =      -8078
362033                 ZDOT =       -2470
739935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12522552
45                 X    =        -3816873
99
 Y    =       -9223560
31  feet           Y    =        -2811341
18  meter
 Z    =       15883718
47                 Z    =         4841357
39
 XDOT =       5893
450658                 XDOT =        1796
323761
 YDOT =     -21991
369446  feet/sec       YDOT =       -6702
969407  meter/sec
 ZDOT =      -8117
097075                 ZDOT =       -2474
091189


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
54391578  
00016717  00000-0  10270-3 0  9020
2 25544  51
6383 268
4917 0004442 173
9947 186
1260 15
53882821 13189


Satellite: ISS
Catalog Number: 25544
Epoch time:      18262
54391578   =   yrday
fracday
Element set:     902
Inclination:       51
6383  deg
RA of node:       268
4917  deg
Eccentricity:     
0004442     
Arg of perigee:   173
9947  deg
Mean anomaly:     186
1260  deg
Mean motion:   15
53882821  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1318
Checksum:              333


Coasting Arc #4 (Orbit 1332)
---------------------------------------

Vector Time (GMT): 2018/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3704357
39                 A    =         6783493
45  meter
 Y    =       -4107919
89  meter          E    =           
0009190
 Z    =       -3937399
16                 I    =           51
25689
 XDOT =       2464
839379                 Wp   =          133
22942
 YDOT =      -6051
574495  meter/sec      RA   =          262
78776  deg
 ZDOT =       3994
435022                 TA   =          178
73957
                                          MA   =          178
73725
                                          Ha   =            222
100  n
mi
                                          Hp   =            214
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12153403
51                 X    =        -3639020
44
 Y    =      -13477427
46  feet           Y    =        -4148979
55  meter
 Z    =      -12917976
23                 Z    =        -3955234
57
 XDOT =       8086
743370                 XDOT =        2512
923794
 YDOT =     -19854
247030  feet/sec       YDOT =       -6023
741806  meter/sec
 ZDOT =      13105
101777                 ZDOT =        4006
525532

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11698532
91                 X    =         3565712
83
 Y    =       13799618
90  feet           Y    =         4206123
84  meter
 Z    =      -12997508
36                 Z    =        -3961640
55
 XDOT =      -7526
864812                 XDOT =       -2294
188395
 YDOT =      18776
746764  feet/sec       YDOT =        5723
152414  meter/sec
 ZDOT =      13160
010648                 ZDOT =        4011
171245


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
50860825  
00016717  00000-0  10270-3 0  9034
2 25544  51
6375 263
6853 0004337 176
6302 183
4880 15
53851833 13338


Satellite: ISS
Catalog Number: 25544
Epoch time:      18263
50860825   =   yrday
fracday
Element set:     903
Inclination:       51
6375  deg
RA of node:       263
6853  deg
Eccentricity:     
0004337     
Arg of perigee:   176
6302  deg
Mean anomaly:     183
4880  deg
Mean motion:   15
53851833  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1333
Checksum:              316


Coasting Arc #5 (Orbit 1336)
---------------------------------------

Vector Time (GMT): 2018/263/18:05:16
983
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4272565
97                 A    =         6780223
06  meter
 Y    =       -1929449
21  meter          E    =           
0013425
 Z    =       -4910683
85                 I    =           51
24775
 XDOT =        724
315495                 Wp   =          123
55807
 YDOT =      -7289
211366  meter/sec      RA   =          261
52512  deg
 ZDOT =       2230
935413                 TA   =          168
39457
                                          MA   =          168
36360
                                          Ha   =            221
982  n
mi
                                          Hp   =            215
238

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14017604
89                 X    =        -4226819
38
 Y    =       -6330213
96  feet           Y    =        -1976972
60  meter
 Z    =      -16111167
49                 Z    =        -4931327
15
 XDOT =       2376
363172                 XDOT =         794
934985
 YDOT =     -23914
735452  feet/sec       YDOT =       -7280
716540  meter/sec
 ZDOT =       7319
341907                 ZDOT =        2234
625947

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6326068
62                 X    =         1928185
71
 Y    =      -13912609
00  feet           Y    =        -4240563
22  meter
 Z    =      -16203540
97                 Z    =        -4938839
29
 XDOT =      22900
568889                 XDOT =        6980
093397
 YDOT =       1857
204424  feet/sec       YDOT =         566
075908  meter/sec
 ZDOT =       7336
710086                 ZDOT =        2236
229234


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
76586051  
00016717  00000-0  10270-3 0  9049
2 25544  51
6396 262
4037 0004001 188
3029 171
8058 15
53714318 13374


Satellite: ISS
Catalog Number: 25544
Epoch time:      18263
76586051   =   yrday
fracday
Element set:     904
Inclination:       51
6396  deg
RA of node:       262
4037  deg
Eccentricity:     
0004001     
Arg of perigee:   188
3029  deg
Mean anomaly:     171
8058  deg
Mean motion:   15
53714318  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1337
Checksum:              307


Coasting Arc #6 (Orbit 1352)
---------------------------------------

Vector Time (GMT): 2018/264/18:05:16
983
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4197780
11                 A    =         6783290
61  meter
 Y    =        3388239
58  meter          E    =           
0009391
 Z    =        4103257
77                 I    =           51
26349
 XDOT =      -1552
516890                 Wp   =           99
02169
 YDOT =       6497
981883  meter/sec      RA   =          256
51070  deg
 ZDOT =      -3771
428992                 TA   =           30
07156
                                          MA   =           30
01767
                                          Ha   =            221
772  n
mi
                                          Hp   =            215
493

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13772244
47                 X    =         4139648
51
 Y    =       11116271
59  feet           Y    =         3434857
41  meter
 Z    =       13462131
79                 Z    =         4123507
54
 XDOT =      -5093
559351                 XDOT =       -1606
744202
 YDOT =      21318
838200  feet/sec       YDOT =        6480
317012  meter/sec
 ZDOT =     -12373
454697                 ZDOT =       -3779
102854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10874945
13                 X    =        -3314683
28
 Y    =       13875808
70  feet           Y    =         4229346
49  meter
 Z    =       13552590
35                 Z    =         4130829
54
 XDOT =     -20390
920811                 XDOT =       -6215
152663
 YDOT =      -3842
552133  feet/sec       YDOT =       -1171
209890  meter/sec
 ZDOT =     -12408
583851                 ZDOT =       -3782
136358


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
79496759  
00016717  00000-0  10270-3 0  9059
2 25544  51
6391 257
2776 0004041 192
2790 167
8264 15
53714264 13536


Satellite: ISS
Catalog Number: 25544
Epoch time:      18264
79496759   =   yrday
fracday
Element set:     905
Inclination:       51
6391  deg
RA of node:       257
2776  deg
Eccentricity:     
0004041     
Arg of perigee:   192
2790  deg
Mean anomaly:     167
8264  deg
Mean motion:   15
53714264  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1353
Checksum:              339


Coasting Arc #7 (Orbit 1367)
---------------------------------------

Vector Time (GMT): 2018/265/18:05:16
983
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4030910
21                 A    =         6786712
24  meter
 Y    =       -4598595
54  meter          E    =           
0003713
 Z    =       -2948925
97                 I    =           51
28520
 XDOT =       2422
440179                 Wp   =          125
55316
 YDOT =      -5306
598007  meter/sec      RA   =          251
50340  deg
 ZDOT =       4966
236250                 TA   =          200
62001
                                          MA   =          200
63500
                                          Ha   =            221
744  n
mi
                                          Hp   =            215
525

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13224771
03                 X    =        -3964863
56
 Y    =      -15087255
69  feet           Y    =        -4643303
00  meter
 Z    =       -9674953
96                 Z    =        -2968345
77
 XDOT =       7947
638382                 XDOT =        2457
476693
 YDOT =     -17410
098448  feet/sec       YDOT =       -5279
312161  meter/sec
 ZDOT =      16293
426016                 ZDOT =        4978
089264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14621124
88                 X    =         4456518
86
 Y    =      -13676950
33  feet           Y    =        -4168734
46  meter
 Z    =       -9761573
85                 Z    =        -2975327
71
 XDOT =      16673
692004                 XDOT =        5082
141323
 YDOT =       6162
732033  feet/sec       YDOT =        1878
400724  meter/sec
 ZDOT =      16347
158056                 ZDOT =        4982
613775


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
75975081  
00016717  00000-0  10270-3 0  9067
2 25544  51
6403 252
4700 0004022 197
2033 162
8984 15
53738412 13689


Satellite: ISS
Catalog Number: 25544
Epoch time:      18265
75975081   =   yrday
fracday
Element set:     906
Inclination:       51
6403  deg
RA of node:       252
4700  deg
Eccentricity:     
0004022     
Arg of perigee:   197
2033  deg
Mean anomaly:     162
8984  deg
Mean motion:   15
53738412  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1368
Checksum:              310


Coasting Arc #8 (Orbit 1383)
---------------------------------------

Vector Time (GMT): 2018/266/18:05:16
983
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3698955
49                 A    =         6789589
64  meter
 Y    =        5479164
45  meter          E    =           
0015056
 Z    =        1508267
12                 I    =           51
30533
 XDOT =      -3341
578448                 Wp   =          133
40353
 YDOT =       3842
647001  meter/sec      RA   =          246
50676  deg
 ZDOT =      -5738
365716                 TA   =           30
03801
                                          MA   =           29
95174
                                          Ha   =            221
711  n
mi
                                          Hp   =            215
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12135680
73                 X    =         3630084
66
 Y    =       17976261
31  feet           Y    =         5520143
84  meter
 Z    =        4948382
93                 Z    =         1526067
42
 XDOT =     -10963
183884                 XDOT =       -3356
425674
 YDOT =      12607
109582  feet/sec       YDOT =        3805
195440  meter/sec
 ZDOT =     -18826
659174                 ZDOT =       -5754
634475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17323421
59                 X    =        -5280178
90
 Y    =       13020326
04  feet           Y    =         3968595
38  meter
 Z    =        5027662
02                 Z    =         1532431
38
 XDOT =     -12202
451605                 XDOT =       -3719
307249
 YDOT =      -8904
826453  feet/sec       YDOT =       -2714
191103  meter/sec
 ZDOT =     -18900
035728                 ZDOT =       -5760
730890


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
78885204  
00016717  00000-0  10270-3 0  9079
2 25544  51
6398 247
3434 0004051 199
0968 161
0033 15
53698030 13843


Satellite: ISS
Catalog Number: 25544
Epoch time:      18266
78885204   =   yrday
fracday
Element set:     907
Inclination:       51
6398  deg
RA of node:       247
3434  deg
Eccentricity:     
0004051     
Arg of perigee:   199
0968  deg
Mean anomaly:     161
0033  deg
Mean motion:   15
53698030  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1384
Checksum:              326


Coasting Arc #9 (Orbit 1388)
---------------------------------------

Vector Time (GMT): 2018/267/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3935183
83                 A    =         6778570
43  meter
 Y    =       -1589588
29  meter          E    =           
0003920
 Z    =        5284499
27                 I    =           51
27051
 XDOT =       3097
431714                 Wp   =          164
77429
 YDOT =       7013
008079  meter/sec      RA   =          244
96735  deg
 ZDOT =       -200
707738                 TA   =          287
12673
                                          MA   =          287
16966
                                          Ha   =            221
687  n
mi
                                          Hp   =            215
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12910708
11                 X    =         3926997
23
 Y    =       -5215184
68  feet           Y    =        -1545627
45  meter
 Z    =       17337596
04                 Z    =         5303595
37
 XDOT =      10162
177538                 XDOT =        3019
755035
 YDOT =      23008
556689  feet/sec       YDOT =        7047
211368  meter/sec
 ZDOT =       -658
489954                 ZDOT =        -185
851004

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9487514
55                 X    =         2891794
43
 Y    =      -10044312
95  feet           Y    =        -3061506
59  meter
 Z    =       17423421
50                 Z    =         5310658
87
 XDOT =      18049
013578                 XDOT =        5501
339339
 YDOT =      16041
446670  feet/sec       YDOT =        4889
432945  meter/sec
 ZDOT =       -592
568204                 ZDOT =        -180
614789


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
11044558  
00016717  00000-0  10270-3 0  9087
2 25544  51
6375 245
7354 0004365 198
6947 161
4046 15
53712062 13896


Satellite: ISS
Catalog Number: 25544
Epoch time:      18267
11044558   =   yrday
fracday
Element set:     908
Inclination:       51
6375  deg
RA of node:       245
7354  deg
Eccentricity:     
0004365     
Arg of perigee:   198
6947  deg
Mean anomaly:     161
4046  deg
Mean motion:   15
53712062  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1389
Checksum:              327


Coasting Arc #10 (Orbit 1403)
---------------------------------------

Vector Time (GMT): 2018/268/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4586156
39                 A    =         6779739
08  meter
 Y    =          81404
01  meter          E    =           
0013033
 Z    =       -5004098
41                 I    =           51
29040
 XDOT =      -2265
244883                 Wp   =          124
50100
 YDOT =      -7048
476446  meter/sec      RA   =          239
94810  deg
 ZDOT =       1957
800851                 TA   =          164
64343
                                          MA   =          164
60384
                                          Ha   =            221
661  n
mi
                                          Hp   =            215
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15046444
87                 X    =        -4562418
42
 Y    =         267073
53  feet           Y    =           30250
51  meter
 Z    =      -16417645
70                 Z    =        -5026318
84
 XDOT =      -7431
905784                 XDOT =       -2195
768520
 YDOT =     -23124
922724  feet/sec       YDOT =       -7073
419268  meter/sec
 ZDOT =       6423
231140                 ZDOT =        1946
966674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13373466
31                 X    =        -4076232
53
 Y    =        6658375
82  feet           Y    =         2029472
95  meter
 Z    =      -16517334
89                 Z    =        -5034483
67
 XDOT =     -16200
091480                 XDOT =       -4937
787883
 YDOT =     -16693
918041  feet/sec       YDOT =       -5088
306219  meter/sec
 ZDOT =       6375
339923                 ZDOT =        1943
203608


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
07522354  
00016717  00000-0  10270-3 0  9099
2 25544  51
6382 240
9294 0004460 202
7537 157
3419 15
53741230 14047


Satellite: ISS
Catalog Number: 25544
Epoch time:      18268
07522354   =   yrday
fracday
Element set:     909
Inclination:       51
6382  deg
RA of node:       240
9294  deg
Eccentricity:     
0004460     
Arg of perigee:   202
7537  deg
Mean anomaly:     157
3419  deg
Mean motion:   15
53741230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1404
Checksum:              300


Coasting Arc #11 (Orbit 1409)
---------------------------------------

Vector Time (GMT): 2018/268/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4424905
93                 A    =         6789551
19  meter
 Y    =       -4952138
78  meter          E    =           
0004672
 Z    =       -1405966
31                 I    =           51
32824
 XDOT =       2838
345480                 Wp   =           50
23809
 YDOT =      -4169
729596  meter/sec      RA   =          237
97334  deg
 ZDOT =       5769
555286                 TA   =          294
37804
                                          MA   =          294
42680
                                          Ha   =            221
575  n
mi
                                          Hp   =            215
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14517407
90                 X    =        -4362371
37
 Y    =      -16247174
46  feet           Y    =        -5001271
67  meter
 Z    =       -4612750
37                 Z    =        -1427308
60
 XDOT =       9312
157086                 XDOT =        2856
735942
 YDOT =     -13680
215209  feet/sec       YDOT =       -4137
885677  meter/sec
 ZDOT =      18928
987159                 ZDOT =        5783
388284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10903181
09                 X    =         3323289
60
 Y    =       18840346
95  feet           Y    =         5742537
75  meter
 Z    =       -4707997
98                 Z    =        -1434997
78
 XDOT =     -10387
607557                 XDOT =       -3166
142783
 YDOT =      10744
573442  feet/sec       YDOT =        3274
945985  meter/sec
 ZDOT =      18991
460435                 ZDOT =        5788
597141


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
46113360  
00016717  00000-0  10270-3 0  9107
2 25544  51
6365 239
0106 0004045 203
2983 156
7987 15
53750191 14105


Satellite: ISS
Catalog Number: 25544
Epoch time:      18268
46113360   =   yrday
fracday
Element set:     910
Inclination:       51
6365  deg
RA of node:       239
0106  deg
Eccentricity:     
0004045     
Arg of perigee:   203
2983  deg
Mean anomaly:     156
7987  deg
Mean motion:   15
53750191  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1410
Checksum:              296


Coasting Arc #12 (Orbit 1425)
---------------------------------------

Vector Time (GMT): 2018/269/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3966073
82                 A    =         6790438
89  meter
 Y    =        5499177
67  meter          E    =           
0013375
 Z    =        -180109
51                 I    =           51
35053
 XDOT =      -3976
953808                 Wp   =          152
06484
 YDOT =       2678
431742  meter/sec      RA   =          232
98315  deg
 ZDOT =      -5987
192596                 TA   =           29
88370
                                          MA   =           29
80740
                                          Ha   =            221
387  n
mi
                                          Hp   =            215
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13012053
22                 X    =         3905160
61
 Y    =       18041921
47  feet           Y    =         5543188
45  meter
 Z    =        -590910
48                 Z    =         -160992
11
 XDOT =     -13047
748713                 XDOT =       -3977
526241
 YDOT =       8787
505716  feet/sec       YDOT =        2633
954746  meter/sec
 ZDOT =     -19643
020328                 ZDOT =       -6006
513196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9447954
96                 X    =        -2879736
67
 Y    =      -20140855
60  feet           Y    =        -6138932
79  meter
 Z    =        -505684
96                 Z    =         -154132
78
 XDOT =      12852
285203                 XDOT =        3917
376530
 YDOT =      -5552
069028  feet/sec       YDOT =       -1692
270640  meter/sec
 ZDOT =     -19729
962093                 ZDOT =       -6013
692446


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
49022624  
00016717  00000-0  10270-3 0  9114
2 25544  51
6375 233
8824 0003835 209
8868 150
2065 15
53744223 14267


Satellite: ISS
Catalog Number: 25544
Epoch time:      18269
49022624   =   yrday
fracday
Element set:     911
Inclination:       51
6375  deg
RA of node:       233
8824  deg
Eccentricity:     
0003835     
Arg of perigee:   209
8868  deg
Mean anomaly:     150
2065  deg
Mean motion:   15
53744223  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1426
Checksum:              315


Coasting Arc #13 (Orbit 1441)
---------------------------------------

Vector Time (GMT): 2018/270/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3269182
25                 A    =         6789097
82  meter
 Y    =       -5690044
24  meter          E    =           
0010640
 Z    =        1724662
75                 I    =           51
36671
 XDOT =       5036
066879                 Wp   =           76
16188
 YDOT =      -1169
319622  meter/sec      RA   =          227
99540  deg
 ZDOT =       5661
312473                 TA   =          302
82733
                                          MA   =          302
92974
                                          Ha   =            221
277  n
mi
                                          Hp   =            215
971

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10725663
55                 X    =        -3213689
25
 Y    =      -18668124
16  feet           Y    =        -5726292
04  meter
 Z    =        5658342
36                 Z    =         1708917
38
 XDOT =      16522
529129                 XDOT =        5021
268156
 YDOT =      -3836
350467  feet/sec       YDOT =       -1113
084941  meter/sec
 ZDOT =      18573
859820                 ZDOT =        5685
740490

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7467154
26                 X    =         2275988
62
 Y    =       20213080
11  feet           Y    =         6160946
82  meter
 Z    =        5588251
62                 Z    =         1703299
09
 XDOT =     -15336
265714                 XDOT =       -4674
493790
 YDOT =        475
404849  feet/sec       YDOT =         144
903398  meter/sec
 ZDOT =      18683
572040                 ZDOT =        5694
752758


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
51931450  
00016717  00000-0  10270-3 0  9126
2 25544  51
6371 228
7561 0004099 213
5233 146
5661 15
53785930 14423


Satellite: ISS
Catalog Number: 25544
Epoch time:      18270
51931450   =   yrday
fracday
Element set:     912
Inclination:       51
6371  deg
RA of node:       228
7561  deg
Eccentricity:     
0004099     
Arg of perigee:   213
5233  deg
Mean anomaly:     146
5661  deg
Mean motion:   15
53785930  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1442
Checksum:              303


Coasting Arc #14 (Orbit 1450)
---------------------------------------

Vector Time (GMT): 2018/271/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -414235
56                 A    =         6782643
79  meter
 Y    =       -5250721
27  meter          E    =           
0009579
 Z    =        4271576
57                 I    =           51
36087
 XDOT =       6371
397604                 Wp   =          133
19269
 YDOT =       2384
062486  meter/sec      RA   =          225
07402  deg
 ZDOT =       3536
949284                 TA   =          280
55513
                                          MA   =          280
66303
                                          Ha   =            221
308  n
mi
                                          Hp   =            216
051

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1359040
54                 X    =         -376239
16
 Y    =      -17226775
80  feet           Y    =        -5255140
65  meter
 Z    =       14014358
82                 Z    =         4269657
15
 XDOT =      20903
535446                 XDOT =        6327
083895
 YDOT =       7821
727315  feet/sec       YDOT =        2455
064462  meter/sec
 ZDOT =      11604
164316                 ZDOT =        3567
791960

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7667375
20                 X    =        -2337015
96
 Y    =      -15493459
05  feet           Y    =        -4722406
32  meter
 Z    =       14006253
35                 Z    =         4269106
02
 XDOT =      21113
919299                 XDOT =        6435
522602
 YDOT =        200
376827  feet/sec       YDOT =          61
074857  meter/sec
 ZDOT =      11742
319294                 ZDOT =        3579
058921


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
09817780  
00016717  00000-0  10270-3 0  9130
2 25544  51
6398 225
8682 0004420 214
4489 145
6377 15
53771206 14510


Satellite: ISS
Catalog Number: 25544
Epoch time:      18271
09817780   =   yrday
fracday
Element set:     913
Inclination:       51
6398  deg
RA of node:       225
8682  deg
Eccentricity:     
0004420     
Arg of perigee:   214
4489  deg
Mean anomaly:     145
6377  deg
Mean motion:   15
53771206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1451
Checksum:              324


Coasting Arc #15 (Orbit 1465)
---------------------------------------

Vector Time (GMT): 2018/272/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -899014
52                 A    =         6779767
09  meter
 Y    =        4480830
78  meter          E    =           
0009704
 Z    =       -5016268
72                 I    =           51
37607
 XDOT =      -6543
668731                 Wp   =           91
25621
 YDOT =      -3479
515498  meter/sec      RA   =          220
06594  deg
 ZDOT =      -1938
821761                 TA   =          159
86105
                                          MA   =          159
82274
                                          Ha   =            221
180  n
mi
                                          Hp   =            216
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2949522
70                 X    =         -924686
77
 Y    =       14700888
38  feet           Y    =         4470633
42  meter
 Z    =      -16457574
55                 Z    =        -5020698
63
 XDOT =     -21468
729434                 XDOT =       -6494
855536
 YDOT =     -11415
733260  feet/sec       YDOT =       -3552
418570  meter/sec
 ZDOT =      -6360
963782                 ZDOT =       -1970
490357

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3000609
22                 X    =          914585
69
 Y    =       14667765
50  feet           Y    =         4470734
93  meter
 Z    =      -16477881
01                 Z    =        -5022458
13
 XDOT =     -23094
071690                 XDOT =       -7039
073051
 YDOT =      -2568
072668  feet/sec       YDOT =        -782
748549  meter/sec
 ZDOT =      -6502
734914                 ZDOT =       -1982
033602


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
06294604  
00016717  00000-0  10270-3 0  9143
2 25544  51
6406 221
0624 0004356 218
5774 141
5068 15
53745433 14665


Satellite: ISS
Catalog Number: 25544
Epoch time:      18272
06294604   =   yrday
fracday
Element set:     914
Inclination:       51
6406  deg
RA of node:       221
0624  deg
Eccentricity:     
0004356     
Arg of perigee:   218
5774  deg
Mean anomaly:     141
5068  deg
Mean motion:   15
53745433  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1466
Checksum:              302


Coasting Arc #16 (Orbit 1481)
---------------------------------------

Vector Time (GMT): 2018/273/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2261158
46                 A    =         6778342
14  meter
 Y    =       -3577644
34  meter          E    =           
0003599
 Z    =        5295174
74                 I    =           51
39794
 XDOT =       6356
013245                 Wp   =          187
57186
 YDOT =       4285
747281  meter/sec      RA   =          215
05317  deg
 ZDOT =        177
985196                 TA   =          260
70579
                                          MA   =          260
74649
                                          Ha   =            220
946  n
mi
                                          Hp   =            216
211

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7418498
90                 X    =         2275275
01
 Y    =      -11737678
27  feet           Y    =        -3552279
24  meter
 Z    =       17372620
54                 Z    =         5306193
36
 XDOT =      20853
061829                 XDOT =        6306
751861
 YDOT =      14060
850658  feet/sec       YDOT =        4356
549204  meter/sec
 ZDOT =        583
940933                 ZDOT =         208
741126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2021490
16                 X    =          616150
20
 Y    =      -13674370
74  feet           Y    =        -4167948
20  meter
 Z    =       17422408
67                 Z    =         5310350
16
 XDOT =      23727
725503                 XDOT =        7232
210733
 YDOT =       4441
548928  feet/sec       YDOT =        1353
784113  meter/sec
 ZDOT =        721
558221                 ZDOT =         219
930946


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   18273
09202570  
00016717  00000-0  10270-3 0  9159
2 25544  51
6407 215
9350 0004256 222
9331 137
1490 15
53792622 14821


Satellite: ISS
Catalog Number: 25544
Epoch time:      18273
09202570   =   yrday
fracday
Element set:     915
Inclination:       51
6407  deg
RA of node:       215
9350  deg
Eccentricity:     
0004256     
Arg of perigee:   222
9331  deg
Mean anomaly:     137
1490  deg
Mean motion:   15
53792622  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1482
Checksum:              294


Coasting Arc #17 (Orbit 1496)
---------------------------------------

Vector Time (GMT): 2018/274/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3620813
08                 A    =         6779176
31  meter
 Y    =        2614136
88  meter          E    =           
0011813
 Z    =       -5110644
23                 I    =           51
42795
 XDOT =      -5743
861367                 Wp   =          119
49669
 YDOT =      -4804
379978  meter/sec      RA   =          210
04323  deg
 ZDOT =       1609
069290                 TA   =          166
10706
                                          MA   =          166
07453
                                          Ha   =            220
928  n
mi
                                          Hp   =            216
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11879307
99                 X    =        -3624950
79
 Y    =        8576564
56  feet           Y    =         2573623
07  meter
 Z    =      -16767205
48                 Z    =        -5128243
31
 XDOT =     -18844
689524                 XDOT =       -5697
526684
 YDOT =     -15762
401501  feet/sec       YDOT =       -4868
352675  meter/sec
 ZDOT =       5279
098719                 ZDOT =        1581
279947

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7159005
42                 X    =        -2182064
85
 Y    =       12679141
72  feet           Y    =         3864602
40  meter
 Z    =      -16846441
89                 Z    =        -5134795
49
 XDOT =     -22787
667390                 XDOT =       -6945
681020
 YDOT =      -6004
957366  feet/sec       YDOT =       -1830
311005  meter/sec
 ZDOT =       5154
824130                 ZDOT =        1571
190395


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   18274
05678714  
00016717  00000-0  10270-3 0  9164
2 25544  51
6402 211
1298 0004179 225
3568 134
7244 15
53784767 14975


Satellite: ISS
Catalog Number: 25544
Epoch time:      18274
05678714   =   yrday
fracday
Element set:     916
Inclination:       51
6402  deg
RA of node:       211
1298  deg
Eccentricity:     
0004179     
Arg of perigee:   225
3568  deg
Mean anomaly:     134
7244  deg
Mean motion:   15
53784767  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1497
Checksum:              333


Coasting Arc #18 (Orbit 1502)
---------------------------------------

Vector Time (GMT): 2018/274/09:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5492662
83                 A    =         6789873
23  meter
 Y    =       -3860377
05  meter          E    =           
0009538
 Z    =         985814
89                 I    =           51
46972
 XDOT =       3488
029840                 Wp   =           58
86446
 YDOT =      -3448
563566  meter/sec      RA   =          208
38563  deg
 ZDOT =       5892
455436                 TA   =          311
83840
                                          MA   =          311
91979
                                          Ha   =            220
838  n
mi
                                          Hp   =            216
257

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18020547
35                 X    =        -5453875
43
 Y    =      -12665279
04  feet           Y    =        -3921582
90  meter
 Z    =        3234300
82                 Z    =          959227
45
 XDOT =      11443
667454                 XDOT =        3497
710568
 YDOT =     -11314
184928  feet/sec       YDOT =       -3409
503631  meter/sec
 ZDOT =      19332
202875                 ZDOT =        5909
422956

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7892890
60                 X    =         2405753
06
 Y    =       20581718
80  feet           Y    =         6273307
89  meter
 Z    =        3115325
18                 Z    =          949551
11
 XDOT =     -14202
978956                 XDOT =       -4329
067986
 YDOT =       2489
612734  feet/sec       YDOT =         758
833961  meter/sec
 ZDOT =      19408
685816                 ZDOT =        5915
767437


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   18274
44268873  
00016717  00000-0  10270-3 0  9179
2 25544  51
6365 209
2096 0004011 227
8824 132
1988 15
53810278 15036


Satellite: ISS
Catalog Number: 25544
Epoch time:      18274
44268873   =   yrday
fracday
Element set:     917
Inclination:       51
6365  deg
RA of node:       209
2096  deg
Eccentricity:     
0004011     
Arg of perigee:   227
8824  deg
Mean anomaly:     132
1988  deg
Mean motion:   15
53810278  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1503
Checksum:              319


Coasting Arc #19 (Orbit 1517)
---------------------------------------

Vector Time (GMT): 2018/275/09:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4700432
54                 A    =         6787779
88  meter
 Y    =        4204013
17  meter          E    =           
0005834
 Z    =       -2502629
42                 I    =           51
49278
 XDOT =      -4986
860580                 Wp   =          171
24961
 YDOT =       2429
715147  meter/sec      RA   =          203
40277  deg
 ZDOT =      -5292
053703                 TA   =           36
87428
                                          MA   =           36
83417
                                          Ha   =            220
767  n
mi
                                          Hp   =            216
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15421366
59                 X    =         4665229
31
 Y    =       13792694
11  feet           Y    =         4256379
74  meter
 Z    =       -8210726
46                 Z    =        -2479881
79
 XDOT =     -16361
091141                 XDOT =       -4987
953448
 YDOT =       7971
506387  feet/sec       YDOT =        2373
942314  meter/sec
 ZDOT =     -17362
380914                 ZDOT =       -5316
281108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5479584
72                 X    =        -1670177
42
 Y    =      -19992280
17  feet           Y    =        -6093647
00  meter
 Z    =       -8108999
46                 Z    =        -2471623
04
 XDOT =      16508
813767                 XDOT =        5031
886436
 YDOT =       2551
882286  feet/sec       YDOT =         777
813721  meter/sec
 ZDOT =     -17471
368107                 ZDOT =       -5325
272999


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   18275
40744614  
00016717  00000-0  10270-3 0  9189
2 25544  51
6373 204
4021 0003802 234
8901 125
1895 15
53770074 15185


Satellite: ISS
Catalog Number: 25544
Epoch time:      18275
40744614   =   yrday
fracday
Element set:     918
Inclination:       51
6373  deg
RA of node:       204
4021  deg
Eccentricity:     
0003802     
Arg of perigee:   234
8901  deg
Mean anomaly:     125
1895  deg
Mean motion:   15
53770074  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1518
Checksum:              298
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