[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 26th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 568 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 2449)
---------------------------------------
Vector Time (GMT): 2015/145/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2640823
23 A = 6774889
96 meter
Y = 3505877
29 meter E =
0012244
Z = -5171067
65 I = 51
51536
XDOT = -6847
629949 Wp = 83
50895
YDOT = -3154
993717 meter/sec RA = 196
47956 deg
ZDOT = 1362
140822 TA = 199
59545
MA = 199
64255
Ha = 219
374 n
mi
Hp = 213
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8664118
21 X = -2654711
28
Y = 11502222
10 feet Y = 3476268
46 meter
Z = -16965445
06 Z = -5183929
90
XDOT = -22465
977523 XDOT = -6818
457926
YDOT = -10351
029254 feet/sec YDOT = -3231
405343 meter/sec
ZDOT = 4468
965951 ZDOT = 1328
946917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1127692
32 X = 343720
62
Y = 14289868
15 feet Y = 4355551
81 meter
Z = -17021232
67 Z = -5188071
72
XDOT = -22705
450763 XDOT = -6920
621392
YDOT = 6929
844197 feet/sec YDOT = 2112
216511 meter/sec
ZDOT = 4327
051257 ZDOT = 1318
885223
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 15145
45630957
00016717 00000-0 10270-3 0 9002
2 25544 51
6428 197
5351 0004242 337
6355 22
4613 15
55172284 24502
Satellite: ISS
Catalog Number: 25544
Epoch time: 15145
45630957 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 197
5351 deg
Eccentricity:
0004242
Arg of perigee: 337
6355 deg
Mean anomaly: 22
4613 deg
Mean motion: 15
55172284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2450
Checksum: 298
Coasting Arc #2 (Orbit 2465)
---------------------------------------
Vector Time (GMT): 2015/146/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4551410
77 A = 6778143
38 meter
Y = -2570095
61 meter E =
0010514
Z = 4313042
47 I = 51
55810
XDOT = 5561
149398 Wp = 47
63784
YDOT = 3959
970842 meter/sec RA = 191
46675 deg
ZDOT = -3496
401123 TA = 78
01194
MA = 77
89411
Ha = 219
337 n
mi
Hp = 213
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14932450
03 X = 4558860
63
Y = -8432072
23 feet Y = -2519157
27 meter
Z = 14150401
81 Z = 4335170
49
XDOT = 18245
240806 XDOT = 5533
439063
YDOT = 12992
030323 feet/sec YDOT = 4022
004449 meter/sec
ZDOT = -11471
132294 ZDOT = -3469
453107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5347384
53 X = 1629882
81
Y = -16210316
38 feet Y = -4940904
43 meter
Z = 14245802
86 Z = 4342120
71
XDOT = 21116
650476 XDOT = 6436
355065
YDOT = -3049
526721 feet/sec YDOT = -929
495744 meter/sec
ZDOT = -11356
142388 ZDOT = -3461
352200
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 15146
48444305
00016717 00000-0 10270-3 0 9017
2 25544 51
6434 192
4011 0004342 340
9537 19
1453 15
55222623 24661
Satellite: ISS
Catalog Number: 25544
Epoch time: 15146
48444305 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 192
4011 deg
Eccentricity:
0004342
Arg of perigee: 340
9537 deg
Mean anomaly: 19
1453 deg
Mean motion: 15
55222623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2466
Checksum: 282
Coasting Arc #3 (Orbit 2480)
---------------------------------------
Vector Time (GMT): 2015/147/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5958934
25 A = 6782714
94 meter
Y = 1576753
53 meter E =
0007001
Z = -2824343
56 I = 51
60364
XDOT = -3591
247710 Wp = 26
83846
YDOT = -4469
281114 meter/sec RA = 186
47073 deg
ZDOT = 5092
945466 TA = 301
05472
MA = 301
12342
Ha = 219
488 n
mi
Hp = 213
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19550309
22 X = -5962403
27
Y = 5173075
89 feet Y = 1510097
54 meter
Z = -9266219
01 Z = -2853299
54
XDOT = -11782
308760 XDOT = -3565
744084
YDOT = -14662
995782 feet/sec YDOT = -4509
298383 meter/sec
ZDOT = 16709
138669 ZDOT = 5075
561500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10688178
62 X = -3257756
84
Y = 17100128
77 feet Y = 5212119
25 meter
Z = -9390769
58 Z = -2862306
57
XDOT = -17452
610205 XDOT = -5319
555590
YDOT = -1792
626872 feet/sec YDOT = -546
392670 meter/sec
ZDOT = 16635
272795 ZDOT = 5070
431148
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 15147
44831331
00016717 00000-0 10270-3 0 9024
2 25544 51
6425 187
5887 0004283 346
2514 13
8522 15
55206394 24817
Satellite: ISS
Catalog Number: 25544
Epoch time: 15147
44831331 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 187
5887 deg
Eccentricity:
0004283
Arg of perigee: 346
2514 deg
Mean anomaly: 13
8522 deg
Mean motion: 15
55206394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2481
Checksum: 305
Coasting Arc #4 (Orbit 2496)
---------------------------------------
Vector Time (GMT): 2015/148/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6705987
62 A = 6785758
31 meter
Y = -516722
31 meter E =
0010891
Z = 873143
90 I = 51
64603
XDOT = 1143
696225 Wp = 108
35999
YDOT = 4724
250109 meter/sec RA = 181
48986 deg
ZDOT = -5930
768456 TA = 62
19116
MA = 62
08082
Ha = 219
685 n
mi
Hp = 212
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22001271
73 X = 6707025
87
Y = -1695283
17 feet Y = -441725
80 meter
Z = 2864645
35 Z = 905723
19
XDOT = 3752
284202 XDOT = 1119
593330
YDOT = 15499
508231 feet/sec YDOT = 4736
905137 meter/sec
ZDOT = -19457
901759 ZDOT = -5925
270890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14601792
30 X = 4450626
29
Y = -16519572
37 feet Y = -5035165
66 meter
Z = 3004584
16 Z = 915797
25
XDOT = 12366
315039 XDOT = 3769
252824
YDOT = 7363
205171 feet/sec YDOT = 2244
304936 meter/sec
ZDOT = -19435
096091 ZDOT = -5923
817289
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 15148
47643270
00016717 00000-0 10270-3 0 9032
2 25544 51
6429 182
4548 0004458 351
6281 8
4797 15
55234886 24972
Satellite: ISS
Catalog Number: 25544
Epoch time: 15148
47643270 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 182
4548 deg
Eccentricity:
0004458
Arg of perigee: 351
6281 deg
Mean anomaly: 8
4797 deg
Mean motion: 15
55234886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2497
Checksum: 338
Coasting Arc #5 (Orbit 2512)
---------------------------------------
Vector Time (GMT): 2015/149/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6650659
78 A = 6785721
89 meter
Y = -532552
31 meter E =
0016437
Z = 1183819
80 I = 51
67621
XDOT = 1430
408427 Wp = 43
88286
YDOT = -4734
623006 meter/sec RA = 176
51604 deg
ZDOT = 5868
915842 TA = 328
98415
MA = 329
08111
Ha = 219
948 n
mi
Hp = 212
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21819749
92 X = -6649960
99
Y = -1747218
88 feet Y = -606920
49 meter
Z = 3883923
22 Z = 1151513
38
XDOT = 4692
941033 XDOT = 1454
736388
YDOT = -15533
540047 feet/sec YDOT = -4718
491502 meter/sec
ZDOT = 19254
973236 ZDOT = 5875
923453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16655760
05 X = -5076675
66
Y = 14240694
20 feet Y = 4340563
59 meter
Z = 3745317
87 Z = 1141572
89
XDOT = -6737
824185 XDOT = -2053
688812
YDOT = -12985
933568 feet/sec YDOT = -3958
112551 meter/sec
ZDOT = 19285
855229 ZDOT = 5878
328674
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 15149
50454668
00016717 00000-0 10270-3 0 9049
2 25544 51
6422 177
3210 0004587 357
2505 2
8622 15
55181936 25139
Satellite: ISS
Catalog Number: 25544
Epoch time: 15149
50454668 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 177
3210 deg
Eccentricity:
0004587
Arg of perigee: 357
2505 deg
Mean anomaly: 2
8622 deg
Mean motion: 15
55181936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2513
Checksum: 302
Coasting Arc #6 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2015/150/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5821325
26 A = 6782114
90 meter
Y = 1605344
19 meter E =
0005364
Z = -3094945
85 I = 51
69693
XDOT = -3835
184701 Wp = 54
88407
YDOT = 4478
371035 meter/sec RA = 171
53786 deg
ZDOT = -4893
712302 TA = 160
65234
MA = 160
63197
Ha = 219
891 n
mi
Hp = 212
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19098836
16 X = 5817975
60
Y = 5266877
26 feet Y = 1670423
52 meter
Z = -10154021
83 Z = -3066674
55
XDOT = -12582
626973 XDOT = -3861
205662
YDOT = 14692
818356 feet/sec YDOT = 4435
338308 meter/sec
ZDOT = -16055
486556 ZDOT = -4912
406116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17084105
18 X = 5207235
26
Y = -10153019
15 feet Y = -3094640
24 meter
Z = -10032908
36 Z = -3058030
47
XDOT = 1187
690779 XDOT = 362
008149
YDOT = 17934
294836 feet/sec YDOT = 5466
373066 meter/sec
ZDOT = -16136
507946 ZDOT = -4918
407622
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 15150
46839292
00016717 00000-0 10270-3 0 9057
2 25544 51
6427 172
5078 0004488
8816 359
2344 15
55245835 25284
Satellite: ISS
Catalog Number: 25544
Epoch time: 15150
46839292 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 172
5078 deg
Eccentricity:
0004488
Arg of perigee:
8816 deg
Mean anomaly: 359
2344 deg
Mean motion: 15
55245835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 325
Coasting Arc #7 (Orbit 2543)
---------------------------------------
Vector Time (GMT): 2015/151/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4313121
66 A = 6777525
22 meter
Y = -2629398
44 meter E =
0008870
Z = 4510447
84 I = 51
71156
XDOT = 5750
539772 Wp = 82
86665
YDOT = -3961
181692 meter/sec RA = 166
54746 deg
ZDOT = 3185
475503 TA = 335
18889
MA = 335
23152
Ha = 220
100 n
mi
Hp = 212
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14150661
61 X = -4305308
98
Y = -8626635
30 feet Y = -2677587
27 meter
Z = 14798057
23 Z = 4489513
93
XDOT = 18866
600302 XDOT = 5778
933145
YDOT = -12996
002925 feet/sec YDOT = -3896
716899 meter/sec
ZDOT = 10451
035116 ZDOT = 3213
479635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16016937
99 X = -4881962
70
Y = 4555980
87 feet Y = 1388662
97 meter
Z = 14708612
92 Z = 4483185
22
XDOT = 3620
514882 XDOT = 1103
532936
YDOT = -21448
162654 feet/sec YDOT = -6537
399977 meter/sec
ZDOT = 10571
962065 ZDOT = 3222
334037
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 15151
49648949
00016717 00000-0 10270-3 0 9069
2 25544 51
6415 167
3737 0004521 5
5678 354
5524 15
55248023 25449
Satellite: ISS
Catalog Number: 25544
Epoch time: 15151
49648949 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 167
3737 deg
Eccentricity:
0004521
Arg of perigee: 5
5678 deg
Mean anomaly: 354
5524 deg
Mean motion: 15
55248023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2544
Checksum: 322
Coasting Arc #8 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2015/152/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2357216
78 A = 6774456
98 meter
Y = 3584634
85 meter E =
0016156
Z = -5256550
63 I = 51
73290
XDOT = -6925
769317 Wp = 66
90791
YDOT = 3120
905117 meter/sec RA = 161
54561 deg
ZDOT = -973
689367 TA = 193
75112
MA = 193
79517
Ha = 220
056 n
mi
Hp = 212
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7733650
86 X = 2342492
11
Y = 11760613
02 feet Y = 3610912
99 meter
Z = -17245901
03 Z = -5245134
95
XDOT = -22722
340280 XDOT = -6955
423387
YDOT = 10239
190015 feet/sec YDOT = 3043
290928 meter/sec
ZDOT = -3194
518920 ZDOT = -1007
405679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13988831
64 X = 4263795
88
Y = 2025195
76 feet Y = 617279
67 meter
Z = -17197489
59 Z = -5241794
83
XDOT = -7409
010540 XDOT = -2258
266413
YDOT = 22709
488894 feet/sec YDOT = 6921
852215 meter/sec
ZDOT = -3339
853893 ZDOT = -1017
987467
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 15152
46032315
00016717 00000-0 10270-3 0 9072
2 25544 51
6424 162
5605 0004532 7
6910 352
4312 15
55243980 25599
Satellite: ISS
Catalog Number: 25544
Epoch time: 15152
46032315 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 162
5605 deg
Eccentricity:
0004532
Arg of perigee: 7
6910 deg
Mean anomaly: 352
4312 deg
Mean motion: 15
55243980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 285
Coasting Arc #9 (Orbit 2574)
---------------------------------------
Vector Time (GMT): 2015/153/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -179567
75 A = 6774595
18 meter
Y = -4366479
16 meter E =
0008386
Z = 5173981
63 I = 51
76231
XDOT = 7285
041537 Wp = 33
66429
YDOT = -1962
685814 meter/sec RA = 156
54037 deg
ZDOT = -1395
635096 TA = 69
77085
MA = 69
68070
Ha = 220
115 n
mi
Hp = 212
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -589133
04 X = -155861
01
Y = -14325719
04 feet Y = -4368355
26 meter
Z = 16975005
35 Z = 5173166
38
XDOT = 23901
054912 XDOT = 7313
226883
YDOT = -6439
257921 feet/sec YDOT = -1881
061960 meter/sec
ZDOT = -4578
855303 ZDOT = -1360
177041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11274843
57 X = -3436572
32
Y = -8862531
45 feet Y = -2701299
58 meter
Z = 16972258
22 Z = 5173144
31
XDOT = 10175
366250 XDOT = 3101
451633
YDOT = -21471
126640 feet/sec YDOT = -6544
399400 meter/sec
ZDOT = -4426
215177 ZDOT = -1349
110386
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 15153
48840399
00016717 00000-0 10270-3 0 9085
2 25544 51
6410 157
4260 0004635 12
8306 347
2964 15
55282175 25757
Satellite: ISS
Catalog Number: 25544
Epoch time: 15153
48840399 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 157
4260 deg
Eccentricity:
0004635
Arg of perigee: 12
8306 deg
Mean anomaly: 347
2964 deg
Mean motion: 15
55282175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2575
Checksum: 316
Coasting Arc #10 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2015/154/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1883522
48 A = 6778074
06 meter
Y = 4882351
81 meter E =
0009430
Z = -4314914
70 I = 51
80376
XDOT = -6778
324388 Wp = 80
92522
YDOT = 505
985185 meter/sec RA = 151
54444 deg
ZDOT = 3539
403347 TA = 225
02876
MA = 225
10525
Ha = 220
202 n
mi
Hp = 212
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6179535
70 X = -1917017
66
Y = 16018214
61 feet Y = 4861102
30 meter
Z = -14156544
29 Z = -4324145
32
XDOT = -22238
597074 XDOT = -6800
671931
YDOT = 1660
056381 feet/sec YDOT = 430
060130 meter/sec
ZDOT = 11612
215705 ZDOT = 3506
420987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8363482
41 X = 2549189
44
Y = 14955721
76 feet Y = 4558503
99 meter
Z = -14197047
43 Z = -4327260
06
XDOT = -11969
015840 XDOT = -3648
156028
YDOT = 17556
861014 feet/sec YDOT = 5351
331237 meter/sec
ZDOT = 11470
439722 ZDOT = 3496
190027
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 15154
45222324
00016717 00000-0 10270-3 0 9096
2 25544 51
6421 152
6129 0004726 15
2324 344
8970 15
55268222 25902
Satellite: ISS
Catalog Number: 25544
Epoch time: 15154
45222324 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 152
6129 deg
Eccentricity:
0004726
Arg of perigee: 15
2324 deg
Mean anomaly: 344
8970 deg
Mean motion: 15
55268222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 292
Coasting Arc #11 (Orbit 2605)
---------------------------------------
Vector Time (GMT): 2015/155/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3653837
01 A = 6782619
95 meter
Y = -5002823
58 meter E =
0014976
Z = 2751375
91 I = 51
84566
XDOT = 5546
135811 Wp = 82
42066
YDOT = 1197
549497 meter/sec RA = 146
56389 deg
ZDOT = -5161
844960 TA = 66
50330
MA = 66
34599
Ha = 220
224 n
mi
Hp = 212
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11987654
24 X = 3696142
98
Y = -16413463
18 feet Y = -4961727
79 meter
Z = 9026823
84 Z = 2769227
77
XDOT = 18195
983633 XDOT = 5557
406799
YDOT = 3928
968166 feet/sec YDOT = 1259
633701 meter/sec
ZDOT = -16935
186877 ZDOT = -5134
875192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5252794
24 X = -1601051
68
Y = -19598653
63 feet Y = -5973669
63 meter
Z = 9104400
31 Z = 2775021
22
XDOT = 13138
272039 XDOT = 4004
545318
YDOT = -11373
869431 feet/sec YDOT = -3466
755403 meter/sec
ZDOT = -16819
520801 ZDOT = -5126
589940
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 15155
48028889
00016717 00000-0 10270-3 0 9102
2 25544 51
6410 147
4780 0004798 19
7386 340
3952 15
55313598 26067
Satellite: ISS
Catalog Number: 25544
Epoch time: 15155
48028889 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 147
4780 deg
Eccentricity:
0004798
Arg of perigee: 19
7386 deg
Mean anomaly: 340
3952 deg
Mean motion: 15
55313598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2606
Checksum: 333
Coasting Arc #12 (Orbit 2620)
---------------------------------------
Vector Time (GMT): 2015/156/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4865993
91 A = 6785496
65 meter
Y = 4651510
62 meter E =
0014736
Z = -793826
40 I = 51
88232
XDOT = -3798
560766 Wp = 35
01285
YDOT = -2966
214505 meter/sec RA = 141
59981 deg
ZDOT = 5970
027340 TA = 316
42635
MA = 316
54265
Ha = 220
197 n
mi
Hp = 211
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15964546
95 X = -4913790
44
Y = 15260861
61 feet Y = 4596828
75 meter
Z = -2604417
33 Z = -817580
04
XDOT = -12462
469705 XDOT = -3794
109761
YDOT = -9731
674886 feet/sec YDOT = -3008
668356 meter/sec
ZDOT = 19586
703872 ZDOT = 5951
585056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2207926
64 X = 672976
04
Y = 21962221
87 feet Y = 6694085
23 meter
Z = -2707308
01 Z = -825187
48
XDOT = -13814
758951 XDOT = -4210
738528
YDOT = 3767
745624 feet/sec YDOT = 1148
408866 meter/sec
ZDOT = 19507
977185 ZDOT = 5946
031446
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 15156
44409364
00016717 00000-0 10270-3 0 9111
2 25544 51
6418 142
6654 0004628 23
9456 336
1912 15
55348062 26219
Satellite: ISS
Catalog Number: 25544
Epoch time: 15156
44409364 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 142
6654 deg
Eccentricity:
0004628
Arg of perigee: 23
9456 deg
Mean anomaly: 336
1912 deg
Mean motion: 15
55348062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2621
Checksum: 304
Coasting Arc #13 (Orbit 2636)
---------------------------------------
Vector Time (GMT): 2015/157/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5494746
75 A = 6785173
95 meter
Y = -3749214
85 meter E =
0008072
Z = -1335000
00 I = 51
90428
XDOT = 1755
385472 Wp = 110
22987
YDOT = 4641
686546 meter/sec RA = 136
64077 deg
ZDOT = -5841
983612 TA = 84
24940
MA = 84
15736
Ha = 220
389 n
mi
Hp = 211
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18027384
33 X = 5542747
91
Y = -12300573
65 feet Y = -3687500
45 meter
Z = -4379921
26 Z = -1308191
43
XDOT = 5759
138688 XDOT = 1731
728714
YDOT = 15228
630401 feet/sec YDOT = 4661
184808 meter/sec
ZDOT = -19166
612899 ZDOT = -5833
513222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1046417
69 X = 318948
11
Y = -21821946
46 feet Y = -6651329
28 meter
Z = -4264043
98 Z = -1299680
61
XDOT = 14107
660712 XDOT = 4300
014985
YDOT = 4394
130862 feet/sec YDOT = 1339
331087 meter/sec
ZDOT = -19131
030326 ZDOT = -5831
138043
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 15157
47214430
00016717 00000-0 10270-3 0 9124
2 25544 51
6410 137
5302 0004798 26
7513 333
3887 15
55310012 26378
Satellite: ISS
Catalog Number: 25544
Epoch time: 15157
47214430 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 137
5302 deg
Eccentricity:
0004798
Arg of perigee: 26
7513 deg
Mean anomaly: 333
3887 deg
Mean motion: 15
55310012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2637
Checksum: 286
Coasting Arc #14 (Orbit 2652)
---------------------------------------
Vector Time (GMT): 2015/158/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5473744
57 A = 6781480
83 meter
Y = 2354375
63 meter E =
0015890
Z = 3219218
32 I = 51
91453
XDOT = 269
198328 Wp = 71
85044
YDOT = -5974
687663 meter/sec RA = 131
67701 deg
ZDOT = 4812
725191 TA = 325
29966
MA = 325
40321
Ha = 220
435 n
mi
Hp = 211
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17958479
54 X = -5515302
66
Y = 7724329
48 feet Y = 2292931
95 meter
Z = 10561739
88 Z = 3192527
26
XDOT = 883
196614 XDOT = 312
610334
YDOT = -19601
993644 feet/sec YDOT = -5971
435050 meter/sec
ZDOT = 15789
780812 ZDOT = 4814
137763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4354026
91 X = -1327107
40
Y = 19121548
39 feet Y = 5828247
95 meter
Z = 10446599
42 Z = 3184123
50
XDOT = -13997
003928 XDOT = -4266
286797
YDOT = -11843
858870 feet/sec YDOT = -3610
008184 meter/sec
ZDOT = 15796
912866 ZDOT = 4814
899042
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 15158
50018537
00016717 00000-0 10270-3 0 9130
2 25544 51
6409 132
3963 0004741 28
5176 331
6236 15
55347067 26532
Satellite: ISS
Catalog Number: 25544
Epoch time: 15158
50018537 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 132
3963 deg
Eccentricity:
0004741
Arg of perigee: 28
5176 deg
Mean anomaly: 331
6236 deg
Mean motion: 15
55347067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2653
Checksum: 306
Coasting Arc #15 (Orbit 2667)
---------------------------------------
Vector Time (GMT): 2015/159/10:37:11
791
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4929708
68 A = 6776876
53 meter
Y = -539358
31 meter E =
0014348
Z = -4633027
60 I = 51
91906
XDOT = -2084
153328 Wp = 58
37411
YDOT = 6730
643813 meter/sec RA = 126
69859 deg
ZDOT = -3000
670728 TA = 181
77031
MA = 181
77540
Ha = 220
463 n
mi
Hp = 211
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16173584
90 X = 4957879
01
Y = -1769548
25 feet Y = -484073
20 meter
Z = -15200221
78 Z = -4609011
67
XDOT = -6837
773386 XDOT = -2144
685980
YDOT = 22082
164741 feet/sec YDOT = 6706
999230 meter/sec
ZDOT = -9844
720236 ZDOT = -3010
941619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7891663
49 X = 2405379
03
Y = -14337656
90 feet Y = -4370117
82 meter
Z = -15096891
52 Z = -4601532
54
XDOT = 13143
288355 XDOT = 4006
074291
YDOT = 17649
785733 feet/sec YDOT = 5379
654691 meter/sec
ZDOT = -9890
071058 ZDOT = -3014
493658
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 15159
46396829
00016717 00000-0 10270-3 0 9140
2 25544 51
6405 127
5822 0004871 32
7481 327
3973 15
55329151 26688
Satellite: ISS
Catalog Number: 25544
Epoch time: 15159
46396829 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 127
5822 deg
Eccentricity:
0004871
Arg of perigee: 32
7481 deg
Mean anomaly: 327
3973 deg
Mean motion: 15
55329151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2668
Checksum: 332
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