[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 28th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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
062/07:21:36
444 -0
6 1
4 1
4
N/A -1
2 -0
1 222
3
000/00:03:12
887 -0
0 0
1 211
3
Coasting Arc #1 (Orbit 1098)
---------------------------------------
Vector Time (GMT): 2015/058/14:47:24
330
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4027816
62 A = 6776341
37 meter
Y = 2053765
60 meter E =
0012925
Z = 5040362
37 I = 51
26144
XDOT = -1486
856385 Wp = 54
85530
YDOT = 7316
249805 meter/sec RA = 270
44553 deg
ZDOT = -1782
373945 TA = 52
52321
MA = 52
40574
Ha = 222
325 n
mi
Hp = 211
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13214621
45 X = 3980067
77
Y = 6738076
11 feet Y = 2098540
67 meter
Z = 16536621
94 Z = 5059812
27
XDOT = -4878
137746 XDOT = -1559
899944
YDOT = 24003
444242 feet/sec YDOT = 7299
214263 meter/sec
ZDOT = -5847
683548 ZDOT = -1789
774653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14556080
94 X = 4436693
47
Y = 2324207
09 feet Y = 708418
32 meter
Z = 16619456
18 Z = 5065610
24
XDOT = 3040
271102 XDOT = 926
674632
YDOT = 23255
912014 feet/sec YDOT = 7088
401982 meter/sec
ZDOT = -5880
615369 ZDOT = -1792
411565
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 15058
66140570
00016717 00000-0 10270-3 0 9005
2 25544 51
6411 271
0632 0007525 54
6802 305
5054 15
54840182 10994
Satellite: ISS
Catalog Number: 25544
Epoch time: 15058
66140570 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 271
0632 deg
Eccentricity:
0007525
Arg of perigee: 54
6802 deg
Mean anomaly: 305
5054 deg
Mean motion: 15
54840182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1099
Checksum: 283
Coasting Arc #2 (Orbit 1113)
---------------------------------------
Vector Time (GMT): 2015/059/14:47:24
330
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3649698
49 A = 6779723
00 meter
Y = -3945011
33 meter E =
0013803
Z = -4143957
23 I = 51
27471
XDOT = 2498
142583 Wp = 84
43624
YDOT = -6210
288194 meter/sec RA = 265
41876 deg
ZDOT = 3724
009066 TA = 224
05576
MA = 224
16583
Ha = 222
359 n
mi
Hp = 210
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11974076
42 X = -3585183
77
Y = -12942950
56 feet Y = -3985464
26 meter
Z = -13595660
19 Z = -4161529
40
XDOT = 8196
005849 XDOT = 2549
312318
YDOT = -20374
961266 feet/sec YDOT = -6182
065918 meter/sec
ZDOT = 12217
877514 ZDOT = 3736
269133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15471857
87 X = -4715822
28
Y = -8336019
01 feet Y = -2540818
59 meter
Z = -13670144
56 Z = -4166660
06
XDOT = 388
825549 XDOT = 118
514027
YDOT = -20780
896662 feet/sec YDOT = -6334
017303 meter/sec
ZDOT = 12271
391157 ZDOT = 3740
320025
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 15059
62546516
00016717 00000-0 10270-3 0 9013
2 25544 51
6417 266
2515 0007551 58
6290 301
5601 15
54902336 11142
Satellite: ISS
Catalog Number: 25544
Epoch time: 15059
62546516 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 266
2515 deg
Eccentricity:
0007551
Arg of perigee: 58
6290 deg
Mean anomaly: 301
5601 deg
Mean motion: 15
54902336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1114
Checksum: 289
Coasting Arc #3 (Orbit 1129)
---------------------------------------
Vector Time (GMT): 2015/060/14:47:24
330
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3053381
93 A = 6784053
94 meter
Y = 5453096
78 meter E =
0019828
Z = 2622607
12 I = 51
29191
XDOT = -3468
035582 Wp = 88
26875
YDOT = 4456
539845 meter/sec RA = 260
40483 deg
ZDOT = -5193
971582 TA = 62
00435
MA = 61
80387
Ha = 222
321 n
mi
Hp = 210
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10017657
24 X = 2979437
79
Y = 17890737
47 feet Y = 5486828
49 meter
Z = 8604354
06 Z = 2637259
43
XDOT = -11378
069494 XDOT = -3492
382051
YDOT = 14621
193717 feet/sec YDOT = 4417
621382 meter/sec
ZDOT = -17040
589179 ZDOT = -5210
877845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15506269
91 X = 4726311
07
Y = 13376138
86 feet Y = 4077047
13 meter
Z = 8666103
79 Z = 2641428
44
XDOT = -4581
756276 XDOT = -1396
519313
YDOT = 16472
156323 feet/sec YDOT = 5020
713247 meter/sec
ZDOT = -17113
668267 ZDOT = -5216
246088
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 15060
65377441
00016717 00000-0 10270-3 0 9028
2 25544 51
6408 261
1185 0007463 61
5935 298
5969 15
54926320 11309
Satellite: ISS
Catalog Number: 25544
Epoch time: 15060
65377441 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 261
1185 deg
Eccentricity:
0007463
Arg of perigee: 61
5935 deg
Mean anomaly: 298
5969 deg
Mean motion: 15
54926320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1130
Checksum: 311
Coasting Arc #4 (Orbit 1144)
---------------------------------------
Vector Time (GMT): 2015/061/14:47:24
330
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2296836
82 A = 6786621
37 meter
Y = -6331471
44 meter E =
0017405
Z = -782973
84 I = 51
30820
XDOT = 4307
192399 Wp = 50
72283
YDOT = -2282
623338 meter/sec RA = 255
40338 deg
ZDOT = 5922
497022 TA = 300
76937
MA = 300
94063
Ha = 222
325 n
mi
Hp = 210
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7535553
86 X = -2222062
79
Y = -20772544
10 feet Y = -6356738
17 meter
Z = -2568811
82 Z = -793948
88
XDOT = 14131
208659 XDOT = 4303
628435
YDOT = -7488
921711 feet/sec YDOT = -2234
476772 meter/sec
ZDOT = 19430
764509 ZDOT = 5943
411688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14490888
66 X = -4416822
86
Y = -16675114
77 feet Y = -5082574
98 meter
Z = -2614698
41 Z = -796960
07
XDOT = 9158
847272 XDOT = 2791
616648
YDOT = -10969
871319 feet/sec YDOT = -3343
616778 meter/sec
ZDOT = 19520
619356 ZDOT = 5949
884780
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 15061
61779526
00016717 00000-0 10270-3 0 9036
2 25544 51
6419 256
3069 0007554 65
6568 294
5373 15
54966832 11459
Satellite: ISS
Catalog Number: 25544
Epoch time: 15061
61779526 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 256
3069 deg
Eccentricity:
0007554
Arg of perigee: 65
6568 deg
Mean anomaly: 294
5373 deg
Mean motion: 15
54966832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1145
Checksum: 339
Coasting Arc #5 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2015/062/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3856414
23 A = 6775633
63 meter
Y = 1829849
60 meter E =
0020979
Z = -5280186
71 I = 51
27777
XDOT = -2728
102143 Wp = 78
53303
YDOT = -7135
345761 meter/sec RA = 251
95086 deg
ZDOT = -477
797813 TA = 186
86332
MA = 186
89209
Ha = 222
335 n
mi
Hp = 211
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12652277
65 X = -3850940
77
Y = 6003443
57 feet Y = 1786754
62 meter
Z = -17323447
21 Z = -5298906
96
XDOT = -8950
466347 XDOT = -2645
789347
YDOT = -23409
927038 feet/sec YDOT = -7165
393000 meter/sec
ZDOT = -1567
578127 ZDOT = -490
849336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6160398
97 X = -1877689
61
Y = -12465118
75 feet Y = -3799368
20 meter
Z = -17403838
27 Z = -5304689
90
XDOT = 22385
900611 XDOT = 6823
222506
YDOT = -8787
127725 feet/sec YDOT = -2678
316530 meter/sec
ZDOT = -1622
225774 ZDOT = -494
454416
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 15062
32473167
00016717 00000-0 10270-3 0 9048
2 25544 51
6445 252
7826 0006665 61
0750 299
1070 15
54749983 11567
Satellite: ISS
Catalog Number: 25544
Epoch time: 15062
32473167 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 252
7826 deg
Eccentricity:
0006665
Arg of perigee: 61
0750 deg
Mean anomaly: 299
1070 deg
Mean motion: 15
54749983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 319
Coasting Arc #6 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2015/063/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4485303
53 A = 6776293
56 meter
Y = 161907
73 meter E =
0011632
Z = 5069570
87 I = 51
29106
XDOT = 1647
626015 Wp = 59
76729
YDOT = 7305
604991 meter/sec RA = 246
91905 deg
ZDOT = -1682
400965 TA = 46
59415
MA = 46
49737
Ha = 222
086 n
mi
Hp = 211
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14715562
77 X = 4458534
07
Y = 531193
34 feet Y = 211916
34 meter
Z = 16632450
35 Z = 5091294
15
XDOT = 5405
597161 XDOT = 1573
982880
YDOT = 23968
520313 feet/sec YDOT = 7323
617828 meter/sec
ZDOT = -5519
688206 ZDOT = -1674
577137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -95987
67 X = -29257
04
Y = 14619214
35 feet Y = 4455936
53 meter
Z = 16725361
49 Z = 5097890
18
XDOT = -22728
767506 XDOT = -6927
728336
YDOT = 6161
050004 feet/sec YDOT = 1877
888041 meter/sec
ZDOT = -5487
415590 ZDOT = -1672
564272
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 15063
35315148
00016717 00000-0 10270-3 0 9057
2 25544 51
6442 247
6506 0006552 63
3413 296
8410 15
54808266 11728
Satellite: ISS
Catalog Number: 25544
Epoch time: 15063
35315148 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 247
6506 deg
Eccentricity:
0006552
Arg of perigee: 63
3413 deg
Mean anomaly: 296
8410 deg
Mean motion: 15
54808266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 299
Coasting Arc #7 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2015/064/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4913393
11 A = 6779707
31 meter
Y = -2021093
05 meter E =
0013705
Z = -4223731
03 I = 51
31599
XDOT = -322
750564 Wp = 90
98167
YDOT = -6745
628997 meter/sec RA = 241
89489 deg
ZDOT = 3613
255841 TA = 216
15360
MA = 216
24633
Ha = 222
227 n
mi
Hp = 211
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16120056
13 X = -4869910
62
Y = -6630882
71 feet Y = -2075795
32 meter
Z = -13857385
28 Z = -4247493
04
XDOT = -1058
892926 XDOT = -264
846920
YDOT = -22131
328731 feet/sec YDOT = -6748
913911 meter/sec
ZDOT = 11854
513914 ZDOT = 3611
829647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5870263
94 X = 1789256
45
Y = -16326237
51 feet Y = -4976237
19 meter
Z = -13958721
71 Z = -4254618
38
XDOT = 20861
869216 XDOT = 6358
697737
YDOT = -2602
336768 feet/sec YDOT = -793
192247 meter/sec
ZDOT = 11849
505875 ZDOT = 3611
729391
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 15064
31727697
00016717 00000-0 10270-3 0 9061
2 25544 51
6445 242
8393 0006565 66
3340 293
8502 15
54800954 11879
Satellite: ISS
Catalog Number: 25544
Epoch time: 15064
31727697 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 242
8393 deg
Eccentricity:
0006565
Arg of perigee: 66
3340 deg
Mean anomaly: 293
8502 deg
Mean motion: 15
54800954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 324
Coasting Arc #8 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2015/065/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5009248
28 A = 6783980
18 meter
Y = 3631863
57 meter E =
0019480
Z = 2764820
30 I = 51
34627
XDOT = -1223
530405 Wp = 90
48245
YDOT = 5596
981425 meter/sec RA = 236
88415 deg
ZDOT = -5104
371229 TA = 58
02307
MA = 57
83386
Ha = 222
227 n
mi
Hp = 211
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16434541
60 X = 4954833
33
Y = 11915562
89 feet Y = 3687576
43 meter
Z = 9070932
73 Z = 2789021
20
XDOT = -4014
207364 XDOT = -1261
231430
YDOT = 18362
799950 feet/sec YDOT = 5583
087516 meter/sec
ZDOT = -16746
624767 ZDOT = -5110
407267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10839756
98 X = -3303957
93
Y = 17108357
73 feet Y = 5214627
44 meter
Z = 9173896
75 Z = 2796203
73
XDOT = -17326
882357 XDOT = -5281
233742
YDOT = -1929
951372 feet/sec YDOT = -588
249178 meter/sec
ZDOT = -16773
347969 ZDOT = -5112
516461
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 15065
34565542
00016717 00000-0 10270-3 0 9075
2 25544 51
6446 237
7070 0006673 70
1612 290
0260 15
54828492 12036
Satellite: ISS
Catalog Number: 25544
Epoch time: 15065
34565542 = yrday
fracday
Element set: 907
Inclination: 51
6446 deg
RA of node: 237
7070 deg
Eccentricity:
0006673
Arg of perigee: 70
1612 deg
Mean anomaly: 290
0260 deg
Mean motion: 15
54828492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 295
Coasting Arc #9 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2015/066/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4728225
21 A = 6786718
51 meter
Y = -4762789
41 meter E =
0015591
Z = -976624
80 I = 51
37422
XDOT = 2836
918604 Wp = 52
32561
YDOT = -4009
005403 meter/sec RA = 231
88586 deg
ZDOT = 5890
314358 TA = 297
05240
MA = 297
21143
Ha = 222
126 n
mi
Hp = 211
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15512549
91 X = -4669871
13
Y = -15625949
52 feet Y = -4815337
39 meter
Z = -3204149
60 Z = -999450
90
XDOT = 9307
475735 XDOT = 2852
924721
YDOT = -13152
904866 feet/sec YDOT = -3977
190704 meter/sec
ZDOT = 19325
178341 ZDOT = 5904
134938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14313444
32 X = 4362737
83
Y = -16712402
00 feet Y = -5093940
13 meter
Z = -3301061
78 Z = -1006163
63
XDOT = 12636
466160 XDOT = 3851
594886
YDOT = 7040
116228 feet/sec YDOT = 2145
827426 meter/sec
ZDOT = 19384
950454 ZDOT = 5908
532898
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 15066
30973796
00016717 00000-0 10270-3 0 9087
2 25544 51
6449 232
8952 0006528 72
3084 287
8781 15
54877766 12186
Satellite: ISS
Catalog Number: 25544
Epoch time: 15066
30973796 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 232
8952 deg
Eccentricity:
0006528
Arg of perigee: 72
3084 deg
Mean anomaly: 287
8781 deg
Mean motion: 15
54877766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 357
Coasting Arc #10 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2015/067/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3958906
93 A = 6786768
17 meter
Y = 5415116
42 meter E =
0013795
Z = -1014454
45 I = 51
39443
XDOT = -4424
476490 Wp = 116
79216
YDOT = 2145
507378 meter/sec RA = 226
89460 deg
ZDOT = -5881
927403 TA = 74
23937
MA = 74
08727
Ha = 222
173 n
mi
Hp = 211
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12988539
81 X = 3902987
40
Y = 17766129
99 feet Y = 5459074
68 meter
Z = -3328262
64 Z = -995359
62
XDOT = -14515
998982 XDOT = -4419
567181
YDOT = 7039
066200 feet/sec YDOT = 2096
056538 meter/sec
ZDOT = -19297
662082 ZDOT = -5903
408931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16397642
44 X = -4998001
42
Y = 14696480
33 feet Y = 4479487
20 meter
Z = -3247408
47 Z = -989810
10
XDOT = -7349
562602 XDOT = -2240
146681
YDOT = -12434
233504 feet/sec YDOT = -3789
954372 meter/sec
ZDOT = -19389
920110 ZDOT = -5910
047649
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 15067
33807198
00016717 00000-0 10270-3 0 9094
2 25544 51
6448 227
7629 0006410 76
7525 283
4343 15
54865118 12349
Satellite: ISS
Catalog Number: 25544
Epoch time: 15067
33807198 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 227
7629 deg
Eccentricity:
0006410
Arg of perigee: 76
7525 deg
Mean anomaly: 283
4343 deg
Mean motion: 15
54865118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 327
Coasting Arc #11 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2015/068/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2765574
51 A = 6783664
60 meter
Y = -5504298
57 meter E =
0019844
Z = 2819324
73 I = 51
40653
XDOT = 5753
226157 Wp = 79
54100
YDOT = -278
208857 meter/sec RA = 221
89861 deg
ZDOT = 5073
488991 TA = 312
63072
MA = 312
79786
Ha = 222
088 n
mi
Hp = 211
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9073407
17 X = -2717513
78
Y = -18058722
33 feet Y = -5534955
89 meter
Z = 9249753
05 Z = 2806007
68
XDOT = 18875
413900 XDOT = 5731
264519
YDOT = -912
758718 feet/sec YDOT = -213
994585 meter/sec
ZDOT = 16645
305087 ZDOT = 5101
383660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16880881
94 X = 5145292
81
Y = -11158635
23 feet Y = -3401152
02 meter
Z = 9193627
48 Z = 2802217
66
XDOT = 2261
775876 XDOT = 689
389287
YDOT = 17307
263688 feet/sec YDOT = 5275
253972 meter/sec
ZDOT = 16764
718078 ZDOT = 5109
886070
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 15068
36638140
00016717 00000-0 10270-3 0 9109
2 25544 51
6445 222
6298 0006438 77
7926 282
3948 15
54931786 12500
Satellite: ISS
Catalog Number: 25544
Epoch time: 15068
36638140 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 222
6298 deg
Eccentricity:
0006438
Arg of perigee: 77
7926 deg
Mean anomaly: 282
3948 deg
Mean motion: 15
54931786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1250
Checksum: 333
Coasting Arc #12 (Orbit 1264)
---------------------------------------
Vector Time (GMT): 2015/069/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1137907
70 A = 6779137
80 meter
Y = 5135286
86 meter E =
0014615
Z = -4291401
65 I = 51
41506
XDOT = -6638
475825 Wp = 75
02861
YDOT = -1467
994750 meter/sec RA = 216
89215 deg
ZDOT = -3523
296692 TA = 158
94304
MA = 158
88280
Ha = 221
999 n
mi
Hp = 211
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3733292
98 X = 1101245
14
Y = 16848054
00 feet Y = 5147806
12 meter
Z = -14079401
75 Z = -4285963
66
XDOT = -21779
776328 XDOT = -6604
452134
YDOT = -4816
255741 feet/sec YDOT = -1542
040750 meter/sec
ZDOT = -11559
372349 ZDOT = -3555
462244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16190599
46 X = -4934894
72
Y = 6024215
01 feet Y = 1836180
74 meter
Z = -14056929
82 Z = -4284552
21
XDOT = 2333
625713 XDOT = 711
289117
YDOT = -20972
702247 feet/sec YDOT = -6392
479645 meter/sec
ZDOT = -11696
799609 ZDOT = -3565
184521
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 15069
33040016
00016717 00000-0 10270-3 0 9117
2 25544 51
6436 217
8178 0006339 81
2860 278
9011 15
54961368 12657
Satellite: ISS
Catalog Number: 25544
Epoch time: 15069
33040016 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 217
8178 deg
Eccentricity:
0006339
Arg of perigee: 81
2860 deg
Mean anomaly: 278
9011 deg
Mean motion: 15
54961368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1265
Checksum: 308
Coasting Arc #13 (Orbit 1280)
---------------------------------------
Vector Time (GMT): 2015/070/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 722745
81 A = 6775652
13 meter
Y = -4363034
33 meter E =
0010570
Z = 5124853
61 I = 51
42960
XDOT = 6943
800025 Wp = 101
94473
YDOT = 2913
013667 meter/sec RA = 211
87410 deg
ZDOT = 1495
959256 TA = 333
59657
MA = 333
65039
Ha = 221
997 n
mi
Hp = 210
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2371213
29 X = 746585
97
Y = -14314417
08 feet Y = -4354818
20 meter
Z = 16813824
18 Z = 5128422
99
XDOT = 22781
496144 XDOT = 6903
443133
YDOT = 9557
131453 feet/sec YDOT = 2990
438301 meter/sec
ZDOT = 4908
002807 ZDOT = 1529
592490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14490658
89 X = 4416752
83
Y = 95995
95 feet Y = 29259
57 meter
Z = 16829779
03 Z = 5129716
65
XDOT = -6036
546538 XDOT = -1839
939385
YDOT = 22867
824617 feet/sec YDOT = 6970
112943 meter/sec
ZDOT = 5051
500370 ZDOT = 1539
697313
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 15070
35866514
00016717 00000-0 10270-3 0 9121
2 25544 51
6437 212
6849 0006471 84
4837 275
7055 15
54978690 12819
Satellite: ISS
Catalog Number: 25544
Epoch time: 15070
35866514 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 212
6849 deg
Eccentricity:
0006471
Arg of perigee: 84
4837 deg
Mean anomaly: 275
7055 deg
Mean motion: 15
54978690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1281
Checksum: 334
Coasting Arc #14 (Orbit 1295)
---------------------------------------
Vector Time (GMT): 2015/071/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2673132
98 A = 6774858
48 meter
Y = 3349249
48 meter E =
0020955
Z = -5265713
80 I = 51
45360
XDOT = -6495
409625 Wp = 93
61682
YDOT = -3975
741392 meter/sec RA = 206
84956 deg
ZDOT = 769
982899 TA = 183
76509
MA = 183
78088
Ha = 221
889 n
mi
Hp = 210
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8770121
32 X = -2684807
58
Y = 10988351
30 feet Y = 3319290
92 meter
Z = -17275963
92 Z = -5278728
06
XDOT = -21310
399031 XDOT = -6454
209473
YDOT = -13043
770972 feet/sec YDOT = -4048
146856 meter/sec
ZDOT = 2526
190615 ZDOT = 738
530017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12276870
93 X = -3741990
26
Y = -6707567
69 feet Y = -2044466
63 meter
Z = -17332189
64 Z = -5282851
40
XDOT = 8816
583533 XDOT = 2687
294661
YDOT = -22306
825850 feet/sec YDOT = -6799
120519 meter/sec
ZDOT = 2392
174210 ZDOT = 729
134699
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 15071
32263944
00016717 00000-0 10270-3 0 9138
2 25544 51
6423 207
8717 0006392 87
6943 272
4942 15
55048973 12967
Satellite: ISS
Catalog Number: 25544
Epoch time: 15071
32263944 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 207
8717 deg
Eccentricity:
0006392
Arg of perigee: 87
6943 deg
Mean anomaly: 272
4942 deg
Mean motion: 15
55048973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1296
Checksum: 329
Coasting Arc #15 (Orbit 1311)
---------------------------------------
Vector Time (GMT): 2015/072/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4454273
13 A = 6777378
26 meter
Y = -2170330
51 meter E =
0014106
Z = 4613822
81 I = 51
49142
XDOT = 5337
294662 Wp = 76
31325
YDOT = 4664
725899 meter/sec RA = 201
83156 deg
ZDOT = -2947
599932 TA = 43
12663
MA = 43
01621
Ha = 221
672 n
mi
Hp = 210
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14613756
98 X = 4455799
09
Y = -7120506
92 feet Y = -2120510
94 meter
Z = 15137213
94 Z = 4635464
63
XDOT = 17510
809258 XDOT = 5299
054195
YDOT = 15304
218828 feet/sec YDOT = 4724
196907 meter/sec
ZDOT = -9670
603453 ZDOT = -2921
765836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9664198
99 X = 2945647
85
Y = 12963144
74 feet Y = 3951166
52 meter
Z = 15230196
79 Z = 4642163
98
XDOT = -10870
773559 XDOT = -3313
411781
YDOT = 19378
633717 feet/sec YDOT = 5906
607557 meter/sec
ZDOT = -9560
729595 ZDOT = -2914
110381
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 15072
35085581
00016717 00000-0 10270-3 0 9142
2 25544 51
6426 202
7388 0006257 90
9837 269
2033 15
55084802 13122
Satellite: ISS
Catalog Number: 25544
Epoch time: 15072
35085581 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 202
7388 deg
Eccentricity:
0006257
Arg of perigee: 90
9837 deg
Mean anomaly: 269
2033 deg
Mean motion: 15
55084802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1312
Checksum: 308
Coasting Arc #16 (Orbit 1326)
---------------------------------------
Vector Time (GMT): 2015/073/07:23:12
887
Vector Time (MET): N/A
Weight (LBS) : 905275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5833738
69 A = 6781675
46 meter
Y = 993373
37 meter E =
0011124
Z = -3322440
15 I = 51
53451
XDOT = -3502
846853 Wp = 92
07498
YDOT = -4947
373149 meter/sec RA = 196
82607 deg
ZDOT = 4684
488918 TA = 229
22459
MA = 229
32117
Ha = 221
751 n
mi
Hp = 210
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19139562
63 X = -5828274
19
Y = 3259098
97 feet Y = 928166
94 meter
Z = -10900394
18 Z = -3350765
94
XDOT = -11492
279701 XDOT = -3470
019154
YDOT = -16231
539202 feet/sec YDOT = -4986
360281 meter/sec
ZDOT = 15369
058131 ZDOT = 4667
553084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7016072
09 X = -2138498
77
Y = -18029345
77 feet Y = -5495344
59 meter
Z = -11021823
83 Z = -3359451
90
XDOT = 12261
747279 XDOT = 3737
380571
YDOT = -14097
115606 feet/sec YDOT = -4296
800837 meter/sec
ZDOT = 15297
309118 ZDOT = 4662
619819
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 15073
31478750
00016717 00000-0 10270-3 0 9154
2 25544 51
6412 197
9253 0006378 94
7138 265
4744 15
55114579 13271
Satellite: ISS
Catalog Number: 25544
Epoch time: 15073
31478750 = yrday
fracday
Element set: 915
Inclination: 51
6412 deg
RA of node: 197
9253 deg
Eccentricity:
0006378
Arg of perigee: 94
7138 deg
Mean anomaly: 265
4744 deg
Mean motion: 15
55114579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1327
Checksum: 329
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