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

 
Date: December 25th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 ET - UTC (sec) : 67 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


There are no maneuvers



Coasting Arc #1 (Orbit 1749)
---------------------------------------

Vector Time (GMT): 2015/357/11:47:00
566
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -530133
73                 A    =         6777985
57  meter
 Y    =       -5017893
24  meter          E    =           
0003348
 Z    =        4522356
41                 I    =           51
40145
 XDOT =       6684
591060                 Wp   =           39
67220
 YDOT =       2104
373549  meter/sec      RA   =          218
29018  deg
 ZDOT =       3119
812908                 TA   =           18
97608
                                          MA   =           18
96361
                                          Ha   =            219
655  n
mi
                                          Hp   =            214
916

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1739283
90                 X    =         -495950
95
 Y    =      -16462904
33  feet           Y    =        -5023630
85  meter
 Z    =       14837127
34                 Z    =         4519863
67
 XDOT =      21931
073031                 XDOT =        6645
407733
 YDOT =       6904
112692  feet/sec       YDOT =        2178
905675  meter/sec
 ZDOT =      10235
606654                 ZDOT =        3152
190409

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16523644
62                 X    =         5036406
88
 Y    =       -1146553
94  feet           Y    =         -349469
64  meter
 Z    =       14827247
14                 Z    =         4519344
93
 XDOT =      -7894
095621                 XDOT =       -2406
120345
 YDOT =      20353
300663  feet/sec       YDOT =        6203
686042  meter/sec
 ZDOT =      10375
242058                 ZDOT =        3162
373779


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   15357
54485237  
00016717  00000-0  10270-3 0  9006
2 25544  51
6428 219
0695 0008510 314
8018  45
2443 15
55045348 17504


Satellite: ISS
Catalog Number: 25544
Epoch time:      15357
54485237   =   yrday
fracday
Element set:     900
Inclination:       51
6428  deg
RA of node:       219
0695  deg
Eccentricity:     
0008510     
Arg of perigee:   314
8018  deg
Mean anomaly:      45
2443  deg
Mean motion:   15
55045348  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1750
Checksum:              304


Coasting Arc #2 (Orbit 1764)
---------------------------------------

Vector Time (GMT): 2015/358/11:47:00
566
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1359741
75                 A    =         6774856
03  meter
 Y    =        4097847
04  meter          E    =           
0011822
 Z    =       -5229361
71                 I    =           51
41592
 XDOT =      -6749
039315                 Wp   =           45
47676
 YDOT =      -3495
273279  meter/sec      RA   =          213
26774  deg
 ZDOT =       -977
325699                 TA   =          215
09412
                                          MA   =          215
17206
                                          Ha   =            219
735  n
mi
                                          Hp   =            214
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4461094
98                 X    =        -1380061
64
 Y    =       13444380
06  feet           Y    =         4082528
45  meter
 Z    =      -17156698
52                 Z    =        -5236015
97
 XDOT =     -22142
517437                 XDOT =       -6704
705243
 YDOT =     -11467
432017  feet/sec       YDOT =       -3570
497503  meter/sec
 ZDOT =      -3206
449143                 ZDOT =       -1010
003798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13332153
18                 X    =        -4063640
29
 Y    =       -4678986
01  feet           Y    =        -1426154
94  meter
 Z    =      -17186209
86                 Z    =        -5238356
77
 XDOT =      11664
867950                 XDOT =        3555
451751
 YDOT =     -20861
844551  feet/sec       YDOT =       -6358
690219  meter/sec
 ZDOT =      -3347
158465                 ZDOT =       -1020
213900


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   15358
50879262  
00016717  00000-0  10270-3 0  9019
2 25544  51
6414 214
2567 0008647 317
6405  42
4079 15
55106270 17658


Satellite: ISS
Catalog Number: 25544
Epoch time:      15358
50879262   =   yrday
fracday
Element set:     901
Inclination:       51
6414  deg
RA of node:       214
2567  deg
Eccentricity:     
0008647     
Arg of perigee:   317
6405  deg
Mean anomaly:      42
4079  deg
Mean motion:   15
55106270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1765
Checksum:              311


Coasting Arc #3 (Orbit 1780)
---------------------------------------

Vector Time (GMT): 2015/359/11:47:00
566
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3274892
84                 A    =         6775020
27  meter
 Y    =       -2916420
23  meter          E    =           
0009323
 Z    =        5167800
77                 I    =           51
44391
 XDOT =       6086
943913                 Wp   =          348
13527
 YDOT =       4469
662273  meter/sec      RA   =          208
24245  deg
 ZDOT =      -1326
413870                 TA   =          114
69410
                                          MA   =          114
59701
                                          Ha   =            219
797  n
mi
                                          Hp   =            214
408

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10744399
09                 X    =         3282158
54
 Y    =       -9568307
85  feet           Y    =        -2879758
16  meter
 Z    =       16954726
92                 Z    =         5183726
76
 XDOT =      19970
288428                 XDOT =        6042
953825
 YDOT =      14664
246302  feet/sec       YDOT =        4537
484682  meter/sec
 ZDOT =      -4351
751543                 ZDOT =       -1296
951278

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9488897
10                 X    =         2892215
83
 Y    =       10704999
85  feet           Y    =         3262883
95  meter
 Z    =       17024135
87                 Z    =         5188956
61
 XDOT =     -14028
618519                 XDOT =       -4275
922925
 YDOT =      19198
389077  feet/sec       YDOT =        5851
668991  meter/sec
 ZDOT =      -4225
099498                 ZDOT =       -1287
810327


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   15359
53698269  
00016717  00000-0  10270-3 0  9020
2 25544  51
6414 209
1232 0008653 321
0102  39
0427 15
55119596 17812


Satellite: ISS
Catalog Number: 25544
Epoch time:      15359
53698269   =   yrday
fracday
Element set:     902
Inclination:       51
6414  deg
RA of node:       209
1232  deg
Eccentricity:     
0008653     
Arg of perigee:   321
0102  deg
Mean anomaly:      39
0427  deg
Mean motion:   15
55119596  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1781
Checksum:              306


Coasting Arc #4 (Orbit 1795)
---------------------------------------

Vector Time (GMT): 2015/360/11:47:00
566
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4924782
21                 A    =         6778222
36  meter
 Y    =        1657151
59  meter          E    =           
0005149
 Z    =       -4353091
97                 I    =           51
48203
 XDOT =      -4705
258997                 Wp   =           40
61987
 YDOT =      -4989
670347  meter/sec      RA   =          203
22383  deg
 ZDOT =       3429
829596                 TA   =          264
21777
                                          MA   =          264
27648
                                          Ha   =            219
896  n
mi
                                          Hp   =            214
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16157421
94                 X    =        -4921801
45
 Y    =        5436849
06  feet           Y    =         1602096
55  meter
 Z    =      -14281797
80                 Z    =        -4377007
89
 XDOT =     -15437
201434                 XDOT =       -4665
774187
 YDOT =     -16370
309538  feet/sec       YDOT =       -5042
067246  meter/sec
 ZDOT =      11252
721772                 ZDOT =        3407
068033

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5594451
74                 X    =        -1705188
89
 Y    =      -16010907
25  feet           Y    =        -4880124
53  meter
 Z    =      -14385559
38                 Z    =        -4384718
50
 XDOT =      15047
186195                 XDOT =        4586
382352
 YDOT =     -15262
526188  feet/sec       YDOT =       -4652
017982  meter/sec
 ZDOT =      11155
127990                 ZDOT =        3400
083011


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   15360
50089772  
00016717  00000-0  10270-3 0  9033
2 25544  51
6398 204
3091 0008687 324
5170  35
5404 15
55140564 17964


Satellite: ISS
Catalog Number: 25544
Epoch time:      15360
50089772   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:       204
3091  deg
Eccentricity:     
0008687     
Arg of perigee:   324
5170  deg
Mean anomaly:      35
5404  deg
Mean motion:   15
55140564  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1796
Checksum:              311


Coasting Arc #5 (Orbit 1811)
---------------------------------------

Vector Time (GMT): 2015/361/11:47:00
566
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6132808
72                 A    =         6782626
45  meter
 Y    =        -383484
29  meter          E    =           
0010157
 Z    =        2871677
15                 I    =           51
52743
 XDOT =       2690
283051                 Wp   =           56
64621
 YDOT =       5106
460040  meter/sec      RA   =          198
22211  deg
 ZDOT =      -5045
113322                 TA   =           90
61677
                                          MA   =           90
50039
                                          Ha   =            220
107  n
mi
                                          Hp   =            213
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20120763
51                 X    =         6122691
82
 Y    =       -1258150
55  feet           Y    =         -314959
99  meter
 Z    =        9421512
95                 Z    =         2901444
06
 XDOT =       8826
387961                 XDOT =        2657
488290
 YDOT =      16753
477822  feet/sec       YDOT =        5136
361652  meter/sec
 ZDOT =     -16552
209063                 ZDOT =       -5032
123849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1800623
69                 X    =          548830
10
 Y    =       20018514
69  feet           Y    =         6101643
28  meter
 Z    =        9550382
04                 Z    =         2910956
45
 XDOT =     -15043
816167                 XDOT =       -4585
355168
 YDOT =       9251
853053  feet/sec       YDOT =        2819
964811  meter/sec
 ZDOT =     -16496
899117                 ZDOT =       -5028
254851


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   15361
52905820  
00016717  00000-0  10270-3 0  9048
2 25544  51
6402 199
1754 0008917 328
3572  31
7044 15
55198804 18128


Satellite: ISS
Catalog Number: 25544
Epoch time:      15361
52905820   =   yrday
fracday
Element set:     904
Inclination:       51
6402  deg
RA of node:       199
1754  deg
Eccentricity:     
0008917     
Arg of perigee:   328
3572  deg
Mean anomaly:      31
7044  deg
Mean motion:   15
55198804  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1812
Checksum:              310


Coasting Arc #6 (Orbit 1826)
---------------------------------------

Vector Time (GMT): 2015/362/11:47:00
566
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6660916
71                 A    =         6785893
29  meter
 Y    =        -772629
23  meter          E    =           
0015444
 Z    =        -973878
19                 I    =           51
56719
 XDOT =       -293
569004                 Wp   =            7
50109
 YDOT =      -4887
456996  meter/sec      RA   =          193
23427  deg
 ZDOT =       5910
917590                 TA   =          341
92643
                                          MA   =          341
98127
                                          Ha   =            220
223  n
mi
                                          Hp   =            213
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21853401
29                 X    =        -6647051
28
 Y    =       -2534872
79  feet           Y    =         -847038
40  meter
 Z    =       -3195138
41                 Z    =        -1006201
44
 XDOT =       -963
152899                 XDOT =        -267
606955
 YDOT =     -16034
963896  feet/sec       YDOT =       -4890
595137  meter/sec
 ZDOT =      19392
774244                 ZDOT =        5909
554223

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1565480
60                 X    =          477158
49
 Y    =      -21923353
75  feet           Y    =        -6682238
22  meter
 Z    =       -3334886
56                 Z    =        -1016473
42
 XDOT =      14370
530743                 XDOT =        4380
137770
 YDOT =      -1910
804427  feet/sec       YDOT =        -582
413189  meter/sec
 ZDOT =      19387
725754                 ZDOT =        5909
378810


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   15362
49294782  
00016717  00000-0  10270-3 0  9054
2 25544  51
6389 194
3612 0008781 331
7997  28
2680 15
55161007 18278


Satellite: ISS
Catalog Number: 25544
Epoch time:      15362
49294782   =   yrday
fracday
Element set:     905
Inclination:       51
6389  deg
RA of node:       194
3612  deg
Eccentricity:     
0008781     
Arg of perigee:   331
7997  deg
Mean anomaly:      28
2680  deg
Mean motion:   15
55161007  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1827
Checksum:              336


Coasting Arc #7 (Orbit 1842)
---------------------------------------

Vector Time (GMT): 2015/363/11:47:00
566
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6446106
58                 A    =         6785710
22  meter
 Y    =        1815331
83  meter          E    =           
0002440
 Z    =       -1098775
92                 I    =           51
59841
 XDOT =      -2234
053446                 Wp   =           77
84563
 YDOT =       4382
486496  meter/sec      RA   =          188
25559  deg
 ZDOT =      -5876
419768                 TA   =          114
07765
                                          MA   =          114
05211
                                          Ha   =            220
386  n
mi
                                          Hp   =            213
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21148643
63                 X    =         6430665
35
 Y    =        5955813
10  feet           Y    =         1887330
18  meter
 Z    =       -3604907
89                 Z    =        -1067499
95
 XDOT =      -7329
571672                 XDOT =       -2254
348507
 YDOT =      14378
236534  feet/sec       YDOT =        4357
390662  meter/sec
 ZDOT =     -19279
592414                 ZDOT =       -5887
321241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4642610
92                 X    =        -1415067
81
 Y    =       21497406
20  feet           Y    =         6552409
41  meter
 Z    =       -3469854
25                 Z    =        -1057611
57
 XDOT =     -13224
608009                 XDOT =       -4030
860521
 YDOT =      -5969
822294  feet/sec       YDOT =       -1819
601835  meter/sec
 ZDOT =     -19327
535245                 ZDOT =       -5891
032743


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   15363
52108117  
00016717  00000-0  10270-3 0  9066
2 25544  51
6390 189
2274 0008806 336
1857  23
8888 15
55208604 18433


Satellite: ISS
Catalog Number: 25544
Epoch time:      15363
52108117   =   yrday
fracday
Element set:     906
Inclination:       51
6390  deg
RA of node:       189
2274  deg
Eccentricity:     
0008806     
Arg of perigee:   336
1857  deg
Mean anomaly:      23
8888  deg
Mean motion:   15
55208604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1843
Checksum:              323


Coasting Arc #8 (Orbit 1858)
---------------------------------------

Vector Time (GMT): 2015/364/11:47:00
566
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5447319
32                 A    =         6782386
60  meter
 Y    =       -2688149
11  meter          E    =           
0013988
 Z    =        2995884
91                 I    =           51
61873
 XDOT =       4550
868159                 Wp   =           45
90286
 YDOT =      -3680
656903  meter/sec      RA   =          183
27139  deg
 ZDOT =       4967
257710                 TA   =          348
44808
                                          MA   =          348
48014
                                          Ha   =            220
489  n
mi
                                          Hp   =            213
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17871782
53                 X    =        -5431407
56
 Y    =       -8819386
85  feet           Y    =        -2748975
78  meter
 Z    =        9829018
74                 Z    =         2969461
87
 XDOT =      14930
669812                 XDOT =        4567
559259
 YDOT =     -12075
646006  feet/sec       YDOT =       -3629
672945  meter/sec
 ZDOT =      16296
777263                 ZDOT =        4989
404987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7380805
06                 X    =         2249669
38
 Y    =      -18572351
99  feet           Y    =        -5660852
89  meter
 Z    =        9715104
88                 Z    =         2961163
97
 XDOT =      11848
287096                 XDOT =        3611
357907
 YDOT =      13292
280113  feet/sec       YDOT =        4051
486978  meter/sec
 ZDOT =      16393
281217                 ZDOT =        4996
672115


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   15364
54919932  
00016717  00000-0  10270-3 0  9075
2 25544  51
6385 184
0920 0008675 339
1205  20
9593 15
55235530 18598


Satellite: ISS
Catalog Number: 25544
Epoch time:      15364
54919932   =   yrday
fracday
Element set:     907
Inclination:       51
6385  deg
RA of node:       184
0920  deg
Eccentricity:     
0008675     
Arg of perigee:   339
1205  deg
Mean anomaly:      20
9593  deg
Mean motion:   15
55235530  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1859
Checksum:              327
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