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

 
Date: April 14th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 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 3492)
---------------------------------------

Vector Time (GMT): 2016/104/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3993702
20                 A    =         6779330
27  meter
 Y    =        2597445
66  meter          E    =           
0008891
 Z    =        4819044
07                 I    =           51
76043
 XDOT =      -5854
544738                 Wp   =           54
18609
 YDOT =      -4248
722071  meter/sec      RA   =           19
81793  deg
 ZDOT =      -2553
432535                 TA   =           60
93269
                                          MA   =           60
84367
                                          Ha   =            221
341  n
mi
                                          Hp   =            214
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13102697
51                 X    =        -4045859
61
 Y    =        8521803
36  feet           Y    =         2552494
05  meter
 Z    =       15810512
03                 Z    =         4799516
76
 XDOT =     -19207
823942                 XDOT =       -5794
195818
 YDOT =     -13939
376872  feet/sec       YDOT =       -4313
854182  meter/sec
 ZDOT =      -8377
403330                 ZDOT =       -2581
725769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4491555
93                 X    =        -1369026
25
 Y    =       15060544
03  feet           Y    =         4590453
82  meter
 Z    =       15725140
51                 Z    =         4793022
83
 XDOT =     -22517
975166                 XDOT =       -6863
478831
 YDOT =       2187
827483  feet/sec       YDOT =         666
849817  meter/sec
 ZDOT =      -8499
509100                 ZDOT =       -2590
650374


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   16104
59714581  
00016717  00000-0  10270-3 0  9009
2 25544  51
6440  20
1964 0001755  26
4811 333
6432 15
54212124 34934


Satellite: ISS
Catalog Number: 25544
Epoch time:      16104
59714581   =   yrday
fracday
Element set:     900
Inclination:       51
6440  deg
RA of node:        20
1964  deg
Eccentricity:     
0001755     
Arg of perigee:    26
4811  deg
Mean anomaly:     333
6432  deg
Mean motion:   15
54212124  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3493
Checksum:              277


Coasting Arc #2 (Orbit 3507)
---------------------------------------

Vector Time (GMT): 2016/105/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5313306
64                 A    =         6782963
92  meter
 Y    =       -1732970
95  meter          E    =           
0006788
 Z    =       -3849507
54                 I    =           51
74245
 XDOT =       4507
849709                 Wp   =           89
22621
 YDOT =       4589
319441  meter/sec      RA   =           14
83407  deg
 ZDOT =       4162
400179                 TA   =          224
52107
                                          MA   =          224
57563
                                          Ha   =            221
309  n
mi
                                          Hp   =            214
331

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17432108
39                 X    =         5350989
54
 Y    =       -5685600
24  feet           Y    =        -1673343
56  meter
 Z    =      -12629617
92                 Z    =        -3823605
14
 XDOT =      14789
533166                 XDOT =        4435
976572
 YDOT =      15056
822312  feet/sec       YDOT =        4639
327602  meter/sec
 ZDOT =      13656
168567                 ZDOT =        4184
123377

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9338023
04                 X    =         2846229
42
 Y    =      -15869618
49  feet           Y    =        -4837059
72  meter
 Z    =      -12516718
29                 Z    =        -3815095
73
 XDOT =      19832
226859                 XDOT =        6044
862747
 YDOT =        841
847347  feet/sec       YDOT =         256
595071  meter/sec
 ZDOT =      13749
651444                 ZDOT =        4190
893760


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   16105
56164073  
00016717  00000-0  10270-3 0  9013
2 25544  51
6445  15
3874 0001734  29
2184 330
9066 15
54196270 35089


Satellite: ISS
Catalog Number: 25544
Epoch time:      16105
56164073   =   yrday
fracday
Element set:     901
Inclination:       51
6445  deg
RA of node:        15
3874  deg
Eccentricity:     
0001734     
Arg of perigee:    29
2184  deg
Mean anomaly:     330
9066  deg
Mean motion:   15
54196270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3508
Checksum:              296


Coasting Arc #3 (Orbit 3523)
---------------------------------------

Vector Time (GMT): 2016/106/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6269210
98                 A    =         6786718
56  meter
 Y    =         861586
03  meter          E    =           
0014483
 Z    =        2436129
97                 I    =           51
72366
 XDOT =      -2743
321927                 Wp   =           99
28355
 YDOT =      -4762
178465  meter/sec      RA   =            9
85904  deg
 ZDOT =      -5350
680235                 TA   =           53
48124
                                          MA   =           53
34795
                                          Ha   =            221
387  n
mi
                                          Hp   =            214
217

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20568277
49                 X    =        -6290213
19
 Y    =        2826725
81  feet           Y    =          791362
29  meter
 Z    =        7992552
39                 Z    =         2405624
60
 XDOT =      -9000
400022                 XDOT =       -2663
874834
 YDOT =     -15623
945096  feet/sec       YDOT =       -4792
412297  meter/sec
 ZDOT =     -17554
725180                 ZDOT =       -5363
813303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13285568
74                 X    =        -4049441
35
 Y    =       16020051
00  feet           Y    =         4882911
54  meter
 Z    =        7859830
81                 Z    =         2395676
43
 XDOT =     -15942
849772                 XDOT =       -4859
380610
 YDOT =      -4540
592459  feet/sec       YDOT =       -1383
972581  meter/sec
 ZDOT =     -17610
843237                 ZDOT =       -5367
785018


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   16106
59042691  
00016717  00000-0  10270-3 0  9029
2 25544  51
6445  10
2581 0001730  37
0720 323
0552 15
54190340 35240


Satellite: ISS
Catalog Number: 25544
Epoch time:      16106
59042691   =   yrday
fracday
Element set:     902
Inclination:       51
6445  deg
RA of node:        10
2581  deg
Eccentricity:     
0001730     
Arg of perigee:    37
0720  deg
Mean anomaly:     323
0552  deg
Mean motion:   15
54190340  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3524
Checksum:              263


Coasting Arc #4 (Orbit 3538)
---------------------------------------

Vector Time (GMT): 2016/107/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6736333
45                 A    =         6788775
75  meter
 Y    =         -53090
96  meter          E    =           
0012111
 Z    =        -794028
68                 I    =           51
69969
 XDOT =        732
379026                 Wp   =           38
55073
 YDOT =       4780
316393  meter/sec      RA   =            4
88974  deg
 ZDOT =       5951
787975                 TA   =          312
87088
                                          MA   =          312
97253
                                          Ha   =            221
272  n
mi
                                          Hp   =            214
137

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22100831
52                 X    =         6740283
52
 Y    =        -174182
96  feet           Y    =           22261
21  meter
 Z    =       -2605080
98                 Z    =         -761295
59
 XDOT =       2402
818326                 XDOT =         649
958618
 YDOT =      15683
452734  feet/sec       YDOT =        4788
046018  meter/sec
 ZDOT =      19526
863436                 ZDOT =        5955
145094

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15920908
78                 X    =         4852692
99
 Y    =      -15353259
53  feet           Y    =        -4679673
50  meter
 Z    =       -2462849
21                 Z    =         -750676
44
 XDOT =      11330
639901                 XDOT =        3453
579042
 YDOT =       8647
372121  feet/sec       YDOT =        2635
719022  meter/sec
 ZDOT =      19540
499393                 ZDOT =        5955
944215


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   16107
55490367  
00016717  00000-0  10270-3 0  9034
2 25544  51
6448   5
4489 0001707  33
5712 326
5549 15
54235932 35399


Satellite: ISS
Catalog Number: 25544
Epoch time:      16107
55490367   =   yrday
fracday
Element set:     903
Inclination:       51
6448  deg
RA of node:         5
4489  deg
Eccentricity:     
0001707     
Arg of perigee:    33
5712  deg
Mean anomaly:     326
5549  deg
Mean motion:   15
54235932  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3539
Checksum:              317


Coasting Arc #5 (Orbit 3554)
---------------------------------------

Vector Time (GMT): 2016/108/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6671507
74                 A    =         6788683
43  meter
 Y    =        -762104
59  meter          E    =           
0009441
 Z    =        -975284
87                 I    =           51
66699
 XDOT =       1392
337018                 Wp   =          131
83100
 YDOT =      -4677
002986  meter/sec      RA   =          359
92234  deg
 ZDOT =      -5912
711275                 TA   =           58
72731
                                          MA   =           58
63487
                                          Ha   =            221
251  n
mi
                                          Hp   =            214
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21888148
74                 X    =        -6657752
32
 Y    =       -2500343
14  feet           Y    =         -836633
01  meter
 Z    =       -3199753
51                 Z    =        -1007660
04
 XDOT =       4568
034835                 XDOT =        1473
254479
 YDOT =     -15344
497987  feet/sec       YDOT =       -4660
981078  meter/sec
 ZDOT =     -19398
659040                 ZDOT =       -5905
750635

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17350879
19                 X    =        -5288547
98
 Y    =       13541449
75  feet           Y    =         4127433
88  meter
 Z    =       -3340258
04                 Z    =        -1018110
65
 XDOT =      -6420
282078                 XDOT =       -1956
901977
 YDOT =     -12970
423483  feet/sec       YDOT =       -3953
385078  meter/sec
 ZDOT =     -19367
489007                 ZDOT =       -5903
210649


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   16108
58367218  
00016717  00000-0  10270-3 0  9047
2 25544  51
6447    
3198 0001544  37
5604 322
5656 15
54198263 35550


Satellite: ISS
Catalog Number: 25544
Epoch time:      16108
58367218   =   yrday
fracday
Element set:     904
Inclination:       51
6447  deg
RA of node:          
3198  deg
Eccentricity:     
0001544     
Arg of perigee:    37
5604  deg
Mean anomaly:     322
5656  deg
Mean motion:   15
54198263  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3555
Checksum:              311


Coasting Arc #6 (Orbit 3570)
---------------------------------------

Vector Time (GMT): 2016/109/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6067830
63                 A    =         6786038
05  meter
 Y    =        1533437
79  meter          E    =           
0014912
 Z    =        2603851
20                 I    =           51
62609
 XDOT =      -3385
999845                 Wp   =           72
47009
 YDOT =       4465
245582  meter/sec      RA   =          354
94757  deg
 ZDOT =       5240
518987                 TA   =          316
86858
                                          MA   =          316
98531
                                          Ha   =            221
181  n
mi
                                          Hp   =            214
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19907580
80                 X    =         6037583
89
 Y    =        5030963
87  feet           Y    =         1601123
45  meter
 Z    =        8542818
90                 Z    =         2633253
80
 XDOT =     -11108
923377                 XDOT =       -3461
136051
 YDOT =      14649
755846  feet/sec       YDOT =        4426
961491  meter/sec
 ZDOT =      17193
303764                 ZDOT =        5223
887586

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17507285
98                 X    =         5336220
77
 Y    =      -10626565
85  feet           Y    =        -3238977
27  meter
 Z    =        8670245
76                 Z    =         2642690
91
 XDOT =       1804
928018                 XDOT =         550
142060
 YDOT =      16995
665921  feet/sec       YDOT =        5180
278973  meter/sec
 ZDOT =      17120
166972                 ZDOT =        5218
226893


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   16109
61243067  
00016717  00000-0  10270-3 0  9058
2 25544  51
6442 355
1897 0001752  35
0099 325
1169 15
54242640 35719


Satellite: ISS
Catalog Number: 25544
Epoch time:      16109
61243067   =   yrday
fracday
Element set:     905
Inclination:       51
6442  deg
RA of node:       355
1897  deg
Eccentricity:     
0001752     
Arg of perigee:    35
0099  deg
Mean anomaly:     325
1169  deg
Mean motion:   15
54242640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3571
Checksum:              301


Coasting Arc #7 (Orbit 3585)
---------------------------------------

Vector Time (GMT): 2016/110/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4978192
77                 A    =         6782152
57  meter
 Y    =       -2327664
65  meter          E    =           
0008357
 Z    =       -3983820
31                 I    =           51
58051
 XDOT =       5099
622135                 Wp   =           65
22485
 YDOT =      -4105
819713  meter/sec      RA   =          349
96193  deg
 ZDOT =      -3976
693893                 TA   =          163
29000
                                          MA   =          163
26245
                                          Ha   =            221
199  n
mi
                                          Hp   =            214
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16332653
44                 X    =        -4932442
36
 Y    =       -7636695
04  feet           Y    =        -2383078
70  meter
 Z    =      -13070276
60                 Z    =        -4007892
02
 XDOT =      16731
043749                 XDOT =        5164
472693
 YDOT =     -13470
537117  feet/sec       YDOT =       -4048
430135  meter/sec
 ZDOT =     -13046
895975                 ZDOT =       -3951
763024

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16728838
26                 X    =        -5098949
90
 Y    =        6518321
85  feet           Y    =         1986784
50  meter
 Z    =      -13174378
96                 Z    =        -4015550
71
 XDOT =       2290
760200                 XDOT =         698
223709
 YDOT =     -20249
221742  feet/sec       YDOT =       -6171
962787  meter/sec
 ZDOT =     -12937
785199                 ZDOT =       -3943
436929


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   16110
57688397  
00016717  00000-0  10270-3 0  9065
2 25544  51
6434 350
3809 0001618  36
4108 323
7155 15
54248538 35864


Satellite: ISS
Catalog Number: 25544
Epoch time:      16110
57688397   =   yrday
fracday
Element set:     906
Inclination:       51
6434  deg
RA of node:       350
3809  deg
Eccentricity:     
0001618     
Arg of perigee:    36
4108  deg
Mean anomaly:     323
7155  deg
Mean motion:   15
54248538  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3586
Checksum:              323


Coasting Arc #8 (Orbit 3601)
---------------------------------------

Vector Time (GMT): 2016/111/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3513395
42                 A    =         6778695
59  meter
 Y    =        3087675
16  meter          E    =           
0007074
 Z    =        4901325
04                 I    =           51
53731
 XDOT =      -6374
076959                 Wp   =          107
18272
 YDOT =       3600
835937  meter/sec      RA   =          344
96281  deg
 ZDOT =       2295
905144                 TA   =          320
32349
                                          MA   =          320
37522
                                          Ha   =            221
209  n
mi
                                          Hp   =            214
032

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11526887
87                 X    =         3454798
28
 Y    =       10130167
86  feet           Y    =         3126637
10  meter
 Z    =       16080462
72                 Z    =         4918249
86
 XDOT =     -20912
325982                 XDOT =       -6425
021344
 YDOT =      11813
766196  feet/sec       YDOT =        3529
272128  meter/sec
 ZDOT =       7532
497190                 ZDOT =        2264
816974

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15188576
06                 X    =         4629477
98
 Y    =       -1564203
79  feet           Y    =         -476769
32  meter
 Z    =       16153363
43                 Z    =         4923545
17
 XDOT =      -5584
274301                 XDOT =       -1702
086807
 YDOT =      22323
048886  feet/sec       YDOT =        6804
065301  meter/sec
 ZDOT =       7396
751237                 ZDOT =        2254
529777


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   16111
60562745  
00016717  00000-0  10270-3 0  9079
2 25544  51
6432 345
2509 0001778  42
4221 317
7069 15
54243152 36025


Satellite: ISS
Catalog Number: 25544
Epoch time:      16111
60562745   =   yrday
fracday
Element set:     907
Inclination:       51
6432  deg
RA of node:       345
2509  deg
Eccentricity:     
0001778     
Arg of perigee:    42
4221  deg
Mean anomaly:     317
7069  deg
Mean motion:   15
54243152  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3602
Checksum:              288


Coasting Arc #9 (Orbit 3616)
---------------------------------------

Vector Time (GMT): 2016/112/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1817566
82                 A    =         6776906
92  meter
 Y    =       -3827203
06  meter          E    =           
0016077
 Z    =       -5303105
13                 I    =           51
49944
 XDOT =       7085
817960                 Wp   =           83
02767
 YDOT =      -2880
754903  meter/sec      RA   =          339
95297  deg
 ZDOT =       -348
552791                 TA   =          183
63193
                                          MA   =          183
64361
                                          Ha   =            221
202  n
mi
                                          Hp   =            213
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5963145
72                 X    =        -1748874
35
 Y    =      -12556440
49  feet           Y    =        -3847144
64  meter
 Z    =      -17398638
89                 Z    =        -5311767
42
 XDOT =      23247
434252                 XDOT =        7119
197792
 YDOT =      -9451
295615  feet/sec       YDOT =       -2801
329962  meter/sec
 ZDOT =      -1143
545903                 ZDOT =        -314
049776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13278077
49                 X    =        -4047158
02
 Y    =       -3953716
98  feet           Y    =        -1205092
94  meter
 Z    =      -17435501
72                 Z    =        -5314340
92
 XDOT =       8068
065256                 XDOT =        2459
146290
 YDOT =     -22701
614097  feet/sec       YDOT =       -6919
451977  meter/sec
 ZDOT =       -993
121608                 ZDOT =        -302
703466


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   16112
57006417  
00016717  00000-0  10270-3 0  9086
2 25544  51
6417 340
4408 0001678  43
5343 316
5942 15
54293950 36173


Satellite: ISS
Catalog Number: 25544
Epoch time:      16112
57006417   =   yrday
fracday
Element set:     908
Inclination:       51
6417  deg
RA of node:       340
4408  deg
Eccentricity:     
0001678     
Arg of perigee:    43
5343  deg
Mean anomaly:     316
5942  deg
Mean motion:   15
54293950  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3617
Checksum:              303


Coasting Arc #10 (Orbit 3632)
---------------------------------------

Vector Time (GMT): 2016/113/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          38359
90                 A    =         6777805
98  meter
 Y    =        4462592
61  meter          E    =           
0006725
 Z    =        5097613
53                 I    =           51
47278
 XDOT =      -7238
263276                 Wp   =           52
40858
 YDOT =       1942
451162  meter/sec      RA   =          334
94084  deg
 ZDOT =      -1640
498319                 TA   =           53
48527
                                          MA   =           53
42335
                                          Ha   =            221
191  n
mi
                                          Hp   =            213
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         125852
68                 X    =          -36307
26
 Y    =       14641051
88  feet           Y    =         4462604
42  meter
 Z    =       16724453
85                 Z    =         5097618
24
 XDOT =     -23747
582927                 XDOT =       -7251
477297
 YDOT =       6372
871265  feet/sec       YDOT =        1861
434097  meter/sec
 ZDOT =      -5382
212332                 ZDOT =       -1675
692876

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11133225
68                 X    =         3393407
19
 Y    =        9510859
29  feet           Y    =         2898909
91  meter
 Z    =       16723589
25                 Z    =         5097350
00
 XDOT =      -9891
045842                 XDOT =       -3014
790773
 YDOT =      21343
394071  feet/sec       YDOT =        6505
466513  meter/sec
 ZDOT =      -5535
444025                 ZDOT =       -1687
203339


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   16113
59878991  
00016717  00000-0  10270-3 0  9094
2 25544  51
6418 335
3111 0001597  45
8731 314
2553 15
54294791 36339


Satellite: ISS
Catalog Number: 25544
Epoch time:      16113
59878991   =   yrday
fracday
Element set:     909
Inclination:       51
6418  deg
RA of node:       335
3111  deg
Eccentricity:     
0001597     
Arg of perigee:    45
8731  deg
Mean anomaly:     314
2553  deg
Mean motion:   15
54294791  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3633
Checksum:              327


Coasting Arc #11 (Orbit 3647)
---------------------------------------

Vector Time (GMT): 2016/114/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1633160
60                 A    =         6780831
75  meter
 Y    =       -4948614
53  meter          E    =           
0009569
 Z    =       -4347933
17                 I    =           51
45293
 XDOT =       6801
603075                 Wp   =          101
70849
 YDOT =       -772
287663  meter/sec      RA   =          329
93068  deg
 ZDOT =       3438
312378                 TA   =          203
29272
                                          MA   =          203
33611
                                          Ha   =            221
205  n
mi
                                          Hp   =            213
932

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5358138
45                 X    =         1709496
67
 Y    =      -16235611
97  feet           Y    =        -4929924
82  meter
 Z    =      -14264872
62                 Z    =        -4339813
88
 XDOT =      22314
970720                 XDOT =        6793
031303
 YDOT =      -2533
752175  feet/sec       YDOT =        -696
275379  meter/sec
 ZDOT =      11280
552421                 ZDOT =        3471
332734

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9038861
78                 X    =        -2755045
07
 Y    =      -14547726
22  feet           Y    =        -4434146
95  meter
 Z    =      -14228632
19                 Z    =        -4336887
09
 XDOT =      11162
719507                 XDOT =        3402
396906
 YDOT =     -18094
628506  feet/sec       YDOT =       -5515
242769  meter/sec
 ZDOT =      11424
102063                 ZDOT =        3482
066309


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   16114
56321280  
00016717  00000-0  10270-3 0  9108
2 25544  51
6404 330
5003 0001617  51
3633 308
7664 15
54311741 36489


Satellite: ISS
Catalog Number: 25544
Epoch time:      16114
56321280   =   yrday
fracday
Element set:     910
Inclination:       51
6404  deg
RA of node:       330
5003  deg
Eccentricity:     
0001617     
Arg of perigee:    51
3633  deg
Mean anomaly:     308
7664  deg
Mean motion:   15
54311741  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3648
Checksum:              271


Coasting Arc #12 (Orbit 3663)
---------------------------------------

Vector Time (GMT): 2016/115/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3102204
16                 A    =         6784700
81  meter
 Y    =        5179890
29  meter          E    =           
0014122
 Z    =        3082252
31                 I    =           51
43938
 XDOT =      -5890
043831                 Wp   =           90
69009
 YDOT =       -614
499114  meter/sec      RA   =          324
93034  deg
 ZDOT =      -4876
272272                 TA   =           53
75638
                                          MA   =           53
62595
                                          Ha   =            221
126  n
mi
                                          Hp   =            213
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10177835
17                 X    =        -3174868
97
 Y    =       16994390
71  feet           Y    =         5144793
18  meter
 Z    =       10112376
35                 Z    =         3067005
63
 XDOT =     -19324
290784                 XDOT =       -5859
047293
 YDOT =      -2016
073209  feet/sec       YDOT =        -680
192338  meter/sec
 ZDOT =     -15998
268609                 ZDOT =       -4904
809881

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6889789
66                 X    =         2100007
89
 Y    =       18608700
20  feet           Y    =         5671931
82  meter
 Z    =       10045141
87                 Z    =         3061759
24
 XDOT =     -12212
974508                 XDOT =       -3722
514630
 YDOT =      13258
869015  feet/sec       YDOT =        4041
303276  meter/sec
 ZDOT =     -16122
071516                 ZDOT =       -4914
007398


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   16115
59192086  
00016717  00000-0  10270-3 0  9113
2 25544  51
6408 325
3701 0001566  46
6887 313
4397 15
54353236 36640


Satellite: ISS
Catalog Number: 25544
Epoch time:      16115
59192086   =   yrday
fracday
Element set:     911
Inclination:       51
6408  deg
RA of node:       325
3701  deg
Eccentricity:     
0001566     
Arg of perigee:    46
6887  deg
Mean anomaly:     313
4397  deg
Mean motion:   15
54353236  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3664
Checksum:              317


Coasting Arc #13 (Orbit 3678)
---------------------------------------

Vector Time (GMT): 2016/116/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4208295
06                 A    =         6787814
33  meter
 Y    =       -5104739
98  meter          E    =           
0009860
 Z    =       -1502325
63                 I    =           51
42292
 XDOT =       4609
387684                 Wp   =           40
70453
 YDOT =       2116
175300  meter/sec      RA   =          319
93737  deg
 ZDOT =       5749
890018                 TA   =          302
84050
                                          MA   =          302
93540
                                          Ha   =            221
220  n
mi
                                          Hp   =            213
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13806742
32                 X    =         4272362
55
 Y    =      -16747834
57  feet           Y    =        -5057321
82  meter
 Z    =       -4928889
87                 Z    =        -1481726
72
 XDOT =      15122
663006                 XDOT =        4557
450510
 YDOT =       6942
832349  feet/sec       YDOT =        2167
430234  meter/sec
 ZDOT =      18864
468564                 ZDOT =        5772
155488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4818381
75                 X    =        -1468642
76
 Y    =      -21184494
76  feet           Y    =        -6457034
00  meter
 Z    =       -4838432
68                 Z    =        -1474754
28
 XDOT =      13112
907007                 XDOT =        3996
814056
 YDOT =      -7291
165207  feet/sec       YDOT =       -2222
347155  meter/sec
 ZDOT =      18960
735786                 ZDOT =        5779
232268


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   16116
55632990  
00016717  00000-0  10270-3 0  9124
2 25544  51
6398 320
5595 0001593  59
4929 300
6381 15
54330827 36793


Satellite: ISS
Catalog Number: 25544
Epoch time:      16116
55632990   =   yrday
fracday
Element set:     912
Inclination:       51
6398  deg
RA of node:       320
5595  deg
Eccentricity:     
0001593     
Arg of perigee:    59
4929  deg
Mean anomaly:     300
6381  deg
Mean motion:   15
54330827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3679
Checksum:              331


Coasting Arc #14 (Orbit 3694)
---------------------------------------

Vector Time (GMT): 2016/117/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4949125
31                 A    =         6788534
64  meter
 Y    =        4630710
15  meter          E    =           
0011833
 Z    =        -289478
83                 I    =           51
40231
 XDOT =      -3090
055070                 Wp   =          128
42939
 YDOT =      -3665
781290  meter/sec      RA   =          314
94997  deg
 ZDOT =      -5984
213593                 TA   =           54
70046
                                          MA   =           54
58985
                                          Ha   =            221
127  n
mi
                                          Hp   =            213
727

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16237287
75                 X    =        -4999133
05
 Y    =       15192618
59  feet           Y    =         4575086
13  meter
 Z    =        -949733
68                 Z    =         -313642
31
 XDOT =     -10137
975953                 XDOT =       -3019
764544
 YDOT =     -12026
841502  feet/sec       YDOT =       -3699
943361  meter/sec
 ZDOT =     -19633
246695                 ZDOT =       -5999
053788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2505896
11                 X    =          763797
13
 Y    =       22090120
44  feet           Y    =         6733068
71  meter
 Z    =       -1055571
30                 Z    =         -321738
13
 XDOT =     -14015
576765                 XDOT =       -4271
947798
 YDOT =        673
169703  feet/sec       YDOT =         205
182125  meter/sec
 ZDOT =     -19696
966057                 ZDOT =       -6003
635254


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   16117
58502221  
00016717  00000-0  10270-3 0  9132
2 25544  51
6401 315
4292 0001743  55
9149 304
2169 15
54386220 36957


Satellite: ISS
Catalog Number: 25544
Epoch time:      16117
58502221   =   yrday
fracday
Element set:     913
Inclination:       51
6401  deg
RA of node:       315
4292  deg
Eccentricity:     
0001743     
Arg of perigee:    55
9149  deg
Mean anomaly:     304
2169  deg
Mean motion:   15
54386220  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3695
Checksum:              293


Coasting Arc #15 (Orbit 3710)
---------------------------------------

Vector Time (GMT): 2016/118/13:16:58
235
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5259640
11                 A    =         6786895
31  meter
 Y    =       -3775623
71  meter          E    =           
0015580
 Z    =        2010854
43                 I    =           51
37411
 XDOT =       1518
662023                 Wp   =           68
59257
 YDOT =       5082
805815  meter/sec      RA   =          309
95855  deg
 ZDOT =       5542
242002                 TA   =          313
72003
                                          MA   =          313
84896
                                          Ha   =            221
163  n
mi
                                          Hp   =            213
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17256037
11                 X    =         5291701
18
 Y    =      -12387216
90  feet           Y    =        -3716627
65  meter
 Z    =        6597291
43                 Z    =         2036482
65
 XDOT =       4982
486953                 XDOT =        1434
789785
 YDOT =      16675
872098  feet/sec       YDOT =        5099
319558  meter/sec
 ZDOT =      18183
208669                 ZDOT =        5549
415647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -32865
50                 X    =          -10017
40
 Y    =      -21206654
66  feet           Y    =        -6463788
34  meter
 Z    =        6709316
76                 Z    =         2044999
75
 XDOT =      14841
345070                 XDOT =        4523
641977
 YDOT =       5769
000203  feet/sec       YDOT =        1758
391262  meter/sec
 ZDOT =      18213
363500                 ZDOT =        5551
433195


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   16118
61370831  
00016717  00000-0  10270-3 0  9148
2 25544  51
6396 310
2981 0001646  68
9656 291
1673 15
54357152 37112


Satellite: ISS
Catalog Number: 25544
Epoch time:      16118
61370831   =   yrday
fracday
Element set:     914
Inclination:       51
6396  deg
RA of node:       310
2981  deg
Eccentricity:     
0001646     
Arg of perigee:    68
9656  deg
Mean anomaly:     291
1673  deg
Mean motion:   15
54357152  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3711
Checksum:              314
Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list