[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 25th 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
057/09:18:52
388 0
1 2
1 2
1
N/A 2
0 -0
1 222
3
000/00:04:44
775 0
6 0
1 211
2
062/07:21:36
422 -0
6 1
4 1
4
N/A -1
2 -0
1 222
4
000/00:03:12
843 -0
1 0
1 211
3
Coasting Arc #1 (Orbit 1065)
---------------------------------------
Vector Time (GMT): 2015/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2179457
47 A = 6779641
03 meter
Y = 5101836
88 meter E =
0016325
Z = 3889315
78 I = 51
28836
XDOT = -4268
424750 Wp = 65
28666
YDOT = 4925
173357 meter/sec RA = 281
05412 deg
ZDOT = -4048
607294 TA = 67
35033
MA = 67
17777
Ha = 221
122 n
mi
Hp = 211
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7150451
03 X = 2103352
90
Y = 16738309
98 feet Y = 5125783
78 meter
Z = 12760222
39 Z = 3899717
80
XDOT = -14004
018208 XDOT = -4303
515547
YDOT = 16158
705241 feet/sec YDOT = 4877
244525 meter/sec
ZDOT = -13282
832330 ZDOT = -4069
427877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -921318
57 X = -280817
90
Y = 18147646
24 feet Y = 5531402
57 meter
Z = 12803802
35 Z = 3902598
96
XDOT = -18241
188642 XDOT = -5559
914298
YDOT = 8555
306031 feet/sec YDOT = 2607
657278 meter/sec
ZDOT = -13372
756952 ZDOT = -4076
016319
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 15056
54062022
00016717 00000-0 10270-3 0 9005
2 25544 51
6455 281
6522 0006291 37
3945 322
7645 15
55236627 10667
Satellite: ISS
Catalog Number: 25544
Epoch time: 15056
54062022 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 281
6522 deg
Eccentricity:
0006291
Arg of perigee: 37
3945 deg
Mean anomaly: 322
7645 deg
Mean motion: 15
55236627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1066
Checksum: 296
Coasting Arc #2 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2015/057/09:21:14
775
Vector Time (MET): N/A
Weight (LBS) : 905208
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4276098
26 A = 6775839
72 meter
Y = -996324
49 meter E =
0009721
Z = 5152213
31 I = 51
26703
XDOT = 181
361601 Wp = 73
51077
YDOT = 7562
108887 meter/sec RA = 276
62606 deg
ZDOT = 1312
478419 TA = 3
83359
MA = 3
82615
Ha = 222
320 n
mi
Hp = 211
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14029193
77 X = 4261894
38
Y = -3268781
12 feet Y = -948585
41 meter
Z = 16903586
98 Z = 5172951
08
XDOT = 595
018376 XDOT = 90
411386
YDOT = 24810
068527 feet/sec YDOT = 7563
628555 meter/sec
ZDOT = 4306
031560 ZDOT = 1313
137963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8920411
93 X = 2718941
55
Y = 11176629
07 feet Y = 3406636
54 meter
Z = 16992459
34 Z = 5179301
61
XDOT = -21356
194276 XDOT = -6509
368015
YDOT = 10499
326895 feet/sec YDOT = 3200
194837 meter/sec
ZDOT = 4307
516049 ZDOT = 1312
930892
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 15057
44024319
00016717 00000-0 10270-3 0 9013
2 25544 51
6454 277
1606 0007792 48
4999 311
6821 15
54838931 10802
Satellite: ISS
Catalog Number: 25544
Epoch time: 15057
44024319 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 277
1606 deg
Eccentricity:
0007792
Arg of perigee: 48
4999 deg
Mean anomaly: 311
6821 deg
Mean motion: 15
54838931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 319
Coasting Arc #3 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2015/058/09:21:14
775
Vector Time (MET): N/A
Weight (LBS) : 905208
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4172998
74 A = 6775472
62 meter
Y = -1110652
46 meter E =
0020715
Z = -5238441
75 I = 51
26363
XDOT = 914
555707 Wp = 81
10150
YDOT = -7549
184585 meter/sec RA = 271
59212 deg
ZDOT = 878
160539 TA = 197
32018
MA = 197
39096
Ha = 222
453 n
mi
Hp = 210
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13690940
76 X = -4134823
02
Y = -3643872
89 feet Y = -1157104
59 meter
Z = -17186488
68 Z = -5258620
25
XDOT = 3000
510849 XDOT = 994
638789
YDOT = -24767
665961 feet/sec YDOT = -7538
509591 meter/sec
ZDOT = 2881
104129 ZDOT = 882
798276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2767050
68 X = -843397
05
Y = -13787519
57 feet Y = -4202435
96 meter
Z = -17272602
49 Z = -5264689
24
XDOT = 22509
052379 XDOT = 6860
759165
YDOT = -8128
194985 feet/sec YDOT = -2477
473832 meter/sec
ZDOT = 2902
261663 ZDOT = 884
609355
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
40433452
00016717 00000-0 10270-3 0 9023
2 25544 51
6457 272
3495 0007824 51
1415 309
0435 15
54864939 10953
Satellite: ISS
Catalog Number: 25544
Epoch time: 15058
40433452 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 272
3495 deg
Eccentricity:
0007824
Arg of perigee: 51
1415 deg
Mean anomaly: 309
0435 deg
Mean motion: 15
54864939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 310
Coasting Arc #4 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2015/059/09:21:14
775
Vector Time (MET): N/A
Weight (LBS) : 905208
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3868230
29 A = 6778010
36 meter
Y = 3152052
08 meter E =
0016157
Z = 4579164
16 I = 51
27247
XDOT = -1985
752040 Wp = 59
77297
YDOT = 6788
414962 meter/sec RA = 266
56150 deg
ZDOT = -2979
432318 TA = 60
14998
MA = 59
98949
Ha = 222
315 n
mi
Hp = 210
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12691044
26 X = 3810452
34
Y = 10341378
23 feet Y = 3194986
47 meter
Z = 15023504
46 Z = 4597814
34
XDOT = -6514
934514 XDOT = -2047
041407
YDOT = 22271
702631 feet/sec YDOT = 6765
866058 meter/sec
ZDOT = -9775
040413 ZDOT = -2989
227954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3397620
51 X = -1035594
73
Y = 15939761
10 feet Y = 4858439
18 meter
Z = 15102734
36 Z = 4603313
43
XDOT = -21582
940943 XDOT = -6578
480400
YDOT = 4751
210131 feet/sec YDOT = 1448
168848 meter/sec
ZDOT = -9818
114960 ZDOT = -2992
561440
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
43267678
00016717 00000-0 10270-3 0 9033
2 25544 51
6454 267
2173 0007818 53
6795 306
5079 15
54922834 11111
Satellite: ISS
Catalog Number: 25544
Epoch time: 15059
43267678 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 267
2173 deg
Eccentricity:
0007818
Arg of perigee: 53
6795 deg
Mean anomaly: 306
5079 deg
Mean motion: 15
54922834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 328
Coasting Arc #5 (Orbit 1125)
---------------------------------------
Vector Time (GMT): 2015/060/09:21:14
775
Vector Time (MET): N/A
Weight (LBS) : 905208
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3415484
69 A = 6782276
73 meter
Y = -4824816
50 meter E =
0012106
Z = -3329839
72 I = 51
28933
XDOT = 2981
009847 Wp = 68
29523
YDOT = -5309
301228 meter/sec RA = 261
54244 deg
ZDOT = 4653
359114 TA = 252
73134
MA = 252
86384
Ha = 222
391 n
mi
Hp = 210
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11205658
42 X = -3345103
81
Y = -15829450
46 feet Y = -4862617
46 meter
Z = -10924671
00 Z = -3346259
76
XDOT = 9780
216033 XDOT = 3017
554325
YDOT = -17418
967282 feet/sec YDOT = -5275
760868 meter/sec
ZDOT = 15266
926227 ZDOT = 4667
929245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8645602
38 X = 2635179
61
Y = -17316764
85 feet Y = -5278149
93 meter
Z = -10994086
28 Z = -3350997
50
XDOT = 18663
962076 XDOT = 5688
775641
YDOT = -377
245494 feet/sec YDOT = -114
984427 meter/sec
ZDOT = 15330
159226 ZDOT = 4672
632532
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
39672950
00016717 00000-0 10270-3 0 9044
2 25544 51
6452 262
4058 0007764 56
7755 303
4141 15
54914780 11261
Satellite: ISS
Catalog Number: 25544
Epoch time: 15060
39672950 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 262
4058 deg
Eccentricity:
0007764
Arg of perigee: 56
7755 deg
Mean anomaly: 303
4141 deg
Mean motion: 15
54914780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1126
Checksum: 309
Coasting Arc #6 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2015/061/09:21:14
775
Vector Time (MET): N/A
Weight (LBS) : 905208
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2722134
64 A = 6785968
11 meter
Y = 6011358
88 meter E =
0019406
Z = 1557865
39 I = 51
30693
XDOT = -3925
653203 Wp = 97
94302
YDOT = 3274
816910 meter/sec RA = 256
53694 deg
ZDOT = -5718
460513 TA = 64
93694
MA = 64
73562
Ha = 222
463 n
mi
Hp = 210
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8930887
93 X = 2647144
52
Y = 19722306
02 feet Y = 6041380
43 meter
Z = 5111106
94 Z = 1570905
93
XDOT = -12879
439642 XDOT = -3934
203650
YDOT = 10744
149968 feet/sec YDOT = 3230
869272 meter/sec
ZDOT = -18761
353388 ZDOT = -5737
551297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12836040
00 X = -3912424
99
Y = 17418475
62 feet Y = 5309151
37 meter
Z = 5165879
63 Z = 1574560
11
XDOT = -14345
654590 XDOT = -4372
555519
YDOT = -4926
634703 feet/sec YDOT = -1501
638257 meter/sec
ZDOT = -18843
573322 ZDOT = -5743
521149
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
42503174
00016717 00000-0 10270-3 0 9051
2 25544 51
6449 257
2733 0007799 61
5778 298
6160 15
54924523 11426
Satellite: ISS
Catalog Number: 25544
Epoch time: 15061
42503174 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 257
2733 deg
Eccentricity:
0007799
Arg of perigee: 61
5778 deg
Mean anomaly: 298
6160 deg
Mean motion: 15
54924523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 321
Coasting Arc #7 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2015/062/07:23:12
843
Vector Time (MET): N/A
Weight (LBS) : 905067
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3845504
01 A = 6775678
61 meter
Y = 1858433
17 meter E =
0021101
Z = -5278324
08 I = 51
27789
XDOT = -2747
698796 Wp = 78
27493
YDOT = -7125
847434 meter/sec RA = 251
95026 deg
ZDOT = -504
609519 TA = 186
86314
MA = 186
89208
Ha = 222
403 n
mi
Hp = 211
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12616482
97 X = -3840360
04
Y = 6097221
67 feet Y = 1815458
35 meter
Z = -17317336
23 Z = -5296992
14
XDOT = -9014
759828 XDOT = -2665
360518
YDOT = -23378
764547 feet/sec YDOT = -7156
113676 meter/sec
ZDOT = -1655
543042 ZDOT = -517
756176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6253677
02 X = -1906120
76
Y = -12428197
84 feet Y = -3788114
70 meter
Z = -17397508
76 Z = -5302760
67
XDOT = 22356
662745 XDOT = 6814
310805
YDOT = -8843
585642 feet/sec YDOT = -2695
524904 meter/sec
ZDOT = -1710
599262 ZDOT = -521
390655
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
32477765
00016717 00000-0 10270-3 0 9068
2 25544 51
6446 252
7814 0006800 61
0784 299
1051 15
54737682 11565
Satellite: ISS
Catalog Number: 25544
Epoch time: 15062
32477765 = yrday
fracday
Element set: 906
Inclination: 51
6446 deg
RA of node: 252
7814 deg
Eccentricity:
0006800
Arg of perigee: 61
0784 deg
Mean anomaly: 299
1051 deg
Mean motion: 15
54737682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 317
Coasting Arc #8 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2015/063/07:23:12
843
Vector Time (MET): N/A
Weight (LBS) : 905067
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4477540
05 A = 6776295
68 meter
Y = 127802
04 meter E =
0011692
Z = 5077317
93 I = 51
29104
XDOT = 1674
546259 Wp = 59
83716
YDOT = 7306
495331 meter/sec RA = 246
91856 deg
ZDOT = -1652
012681 TA = 46
22143
MA = 46
12475
Ha = 222
153 n
mi
Hp = 211
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14690092
04 X = 4451114
92
Y = 419298
03 feet Y = 177725
76 meter
Z = 16657867
23 Z = 5099004
34
XDOT = 5493
918174 XDOT = 1600
743555
YDOT = 23971
441374 feet/sec YDOT = 7324
808319 meter/sec
ZDOT = -5419
989110 ZDOT = -1644
058469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15042
96 X = 4585
10
Y = 14590251
90 feet Y = 4447108
78 meter
Z = 16750626
23 Z = 5105590
87
XDOT = -22731
208609 XDOT = -6928
472384
YDOT = 6240
612715 feet/sec YDOT = 1902
138756 meter/sec
ZDOT = -5387
158826 ZDOT = -1642
006010
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
35320566
00016717 00000-0 10270-3 0 9079
2 25544 51
6443 247
6495 0006686 63
3847 296
7990 15
54795936 11726
Satellite: ISS
Catalog Number: 25544
Epoch time: 15063
35320566 = yrday
fracday
Element set: 907
Inclination: 51
6443 deg
RA of node: 247
6495 deg
Eccentricity:
0006686
Arg of perigee: 63
3847 deg
Mean anomaly: 296
7990 deg
Mean motion: 15
54795936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 349
Coasting Arc #9 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2015/064/07:23:12
843
Vector Time (MET): N/A
Weight (LBS) : 905067
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4911652
73 A = 6779673
42 meter
Y = -1984693
22 meter E =
0013922
Z = -4243160
22 I = 51
31584
XDOT = -356
463338 Wp = 90
96959
YDOT = -6759
254394 meter/sec RA = 241
89436 deg
ZDOT = 3584
185015 TA = 215
81740
MA = 215
91084
Ha = 222
296 n
mi
Hp = 211
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16114346
23 X = -4868483
03
Y = -6511460
69 feet Y = -2039377
78 meter
Z = -13921129
32 Z = -4266914
53
XDOT = -1169
499141 XDOT = -298
263613
YDOT = -22176
031478 feet/sec YDOT = -6762
914655 meter/sec
ZDOT = 11759
137187 ZDOT = 3582
595775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5751319
94 X = 1753002
32
Y = -16314491
91 feet Y = -4972657
14 meter
Z = -14022438
76 Z = -4274039
33
XDOT = 20902
217885 XDOT = 6370
996011
YDOT = -2705
573978 feet/sec YDOT = -824
658949 meter/sec
ZDOT = 11753
433774 ZDOT = 3582
446614
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
31733886
00016717 00000-0 10270-3 0 9080
2 25544 51
6446 242
8382 0006699 66
3836 293
8020 15
54788646 11874
Satellite: ISS
Catalog Number: 25544
Epoch time: 15064
31733886 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 242
8382 deg
Eccentricity:
0006699
Arg of perigee: 66
3836 deg
Mean anomaly: 293
8020 deg
Mean motion: 15
54788646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 348
Coasting Arc #10 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2015/065/07:23:12
843
Vector Time (MET): N/A
Weight (LBS) : 905067
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5016569
27 A = 6783940
34 meter
Y = 3597966
77 meter E =
0019589
Z = 2795539
72 I = 51
34611
XDOT = -1184
649363 Wp = 90
00904
YDOT = 5624
970036 meter/sec RA = 236
88348 deg
ZDOT = -5082
804877 TA = 58
10522
MA = 57
91479
Ha = 222
293 n
mi
Hp = 211
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16458560
60 X = 4962383
60
Y = 11804352
90 feet Y = 3653762
78 meter
Z = 9171718
23 Z = 2819776
75
XDOT = -3886
644893 XDOT = -1222
771014
YDOT = 18454
626102 feet/sec YDOT = 5611
508572 meter/sec
ZDOT = -16675
869019 ZDOT = -5088
653066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10727338
63 X = -3269692
81
Y = 17124511
29 feet Y = 5219551
04 meter
Z = 9274842
25 Z = 2826971
92
XDOT = -17409
173559 XDOT = -5306
316101
YDOT = -1805
461044 feet/sec YDOT = -550
304526 meter/sec
ZDOT = -16701
792978 ZDOT = -5090
706500
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
34572550
00016717 00000-0 10270-3 0 9094
2 25544 51
6447 237
7060 0006807 70
1762 290
0125 15
54816906 12038
Satellite: ISS
Catalog Number: 25544
Epoch time: 15065
34572550 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 237
7060 deg
Eccentricity:
0006807
Arg of perigee: 70
1762 deg
Mean anomaly: 290
0125 deg
Mean motion: 15
54816906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 296
Coasting Arc #11 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2015/066/07:23:12
843
Vector Time (MET): N/A
Weight (LBS) : 905067
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4747369
10 A = 6786720
73 meter
Y = -4735480
98 meter E =
0015601
Z = -1016456
18 I = 51
37419
XDOT = 2795
905993 Wp = 52
51942
YDOT = -4050
073272 meter/sec RA = 231
88508 deg
ZDOT = 5881
672897 TA = 296
42019
MA = 296
58020
Ha = 222
195 n
mi
Hp = 211
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15575357
93 X = -4689125
48
Y = -15536354
93 feet Y = -4788243
66 meter
Z = -3334829
98 Z = -1039375
55
XDOT = 9172
919926 XDOT = 2812
416366
YDOT = -13287
641967 feet/sec YDOT = -4018
714384 meter/sec
ZDOT = 19296
827089 ZDOT = 5895
295479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14219167
62 X = 4334002
29
Y = -16766837
48 feet Y = -5110532
06 meter
Z = -3432145
58 Z = -1046117
97
XDOT = 12755
826616 XDOT = 3887
975952
YDOT = 6902
141367 feet/sec YDOT = 2103
772689 meter/sec
ZDOT = 19355
758527 ZDOT = 5899
635199
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
30981577
00016717 00000-0 10270-3 0 9106
2 25544 51
6449 232
8943 0006662 72
3692 287
8188 15
54864963 12186
Satellite: ISS
Catalog Number: 25544
Epoch time: 15066
30981577 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 232
8943 deg
Eccentricity:
0006662
Arg of perigee: 72
3692 deg
Mean anomaly: 287
8188 deg
Mean motion: 15
54864963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 346
Coasting Arc #12 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2015/067/07:23:12
843
Vector Time (MET): N/A
Weight (LBS) : 905067
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3991667
19 A = 6786841
08 meter
Y = 5399027
81 meter E =
0014030
Z = -970841
12 I = 51
39464
XDOT = -4386
695458 Wp = 116
54514
YDOT = 2196
839500 meter/sec RA = 226
89389 deg
ZDOT = -5891
335248 TA = 74
00654
MA = 73
85204
Ha = 222
243 n
mi
Hp = 211
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13096020
96 X = 3935713
27
Y = 17713345
82 feet Y = 5443352
23 meter
Z = -3185174
26 Z = -951587
22
XDOT = -14392
045465 XDOT = -4382
317266
YDOT = 7207
478675 feet/sec YDOT = 2147
808181 meter/sec
ZDOT = -19328
527717 ZDOT = -5912
634542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16334675
03 X = -4978808
95
Y = 14797281
84 feet Y = 4510211
50 meter
Z = -3103636
93 Z = -945988
54
XDOT = -7497
527492 XDOT = -2285
246380
YDOT = -12298
717264 feet/sec YDOT = -3748
649022 meter/sec
ZDOT = -19420
014047 ZDOT = -5919
220282
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
33815803
00016717 00000-0 10270-3 0 9119
2 25544 51
6449 227
7620 0006546 76
8356 283
3527 15
54852439 12349
Satellite: ISS
Catalog Number: 25544
Epoch time: 15067
33815803 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 227
7620 deg
Eccentricity:
0006546
Arg of perigee: 76
8356 deg
Mean anomaly: 283
3527 deg
Mean motion: 15
54852439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 322
Coasting Arc #13 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2015/068/07:23:12
843
Vector Time (MET): N/A
Weight (LBS) : 905067
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2812363
26 A = 6783796
96 meter
Y = -5501746
51 meter E =
0020025
Z = 2777888
36 I = 51
40695
XDOT = 5724
160967 Wp = 79
14256
YDOT = -335
667269 meter/sec RA = 221
89819 deg
ZDOT = 5102
794861 TA = 312
50040
MA = 312
66941
Ha = 222
154 n
mi
Hp = 211
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9226913
57 X = -2764126
31
Y = -18050349
45 feet Y = -5532926
08 meter
Z = 9113806
94 Z = 2764344
44
XDOT = 18780
055666 XDOT = 5702
701646
YDOT = -1101
270566 feet/sec YDOT = -271
775210 meter/sec
ZDOT = 16741
452957 ZDOT = 5130
549567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16854963
66 X = 5137392
92
Y = -11309231
96 feet Y = -3447053
90 meter
Z = 9056710
16 Z = 2760485
26
XDOT = 2426
877684 XDOT = 739
712318
YDOT = 17192
045442 feet/sec YDOT = 5240
135451 meter/sec
ZDOT = 16860
275998 ZDOT = 5139
012124
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
36647562
00016717 00000-0 10270-3 0 9129
2 25544 51
6446 222
6290 0006569 77
9333 282
2556 15
54920268 12509
Satellite: ISS
Catalog Number: 25544
Epoch time: 15068
36647562 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 222
6290 deg
Eccentricity:
0006569
Arg of perigee: 77
9333 deg
Mean anomaly: 282
2556 deg
Mean motion: 15
54920268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1250
Checksum: 322
Coasting Arc #14 (Orbit 1264)
---------------------------------------
Vector Time (GMT): 2015/069/07:23:12
843
Vector Time (MET): N/A
Weight (LBS) : 905067
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1196362
98 A = 6779288
23 meter
Y = 5148021
51 meter E =
0014580
Z = -4260252
29 I = 51
41553
XDOT = -6625
315159 Wp = 75
29060
YDOT = -1410
277033 meter/sec RA = 216
89220 deg
ZDOT = -3571
316901 TA = 158
11172
MA = 158
04937
Ha = 222
068 n
mi
Hp = 211
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3925075
38 X = 1159402
36
Y = 16889834
34 feet Y = 5161192
79 meter
Z = -13977205
67 Z = -4254531
05
XDOT = -21736
598290 XDOT = -6591
704596
YDOT = -4626
893153 feet/sec YDOT = -1484
178179 meter/sec
ZDOT = -11716
918968 ZDOT = -3603
419533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16206676
64 X = -4939795
04
Y = 6219148
74 feet Y = 1895596
54 meter
Z = -13953523
58 Z = -4253033
99
XDOT = 2166
099182 XDOT = 660
227031
YDOT = -20902
612852 feet/sec YDOT = -6371
116397 meter/sec
ZDOT = -11854
085949 ZDOT = -3613
125397
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
33050214
00016717 00000-0 10270-3 0 9130
2 25544 51
6437 217
8171 0006472 81
4211 278
7675 15
54948736 12659
Satellite: ISS
Catalog Number: 25544
Epoch time: 15069
33050214 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 217
8171 deg
Eccentricity:
0006472
Arg of perigee: 81
4211 deg
Mean anomaly: 278
7675 deg
Mean motion: 15
54948736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1265
Checksum: 313
Coasting Arc #15 (Orbit 1280)
---------------------------------------
Vector Time (GMT): 2015/070/07:23:12
843
Vector Time (MET): N/A
Weight (LBS) : 905067
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 656588
44 A = 6775755
07 meter
Y = -4390462
83 meter E =
0010839
Z = 5110290
35 I = 51
42990
XDOT = 6952
306814 Wp = 102
09594
YDOT = 2859
626247 meter/sec RA = 211
87457 deg
ZDOT = 1558
537506 TA = 332
82647
MA = 332
88315
Ha = 222
069 n
mi
Hp = 210
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2154161
56 X = 680810
97
Y = -14404405
61 feet Y = -4382984
38 meter
Z = 16766044
44 Z = 5113539
28
XDOT = 22809
405558 XDOT = 6912
242299
YDOT = 9381
975875 feet/sec YDOT = 2937
147652 meter/sec
ZDOT = 5113
312029 ZDOT = 1592
212781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14547185
08 X = 4433982
01
Y = -131732
91 feet Y = -40152
19 meter
Z = 16780632
05 Z = 5114736
65
XDOT = -5876
082523 XDOT = -1791
029953
YDOT = 22863
768165 feet/sec YDOT = 6968
876537 meter/sec
ZDOT = 5256
997820 ZDOT = 1602
332936
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
35877537
00016717 00000-0 10270-3 0 9140
2 25544 51
6438 212
6843 0006606 84
5967 275
5940 15
54965748 12810
Satellite: ISS
Catalog Number: 25544
Epoch time: 15070
35877537 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 212
6843 deg
Eccentricity:
0006606
Arg of perigee: 84
5967 deg
Mean anomaly: 275
5940 deg
Mean motion: 15
54965748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1281
Checksum: 344
Coasting Arc #16 (Orbit 1295)
---------------------------------------
Vector Time (GMT): 2015/071/07:23:12
843
Vector Time (MET): N/A
Weight (LBS) : 905067
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2606715
89 A = 6774863
48 meter
Y = 3389661
95 meter E =
0021144
Z = -5273324
02 I = 51
45357
XDOT = -6529
542442 Wp = 93
26430
YDOT = -3931
967656 meter/sec RA = 206
85023 deg
ZDOT = 701
504824 TA = 183
45793
MA = 183
47257
Ha = 221
958 n
mi
Hp = 210
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8552217
50 X = -2618810
37
Y = 11120938
15 feet Y = 3360443
76 meter
Z = -17300931
81 Z = -5286016
65
XDOT = -21422
383340 XDOT = -6488
496602
YDOT = -12900
156352 feet/sec YDOT = -4004
755685 meter/sec
ZDOT = 2301
525014 ZDOT = 669
885752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12371226
46 X = -3770749
83
Y = -6470497
69 feet Y = -1972207
70 meter
Z = -17355787
12 Z = -5290043
91
XDOT = 8673
929092 XDOT = 2643
813587
YDOT = -22384
987306 feet/sec YDOT = -6822
944131 meter/sec
ZDOT = 2166
790463 ZDOT = 660
437733
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
32275738
00016717 00000-0 10270-3 0 9154
2 25544 51
6424 207
8711 0006525 87
8305 272
3595 15
55036449 12962
Satellite: ISS
Catalog Number: 25544
Epoch time: 15071
32275738 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 207
8711 deg
Eccentricity:
0006525
Arg of perigee: 87
8305 deg
Mean anomaly: 272
3595 deg
Mean motion: 15
55036449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1296
Checksum: 320
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