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

 
Date: September 4th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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


246/19:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 215 3

250/21:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 8
000/00:00:00 000 0 0 0 0 215 0

250/21:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 7
000/00:00:00 000 0 0 0 0 215 1

254/00:41:33 991 3 4 3 8 3 9
N/A -1 5 -0 4 220 0
000/00:11:03 983 -0 9 0 1 217 1

257/20:34:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 216 8

Coasting Arc #1 (Orbit 1700)
---------------------------------------

Vector Time (GMT): 2016/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4119186
39                 A    =         6785937
52  meter
 Y    =       -4802336
93  meter          E    =           
0003257
 Z    =       -2449264
42                 I    =           51
85111
 XDOT =       5202
780504                 Wp   =          158
91794
 YDOT =      -1733
469033  meter/sec      RA   =           31
67643  deg
 ZDOT =      -5356
378118                 TA   =           48
40868
                                          MA   =           48
38077
                                          Ha   =            219
511  n
mi
                                          Hp   =            215
272

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13514391
03                 X    =        -4053281
94
 Y    =      -15755698
60  feet           Y    =        -4848032
22  meter
 Z    =       -8035644
42                 Z    =        -2469113
55
 XDOT =      17069
489844                 XDOT =        5247
796621
 YDOT =      -5687
234360  feet/sec       YDOT =       -1675
036976  meter/sec
 ZDOT =     -17573
419022                 ZDOT =       -5330
995045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7670579
44                 X    =         2337992
61
 Y    =       19252428
37  feet           Y    =         5868140
17  meter
 Z    =       -8121489
86                 Z    =        -2475430
11
 XDOT =     -16695
507201                 XDOT =       -5088
790595
 YDOT =       -707
342294  feet/sec       YDOT =        -215
597931  meter/sec
 ZDOT =     -17462
141797                 ZDOT =       -5322
460820


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   16246
52721698  
00016717  00000-0  10270-3 0  9006
2 25544  51
6415  32
1269 0002931 280
0688  80
0134 15
54400533 17019


Satellite: ISS
Catalog Number: 25544
Epoch time:      16246
52721698   =   yrday
fracday
Element set:     900
Inclination:       51
6415  deg
RA of node:        32
1269  deg
Eccentricity:     
0002931     
Arg of perigee:   280
0688  deg
Mean anomaly:      80
0134  deg
Mean motion:   15
54400533  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1701
Checksum:              279


Coasting Arc #2 (Orbit 1705)
---------------------------------------

Vector Time (GMT): 2016/246/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         436476
07                 A    =         6777426
08  meter
 Y    =       -4412765
73  meter          E    =           
0011027
 Z    =       -5135329
83                 I    =           51
81605
 XDOT =       7025
549506                 Wp   =           70
45031
 YDOT =       2585
976190  meter/sec      RA   =           30
03221  deg
 ZDOT =      -1624
223596                 TA   =          183
89650
                                          MA   =          183
90510
                                          Ha   =            219
576  n
mi
                                          Hp   =            215
328

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1432008
12                 X    =          510733
29
 Y    =      -14477577
84  feet           Y    =        -4407470
17  meter
 Z    =      -16848195
00                 Z    =        -5133028
68
 XDOT =      23049
703103                 XDOT =        7004
000017
 YDOT =       8484
173853  feet/sec       YDOT =        2664
419909  meter/sec
 ZDOT =      -5328
817573                 ZDOT =       -1590
148206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14521486
25                 X    =         4426149
01
 Y    =       -1069792
04  feet           Y    =         -326072
61  meter
 Z    =      -16837296
82                 Z    =        -5132008
07
 XDOT =      -4302
564665                 XDOT =       -1311
421710
 YDOT =      23168
812545  feet/sec       YDOT =        7061
854064  meter/sec
 ZDOT =      -5180
372949                 ZDOT =       -1578
977675


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   16246
84867208  
00016717  00000-0  10270-3 0  9010
2 25544  51
6441  30
5281 0002982 285
6684  74
4140 15
54387475 17065


Satellite: ISS
Catalog Number: 25544
Epoch time:      16246
84867208   =   yrday
fracday
Element set:     901
Inclination:       51
6441  deg
RA of node:        30
5281  deg
Eccentricity:     
0002982     
Arg of perigee:   285
6684  deg
Mean anomaly:      74
4140  deg
Mean motion:   15
54387475  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1706
Checksum:              319


Coasting Arc #3 (Orbit 1721)
---------------------------------------

Vector Time (GMT): 2016/247/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2188457
52                 A    =         6776585
81  meter
 Y    =        3594158
19  meter          E    =           
0001965
 Z    =        5311990
77                 I    =           51
78333
 XDOT =      -6795
965989                 Wp   =          356
09208
 YDOT =      -3530
523213  meter/sec      RA   =           25
04114  deg
 ZDOT =       -409
131794                 TA   =           97
81244
                                          MA   =           97
79012
                                          Ha   =            219
726  n
mi
                                          Hp   =            215
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7179978
74                 X    =        -2254288
88
 Y    =       11791857
58  feet           Y    =         3569317
95  meter
 Z    =       17427791
25                 Z    =         5301199
53
 XDOT =     -22296
476341                 XDOT =       -6753
994317
 YDOT =     -11583
081408  feet/sec       YDOT =       -3606
285630  meter/sec
 ZDOT =      -1342
295912                 ZDOT =        -442
042332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12991516
24                 X    =        -3959814
15
 Y    =       -4846239
51  feet           Y    =        -1477133
80  meter
 Z    =       17379941
77                 Z    =         5297406
25
 XDOT =       6649
164167                 XDOT =        2026
665238
 YDOT =     -23174
418082  feet/sec       YDOT =       -7063
562632  meter/sec
 ZDOT =      -1485
455469                 ZDOT =        -452
766827


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   16247
87732410  
00016717  00000-0  10270-3 0  9021
2 25544  51
6424  25
3986 0002862 291
8435  68
2414 15
54413265 17220


Satellite: ISS
Catalog Number: 25544
Epoch time:      16247
87732410   =   yrday
fracday
Element set:     902
Inclination:       51
6424  deg
RA of node:        25
3986  deg
Eccentricity:     
0002862     
Arg of perigee:   291
8435  deg
Mean anomaly:      68
2414  deg
Mean motion:   15
54413265  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1722
Checksum:              305


Coasting Arc #4 (Orbit 1736)
---------------------------------------

Vector Time (GMT): 2016/248/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3857686
39                 A    =         6778501
09  meter
 Y    =       -2692671
53  meter          E    =           
0008722
 Z    =       -4888248
13                 I    =           51
76111
 XDOT =       5954
711104                 Wp   =          104
10910
 YDOT =       4183
456216  meter/sec      RA   =           20
04998  deg
 ZDOT =       2396
381168                 TA   =          189
34932
                                          MA   =          189
36557
                                          Ha   =            219
659  n
mi
                                          Hp   =            215
367

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12656451
40                 X    =         3911254
76
 Y    =       -8834224
18  feet           Y    =        -2649233
35  meter
 Z    =      -16037559
48                 Z    =        -4869378
08
 XDOT =      19536
453754                 XDOT =        5895
847508
 YDOT =      13725
250051  feet/sec       YDOT =        4249
716939  meter/sec
 ZDOT =       7862
142941                 ZDOT =        2425
164126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11343581
47                 X    =         3457523
63
 Y    =       10592788
41  feet           Y    =         3228681
91  meter
 Z    =      -15954578
85                 Z    =        -4862955
63
 XDOT =      -8503
041428                 XDOT =       -2591
727027
 YDOT =      21128
224941  feet/sec       YDOT =        6439
882962  meter/sec
 ZDOT =       7987
125059                 ZDOT =        2434
475718


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   16248
84167451  
00016717  00000-0  10270-3 0  9037
2 25544  51
6435  20
5903 0003124 295
6796  64
4034 15
54407519 17379


Satellite: ISS
Catalog Number: 25544
Epoch time:      16248
84167451   =   yrday
fracday
Element set:     903
Inclination:       51
6435  deg
RA of node:        20
5903  deg
Eccentricity:     
0003124     
Arg of perigee:   295
6796  deg
Mean anomaly:      64
4034  deg
Mean motion:   15
54407519  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1737
Checksum:              310


Coasting Arc #5 (Orbit 1752)
---------------------------------------

Vector Time (GMT): 2016/249/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5279349
73                 A    =         6782058
48  meter
 Y    =        1745997
85  meter          E    =           
0009234
 Z    =        3878097
60                 I    =           51
74212
 XDOT =      -4554
649390                 Wp   =           68
74497
 YDOT =      -4591
874311  meter/sec      RA   =           15
06426  deg
 ZDOT =      -4121
833093                 TA   =           64
49384
                                          MA   =           64
39837
                                          Ha   =            219
749  n
mi
                                          Hp   =            215
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17320701
22                 X    =        -5317319
68
 Y    =        5728339
41  feet           Y    =         1686748
75  meter
 Z    =       12723417
33                 Z    =         3852359
43
 XDOT =     -14943
075428                 XDOT =       -4482
941283
 YDOT =     -15065
204433  feet/sec       YDOT =       -4642
406960  meter/sec
 ZDOT =     -13523
074452                 ZDOT =       -4143
783764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9564285
53                 X    =        -2915194
23
 Y    =      -15626990
65  feet           Y    =        -4763106
75  meter
 Z    =       12610611
31                 Z    =         3843714
33
 XDOT =      10122
491289                 XDOT =        3085
335345
 YDOT =     -17214
658234  feet/sec       YDOT =       -5247
027830  meter/sec
 ZDOT =     -13618
109498                 ZDOT =       -4150
799775


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   16249
87030267  
00016717  00000-0  10270-3 0  9046
2 25544  51
6427  15
4603 0003111 303
1355  56
9499 15
54473443 17530


Satellite: ISS
Catalog Number: 25544
Epoch time:      16249
87030267   =   yrday
fracday
Element set:     904
Inclination:       51
6427  deg
RA of node:        15
4603  deg
Eccentricity:     
0003111     
Arg of perigee:   303
1355  deg
Mean anomaly:      56
9499  deg
Mean motion:   15
54473443  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1753
Checksum:              300


Coasting Arc #6 (Orbit 1767)
---------------------------------------

Vector Time (GMT): 2016/250/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6277716
10                 A    =         6785899
50  meter
 Y    =        -831175
88  meter          E    =           
0005905
 Z    =       -2430650
95                 I    =           51
72282
 XDOT =       2702
760504                 Wp   =           15
81979
 YDOT =       4774
176166  meter/sec      RA   =           10
08902  deg
 ZDOT =       5356
553666                 TA   =          317
02010
                                          MA   =          317
06622
                                          Ha   =            219
818  n
mi
                                          Hp   =            215
051

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20596181
42                 X    =         6298351
02
 Y    =       -2726954
98  feet           Y    =         -760859
12  meter
 Z    =       -7974576
62                 Z    =        -2400105
13
 XDOT =       8867
324487                 XDOT =        2623
153703
 YDOT =      15663
307631  feet/sec       YDOT =        4803
955672  meter/sec
 ZDOT =      17573
994966                 ZDOT =        5369
489187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7719616
25                 X    =         2352939
03
 Y    =       19343213
61  feet           Y    =         5895811
51  meter
 Z    =       -7840947
44                 Z    =        -2389920
78
 XDOT =     -11621
810022                 XDOT =       -3542
327695
 YDOT =      11772
777432  feet/sec       YDOT =        3588
342561  meter/sec
 ZDOT =      17629
593439                 ZDOT =        5373
500080


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   16250
83463265  
00016717  00000-0  10270-3 0  9053
2 25544  51
6419  10
6522 0003012 306
9814  53
1063 15
54473738 17688


Satellite: ISS
Catalog Number: 25544
Epoch time:      16250
83463265   =   yrday
fracday
Element set:     905
Inclination:       51
6419  deg
RA of node:        10
6522  deg
Eccentricity:     
0003012     
Arg of perigee:   306
9814  deg
Mean anomaly:      53
1063  deg
Mean motion:   15
54473738  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1768
Checksum:              295


Coasting Arc #7 (Orbit 1768)
---------------------------------------

Vector Time (GMT): 2016/250/21:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2158273
21                 A    =         6778455
79  meter
 Y    =       -4248855
61  meter          E    =           
0010211
 Z    =       -4830063
66                 I    =           51
69511
 XDOT =       7189
405578                 Wp   =           57
11014
 YDOT =       -775
014730  meter/sec      RA   =            9
88582  deg
 ZDOT =      -2529
237988                 TA   =          188
00071
                                          MA   =          188
01701
                                          Ha   =            219
773  n
mi
                                          Hp   =            215
005

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7080948
84                 X    =        -2087138
61
 Y    =      -13939814
99  feet           Y    =        -4272593
61  meter
 Z    =      -15846665
57                 Z    =        -4840374
83
 XDOT =      23587
288642                 XDOT =        7209
823628
 YDOT =      -2542
699245  feet/sec       YDOT =        -694
504068  meter/sec
 ZDOT =      -8298
024896                 ZDOT =       -2494
263931

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8176244
99                 X    =         2492119
47
 Y    =      -13274164
88  feet           Y    =        -4045965
46  meter
 Z    =      -15890898
42                 Z    =        -4843545
84
 XDOT =      13644
148873                 XDOT =        4158
736576
 YDOT =      18160
825749  feet/sec       YDOT =        5535
419688  meter/sec
 ZDOT =      -8145
058027                 ZDOT =       -2482
613687


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   16250
89892166  
00016717  00000-0  10270-3 0  9066
2 25544  51
6405  10
3305 0003149 307
5908  52
4959 15
54452126 17696


Satellite: ISS
Catalog Number: 25544
Epoch time:      16250
89892166   =   yrday
fracday
Element set:     906
Inclination:       51
6405  deg
RA of node:        10
3305  deg
Eccentricity:     
0003149     
Arg of perigee:   307
5908  deg
Mean anomaly:      52
4959  deg
Mean motion:   15
54452126  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1769
Checksum:              316


Coasting Arc #8 (Orbit 1769)
---------------------------------------

Vector Time (GMT): 2016/250/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894307
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1859597
36                 A    =         6777970
70  meter
 Y    =        4266353
53  meter          E    =           
0003148
 Z    =        4925682
59                 I    =           51
69292
 XDOT =      -7305
904919                 Wp   =          117
68319
 YDOT =        564
790951  meter/sec      RA   =            9
72198  deg
 ZDOT =       2266
477146                 TA   =          310
18194
                                          MA   =          310
20949
                                          Ha   =            219
657  n
mi
                                          Hp   =            215
097

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6101041
19                 X    =         1787824
81
 Y    =       13997222
86  feet           Y    =         4286747
98  meter
 Z    =       16160375
95                 Z    =         4934541
31
 XDOT =     -23969
504329                 XDOT =       -7322
687154
 YDOT =       1852
988686  feet/sec       YDOT =         482
997818  meter/sec
 ZDOT =       7435
948642                 ZDOT =        2230
946014

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6011790
87                 X    =        -1832393
86
 Y    =       13992050
68  feet           Y    =         4264777
05  meter
 Z    =       16198258
88                 Z    =         4937229
31
 XDOT =     -16873
660601                 XDOT =       -5143
091751
 YDOT =     -15688
071411  feet/sec       YDOT =       -4781
724166  meter/sec
 ZDOT =       7280
588635                 ZDOT =        2219
123416


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   16250
96320960  
00016717  00000-0  10270-3 0  9073
2 25544  51
6408  10
0103 0003317 306
2949  53
7897 15
54474660 17704


Satellite: ISS
Catalog Number: 25544
Epoch time:      16250
96320960   =   yrday
fracday
Element set:     907
Inclination:       51
6408  deg
RA of node:        10
0103  deg
Eccentricity:     
0003317     
Arg of perigee:   306
2949  deg
Mean anomaly:      53
7897  deg
Mean motion:   15
54474660  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1770
Checksum:              301


Coasting Arc #9 (Orbit 1784)
---------------------------------------

Vector Time (GMT): 2016/251/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894307
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          71232
83                 A    =         6776357
85  meter
 Y    =       -4214142
20  meter          E    =           
0012638
 Z    =       -5316897
86                 I    =           51
65576
 XDOT =       7643
597512                 Wp   =           77
89431
 YDOT =        438
487915  meter/sec      RA   =            4
72211  deg
 ZDOT =       -243
038385                 TA   =          189
77489
                                          MA   =          189
79950
                                          Ha   =            219
790  n
mi
                                          Hp   =            215
010

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         233703
51                 X    =          144178
40
 Y    =      -13825925
84  feet           Y    =        -4212938
23  meter
 Z    =      -17443890
61                 Z    =        -5316374
28
 XDOT =      25077
419658                 XDOT =        7639
306718
 YDOT =       1438
608645  feet/sec       YDOT =         523
939730  meter/sec
 ZDOT =       -797
370030                 ZDOT =        -205
918083

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10097689
65                 X    =         3077775
80
 Y    =       -9452819
84  feet           Y    =        -2881219
49  meter
 Z    =      -17440786
20                 Z    =        -5315951
63
 XDOT =      15880
180840                 XDOT =        4840
279120
 YDOT =      18148
334766  feet/sec       YDOT =        5531
612437  meter/sec
 ZDOT =       -635
270756                 ZDOT =        -193
630526


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   16251
92752660  
00016717  00000-0  10270-3 0  9087
2 25544  51
6411   5
2006 0003285 311
0938  48
9931 15
54475499 17854


Satellite: ISS
Catalog Number: 25544
Epoch time:      16251
92752660   =   yrday
fracday
Element set:     908
Inclination:       51
6411  deg
RA of node:         5
2006  deg
Eccentricity:     
0003285     
Arg of perigee:   311
0938  deg
Mean anomaly:      48
9931  deg
Mean motion:   15
54475499  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1785
Checksum:              315


Coasting Arc #10 (Orbit 1800)
---------------------------------------

Vector Time (GMT): 2016/252/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894307
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2035255
67                 A    =         6777405
78  meter
 Y    =        4018975
84  meter          E    =           
0006015
 Z    =        5063126
61                 I    =           51
62797
 XDOT =      -7316
586901                 Wp   =           21
29495
 YDOT =      -1405
001591  meter/sec      RA   =          359
71943  deg
 ZDOT =      -1819
677220                 TA   =           86
35568
                                          MA   =           86
28689
                                          Ha   =            219
907  n
mi
                                          Hp   =            214
923

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6677348
01                 X    =        -2104640
15
 Y    =       13185616
28  feet           Y    =         3995828
69  meter
 Z    =       16611307
76                 Z    =         5053070
99
 XDOT =     -24004
550199                 XDOT =       -7291
492808
 YDOT =      -4609
585273  feet/sec       YDOT =       -1486
680398  meter/sec
 ZDOT =      -5970
069618                 ZDOT =       -1855
158365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14079514
61                 X    =        -4291436
05
 Y    =        4658130
93  feet           Y    =         1419798
31  meter
 Z    =       16566595
41                 Z    =         5049498
28
 XDOT =     -13533
612334                 XDOT =       -4125
045039
 YDOT =     -19051
328247  feet/sec       YDOT =       -5806
844850  meter/sec
 ZDOT =      -6124
810777                 ZDOT =       -1866
842325


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   16252
95611528  
00016717  00000-0  10270-3 0  9099
2 25544  51
6418    
0706 0003405 315
8830  44
2051 15
54506315 18011


Satellite: ISS
Catalog Number: 25544
Epoch time:      16252
95611528   =   yrday
fracday
Element set:     909
Inclination:       51
6418  deg
RA of node:          
0706  deg
Eccentricity:     
0003405     
Arg of perigee:   315
8830  deg
Mean anomaly:      44
2051  deg
Mean motion:   15
54506315  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1801
Checksum:              274


Coasting Arc #11 (Orbit 1815)
---------------------------------------

Vector Time (GMT): 2016/253/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894307
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3806732
32                 A    =         6780757
46  meter
 Y    =       -3707313
43  meter          E    =           
0005207
 Z    =       -4216726
02                 I    =           51
60637
 XDOT =       6317
930180                 Wp   =           89
06141
 YDOT =       2328
906065  meter/sec      RA   =          354
72135  deg
 ZDOT =       3660
073733                 TA   =          218
46109
                                          MA   =          218
49821
                                          Ha   =            219
982  n
mi
                                          Hp   =            214
911

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12489279
25                 X    =         3868388
55
 Y    =      -12163101
82  feet           Y    =        -3664399
55  meter
 Z    =      -13834402
97                 Z    =        -4198083
87
 XDOT =      20728
117390                 XDOT =        6273
639136
 YDOT =       7640
767930  feet/sec       YDOT =        2399
309995  meter/sec
 ZDOT =      12008
115922                 ZDOT =        3690
656919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17497445
84                 X    =         5333221
49
 Y    =        -170593
68  feet           Y    =          -51996
95  meter
 Z    =      -13752241
07                 Z    =        -4191683
08
 XDOT =       9712
318487                 XDOT =        2960
314675
 YDOT =      18478
802494  feet/sec       YDOT =        5632
339000  meter/sec
 ZDOT =      12141
272493                 ZDOT =        3700
659856


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   16253
92040360  
00016717  00000-0  10270-3 0  9109
2 25544  51
6412 355
2613 0003489 320
8220  39
2680 15
54514493 18162


Satellite: ISS
Catalog Number: 25544
Epoch time:      16253
92040360   =   yrday
fracday
Element set:     910
Inclination:       51
6412  deg
RA of node:       355
2613  deg
Eccentricity:     
0003489     
Arg of perigee:   320
8220  deg
Mean anomaly:      39
2680  deg
Mean motion:   15
54514493  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1816
Checksum:              285


Coasting Arc #12 (Orbit 1817)
---------------------------------------

Vector Time (GMT): 2016/254/00:47:05
983
Vector Time (MET): N/A
Weight (LBS)     : 893896
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -607044
21                 A    =         6778322
20  meter
 Y    =       -4173836
55  meter          E    =           
0010004
 Z    =       -5314793
25                 I    =           51
58974
 XDOT =       7605
620527                 Wp   =           79
29968
 YDOT =       -905
143611  meter/sec      RA   =          354
14025  deg
 ZDOT =       -156
300533                 TA   =          189
19915
                                          MA   =          189
21749
                                          Ha   =            219
950  n
mi
                                          Hp   =            217
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1991614
87                 X    =         -534509
22
 Y    =      -13693689
48  feet           Y    =        -4180219
72  meter
 Z    =      -17436985
73                 Z    =        -5317565
66
 XDOT =      24952
823250                 XDOT =        7615
936047
 YDOT =      -2969
631271  feet/sec       YDOT =        -820
034801  meter/sec
 ZDOT =       -512
797024                 ZDOT =        -119
329228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1977299
04                 X    =         -602680
75
 Y    =      -13681363
11  feet           Y    =        -4170079
48  meter
 Z    =      -17448287
16                 Z    =        -5318237
93
 XDOT =      23935
936886                 XDOT =        7295
673563
 YDOT =      -3005
018146  feet/sec       YDOT =        -915
929531  meter/sec
 ZDOT =       -351
105504                 ZDOT =        -107
016958


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   16254
04897831  
00016717  00000-0  10270-3 0  9117
2 25544  51
6435 354
6199 0005261 287
2984  72
7593 15
53796924 18189


Satellite: ISS
Catalog Number: 25544
Epoch time:      16254
04897831   =   yrday
fracday
Element set:     911
Inclination:       51
6435  deg
RA of node:       354
6199  deg
Eccentricity:     
0005261     
Arg of perigee:   287
2984  deg
Mean anomaly:      72
7593  deg
Mean motion:   15
53796924  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1818
Checksum:              350


Coasting Arc #13 (Orbit 1833)
---------------------------------------

Vector Time (GMT): 2016/255/00:47:05
983
Vector Time (MET): N/A
Weight (LBS)     : 893896
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1063356
91                 A    =         6779144
63  meter
 Y    =        4331574
02  meter          E    =           
0004974
 Z    =        5107266
67                 I    =           51
56073
 XDOT =      -7486
954394                 Wp   =          349
07284
 YDOT =        106
852948  meter/sec      RA   =          349
14068  deg
 ZDOT =      -1644
925762                 TA   =          116
85132
                                          MA   =          116
80047
                                          Ha   =            220
046  n
mi
                                          Hp   =            217
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3488703
79                 X    =        -1136523
48
 Y    =       14211200
84  feet           Y    =         4319274
08  meter
 Z    =       16756124
23                 Z    =         5101923
17
 XDOT =     -24563
498667                 XDOT =       -7479
602485
 YDOT =        350
567414  feet/sec       YDOT =          23
169810  meter/sec
 ZDOT =      -5396
738064                 ZDOT =       -1681
277560

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3249205
82                 X    =         -990357
93
 Y    =       14296215
11  feet           Y    =         4357486
37  meter
 Z    =       16731941
84                 Z    =         5099895
87
 XDOT =     -23469
733924                 XDOT =       -7153
574900
 YDOT =       1185
326069  feet/sec       YDOT =         361
287386  meter/sec
 ZDOT =      -5555
561465                 ZDOT =       -1693
335135


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   16255
07803273  
00016717  00000-0  10270-3 0  9129
2 25544  51
6433 349
4936 0005488 290
8269  69
2295 15
53838863 18342


Satellite: ISS
Catalog Number: 25544
Epoch time:      16255
07803273   =   yrday
fracday
Element set:     912
Inclination:       51
6433  deg
RA of node:       349
4936  deg
Eccentricity:     
0005488     
Arg of perigee:   290
8269  deg
Mean anomaly:      69
2295  deg
Mean motion:   15
53838863  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1834
Checksum:              345


Coasting Arc #14 (Orbit 1848)
---------------------------------------

Vector Time (GMT): 2016/256/00:47:05
983
Vector Time (MET): N/A
Weight (LBS)     : 893896
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2620212
89                 A    =         6781906
50  meter
 Y    =       -4410254
33  meter          E    =           
0003708
 Z    =       -4439642
05                 I    =           51
53953
 XDOT =       6875
919752                 Wp   =          103
16299
 YDOT =        768
551091  meter/sec      RA   =          344
14243  deg
 ZDOT =       3296
101217                 TA   =          200
14579
                                          MA   =          200
16042
                                          Ha   =            220
236  n
mi
                                          Hp   =            217
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8596498
98                 X    =         2690900
49
 Y    =      -14469338
35  feet           Y    =        -4380558
43  meter
 Z    =      -14565754
74                 Z    =        -4426741
78
 XDOT =      22558
791836                 XDOT =        6850
803631
 YDOT =       2521
493081  feet/sec       YDOT =         845
302030  meter/sec
 ZDOT =      10813
980370                 ZDOT =        3329
441473

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8081198
92                 X    =         2463149
43
 Y    =      -14819545
53  feet           Y    =        -4516997
48  meter
 Z    =      -14508551
02                 Z    =        -4422206
35
 XDOT =      21493
152555                 XDOT =        6551
112899
 YDOT =        995
702598  feet/sec       YDOT =         303
490152  meter/sec
 ZDOT =      10959
472966                 ZDOT =        3340
447360


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   16256
04275874  
00016717  00000-0  10270-3 0  9138
2 25544  51
6444 344
6865 0005461 295
2853  64
7733 15
53831620 18498


Satellite: ISS
Catalog Number: 25544
Epoch time:      16256
04275874   =   yrday
fracday
Element set:     913
Inclination:       51
6444  deg
RA of node:       344
6865  deg
Eccentricity:     
0005461     
Arg of perigee:   295
2853  deg
Mean anomaly:      64
7733  deg
Mean motion:   15
53831620  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1849
Checksum:              330


Coasting Arc #15 (Orbit 1864)
---------------------------------------

Vector Time (GMT): 2016/257/00:47:05
983
Vector Time (MET): N/A
Weight (LBS)     : 893896
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3976269
80                 A    =         6785498
10  meter
 Y    =        4359958
32  meter          E    =           
0008306
 Z    =        3345703
20                 I    =           51
52031
 XDOT =      -5836
142201                 Wp   =           73
42762
 YDOT =      -1739
116743  meter/sec      RA   =          339
15166  deg
 ZDOT =      -4657
824691                 TA   =           67
51834
                                          MA   =           67
43042
                                          Ha   =            220
410  n
mi
                                          Hp   =            216
870

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13045504
59                 X    =        -4040980
30
 Y    =       14304325
19  feet           Y    =         4315131
47  meter
 Z    =       10976716
52                 Z    =         3326230
08
 XDOT =     -19147
448166                 XDOT =       -5793
635665
 YDOT =      -5705
763591  feet/sec       YDOT =       -1804
143118  meter/sec
 ZDOT =     -15281
577071                 ZDOT =       -4686
071604

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12252850
76                 X    =        -3734668
91
 Y    =       15051409
55  feet           Y    =         4587669
63  meter
 Z    =       10890818
77                 Z    =         3319521
56
 XDOT =     -18253
099536                 XDOT =       -5563
544739
 YDOT =      -3684
305306  feet/sec       YDOT =       -1122
976257  meter/sec
 ZDOT =     -15404
629758                 ZDOT =       -4695
331150


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   16257
07178585  
00016717  00000-0  10270-3 0  9144
2 25544  51
6439 339
5601 0005330 300
0835  59
9789 15
53840367 18656


Satellite: ISS
Catalog Number: 25544
Epoch time:      16257
07178585   =   yrday
fracday
Element set:     914
Inclination:       51
6439  deg
RA of node:       339
5601  deg
Eccentricity:     
0005330     
Arg of perigee:   300
0835  deg
Mean anomaly:      59
9789  deg
Mean motion:   15
53840367  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1865
Checksum:              334


Coasting Arc #16 (Orbit 1877)
---------------------------------------

Vector Time (GMT): 2016/257/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893896
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3344213
57                 A    =         6778827
20  meter
 Y    =        2936129
67  meter          E    =           
0000771
 Z    =        5114119
06                 I    =           51
47185
 XDOT =      -6171
975584                 Wp   =          281
26655
 YDOT =       4263
279948  meter/sec      RA   =          335
07367  deg
 ZDOT =       1588
672156                 TA   =          153
37746
                                          MA   =          153
37350
                                          Ha   =            220
309  n
mi
                                          Hp   =            216
794

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10971829
29                 X    =         3286290
49
 Y    =        9632971
35  feet           Y    =         2973203
55  meter
 Z    =       16778605
84                 Z    =         5130223
29
 XDOT =     -20249
263727                 XDOT =       -6226
906971
 YDOT =      13987
138937  feet/sec       YDOT =        4193
953800  meter/sec
 ZDOT =       5212
178989                 ZDOT =        1558
556653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2686708
94                 X    =         -818908
88
 Y    =       14269203
84  feet           Y    =         4349253
33  meter
 Z    =       16848388
82                 Z    =         5135388
91
 XDOT =     -21378
855367                 XDOT =       -6516
275116
 YDOT =     -10022
019979  feet/sec       YDOT =       -3054
711689  meter/sec
 ZDOT =       5079
822504                 ZDOT =        1548
329899


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   16257
90785819  
00016717  00000-0  10270-3 0  9151
2 25544  51
6416 335
3930 0005529 302
1411  57
9204 15
53892804 18780


Satellite: ISS
Catalog Number: 25544
Epoch time:      16257
90785819   =   yrday
fracday
Element set:     915
Inclination:       51
6416  deg
RA of node:       335
3930  deg
Eccentricity:     
0005529     
Arg of perigee:   302
1411  deg
Mean anomaly:      57
9204  deg
Mean motion:   15
53892804  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1878
Checksum:              325


Coasting Arc #17 (Orbit 1892)
---------------------------------------

Vector Time (GMT): 2016/258/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893896
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1876829
19                 A    =         6778111
30  meter
 Y    =       -3795814
29  meter          E    =           
0010748
 Z    =       -5301550
07                 I    =           51
44085
 XDOT =       6728
194997                 Wp   =           74
97149
 YDOT =      -3655
276798  meter/sec      RA   =          330
06384  deg
 ZDOT =        238
364379                 TA   =          197
29065
                                          MA   =          197
32728
                                          Ha   =            220
554  n
mi
                                          Hp   =            216
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6157576
07                 X    =        -1808491
49
 Y    =      -12453458
94  feet           Y    =        -3816420
79  meter
 Z    =      -17393536
98                 Z    =        -5310500
72
 XDOT =      22074
130567                 XDOT =        6767
411316
 YDOT =     -11992
377946  feet/sec       YDOT =       -3579
818311  meter/sec
 ZDOT =        782
035365                 ZDOT =         271
143693

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7381153
69                 X    =         2249775
64
 Y    =      -11712663
00  feet           Y    =        -3570019
68  meter
 Z    =      -17431913
46                 Z    =        -5313247
22
 XDOT =      20987
249572                 XDOT =        6396
913670
 YDOT =      11863
131609  feet/sec       YDOT =        3615
882514  meter/sec
 ZDOT =        925
897486                 ZDOT =         282
213554


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   16258
87254929  
00016717  00000-0  10270-3 0  9162
2 25544  51
6420 330
5857 0005506 306
5722  53
4923 15
53877145 18935


Satellite: ISS
Catalog Number: 25544
Epoch time:      16258
87254929   =   yrday
fracday
Element set:     916
Inclination:       51
6420  deg
RA of node:       330
5857  deg
Eccentricity:     
0005506     
Arg of perigee:   306
5722  deg
Mean anomaly:      53
4923  deg
Mean motion:   15
53877145  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1893
Checksum:              331


Coasting Arc #18 (Orbit 1908)
---------------------------------------

Vector Time (GMT): 2016/259/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893896
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         363843
83                 A    =         6779504
06  meter
 Y    =        4590028
67  meter          E    =           
0007092
 Z    =        4977401
02                 I    =           51
41822
 XDOT =      -6842
472947                 Wp   =            8
03422
 YDOT =       2780
181270  meter/sec      RA   =          325
05385  deg
 ZDOT =      -2056
387471                 TA   =          102
07271
                                          MA   =          101
99324
                                          Ha   =            220
766  n
mi
                                          Hp   =            216
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1193713
36                 X    =          288311
98
 Y    =       15059149
18  feet           Y    =         4593675
77  meter
 Z    =       16330055
84                 Z    =         4978984
39
 XDOT =     -22449
058226                 XDOT =       -6863
064103
 YDOT =       9121
329625  feet/sec       YDOT =        2703
548735  meter/sec
 ZDOT =      -6746
678055                 ZDOT =       -2089
676699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12057684
41                 X    =        -3675182
21
 Y    =        9089409
63  feet           Y    =         2770452
05  meter
 Z    =       16336111
19                 Z    =         4979246
69
 XDOT =     -19159
573005                 XDOT =       -5839
837852
 YDOT =     -12985
871933  feet/sec       YDOT =       -3958
093765  meter/sec
 ZDOT =      -6892
587877                 ZDOT =       -2100
860785


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   16259
90154025  
00016717  00000-0  10270-3 0  9174
2 25544  51
6421 325
4590 0005515 311
7239  48
3441 15
53892355 19090


Satellite: ISS
Catalog Number: 25544
Epoch time:      16259
90154025   =   yrday
fracday
Element set:     917
Inclination:       51
6421  deg
RA of node:       325
4590  deg
Eccentricity:     
0005515     
Arg of perigee:   311
7239  deg
Mean anomaly:      48
3441  deg
Mean motion:   15
53892355  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1909
Checksum:              308


Coasting Arc #19 (Orbit 1923)
---------------------------------------

Vector Time (GMT): 2016/260/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893896
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1038574
38                 A    =         6782552
91  meter
 Y    =       -5233106
92  meter          E    =           
0003706
 Z    =       -4190054
95                 I    =           51
40182
 XDOT =       6524
405662                 Wp   =           68
83939
 YDOT =      -1641
950304  meter/sec      RA   =          320
04753  deg
 ZDOT =       3671
811920                 TA   =          238
94702
                                          MA   =          238
98341
                                          Ha   =            220
875  n
mi
                                          Hp   =            216
374

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3407396
27                 X    =         1117368
59
 Y    =      -17168985
97  feet           Y    =        -5221052
94  meter
 Z    =      -13746899
44                 Z    =        -4184817
68
 XDOT =      21405
530388                 XDOT =        6524
445401
 YDOT =      -5386
976062  feet/sec       YDOT =       -1568
989265  meter/sec
 ZDOT =      12046
627034                 ZDOT =        3703
506139

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16205745
09                 X    =         4939511
10
 Y    =       -6664326
66  feet           Y    =        -2031286
77  meter
 Z    =      -13723055
39                 Z    =        -4182787
28
 XDOT =      15870
141419                 XDOT =        4837
219105
 YDOT =      13526
502192  feet/sec       YDOT =        4122
877868  meter/sec
 ZDOT =      12185
345173                 ZDOT =        3714
093209


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   16260
86620877  
00016717  00000-0  10270-3 0  9185
2 25544  51
6412 320
6522 0005555 315
3580  44
7125 15
53908399 19247


Satellite: ISS
Catalog Number: 25544
Epoch time:      16260
86620877   =   yrday
fracday
Element set:     918
Inclination:       51
6412  deg
RA of node:       320
6522  deg
Eccentricity:     
0005555     
Arg of perigee:   315
3580  deg
Mean anomaly:      44
7125  deg
Mean motion:   15
53908399  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1924
Checksum:              316
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