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

 
Date: October 17th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15281 523 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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


291/23:40:36 600 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 212 0

293/08:05:14 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 211 9

294/03:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 211 9

295/09:59:09 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 211 9

297/11:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 212 0

304/00:37:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 1

304/02:12:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 1

Coasting Arc #1 (Orbit 2400)
---------------------------------------

Vector Time (GMT): 2016/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 880841
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3842398
96                 A    =         6782453
49  meter
 Y    =       -4029571
53  meter          E    =           
0018042
 Z    =        3860105
10                 I    =           51
72016
 XDOT =       6175
783769                 Wp   =           80
35823
 YDOT =       1906
438496  meter/sec      RA   =          166
80777  deg
 ZDOT =      -4137
906015                 TA   =           53
10628
                                          MA   =           52
94107
                                          Ha   =            223
159  n
mi
                                          Hp   =            211
936

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12606295
80                 X    =         3868421
86
 Y    =      -13220379
03  feet           Y    =        -3986457
41  meter
 Z    =       12664386
82                 Z    =         3878834
56
 XDOT =      20261
757773                 XDOT =        6174
107181
 YDOT =       6254
719476  feet/sec       YDOT =        1975
490523  meter/sec
 ZDOT =     -13575
807137                 ZDOT =       -4107
909056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5593112
21                 X    =        -1704780
60
 Y    =       17329657
47  feet           Y    =         5282079
60  meter
 Z    =       12746916
35                 Z    =         3885260
10
 XDOT =     -19791
844147                 XDOT =       -6032
554096
 YDOT =       3548
227240  feet/sec       YDOT =        1081
499663  meter/sec
 ZDOT =     -13444
890234                 ZDOT =       -4098
002543


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   16291
54060130  
00016717  00000-0  10270-3 0  9005
2 25544  51
6428 167
7731 0006827  78
0372 282
1545 15
54288737 24014


Satellite: ISS
Catalog Number: 25544
Epoch time:      16291
54060130   =   yrday
fracday
Element set:     900
Inclination:       51
6428  deg
RA of node:       167
7731  deg
Eccentricity:     
0006827     
Arg of perigee:    78
0372  deg
Mean anomaly:     282
1545  deg
Mean motion:   15
54288737  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2401
Checksum:              303


Coasting Arc #2 (Orbit 2407)
---------------------------------------

Vector Time (GMT): 2016/291/23:40:36
600
Vector Time (MET): N/A
Weight (LBS)     : 880841
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5592949
23                 A    =         6787123
14  meter
 Y    =        3246812
35  meter          E    =           
0012311
 Z    =       -2057450
11                 I    =           51
74901
 XDOT =      -4019
772406                 Wp   =           62
77544
 YDOT =      -3423
982728  meter/sec      RA   =          164
38963  deg
 ZDOT =       5555
023700                 TA   =          274
51541
                                          MA   =          274
65604
                                          Ha   =            223
225  n
mi
                                          Hp   =            212
010

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18349570
98                 X    =        -5618845
77
 Y    =       10652271
49  feet           Y    =         3184123
29  meter
 Z    =       -6750164
41                 Z    =        -2084683
11
 XDOT =     -13188
229678                 XDOT =       -4008
170418
 YDOT =     -11233
539133  feet/sec       YDOT =       -3468
869237  meter/sec
 ZDOT =      18225
143373                 ZDOT =        5535
524577

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13215391
20                 X    =        -4028051
24
 Y    =       16549983
00  feet           Y    =         5044434
82  meter
 Z    =       -6869778
77                 Z    =        -2093908
57
 XDOT =     -15260
131494                 XDOT =       -4651
288079
 YDOT =      -4697
004671  feet/sec       YDOT =       -1431
647024  meter/sec
 ZDOT =      18140
369625                 ZDOT =        5529
184662


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   16291
99067858  
00016717  00000-0  10270-3 0  9019
2 25544  51
6412 165
5267 0006705  82
6540 277
5374 15
54245574 24087


Satellite: ISS
Catalog Number: 25544
Epoch time:      16291
99067858   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:       165
5267  deg
Eccentricity:     
0006705     
Arg of perigee:    82
6540  deg
Mean anomaly:     277
5374  deg
Mean motion:   15
54245574  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2408
Checksum:              330


Coasting Arc #3 (Orbit 2423)
---------------------------------------

Vector Time (GMT): 2016/292/23:40:36
600
Vector Time (MET): N/A
Weight (LBS)     : 880841
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6254356
47                 A    =         6788809
46  meter
 Y    =       -2606571
88  meter          E    =           
0018236
 Z    =         307936
93                 I    =           51
78594
 XDOT =       2090
568683                 Wp   =          115
77637
 YDOT =       4273
825108  meter/sec      RA   =          159
42607  deg
 ZDOT =      -6015
214510                 TA   =           60
91110
                                          MA   =           60
72862
                                          Ha   =            223
286  n
mi
                                          Hp   =            211
865

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20519542
21                 X    =         6281543
11
 Y    =       -8551745
03  feet           Y    =        -2536479
45  meter
 Z    =        1010291
78                 Z    =          338385
94
 XDOT =       6858
821140                 XDOT =        2071
842333
 YDOT =      14021
735920  feet/sec       YDOT =        4297
098229  meter/sec
 ZDOT =     -19734
955742                 ZDOT =       -6005
104516

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15765382
78                 X    =         4805288
67
 Y    =      -15663615
45  feet           Y    =        -4774269
99  meter
 Z    =        1143897
56                 Z    =          348659
98
 XDOT =      10620
662588                 XDOT =        3237
177957
 YDOT =       9194
709416  feet/sec       YDOT =        2802
547430  meter/sec
 ZDOT =     -19691
380945                 ZDOT =       -6001
932912


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   16293
01942034  
00016717  00000-0  10270-3 0  9023
2 25544  51
6413 160
3970 0006919  85
3921 274
8022 15
54290066 24246


Satellite: ISS
Catalog Number: 25544
Epoch time:      16293
01942034   =   yrday
fracday
Element set:     902
Inclination:       51
6413  deg
RA of node:       160
3970  deg
Eccentricity:     
0006919     
Arg of perigee:    85
3921  deg
Mean anomaly:     274
8022  deg
Mean motion:   15
54290066  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2424
Checksum:              293


Coasting Arc #4 (Orbit 2428)
---------------------------------------

Vector Time (GMT): 2016/293/08:05:14
000
Vector Time (MET): N/A
Weight (LBS)     : 880841
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5252582
55                 A    =         6787238
09  meter
 Y    =        3824698
29  meter          E    =           
0012641
 Z    =       -1958966
95                 I    =           51
79009
 XDOT =      -4272
332062                 Wp   =           63
04502
 YDOT =      -3014
175560  meter/sec      RA   =          157
66896  deg
 ZDOT =       5603
931501                 TA   =          275
40156
                                          MA   =          275
54576
                                          Ha   =            223
273  n
mi
                                          Hp   =            211
906

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17232882
37                 X    =        -5285444
88
 Y    =       12548222
73  feet           Y    =         3765776
55  meter
 Z    =       -6427056
92                 Z    =        -1984563
27
 XDOT =     -14016
837473                 XDOT =       -4265
531364
 YDOT =      -9889
027429  feet/sec       YDOT =       -3061
913357  meter/sec
 ZDOT =      18385
602037                 ZDOT =        5583
193764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21208140
75                 X    =         6464241
30
 Y    =       -1784721
87  feet           Y    =         -543983
22  meter
 Z    =       -6539627
13                 Z    =        -1993278
35
 XDOT =       6807
191290                 XDOT =        2074
831905
 YDOT =      14247
430979  feet/sec       YDOT =        4342
616962  meter/sec
 ZDOT =      18295
337817                 ZDOT =        5576
418967


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   16293
34090182  
00016717  00000-0  10270-3 0  9038
2 25544  51
6402 158
7955 0006901  84
7200 275
4740 15
54265957 24292


Satellite: ISS
Catalog Number: 25544
Epoch time:      16293
34090182   =   yrday
fracday
Element set:     903
Inclination:       51
6402  deg
RA of node:       158
7955  deg
Eccentricity:     
0006901     
Arg of perigee:    84
7200  deg
Mean anomaly:     275
4740  deg
Mean motion:   15
54265957  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2429
Checksum:              314


Coasting Arc #5 (Orbit 2441)
---------------------------------------

Vector Time (GMT): 2016/294/03:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 880841
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3729823
40                 A    =         6784388
94  meter
 Y    =       -4660468
42  meter          E    =           
0019612
 Z    =        3206748
69                 I    =           51
80257
 XDOT =       5828
749139                 Wp   =           91
72187
 YDOT =       1338
453235  meter/sec      RA   =          153
67627  deg
 ZDOT =      -4809
526309                 TA   =           51
25159
                                          MA   =           51
07648
                                          Ha   =            223
191  n
mi
                                          Hp   =            211
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12236953
43                 X    =         3766083
43
 Y    =      -15290250
71  feet           Y    =        -4618556
16  meter
 Z    =       10520829
05                 Z    =         3224955
86
 XDOT =      19123
192714                 XDOT =        5836
712080
 YDOT =       4391
250771  feet/sec       YDOT =        1403
678557  meter/sec
 ZDOT =     -15779
285792                 ZDOT =       -4781
191851

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12370001
42                 X    =        -3770376
43
 Y    =      -15126796
14  feet           Y    =        -4610647
46  meter
 Z    =       10601214
24                 Z    =         3231250
10
 XDOT =       7253
296546                 XDOT =        2210
804787
 YDOT =     -16959
698118  feet/sec       YDOT =       -5169
315986  meter/sec
 ZDOT =     -15655
516301                 ZDOT =       -4771
801369


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   16294
17674582  
00016717  00000-0  10270-3 0  9043
2 25544  51
6382 154
6272 0006865  88
1475 272
0464 15
54304289 24420


Satellite: ISS
Catalog Number: 25544
Epoch time:      16294
17674582   =   yrday
fracday
Element set:     904
Inclination:       51
6382  deg
RA of node:       154
6272  deg
Eccentricity:     
0006865     
Arg of perigee:    88
1475  deg
Mean anomaly:     272
0464  deg
Mean motion:   15
54304289  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2442
Checksum:              327


Coasting Arc #6 (Orbit 2456)
---------------------------------------

Vector Time (GMT): 2016/295/03:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 880841
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4828640
36                 A    =         6787581
51  meter
 Y    =        4467642
50  meter          E    =           
0013077
 Z    =       -1667508
83                 I    =           51
84212
 XDOT =      -4375
737026                 Wp   =           64
67530
 YDOT =      -2606
747410  meter/sec      RA   =          148
71218  deg
 ZDOT =       5727
303667                 TA   =          277
11563
                                          MA   =          277
26431
                                          Ha   =            223
276  n
mi
                                          Hp   =            211
793

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15841995
93                 X    =        -4870139
63
 Y    =       14657619
74  feet           Y    =         4413413
30  meter
 Z    =       -5470829
51                 Z    =        -1691066
50
 XDOT =     -14356
092606                 XDOT =       -4374
083716
 YDOT =      -8552
320900  feet/sec       YDOT =       -2655
670379  meter/sec
 ZDOT =      18790
366363                 ZDOT =        5706
051206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11300238
64                 X    =         3444312
74
 Y    =       18356821
51  feet           Y    =         5595159
20  meter
 Z    =       -5574615
49                 Z    =        -1699142
80
 XDOT =      -9866
434811                 XDOT =       -3007
289330
 YDOT =      11712
242623  feet/sec       YDOT =        3569
891552  meter/sec
 ZDOT =      18697
769832                 ZDOT =        5699
080245


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   16295
14117818  
00016717  00000-0  10270-3 0  9056
2 25544  51
6385 149
8192 0007055  92
9867 267
2093 15
54306147 24575


Satellite: ISS
Catalog Number: 25544
Epoch time:      16295
14117818   =   yrday
fracday
Element set:     905
Inclination:       51
6385  deg
RA of node:       149
8192  deg
Eccentricity:     
0007055     
Arg of perigee:    92
9867  deg
Mean anomaly:     267
2093  deg
Mean motion:   15
54306147  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2457
Checksum:              335


Coasting Arc #7 (Orbit 2461)
---------------------------------------

Vector Time (GMT): 2016/295/09:59:09
000
Vector Time (MET): N/A
Weight (LBS)     : 895949
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1252839
67                 A    =         6777046
30  meter
 Y    =       -4095423
42  meter          E    =           
0009766
 Z    =        5244177
46                 I    =           51
81923
 XDOT =       6804
114560                 Wp   =           80
96862
 YDOT =      -3401
814405  meter/sec      RA   =          147
33633  deg
 ZDOT =      -1028
000041                 TA   =           18
85859
                                          MA   =           18
82244
                                          Ha   =            223
142  n
mi
                                          Hp   =            211
915

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4110366
38                 X    =        -1232424
83
 Y    =      -13436428
55  feet           Y    =        -4109319
17  meter
 Z    =       17205306
63                 Z    =         5238141
13
 XDOT =      22323
210498                 XDOT =        6846
642474
 YDOT =     -11160
808415  feet/sec       YDOT =       -3325
488483  meter/sec
 ZDOT =      -3372
703546                 ZDOT =        -994
843433

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4036750
85                 X    =         1230401
66
 Y    =       13491616
59  feet           Y    =         4112244
74  meter
 Z    =       17179529
22                 Z    =         5236320
51
 XDOT =     -21511
967898                 XDOT =       -6556
847815
 YDOT =      10558
738643  feet/sec       YDOT =        3218
303538  meter/sec
 ZDOT =      -3227
071344                 ZDOT =        -983
611346


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   16295
46265243  
00016717  00000-0  10270-3 0  9068
2 25544  51
6429 148
2171 0006610  92
7067 267
4842 15
54339470 24625


Satellite: ISS
Catalog Number: 25544
Epoch time:      16295
46265243   =   yrday
fracday
Element set:     906
Inclination:       51
6429  deg
RA of node:       148
2171  deg
Eccentricity:     
0006610     
Arg of perigee:    92
7067  deg
Mean anomaly:     267
4842  deg
Mean motion:   15
54339470  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2462
Checksum:              317


Coasting Arc #8 (Orbit 2476)
---------------------------------------

Vector Time (GMT): 2016/296/09:59:09
000
Vector Time (MET): N/A
Weight (LBS)     : 895949
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -357392
62                 A    =         6779529
11  meter
 Y    =        4912733
99  meter          E    =           
0017149
 Z    =       -4674618
24                 I    =           51
85383
 XDOT =      -6701
711799                 Wp   =          104
41117
 YDOT =       2280
114669  meter/sec      RA   =          142
35127  deg
 ZDOT =       2913
416055                 TA   =          194
50711
                                          MA   =          194
55640
                                          Ha   =            223
136  n
mi
                                          Hp   =            211
923

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1172547
96                 X    =         -389593
95
 Y    =       16117893
66  feet           Y    =         4908557
11  meter
 Z    =      -15336674
02                 Z    =        -4676432
83
 XDOT =     -21987
243435                 XDOT =       -6740
862826
 YDOT =       7480
691171  feet/sec       YDOT =        2204
952863  meter/sec
 ZDOT =       9558
451624                 ZDOT =        2880
765225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1017348
34                 X    =          310087
77
 Y    =      -16120143
35  feet           Y    =        -4913419
69  meter
 Z    =      -15345387
43                 Z    =        -4677274
09
 XDOT =      20847
129709                 XDOT =        6354
205135
 YDOT =      -7632
074050  feet/sec       YDOT =       -2326
256170  meter/sec
 ZDOT =       9415
187180                 ZDOT =        2869
749052


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   16296
42707498  
00016717  00000-0  10270-3 0  9079
2 25544  51
6427 143
4081 0006672  95
2886 264
9028 15
54318646 24771


Satellite: ISS
Catalog Number: 25544
Epoch time:      16296
42707498   =   yrday
fracday
Element set:     907
Inclination:       51
6427  deg
RA of node:       143
4081  deg
Eccentricity:     
0006672     
Arg of perigee:    95
2886  deg
Mean anomaly:     264
9028  deg
Mean motion:   15
54318646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2477
Checksum:              344


Coasting Arc #9 (Orbit 2492)
---------------------------------------

Vector Time (GMT): 2016/297/09:59:09
000
Vector Time (MET): N/A
Weight (LBS)     : 895949
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1842201
51                 A    =         6783314
73  meter
 Y    =       -5472305
43  meter          E    =           
0018712
 Z    =        3543393
58                 I    =           51
89136
 XDOT =       6153
559834                 Wp   =           91
49722
 YDOT =       -859
390277  meter/sec      RA   =          137
37772  deg
 ZDOT =      -4506
430480                 TA   =           46
84097
                                          MA   =           46
68471
                                          Ha   =            223
074  n
mi
                                          Hp   =            211
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6043968
22                 X    =         1886044
86
 Y    =      -17953757
96  feet           Y    =        -5451459
33  meter
 Z    =       11625307
04                 Z    =         3552449
45
 XDOT =      20188
844600                 XDOT =        6184
602933
 YDOT =      -2819
521905  feet/sec       YDOT =        -790
403741  meter/sec
 ZDOT =     -14784
876903                 ZDOT =       -4476
462268

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5596268
71                 X    =        -1705742
70
 Y    =       18072226
19  feet           Y    =         5508414
54  meter
 Z    =       11665811
48                 Z    =         3555739
34
 XDOT =     -18903
701898                 XDOT =       -5761
848339
 YDOT =       3647
503109  feet/sec       YDOT =        1111
758948  meter/sec
 ZDOT =     -14653
561082                 ZDOT =       -4466
405418


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   16297
45578440  
00016717  00000-0  10270-3 0  9087
2 25544  51
6423 138
2790 0006695  98
1554 262
0358 15
54350775 24937


Satellite: ISS
Catalog Number: 25544
Epoch time:      16297
45578440   =   yrday
fracday
Element set:     908
Inclination:       51
6423  deg
RA of node:       138
2790  deg
Eccentricity:     
0006695     
Arg of perigee:    98
1554  deg
Mean anomaly:     262
0358  deg
Mean motion:   15
54350775  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2493
Checksum:              338


Coasting Arc #10 (Orbit 2493)
---------------------------------------

Vector Time (GMT): 2016/297/11:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910476
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5710727
22                 A    =         6785079
21  meter
 Y    =        2093300
71  meter          E    =           
0019618
 Z    =        2989456
02                 I    =           51
89655
 XDOT =        501
929091                 Wp   =           88
17471
 YDOT =      -5803
488446  meter/sec      RA   =          137
19861  deg
 ZDOT =       4994
988446                 TA   =          305
91964
                                          MA   =          306
10154
                                          Ha   =            223
176  n
mi
                                          Hp   =            212
013

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18735981
69                 X    =        -5748232
25
 Y    =        6867784
49  feet           Y    =         2029230
01  meter
 Z    =        9807926
57                 Z    =         2961623
23
 XDOT =       1646
748985                 XDOT =         542
524122
 YDOT =     -19040
316425  feet/sec       YDOT =       -5797
648253  meter/sec
 ZDOT =      16387
757368                 ZDOT =        4997
525673

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15822663
76                 X    =         4822747
91
 Y    =      -12256761
78  feet           Y    =        -3735860
99  meter
 Z    =        9685762
73                 Z    =         2952220
48
 XDOT =       3424
323172                 XDOT =        1043
733703
 YDOT =      17452
784492  feet/sec       YDOT =        5319
608713  meter/sec
 ZDOT =      16399
780210                 ZDOT =        4998
653008


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   16297
52007852  
00016717  00000-0  10270-3 0  9090
2 25544  51
6410 137
9577 0006588  99
1008 261
0890 15
54319806 24949


Satellite: ISS
Catalog Number: 25544
Epoch time:      16297
52007852   =   yrday
fracday
Element set:     909
Inclination:       51
6410  deg
RA of node:       137
9577  deg
Eccentricity:     
0006588     
Arg of perigee:    99
1008  deg
Mean anomaly:     261
0890  deg
Mean motion:   15
54319806  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2494
Checksum:              333


Coasting Arc #11 (Orbit 2508)
---------------------------------------

Vector Time (GMT): 2016/298/11:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910476
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5203630
91                 A    =         6781036
14  meter
 Y    =        -715381
67  meter          E    =           
0014118
 Z    =       -4301648
66                 I    =           51
90593
 XDOT =      -2064
320923                 Wp   =           84
64524
 YDOT =       6447
806063  meter/sec      RA   =          132
23034  deg
 ZDOT =      -3578
275593                 TA   =          148
97291
                                          MA   =          148
88944
                                          Ha   =            223
051  n
mi
                                          Hp   =            212
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17072279
88                 X    =         5232139
51
 Y    =       -2347052
72  feet           Y    =         -657032
09  meter
 Z    =      -14113020
54                 Z    =        -4276301
17
 XDOT =      -6772
706441                 XDOT =       -2118
886610
 YDOT =      21154
219367  feet/sec       YDOT =        6424
416080  meter/sec
 ZDOT =     -11739
749321                 ZDOT =       -3588
436663

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15507440
98                 X    =        -4726668
01
 Y    =        7720986
88  feet           Y    =         2353356
80  meter
 Z    =      -14001942
05                 Z    =        -4267791
94
 XDOT =        132
841967                 XDOT =          40
490231
 YDOT =     -21052
843216  feet/sec       YDOT =       -6416
906612  meter/sec
 ZDOT =     -11785
256637                 ZDOT =       -3592
146223


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   16298
48448642  
00016717  00000-0  10270-3 0  9104
2 25544  51
6407 133
1484 0006468 103
0848 257
1027 15
54329768 25097


Satellite: ISS
Catalog Number: 25544
Epoch time:      16298
48448642   =   yrday
fracday
Element set:     910
Inclination:       51
6407  deg
RA of node:       133
1484  deg
Eccentricity:     
0006468     
Arg of perigee:   103
0848  deg
Mean anomaly:     257
1027  deg
Mean motion:   15
54329768  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2509
Checksum:              325


Coasting Arc #12 (Orbit 2524)
---------------------------------------

Vector Time (GMT): 2016/299/11:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910476
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4391638
23                 A    =         6777890
49  meter
 Y    =        -814637
75  meter          E    =           
0011908
 Z    =        5090009
25                 I    =           51
91626
 XDOT =       3322
311430                 Wp   =          114
61115
 YDOT =      -6684
050496  meter/sec      RA   =          127
25296  deg
 ZDOT =       1788
607772                 TA   =          318
12253
                                          MA   =          318
21356
                                          Ha   =            223
243  n
mi
                                          Hp   =            212
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14408261
92                 X    =        -4406927
72
 Y    =       -2672696
03  feet           Y    =         -863833
05  meter
 Z    =       16699505
42                 Z    =         5068638
46
 XDOT =      10899
971882                 XDOT =        3388
118877
 YDOT =     -21929
299528  feet/sec       YDOT =       -6646
530075  meter/sec
 ZDOT =       5868
135735                 ZDOT =        1804
907329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14568489
11                 X    =         4440475
48
 Y    =       -2369022
93  feet           Y    =         -722078
19  meter
 Z    =       16606072
76                 Z    =         5061530
98
 XDOT =      -3022
393244                 XDOT =        -921
225461
 YDOT =      23242
541366  feet/sec       YDOT =        7084
326608  meter/sec
 ZDOT =       5940
566718                 ZDOT =        1810
684736


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   16299
51318177  
00016717  00000-0  10270-3 0  9119
2 25544  51
6407 128
0183 0006625 106
0926 254
0957 15
54314560 25251


Satellite: ISS
Catalog Number: 25544
Epoch time:      16299
51318177   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       128
0183  deg
Eccentricity:     
0006625     
Arg of perigee:   106
0926  deg
Mean anomaly:     254
0957  deg
Mean motion:   15
54314560  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2525
Checksum:              304


Coasting Arc #13 (Orbit 2539)
---------------------------------------

Vector Time (GMT): 2016/300/11:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910476
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3401253
36                 A    =         6776708
74  meter
 Y    =        2451106
17  meter          E    =           
0021222
 Z    =       -5342433
12                 I    =           51
92945
 XDOT =      -4233
154813                 Wp   =           97
56372
 YDOT =       6371
838534  meter/sec      RA   =          122
26982  deg
 ZDOT =        226
417722                 TA   =          174
60142
                                          MA   =          174
57850
                                          Ha   =            222
997  n
mi
                                          Hp   =            212
100

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11158967
71                 X    =         3399543
29
 Y    =        8041686
89  feet           Y    =         2489131
21  meter
 Z    =      -17527667
73                 Z    =        -5325914
83
 XDOT =     -13888
303193                 XDOT =       -4305
191577
 YDOT =      20904
982066  feet/sec       YDOT =        6324
097793  meter/sec
 ZDOT =        742
840295                 ZDOT =         205
678257

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13383371
13                 X    =        -4079251
52
 Y    =       -3548650
17  feet           Y    =        -1081628
57  meter
 Z    =      -17455740
71                 Z    =        -5320509
77
 XDOT =       5369
747565                 XDOT =        1636
699058
 YDOT =     -23485
283666  feet/sec       YDOT =       -7158
314461  meter/sec
 ZDOT =        651
006216                 ZDOT =         198
426695


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   16300
47757526  
00016717  00000-0  10270-3 0  9123
2 25544  51
6387 123
2084 0006613 110
3871 249
7992 15
54357829 25401


Satellite: ISS
Catalog Number: 25544
Epoch time:      16300
47757526   =   yrday
fracday
Element set:     912
Inclination:       51
6387  deg
RA of node:       123
2084  deg
Eccentricity:     
0006613     
Arg of perigee:   110
3871  deg
Mean anomaly:     249
7992  deg
Mean motion:   15
54357829  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2540
Checksum:              318


Coasting Arc #14 (Orbit 2555)
---------------------------------------

Vector Time (GMT): 2016/301/11:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910476
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2309260
95                 A    =         6778260
49  meter
 Y    =       -3990042
22  meter          E    =           
0011255
 Z    =        4959632
24                 I    =           51
95170
 XDOT =       4816
611602                 Wp   =           86
59723
 YDOT =      -5550
476869  meter/sec      RA   =          117
28957  deg
 ZDOT =      -2217
738840                 TA   =           24
95262
                                          MA   =           24
89825
                                          Ha   =            223
010  n
mi
                                          Hp   =            212
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7576315
44                 X    =        -2288563
83
 Y    =      -13090689
71  feet           Y    =        -4015749
74  meter
 Z    =       16271759
32                 Z    =         4948464
88
 XDOT =      15802
531503                 XDOT =        4889
093483
 YDOT =     -18210
225949  feet/sec       YDOT =       -5496
209222  meter/sec
 ZDOT =      -7276
046063                 ZDOT =       -2194
163955

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11966164
20                 X    =         3647286
85
 Y    =        9335169
29  feet           Y    =         2845359
60  meter
 Z    =       16223513
57                 Z    =         4944926
94
 XDOT =      -7338
156655                 XDOT =       -2236
670148
 YDOT =      21898
760525  feet/sec       YDOT =        6674
742208  meter/sec
 ZDOT =      -7171
915318                 ZDOT =       -2185
999789


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   16301
50625585  
00016717  00000-0  10270-3 0  9138
2 25544  51
6392 118
0787 0006459 114
9139 245
2685 15
54356926 25568


Satellite: ISS
Catalog Number: 25544
Epoch time:      16301
50625585   =   yrday
fracday
Element set:     913
Inclination:       51
6392  deg
RA of node:       118
0787  deg
Eccentricity:     
0006459     
Arg of perigee:   114
9139  deg
Mean anomaly:     245
2685  deg
Mean motion:   15
54356926  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2556
Checksum:              330


Coasting Arc #15 (Orbit 2570)
---------------------------------------

Vector Time (GMT): 2016/302/11:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910476
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1240662
14                 A    =         6781700
66  meter
 Y    =        5310178
54  meter          E    =           
0013660
 Z    =       -4046471
55                 I    =           51
97660
 XDOT =      -5053
527146                 Wp   =          113
06488
 YDOT =       4184
193272  meter/sec      RA   =          112
31625  deg
 ZDOT =       3946
849077                 TA   =          197
78294
                                          MA   =          197
83080
                                          Ha   =            222
912  n
mi
                                          Hp   =            212
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4070413
84                 X    =         1200846
59
 Y    =       17421845
60  feet           Y    =         5323829
47  meter
 Z    =      -13275825
28                 Z    =        -4040541
78
 XDOT =     -16579
813471                 XDOT =       -5119
112773
 YDOT =      13727
668214  feet/sec       YDOT =        4127
314982  meter/sec
 ZDOT =      12948
979910                 ZDOT =        3922
140109

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10536833
26                 X    =        -3211626
78
 Y    =      -14482044
00  feet           Y    =        -4414127
01  meter
 Z    =      -13250737
95                 Z    =        -4038824
93
 XDOT =       9045
210685                 XDOT =        2756
980217
 YDOT =     -18313
354678  feet/sec       YDOT =       -5581
910506  meter/sec
 ZDOT =      12840
093357                 ZDOT =        3913
660455


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   16302
47063682  
00016717  00000-0  10270-3 0  9140
2 25544  51
6384 113
2681 0006619 118
0379 242
1444 15
54378483 25716


Satellite: ISS
Catalog Number: 25544
Epoch time:      16302
47063682   =   yrday
fracday
Element set:     914
Inclination:       51
6384  deg
RA of node:       113
2681  deg
Eccentricity:     
0006619     
Arg of perigee:   118
0379  deg
Mean anomaly:     242
1444  deg
Mean motion:   15
54378483  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2571
Checksum:              310


Coasting Arc #16 (Orbit 2586)
---------------------------------------

Vector Time (GMT): 2016/303/11:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910476
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -201469
58                 A    =         6785581
89  meter
 Y    =       -6241344
62  meter          E    =           
0019749
 Z    =        2629295
65                 I    =           52
00106
 XDOT =       5052
822514                 Wp   =          108
85034
 YDOT =      -2390
104654  meter/sec      RA   =          107
35613  deg
 ZDOT =      -5260
466650                 TA   =           41
64838
                                          MA   =           41
49815
                                          Ha   =            222
774  n
mi
                                          Hp   =            212
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -660989
43                 X    =         -144434
59
 Y    =      -20476852
43  feet           Y    =        -6243278
48  meter
 Z    =        8626298
07                 Z    =         2628455
97
 XDOT =      16577
501685                 XDOT =        5104
727434
 YDOT =      -7841
550703  feet/sec       YDOT =       -2333
310805  meter/sec
 ZDOT =     -17258
748853                 ZDOT =       -5235
794448

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8856211
60                 X    =         2699373
29
 Y    =       18475694
60  feet           Y    =         5631391
71  meter
 Z    =        8623667
20                 Z    =         2628493
76
 XDOT =     -10804
579326                 XDOT =       -3293
235779
 YDOT =      13223
850233  feet/sec       YDOT =        4030
629551  meter/sec
 ZDOT =     -17150
310062                 ZDOT =       -5227
414507


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   16303
49930073  
00016717  00000-0  10270-3 0  9151
2 25544  51
6383 108
1379 0006393 121
6965 238
4811 15
54410159 25872


Satellite: ISS
Catalog Number: 25544
Epoch time:      16303
49930073   =   yrday
fracday
Element set:     915
Inclination:       51
6383  deg
RA of node:       108
1379  deg
Eccentricity:     
0006393     
Arg of perigee:   121
6965  deg
Mean anomaly:     238
4811  deg
Mean motion:   15
54410159  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2587
Checksum:              317


Coasting Arc #17 (Orbit 2595)
---------------------------------------

Vector Time (GMT): 2016/304/00:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 895244
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4378418
38                 A    =         6778015
74  meter
 Y    =        1289429
90  meter          E    =           
0012667
 Z    =        5003837
92                 I    =           51
98093
 XDOT =        230
873613                 Wp   =          122
80069
 YDOT =      -7379
881535  meter/sec      RA   =          104
59756  deg
 ZDOT =       2093
209038                 TA   =          306
88536
                                          MA   =          307
00140
                                          Ha   =            222
945  n
mi
                                          Hp   =            212
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14364889
69                 X    =        -4416818
80
 Y    =        4230413
06  feet           Y    =         1240253
14  meter
 Z    =       16416791
09                 Z    =         4982474
76
 XDOT =        757
459361                 XDOT =         303
212008
 YDOT =     -24212
209759  feet/sec       YDOT =       -7376
895130  meter/sec
 ZDOT =       6867
483722                 ZDOT =        2094
506837

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6706710
30                 X    =        -2044205
30
 Y    =       13503200
82  feet           Y    =         4115775
61  meter
 Z    =       16323023
15                 Z    =         4975257
46
 XDOT =     -16321
293210                 XDOT =       -4974
730170
 YDOT =     -16458
307073  feet/sec       YDOT =       -5016
491996  meter/sec
 ZDOT =       6874
413906                 ZDOT =        2095
321359


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   16304
07792374  
00016717  00000-0  10270-3 0  9167
2 25544  51
6383 105
2555 0006522 122
5019 237
6765 15
54399728 25967


Satellite: ISS
Catalog Number: 25544
Epoch time:      16304
07792374   =   yrday
fracday
Element set:     916
Inclination:       51
6383  deg
RA of node:       105
2555  deg
Eccentricity:     
0006522     
Arg of perigee:   122
5019  deg
Mean anomaly:     237
6765  deg
Mean motion:   15
54399728  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2596
Checksum:              328


Coasting Arc #18 (Orbit 2596)
---------------------------------------

Vector Time (GMT): 2016/304/02:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895244
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4312155
98                 A    =         6777091
01  meter
 Y    =         454965
15  meter          E    =           
0010783
 Z    =        5201830
37                 I    =           51
97994
 XDOT =        830
738213                 Wp   =          123
65143
 YDOT =      -7511
555381  meter/sec      RA   =          104
26656  deg
 ZDOT =       1337
828678                 TA   =          313
52033
                                          MA   =          313
60988
                                          Ha   =            222
887  n
mi
                                          Hp   =            212
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14147493
38                 X    =        -4342191
93
 Y    =        1492667
81  feet           Y    =          406576
16  meter
 Z    =       17066372
59                 Z    =         5180809
47
 XDOT =       2725
519070                 XDOT =         908
173839
 YDOT =     -24644
210569  feet/sec       YDOT =       -7501
832444  meter/sec
 ZDOT =       4389
201699                 ZDOT =        1342
052926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3234887
84                 X    =         -985993
81
 Y    =       13966074
44  feet           Y    =         4256859
49  meter
 Z    =       16974244
17                 Z    =         5173749
62
 XDOT =     -21400
299621                 XDOT =       -6522
811325
 YDOT =     -10346
761527  feet/sec       YDOT =       -3153
692913  meter/sec
 ZDOT =       4408
970472                 ZDOT =        1343
854200


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   16304
14221440  
00016717  00000-0  10270-3 0  9177
2 25544  51
6396 104
9351 0006437 122
8522 237
3251 15
54421667 25974


Satellite: ISS
Catalog Number: 25544
Epoch time:      16304
14221440   =   yrday
fracday
Element set:     917
Inclination:       51
6396  deg
RA of node:       104
9351  deg
Eccentricity:     
0006437     
Arg of perigee:   122
8522  deg
Mean anomaly:     237
3251  deg
Mean motion:   15
54421667  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2597
Checksum:              295


Coasting Arc #19 (Orbit 2611)
---------------------------------------

Vector Time (GMT): 2016/305/02:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895244
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3968633
80                 A    =         6776739
66  meter
 Y    =        1462245
05  meter          E    =           
0020439
 Z    =       -5312449
22                 I    =           51
98632
 XDOT =      -1775
047820                 Wp   =          104
68712
 YDOT =       7411
126409  meter/sec      RA   =           99
28640  deg
 ZDOT =        711
110877                 TA   =          172
10139
                                          MA   =          172
06915
                                          Ha   =            222
745  n
mi
                                          Hp   =            212
346

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13020452
11                 X    =         3977793
94
 Y    =        4797391
89  feet           Y    =         1506675
89  meter
 Z    =      -17429295
34                 Z    =        -5293147
90
 XDOT =      -5823
647703                 XDOT =       -1861
243367
 YDOT =      24314
719188  feet/sec       YDOT =        7390
794724  meter/sec
 ZDOT =       2333
040934                 ZDOT =         702
278121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8626790
79                 X    =         2629445
83
 Y    =      -11002553
16  feet           Y    =        -3353578
20  meter
 Z    =      -17345021
85                 Z    =        -5286762
66
 XDOT =      20509
594708                 XDOT =        6251
324467
 YDOT =      12451
735330  feet/sec       YDOT =        3795
288929  meter/sec
 ZDOT =       2293
087448                 ZDOT =         698
933054


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   16305
10657797  
00016717  00000-0  10270-3 0  9183
2 25544  51
6404 100
1249 0006444 125
8941 234
2811 15
54398180 26123


Satellite: ISS
Catalog Number: 25544
Epoch time:      16305
10657797   =   yrday
fracday
Element set:     918
Inclination:       51
6404  deg
RA of node:       100
1249  deg
Eccentricity:     
0006444     
Arg of perigee:   125
8941  deg
Mean anomaly:     234
2811  deg
Mean motion:   15
54398180  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2612
Checksum:              300


Coasting Arc #20 (Orbit 2627)
---------------------------------------

Vector Time (GMT): 2016/306/02:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895244
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3499312
72                 A    =         6778863
71  meter
 Y    =       -3278408
62  meter          E    =           
0011706
 Z    =        4781400
40                 I    =           51
99851
 XDOT =       2607
265489                 Wp   =           92
09005
 YDOT =      -6703
106634  meter/sec      RA   =           94
31078  deg
 ZDOT =      -2682
667088                 TA   =           24
26461
                                          MA   =           24
20953
                                          Ha   =            222
812  n
mi
                                          Hp   =            212
256

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11480684
78                 X    =        -3485619
26
 Y    =      -10755933
78  feet           Y    =        -3317463
52  meter
 Z    =       15687009
18                 Z    =         4764434
54
 XDOT =       8554
020634                 XDOT =        2695
059161
 YDOT =     -21991
819664  feet/sec       YDOT =       -6673
459665  meter/sec
 ZDOT =      -8801
401206                 ZDOT =       -2669
787780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13678147
11                 X    =        -4169099
24
 Y    =        7919106
30  feet           Y    =         2413743
60  meter
 Z    =       15613280
83                 Z    =         4758928
00
 XDOT =     -17923
126993                 XDOT =       -5462
969107
 YDOT =     -13684
175444  feet/sec       YDOT =       -4170
936675  meter/sec
 ZDOT =      -8743
828359                 ZDOT =       -2665
118884


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   16306
13522293  
00016717  00000-0  10270-3 0  9190
2 25544  51
6410  94
9956 0006419 128
6695 231
5033 15
54413945 26284


Satellite: ISS
Catalog Number: 25544
Epoch time:      16306
13522293   =   yrday
fracday
Element set:     919
Inclination:       51
6410  deg
RA of node:        94
9956  deg
Eccentricity:     
0006419     
Arg of perigee:   128
6695  deg
Mean anomaly:     231
5033  deg
Mean motion:   15
54413945  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2628
Checksum:              318
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