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

 
Date: July 30th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13813 3257 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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


213/16:38:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 212 8

217/02:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 212 8

220/05:58:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 212 7

223/08:44:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 212 9

Coasting Arc #1 (Orbit 1156)
---------------------------------------

Vector Time (GMT): 2016/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5607679
79                 A    =         6786537
52  meter
 Y    =       -3657218
31  meter          E    =           
0015300
 Z    =        1069016
01                 I    =           51
49057
 XDOT =       3436
107671                 Wp   =           60
38795
 YDOT =      -3533
996104  meter/sec      RA   =          205
81212  deg
 ZDOT =       5878
503749                 TA   =          311
23707
                                          MA   =          311
36882
                                          Ha   =            220
446  n
mi
                                          Hp   =            212
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18397899
57                 X    =        -5571559
84
 Y    =      -11998747
74  feet           Y    =        -3719725
25  meter
 Z    =        3507270
37                 Z    =         1041863
04
 XDOT =      11273
319130                 XDOT =        3446
815377
 YDOT =     -11594
475408  feet/sec       YDOT =       -3495
511806  meter/sec
 ZDOT =      19286
429623                 ZDOT =        5895
221089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1394702
55                 X    =          425105
34
 Y    =       21939007
02  feet           Y    =         6687009
34  meter
 Z    =        3389450
84                 Z    =         1033104
62
 XDOT =     -14358
118931                 XDOT =       -4376
354650
 YDOT =      -2107
556622  feet/sec       YDOT =        -642
383258  meter/sec
 ZDOT =      19359
926763                 ZDOT =        5900
905677


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   16211
56227129  
00016717  00000-0  10270-3 0  9002
2 25544  51
6387 206
6068 0001954  87
3196 272
8181 15
54934887 11570


Satellite: ISS
Catalog Number: 25544
Epoch time:      16211
56227129   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:       206
6068  deg
Eccentricity:     
0001954     
Arg of perigee:    87
3196  deg
Mean anomaly:     272
8181  deg
Mean motion:   15
54934887  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1157
Checksum:              326


Coasting Arc #2 (Orbit 1171)
---------------------------------------

Vector Time (GMT): 2016/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4486421
30                 A    =         6783621
40  meter
 Y    =        4178645
00  meter          E    =           
0006442
 Z    =       -2905988
27                 I    =           51
50879
 XDOT =      -5336
138426                 Wp   =          107
18574
 YDOT =       2243
751828  meter/sec      RA   =          200
82367  deg
 ZDOT =      -5022
914314                 TA   =          105
99042
                                          MA   =          105
91945
                                          Ha   =            220
579  n
mi
                                          Hp   =            212
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14719229
99                 X    =         4453477
04
 Y    =       13709465
21  feet           Y    =         4228631
17  meter
 Z    =       -9534082
23                 Z    =        -2884274
36
 XDOT =     -17507
015834                 XDOT =       -5336
433222
 YDOT =       7361
390513  feet/sec       YDOT =        2184
078296  meter/sec
 ZDOT =     -16479
377671                 ZDOT =       -5048
836127

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1807062
44                 X    =          550792
63
 Y    =      -20077943
12  feet           Y    =        -6119757
06  meter
 Z    =       -9440053
89                 Z    =        -2877328
43
 XDOT =      15000
242721                 XDOT =        4572
073981
 YDOT =       9134
243427  feet/sec       YDOT =        2784
117397  meter/sec
 ZDOT =     -16592
820660                 ZDOT =       -5057
491737


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   16212
52633186  
00016717  00000-0  10270-3 0  9014
2 25544  51
6378 201
7947 0002043  84
3398 275
7988 15
54883111 11720


Satellite: ISS
Catalog Number: 25544
Epoch time:      16212
52633186   =   yrday
fracday
Element set:     901
Inclination:       51
6378  deg
RA of node:       201
7947  deg
Eccentricity:     
0002043     
Arg of perigee:    84
3398  deg
Mean anomaly:     275
7988  deg
Mean motion:   15
54883111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1172
Checksum:              318


Coasting Arc #3 (Orbit 1187)
---------------------------------------

Vector Time (GMT): 2016/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2864896
56                 A    =         6779221
09  meter
 Y    =       -4371728
43  meter          E    =           
0011572
 Z    =        4309329
12                 I    =           51
52516
 XDOT =       6760
726830                 Wp   =          104
72447
 YDOT =       -972
475898  meter/sec      RA   =          195
82605  deg
 ZDOT =       3497
315074                 TA   =          309
62222
                                          MA   =          309
72431
                                          Ha   =            220
493  n
mi
                                          Hp   =            212
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9399266
93                 X    =        -2836730
35
 Y    =      -14342941
05  feet           Y    =        -4403608
43  meter
 Z    =       14138218
88                 Z    =         4295480
52
 XDOT =      22180
862303                 XDOT =        6754
110690
 YDOT =      -3190
537723  feet/sec       YDOT =        -896
910174  meter/sec
 ZDOT =      11474
130821                 ZDOT =        3530
140265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5262287
89                 X    =        -1603945
35
 Y    =       16372509
42  feet           Y    =         4990340
87  meter
 Z    =       14078518
09                 Z    =         4291132
31
 XDOT =     -15113
817806                 XDOT =       -4606
691667
 YDOT =     -14877
914678  feet/sec       YDOT =       -4534
788394  meter/sec
 ZDOT =      11617
498283                 ZDOT =        3541
013477


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   16213
55465791  
00016717  00000-0  10270-3 0  9024
2 25544  51
6382 196
6630 0001832  87
8120 272
3243 15
54913888 11881


Satellite: ISS
Catalog Number: 25544
Epoch time:      16213
55465791   =   yrday
fracday
Element set:     902
Inclination:       51
6382  deg
RA of node:       196
6630  deg
Eccentricity:     
0001832     
Arg of perigee:    87
8120  deg
Mean anomaly:     272
3243  deg
Mean motion:   15
54913888  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1188
Checksum:              319


Coasting Arc #4 (Orbit 1190)
---------------------------------------

Vector Time (GMT): 2016/213/16:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2795145
73                 A    =         6779013
46  meter
 Y    =       -4343962
44  meter          E    =           
0011303
 Z    =        4382344
09                 I    =           51
53290
 XDOT =       6820
711651                 Wp   =          105
41773
 YDOT =       -968
536905  meter/sec      RA   =          194
86112  deg
 ZDOT =       3380
112432                 TA   =          310
29844
                                          MA   =          310
39717
                                          Ha   =            220
556  n
mi
                                          Hp   =            212
776

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9170425
63                 X    =        -2767649
85
 Y    =      -14251845
28  feet           Y    =        -4375066
19  meter
 Z    =       14377769
31                 Z    =         4368832
71
 XDOT =      22377
662898                 XDOT =        6814
616329
 YDOT =      -3177
614518  feet/sec       YDOT =        -892
297464  meter/sec
 ZDOT =      11089
607716                 ZDOT =        3413
230251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13283695
33                 X    =         4048870
34
 Y    =       10603135
23  feet           Y    =         3231835
62  meter
 Z    =       14319532
55                 Z    =         4364593
52
 XDOT =     -19393
142030                 XDOT =       -5911
029691
 YDOT =       9078
569928  feet/sec       YDOT =        2767
148114  meter/sec
 ZDOT =      11234
255283                 ZDOT =        3424
201010


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   16213
74747083  
00016717  00000-0  10270-3 0  9033
2 25544  51
6408 195
7011 0001914  84
8224 275
3148 15
54892111 11912


Satellite: ISS
Catalog Number: 25544
Epoch time:      16213
74747083   =   yrday
fracday
Element set:     903
Inclination:       51
6408  deg
RA of node:       195
7011  deg
Eccentricity:     
0001914     
Arg of perigee:    84
8224  deg
Mean anomaly:     275
3148  deg
Mean motion:   15
54892111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1191
Checksum:              299


Coasting Arc #5 (Orbit 1205)
---------------------------------------

Vector Time (GMT): 2016/214/16:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         781065
47                 A    =         6775705
55  meter
 Y    =        4311446
20  meter          E    =           
0015855
 Z    =       -5182372
35                 I    =           51
55437
 XDOT =      -7537
296976                 Wp   =           80
61176
 YDOT =       -235
188542  meter/sec      RA   =          189
85203  deg
 ZDOT =      -1332
610302                 TA   =          176
55594
                                          MA   =          176
54501
                                          Ha   =            220
484  n
mi
                                          Hp   =            212
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2562550
75                 X    =          757968
92
 Y    =       14145164
69  feet           Y    =         4320051
74  meter
 Z    =      -17002533
97                 Z    =        -5178634
08
 XDOT =     -24728
664619                 XDOT =       -7527
633750
 YDOT =       -771
615951  feet/sec       YDOT =        -319
421527  meter/sec
 ZDOT =      -4372
081044                 ZDOT =       -1369
200347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7210719
91                 X    =        -2197827
43
 Y    =      -12457466
02  feet           Y    =        -3797035
64  meter
 Z    =      -16986923
52                 Z    =        -5177614
29
 XDOT =      22650
246318                 XDOT =        6903
795078
 YDOT =      -6935
457583  feet/sec       YDOT =       -2113
927471  meter/sec
 ZDOT =      -4531
704557                 ZDOT =       -1381
263549


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   16214
71152506  
00016717  00000-0  10270-3 0  9042
2 25544  51
6417 190
8898 0001972  85
0276 275
1102 15
54913270 12060


Satellite: ISS
Catalog Number: 25544
Epoch time:      16214
71152506   =   yrday
fracday
Element set:     904
Inclination:       51
6417  deg
RA of node:       190
8898  deg
Eccentricity:     
0001972     
Arg of perigee:    85
0276  deg
Mean anomaly:     275
1102  deg
Mean motion:   15
54913270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1206
Checksum:              296


Coasting Arc #6 (Orbit 1221)
---------------------------------------

Vector Time (GMT): 2016/215/16:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1350450
59                 A    =         6775223
84  meter
 Y    =       -4062138
86  meter          E    =           
0004910
 Z    =        5247776
14                 I    =           51
58486
 XDOT =       7502
645610                 Wp   =           70
56735
 YDOT =       1342
805697  meter/sec      RA   =          184
83991  deg
 ZDOT =       -889
011934                 TA   =           27
94888
                                          MA   =           27
92252
                                          Ha   =            220
325  n
mi
                                          Hp   =            212
753

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4430612
16                 X    =         1370283
25
 Y    =      -13327227
24  feet           Y    =        -4046926
52  meter
 Z    =       17217113
34                 Z    =         5254384
16
 XDOT =      24614
979035                 XDOT =        7491
390744
 YDOT =       4405
530502  feet/sec       YDOT =        1426
642394  meter/sec
 ZDOT =      -2916
705819                 ZDOT =        -852
594104

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         584225
49                 X    =          178071
93
 Y    =       13995981
21  feet           Y    =         4265975
07  meter
 Z    =       17246608
14                 Z    =         5256766
16
 XDOT =     -23607
238168                 XDOT =       -7195
486194
 YDOT =       4393
160376  feet/sec       YDOT =        1339
035283  meter/sec
 ZDOT =      -2757
990132                 ZDOT =        -840
635392


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   16215
73984838  
00016717  00000-0  10270-3 0  9057
2 25544  51
6415 185
7583 0001753  89
1275 271
0079 15
54937360 12225


Satellite: ISS
Catalog Number: 25544
Epoch time:      16215
73984838   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       185
7583  deg
Eccentricity:     
0001753     
Arg of perigee:    89
1275  deg
Mean anomaly:     271
0079  deg
Mean motion:   15
54937360  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1222
Checksum:              326


Coasting Arc #7 (Orbit 1236)
---------------------------------------

Vector Time (GMT): 2016/216/16:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3362217
85                 A    =         6777968
28  meter
 Y    =        3665150
63  meter          E    =           
0012045
 Z    =       -4616410
79                 I    =           51
62726
 XDOT =      -6652
369511                 Wp   =          107
61437
 YDOT =      -2345
064758  meter/sec      RA   =          179
83321  deg
 ZDOT =       2986
071991                 TA   =          192
18985
                                          MA   =          192
21902
                                          Ha   =            220
406  n
mi
                                          Hp   =            212
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11030898
45                 X    =        -3380528
60
 Y    =       12024772
42  feet           Y    =         3627449
76  meter
 Z    =      -15145704
70                 Z    =        -4632787
64
 XDOT =     -21825
359287                 XDOT =       -6640
156698
 YDOT =      -7693
782015  feet/sec       YDOT =       -2419
387760  meter/sec
 ZDOT =       9796
824119                 ZDOT =        2953
786834

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5809199
87                 X    =         1770644
12
 Y    =      -15176983
18  feet           Y    =        -4625944
47  meter
 Z    =      -15217773
22                 Z    =        -4638377
28
 XDOT =      22080
303087                 XDOT =        6730
076381
 YDOT =      -1221
310432  feet/sec       YDOT =        -372
255420  meter/sec
 ZDOT =       9656
285482                 ZDOT =        2943
235815


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   16216
70390204  
00016717  00000-0  10270-3 0  9064
2 25544  51
6428 180
9470 0001733  91
0098 269
1253 15
54902760 12378


Satellite: ISS
Catalog Number: 25544
Epoch time:      16216
70390204   =   yrday
fracday
Element set:     906
Inclination:       51
6428  deg
RA of node:       180
9470  deg
Eccentricity:     
0001733     
Arg of perigee:    91
0098  deg
Mean anomaly:     269
1253  deg
Mean motion:   15
54902760  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1237
Checksum:              296


Coasting Arc #8 (Orbit 1243)
---------------------------------------

Vector Time (GMT): 2016/217/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3202206
54                 A    =         6777536
74  meter
 Y    =       -3631200
70  meter          E    =           
0009677
 Z    =        4737270
04                 I    =           51
63901
 XDOT =       6760
738435                 Wp   =          116
12450
 YDOT =      -2406
957548  meter/sec      RA   =          177
83715  deg
 ZDOT =       2716
540315                 TA   =          306
99183
                                          MA   =          307
08036
                                          Ha   =            220
476  n
mi
                                          Hp   =            212
765

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10505926
97                 X    =        -3184374
63
 Y    =      -11913388
12  feet           Y    =        -3666910
24  meter
 Z    =       15542224
55                 Z    =         4721758
17
 XDOT =      22180
900378                 XDOT =        6773
955697
 YDOT =      -7896
842348  feet/sec       YDOT =       -2331
280571  meter/sec
 ZDOT =       8912
533842                 ZDOT =        2749
413613

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8015185
98                 X    =        -2443028
69
 Y    =      -13789205
55  feet           Y    =        -4202949
85  meter
 Z    =       15475098
26                 Z    =         4716809
95
 XDOT =      22248
171774                 XDOT =        6781
242757
 YDOT =      -2737
086947  feet/sec       YDOT =        -834
264101  meter/sec
 ZDOT =       9056
408445                 ZDOT =        2760
393294


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   16217
15379138  
00016717  00000-0  10270-3 0  9078
2 25544  51
6428 178
6973 0001863 109
5095 250
6259 15
54931644 12448


Satellite: ISS
Catalog Number: 25544
Epoch time:      16217
15379138   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:       178
6973  deg
Eccentricity:     
0001863     
Arg of perigee:   109
5095  deg
Mean anomaly:     250
6259  deg
Mean motion:   15
54931644  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1244
Checksum:              330


Coasting Arc #9 (Orbit 1258)
---------------------------------------

Vector Time (GMT): 2016/218/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1160210
26                 A    =         6775239
30  meter
 Y    =        4077633
75  meter          E    =           
0016363
 Z    =       -5299123
31                 I    =           51
66326
 XDOT =      -7507
504919                 Wp   =           88
31227
 YDOT =       1397
655112  meter/sec      RA   =          172
83378  deg
 ZDOT =       -569
286853                 TA   =          176
25532
                                          MA   =          176
24305
                                          Ha   =            220
423  n
mi
                                          Hp   =            212
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3806464
09                 X    =         1140267
21
 Y    =       13378063
50  feet           Y    =         4090496
43  meter
 Z    =      -17385575
18                 Z    =        -5293535
91
 XDOT =     -24630
921651                 XDOT =       -7519
810590
 YDOT =       4585
482650  feet/sec       YDOT =        1313
632363  meter/sec
 ZDOT =      -1867
739019                 ZDOT =        -605
785562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1408775
11                 X    =          429394
65
 Y    =       13867301
06  feet           Y    =         4226753
36  meter
 Z    =      -17361834
30                 Z    =        -5291887
09
 XDOT =     -24030
493265                 XDOT =       -7324
494347
 YDOT =        -92
598495  feet/sec       YDOT =         -28
224021  meter/sec
 ZDOT =      -2027
293192                 ZDOT =        -617
918965


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   16218
11784273  
00016717  00000-0  10270-3 0  9086
2 25544  51
6428 173
8873 0001822 109
6175 250
5175 15
54899782 12597


Satellite: ISS
Catalog Number: 25544
Epoch time:      16218
11784273   =   yrday
fracday
Element set:     908
Inclination:       51
6428  deg
RA of node:       173
8873  deg
Eccentricity:     
0001822     
Arg of perigee:   109
6175  deg
Mean anomaly:     250
5175  deg
Mean motion:   15
54899782  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1259
Checksum:              337


Coasting Arc #10 (Orbit 1274)
---------------------------------------

Vector Time (GMT): 2016/219/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         967326
73                 A    =         6775849
77  meter
 Y    =       -4337669
24  meter          E    =           
0006103
 Z    =        5110358
70                 I    =           51
69789
 XDOT =       7488
483690                 Wp   =           69
83376
 YDOT =       -280
456304  meter/sec      RA   =          167
82882  deg
 ZDOT =      -1651
871185                 TA   =           36
10773
                                          MA   =           36
06653
                                          Ha   =            220
335  n
mi
                                          Hp   =            212
784

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3173644
11                 X    =          990936
28
 Y    =      -14231198
31  feet           Y    =        -4326719
82  meter
 Z    =       16766268
71                 Z    =         5115115
10
 XDOT =      24568
516044                 XDOT =        7499
087198
 YDOT =       -920
132232  feet/sec       YDOT =        -196
655826  meter/sec
 ZDOT =      -5419
524886                 ZDOT =       -1615
468915

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5381666
48                 X    =         1640331
94
 Y    =      -13524672
10  feet           Y    =        -4122320
06  meter
 Z    =       16787724
66                 Z    =         5116898
48
 XDOT =      23429
005761                 XDOT =        7141
160956
 YDOT =       2778
127635  feet/sec       YDOT =         846
773303  meter/sec
 ZDOT =      -5260
553855                 ZDOT =       -1603
416815


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   16219
14616206  
00016717  00000-0  10270-3 0  9091
2 25544  51
6430 168
7552 0001808 112
7154 247
4190 15
54934624 12758


Satellite: ISS
Catalog Number: 25544
Epoch time:      16219
14616206   =   yrday
fracday
Element set:     909
Inclination:       51
6430  deg
RA of node:       168
7552  deg
Eccentricity:     
0001808     
Arg of perigee:   112
7154  deg
Mean anomaly:     247
4190  deg
Mean motion:   15
54934624  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1275
Checksum:              303


Coasting Arc #11 (Orbit 1289)
---------------------------------------

Vector Time (GMT): 2016/220/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2935307
86                 A    =         6779303
16  meter
 Y    =        4408322
10  meter          E    =           
0010079
 Z    =       -4242513
20                 I    =           51
74078
 XDOT =      -6673
753820                 Wp   =          111
70280
 YDOT =       -943
296951  meter/sec      RA   =          162
83423  deg
 ZDOT =       3640
579220                 TA   =          195
52766
                                          MA   =          195
55860
                                          Ha   =            220
356  n
mi
                                          Hp   =            212
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9630275
13                 X    =        -2963776
69
 Y    =       14462999
01  feet           Y    =         4375338
22  meter
 Z    =      -13919006
57                 Z    =        -4256841
25
 XDOT =     -21895
517781                 XDOT =       -6680
393726
 YDOT =      -3094
806271  feet/sec       YDOT =       -1017
964346  meter/sec
 ZDOT =      11944
157547                 ZDOT =        3608
144190

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11585583
92                 X    =        -3531285
98
 Y    =       12881370
42  feet           Y    =         3926241
71  meter
 Z    =      -13982268
21                 Z    =        -4261795
35
 XDOT =     -20328
084210                 XDOT =       -6196
000067
 YDOT =      -5483
539474  feet/sec       YDOT =       -1671
382832  meter/sec
 ZDOT =      11802
688019                 ZDOT =        3597
459308


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   16220
11021068  
00016717  00000-0  10270-3 0  9108
2 25544  51
6430 163
9451 0001851 116
0302 244
1042 15
54930656 12901


Satellite: ISS
Catalog Number: 25544
Epoch time:      16220
11021068   =   yrday
fracday
Element set:     910
Inclination:       51
6430  deg
RA of node:       163
9451  deg
Eccentricity:     
0001851     
Arg of perigee:   116
0302  deg
Mean anomaly:     244
1042  deg
Mean motion:   15
54930656  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1290
Checksum:              253


Coasting Arc #12 (Orbit 1292)
---------------------------------------

Vector Time (GMT): 2016/220/05:58:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4693076
37                 A    =         6778945
76  meter
 Y    =       -2130398
36  meter          E    =           
0011560
 Z    =        4396214
02                 I    =           51
74247
 XDOT =       5221
121727                 Wp   =          108
83940
 YDOT =      -4488
271784  meter/sec      RA   =          162
14644  deg
 ZDOT =       3387
754275                 TA   =          306
89677
                                          MA   =          307
00266
                                          Ha   =            220
604  n
mi
                                          Hp   =            212
728

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15397232
18                 X    =        -4690259
52
 Y    =       -6989495
95  feet           Y    =        -2182863
60  meter
 Z    =       14423274
34                 Z    =         4373423
47
 XDOT =      17129
664458                 XDOT =        5254
466665
 YDOT =     -14725
301130  feet/sec       YDOT =       -4429
699167  meter/sec
 ZDOT =      11114
679380                 ZDOT =        3413
197926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15911353
24                 X    =        -4849780
47
 Y    =        5967207
99  feet           Y    =         1818804
99  meter
 Z    =       14324102
83                 Z    =         4365986
54
 XDOT =       2147
923825                 XDOT =         654
687182
 YDOT =     -21308
110224  feet/sec       YDOT =       -6494
711996  meter/sec
 ZDOT =      11226
488929                 ZDOT =        3421
833826


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   16220
30302032  
00016717  00000-0  10270-3 0  9113
2 25544  51
6418 162
9838 0002037 105
7521 254
3857 15
54913869 12937


Satellite: ISS
Catalog Number: 25544
Epoch time:      16220
30302032   =   yrday
fracday
Element set:     911
Inclination:       51
6418  deg
RA of node:       162
9838  deg
Eccentricity:     
0002037     
Arg of perigee:   105
7521  deg
Mean anomaly:     254
3857  deg
Mean motion:   15
54913869  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1293
Checksum:              294


Coasting Arc #13 (Orbit 1307)
---------------------------------------

Vector Time (GMT): 2016/221/05:58:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2973076
00                 A    =         6775731
90  meter
 Y    =        3192244
85  meter          E    =           
0015602
 Z    =       -5198407
60                 I    =           51
76303
 XDOT =      -6475
118958                 Wp   =           83
50973
 YDOT =       3866
168594  meter/sec      RA   =          157
15224  deg
 ZDOT =      -1330
821079                 TA   =          173
71771
                                          MA   =          173
69813
                                          Ha   =            220
461  n
mi
                                          Hp   =            212
866

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9754186
36                 X    =         2962409
87
 Y    =       10473244
26  feet           Y    =         3225431
99  meter
 Z    =      -17055143
03                 Z    =        -5183991
31
 XDOT =     -21243
828601                 XDOT =       -6511
405711
 YDOT =      12684
280164  feet/sec       YDOT =        3793
556556  meter/sec
 ZDOT =      -4366
210890                 ZDOT =       -1362
363455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14384350
22                 X    =         4384349
95
 Y    =         222460
10  feet           Y    =           67805
84  meter
 Z    =      -16992700
81                 Z    =        -5179375
21
 XDOT =      -5670
532483                 XDOT =       -1728
378301
 YDOT =      23005
696341  feet/sec       YDOT =        7012
136245  meter/sec
 ZDOT =      -4504
565169                 ZDOT =       -1372
991464


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   16221
26706662  
00016717  00000-0  10270-3 0  9127
2 25544  51
6428 158
1731 0001927 109
6277 250
5084 15
54901214 13083


Satellite: ISS
Catalog Number: 25544
Epoch time:      16221
26706662   =   yrday
fracday
Element set:     912
Inclination:       51
6428  deg
RA of node:       158
1731  deg
Eccentricity:     
0001927     
Arg of perigee:   109
6277  deg
Mean anomaly:     250
5084  deg
Mean motion:   15
54901214  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1308
Checksum:              294


Coasting Arc #14 (Orbit 1323)
---------------------------------------

Vector Time (GMT): 2016/222/05:58:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1040299
44                 A    =         6775281
47  meter
 Y    =       -4134829
14  meter          E    =           
0004875
 Z    =        5261480
03                 I    =           51
78934
 XDOT =       7039
993320                 Wp   =           79
28777
 YDOT =      -2918
028326  meter/sec      RA   =          152
15396  deg
 ZDOT =       -899
647492                 TA   =           19
30239
                                          MA   =           19
28393
                                          Ha   =            220
512  n
mi
                                          Hp   =            212
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3413055
91                 X    =        -1019543
18
 Y    =      -13565712
41  feet           Y    =        -4146346
29  meter
 Z    =       17262073
59                 Z    =         5256477
07
 XDOT =      23097
090944                 XDOT =        7076
470282
 YDOT =      -9573
583747  feet/sec       YDOT =       -2839
098480  meter/sec
 ZDOT =      -2951
599382                 ZDOT =        -865
360635

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12301804
04                 X    =        -3749589
87
 Y    =       -6713722
39  feet           Y    =        -2046342
58  meter
 Z    =       17240888
54                 Z    =         5255022
83
 XDOT =       8350
816737                 XDOT =        2545
328941
 YDOT =     -22508
936643  feet/sec       YDOT =       -6860
723889  meter/sec
 ZDOT =      -2801
395382                 ZDOT =        -853
865313


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   16222
29538133  
00016717  00000-0  10270-3 0  9138
2 25544  51
6410 153
0413 0002037 110
9223 249
2148 15
54919986 13243


Satellite: ISS
Catalog Number: 25544
Epoch time:      16222
29538133   =   yrday
fracday
Element set:     913
Inclination:       51
6410  deg
RA of node:       153
0413  deg
Eccentricity:     
0002037     
Arg of perigee:   110
9223  deg
Mean anomaly:     249
2148  deg
Mean motion:   15
54919986  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1324
Checksum:              285


Coasting Arc #15 (Orbit 1338)
---------------------------------------

Vector Time (GMT): 2016/223/05:58:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -873445
45                 A    =         6778012
88  meter
 Y    =        4889854
71  meter          E    =           
0012157
 Z    =       -4623654
25                 I    =           51
82779
 XDOT =      -6857
859309                 Wp   =          110
65491
 YDOT =       1614
406513  meter/sec      RA   =          147
16159  deg
 ZDOT =       3005
062934                 TA   =          189
27129
                                          MA   =          189
29376
                                          Ha   =            220
413  n
mi
                                          Hp   =            212
816

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2865634
66                 X    =         -905600
59
 Y    =       16042830
40  feet           Y    =         4879907
40  meter
 Z    =      -15169469
32                 Z    =        -4627975
36
 XDOT =     -22499
538415                 XDOT =       -6889
999502
 YDOT =       5296
609295  feet/sec       YDOT =        1537
537682  meter/sec
 ZDOT =       9859
130361                 ZDOT =        2971
671359

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10023736
01                 X    =         3055234
74
 Y    =       12826225
19  feet           Y    =         3909433
44  meter
 Z    =      -15189132
05                 Z    =        -4629647
45
 XDOT =     -10297
495194                 XDOT =       -3138
676535
 YDOT =      19541
380092  feet/sec       YDOT =        5956
212652  meter/sec
 ZDOT =       9713
029114                 ZDOT =        2960
531274


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   16223
25942410  
00016717  00000-0  10270-3 0  9143
2 25544  51
6424 148
2305 0001821 112
5213 247
6133 15
54899461 13398


Satellite: ISS
Catalog Number: 25544
Epoch time:      16223
25942410   =   yrday
fracday
Element set:     914
Inclination:       51
6424  deg
RA of node:       148
2305  deg
Eccentricity:     
0001821     
Arg of perigee:   112
5213  deg
Mean anomaly:     247
6133  deg
Mean motion:   15
54899461  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1339
Checksum:              285


Coasting Arc #16 (Orbit 1340)
---------------------------------------

Vector Time (GMT): 2016/223/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5605437
41                 A    =         6780967
47  meter
 Y    =         -95255
82  meter          E    =           
0007624
 Z    =       -3821764
68                 I    =           51
83822
 XDOT =      -2764
701392                 Wp   =           84
90767
 YDOT =       5777
740654  meter/sec      RA   =          146
63457  deg
 ZDOT =      -4205
587313                 TA   =          140
84887
                                          MA   =          140
79368
                                          Ha   =            220
443  n
mi
                                          Hp   =            212
898

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18390542
69                 X    =         5624650
31
 Y    =        -312519
11  feet           Y    =          -32464
70  meter
 Z    =      -12538598
02                 Z    =        -3794488
42
 XDOT =      -9070
542624                 XDOT =       -2808
675306
 YDOT =      18955
842040  feet/sec       YDOT =        5746
577986  meter/sec
 ZDOT =     -13797
858639                 ZDOT =       -4219
124313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -123396
89                 X    =          -37611
37
 Y    =      -18473445
92  feet           Y    =        -5630706
32  meter
 Z    =      -12419449
99                 Z    =        -3785448
36
 XDOT =      17513
974072                 XDOT =        5338
259297
 YDOT =       9184
913464  feet/sec       YDOT =        2799
561624  meter/sec
 ZDOT =     -13857
917305                 ZDOT =       -4223
893195


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   16223
38796391  
00016717  00000-0  10270-3 0  9153
2 25544  51
6399 147
5883 0001858 110
4645 249
6707 15
54915020 13410


Satellite: ISS
Catalog Number: 25544
Epoch time:      16223
38796391   =   yrday
fracday
Element set:     915
Inclination:       51
6399  deg
RA of node:       147
5883  deg
Eccentricity:     
0001858     
Arg of perigee:   110
4645  deg
Mean anomaly:     249
6707  deg
Mean motion:   15
54915020  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1341
Checksum:              327


Coasting Arc #17 (Orbit 1356)
---------------------------------------

Vector Time (GMT): 2016/224/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4464092
84                 A    =         6776859
58  meter
 Y    =       -1379827
02  meter          E    =           
0008511
 Z    =        4903756
52                 I    =           51
85098
 XDOT =       4395
146887                 Wp   =          120
13278
 YDOT =      -5833
219216  meter/sec      RA   =          141
65219  deg
 ZDOT =       2352
511892                 TA   =          306
88250
                                          MA   =          306
96048
                                          Ha   =            220
418  n
mi
                                          Hp   =            212
843

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14645973
87                 X    =        -4472151
63
 Y    =       -4526991
54  feet           Y    =        -1429792
54  meter
 Z    =       16088440
02                 Z    =         4882051
67
 XDOT =      14419
773250                 XDOT =        4448
621364
 YDOT =     -19137
858320  feet/sec       YDOT =       -5783
770745  meter/sec
 ZDOT =       7718
214868                 ZDOT =        2373
992146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4423612
64                 X    =        -1348317
13
 Y    =       14780538
64  feet           Y    =         4505108
18  meter
 Z    =       15993856
14                 Z    =         4874927
35
 XDOT =     -18158
069726                 XDOT =       -5534
579653
 YDOT =     -13914
568246  feet/sec       YDOT =       -4241
160401  meter/sec
 ZDOT =       7812
992890                 ZDOT =        2381
400233


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   16224
41627296  
00016717  00000-0  10270-3 0  9166
2 25544  51
6397 142
4569 0001656 115
2689 244
8636 15
54942429 13578


Satellite: ISS
Catalog Number: 25544
Epoch time:      16224
41627296   =   yrday
fracday
Element set:     916
Inclination:       51
6397  deg
RA of node:       142
4569  deg
Eccentricity:     
0001656     
Arg of perigee:   115
2689  deg
Mean anomaly:     244
8636  deg
Mean motion:   15
54942429  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1357
Checksum:              338


Coasting Arc #18 (Orbit 1371)
---------------------------------------

Vector Time (GMT): 2016/225/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3004679
59                 A    =         6775095
04  meter
 Y    =        2923884
74  meter          E    =           
0016382
 Z    =       -5336196
69                 I    =           51
86943
 XDOT =      -5481
832939                 Wp   =           91
64689
 YDOT =       5344
649643  meter/sec      RA   =          136
66031  deg
 ZDOT =       -159
046725                 TA   =          176
84528
                                          MA   =          176
83493
                                          Ha   =            220
341  n
mi
                                          Hp   =            212
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9857872
67                 X    =         2997681
38
 Y    =        9592797
71  feet           Y    =         2957445
99  meter
 Z    =      -17507207
00                 Z    =        -5321617
81
 XDOT =     -17985
016204                 XDOT =       -5540
418169
 YDOT =      17534
939772  feet/sec       YDOT =        5283
020554  meter/sec
 ZDOT =       -521
806841                 ZDOT =        -185
818116

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9348098
55                 X    =         2849300
44
 Y    =      -10199102
36  feet           Y    =        -3108686
40  meter
 Z    =      -17443998
48                 Z    =        -5316930
74
 XDOT =      17219
456482                 XDOT =        5248
490336
 YDOT =      16871
729780  feet/sec       YDOT =        5142
503237  meter/sec
 ZDOT =       -639
637382                 ZDOT =        -194
961474


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   16225
38031344  
00016717  00000-0  10270-3 0  9177
2 25544  51
6396 137
6452 0001701 116
7524 243
3803 15
54910646 13722


Satellite: ISS
Catalog Number: 25544
Epoch time:      16225
38031344   =   yrday
fracday
Element set:     917
Inclination:       51
6396  deg
RA of node:       137
6452  deg
Eccentricity:     
0001701     
Arg of perigee:   116
7524  deg
Mean anomaly:     243
3803  deg
Mean motion:   15
54910646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1372
Checksum:              293


Coasting Arc #19 (Orbit 1387)
---------------------------------------

Vector Time (GMT): 2016/226/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1399975
58                 A    =         6776376
08  meter
 Y    =       -4336714
93  meter          E    =           
0006820
 Z    =        5010471
92                 I    =           51
89801
 XDOT =       6001
101938                 Wp   =           69
12070
 YDOT =      -4317
796360  meter/sec      RA   =          131
67029  deg
 ZDOT =      -2055
794686                 TA   =           40
80935
                                          MA   =           40
75829
                                          Ha   =            220
343  n
mi
                                          Hp   =            212
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4593095
72                 X    =        -1375715
74
 Y    =      -14228067
35  feet           Y    =        -4352234
83  meter
 Z    =       16438556
18                 Z    =         5003730
12
 XDOT =      19688
654652                 XDOT =        6058
924673
 YDOT =     -14165
998558  feet/sec       YDOT =       -4250
364687  meter/sec
 ZDOT =      -6744
733222                 ZDOT =       -2026
502778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14020379
76                 X    =        -4273411
75
 Y    =        5282740
88  feet           Y    =         1610179
42  meter
 Z    =       16409818
97                 Z    =         5001712
82
 XDOT =     -14584
130684                 XDOT =       -4445
243033
 YDOT =     -18107
607553  feet/sec       YDOT =       -5519
198782  meter/sec
 ZDOT =      -6616
040202                 ZDOT =       -2016
569053


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   16226
40861976  
00016717  00000-0  10270-3 0  9184
2 25544  51
6408 132
5135 0001631 120
4829 239
6485 15
54924596 13880


Satellite: ISS
Catalog Number: 25544
Epoch time:      16226
40861976   =   yrday
fracday
Element set:     918
Inclination:       51
6408  deg
RA of node:       132
5135  deg
Eccentricity:     
0001631     
Arg of perigee:   120
4829  deg
Mean anomaly:     239
6485  deg
Mean motion:   15
54924596  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1388
Checksum:              328
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