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

 
Date: December 18th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


354/01:40:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 214 1

358/04:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 214 6

361/02:52:50 495 -1 8 2 2 2 2
N/A 1 1 -0 0 221 4
000/00:05:40 991 0 6 -0 0 216 2

361/09:08:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 216 2

364/12:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 216 7

Coasting Arc #1 (Orbit 2693)
---------------------------------------

Vector Time (GMT): 2018/351/00:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6402949
33                 A    =         6787642
74  meter
 Y    =        -895374
64  meter          E    =           
0017980
 Z    =        2034308
32                 I    =           51
60338
 XDOT =       2431
049173                 Wp   =          121
59194
 YDOT =       4705
618394  meter/sec      RA   =          186
47917  deg
 ZDOT =      -5553
654440                 TA   =           35
89028
                                          MA   =           35
76962
                                          Ha   =            222
332  n
mi
                                          Hp   =            213
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21007051
60                 X    =         6402604
13
 Y    =       -2937580
84  feet           Y    =         -823774
45  meter
 Z    =        6674239
89                 Z    =         2065410
88
 XDOT =       7975
883115                 XDOT =        2405
225800
 YDOT =      15438
380559  feet/sec       YDOT =        4732
660004  meter/sec
 ZDOT =     -18220
651051                 ZDOT =       -5541
907644

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -985358
70                 X    =         -300337
33
 Y    =      -21143889
61  feet           Y    =        -6444657
55  meter
 Z    =        6814402
16                 Z    =         2077029
78
 XDOT =      14578
040202                 XDOT =        4443
386653
 YDOT =      -6562
622478  feet/sec       YDOT =       -2000
287331  meter/sec
 ZDOT =     -18168
206441                 ZDOT =       -5537
669323


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   18351
03630475  
00016717  00000-0  10270-3 0  9003
2 25544  51
6379 187
5003 0004979 151
7704 208
3720 15
54080793 26946


Satellite: ISS
Catalog Number: 25544
Epoch time:      18351
03630475   =   yrday
fracday
Element set:     900
Inclination:       51
6379  deg
RA of node:       187
5003  deg
Eccentricity:     
0004979     
Arg of perigee:   151
7704  deg
Mean anomaly:     208
3720  deg
Mean motion:   15
54080793  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2694
Checksum:              313


Coasting Arc #2 (Orbit 2708)
---------------------------------------

Vector Time (GMT): 2018/352/00:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6773770
26                 A    =         6789289
54  meter
 Y    =         141728
75  meter          E    =           
0010116
 Z    =        -404141
78                 I    =           51
64320
 XDOT =       -449
660197                 Wp   =           68
82380
 YDOT =      -4756
349050  meter/sec      RA   =          181
50699  deg
 ZDOT =       5993
301164                 TA   =          286
82136
                                          MA   =          286
93230
                                          Ha   =            222
242  n
mi
                                          Hp   =            213
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22223655
72                 X    =        -6772888
55
 Y    =         464989
34  feet           Y    =           65984
70  meter
 Z    =       -1325924
48                 Z    =         -437044
50
 XDOT =      -1475
263113                 XDOT =        -425
552460
 YDOT =     -15604
819717  feet/sec       YDOT =       -4761
243067  meter/sec
 ZDOT =      19663
061563                 ZDOT =        5991
175092

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1210622
09                 X    =         -368997
61
 Y    =       22186177
51  feet           Y    =         6762346
91  meter
 Z    =       -1474139
01                 Z    =         -449317
57
 XDOT =     -14062
200603                 XDOT =       -4286
158744
 YDOT =        514
129685  feet/sec       YDOT =         156
706728  meter/sec
 ZDOT =      19653
949167                 ZDOT =        5990
523706


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   18352
00086897  
00016717  00000-0  10270-3 0  9015
2 25544  51
6388 182
6927 0004966 156
8462 203
2916 15
54110660 27095


Satellite: ISS
Catalog Number: 25544
Epoch time:      18352
00086897   =   yrday
fracday
Element set:     901
Inclination:       51
6388  deg
RA of node:       182
6927  deg
Eccentricity:     
0004966     
Arg of perigee:   156
8462  deg
Mean anomaly:     203
2916  deg
Mean motion:   15
54110660  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2709
Checksum:              324


Coasting Arc #3 (Orbit 2724)
---------------------------------------

Vector Time (GMT): 2018/353/00:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6623788
91                 A    =         6788825
44  meter
 Y    =         637638
28  meter          E    =           
0013717
 Z    =       -1311067
00                 I    =           51
67269
 XDOT =      -1600
782827                 Wp   =          148
40035
 YDOT =       4716
229205  meter/sec      RA   =          176
53825  deg
 ZDOT =      -5832
777225                 TA   =           45
86499
                                          MA   =           45
75226
                                          Ha   =            222
314  n
mi
                                          Hp   =            213
951

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21731590
92                 X    =         6622534
90
 Y    =        2091989
09  feet           Y    =          711703
19  meter
 Z    =       -4301400
91                 Z    =        -1278893
62
 XDOT =      -5251
912161                 XDOT =       -1625
069233
 YDOT =      15473
192930  feet/sec       YDOT =        4698
192840  meter/sec
 ZDOT =     -19136
408220                 ZDOT =       -5840
611934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3354581
72                 X    =         1022476
51
 Y    =      -21601170
44  feet           Y    =        -6584036
75  meter
 Z    =       -4156528
50                 Z    =        -1266909
89
 XDOT =      13572
118947                 XDOT =        4136
781855
 YDOT =       5771
341025  feet/sec       YDOT =        1759
104744  meter/sec
 ZDOT =     -19172
164225                 ZDOT =       -5843
675656


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   18353
02973733  
00016717  00000-0  10270-3 0  9023
2 25544  51
6372 177
5636 0004861 158
6104 201
5252 15
54067346 27259


Satellite: ISS
Catalog Number: 25544
Epoch time:      18353
02973733   =   yrday
fracday
Element set:     902
Inclination:       51
6372  deg
RA of node:       177
5636  deg
Eccentricity:     
0004861     
Arg of perigee:   158
6104  deg
Mean anomaly:     201
5252  deg
Mean motion:   15
54067346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2725
Checksum:              306


Coasting Arc #4 (Orbit 2740)
---------------------------------------

Vector Time (GMT): 2018/354/00:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5995706
98                 A    =         6786094
97  meter
 Y    =       -1387321
92  meter          E    =           
0014630
 Z    =        2850496
54                 I    =           51
69540
 XDOT =       3483
218215                 Wp   =           99
48074
 YDOT =      -4570
773338  meter/sec      RA   =          171
56751  deg
 ZDOT =       5077
421546                 TA   =          292
90302
                                          MA   =          293
05738
                                          Ha   =            222
129  n
mi
                                          Hp   =            214
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19670954
65                 X    =        -5993594
28
 Y    =       -4551581
10  feet           Y    =        -1454358
58  meter
 Z    =        9352022
77                 Z    =         2821376
17
 XDOT =      11427
881283                 XDOT =        3509
407332
 YDOT =     -14995
975520  feet/sec       YDOT =       -4531
675688  meter/sec
 ZDOT =      16658
207172                 ZDOT =        5094
405091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5356514
31                 X    =        -1632665
56
 Y    =       19529601
80  feet           Y    =         5952622
63  meter
 Z    =        9220959
02                 Z    =         2810548
31
 XDOT =     -13093
771330                 XDOT =       -3990
981501
 YDOT =     -11531
487697  feet/sec       YDOT =       -3514
797450  meter/sec
 ZDOT =      16735
177569                 ZDOT =        5100
882123


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   18354
05860460  
00016717  00000-0  10270-3 0  9030
2 25544  51
6357 172
4354 0004768 164
9787 195
1508 15
54090457 27415


Satellite: ISS
Catalog Number: 25544
Epoch time:      18354
05860460   =   yrday
fracday
Element set:     903
Inclination:       51
6357  deg
RA of node:       172
4354  deg
Eccentricity:     
0004768     
Arg of perigee:   164
9787  deg
Mean anomaly:     195
1508  deg
Mean motion:   15
54090457  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2741
Checksum:              329


Coasting Arc #5 (Orbit 2741)
---------------------------------------

Vector Time (GMT): 2018/354/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3600125
85                 A    =         6779982
15  meter
 Y    =       -3237150
47  meter          E    =           
0011444
 Z    =        4742979
15                 I    =           51
67692
 XDOT =       6437
810744                 Wp   =          135
33210
 YDOT =      -3165
402514  meter/sec      RA   =          171
21740  deg
 ZDOT =       2714
204614                 TA   =          287
79421
                                          MA   =          287
91905
                                          Ha   =            222
115  n
mi
                                          Hp   =            214
147

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11811436
53                 X    =        -3586698
67
 Y    =      -10620572
41  feet           Y    =        -3277335
03  meter
 Z    =       15560955
20                 Z    =         4725523
07
 XDOT =      21121
426325                 XDOT =        6459
544390
 YDOT =     -10385
178853  feet/sec       YDOT =       -3093
289217  meter/sec
 ZDOT =       8904
870781                 ZDOT =        2745
530008

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5161126
95                 X    =        -1573111
49
 Y    =       15103011
50  feet           Y    =         4603397
90  meter
 Z    =       15482626
73                 Z    =         4719104
63
 XDOT =     -16644
944525                 XDOT =       -5073
379091
 YDOT =     -15002
109155  feet/sec       YDOT =       -4572
642871  meter/sec
 ZDOT =       9046
320809                 ZDOT =        2757
318583


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   18354
12290960  
00016717  00000-0  10270-3 0  9041
2 25544  51
6353 172
1147 0004648 165
9021 194
2262 15
54092607 27424


Satellite: ISS
Catalog Number: 25544
Epoch time:      18354
12290960   =   yrday
fracday
Element set:     904
Inclination:       51
6353  deg
RA of node:       172
1147  deg
Eccentricity:     
0004648     
Arg of perigee:   165
9021  deg
Mean anomaly:     194
2262  deg
Mean motion:   15
54092607  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2742
Checksum:              299


Coasting Arc #6 (Orbit 2756)
---------------------------------------

Vector Time (GMT): 2018/355/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1945777
04                 A    =         6777821
21  meter
 Y    =        3808544
46  meter          E    =           
0015542
 Z    =       -5270953
25                 I    =           51
70272
 XDOT =      -7194
056473                 Wp   =          100
60650
 YDOT =       2473
874723  meter/sec      RA   =          166
22326  deg
 ZDOT =       -873
165804                 TA   =          161
06810
                                          MA   =          161
01025
                                          Ha   =            222
021  n
mi
                                          Hp   =            214
293

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6383782
95                 X    =         1928647
92
 Y    =       12495224
61  feet           Y    =         3830208
42  meter
 Z    =      -17293153
72                 Z    =        -5261542
37
 XDOT =     -23602
547484                 XDOT =       -7216
943945
 YDOT =       8116
386886  feet/sec       YDOT =        2393
297927  meter/sec
 ZDOT =      -2864
717204                 ZDOT =        -908
167564

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8803352
76                 X    =         2683261
92
 Y    =      -10992547
75  feet           Y    =        -3350528
56  meter
 Z    =      -17251126
41                 Z    =        -5258143
33
 XDOT =      16150
225930                 XDOT =        4922
588863
 YDOT =      17651
815810  feet/sec       YDOT =        5380
273459  meter/sec
 ZDOT =      -3022
690980                 ZDOT =        -921
316211


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   18355
08747389  
00016717  00000-0  10270-3 0  9050
2 25544  51
6359 167
3055 0004621 167
8673 192
2592 15
54065581 27570


Satellite: ISS
Catalog Number: 25544
Epoch time:      18355
08747389   =   yrday
fracday
Element set:     905
Inclination:       51
6359  deg
RA of node:       167
3055  deg
Eccentricity:     
0004621     
Arg of perigee:   167
8673  deg
Mean anomaly:     192
2592  deg
Mean motion:   15
54065581  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2757
Checksum:              344


Coasting Arc #7 (Orbit 2772)
---------------------------------------

Vector Time (GMT): 2018/356/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -220292
35                 A    =         6777847
38  meter
 Y    =       -4289802
94  meter          E    =           
0004501
 Z    =        5239351
02                 I    =           51
73536
 XDOT =       7418
830633                 Wp   =          124
95136
 YDOT =      -1652
450167  meter/sec      RA   =          161
22984  deg
 ZDOT =      -1042
925741                 TA   =          335
00815
                                          MA   =          335
02993
                                          Ha   =            221
940  n
mi
                                          Hp   =            214
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -722743
95                 X    =         -197756
28
 Y    =      -14074156
64  feet           Y    =        -4292141
18  meter
 Z    =       17189471
85                 Z    =         5238335
01
 XDOT =      24339
995515                 XDOT =        7441
823409
 YDOT =      -5421
424431  feet/sec       YDOT =       -1569
358930  meter/sec
 ZDOT =      -3421
672378                 ZDOT =       -1006
831918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12422151
37                 X    =        -3786271
74
 Y    =        6666103
01  feet           Y    =         2031828
20  meter
 Z    =       17185325
49                 Z    =         5238087
21
 XDOT =     -14659
242393                 XDOT =       -4468
137081
 YDOT =     -18931
846406  feet/sec       YDOT =       -5770
426784  meter/sec
 ZDOT =      -3258
829089                 ZDOT =        -993
291106


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   18356
11634065  
00016717  00000-0  10270-3 0  9062
2 25544  51
6363 162
1769 0004504 171
6828 188
4400 15
54067837 27734


Satellite: ISS
Catalog Number: 25544
Epoch time:      18356
11634065   =   yrday
fracday
Element set:     906
Inclination:       51
6363  deg
RA of node:       162
1769  deg
Eccentricity:     
0004504     
Arg of perigee:   171
6828  deg
Mean anomaly:     188
4400  deg
Mean motion:   15
54067837  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2773
Checksum:              320


Coasting Arc #8 (Orbit 2787)
---------------------------------------

Vector Time (GMT): 2018/357/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1463275
01                 A    =         6780182
76  meter
 Y    =        4682651
42  meter          E    =           
0013170
 Z    =       -4692763
84                 I    =           51
77405
 XDOT =      -7074
176025                 Wp   =          127
72610
 YDOT =        655
108476  meter/sec      RA   =          156
24163  deg
 ZDOT =       2857
157115                 TA   =          170
64325
                                          MA   =          170
61869
                                          Ha   =            221
808  n
mi
                                          Hp   =            214
464

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4800771
03                 X    =        -1492734
08
 Y    =       15363029
59  feet           Y    =         4666124
07  meter
 Z    =      -15396206
83                 Z    =        -4699942
73
 XDOT =     -23209
238927                 XDOT =       -7094
854384
 YDOT =       2149
306022  feet/sec       YDOT =         575
884060  meter/sec
 ZDOT =       9373
875048                 ZDOT =        2822
743196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15875290
93                 X    =         4838788
68
 Y    =       -2456212
79  feet           Y    =         -748653
66  meter
 Z    =      -15429044
75                 Z    =        -4702772
84
 XDOT =      11884
830442                 XDOT =        3622
496319
 YDOT =      18858
229337  feet/sec       YDOT =        5747
988302  meter/sec
 ZDOT =       9218
674546                 ZDOT =        2809
852002


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   18357
08090291  
00016717  00000-0  10270-3 0  9077
2 25544  51
6361 157
3688 0004429 175
9159 184
2031 15
54057922 27882


Satellite: ISS
Catalog Number: 25544
Epoch time:      18357
08090291   =   yrday
fracday
Element set:     907
Inclination:       51
6361  deg
RA of node:       157
3688  deg
Eccentricity:     
0004429     
Arg of perigee:   175
9159  deg
Mean anomaly:     184
2031  deg
Mean motion:   15
54057922  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2788
Checksum:              333


Coasting Arc #9 (Orbit 2803)
---------------------------------------

Vector Time (GMT): 2018/358/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2950962
50                 A    =         6783747
55  meter
 Y    =       -4889551
88  meter          E    =           
0012266
 Z    =        3647700
06                 I    =           51
81755
 XDOT =       6271
631231                 Wp   =          106
64627
 YDOT =        501
282656  meter/sec      RA   =          151
26424  deg
 ZDOT =      -4392
991393                 TA   =           30
13401
                                          MA   =           30
06350
                                          Ha   =            221
635  n
mi
                                          Hp   =            214
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9681635
49                 X    =         2987701
08
 Y    =      -16041836
86  feet           Y    =        -4856347
28  meter
 Z    =       11967519
89                 Z    =         3662123
20
 XDOT =      20576
217950                 XDOT =        6286
898263
 YDOT =       1644
628138  feet/sec       YDOT =         571
502407  meter/sec
 ZDOT =     -14412
701420                 ZDOT =       -4362
489107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18646701
15                 X    =        -5683514
51
 Y    =       -1342527
29  feet           Y    =         -409202
32  meter
 Z    =       12033049
69                 Z    =         3667673
54
 XDOT =      -7946
452682                 XDOT =       -2422
078778
 YDOT =     -17834
781303  feet/sec       YDOT =       -5436
041341  meter/sec
 ZDOT =     -14275
226860                 ZDOT =       -4351
089147


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   18358
10976968  
00016717  00000-0  10270-3 0  9086
2 25544  51
6374 152
2403 0004393 180
1713 179
9438 15
54083834 28041


Satellite: ISS
Catalog Number: 25544
Epoch time:      18358
10976968   =   yrday
fracday
Element set:     908
Inclination:       51
6374  deg
RA of node:       152
2403  deg
Eccentricity:     
0004393     
Arg of perigee:   180
1713  deg
Mean anomaly:     179
9438  deg
Mean motion:   15
54083834  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2804
Checksum:              331


Coasting Arc #10 (Orbit 2805)
---------------------------------------

Vector Time (GMT): 2018/358/04:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4994923
40                 A    =         6781305
71  meter
 Y    =       -1192101
10  meter          E    =           
0011697
 Z    =        4425770
24                 I    =           51
81404
 XDOT =       4273
532718                 Wp   =          130
96863
 YDOT =      -5414
891943  meter/sec      RA   =          150
74615  deg
 ZDOT =       3351
326331                 TA   =          285
18985
                                          MA   =          285
31917
                                          Ha   =            221
808  n
mi
                                          Hp   =            214
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16387543
97                 X    =        -5002719
60
 Y    =       -3911092
86  feet           Y    =        -1248002
04  meter
 Z    =       14520243
56                 Z    =         4401487
76
 XDOT =      14020
776634                 XDOT =        4317
487129
 YDOT =     -17765
393514  feet/sec       YDOT =       -5366
857053  meter/sec
 ZDOT =      10995
165127                 ZDOT =        3372
191436

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13822942
72                 X    =         4213232
94
 Y    =        9794819
25  feet           Y    =         2985460
91  meter
 Z    =       14410880
89                 Z    =         4392436
50
 XDOT =     -18867
515954                 XDOT =       -5750
818863
 YDOT =      10246
166966  feet/sec       YDOT =        3123
031691  meter/sec
 ZDOT =      11089
795664                 ZDOT =        3380
169718


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   18358
23837854  
00016717  00000-0  10270-3 0  9091
2 25544  51
6391 151
6000 0004456 180
1487 179
9665 15
54073573 28067


Satellite: ISS
Catalog Number: 25544
Epoch time:      18358
23837854   =   yrday
fracday
Element set:     909
Inclination:       51
6391  deg
RA of node:       151
6000  deg
Eccentricity:     
0004456     
Arg of perigee:   180
1487  deg
Mean anomaly:     179
9665  deg
Mean motion:   15
54073573  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2806
Checksum:              332


Coasting Arc #11 (Orbit 2820)
---------------------------------------

Vector Time (GMT): 2018/359/04:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3755232
83                 A    =         6778312
98  meter
 Y    =        2337554
29  meter          E    =           
0013012
 Z    =       -5146885
50                 I    =           51
83433
 XDOT =      -5403
842768                 Wp   =           96
80343
 YDOT =       5189
585591  meter/sec      RA   =          145
76455  deg
 ZDOT =      -1590
713142                 TA   =          157
90788
                                          MA   =          157
85175
                                          Ha   =            221
583  n
mi
                                          Hp   =            214
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12320317
68                 X    =         3753815
04
 Y    =        7669141
37  feet           Y    =         2379540
63  meter
 Z    =      -16886107
28                 Z    =        -5128647
29
 XDOT =     -17729
142939                 XDOT =       -5453
745814
 YDOT =      17026
199444  feet/sec       YDOT =        5128
877238  meter/sec
 ZDOT =      -5218
875138                 ZDOT =       -1617
083313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8860730
49                 X    =        -2700750
65
 Y    =      -11612760
78  feet           Y    =        -3539569
49  meter
 Z    =      -16804101
24                 Z    =        -5121890
06
 XDOT =      21771
974884                 XDOT =        6636
097945
 YDOT =      -8911
229994  feet/sec       YDOT =       -2716
142902  meter/sec
 ZDOT =      -5338
325511                 ZDOT =       -1627
121616


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   18359
20293915  
00016717  00000-0  10270-3 0  9105
2 25544  51
6406 146
7921 0004331 183
5585 176
5538 15
54099566 28218


Satellite: ISS
Catalog Number: 25544
Epoch time:      18359
20293915   =   yrday
fracday
Element set:     910
Inclination:       51
6406  deg
RA of node:       146
7921  deg
Eccentricity:     
0004331     
Arg of perigee:   183
5585  deg
Mean anomaly:     176
5538  deg
Mean motion:   15
54099566  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2821
Checksum:              327


Coasting Arc #12 (Orbit 2836)
---------------------------------------

Vector Time (GMT): 2018/360/04:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2370499
26                 A    =         6777409
26  meter
 Y    =       -3459929
70  meter          E    =           
0004164
 Z    =        5322120
49                 I    =           51
85813
 XDOT =       6090
781627                 Wp   =          155
04091
 YDOT =      -4651
808112  meter/sec      RA   =          140
78045  deg
 ZDOT =       -314
884850                 TA   =          297
93000
                                          MA   =          297
97216
                                          Ha   =            221
515  n
mi
                                          Hp   =            214
780

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7777228
55                 X    =        -2357484
80
 Y    =      -11351475
38  feet           Y    =        -3486366
02  meter
 Z    =       17461025
22                 Z    =         5310636
88
 XDOT =      19982
879355                 XDOT =        6143
876293
 YDOT =     -15261
837638  feet/sec       YDOT =       -4583
399854  meter/sec
 ZDOT =      -1033
086778                 ZDOT =        -285
169933

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3534158
45                 X    =         1077211
49
 Y    =       13365801
35  feet           Y    =         4073896
25  meter
 Z    =       17409588
08                 Z    =         5306442
45
 XDOT =     -23029
826994                 XDOT =       -7019
491268
 YDOT =       7244
555861  feet/sec       YDOT =        2208
140626  meter/sec
 ZDOT =       -898
587414                 ZDOT =        -273
889444


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   18360
23180351  
00016717  00000-0  10270-3 0  9110
2 25544  51
6403 141
6641 0004362 189
0394 171
0681 15
54114975 28379


Satellite: ISS
Catalog Number: 25544
Epoch time:      18360
23180351   =   yrday
fracday
Element set:     911
Inclination:       51
6403  deg
RA of node:       141
6641  deg
Eccentricity:     
0004362     
Arg of perigee:   189
0394  deg
Mean anomaly:     171
0681  deg
Mean motion:   15
54114975  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2837
Checksum:              293


Coasting Arc #13 (Orbit 2850)
---------------------------------------

Vector Time (GMT): 2018/361/02:55:40
991
Vector Time (MET): N/A
Weight (LBS)     : 950680
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -340907
84                 A    =         6782370
07  meter
 Y    =        5140076
36  meter          E    =           
0009068
 Z    =       -4420949
72                 I    =           51
89364
 XDOT =      -6407
403711                 Wp   =          138
47942
 YDOT =       2485
625070  meter/sec      RA   =          136
09938  deg
 ZDOT =       3381
388961                 TA   =          165
66152
                                          MA   =          165
63577
                                          Ha   =            221
413  n
mi
                                          Hp   =            216
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1118464
05                 X    =         -376885
98
 Y    =       16863767
59  feet           Y    =         5136063
26  meter
 Z    =      -14504428
23                 Z    =        -4422692
71
 XDOT =     -21021
665720                 XDOT =       -6451
147201
 YDOT =       8154
937893  feet/sec       YDOT =        2413
728186  meter/sec
 ZDOT =      11093
795804                 ZDOT =        3350
158452

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11920071
03                 X    =         3633237
65
 Y    =      -11971047
03  feet           Y    =        -3648775
13  meter
 Z    =      -14512821
81                 Z    =        -4423508
09
 XDOT =      20342
861178                 XDOT =        6200
504087
 YDOT =       6967
516045  feet/sec       YDOT =        2123
698891  meter/sec
 ZDOT =      10952
666565                 ZDOT =        3338
372769


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   18361
13206241  
00016717  00000-0  10270-3 0  9128
2 25544  51
6398 137
1761 0004334 214
9459 145
1409 15
53675157 28513


Satellite: ISS
Catalog Number: 25544
Epoch time:      18361
13206241   =   yrday
fracday
Element set:     912
Inclination:       51
6398  deg
RA of node:       137
1761  deg
Eccentricity:     
0004334     
Arg of perigee:   214
9459  deg
Mean anomaly:     145
1409  deg
Mean motion:   15
53675157  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2851
Checksum:              305


Coasting Arc #14 (Orbit 2854)
---------------------------------------

Vector Time (GMT): 2018/361/09:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950680
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -918690
44                 A    =         6783813
19  meter
 Y    =        5394388
19  meter          E    =           
0007216
 Z    =       -4017587
78                 I    =           51
90136
 XDOT =      -6270
149094                 Wp   =          145
78940
 YDOT =       1892
410399  meter/sec      RA   =          134
81079  deg
 ZDOT =       3972
354824                 TA   =          165
44315
                                          MA   =          165
42235
                                          Ha   =            221
465  n
mi
                                          Hp   =            216
246

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3014076
23                 X    =         -959428
70
 Y    =       17698123
97  feet           Y    =         5383887
25  meter
 Z    =      -13181062
25                 Z    =        -4022148
96
 XDOT =     -20571
355295                 XDOT =       -6310
139856
 YDOT =       6208
695535  feet/sec       YDOT =        1822
069352  meter/sec
 ZDOT =      13032
660183                 ZDOT =        3941
800084

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12126423
13                 X    =        -3696133
77
 Y    =      -13217433
17  feet           Y    =        -4028673
63  meter
 Z    =      -13202195
73                 Z    =        -4024029
26
 XDOT =       6888
013643                 XDOT =        2099
466558
 YDOT =     -19206
911645  feet/sec       YDOT =       -5854
266669  meter/sec
 ZDOT =      12894
636282                 ZDOT =        3930
285139


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   18361
38934599  
00016717  00000-0  10270-3 0  9130
2 25544  51
6366 135
8908 0004588 214
4490 145
6365 15
53669069 28552


Satellite: ISS
Catalog Number: 25544
Epoch time:      18361
38934599   =   yrday
fracday
Element set:     913
Inclination:       51
6366  deg
RA of node:       135
8908  deg
Eccentricity:     
0004588     
Arg of perigee:   214
4490  deg
Mean anomaly:     145
6365  deg
Mean motion:   15
53669069  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2855
Checksum:              356


Coasting Arc #15 (Orbit 2870)
---------------------------------------

Vector Time (GMT): 2018/362/09:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950680
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1998112
33                 A    =         6787236
11  meter
 Y    =       -5835238
66  meter          E    =           
0011681
 Z    =        2815973
29                 I    =           51
93591
 XDOT =       5679
075881                 Wp   =          119
48726
 YDOT =       -535
652011  meter/sec      RA   =          129
85053  deg
 ZDOT =      -5129
297042                 TA   =           28
67552
                                          MA   =           28
61134
                                          Ha   =            221
258  n
mi
                                          Hp   =            216
395

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6555486
63                 X    =         2049536
76
 Y    =      -19144483
79  feet           Y    =        -5812607
00  meter
 Z    =        9238757
50                 Z    =         2825803
89
 XDOT =      18632
138717                 XDOT =        5709
558719
 YDOT =      -1757
388486  feet/sec       YDOT =        -471
973917  meter/sec
 ZDOT =     -16828
402370                 ZDOT =       -5101
636399

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11354371
42                 X    =         3460812
41
 Y    =       16725165
96  feet           Y    =         5097830
59  meter
 Z    =        9283715
75                 Z    =         2829676
56
 XDOT =      -8681
755400                 XDOT =       -2646
199046
 YDOT =      15184
333168  feet/sec       YDOT =        4628
184750  meter/sec
 ZDOT =     -16703
561170                 ZDOT =       -5091
245445


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   18362
41848312  
00016717  00000-0  10270-3 0  9143
2 25544  51
6369 130
7638 0004563 220
8816 139
1995 15
53681057 28711


Satellite: ISS
Catalog Number: 25544
Epoch time:      18362
41848312   =   yrday
fracday
Element set:     914
Inclination:       51
6369  deg
RA of node:       130
7638  deg
Eccentricity:     
0004563     
Arg of perigee:   220
8816  deg
Mean anomaly:     139
1995  deg
Mean motion:   15
53681057  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2871
Checksum:              328


Coasting Arc #16 (Orbit 2885)
---------------------------------------

Vector Time (GMT): 2018/363/09:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950680
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2859705
44                 A    =         6789827
44  meter
 Y    =        5997703
83  meter          E    =           
0004064
 Z    =       -1388311
15                 I    =           51
96452
 XDOT =      -4877
649878                 Wp   =           35
16397
 YDOT =       -978
930233  meter/sec      RA   =          124
89899  deg
 ZDOT =       5829
780513                 TA   =          309
78564
                                          MA   =          309
82141
                                          Ha   =            221
289  n
mi
                                          Hp   =            216
405

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9382235
69                 X    =        -2919817
28
 Y    =       19677505
99  feet           Y    =         5965388
57  meter
 Z    =       -4554826
62                 Z    =        -1402348
19
 XDOT =     -16002
788314                 XDOT =       -4894
658434
 YDOT =      -3211
713364  feet/sec       YDOT =       -1033
570895  meter/sec
 ZDOT =      19126
576487                 ZDOT =        5806
045435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10387207
57                 X    =        -3166020
87
 Y    =      -19150710
57  feet           Y    =        -5837136
58  meter
 Z    =       -4618791
81                 Z    =        -1407807
74
 XDOT =      10702
227233                 XDOT =        3262
038861
 YDOT =     -10382
851770  feet/sec       YDOT =       -3164
693219  meter/sec
 ZDOT =      19019
595188                 ZDOT =        5797
172613


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   18363
38330147  
00016717  00000-0  10270-3 0  9153
2 25544  51
6366 125
9570 0004509 220
1005 139
9815 15
53666677 28868


Satellite: ISS
Catalog Number: 25544
Epoch time:      18363
38330147   =   yrday
fracday
Element set:     915
Inclination:       51
6366  deg
RA of node:       125
9570  deg
Eccentricity:     
0004509     
Arg of perigee:   220
1005  deg
Mean anomaly:     139
9815  deg
Mean motion:   15
53666677  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2886
Checksum:              325


Coasting Arc #17 (Orbit 2901)
---------------------------------------

Vector Time (GMT): 2018/364/09:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950680
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3507197
59                 A    =         6790551
53  meter
 Y    =       -5802934
15  meter          E    =           
0012516
 Z    =        -180801
89                 I    =           51
98522
 XDOT =       3963
052365                 Wp   =          156
75305
 YDOT =       2578
610946  meter/sec      RA   =          119
95370  deg
 ZDOT =      -6039
655348                 TA   =           25
18583
                                          MA   =           25
12484
                                          Ha   =            221
062  n
mi
                                          Hp   =            216
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11506553
79                 X    =         3572705
21
 Y    =      -19038497
87  feet           Y    =        -5763347
94  meter
 Z    =        -593182
04                 Z    =         -163606
44
 XDOT =      13002
140306                 XDOT =        3963
260364
 YDOT =       8460
009666  feet/sec       YDOT =        2622
930045  meter/sec
 ZDOT =     -19815
142218                 ZDOT =       -6020
403678

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8950891
41                 X    =         2728231
70
 Y    =       20367459
19  feet           Y    =         6208001
56  meter
 Z    =        -514971
19                 Z    =         -156963
22
 XDOT =     -12989
339959                 XDOT =       -3959
150819
 YDOT =       5224
238811  feet/sec       YDOT =        1592
347990  meter/sec
 ZDOT =     -19728
555781                 ZDOT =       -6013
263802


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   18364
41243837  
00016717  00000-0  10270-3 0  9168
2 25544  51
6364 120
8301 0004425 227
0176 133
0605 15
53705298 29028


Satellite: ISS
Catalog Number: 25544
Epoch time:      18364
41243837   =   yrday
fracday
Element set:     916
Inclination:       51
6364  deg
RA of node:       120
8301  deg
Eccentricity:     
0004425     
Arg of perigee:   227
0176  deg
Mean anomaly:     133
0605  deg
Mean motion:   15
53705298  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2902
Checksum:              290


Coasting Arc #18 (Orbit 2903)
---------------------------------------

Vector Time (GMT): 2018/364/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950680
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4930869
77                 A    =         6784199
51  meter
 Y    =       -2477502
71  meter          E    =           
0003357
 Z    =       -3947655
87                 I    =           51
96941
 XDOT =          6
994506                 Wp   =          118
48103
 YDOT =       6493
791195  meter/sec      RA   =          119
29965  deg
 ZDOT =      -4070
868783                 TA   =          109
13599
                                          MA   =          109
09965
                                          Ha   =            221
290  n
mi
                                          Hp   =            216
682

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16177394
27                 X    =         4977382
96
 Y    =       -8128289
72  feet           Y    =        -2422102
00  meter
 Z    =      -12951626
86                 Z    =        -3923590
70
 XDOT =         22
947855                 XDOT =         -45
847382
 YDOT =      21305
089221  feet/sec       YDOT =        6493
574180  meter/sec
 ZDOT =     -13355
868712                 ZDOT =       -4070
962790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11886037
42                 X    =         3622864
21
 Y    =       13758889
48  feet           Y    =         4193709
51  meter
 Z    =      -12842775
88                 Z    =        -3914478
09
 XDOT =     -19616
281730                 XDOT =       -5979
042671
 YDOT =       4491
387897  feet/sec       YDOT =        1368
975031  meter/sec
 ZDOT =     -13356
993645                 ZDOT =       -4071
211663


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   18364
54108177  
00016717  00000-0  10270-3 0  9170
2 25544  51
6401 120
1900 0004758 224
4459 135
6312 15
53659573 29041


Satellite: ISS
Catalog Number: 25544
Epoch time:      18364
54108177   =   yrday
fracday
Element set:     917
Inclination:       51
6401  deg
RA of node:       120
1900  deg
Eccentricity:     
0004758     
Arg of perigee:   224
4459  deg
Mean anomaly:     135
6312  deg
Mean motion:   15
53659573  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2904
Checksum:              305


Coasting Arc #19 (Orbit 2919)
---------------------------------------

Vector Time (GMT): 2018/365/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950680
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4640080
48                 A    =         6780873
80  meter
 Y    =        1119823
28  meter          E    =           
0007287
 Z    =        4816348
37                 I    =           51
97490
 XDOT =        991
586149                 Wp   =          155
54171
 YDOT =      -7141
253508  meter/sec      RA   =          114
33553  deg
 ZDOT =       2607
806626                 TA   =          268
83538
                                          MA   =          268
91886
                                          Ha   =            221
073  n
mi
                                          Hp   =            216
615

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15223361
15                 X    =        -4675652
99
 Y    =        3673960
91  feet           Y    =         1067735
45  meter
 Z    =       15801667
89                 Z    =         4793722
22
 XDOT =       3253
235396                 XDOT =        1058
700649
 YDOT =     -23429
309411  feet/sec       YDOT =       -7129
789820  meter/sec
 ZDOT =       8555
796016                 ZDOT =        2612
785911

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7577747
06                 X    =        -2309697
30
 Y    =      -13821959
65  feet           Y    =        -4212933
30  meter
 Z    =       15699445
93                 Z    =         4785191
12
 XDOT =      22436
402206                 XDOT =        6838
615392
 YDOT =      -2526
655707  feet/sec       YDOT =        -770
124659  meter/sec
 ZDOT =       8579
051204                 ZDOT =        2614
894807


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   18365
57021737  
00016717  00000-0  10270-3 0  9181
2 25544  51
6409 115
0629 0004645 229
2010 130
8740 15
53698262 29209


Satellite: ISS
Catalog Number: 25544
Epoch time:      18365
57021737   =   yrday
fracday
Element set:     918
Inclination:       51
6409  deg
RA of node:       115
0629  deg
Eccentricity:     
0004645     
Arg of perigee:   229
2010  deg
Mean anomaly:     130
8740  deg
Mean motion:   15
53698262  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2920
Checksum:              304
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