[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 27th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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 1972)
---------------------------------------
Vector Time (GMT): 2013/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6167709
89 A = 6799616
53 meter
Y = -2771945
26 meter E =
0013793
Z = 651166
49 I = 51
84277
XDOT = 1417
491679 Wp = 125
63360
YDOT = -4577
886562 meter/sec RA = 28
53983 deg
ZDOT = -5980
340441 TA = 47
36444
MA = 47
24825
Ha = 226
977 n
mi
Hp = 220
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20235268
65 X = -6139418
20
Y = -9094308
60 feet Y = -2840758
34 meter
Z = 2136373
01 Z = 621272
66
XDOT = 4650
563251 XDOT = 1497
628469
YDOT = -15019
312868 feet/sec YDOT = -4561
587124 meter/sec
ZDOT = -19620
539505 ZDOT = -5973
259722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17106028
74 X = 5213917
56
Y = -14144818
42 feet Y = -4311340
65 meter
Z = 2011101
35 Z = 612983
69
XDOT = 10334
001932 XDOT = 3149
803789
YDOT = 9671
968363 feet/sec YDOT = 2948
015957 meter/sec
ZDOT = -19589
972133 ZDOT = -5971
023506
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 13329
53345040
00016717 00000-0 10270-3 0 9009
2 25544 51
6493 28
9529 0000902 89
4027 270
7227 15
50542373 19738
Satellite: ISS
Catalog Number: 25544
Epoch time: 13329
53345040 = yrday
fracday
Element set: 900
Inclination: 51
6493 deg
RA of node: 28
9529 deg
Eccentricity:
0000902
Arg of perigee: 89
4027 deg
Mean anomaly: 270
7227 deg
Mean motion: 15
50542373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1973
Checksum: 301
Coasting Arc #2 (Orbit 1987)
---------------------------------------
Vector Time (GMT): 2013/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6270012
09 A = 6799842
62 meter
Y = 2612506
98 meter E =
0012659
Z = -147399
37 I = 51
81549
XDOT = -1708
464168 Wp = 46
74073
YDOT = 4421
193109 meter/sec RA = 23
59779 deg
ZDOT = 6020
977468 TA = 311
67764
MA = 311
78592
Ha = 227
050 n
mi
Hp = 219
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20570905
82 X = 6241048
49
Y = 8571217
11 feet Y = 2682460
30 meter
Z = -483593
74 Z = -117010
16
XDOT = -5605
197402 XDOT = -1787
024613
YDOT = 14505
226736 feet/sec YDOT = 4401
648699 meter/sec
ZDOT = 19753
863084 ZDOT = 6012
486986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16525896
42 X = -5037093
23
Y = 14954251
84 feet Y = 4558055
96 meter
Z = -356218
07 Z = -108575
27
XDOT = -9588
702701 XDOT = -2922
636583
YDOT = -10162
166781 feet/sec YDOT = -3097
428435 meter/sec
ZDOT = 19717
391046 ZDOT = 6009
860791
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 13330
50021195
00016717 00000-0 10270-3 0 9011
2 25544 51
6491 24
1599 0000951 79
8264 280
2994 15
50516516 19884
Satellite: ISS
Catalog Number: 25544
Epoch time: 13330
50021195 = yrday
fracday
Element set: 901
Inclination: 51
6491 deg
RA of node: 24
1599 deg
Eccentricity:
0000951
Arg of perigee: 79
8264 deg
Mean anomaly: 280
2994 deg
Mean motion: 15
50516516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1988
Checksum: 309
Coasting Arc #3 (Orbit 2003)
---------------------------------------
Vector Time (GMT): 2013/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6315584
39 A = 6799498
02 meter
Y = -2471852
47 meter E =
0011819
Z = -408940
40 I = 51
78731
XDOT = 2061
157506 Wp = 133
70064
YDOT = -4292
357065 meter/sec RA = 18
65395 deg
ZDOT = -6003
108623 TA = 50
69264
MA = 50
58791
Ha = 226
902 n
mi
Hp = 219
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20720421
22 X = -6285487
64
Y = -8109752
20 feet Y = -2542309
08 meter
Z = -1341667
96 Z = -439548
31
XDOT = 6762
327777 XDOT = 2138
164340
YDOT = -14082
536302 feet/sec YDOT = -4268
877324 meter/sec
ZDOT = -19695
238266 ZDOT = -5992
908495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15902378
30 X = 4847044
91
Y = -15551769
47 feet Y = -4740179
33 meter
Z = -1469979
57 Z = -448049
77
XDOT = 8878
507557 XDOT = 2706
169103
YDOT = 10903
245519 feet/sec YDOT = 3323
309234 meter/sec
ZDOT = -19651
596124 ZDOT = -5989
806498
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 13331
53140299
00016717 00000-0 10270-3 0 9023
2 25544 51
6498 19
0469 0001040 87
5360 272
5910 15
50607254 20045
Satellite: ISS
Catalog Number: 25544
Epoch time: 13331
53140299 = yrday
fracday
Element set: 902
Inclination: 51
6498 deg
RA of node: 19
0469 deg
Eccentricity:
0001040
Arg of perigee: 87
5360 deg
Mean anomaly: 272
5910 deg
Mean motion: 15
50607254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2004
Checksum: 282
Coasting Arc #4 (Orbit 2019)
---------------------------------------
Vector Time (GMT): 2013/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6323887
05 A = 6799254
35 meter
Y = 2297777
52 meter E =
0014565
Z = 930954
73 I = 51
75619
XDOT = -2413
982702 Wp = 57
07924
YDOT = 4218
678454 meter/sec RA = 13
70791 deg
ZDOT = 5925
897676 TA = 312
97083
MA = 313
09286
Ha = 227
003 n
mi
Hp = 219
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20747660
94 X = 6293200
38
Y = 7538640
17 feet Y = 2368323
67 meter
Z = 3054313
42 Z = 961601
65
XDOT = -7919
890753 XDOT = -2489
764432
YDOT = 13840
808575 feet/sec YDOT = 4191
260023 meter/sec
ZDOT = 19441
921510 ZDOT = 5913
986485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15114537
28 X = -4606910
96
Y = 16063805
31 feet Y = 4896247
86 meter
Z = 3182810
44 Z = 970120
62
XDOT = -8368
428309 XDOT = -2550
696949
YDOT = -11753
112406 feet/sec YDOT = -3582
348661 meter/sec
ZDOT = 19391
094238 ZDOT = 5910
405524
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 13332
56257368
00016717 00000-0 10270-3 0 9034
2 25544 51
6492 13
9342 0001180 81
3504 278
7781 15
50585373 20208
Satellite: ISS
Catalog Number: 25544
Epoch time: 13332
56257368 = yrday
fracday
Element set: 903
Inclination: 51
6492 deg
RA of node: 13
9342 deg
Eccentricity:
0001180
Arg of perigee: 81
3504 deg
Mean anomaly: 278
7781 deg
Mean motion: 15
50585373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2020
Checksum: 296
Coasting Arc #5 (Orbit 2034)
---------------------------------------
Vector Time (GMT): 2013/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6267983
65 A = 6798418
66 meter
Y = -2158360
74 meter E =
0008938
Z = -1493803
10 I = 51
72493
XDOT = 2808
263073 Wp = 135
90239
YDOT = -4177
474323 meter/sec RA = 8
75926 deg
ZDOT = -5774
571195 TA = 60
35877
MA = 60
26978
Ha = 226
844 n
mi
Hp = 219
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20564250
81 X = -6236125
88
Y = -7081236
01 feet Y = -2228275
17 meter
Z = -4900928
81 Z = -1524175
71
XDOT = 9213
461527 XDOT = 2882
819704
YDOT = -13705
624419 feet/sec YDOT = -4145
653568 meter/sec
ZDOT = -18945
443553 ZDOT = -5760
747586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14338973
14 X = 4370519
01
Y = -16314459
45 feet Y = -4972647
24 meter
Z = -5028287
97 Z = -1532622
17
XDOT = 7955
404079 XDOT = 2424
807163
YDOT = 12786
472332 feet/sec YDOT = 3897
316767 meter/sec
ZDOT = -18886
578739 ZDOT = -5756
629200
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 13333
52927270
00016717 00000-0 10270-3 0 9048
2 25544 51
6501 9
1407 0001164 90
2022 269
9262 15
50665572 20356
Satellite: ISS
Catalog Number: 25544
Epoch time: 13333
52927270 = yrday
fracday
Element set: 904
Inclination: 51
6501 deg
RA of node: 9
1407 deg
Eccentricity:
0001164
Arg of perigee: 90
2022 deg
Mean anomaly: 269
9262 deg
Mean motion: 15
50665572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 278
Coasting Arc #6 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2013/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6169658
27 A = 6797657
55 meter
Y = 2002162
49 meter E =
0015186
Z = 2010092
99 I = 51
69065
XDOT = -3185
335686 Wp = 69
96573
YDOT = 4196
446896 meter/sec RA = 3
80788 deg
ZDOT = 5567
881734 TA = 312
19672
MA = 312
32554
Ha = 226
910 n
mi
Hp = 219
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20241660
98 X = 6137046
38
Y = 6568774
59 feet Y = 2070973
12 meter
Z = 6594793
26 Z = 2039986
19
XDOT = -10450
576399 XDOT = -3259
072425
YDOT = 13767
870395 feet/sec YDOT = 4160
413938 meter/sec
ZDOT = 18267
328525 ZDOT = 5552
228363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13457890
09 X = -4101964
90
Y = 16434403
79 feet Y = 5009206
27 meter
Z = 6720156
49 Z = 2048303
70
XDOT = -7793
369739 XDOT = -2375
419096
YDOT = -13862
627713 feet/sec YDOT = -4225
328927 meter/sec
ZDOT = 18200
763015 ZDOT = 5547
592567
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 13334
56040046
00016717 00000-0 10270-3 0 9051
2 25544 51
6490 4
0277 0001337 86
1767 273
9537 15
50661934 20510
Satellite: ISS
Catalog Number: 25544
Epoch time: 13334
56040046 = yrday
fracday
Element set: 905
Inclination: 51
6490 deg
RA of node: 4
0277 deg
Eccentricity:
0001337
Arg of perigee: 86
1767 deg
Mean anomaly: 273
9537 deg
Mean motion: 15
50661934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2051
Checksum: 295
Coasting Arc #7 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2013/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6006278
81 A = 6796414
38 meter
Y = -1898290
14 meter E =
0006181
Z = -2551441
18 I = 51
65688
XDOT = 3577
410502 Wp = 121
07792
YDOT = -4245
287965 meter/sec RA = 358
85314 deg
ZDOT = -5275
558008 TA = 87
52020
MA = 87
44944
Ha = 226
777 n
mi
Hp = 219
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19705639
13 X = -5972210
81
Y = -6227986
04 feet Y = -1965265
52 meter
Z = -8370870
01 Z = -2580537
18
XDOT = 11736
911097 XDOT = 3650
244179
YDOT = -13928
110123 feet/sec YDOT = -4204
875500 meter/sec
ZDOT = -17308
261181 ZDOT = -5258
002242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12663835
97 X = 3859937
20
Y = -16268666
07 feet Y = -4958689
42 meter
Z = -8492894
17 Z = -2588634
14
XDOT = 7765
199960 XDOT = 2366
832948
YDOT = 15019
985320 feet/sec YDOT = 4578
091525 meter/sec
ZDOT = -17233
683765 ZDOT = -5252
826812
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 13335
52706011
00016717 00000-0 10270-3 0 9060
2 25544 51
6496 359
2338 0001238 93
9884 266
1409 15
50723097 20662
Satellite: ISS
Catalog Number: 25544
Epoch time: 13335
52706011 = yrday
fracday
Element set: 906
Inclination: 51
6496 deg
RA of node: 359
2338 deg
Eccentricity:
0001238
Arg of perigee: 93
9884 deg
Mean anomaly: 266
1409 deg
Mean motion: 15
50723097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 316
Coasting Arc #8 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2013/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5801656
55 A = 6795219
97 meter
Y = 1795971
80 meter E =
0014379
Z = 3033854
18 I = 51
62093
XDOT = -3936
653389 Wp = 84
42659
YDOT = 4350
820846 meter/sec RA = 353
89498 deg
ZDOT = 4933
711556 TA = 310
32815
MA = 310
45368
Ha = 226
766 n
mi
Hp = 219
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19034306
28 X = 5766404
47
Y = 5892295
92 feet Y = 1860652
24 meter
Z = 9953589
82 Z = 3061953
19
XDOT = -12915
529491 XDOT = -4008
979752
YDOT = 14274
346608 feet/sec YDOT = 4306
393842 meter/sec
ZDOT = 16186
717703 ZDOT = 4914
411977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11840029
04 X = -3608840
85
Y = 15952359
65 feet Y = 4862279
22 meter
Z = 10071437
39 Z = 3069774
12
XDOT = -8000
066862 XDOT = -2438
420380
YDOT = -16143
873614 feet/sec YDOT = -4920
652677 meter/sec
ZDOT = 16104
784889 ZDOT = 4908
738434
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 13336
55814497
00016717 00000-0 10270-3 0 9073
2 25544 51
6483 354
1201 0001370 91
8962 268
2346 15
50739739 20823
Satellite: ISS
Catalog Number: 25544
Epoch time: 13336
55814497 = yrday
fracday
Element set: 907
Inclination: 51
6483 deg
RA of node: 354
1201 deg
Eccentricity:
0001370
Arg of perigee: 91
8962 deg
Mean anomaly: 268
2346 deg
Mean motion: 15
50739739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2082
Checksum: 320
Coasting Arc #9 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2013/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5539473
61 A = 6793736
64 meter
Y = -1762422
24 meter E =
0006462
Z = -3522095
03 I = 51
58604
XDOT = 4281
517806 Wp = 86
36328
YDOT = -4474
717417 meter/sec RA = 348
93312 deg
ZDOT = -4501
520820 TA = 135
03966
MA = 134
98732
Ha = 226
703 n
mi
Hp = 219
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18174126
01 X = -5502244
47
Y = -5782225
19 feet Y = -1824159
63 meter
Z = -11555429
88 Z = -3548915
44
XDOT = 14046
974429 XDOT = 4353
104359
YDOT = -14680
831420 feet/sec YDOT = -4426
438031 meter/sec
ZDOT = -14768
769096 ZDOT = -4480
547865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11185706
53 X = 3409403
35
Y = -15362319
51 feet Y = -4682434
99 meter
Z = -11667906
95 Z = -3556378
04
XDOT = 8366
747415 XDOT = 2550
184612
YDOT = 17224
895853 feet/sec YDOT = 5250
148256 meter/sec
ZDOT = -14679
774090 ZDOT = -4474
395143
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 13337
52476562
00016717 00000-0 10270-3 0 9089
2 25544 51
6485 349
3257 0001280 97
3537 262
7760 15
50782374 20979
Satellite: ISS
Catalog Number: 25544
Epoch time: 13337
52476562 = yrday
fracday
Element set: 908
Inclination: 51
6485 deg
RA of node: 349
3257 deg
Eccentricity:
0001280
Arg of perigee: 97
3537 deg
Mean anomaly: 262
7760 deg
Mean motion: 15
50782374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2097
Checksum: 332
Coasting Arc #10 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2013/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5243410
89 A = 6792321
65 meter
Y = 1747624
22 meter E =
0012274
Z = 3939289
11 I = 51
55056
XDOT = -4582
384175 Wp = 99
63369
YDOT = 4643
350365 meter/sec RA = 343
96761 deg
ZDOT = 4026
699504 TA = 308
19210
MA = 308
30258
Ha = 226
600 n
mi
Hp = 219
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17202791
65 X = 5204342
70
Y = 5733675
26 feet Y = 1806040
52 meter
Z = 12924176
87 Z = 3964666
64
XDOT = -15034
068816 XDOT = -4653
527355
YDOT = 15234
089124 feet/sec YDOT = 4591
709021 meter/sec
ZDOT = 13210
956379 ZDOT = 4004
266182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10581273
81 X = -3225172
26
Y = 14631670
00 feet Y = 4459733
01 meter
Z = 13030590
85 Z = 3971724
09
XDOT = -8965
329404 XDOT = -2732
632402
YDOT = -18200
996451 feet/sec YDOT = -5547
663718 meter/sec
ZDOT = 13115
788363 ZDOT = 3997
692293
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 13338
55580783
00016717 00000-0 10270-3 0 9095
2 25544 51
6476 344
2114 0001315 97
0376 263
0925 15
50811590 21131
Satellite: ISS
Catalog Number: 25544
Epoch time: 13338
55580783 = yrday
fracday
Element set: 909
Inclination: 51
6476 deg
RA of node: 344
2114 deg
Eccentricity:
0001315
Arg of perigee: 97
0376 deg
Mean anomaly: 263
0925 deg
Mean motion: 15
50811590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 300
Coasting Arc #11 (Orbit 2127)
---------------------------------------
Vector Time (GMT): 2013/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4906006
05 A = 6790845
08 meter
Y = -1813246
76 meter E =
0009925
Z = -4341170
57 I = 51
51654
XDOT = 4841
315315 Wp = 72
97444
YDOT = -4809
911804 meter/sec RA = 338
99839 deg
ZDOT = -3465
930142 TA = 161
70070
MA = 161
66497
Ha = 226
627 n
mi
Hp = 219
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16095820
38 X = -4864277
00
Y = -5948972
33 feet Y = -1867875
11 meter
Z = -14242685
60 Z = -4364902
41
XDOT = 15883
580431 XDOT = 4911
577602
YDOT = -15780
550538 feet/sec YDOT = -4755
379946 meter/sec
ZDOT = -11371
161882 ZDOT = -3442
241177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10220392
76 X = 3115175
71
Y = -13680845
64 feet Y = -4169921
75 meter
Z = -14342169
75 Z = -4371493
34
XDOT = 9647
495387 XDOT = 2940
556594
YDOT = 19009
978420 feet/sec YDOT = 5794
241423 meter/sec
ZDOT = -11270
684677 ZDOT = -3435
304689
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 13339
52238955
00016717 00000-0 10270-3 0 9106
2 25544 51
6476 339
4168 0001311 100
5892 259
5407 15
50841894 21286
Satellite: ISS
Catalog Number: 25544
Epoch time: 13339
52238955 = yrday
fracday
Element set: 910
Inclination: 51
6476 deg
RA of node: 339
4168 deg
Eccentricity:
0001311
Arg of perigee: 100
5892 deg
Mean anomaly: 259
5407 deg
Mean motion: 15
50841894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2128
Checksum: 316
Coasting Arc #12 (Orbit 2143)
---------------------------------------
Vector Time (GMT): 2013/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4547066
94 A = 6789503
87 meter
Y = 1910742
84 meter E =
0009224
Z = 4660334
66 I = 51
48343
XDOT = -5051
648483 Wp = 113
80332
YDOT = 5001
880811 meter/sec RA = 334
02589 deg
ZDOT = 2869
936385 TA = 307
57083
MA = 307
65457
Ha = 226
451 n
mi
Hp = 219
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14918198
64 X = 4502724
00
Y = 6268841
33 feet Y = 1961342
74 meter
Z = 15289811
89 Z = 4682316
35
XDOT = -16573
649880 XDOT = -5121
146546
YDOT = 16410
370115 feet/sec YDOT = 4945
001253 meter/sec
ZDOT = 9415
801789 ZDOT = 2845
227506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9977892
39 X = -3041261
60
Y = 12628045
86 feet Y = 3849028
38 meter
Z = 15381920
91 Z = 4688409
49
XDOT = -10489
758781 XDOT = -3197
278476
YDOT = -19662
265454 feet/sec YDOT = -5993
058510 meter/sec
ZDOT = 9311
005416 ZDOT = 2837
994451
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 13340
55338932
00016717 00000-0 10270-3 0 9118
2 25544 51
6472 334
3025 0001244 101
2439 258
8852 15
50876044 21447
Satellite: ISS
Catalog Number: 25544
Epoch time: 13340
55338932 = yrday
fracday
Element set: 911
Inclination: 51
6472 deg
RA of node: 334
3025 deg
Eccentricity:
0001244
Arg of perigee: 101
2439 deg
Mean anomaly: 258
8852 deg
Mean motion: 15
50876044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2144
Checksum: 289
Coasting Arc #13 (Orbit 2158)
---------------------------------------
Vector Time (GMT): 2013/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4170228
58 A = 6788325
82 meter
Y = -2092071
91 meter E =
0013564
Z = -4943445
24 I = 51
45233
XDOT = 5199
632269 Wp = 76
47413
YDOT = -5164
595715 meter/sec RA = 329
04972 deg
ZDOT = -2202
685023 TA = 171
94218
MA = 171
92037
Ha = 226
541 n
mi
Hp = 219
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13681852
29 X = -4122510
73
Y = -6863753
00 feet Y = -2138438
97 meter
Z = -16218652
36 Z = -4963588
03
XDOT = 17059
160987 XDOT = 5267
697510
YDOT = -16944
211665 feet/sec YDOT = -5106
069414 meter/sec
ZDOT = -7226
656900 ZDOT = -2177
260671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10026609
93 X = 3056110
71
Y = -11446756
43 feet Y = -3488971
36 meter
Z = -16302997
64 Z = -4969153
68
XDOT = 11324
496109 XDOT = 3451
706414
YDOT = 20049
170600 feet/sec YDOT = 6110
987199 meter/sec
ZDOT = -7118
829843 ZDOT = -2169
819336
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 13341
51993162
00016717 00000-0 10270-3 0 9128
2 25544 51
6471 329
5077 0001318 104
1373 255
9925 15
50901480 21598
Satellite: ISS
Catalog Number: 25544
Epoch time: 13341
51993162 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 329
5077 deg
Eccentricity:
0001318
Arg of perigee: 104
1373 deg
Mean anomaly: 255
9925 deg
Mean motion: 15
50901480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2159
Checksum: 300
Coasting Arc #14 (Orbit 2174)
---------------------------------------
Vector Time (GMT): 2013/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3787048
08 A = 6787374
54 meter
Y = 2311666
79 meter E =
0005787
Z = 5132768
34 I = 51
42318
XDOT = -5302
149416 Wp = 120
56413
YDOT = 5327
946010 meter/sec RA = 324
07090 deg
ZDOT = 1508
293524 TA = 314
83675
MA = 314
88376
Ha = 226
333 n
mi
Hp = 219
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12424698
43 X = 3735983
45
Y = 7584208
61 feet Y = 2353730
23 meter
Z = 16839791
15 Z = 5151041
55
XDOT = -17395
503334 XDOT = -5368
660502
YDOT = 17480
137829 feet/sec YDOT = 5268
282050 meter/sec
ZDOT = 4948
469566 ZDOT = 1482
374827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10236552
95 X = -3120101
34
Y = 10223788
10 feet Y = 3116210
61 meter
Z = 16916236
52 Z = 5156068
89
XDOT = -12215
717251 XDOT = -3723
350618
YDOT = -20259
267993 feet/sec YDOT = -6175
024884 meter/sec
ZDOT = 4838
543685 ZDOT = 1474
788115
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 13342
55088880
00016717 00000-0 10270-3 0 9136
2 25544 51
6468 324
3934 0001204 105
0955 255
0329 15
50936808 21758
Satellite: ISS
Catalog Number: 25544
Epoch time: 13342
55088880 = yrday
fracday
Element set: 913
Inclination: 51
6468 deg
RA of node: 324
3934 deg
Eccentricity:
0001204
Arg of perigee: 105
0955 deg
Mean anomaly: 255
0329 deg
Mean motion: 15
50936808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2175
Checksum: 308
Coasting Arc #15 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2013/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3413339
06 A = 6786767
46 meter
Y = -2607677
74 meter E =
0015755
Z = -5268241
25 I = 51
39691
XDOT = 5333
446947 Wp = 85
85401
YDOT = -5432
580384 meter/sec RA = 319
08866 deg
ZDOT = -767
439756 TA = 176
77728
MA = 176
76712
Ha = 226
430 n
mi
Hp = 219
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11198618
96 X = -3358333
99
Y = -8555373
18 feet Y = -2645540
15 meter
Z = -17284256
09 Z = -5284689
47
XDOT = 17498
185523 XDOT = 5397
526894
YDOT = -17823
426456 feet/sec YDOT = -5372
580065 meter/sec
ZDOT = -2517
846970 ZDOT = -741
374820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10743160
71 X = 3274515
39
Y = -8989310
86 feet Y = -2739941
95 meter
Z = -17352975
92 Z = -5289187
06
XDOT = 12981
352860 XDOT = 3956
716352
YDOT = 20155
589844 feet/sec YDOT = 6143
423785 meter/sec
ZDOT = -2407
297007 ZDOT = -733
744128
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 13343
51739083
00016717 00000-0 10270-3 0 9142
2 25544 51
6469 319
5983 0001283 108
1178 252
0113 15
50963056 21907
Satellite: ISS
Catalog Number: 25544
Epoch time: 13343
51739083 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 319
5983 deg
Eccentricity:
0001283
Arg of perigee: 108
1178 deg
Mean anomaly: 252
0113 deg
Mean motion: 15
50963056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 303
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