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

 
Date: July 26th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14678 7446 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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


207/16:11:39 616 -1 1 1 3 1 3
N/A -0 4 -0 1 222 1
000/00:03:19 233 0 7 -0 1 215 2

209/20:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 215 1

212/23:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 214 7

215/16:42:42 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 214 5

216/02:32:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 214 4

Coasting Arc #1 (Orbit 446)
---------------------------------------

Vector Time (GMT): 2018/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5482656
14                 A    =         6786446
87  meter
 Y    =        2865656
84  meter          E    =           
0004307
 Z    =       -2796073
63                 I    =           51
59602
 XDOT =      -4463
667327                 Wp   =           63
63813
 YDOT =       3559
886848  meter/sec      RA   =          186
60047  deg
 ZDOT =      -5108
303503                 TA   =          148
06805
                                          MA   =          148
04194
                                          Ha   =            221
746  n
mi
                                          Hp   =            214
827

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17987717
01                 X    =         5463785
74
 Y    =        9401761
28  feet           Y    =         2926862
48  meter
 Z    =       -9173469
90                 Z    =        -2769486
72
 XDOT =     -14644
577844                 XDOT =       -4478
330164
 YDOT =      11679
418793  feet/sec       YDOT =        3509
889605  meter/sec
 ZDOT =     -16759
525928                 ZDOT =       -5130
021340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1687557
58                 X    =         -514367
55
 Y    =      -20279772
87  feet           Y    =        -6181274
77  meter
 Z    =       -9054644
66                 Z    =        -2759855
69
 XDOT =      16154
958270                 XDOT =        4924
031281
 YDOT =       6175
924717  feet/sec       YDOT =        1882
421854  meter/sec
 ZDOT =     -16857
245158                 ZDOT =       -5138
088324


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   18206
52660406  
00016717  00000-0  10270-3 0  9003
2 25544  51
6358 187
6223 0004463 357
2113   2
9014 15
54009256  4476


Satellite: ISS
Catalog Number: 25544
Epoch time:      18206
52660406   =   yrday
fracday
Element set:     900
Inclination:       51
6358  deg
RA of node:       187
6223  deg
Eccentricity:     
0004463     
Arg of perigee:   357
2113  deg
Mean anomaly:       2
9014  deg
Mean motion:   15
54009256  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             447
Checksum:              283


Coasting Arc #2 (Orbit 462)
---------------------------------------

Vector Time (GMT): 2018/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4283113
15                 A    =         6782694
01  meter
 Y    =       -3335109
19  meter          E    =           
0010605
 Z    =        4056050
55                 I    =           51
61646
 XDOT =       5946
077059                 Wp   =           78
71799
 YDOT =      -2907
854744  meter/sec      RA   =          181
61739  deg
 ZDOT =       3881
374808                 TA   =          331
06360
                                          MA   =          331
12236
                                          Ha   =            221
772  n
mi
                                          Hp   =            214
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14052208
49                 X    =        -4265202
50
 Y    =      -10941959
30  feet           Y    =        -3382906
19  meter
 Z    =       13307252
46                 Z    =         4035288
22
 XDOT =      19508
126834                 XDOT =        5959
298252
 YDOT =      -9540
205852  feet/sec       YDOT =       -2841
288071  meter/sec
 ZDOT =      12734
169318                 ZDOT =        3910
290072

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1394640
72                 X    =         -425086
49
 Y    =       17824261
08  feet           Y    =         5432834
78  meter
 Z    =       13214563
88                 Z    =         4027799
07
 XDOT =     -17328
656523                 XDOT =       -5281
774508
 YDOT =     -10909
146976  feet/sec       YDOT =       -3325
107998  meter/sec
 ZDOT =      12864
088434                 ZDOT =        3920
974155


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   18207
55551361  
00016717  00000-0  10270-3 0  9017
2 25544  51
6356 182
4947 0004358 357
9551   2
1583 15
54041163  4630


Satellite: ISS
Catalog Number: 25544
Epoch time:      18207
55551361   =   yrday
fracday
Element set:     901
Inclination:       51
6356  deg
RA of node:       182
4947  deg
Eccentricity:     
0004358     
Arg of perigee:   357
9551  deg
Mean anomaly:       2
1583  deg
Mean motion:   15
54041163  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             463
Checksum:              301


Coasting Arc #3 (Orbit 464)
---------------------------------------

Vector Time (GMT): 2018/207/16:13:19
233
Vector Time (MET): N/A
Weight (LBS)     : 944330
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4794175
66                 A    =         6784140
42  meter
 Y    =        2944907
46  meter          E    =           
0006271
 Z    =       -3791902
37                 I    =           51
62810
 XDOT =      -5419
582510                 Wp   =           55
11078
 YDOT =      -3404
232994  meter/sec      RA   =          180
68964  deg
 ZDOT =       4216
706737                 TA   =          259
42203
                                          MA   =          259
49268
                                          Ha   =            222
051  n
mi
                                          Hp   =            215
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15728922
78                 X    =        -4808331
41
 Y    =        9661769
87  feet           Y    =         2891216
90  meter
 Z    =      -12440624
59                 Z    =        -3815224
46
 XDOT =     -17780
782514                 XDOT =       -5401
594792
 YDOT =     -11168
743418  feet/sec       YDOT =       -3464
738350  meter/sec
 ZDOT =      13834
339687                 ZDOT =        4190
424135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14399997
50                 X    =         4389119
24
 Y    =      -11435423
36  feet           Y    =        -3485517
04  meter
 Z    =      -12545481
80                 Z    =        -3823862
85
 XDOT =      18228
674140                 XDOT =        5556
099878
 YDOT =       7936
101329  feet/sec       YDOT =        2418
923685  meter/sec
 ZDOT =      13716
913081                 ZDOT =        4180
915107


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   18207
68412896  
00016717  00000-0  10270-3 0  9021
2 25544  51
6387 181
8536 0005209 350
5334   9
5719 15
53781200  4651


Satellite: ISS
Catalog Number: 25544
Epoch time:      18207
68412896   =   yrday
fracday
Element set:     902
Inclination:       51
6387  deg
RA of node:       181
8536  deg
Eccentricity:     
0005209     
Arg of perigee:   350
5334  deg
Mean anomaly:       9
5719  deg
Mean motion:   15
53781200  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             465
Checksum:              316


Coasting Arc #4 (Orbit 480)
---------------------------------------

Vector Time (GMT): 2018/208/16:13:19
233
Vector Time (MET): N/A
Weight (LBS)     : 944330
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5828548
61                 A    =         6787675
46  meter
 Y    =       -2415090
69  meter          E    =           
0012822
 Z    =        2495330
60                 I    =           51
67323
 XDOT =       3906
145329                 Wp   =           82
39726
 YDOT =       3915
764312  meter/sec      RA   =          175
71254  deg
 ZDOT =      -5309
008340                 TA   =           69
64434
                                          MA   =           69
50663
                                          Ha   =            222
197  n
mi
                                          Hp   =            215
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19122534
81                 X    =         5843000
89
 Y    =       -7923525
88  feet           Y    =        -2349831
24  meter
 Z    =        8186780
17                 Z    =         2523677
96
 XDOT =      12815
437430                 XDOT =        3887
855676
 YDOT =      12846
995773  feet/sec       YDOT =        3959
343720  meter/sec
 ZDOT =     -17418
006366                 ZDOT =       -5290
078126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17825941
11                 X    =        -5433346
85
 Y    =       10420565
85  feet           Y    =         3176188
47  meter
 Z    =        8314120
55                 Z    =         2534143
94
 XDOT =     -13784
232267                 XDOT =       -4201
433995
 YDOT =      -9685
724257  feet/sec       YDOT =       -2952
208754  meter/sec
 ZDOT =     -17333
574672                 ZDOT =       -5283
273560


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   18208
71319792  
00016717  00000-0  10270-3 0  9038
2 25544  51
6392 176
7268 0005177 353
8799   6
2290 15
53762294  4815


Satellite: ISS
Catalog Number: 25544
Epoch time:      18208
71319792   =   yrday
fracday
Element set:     903
Inclination:       51
6392  deg
RA of node:       176
7268  deg
Eccentricity:     
0005177     
Arg of perigee:   353
8799  deg
Mean anomaly:       6
2290  deg
Mean motion:   15
53762294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             481
Checksum:              337


Coasting Arc #5 (Orbit 495)
---------------------------------------

Vector Time (GMT): 2018/209/16:13:19
233
Vector Time (MET): N/A
Weight (LBS)     : 944330
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6446283
16                 A    =         6789860
12  meter
 Y    =        1853231
53  meter          E    =           
0014060
 Z    =       -1003703
74                 I    =           51
71475
 XDOT =      -2172
222446                 Wp   =           24
47556
 YDOT =      -4375
682200  meter/sec      RA   =          170
74413  deg
 ZDOT =       5913
968261                 TA   =          324
65671
                                          MA   =          324
74983
                                          Ha   =            222
261  n
mi
                                          Hp   =            215
031

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21149222
96                 X    =        -6461652
05
 Y    =        6080155
94  feet           Y    =         1781058
88  meter
 Z    =       -3292991
29                 Z    =        -1035054
06
 XDOT =      -7126
714061                 XDOT =       -2151
857217
 YDOT =     -14355
912731  feet/sec       YDOT =       -4399
860037  meter/sec
 ZDOT =      19402
783007                 ZDOT =        5903
465748

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19959087
36                 X    =         6083529
83
 Y    =       -9216610
40  feet           Y    =        -2809222
85  meter
 Z    =       -3433750
75                 Z    =        -1046607
23
 XDOT =       8678
236022                 XDOT =        2645
126339
 YDOT =      11631
208845  feet/sec       YDOT =        3545
192456  meter/sec
 ZDOT =      19356
171748                 ZDOT =        5899
761149


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   18209
67794618  
00016717  00000-0  10270-3 0  9049
2 25544  51
6404 171
9195 0005323 357
1977   2
9145 15
53786124  4969


Satellite: ISS
Catalog Number: 25544
Epoch time:      18209
67794618   =   yrday
fracday
Element set:     904
Inclination:       51
6404  deg
RA of node:       171
9195  deg
Eccentricity:     
0005323     
Arg of perigee:   357
1977  deg
Mean anomaly:       2
9145  deg
Mean motion:   15
53786124  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             496
Checksum:              332


Coasting Arc #6 (Orbit 498)
---------------------------------------

Vector Time (GMT): 2018/209/20:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 944330
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5441530
44                 A    =         6784997
63  meter
 Y    =        1909095
49  meter          E    =           
0007628
 Z    =       -3584902
18                 I    =           51
70021
 XDOT =      -4459
102012                 Wp   =           40
56548
 YDOT =       4358
793346  meter/sec      RA   =          169
92977  deg
 ZDOT =      -4446
927300                 TA   =          181
71368
                                          MA   =          181
71629
                                          Ha   =            222
318  n
mi
                                          Hp   =            215
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17852790
15                 X    =         5437191
16
 Y    =        6263436
64  feet           Y    =         1969922
42  meter
 Z    =      -11761490
09                 Z    =        -3558480
11
 XDOT =     -14629
599778                 XDOT =       -4485
911490
 YDOT =      14300
503103  feet/sec       YDOT =        4308
778983  meter/sec
 ZDOT =     -14589
656497                 ZDOT =       -4468
652412

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11967499
80                 X    =        -3647693
94
 Y    =       14747863
61  feet           Y    =         4495148
83  meter
 Z    =      -11643232
86                 Z    =        -3548857
38
 XDOT =      -7454
019059                 XDOT =       -2271
985009
 YDOT =     -17645
210441  feet/sec       YDOT =       -5378
260143  meter/sec
 ZDOT =     -14687
536354                 ZDOT =       -4476
761081


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   18209
87089428  
00016717  00000-0  10270-3 0  9058
2 25544  51
6368 170
9564 0005337 357
3187   2
7936 15
53785238  4991


Satellite: ISS
Catalog Number: 25544
Epoch time:      18209
87089428   =   yrday
fracday
Element set:     905
Inclination:       51
6368  deg
RA of node:       170
9564  deg
Eccentricity:     
0005337     
Arg of perigee:   357
3187  deg
Mean anomaly:       2
7936  deg
Mean motion:   15
53785238  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             499
Checksum:              353


Coasting Arc #7 (Orbit 514)
---------------------------------------

Vector Time (GMT): 2018/210/20:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 944330
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4254714
01                 A    =         6781577
79  meter
 Y    =       -2603928
21  meter          E    =           
0008168
 Z    =        4586412
96                 I    =           51
72081
 XDOT =       5764
386879                 Wp   =           77
19311
 YDOT =      -4042
224578  meter/sec      RA   =          164
94955  deg
 ZDOT =       3049
726301                 TA   =          342
37189
                                          MA   =          342
40022
                                          Ha   =            222
531  n
mi
                                          Hp   =            214
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13959035
47                 X    =        -4247557
84
 Y    =       -8543071
56  feet           Y    =        -2651467
58  meter
 Z    =       15047286
61                 Z    =         4565762
74
 XDOT =      18912
030442                 XDOT =        5794
346094
 YDOT =     -13261
891659  feet/sec       YDOT =       -3977
595858  meter/sec
 ZDOT =      10005
663718                 ZDOT =        3077
799648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12620508
82                 X    =         3846731
09
 Y    =      -10551360
49  feet           Y    =        -3216054
68  meter
 Z    =       14954969
95                 Z    =         4558274
84
 XDOT =       5703
269527                 XDOT =        1738
356552
 YDOT =      21195
374566  feet/sec       YDOT =        6460
350168  meter/sec
 ZDOT =      10131
986244                 ZDOT =        3088
229407


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   18210
89995907  
00016717  00000-0  10270-3 0  9061
2 25544  51
6367 165
8288 0005309    
1957 359
9196 15
53759424  5155


Satellite: ISS
Catalog Number: 25544
Epoch time:      18210
89995907   =   yrday
fracday
Element set:     906
Inclination:       51
6367  deg
RA of node:       165
8288  deg
Eccentricity:     
0005309     
Arg of perigee:      
1957  deg
Mean anomaly:     359
9196  deg
Mean motion:   15
53759424  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             515
Checksum:              350


Coasting Arc #8 (Orbit 529)
---------------------------------------

Vector Time (GMT): 2018/211/20:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 944330
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2852885
26                 A    =         6779011
12  meter
 Y    =        3317079
77  meter          E    =           
0016026
 Z    =       -5191840
21                 I    =           51
74420
 XDOT =      -6636
497473                 Wp   =           61
58822
 YDOT =       3565
507554  meter/sec      RA   =          159
96328  deg
 ZDOT =      -1364
471796                 TA   =          195
26970
                                          MA   =          195
31812
                                          Ha   =            222
463  n
mi
                                          Hp   =            214
874

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9359859
77                 X    =         2840799
44
 Y    =       10882807
66  feet           Y    =         3348915
30  meter
 Z    =      -17033596
50                 Z    =        -5178011
41
 XDOT =     -21773
285672                 XDOT =       -6669
246977
 YDOT =      11697
859430  feet/sec       YDOT =        3491
110583  meter/sec
 ZDOT =      -4476
613505                 ZDOT =       -1396
788374

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13259785
49                 X    =        -4041582
62
 Y    =        5684833
37  feet           Y    =         1732737
21  meter
 Z    =      -16971937
00                 Z    =        -5173046
40
 XDOT =      -4061
604850                 XDOT =       -1237
977158
 YDOT =     -23313
892964  feet/sec       YDOT =       -7106
074575  meter/sec
 ZDOT =      -4621
927913                 ZDOT =       -1408
763628


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   18211
86470393  
00016717  00000-0  10270-3 0  9077
2 25544  51
6367 161
0215 0005177   4
9879 355
1324 15
53788304  5308


Satellite: ISS
Catalog Number: 25544
Epoch time:      18211
86470393   =   yrday
fracday
Element set:     907
Inclination:       51
6367  deg
RA of node:       161
0215  deg
Eccentricity:     
0005177     
Arg of perigee:     4
9879  deg
Mean anomaly:     355
1324  deg
Mean motion:   15
53788304  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             530
Checksum:              309


Coasting Arc #9 (Orbit 545)
---------------------------------------

Vector Time (GMT): 2018/212/20:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 944330
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1308014
14                 A    =         6778487
00  meter
 Y    =       -4003874
07  meter          E    =           
0006828
 Z    =        5308389
69                 I    =           51
77321
 XDOT =       7080
666578                 Wp   =           29
73350
 YDOT =      -2915
712574  meter/sec      RA   =          154
97498  deg
 ZDOT =       -448
439010                 TA   =           64
56972
                                          MA   =           64
49907
                                          Ha   =            222
638  n
mi
                                          Hp   =            214
715

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4291384
96                 X    =        -1288929
40
 Y    =      -13136069
79  feet           Y    =        -4018394
58  meter
 Z    =       17415976
69                 Z    =         5302082
20
 XDOT =      23230
533393                 XDOT =        7114
922877
 YDOT =      -9565
986134  feet/sec       YDOT =       -2836
340118  meter/sec
 ZDOT =      -1471
256594                 ZDOT =        -413
961044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13848222
37                 X    =         4220938
18
 Y    =        -410621
52  feet           Y    =         -125157
44  meter
 Z    =       17388119
09                 Z    =         5299898
70
 XDOT =       2389
472270                 XDOT =         728
311148
 YDOT =      24005
050172  feet/sec       YDOT =        7316
739292  meter/sec
 ZDOT =      -1316
302454                 ZDOT =        -401
208988


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   18212
89376326  
00016717  00000-0  10270-3 0  9083
2 25544  51
6370 155
8936 0005215   9
2885 350
8363 15
53755443  5461


Satellite: ISS
Catalog Number: 25544
Epoch time:      18212
89376326   =   yrday
fracday
Element set:     908
Inclination:       51
6370  deg
RA of node:       155
8936  deg
Eccentricity:     
0005215     
Arg of perigee:     9
2885  deg
Mean anomaly:     350
8363  deg
Mean motion:   15
53755443  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             546
Checksum:              328


Coasting Arc #10 (Orbit 547)
---------------------------------------

Vector Time (GMT): 2018/212/23:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944330
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1338877
35                 A    =         6781094
47  meter
 Y    =       -4726139
24  meter          E    =           
0011682
 Z    =        4671622
67                 I    =           51
78859
 XDOT =       7051
058451                 Wp   =           44
97322
 YDOT =       -870
271379  meter/sec      RA   =          154
29493  deg
 ZDOT =      -2888
769909                 TA   =           73
73563
                                          MA   =           73
60716
                                          Ha   =            222
517  n
mi
                                          Hp   =            214
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4392642
21                 X    =         1368934
94
 Y    =      -15505706
17  feet           Y    =        -4710999
01  meter
 Z    =       15326846
04                 Z    =         4678199
29
 XDOT =      23133
393867                 XDOT =        7074
297900
 YDOT =      -2855
221060  feet/sec       YDOT =        -791
291578  meter/sec
 ZDOT =      -9477
591564                 ZDOT =       -2854
462470

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15488033
31                 X    =         4720752
55
 Y    =       -4349975
90  feet           Y    =        -1325872
65  meter
 Z    =       15356854
26                 Z    =         4680769
18
 XDOT =      14127
977418                 XDOT =        4306
207517
 YDOT =      17242
794692  feet/sec       YDOT =        5255
603822  meter/sec
 ZDOT =      -9323
621019                 ZDOT =       -2841
839687


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   18213
02239625  
00016717  00000-0  10270-3 0  9090
2 25544  51
6394 155
2515 0004878  11
7068 348
4197 15
53764230  5483


Satellite: ISS
Catalog Number: 25544
Epoch time:      18213
02239625   =   yrday
fracday
Element set:     909
Inclination:       51
6394  deg
RA of node:       155
2515  deg
Eccentricity:     
0004878     
Arg of perigee:    11
7068  deg
Mean anomaly:     348
4197  deg
Mean motion:   15
53764230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             548
Checksum:              317


Coasting Arc #11 (Orbit 562)
---------------------------------------

Vector Time (GMT): 2018/213/23:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944330
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2696104
27                 A    =         6784436
89  meter
 Y    =        4996615
53  meter          E    =           
0007716
 Z    =       -3716686
16                 I    =           51
82904
 XDOT =      -6322
871509                 Wp   =           62
50049
 YDOT =       -202
226324  meter/sec      RA   =          149
32142  deg
 ZDOT =       4325
122260                 TA   =          253
33873
                                          MA   =          253
42345
                                          Ha   =            222
555  n
mi
                                          Hp   =            214
558

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8845486
47                 X    =        -2733723
97
 Y    =       16393095
57  feet           Y    =         4966255
52  meter
 Z    =      -12193852
24                 Z    =        -3729874
04
 XDOT =     -20744
329098                 XDOT =       -6341
149109
 YDOT =       -663
472190  feet/sec       YDOT =        -273
035290  meter/sec
 ZDOT =      14190
033661                 ZDOT =        4294
363967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18542556
02                 X    =        -5651771
07
 Y    =        1300136
27  feet           Y    =          396281
54  meter
 Z    =      -12253550
81                 Z    =        -3734882
29
 XDOT =     -10430
817864                 XDOT =       -3179
313285
 YDOT =     -16644
371272  feet/sec       YDOT =       -5073
204364  meter/sec
 ZDOT =      14052
084231                 ZDOT =        4283
075274


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   18213
98713515  
00016717  00000-0  10270-3 0  9102
2 25544  51
6392 150
4458 0004937  13
2366 346
8915 15
53777568  5633


Satellite: ISS
Catalog Number: 25544
Epoch time:      18213
98713515   =   yrday
fracday
Element set:     910
Inclination:       51
6392  deg
RA of node:       150
4458  deg
Eccentricity:     
0004937     
Arg of perigee:    13
2366  deg
Mean anomaly:     346
8915  deg
Mean motion:   15
53777568  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             563
Checksum:              329


Coasting Arc #12 (Orbit 578)
---------------------------------------

Vector Time (GMT): 2018/214/23:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944330
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3839974
81                 A    =         6787862
37  meter
 Y    =       -5057947
64  meter          E    =           
0014724
 Z    =        2385777
63                 I    =           51
86863
 XDOT =       5259
628893                 Wp   =           87
23980
 YDOT =       1436
226169  meter/sec      RA   =          144
35765  deg
 ZDOT =      -5391
303023                 TA   =           66
20251
                                          MA   =           66
04820
                                          Ha   =            222
600  n
mi
                                          Hp   =            214
461

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12598342
56                 X    =         3884660
05
 Y    =      -16594316
41  feet           Y    =        -5014756
57  meter
 Z    =        7827354
42                 Z    =         2404539
17
 XDOT =      17256
000306                 XDOT =        5269
365553
 YDOT =       4712
028113  feet/sec       YDOT =        1495
097487  meter/sec
 ZDOT =     -17688
002043                 ZDOT =       -5365
730161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20753033
13                 X    =         6325524
50
 Y    =        1437969
39  feet           Y    =          438293
07  meter
 Z    =        7912073
64                 Z    =         2411600
05
 XDOT =       5654
560735                 XDOT =        1723
510112
 YDOT =      15610
136665  feet/sec       YDOT =        4757
969656  meter/sec
 ZDOT =     -17573
437092                 ZDOT =       -5356
383626


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   18215
01618847  
00016717  00000-0  10270-3 0  9111
2 25544  51
6395 145
3181 0004820  17
8352 342
2969 15
53786423  5794


Satellite: ISS
Catalog Number: 25544
Epoch time:      18215
01618847   =   yrday
fracday
Element set:     911
Inclination:       51
6395  deg
RA of node:       145
3181  deg
Eccentricity:     
0004820     
Arg of perigee:    17
8352  deg
Mean anomaly:     342
2969  deg
Mean motion:   15
53786423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             579
Checksum:              319


Coasting Arc #13 (Orbit 589)
---------------------------------------

Vector Time (GMT): 2018/215/16:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 919623
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5892315
87                 A    =         6787806
71  meter
 Y    =       -2298640
82  meter          E    =           
0005715
 Z    =       -2471137
18                 I    =           51
88757
 XDOT =        -97
428155                 Wp   =           75
39458
 YDOT =       5486
522841  meter/sec      RA   =          140
84105  deg
 ZDOT =      -5344
773575                 TA   =          132
15563
                                          MA   =          132
10707
                                          Ha   =            222
759  n
mi
                                          Hp   =            214
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19331744
99                 X    =         5929585
37
 Y    =       -7541472
51  feet           Y    =        -2232540
44  meter
 Z    =       -8107405
45                 Z    =        -2442424
10
 XDOT =       -319
646179                 XDOT =        -132
810843
 YDOT =      18000
403021  feet/sec       YDOT =        5485
235597  meter/sec
 ZDOT =     -17535
346375                 ZDOT =       -5345
332677

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15145722
27                 X    =        -4616416
15
 Y    =       14257400
81  feet           Y    =         4345655
77  meter
 Z    =       -7978334
04                 Z    =        -2431796
21
 XDOT =      -5517
446138                 XDOT =       -1681
717583
 YDOT =     -15658
961991  feet/sec       YDOT =       -4772
851615  meter/sec
 ZDOT =     -17538
459753                 ZDOT =       -5345
722533


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   18215
72365881  
00016717  00000-0  10270-3 0  9127
2 25544  51
6398 141
7973 0005398  15
9357 344
1964 15
53789316  5904


Satellite: ISS
Catalog Number: 25544
Epoch time:      18215
72365881   =   yrday
fracday
Element set:     912
Inclination:       51
6398  deg
RA of node:       141
7973  deg
Eccentricity:     
0005398     
Arg of perigee:    15
9357  deg
Mean anomaly:     344
1964  deg
Mean motion:   15
53789316  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             590
Checksum:              345


Coasting Arc #14 (Orbit 595)
---------------------------------------

Vector Time (GMT): 2018/216/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919623
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3697655
66                 A    =         6788594
80  meter
 Y    =        5324684
43  meter          E    =           
0011695
 Z    =       -1998918
01                 I    =           51
90078
 XDOT =      -5046
941059                 Wp   =           31
34621
 YDOT =      -1412
629418  meter/sec      RA   =          138
76851  deg
 ZDOT =       5597
432860                 TA   =          306
66445
                                          MA   =          306
77190
                                          Ha   =            222
746  n
mi
                                          Hp   =            214
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12131416
20                 X    =        -3747213
31
 Y    =       17469437
11  feet           Y    =         5283057
64  meter
 Z    =       -6558129
94                 Z    =        -2017000
05
 XDOT =     -16558
205574                 XDOT =       -5057
958735
 YDOT =      -4634
610951  feet/sec       YDOT =       -1469
129540  meter/sec
 ZDOT =      18364
281036                 ZDOT =        5572
889949

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15006189
50                 X    =        -4573886
56
 Y    =       15036232
06  feet           Y    =         4583043
53  meter
 Z    =       -6639846
58                 Z    =        -2023825
24
 XDOT =     -14491
128221                 XDOT =       -4416
895882
 YDOT =      -6436
160692  feet/sec       YDOT =       -1961
741779  meter/sec
 ZDOT =      18254
324322                 ZDOT =        5563
918053


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   18216
10955199  
00016717  00000-0  10270-3 0  9138
2 25544  51
6398 139
8729 0005231  18
9892 341
1455 15
53782517  5968


Satellite: ISS
Catalog Number: 25544
Epoch time:      18216
10955199   =   yrday
fracday
Element set:     913
Inclination:       51
6398  deg
RA of node:       139
8729  deg
Eccentricity:     
0005231     
Arg of perigee:    18
9892  deg
Mean anomaly:     341
1455  deg
Mean motion:   15
53782517  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             596
Checksum:              340


Coasting Arc #15 (Orbit 611)
---------------------------------------

Vector Time (GMT): 2018/217/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919623
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4456870
26                 A    =         6790132
45  meter
 Y    =       -5102668
63  meter          E    =           
0012513
 Z    =         404816
73                 I    =           51
92988
 XDOT =       3808
594886                 Wp   =          106
46079
 YDOT =       2837
332381  meter/sec      RA   =          133
81770  deg
 ZDOT =      -6016
597299                 TA   =           69
19414
                                          MA   =           69
06015
                                          Ha   =            222
845  n
mi
                                          Hp   =            214
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14622277
75                 X    =         4511632
09
 Y    =      -16741038
81  feet           Y    =        -5052522
65  meter
 Z    =        1328138
89                 Z    =          426599
35
 XDOT =      12495
390045                 XDOT =        3805
809278
 YDOT =       9308
833270  feet/sec       YDOT =        2879
907382  meter/sec
 ZDOT =     -19739
492451                 ZDOT =       -5998
103226

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17120478
93                 X    =         5218321
98
 Y    =      -14166572
48  feet           Y    =        -4317971
29  meter
 Z    =        1426452
01                 Z    =          434782
57
 XDOT =       9927
776175                 XDOT =        3025
986178
 YDOT =       9972
350273  feet/sec       YDOT =        3039
572363  meter/sec
 ZDOT =     -19656
828634                 ZDOT =       -5991
401368


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   18217
13859829  
00016717  00000-0  10270-3 0  9146
2 25544  51
6393 134
7457 0005317  24
6995 335
4411 15
53823931  6121


Satellite: ISS
Catalog Number: 25544
Epoch time:      18217
13859829   =   yrday
fracday
Element set:     914
Inclination:       51
6393  deg
RA of node:       134
7457  deg
Eccentricity:     
0005317     
Arg of perigee:    24
6995  deg
Mean anomaly:     335
4411  deg
Mean motion:   15
53823931  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             612
Checksum:              321


Coasting Arc #16 (Orbit 627)
---------------------------------------

Vector Time (GMT): 2018/218/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919623
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4870195
60                 A    =         6789792
34  meter
 Y    =        4565439
99  meter          E    =           
0018573
 Z    =        1184126
40                 I    =           51
94996
 XDOT =      -2516
400839                 Wp   =           49
64727
 YDOT =      -4224
871967  meter/sec      RA   =          128
86933  deg
 ZDOT =       5890
585331                 TA   =          323
16724
                                          MA   =          323
29469
                                          Ha   =            223
033  n
mi
                                          Hp   =            214
114

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15978332
03                 X    =        -4926637
48
 Y    =       14978477
66  feet           Y    =         4510662
44  meter
 Z    =        3884929
14                 Z    =         1160332
00
 XDOT =      -8255
908263                 XDOT =       -2497
583309
 YDOT =     -13861
128502  feet/sec       YDOT =       -4252
907218  meter/sec
 ZDOT =      19326
067358                 ZDOT =        5878
407069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17996278
68                 X    =        -5485265
74
 Y    =       12514712
58  feet           Y    =         3814484
39  meter
 Z    =        3777629
50                 Z    =         1151421
47
 XDOT =      -5385
438226                 XDOT =       -1641
481571
 YDOT =     -13611
379814  feet/sec       YDOT =       -4148
748567  meter/sec
 ZDOT =      19271
900802                 ZDOT =        5874
075365


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   18218
16764261  
00016717  00000-0  10270-3 0  9156
2 25544  51
6389 129
6183 0005404  28
2732 331
8713 15
53778416  6280


Satellite: ISS
Catalog Number: 25544
Epoch time:      18218
16764261   =   yrday
fracday
Element set:     915
Inclination:       51
6389  deg
RA of node:       129
6183  deg
Eccentricity:     
0005404     
Arg of perigee:    28
2732  deg
Mean anomaly:     331
8713  deg
Mean motion:   15
53778416  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             628
Checksum:              320


Coasting Arc #17 (Orbit 642)
---------------------------------------

Vector Time (GMT): 2018/219/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919623
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5025947
01                 A    =         6787158
62  meter
 Y    =       -3675675
97  meter          E    =           
0007169
 Z    =       -2709401
00                 I    =           51
96282
 XDOT =       1214
464692                 Wp   =           76
19550
 YDOT =       5488
534253  meter/sec      RA   =          123
91819  deg
 ZDOT =      -5202
982316                 TA   =          134
24144
                                          MA   =          134
18256
                                          Ha   =            223
004  n
mi
                                          Hp   =            213
972

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16489327
46                 X    =         5079836
63
 Y    =      -12059304
36  feet           Y    =        -3619170
85  meter
 Z    =       -8889110
88                 Z    =        -2684856
27
 XDOT =       3984
464211                 XDOT =        1178
273254
 YDOT =      18007
002144  feet/sec       YDOT =        5501
913250  meter/sec
 ZDOT =     -17070
151957                 ZDOT =       -5197
170428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17947028
83                 X    =         5470254
39
 Y    =       -9858127
04  feet           Y    =        -3004757
12  meter
 Z    =       -8778526
16                 Z    =        -2675694
77
 XDOT =       1056
258491                 XDOT =         321
947588
 YDOT =      17071
844679  feet/sec       YDOT =        5203
498258  meter/sec
 ZDOT =     -17044
706438                 ZDOT =       -5195
226522


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   18219
13236485  
00016717  00000-0  10270-3 0  9167
2 25544  51
6401 124
8110 0005421  32
5912 327
5574 15
53830980  6438


Satellite: ISS
Catalog Number: 25544
Epoch time:      18219
13236485   =   yrday
fracday
Element set:     916
Inclination:       51
6401  deg
RA of node:       124
8110  deg
Eccentricity:     
0005421     
Arg of perigee:    32
5912  deg
Mean anomaly:     327
5574  deg
Mean motion:   15
53830980  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             643
Checksum:              289


Coasting Arc #18 (Orbit 658)
---------------------------------------

Vector Time (GMT): 2018/220/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919623
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4909361
16                 A    =         6783678
24  meter
 Y    =        2490511
68  meter          E    =           
0014430
 Z    =        3949867
50                 I    =           51
96837
 XDOT =        -27
334196                 Wp   =           79
94889
 YDOT =      -6511
799826  meter/sec      RA   =          118
96118  deg
 ZDOT =       4061
800887                 TA   =          327
79294
                                          MA   =          327
88099
                                          Ha   =            223
204  n
mi
                                          Hp   =            213
803

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16106827
97                 X    =        -4956032
01
 Y    =        8170970
08  feet           Y    =         2435350
55  meter
 Z    =       12958882
87                 Z    =         3925906
66
 XDOT =        -89
679122                 XDOT =          25
754739
 YDOT =     -21364
172659  feet/sec       YDOT =       -6511
808979  meter/sec
 ZDOT =      13326
118397                 ZDOT =        4061
796537

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16993562
74                 X    =        -5179637
92
 Y    =        6340104
56  feet           Y    =         1932463
87  meter
 Z    =       12851039
02                 Z    =         3916996
69
 XDOT =       2636
563949                 XDOT =         803
624692
 YDOT =     -20013
777700  feet/sec       YDOT =       -6100
199443  meter/sec
 ZDOT =      13326
867642                 ZDOT =        4062
029257


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   18220
16139908  
00016717  00000-0  10270-3 0  9175
2 25544  51
6397 119
6841 0005470  36
3603 323
7920 15
53831088  6598


Satellite: ISS
Catalog Number: 25544
Epoch time:      18220
16139908   =   yrday
fracday
Element set:     917
Inclination:       51
6397  deg
RA of node:       119
6841  deg
Eccentricity:     
0005470     
Arg of perigee:    36
3603  deg
Mean anomaly:     323
7920  deg
Mean motion:   15
53831088  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             659
Checksum:              317


Coasting Arc #19 (Orbit 673)
---------------------------------------

Vector Time (GMT): 2018/221/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919623
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4627021
92                 A    =         6780371
00  meter
 Y    =       -1050164
34  meter          E    =           
0016355
 Z    =       -4859167
67                 I    =           51
97321
 XDOT =      -1025
798395                 Wp   =           62
01532
 YDOT =       7154
241114  meter/sec      RA   =          113
99589  deg
 ZDOT =      -2521
971939                 TA   =          183
25534
                                          MA   =          183
26599
                                          Ha   =            223
104  n
mi
                                          Hp   =            213
886

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15180518
11                 X    =         4662024
12
 Y    =       -3445421
06  feet           Y    =         -998225
71  meter
 Z    =      -15942151
16                 Z    =        -4836606
66
 XDOT =      -3365
480300                 XDOT =       -1093
472661
 YDOT =      23471
919664  feet/sec       YDOT =        7142
391726  meter/sec
 ZDOT =      -8274
186150                 ZDOT =       -2527
118653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15540218
05                 X    =         4736658
46
 Y    =       -2010871
01  feet           Y    =         -612913
48  meter
 Z    =      -15840746
85                 Z    =        -4828259
64
 XDOT =      -5624
437472                 XDOT =       -1714
328542
 YDOT =      21928
751384  feet/sec       YDOT =        6683
883422  meter/sec
 ZDOT =      -8298
145391                 ZDOT =       -2529
274715


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   18221
12611709  
00016717  00000-0  10270-3 0  9187
2 25544  51
6406 114
8775 0005396  39
6633 320
4914 15
53822846  6744


Satellite: ISS
Catalog Number: 25544
Epoch time:      18221
12611709   =   yrday
fracday
Element set:     918
Inclination:       51
6406  deg
RA of node:       114
8775  deg
Eccentricity:     
0005396     
Arg of perigee:    39
6633  deg
Mean anomaly:     320
4914  deg
Mean motion:   15
53822846  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             674
Checksum:              315
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