[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 21st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22184 42 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 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
295/11:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 220
5
297/11:20:09
354 -2
0 2
0 2
0
N/A -0
1 0
0 228
5
000/00:04:14
707 -0
2 0
0 221
6
301/09:00:02
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 221
4
Coasting Arc #1 (Orbit 1429)
---------------------------------------
Vector Time (GMT): 2013/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3212592
35 A = 6795589
37 meter
Y = 4571999
17 meter E =
0008777
Z = -3877225
76 I = 51
51493
XDOT = -6379
003739 Wp = 65
52232
YDOT = 1003
430696 meter/sec RA = 201
42644 deg
ZDOT = -4106
072997 TA = 161
22015
MA = 161
18775
Ha = 228
594 n
mi
Hp = 220
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10540001
14 X = 3180063
46
Y = 14999997
27 feet Y = 4607742
32 meter
Z = -12720556
96 Z = -3861698
17
XDOT = -20928
489957 XDOT = -6369
803526
YDOT = 3292
095458 feet/sec YDOT = 932
147826 meter/sec
ZDOT = -13471
368101 ZDOT = -4137
040099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16597490
30 X = -5058915
04
Y = -7890121
32 feet Y = -2404908
98 meter
Z = -12655963
53 Z = -3857537
69
XDOT = 15997
007687 XDOT = 4875
887943
YDOT = -11853
918370 feet/sec YDOT = -3613
074319 meter/sec
ZDOT = -13601
472976 ZDOT = -4145
728963
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 13294
52397781
00016717 00000-0 10270-3 0 9008
2 25544 51
6510 202
3612 0002846 42
3267 317
8103 15
49829514 14309
Satellite: ISS
Catalog Number: 25544
Epoch time: 13294
52397781 = yrday
fracday
Element set: 900
Inclination: 51
6510 deg
RA of node: 202
3612 deg
Eccentricity:
0002846
Arg of perigee: 42
3267 deg
Mean anomaly: 317
8103 deg
Mean motion: 15
49829514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1430
Checksum: 291
Coasting Arc #2 (Orbit 1444)
---------------------------------------
Vector Time (GMT): 2013/295/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 927096
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3694424
86 A = 6791668
47 meter
Y = 2953585
15 meter E =
0013549
Z = -4886119
12 I = 51
53000
XDOT = -6191
787867 Wp = 96
79846
YDOT = -3811
247119 meter/sec RA = 196
52524 deg
ZDOT = 2381
937314 TA = 196
60994
MA = 196
65436
Ha = 228
563 n
mi
Hp = 220
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12120816
46 X = -3703441
93
Y = 9690239
98 feet Y = 2912221
11 meter
Z = -16030574
53 Z = -4904088
74
XDOT = -20314
264657 XDOT = -6160
280542
YDOT = -12504
091597 feet/sec YDOT = -3880
311358 meter/sec
ZDOT = 7814
754967 ZDOT = 2351
934177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7340733
28 X = 2237455
50
Y = -13582796
11 feet Y = -4140036
26 meter
Z = -16106382
18 Z = -4909225
29
XDOT = 22622
538177 XDOT = 6895
349636
YDOT = 3124
283515 feet/sec YDOT = 952
281615 meter/sec
ZDOT = 7689
293493 ZDOT = 2343
696657
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 13295
49118559
00016717 00000-0 10270-3 0 9010
2 25544 51
6504 197
5711 0002818 44
9718 315
1660 15
49845765 14456
Satellite: ISS
Catalog Number: 25544
Epoch time: 13295
49118559 = yrday
fracday
Element set: 901
Inclination: 51
6504 deg
RA of node: 197
5711 deg
Eccentricity:
0002818
Arg of perigee: 44
9718 deg
Mean anomaly: 315
1660 deg
Mean motion: 15
49845765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1445
Checksum: 330
Coasting Arc #3 (Orbit 1460)
---------------------------------------
Vector Time (GMT): 2013/296/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 927096
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3748678
59 A = 6792047
82 meter
Y = -3079639
33 meter E =
0010294
Z = 4748195
10 I = 51
56099
XDOT = 6279
501574 Wp = 58
32215
YDOT = 3470
186915 meter/sec RA = 191
56482 deg
ZDOT = -2697
299000 TA = 58
42539
MA = 58
32494
Ha = 228
421 n
mi
Hp = 220
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12298814
28 X = 3759771
27
Y = -10103803
57 feet Y = -3037657
03 meter
Z = 15578067
90 Z = 4766433
27
XDOT = 20602
039285 XDOT = 6253
333483
YDOT = 11385
127673 feet/sec YDOT = 3540
261884 meter/sec
ZDOT = -8849
406169 ZDOT = -2666
856816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7105096
42 X = -2165633
39
Y = 14158444
76 feet Y = 4315493
96 meter
Z = 15655028
77 Z = 4771652
77
XDOT = -22459
056948 XDOT = -6845
520558
YDOT = -1591
913533 feet/sec YDOT = -485
215245 meter/sec
ZDOT = -8722
043010 ZDOT = -2658
478709
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 13296
52285373
00016717 00000-0 10270-3 0 9025
2 25544 51
6498 192
4619 0002804 47
2841 312
8545 15
49894297 14615
Satellite: ISS
Catalog Number: 25544
Epoch time: 13296
52285373 = yrday
fracday
Element set: 902
Inclination: 51
6498 deg
RA of node: 192
4619 deg
Eccentricity:
0002804
Arg of perigee: 47
2841 deg
Mean anomaly: 312
8545 deg
Mean motion: 15
49894297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1461
Checksum: 334
Coasting Arc #4 (Orbit 1475)
---------------------------------------
Vector Time (GMT): 2013/297/11:22:16
707
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -490640
12 A = 6790755
86 meter
Y = 4197494
81 meter E =
0015481
Z = -5328874
10 I = 51
58377
XDOT = -7597
941877 Wp = 84
49919
YDOT = -887
804823 meter/sec RA = 186
65460 deg
ZDOT = 1
696850 TA = 185
50850
MA = 185
52555
Ha = 228
508 n
mi
Hp = 221
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1609711
67 X = -511654
27
Y = 13771308
45 feet Y = 4191890
48 meter
Z = -17483182
76 Z = -5331308
83
XDOT = -24927
630830 XDOT = -7587
457789
YDOT = -2912
745481 feet/sec YDOT = -972
711222 meter/sec
ZDOT = 5
567093 ZDOT = -35
188428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3947199
62 X = -1203106
44
Y = -13277178
24 feet Y = -4046883
93 meter
Z = -17493940
11 Z = -5332152
95
XDOT = 23142
716359 XDOT = 7053
899946
YDOT = -6677
290951 feet/sec YDOT = -2035
238282 meter/sec
ZDOT = -149
193971 ZDOT = -45
474322
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 13297
49002580
00016717 00000-0 10270-3 0 9030
2 25544 51
6504 187
6713 0001611 20
2926 339
8288 15
49537937 14768
Satellite: ISS
Catalog Number: 25544
Epoch time: 13297
49002580 = yrday
fracday
Element set: 903
Inclination: 51
6504 deg
RA of node: 187
6713 deg
Eccentricity:
0001611
Arg of perigee: 20
2926 deg
Mean anomaly: 339
8288 deg
Mean motion: 15
49537937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1476
Checksum: 322
Coasting Arc #5 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2013/298/11:22:16
707
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 370166
63 A = 6790614
88 meter
Y = -4203552
59 meter E =
0003442
Z = 5317806
03 I = 51
61426
XDOT = 7650
315307 Wp = 58
70987
YDOT = 398
224281 meter/sec RA = 181
70048 deg
ZDOT = -215
895517 TA = 33
36060
MA = 33
33891
Ha = 228
390 n
mi
Hp = 221
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1214457
44 X = 391311
29
Y = -13791183
04 feet Y = -4199294
71 meter
Z = 17446870
18 Z = 5319655
82
XDOT = 25099
459670 XDOT = 7646
342461
YDOT = 1306
510107 feet/sec YDOT = 483
752751 meter/sec
ZDOT = -708
318624 ZDOT = -178
740050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4544545
26 X = 1385177
39
Y = 13066329
01 feet Y = 3982617
08 meter
Z = 17455173
16 Z = 5320336
78
XDOT = -22548
702040 XDOT = -6872
844382
YDOT = 8588
546432 feet/sec YDOT = 2617
788953 meter/sec
ZDOT = -552
341362 ZDOT = -168
353647
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 13298
52190837
00016717 00000-0 10270-3 0 9049
2 25544 51
6501 182
5631 0001554 18
9210 341
1998 15
49584554 14923
Satellite: ISS
Catalog Number: 25544
Epoch time: 13298
52190837 = yrday
fracday
Element set: 904
Inclination: 51
6501 deg
RA of node: 182
5631 deg
Eccentricity:
0001554
Arg of perigee: 18
9210 deg
Mean anomaly: 341
1998 deg
Mean motion: 15
49584554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 316
Coasting Arc #6 (Orbit 1506)
---------------------------------------
Vector Time (GMT): 2013/299/11:22:16
707
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -252881
50 A = 6790632
12 meter
Y = 4230270
42 meter E =
0015376
Z = -5319263
86 I = 51
64557
XDOT = -7636
887166 Wp = 87
72813
YDOT = 88
834499 meter/sec RA = 176
74803 deg
ZDOT = 435
395899 TA = 186
42416
MA = 186
44390
Ha = 228
434 n
mi
Hp = 221
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -829663
71 X = -274326
59
Y = 13878839
95 feet Y = 4227322
37 meter
Z = -17451653
07 Z = -5320544
64
XDOT = -25055
404088 XDOT = -7639
428004
YDOT = 291
451767 feet/sec YDOT = 3
419782 meter/sec
ZDOT = 1428
464237 ZDOT = 398
289870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5154803
33 X = -1571184
05
Y = -12904726
76 feet Y = -3933360
72 meter
Z = -17457570
42 Z = -5321067
47
XDOT = 21698
633888 XDOT = 6613
743609
YDOT = -10381
657214 feet/sec YDOT = -3164
329119 meter/sec
ZDOT = 1272
614082 ZDOT = 387
892772
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 13299
48928239
00016717 00000-0 10270-3 0 9051
2 25544 51
6505 177
7739 0001626 22
2679 337
8541 15
49596833 15075
Satellite: ISS
Catalog Number: 25544
Epoch time: 13299
48928239 = yrday
fracday
Element set: 905
Inclination: 51
6505 deg
RA of node: 177
7739 deg
Eccentricity:
0001626
Arg of perigee: 22
2679 deg
Mean anomaly: 337
8541 deg
Mean motion: 15
49596833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1507
Checksum: 350
Coasting Arc #7 (Orbit 1522)
---------------------------------------
Vector Time (GMT): 2013/300/11:22:16
707
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 155211
77 A = 6790576
08 meter
Y = -4248740
28 meter E =
0004235
Z = 5292327
38 I = 51
67664
XDOT = 7613
682385 Wp = 50
78277
YDOT = -561
527660 meter/sec RA = 171
79762 deg
ZDOT = -671
116707 TA = 45
64337
MA = 45
60868
Ha = 228
349 n
mi
Hp = 221
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 509224
96 X = 177001
52
Y = -13939436
61 feet Y = -4246882
46 meter
Z = 17363278
82 Z = 5293134
58
XDOT = 24979
272917 XDOT = 7622
655791
YDOT = -1842
282349 feet/sec YDOT = -476
336485 meter/sec
ZDOT = -2201
826468 ZDOT = -634
107766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5690492
71 X = 1734462
18
Y = 12729845
65 feet Y = 3880056
95 meter
Z = 17367209
82 Z = 5293525
55
XDOT = -20785
345636 XDOT = -6335
373350
YDOT = 12096
534511 feet/sec YDOT = 3687
023719 meter/sec
ZDOT = -2046
306777 ZDOT = -623
714306
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 13300
52112775
00016717 00000-0 10270-3 0 9060
2 25544 51
6507 172
6656 0001587 22
2574 337
8646 15
49638807 15231
Satellite: ISS
Catalog Number: 25544
Epoch time: 13300
52112775 = yrday
fracday
Element set: 906
Inclination: 51
6507 deg
RA of node: 172
6656 deg
Eccentricity:
0001587
Arg of perigee: 22
2574 deg
Mean anomaly: 337
8646 deg
Mean motion: 15
49638807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1523
Checksum: 315
Coasting Arc #8 (Orbit 1536)
---------------------------------------
Vector Time (GMT): 2013/301/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1234004
42 A = 6790399
03 meter
Y = -4029828
23 meter E =
0003236
Z = 5321455
71 I = 51
70245
XDOT = 7420
242401 Wp = 76
88737
YDOT = -1896
504030 meter/sec RA = 167
34740 deg
ZDOT = 285
084442 TA = 10
39930
MA = 10
39261
Ha = 228
368 n
mi
Hp = 221
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4048570
94 X = -1214700
86
Y = -13221221
22 feet Y = -4043519
35 meter
Z = 17458844
19 Z = 5315508
10
XDOT = 24344
627299 XDOT = 7439
513149
YDOT = -6222
126083 feet/sec YDOT = -1813
418389 meter/sec
ZDOT = 935
316412 ZDOT = 321
178786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2052556
67 X = 625619
27
Y = 13705199
57 feet Y = 4177344
83 meter
Z = 17434373
33 Z = 5313996
99
XDOT = -24010
113006 XDOT = -7318
282444
YDOT = 2215
257343 feet/sec YDOT = 675
210438 meter/sec
ZDOT = 1087
178277 ZDOT = 331
371939
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 13301
42397802
00016717 00000-0 10270-3 0 9077
2 25544 51
6495 168
1955 0001569 25
2637 334
8590 15
49667447 15374
Satellite: ISS
Catalog Number: 25544
Epoch time: 13301
42397802 = yrday
fracday
Element set: 907
Inclination: 51
6495 deg
RA of node: 168
1955 deg
Eccentricity:
0001569
Arg of perigee: 25
2637 deg
Mean anomaly: 334
8590 deg
Mean motion: 15
49667447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1537
Checksum: 335
Coasting Arc #9 (Orbit 1551)
---------------------------------------
Vector Time (GMT): 2013/302/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1311059
59 A = 6790362
21 meter
Y = 4002959
41 meter E =
0015794
Z = -5339629
81 I = 51
73291
XDOT = -7283
342616 Wp = 84
60074
YDOT = 2338
441424 meter/sec RA = 162
40010 deg
ZDOT = -33
886282 TA = 185
06798
MA = 185
08399
Ha = 228
402 n
mi
Hp = 221
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4301376
60 X = 1292139
08
Y = 13133068
93 feet Y = 4017514
29 meter
Z = -17518470
51 Z = -5333306
98
XDOT = -23895
481022 XDOT = -7308
785651
YDOT = 7672
051916 feet/sec YDOT = 2256
852188 meter/sec
ZDOT = -111
175466 ZDOT = -69
330679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2550936
69 X = -777525
50
Y = -13615585
09 feet Y = -4150030
34 meter
Z = -17492418
75 Z = -5331689
23
XDOT = 23733
144095 XDOT = 7233
862320
YDOT = -4106
240209 feet/sec YDOT = -1251
582016 meter/sec
ZDOT = -260
377535 ZDOT = -79
363073
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 13302
39130183
00016717 00000-0 10270-3 0 9082
2 25544 51
6502 163
4060 0001688 31
2338 328
8913 15
49673056 15527
Satellite: ISS
Catalog Number: 25544
Epoch time: 13302
39130183 = yrday
fracday
Element set: 908
Inclination: 51
6502 deg
RA of node: 163
4060 deg
Eccentricity:
0001688
Arg of perigee: 31
2338 deg
Mean anomaly: 328
8913 deg
Mean motion: 15
49673056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1552
Checksum: 293
Coasting Arc #10 (Orbit 1567)
---------------------------------------
Vector Time (GMT): 2013/303/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1367784
97 A = 6790204
12 meter
Y = -3977798
37 meter E =
0003675
Z = 5327668
17 I = 51
76171
XDOT = 7143
054904 Wp = 61
40608
YDOT = -2768
165535 meter/sec RA = 157
45485 deg
ZDOT = -231
105317 TA = 30
80489
MA = 30
78333
Ha = 228
324 n
mi
Hp = 221
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4487483
49 X = -1349083
56
Y = -13050519
60 feet Y = -3992988
77 meter
Z = 17479226
30 Z = 5321069
25
XDOT = 23435
219502 XDOT = 7174
600917
YDOT = -9081
907922 feet/sec YDOT = -2688
110984 meter/sec
ZDOT = -758
219544 ZDOT = -196
327459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2979266
81 X = 908080
52
Y = 13510299
28 feet Y = 4117939
22 meter
Z = 17452011
47 Z = 5319373
10
XDOT = -23382
870554 XDOT = -7127
098945
YDOT = 5954
378338 feet/sec YDOT = 1814
894518 meter/sec
ZDOT = -611
749393 ZDOT = -186
461215
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 13303
42309226
00016717 00000-0 10270-3 0 9094
2 25544 51
6499 158
2974 0001610 29
2486 330
8754 15
49725620 15682
Satellite: ISS
Catalog Number: 25544
Epoch time: 13303
42309226 = yrday
fracday
Element set: 909
Inclination: 51
6499 deg
RA of node: 158
2974 deg
Eccentricity:
0001610
Arg of perigee: 29
2486 deg
Mean anomaly: 330
8754 deg
Mean motion: 15
49725620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1568
Checksum: 320
Coasting Arc #11 (Orbit 1582)
---------------------------------------
Vector Time (GMT): 2013/304/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1432637
01 A = 6790252
63 meter
Y = 3980053
03 meter E =
0015648
Z = -5325205
06 I = 51
79034
XDOT = -6944
691903 Wp = 88
52168
YDOT = 3168
491146 meter/sec RA = 152
51099 deg
ZDOT = 501
468489 TA = 186
25412
MA = 186
27368
Ha = 228
327 n
mi
Hp = 221
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4700252
66 X = 1413893
70
Y = 13057916
78 feet Y = 3995968
42 meter
Z = -17471145
22 Z = -5318291
17
XDOT = -22784
422254 XDOT = -6982
042573
YDOT = 10395
312158 feet/sec YDOT = 3090
622385 meter/sec
ZDOT = 1645
237826 ZDOT = 467
640025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3422008
12 X = -1043028
08
Y = -13486576
12 feet Y = -4110708
40 meter
Z = -17442608
92 Z = -5316507
20
XDOT = 22769
956952 XDOT = 6940
282879
YDOT = -7713
909690 feet/sec YDOT = -2351
199674 meter/sec
ZDOT = 1502
691601 ZDOT = 458
020400
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 13304
39037996
00016717 00000-0 10270-3 0 9105
2 25544 51
6503 153
5077 0001704 33
2595 326
8663 15
49733330 15838
Satellite: ISS
Catalog Number: 25544
Epoch time: 13304
39037996 = yrday
fracday
Element set: 910
Inclination: 51
6503 deg
RA of node: 153
5077 deg
Eccentricity:
0001704
Arg of perigee: 33
2595 deg
Mean anomaly: 326
8663 deg
Mean motion: 15
49733330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1583
Checksum: 307
Coasting Arc #12 (Orbit 1598)
---------------------------------------
Vector Time (GMT): 2013/305/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1479196
45 A = 6790207
61 meter
Y = -3988695
21 meter E =
0004641
Z = 5289530
28 I = 51
81723
XDOT = 6745
780435 Wp = 52
18290
YDOT = -3551
534296 meter/sec RA = 147
56873 deg
ZDOT = -788
440665 TA = 45
35612
MA = 45
31829
Ha = 228
271 n
mi
Hp = 221
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4853006
74 X = -1460179
84
Y = -13086270
37 feet Y = -4005129
78 meter
Z = 17354101
95 Z = 5282390
79
XDOT = 22131
825575 XDOT = 6788
823241
YDOT = -11652
015407 feet/sec YDOT = -3475
858081 meter/sec
ZDOT = -2586
747588 ZDOT = -755
564571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3802465
99 X = 1158991
63
Y = 13467209
17 feet Y = 4104805
36 meter
Z = 17324622
09 Z = 5280544
81
XDOT = -22096
050176 XDOT = -6734
876094
YDOT = 9401
903499 feet/sec YDOT = 2865
700187 meter/sec
ZDOT = -2448
138702 ZDOT = -746
192677
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 13305
42213216
00016717 00000-0 10270-3 0 9112
2 25544 51
6499 148
3987 0001657 32
0305 328
0946 15
49783828 15999
Satellite: ISS
Catalog Number: 25544
Epoch time: 13305
42213216 = yrday
fracday
Element set: 911
Inclination: 51
6499 deg
RA of node: 148
3987 deg
Eccentricity:
0001657
Arg of perigee: 32
0305 deg
Mean anomaly: 328
0946 deg
Mean motion: 15
49783828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 325
Coasting Arc #13 (Orbit 1613)
---------------------------------------
Vector Time (GMT): 2013/306/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1544218
02 A = 6790364
84 meter
Y = 4022405
04 meter E =
0015127
Z = -5261463
94 I = 51
84306
XDOT = -6494
594586 Wp = 92
46479
YDOT = 3897
305700 meter/sec RA = 142
62765 deg
ZDOT = 1075
403790 TA = 187
82165
MA = 187
84526
Ha = 228
246 n
mi
Hp = 221
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5066332
08 X = 1524683
35
Y = 13196866
94 feet Y = 4039563
93 meter
Z = -17262020
78 Z = -5254009
73
XDOT = -21307
725021 XDOT = -6542
916594
YDOT = 12786
436024 feet/sec YDOT = 3824
408890 meter/sec
ZDOT = 3528
227656 ZDOT = 1043
735097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4238051
74 X = -1291758
17
Y = -13525017
45 feet Y = -4122425
32 meter
Z = -17231227
46 Z = -5252078
13
XDOT = 21185
044159 XDOT = 6457
201460
YDOT = -10954
625703 feet/sec YDOT = -3338
969914 meter/sec
ZDOT = 3394
630235 ZDOT = 1034
683296
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 13306
38938356
00016717 00000-0 10270-3 0 9128
2 25544 51
6497 143
6085 0001720 34
2311 325
8950 15
49792145 16146
Satellite: ISS
Catalog Number: 25544
Epoch time: 13306
38938356 = yrday
fracday
Element set: 912
Inclination: 51
6497 deg
RA of node: 143
6085 deg
Eccentricity:
0001720
Arg of perigee: 34
2311 deg
Mean anomaly: 325
8950 deg
Mean motion: 15
49792145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1614
Checksum: 308
Coasting Arc #14 (Orbit 1629)
---------------------------------------
Vector Time (GMT): 2013/307/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1593575
47 A = 6790454
11 meter
Y = -4065979
49 meter E =
0005957
Z = 5196729
96 I = 51
86764
XDOT = 6246
907809 Wp = 49
64552
YDOT = -4220
116809 meter/sec RA = 137
68816 deg
ZDOT = -1381
454145 TA = 53
62889
MA = 53
57394
Ha = 228
212 n
mi
Hp = 221
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5228265
98 X = -1573235
44
Y = -13339827
73 feet Y = -4083685
96 meter
Z = 17049638
99 Z = 5189037
82
XDOT = 20495
104360 XDOT = 6300
344734
YDOT = -13845
527589 feet/sec YDOT = -4149
961175 meter/sec
ZDOT = -4532
329873 ZDOT = -1350
976346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4622917
90 X = 1409065
38
Y = 13601365
04 feet Y = 4145696
06 meter
Z = 17017857
02 Z = 5187042
82
XDOT = -20233
101170 XDOT = -6167
049237
YDOT = 12406
517980 feet/sec YDOT = 3781
506680 meter/sec
ZDOT = -4403
674705 ZDOT = -1342
240050
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 13307
42109725
00016717 00000-0 10270-3 0 9135
2 25544 51
6496 138
4989 0001702 34
0614 326
0645 15
49841069 16306
Satellite: ISS
Catalog Number: 25544
Epoch time: 13307
42109725 = yrday
fracday
Element set: 913
Inclination: 51
6496 deg
RA of node: 138
4989 deg
Eccentricity:
0001702
Arg of perigee: 34
0614 deg
Mean anomaly: 326
0645 deg
Mean motion: 15
49841069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1630
Checksum: 305
Coasting Arc #15 (Orbit 1644)
---------------------------------------
Vector Time (GMT): 2013/308/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1671263
64 A = 6790736
41 meter
Y = 4129242
89 meter E =
0014213
Z = -5138047
40 I = 51
89021
XDOT = -5955
045598 Wp = 96
26323
YDOT = 4499
323117 meter/sec RA = 132
74944 deg
ZDOT = 1681
403551 TA = 189
94180
MA = 189
96995
Ha = 228
172 n
mi
Hp = 221
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5483148
41 X = 1649925
32
Y = 13547384
80 feet Y = 4147812
66 meter
Z = -16857110
90 Z = -5129980
18
XDOT = -19537
551175 XDOT = -6013
083474
YDOT = 14761
558784 feet/sec YDOT = 4432
405517 meter/sec
ZDOT = 5516
415850 ZDOT = 1652
332581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5102333
73 X = -1555191
32
Y = -13736295
14 feet Y = -4186822
76 meter
Z = -16823766
69 Z = -5127884
09
XDOT = 19082
702143 XDOT = 5816
407613
YDOT = -13684
156029 feet/sec YDOT = -4170
930757 meter/sec
ZDOT = 5393
613819 ZDOT = 1643
973492
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 13308
38831217
00016717 00000-0 10270-3 0 9140
2 25544 51
6490 133
7080 0001737 35
5594 324
5672 15
49849500 16458
Satellite: ISS
Catalog Number: 25544
Epoch time: 13308
38831217 = yrday
fracday
Element set: 914
Inclination: 51
6490 deg
RA of node: 133
7080 deg
Eccentricity:
0001737
Arg of perigee: 35
5594 deg
Mean anomaly: 324
5672 deg
Mean motion: 15
49849500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1645
Checksum: 312
Coasting Arc #16 (Orbit 1660)
---------------------------------------
Vector Time (GMT): 2013/309/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1736163
07 A = 6790977
99 meter
Y = -4204358
43 meter E =
0007462
Z = 5038808
42 I = 51
91205
XDOT = 5672
245286 Wp = 51
81442
YDOT = -4749
681626 meter/sec RA = 127
81269 deg
ZDOT = -2002
190437 TA = 57
60631
MA = 57
53414
Ha = 228
149 n
mi
Hp = 220
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5696073
05 X = -1713497
80
Y = -13793826
87 feet Y = -4223646
63 meter
Z = 16531523
70 Z = 5030429
08
XDOT = 18609
728629 XDOT = 5734
662060
YDOT = -15582
944966 feet/sec YDOT = -4685
901959 meter/sec
ZDOT = -6568
866263 ZDOT = -1974
482860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5544195
45 X = 1689870
77
Y = 13896795
85 feet Y = 4235743
37 meter
Z = 16496882
90 Z = 5028249
91
XDOT = -17920
245071 XDOT = -5462
090698
YDOT = 14833
606635 feet/sec YDOT = 4521
283302 meter/sec
ZDOT = -6451
737552 ZDOT = -1966
489606
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 13309
41998707
00016717 00000-0 10270-3 0 9154
2 25544 51
6493 128
5984 0001730 35
7694 324
3572 15
49896597 16615
Satellite: ISS
Catalog Number: 25544
Epoch time: 13309
41998707 = yrday
fracday
Element set: 915
Inclination: 51
6493 deg
RA of node: 128
5984 deg
Eccentricity:
0001730
Arg of perigee: 35
7694 deg
Mean anomaly: 324
3572 deg
Mean motion: 15
49896597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1661
Checksum: 353
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