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

 
Date: December 10th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 298 16 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


342/17:12:15 308 5 5 -10 9 10 9
N/A -9 2 0 0 223 0
000/00:00:53 177 2 0 0 0 214 3

342/18:02:48 487 -11 2 -18 2 18 2
N/A 12 4 -0 0 214 2
000/00:01:27 994 -7 1 0 0 212 0

342/21:12:15 274 5 0 1 4 5 7
N/A 1 0 5 6 214 4
000/00:00:27 808 -2 7 -0 0 212 6

342/22:31:42 277 0 9 2 6 2 6
N/A -2 5 0 0 214 6
000/00:00:12 695 -0 1 0 0 214 0

343/01:10:46 376 -1 7 2 6 2 6
N/A 0 0 -0 0 216 9
000/00:00:12 692 -2 0 -0 0 215 1

343/07:50:50 000 0 0 0 0 0 0
N/A 0 0 0 0 216 6
000/00:00:00 000 0 0 0 0 215 0

Coasting Arc #1 (Orbit 6)
---------------------------------------

Vector Time (GMT): 2015/341/05:51:13
813
Vector Time (MET): N/A
Weight (LBS)     : 15641
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1064994
43                 A    =         6793362
91  meter
 Y    =        6161506
51  meter          E    =           
0003215
 Z    =        2653587
62                 I    =           51
34720
 XDOT =      -5496
819778                 Wp   =           79
40675
 YDOT =       1283
079675  meter/sec      RA   =          299
64791  deg
 ZDOT =      -5179
406210                 TA   =           70
57767
                                          MA   =           70
54292
                                          Ha   =            223
927  n
mi
                                          Hp   =            221
125

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3494076
20                 X    =        -1146705
06
 Y    =       20214916
39  feet           Y    =         6149140
08  meter
 Z    =        8705996
11                 Z    =         2648215
76
 XDOT =     -18034
185622                 XDOT =       -5485
598991
 YDOT =       4209
578985  feet/sec       YDOT =        1221
673529  meter/sec
 ZDOT =     -16992
802525                 ZDOT =       -5206
081761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9415773
39                 X    =         2869927
73
 Y    =      -18237867
02  feet           Y    =        -5558901
87  meter
 Z    =        8681543
61                 Z    =         2646134
49
 XDOT =      17034
459114                 XDOT =        5192
103138
 YDOT =        641
324029  feet/sec       YDOT =         195
475564  meter/sec
 ZDOT =     -17108
292942                 ZDOT =       -5214
607689


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   15341
28144070  
00016717  00000-0  10270-3 0  9007
2 25544  51
6534 300
1802 0010668 289
3670  70
6328 15
51725938    75


Satellite: ISS
Catalog Number: 25544
Epoch time:      15341
28144070   =   yrday
fracday
Element set:     900
Inclination:       51
6534  deg
RA of node:       300
1802  deg
Eccentricity:     
0010668     
Arg of perigee:   289
3670  deg
Mean anomaly:      70
6328  deg
Mean motion:   15
51725938  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:               7
Checksum:              286


Coasting Arc #2 (Orbit 21)
---------------------------------------

Vector Time (GMT): 2015/342/05:51:13
813
Vector Time (MET): N/A
Weight (LBS)     : 15641
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1332819
00                 A    =         6794950
88  meter
 Y    =       -6400394
75  meter          E    =           
0011084
 Z    =       -1824435
06                 I    =           51
33714
 XDOT =       5188
760609                 Wp   =          332
00602
 YDOT =       -522
938177  meter/sec      RA   =          294
66466  deg
 ZDOT =       5620
814594                 TA   =            7
85866
                                          MA   =            7
84131
                                          Ha   =            224
154  n
mi
                                          Hp   =            221
071

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4372765
76                 X    =         1413153
28
 Y    =      -20998670
43  feet           Y    =        -6385041
02  meter
 Z    =       -5985679
34                 Z    =        -1817765
59
 XDOT =      17023
492811                 XDOT =        5166
918383
 YDOT =      -1715
676435  feet/sec       YDOT =        -465
036443  meter/sec
 ZDOT =      18440
992761                 ZDOT =        5645
967872

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10147754
37                 X    =        -3093035
53
 Y    =       18906288
78  feet           Y    =         5762636
82  meter
 Z    =       -5955579
17                 Z    =        -1815260
53
 XDOT =     -15324
638964                 XDOT =       -4670
949956
 YDOT =      -2377
587150  feet/sec       YDOT =        -724
688563  meter/sec
 ZDOT =      18549
752830                 ZDOT =        5653
964663


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   15342
24747717  
00016717  00000-0  10270-3 0  9012
2 25544  51
6531 295
3824 0010563 292
8638  67
1398 15
51718463   228


Satellite: ISS
Catalog Number: 25544
Epoch time:      15342
24747717   =   yrday
fracday
Element set:     901
Inclination:       51
6531  deg
RA of node:       295
3824  deg
Eccentricity:     
0010563     
Arg of perigee:   292
8638  deg
Mean anomaly:      67
1398  deg
Mean motion:   15
51718463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              22
Checksum:              314


Coasting Arc #3 (Orbit 29)
---------------------------------------

Vector Time (GMT): 2015/342/17:12:41
897
Vector Time (MET): N/A
Weight (LBS)     : 15624
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3106732
38                 A    =         6779168
61  meter
 Y    =        3214690
33  meter          E    =           
0017064
 Z    =        5110774
00                 I    =           51
30032
 XDOT =      -3971
201267                 Wp   =          303
74483
 YDOT =       6352
404666  meter/sec      RA   =          292
30771  deg
 ZDOT =      -1576
176856                 TA   =          161
58235
                                          MA   =          161
52050
                                          Ha   =            222
968  n
mi
                                          Hp   =            214
293

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10192691
53                 X    =         3045727
44
 Y    =       10546884
27  feet           Y    =         3249090
46  meter
 Z    =       16767631
25                 Z    =         5125718
14
 XDOT =     -13028
875548                 XDOT =       -4034
283675
 YDOT =      20841
222658  feet/sec       YDOT =        6307
643450  meter/sec
 ZDOT =      -5171
183910                 ZDOT =       -1595
621309

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4554696
29                 X    =         1388271
43
 Y    =       13864891
29  feet           Y    =         4226018
87  meter
 Z    =       16831539
36                 Z    =         5130253
20
 XDOT =     -19697
120577                 XDOT =       -6003
682352
 YDOT =      12873
580907  feet/sec       YDOT =        3923
867460  meter/sec
 ZDOT =      -5256
456155                 ZDOT =       -1602
167836


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   15342
76260965  
00016717  00000-0  10270-3 0  9025
2 25544  51
6549 292
8242 0019397 290
3063  69
6005 15
53799449   308


Satellite: ISS
Catalog Number: 25544
Epoch time:      15342
76260965   =   yrday
fracday
Element set:     902
Inclination:       51
6549  deg
RA of node:       292
8242  deg
Eccentricity:     
0019397     
Arg of perigee:   290
3063  deg
Mean anomaly:      69
6005  deg
Mean motion:   15
53799449  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              30
Checksum:              327


Coasting Arc #4 (Orbit 29)
---------------------------------------

Vector Time (GMT): 2015/342/18:03:32
484
Vector Time (MET): N/A
Weight (LBS)     : 15597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1907792
48                 A    =         6772128
69  meter
 Y    =       -4749261
77  meter          E    =           
0004844
 Z    =       -4439437
82                 I    =           51
30773
 XDOT =       4836
761069                 Wp   =          141
81080
 YDOT =      -4983
917319  meter/sec      RA   =          292
11969  deg
 ZDOT =       3251
365910                 TA   =          161
10143
                                          MA   =          161
08345
                                          Ha   =            214
208  n
mi
                                          Hp   =            211
986

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6259161
68                 X    =        -1832977
85
 Y    =      -15581567
49  feet           Y    =        -4770177
39  meter
 Z    =      -14565084
73                 Z    =        -4448524
21
 XDOT =      15868
638678                 XDOT =        4876
338828
 YDOT =     -16351
434773  feet/sec       YDOT =       -4929
608365  meter/sec
 ZDOT =      10667
210991                 ZDOT =        3274
958131

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2565279
08                 X    =         -781897
06
 Y    =      -16560937
91  feet           Y    =        -5047773
87  meter
 Z    =      -14603380
51                 Z    =        -4451110
38
 XDOT =      17818
327739                 XDOT =        5431
026295
 YDOT =     -12262
409113  feet/sec       YDOT =       -3737
582298  meter/sec
 ZDOT =      10770
125106                 ZDOT =        3282
734132


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   15342
76261220  
00016717  00000-0  10270-3 0  9031
2 25544  51
6537 292
8231 0005787 264
7027  95
3467 15
57151568   302


Satellite: ISS
Catalog Number: 25544
Epoch time:      15342
76261220   =   yrday
fracday
Element set:     903
Inclination:       51
6537  deg
RA of node:       292
8231  deg
Eccentricity:     
0005787     
Arg of perigee:   264
7027  deg
Mean anomaly:      95
3467  deg
Mean motion:   15
57151568  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              30
Checksum:              307


Coasting Arc #5 (Orbit 31)
---------------------------------------

Vector Time (GMT): 2015/342/21:12:29
178
Vector Time (MET): N/A
Weight (LBS)     : 15588
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -721051
11                 A    =         6776176
40  meter
 Y    =       -5772194
87  meter          E    =           
0001295
 Z    =       -3474630
87                 I    =           51
30456
 XDOT =       5208
212011                 Wp   =          255
70652
 YDOT =      -3367
950153  meter/sec      RA   =          291
46472  deg
 ZDOT =       4512
442090                 TA   =           63
21947
                                          MA   =           63
20623
                                          Ha   =            214
368  n
mi
                                          Hp   =            212
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2365653
25                 X    =         -639572
73
 Y    =      -18937647
22  feet           Y    =        -5779802
36  meter
 Z    =      -11399707
57                 Z    =        -3477936
10
 XDOT =      17087
309748                 XDOT =        5223
566101
 YDOT =     -11049
705226  feet/sec       YDOT =       -3309
622918  meter/sec
 ZDOT =      14804
600033                 ZDOT =        4537
780023

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12637182
14                 X    =        -3851813
12
 Y    =      -14291017
25  feet           Y    =        -4355902
06  meter
 Z    =      -11412825
42                 Z    =        -3478629
19
 XDOT =       6676
574094                 XDOT =        2035
019784
 YDOT =     -17819
371935  feet/sec       YDOT =       -5431
344566  meter/sec
 ZDOT =      14914
730049                 ZDOT =        4546
009719


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   15342
89096908  
00016717  00000-0  10270-3 0  9045
2 25544  51
6412 292
1874 0006282 269
6078  90
4356 15
56885966   321


Satellite: ISS
Catalog Number: 25544
Epoch time:      15342
89096908   =   yrday
fracday
Element set:     904
Inclination:       51
6412  deg
RA of node:       292
1874  deg
Eccentricity:     
0006282     
Arg of perigee:   269
6078  deg
Mean anomaly:      90
4356  deg
Mean motion:   15
56885966  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              32
Checksum:              340


Coasting Arc #6 (Orbit 32)
---------------------------------------

Vector Time (GMT): 2015/342/22:31:48
625
Vector Time (MET): N/A
Weight (LBS)     : 15585
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4038282
88                 A    =         6770703
70  meter
 Y    =       -1299737
34  meter          E    =           
0006687
 Z    =       -5282680
29                 I    =           51
28208
 XDOT =       2608
022796                 Wp   =           88
52724
 YDOT =      -7207
099272  meter/sec      RA   =          291
21531  deg
 ZDOT =       -220
529270                 TA   =          179
36067
                                          MA   =          179
35981
                                          Ha   =            214
568  n
mi
                                          Hp   =            214
039

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13248959
57                 X    =        -3997787
11
 Y    =       -4264230
13  feet           Y    =        -1344669
33  meter
 Z    =      -17331628
26                 Z    =        -5302199
49
 XDOT =       8556
505236                 XDOT =        2689
491774
 YDOT =     -23645
338818  feet/sec       YDOT =       -7177
479105  meter/sec
 ZDOT =       -723
521228                 ZDOT =        -207
662391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11106560
32                 X    =        -3385279
58
 Y    =        8212317
30  feet           Y    =         2503114
31  meter
 Z    =      -17415685
14                 Z    =        -5308300
83
 XDOT =     -13668
470496                 XDOT =       -4166
149807
 YDOT =     -19898
515910  feet/sec       YDOT =       -6065
067649  meter/sec
 ZDOT =       -666
491713                 ZDOT =        -203
146674


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   15342
95515870  
00016717  00000-0  10270-3 0  9057
2 25544  51
6422 291
8665 0008193 268
2506  91
7710 15
56418617   334


Satellite: ISS
Catalog Number: 25544
Epoch time:      15342
95515870   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:       291
8665  deg
Eccentricity:     
0008193     
Arg of perigee:   268
2506  deg
Mean anomaly:      91
7710  deg
Mean motion:   15
56418617  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              33
Checksum:              315


Coasting Arc #7 (Orbit 34)
---------------------------------------

Vector Time (GMT): 2015/343/01:10:52
722
Vector Time (MET): N/A
Weight (LBS)     : 15581
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1455659
15                 A    =         6783581
57  meter
 Y    =        6514569
90  meter          E    =           
0010344
 Z    =        1167974
42                 I    =           51
32108
 XDOT =      -4974
343747                 Wp   =          159
33204
 YDOT =        -62
925377  meter/sec      RA   =          290
64772  deg
 ZDOT =      -5842
267859                 TA   =            7
91318
                                          MA   =            7
89687
                                          Ha   =            216
889  n
mi
                                          Hp   =            215
122

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4775784
61                 X    =        -1534072
14
 Y    =       21373260
84  feet           Y    =         6497853
25  meter
 Z    =        3831937
07                 Z    =         1160712
97
 XDOT =     -16320
025418                 XDOT =       -4944
890445
 YDOT =       -206
448087  feet/sec       YDOT =        -118
386710  meter/sec
 ZDOT =     -19167
545469                 ZDOT =       -5866
361064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21675833
30                 X    =         6606793
99
 Y    =        3167333
78  feet           Y    =          965403
34  meter
 Z    =        3799261
36                 Z    =         1158014
86
 XDOT =       1250
242881                 XDOT =         381
074030
 YDOT =      14585
597090  feet/sec       YDOT =        4445
689993  meter/sec
 ZDOT =     -19271
609462                 ZDOT =       -5873
986564


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   15343
08358606  
00016717  00000-0  10270-3 0  9065
2 25544  51
6444 291
2246 0008293 253
5992 106
4250 15
55912020   355


Satellite: ISS
Catalog Number: 25544
Epoch time:      15343
08358606   =   yrday
fracday
Element set:     906
Inclination:       51
6444  deg
RA of node:       291
2246  deg
Eccentricity:     
0008293     
Arg of perigee:   253
5992  deg
Mean anomaly:     106
4250  deg
Mean motion:   15
55912020  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              35
Checksum:              294


Coasting Arc #8 (Orbit 38)
---------------------------------------

Vector Time (GMT): 2015/343/07:50:50
000
Vector Time (MET): N/A
Weight (LBS)     : 15581
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3339088
33                 A    =         6772878
78  meter
 Y    =       -2910647
24  meter          E    =           
0007211
 Z    =       -5129419
66                 I    =           51
28157
 XDOT =       3551
262514                 Wp   =          128
08297
 YDOT =      -6637
487526  meter/sec      RA   =          289
25485  deg
 ZDOT =       1451
654300                 TA   =          155
97898
                                          MA   =          155
94533
                                          Ha   =            216
567  n
mi
                                          Hp   =            215
030

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10955014
20                 X    =        -3281375
44
 Y    =       -9549367
58  feet           Y    =        -2947664
08  meter
 Z    =      -16828804
65                 Z    =        -5145500
55
 XDOT =      11651
123734                 XDOT =        3618
168896
 YDOT =     -21776
533878  feet/sec       YDOT =       -6597
400970  meter/sec
 ZDOT =       4762
645341                 ZDOT =        1469
067932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12905076
83                 X    =         3933467
42
 Y    =        6506810
96  feet           Y    =         1983275
98  meter
 Z    =      -16897687
01                 Z    =        -5150415
00
 XDOT =      -5278
735535                 XDOT =       -1608
958591
 YDOT =      23061
686696  feet/sec       YDOT =        7029
202105  meter/sec
 ZDOT =       4839
199315                 ZDOT =        1474
987951


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   15343
34049583  
00016717  00000-0  10270-3 0  9076
2 25544  51
6438 289
9437 0008039 257
1956 102
8300 15
55913858   392


Satellite: ISS
Catalog Number: 25544
Epoch time:      15343
34049583   =   yrday
fracday
Element set:     907
Inclination:       51
6438  deg
RA of node:       289
9437  deg
Eccentricity:     
0008039     
Arg of perigee:   257
1956  deg
Mean anomaly:     102
8300  deg
Mean motion:   15
55913858  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              39
Checksum:              332
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