[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 1st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
274/22:54:34
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
8
Coasting Arc #1 (Orbit 442)
---------------------------------------
Vector Time (GMT): 2015/273/11:38:46
178
Vector Time (MET): N/A
Weight (LBS) : 894988
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3763177
67 A = 6778547
17 meter
Y = 2487005
84 meter E =
0009593
Z = 5059885
06 I = 51
26328
XDOT = -2346
950230 Wp = 16
53192
YDOT = 7092
221494 meter/sec RA = 277
60049 deg
ZDOT = -1730
581428 TA = 90
34045
MA = 90
23052
Ha = 221
748 n
mi
Hp = 214
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12346383
42 X = 3710508
26
Y = 8159467
98 feet Y = 2528794
28 meter
Z = 16600672
77 Z = 5078037
91
XDOT = -7699
967947 XDOT = -2417
676092
YDOT = 23268
443222 feet/sec YDOT = 7065
580692 meter/sec
ZDOT = -5677
760589 ZDOT = -1742
155269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12618107
88 X = -3845999
28
Y = -7563407
43 feet Y = -2305326
59 meter
Z = 16678448
94 Z = 5083591
24
XDOT = 5985
171010 XDOT = 1824
280124
YDOT = -22689
155066 feet/sec YDOT = -6915
654464 meter/sec
ZDOT = -5728
894561 ZDOT = -1746
167062
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 15273
53049397
00016717 00000-0 10270-3 0 9005
2 25544 51
6420 278
1889 0006381 345
5733 14
5236 15
54065778 4431
Satellite: ISS
Catalog Number: 25544
Epoch time: 15273
53049397 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 278
1889 deg
Eccentricity:
0006381
Arg of perigee: 345
5733 deg
Mean anomaly: 14
5236 deg
Mean motion: 15
54065778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 443
Checksum: 320
Coasting Arc #2 (Orbit 457)
---------------------------------------
Vector Time (GMT): 2015/274/11:38:46
178
Vector Time (MET): N/A
Weight (LBS) : 894988
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3294443
34 A = 6781506
72 meter
Y = -4051125
90 meter E =
0007658
Z = -4331084
16 I = 51
27045
XDOT = 3037
601417 Wp = 64
37494
YDOT = -6138
364257 meter/sec RA = 272
58087 deg
ZDOT = 3439
050585 TA = 240
70244
MA = 240
77899
Ha = 221
897 n
mi
Hp = 214
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10808541
15 X = -3227858
71
Y = -13291095
48 feet Y = -4087594
67 meter
Z = -14209593
70 Z = -4346926
04
XDOT = 9965
883914 XDOT = 3089
310455
YDOT = -20138
990344 feet/sec YDOT = -6104
106334 meter/sec
ZDOT = 11282
974360 ZDOT = 3453
933095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11561726
86 X = 3524014
35
Y = 12565035
12 feet Y = 3829822
71 meter
Z = -14277139
01 Z = -4351671
97
XDOT = -7642
838730 XDOT = -2329
537245
YDOT = 19897
294580 feet/sec YDOT = 6064
695388 meter/sec
ZDOT = 11348
190664 ZDOT = 3458
928514
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 15274
49506291
00016717 00000-0 10270-3 0 9013
2 25544 51
6426 273
3812 0006491 348
7463 11
3544 15
54058083 4581
Satellite: ISS
Catalog Number: 25544
Epoch time: 15274
49506291 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 273
3812 deg
Eccentricity:
0006491
Arg of perigee: 348
7463 deg
Mean anomaly: 11
3544 deg
Mean motion: 15
54058083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 458
Checksum: 308
Coasting Arc #3 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2015/274/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3385201
62 A = 6781914
19 meter
Y = -4104217
73 meter E =
0009153
Z = 4196206
13 I = 51
27016
XDOT = 2889
231078 Wp = 65
50618
YDOT = 6106
383733 meter/sec RA = 270
27611 deg
ZDOT = 3639
152915 TA = 347
04072
MA = 347
06423
Ha = 221
848 n
mi
Hp = 214
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11106304
51 X = 3410460
48
Y = -13465281
27 feet Y = -4066220
56 meter
Z = 13767080
49 Z = 4212712
75
XDOT = 9479
104585 XDOT = 2803
055372
YDOT = 20034
067365 feet/sec YDOT = 6138
211514 meter/sec
ZDOT = 11939
478066 ZDOT = 3652
978571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12545058
80 X = 3823733
92
Y = -12054115
82 feet Y = -3674094
50 meter
Z = 13838934
08 Z = 4218107
11
XDOT = 6067
487144 XDOT = 1849
370082
YDOT = 20098
607930 feet/sec YDOT = 6126
055697 meter/sec
ZDOT = 11997
975382 ZDOT = 3656
982896
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 15275
00949406
00016717 00000-0 10270-3 0 9021
2 25544 51
6414 270
8144 0006685 348
0904 12
0090 15
54079128 4662
Satellite: ISS
Catalog Number: 25544
Epoch time: 15275
00949406 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 270
8144 deg
Eccentricity:
0006685
Arg of perigee: 348
0904 deg
Mean anomaly: 12
0090 deg
Mean motion: 15
54079128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 297
Coasting Arc #4 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2015/275/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3820519
16 A = 6778675
10 meter
Y = 2533236
90 meter E =
0015183
Z = -5006726
66 I = 51
25970
XDOT = -2150
218616 Wp = 50
24407
YDOT = -7088
558907 meter/sec RA = 265
25623 deg
ZDOT = -1940
194232 TA = 200
76887
MA = 200
83063
Ha = 222
009 n
mi
Hp = 214
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12534511
67 X = -3824241
37
Y = 8311144
69 feet Y = 2490492
12 meter
Z = -16426268
58 Z = -5025295
48
XDOT = -7054
523018 XDOT = -2061
367964
YDOT = -23256
426859 feet/sec YDOT = -7112
107432 meter/sec
ZDOT = -6365
466641 ZDOT = -1950
423318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13213152
96 X = -4027369
02
Y = 6996556
60 feet Y = 2132550
45 meter
Z = -16506731
75 Z = -5031251
84
XDOT = -4091
172039 XDOT = -1246
989238
YDOT = -22888
271988 feet/sec YDOT = -6976
345302 meter/sec
ZDOT = -6408
303427 ZDOT = -1953
250885
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 15275
97404341
00016717 00000-0 10270-3 0 9032
2 25544 51
6406 266
0057 0006530 353
0099 7
0961 15
54111943 4813
Satellite: ISS
Catalog Number: 25544
Epoch time: 15275
97404341 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 266
0057 deg
Eccentricity:
0006530
Arg of perigee: 353
0099 deg
Mean anomaly: 7
0961 deg
Mean motion: 15
54111943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 289
Coasting Arc #5 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2015/276/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4173403
79 A = 6777456
94 meter
Y = -751435
07 meter E =
0006740
Z = 5285125
60 I = 51
25904
XDOT = 1327
266910 Wp = 17
96759
YDOT = 7554
793069 meter/sec RA = 260
22954 deg
ZDOT = 32
350968 TA = 71
75926
MA = 71
68592
Ha = 222
031 n
mi
Hp = 214
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13692269
65 X = 4155822
94
Y = -2465338
16 feet Y = -704863
20 meter
Z = 17339650
91 Z = 5305356
73
XDOT = 4354
550230 XDOT = 1242
531582
YDOT = 24786
066499 feet/sec YDOT = 7569
161662 meter/sec
ZDOT = 106
138347 ZDOT = 38
592220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13741542
86 X = 4188422
26
Y = -1300145
75 feet Y = -396284
43 meter
Z = 17426969
19 Z = 5311740
21
XDOT = 2135
846583 XDOT = 651
006039
YDOT = 24064
448325 feet/sec YDOT = 7334
843850 meter/sec
ZDOT = 131
721423 ZDOT = 40
148690
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 15277
00288281
00016717 00000-0 10270-3 0 9042
2 25544 51
6406 260
8760 0006499 357
2183 2
8932 15
54090295 4974
Satellite: ISS
Catalog Number: 25544
Epoch time: 15277
00288281 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 260
8760 deg
Eccentricity:
0006499
Arg of perigee: 357
2183 deg
Mean anomaly: 2
8932 deg
Mean motion: 15
54090295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 497
Checksum: 320
Coasting Arc #6 (Orbit 511)
---------------------------------------
Vector Time (GMT): 2015/277/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4441078
98 A = 6778430
95 meter
Y = -1022253
52 meter E =
0013216
Z = -5028082
32 I = 51
26901
XDOT = -405
257152 Wp = 75
93086
YDOT = -7416
237008 meter/sec RA = 255
20301 deg
ZDOT = 1873
039925 TA = 212
29649
MA = 212
37748
Ha = 222
081 n
mi
Hp = 214
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14570469
08 X = -4404893
11
Y = -3353850
12 feet Y = -1071714
69 meter
Z = -16496333
06 Z = -5049568
38
XDOT = -1329
583831 XDOT = -331
395455
YDOT = -24331
486247 feet/sec YDOT = -7420
355718 meter/sec
ZDOT = 6145
144111 ZDOT = 1871
251280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14203725
02 X = -4329295
39
Y = -4329336
67 feet Y = -1319581
82 meter
Z = -16588758
97 Z = -5056253
73
XDOT = -29
998900 XDOT = -9
143665
YDOT = -23331
980705 feet/sec YDOT = -7111
587719 meter/sec
ZDOT = 6138
712460 ZDOT = 1871
079558
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 15277
96740400
00016717 00000-0 10270-3 0 9054
2 25544 51
6404 256
0667 0006391 1
2582 358
8586 15
54154943 5123
Satellite: ISS
Catalog Number: 25544
Epoch time: 15277
96740400 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 256
0667 deg
Eccentricity:
0006391
Arg of perigee: 1
2582 deg
Mean anomaly: 358
8586 deg
Mean motion: 15
54154943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 512
Checksum: 311
Coasting Arc #7 (Orbit 527)
---------------------------------------
Vector Time (GMT): 2015/278/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4566968
20 A = 6781604
57 meter
Y = 2712093
63 meter E =
0013634
Z = 4213530
02 I = 51
28831
XDOT = -650
844268 Wp = 48
01367
YDOT = 6733
267700 meter/sec RA = 250
18327 deg
ZDOT = -3611
996870 TA = 79
19325
MA = 79
03982
Ha = 222
136 n
mi
Hp = 214
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14983491
46 X = 4515833
63
Y = 8897944
97 feet Y = 2762878
96 meter
Z = 13823917
39 Z = 4235591
11
XDOT = -2135
315841 XDOT = -708
543122
YDOT = 22090
773294 feet/sec YDOT = 6725
666577 meter/sec
ZDOT = -11850
383432 ZDOT = -3615
299338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14424553
76 X = 4396603
99
Y = 9642902
49 feet Y = 2939156
68 meter
Z = 13918542
07 Z = 4242371
62
XDOT = -2473
679410 XDOT = -753
977484
YDOT = 20905
027223 feet/sec YDOT = 6371
852297 meter/sec
ZDOT = -11865
764363 ZDOT = -3616
684978
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 15278
99621248
00016717 00000-0 10270-3 0 9067
2 25544 51
6400 250
9372 0006369 4
4459 355
6749 15
54160441 5281
Satellite: ISS
Catalog Number: 25544
Epoch time: 15278
99621248 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 250
9372 deg
Eccentricity:
0006369
Arg of perigee: 4
4459 deg
Mean anomaly: 355
6749 deg
Mean motion: 15
54160441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 528
Checksum: 322
Coasting Arc #8 (Orbit 542)
---------------------------------------
Vector Time (GMT): 2015/279/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4518746
32 A = 6785290
16 meter
Y = -4089703
22 meter E =
0009396
Z = -2977190
99 I = 51
31330
XDOT = 1791
093894 Wp = 34
29709
YDOT = -5572
756898 meter/sec RA = 245
17409 deg
ZDOT = 4951
941174 TA = 291
48744
MA = 291
58760
Ha = 222
164 n
mi
Hp = 213
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14825283
19 X = -4458216
28
Y = -13417661
47 feet Y = -4139896
69 meter
Z = -9767686
98 Z = -2998994
81
XDOT = 5876
292303 XDOT = 1829
221929
YDOT = -18283
323157 feet/sec YDOT = -5552
513993 meter/sec
ZDOT = 16246
526163 ZDOT = 4960
735195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14304613
71 X = -4360046
26
Y = -13905733
57 feet Y = -4238467
59 meter
Z = -9860982
22 Z = -3005627
38
XDOT = 5367
793920 XDOT = 1636
103587
YDOT = -17035
039957 feet/sec YDOT = -5192
280179 meter/sec
ZDOT = 16285
370346 ZDOT = 4963
780881
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 15279
96070640
00016717 00000-0 10270-3 0 9070
2 25544 51
6406 246
1279 0006298 9
3349 350
7919 15
54198316 5437
Satellite: ISS
Catalog Number: 25544
Epoch time: 15279
96070640 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 246
1279 deg
Eccentricity:
0006298
Arg of perigee: 9
3349 deg
Mean anomaly: 350
7919 deg
Mean motion: 15
54198316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 543
Checksum: 331
Coasting Arc #9 (Orbit 558)
---------------------------------------
Vector Time (GMT): 2015/280/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213447
14 A = 6788162
43 meter
Y = 5137908
17 meter E =
0013367
Z = 1374972
18 I = 51
33687
XDOT = -3017
107912 Wp = 92
54594
YDOT = 4033
620579 meter/sec RA = 240
17579 deg
ZDOT = -5778
803440 TA = 72
41287
MA = 72
26690
Ha = 222
255 n
mi
Hp = 213
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13823645
47 X = 4149001
52
Y = 16856654
11 feet Y = 5184665
54 meter
Z = 4511063
60 Z = 1395283
24
XDOT = -9898
648004 XDOT = -3033
917212
YDOT = 13233
663316 feet/sec YDOT = 3999
786616 meter/sec
ZDOT = -18959
328873 ZDOT = -5793
501334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13517681
72 X = 4120189
39
Y = 17079886
17 feet Y = 5205949
31 meter
Z = 4597763
14 Z = 1401398
21
XDOT = -8746
436728 XDOT = -2665
913915
YDOT = 12084
951108 feet/sec YDOT = 3683
493098 meter/sec
ZDOT = -19023
358208 ZDOT = -5798
319582
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 15280
98948303
00016717 00000-0 10270-3 0 9085
2 25544 51
6399 240
9979 0006392 11
8607 348
2695 15
54243575 5595
Satellite: ISS
Catalog Number: 25544
Epoch time: 15280
98948303 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 240
9979 deg
Eccentricity:
0006392
Arg of perigee: 11
8607 deg
Mean anomaly: 348
2695 deg
Mean motion: 15
54243575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 559
Checksum: 354
Coasting Arc #10 (Orbit 574)
---------------------------------------
Vector Time (GMT): 2015/281/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3637653
84 A = 6788917
84 meter
Y = -5709799
25 meter E =
0018292
Z = 342070
99 I = 51
35739
XDOT = 4213
424356 Wp = 38
74081
YDOT = -2316
465189 meter/sec RA = 235
18403 deg
ZDOT = 5980
864779 TA = 324
96352
MA = 325
08372
Ha = 222
275 n
mi
Hp = 213
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11934559
84 X = -3575196
78
Y = -18732937
16 feet Y = -5750128
63 meter
Z = 1122280
16 Z = 324552
31
XDOT = 13823
570722 XDOT = 4209
961498
YDOT = -7599
951407 feet/sec YDOT = -2269
366486 meter/sec
ZDOT = 19622
259773 ZDOT = 6001
324788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11958078
76 X = -3644822
41
Y = -18722255
39 feet Y = -5706543
44 meter
Z = 1047698
24 Z = 319338
42
XDOT = 12325
958253 XDOT = 3756
952076
YDOT = -6738
323698 feet/sec YDOT = -2053
841063 meter/sec
ZDOT = 19710
842907 ZDOT = 6007
864918
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 15282
01824543
00016717 00000-0 10270-3 0 9091
2 25544 51
6412 235
8681 0006218 17
7726 342
3643 15
54257582 5757
Satellite: ISS
Catalog Number: 25544
Epoch time: 15282
01824543 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 235
8681 deg
Eccentricity:
0006218
Arg of perigee: 17
7726 deg
Mean anomaly: 342
3643 deg
Mean motion: 15
54257582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 575
Checksum: 312
Coasting Arc #11 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2015/282/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2729883
48 A = 6787066
55 meter
Y = 5861124
48 meter E =
0006621
Z = -2071368
89 I = 51
37040
XDOT = -5295
895943 Wp = 82
04585
YDOT = 524
122180 meter/sec RA = 230
19206 deg
ZDOT = -5510
742960 TA = 120
94231
MA = 120
87721
Ha = 222
378 n
mi
Hp = 213
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8956310
62 X = 2674202
09
Y = 19229411
03 feet Y = 5891340
22 meter
Z = -6795829
71 Z = -2058243
58
XDOT = -17374
986690 XDOT = -5274
593833
YDOT = 1719
560958 feet/sec YDOT = 465
018331 meter/sec
ZDOT = -18079
865355 ZDOT = -5536
417950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9345862
87 X = 2848619
00
Y = 19062885
51 feet Y = 5810367
50 meter
Z = -6740199
80 Z = -2054412
90
XDOT = -15835
155963 XDOT = -4826
555537
YDOT = 1348
311054 feet/sec YDOT = 410
965209 meter/sec
ZDOT = -18190
640210 ZDOT = -5544
507136
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 15282
98269438
00016717 00000-0 10270-3 0 9105
2 25544 51
6412 231
0587 0006356 20
9868 339
1545 15
54289563 5902
Satellite: ISS
Catalog Number: 25544
Epoch time: 15282
98269438 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 231
0587 deg
Eccentricity:
0006356
Arg of perigee: 20
9868 deg
Mean anomaly: 339
1545 deg
Mean motion: 15
54289563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 590
Checksum: 331
Coasting Arc #12 (Orbit 605)
---------------------------------------
Vector Time (GMT): 2015/283/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1539353
67 A = 6783471
60 meter
Y = -5565297
34 meter E =
0015554
Z = 3542354
83 I = 51
38078
XDOT = 6147
256634 Wp = 71
09657
YDOT = 1141
132782 meter/sec RA = 225
19372 deg
ZDOT = 4453
049532 TA = 330
91485
MA = 331
00140
Ha = 222
330 n
mi
Hp = 213
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5050372
93 X = -1494214
40
Y = -18258849
55 feet Y = -5582258
52 meter
Z = 11621899
06 Z = 3534987
28
XDOT = 20168
164810 XDOT = 6112
407814
YDOT = 3743
873957 feet/sec YDOT = 1209
681234 meter/sec
ZDOT = 14609
742559 ZDOT = 4482
827267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5765510
95 X = -1757327
74
Y = -18065635
67 feet Y = -5506405
75 meter
Z = 11591034
58 Z = 3532947
34
XDOT = 18876
703003 XDOT = 5753
619075
YDOT = 3455
001196 feet/sec YDOT = 1053
084365 meter/sec
ZDOT = 14737
942322 ZDOT = 4492
124820
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 15284
01142356
00016717 00000-0 10270-3 0 9111
2 25544 51
6422 225
9289 0006152 24
7167 335
4279 15
54319694 6062
Satellite: ISS
Catalog Number: 25544
Epoch time: 15284
01142356 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 225
9289 deg
Eccentricity:
0006152
Arg of perigee: 24
7167 deg
Mean anomaly: 335
4279 deg
Mean motion: 15
54319694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 606
Checksum: 307
Coasting Arc #13 (Orbit 620)
---------------------------------------
Vector Time (GMT): 2015/284/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 89728
04 A = 6779611
86 meter
Y = 4942090
05 meter E =
0015677
Z = -4655556
62 I = 51
39161
XDOT = -6610
503188 Wp = 55
11180
YDOT = -2584
595057 meter/sec RA = 220
18655 deg
ZDOT = -2869
174935 TA = 186
21928
MA = 186
23877
Ha = 222
432 n
mi
Hp = 212
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 294383
33 X = 57073
03
Y = 16214206
19 feet Y = 4942910
22 meter
Z = -15274135
89 Z = -4655200
73
XDOT = -21688
002585 XDOT = -6567
172707
YDOT = -8479
642576 feet/sec YDOT = -2658
276186 meter/sec
ZDOT = -9413
303592 ZDOT = -2901
182374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1242070
91 X = 378583
21
Y = 16169941
58 feet Y = 4928598
19 meter
Z = -15273395
84 Z = -4655331
05
XDOT = -20863
466367 XDOT = -6359
184549
YDOT = -7424
631755 feet/sec YDOT = -2263
027759 meter/sec
ZDOT = -9550
894015 ZDOT = -2911
112496
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 15284
97584328
00016717 00000-0 10270-3 0 9126
2 25544 51
6428 221
1204 0006252 28
1831 331
9660 15
54320013 6219
Satellite: ISS
Catalog Number: 25544
Epoch time: 15284
97584328 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 221
1204 deg
Eccentricity:
0006252
Arg of perigee: 28
1831 deg
Mean anomaly: 331
9660 deg
Mean motion: 15
54320013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 621
Checksum: 279
Coasting Arc #14 (Orbit 636)
---------------------------------------
Vector Time (GMT): 2015/285/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1507101
77 A = 6776966
81 meter
Y = -4037904
94 meter E =
0007117
Z = 5223918
82 I = 51
40895
XDOT = 6636
773083 Wp = 62
04662
YDOT = 3729
375824 meter/sec RA = 215
17023 deg
ZDOT = 970
229116 TA = 18
65811
MA = 18
63204
Ha = 222
313 n
mi
Hp = 212
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4944559
61 X = 1526766
26
Y = -13247719
60 feet Y = -4020940
89 meter
Z = 17138841
27 Z = 5231288
46
XDOT = 21774
189904 XDOT = 6589
863931
YDOT = 12235
484988 feet/sec YDOT = 3803
330442 meter/sec
ZDOT = 3183
166390 ZDOT = 1002
355452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3900796
05 X = 1188962
64
Y = -13550721
85 feet Y = -4130260
02 meter
Z = 17171265
30 Z = 5233801
66
XDOT = 21564
546468 XDOT = 6572
873764
YDOT = 10406
755764 feet/sec YDOT = 3171
979157 meter/sec
ZDOT = 3321
097368 ZDOT = 1012
270478
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 15286
00453981
00016717 00000-0 10270-3 0 9133
2 25544 51
6435 215
9899 0006207 31
2227 328
9294 15
54372989 6377
Satellite: ISS
Catalog Number: 25544
Epoch time: 15286
00453981 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 215
9899 deg
Eccentricity:
0006207
Arg of perigee: 31
2227 deg
Mean anomaly: 328
9294 deg
Mean motion: 15
54372989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 637
Checksum: 334
Coasting Arc #15 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2015/286/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3114787
82 A = 6776924
67 meter
Y = 3010024
21 meter E =
0018188
Z = -5227048
07 I = 51
43588
XDOT = -6099
750618 Wp = 80
41208
YDOT = -4507
389573 meter/sec RA = 210
15397 deg
ZDOT = 1045
304236 TA = 199
60902
MA = 199
67906
Ha = 222
445 n
mi
Hp = 212
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10219120
15 X = -3122823
55
Y = 9875407
50 feet Y = 2975147
03 meter
Z = -17149107
85 Z = -5242199
31
XDOT = -20012
305176 XDOT = -6053
972347
YDOT = -14788
023534 feet/sec YDOT = -4575
344920 meter/sec
ZDOT = 3429
475840 ZDOT = 1015
783928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9214289
13 X = -2808515
33
Y = 10713972
79 feet Y = 3265618
91 meter
Z = -17214925
29 Z = -5247109
23
XDOT = -20460
330095 XDOT = -6236
308613
YDOT = -12321
327507 feet/sec YDOT = -3755
540624 meter/sec
ZDOT = 3302
894850 ZDOT = 1006
722350
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 15286
96892917
00016717 00000-0 10270-3 0 9145
2 25544 51
6438 211
1821 0006282 35
9859 324
1715 15
54391703 6526
Satellite: ISS
Catalog Number: 25544
Epoch time: 15286
96892917 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 211
1821 deg
Eccentricity:
0006282
Arg of perigee: 35
9859 deg
Mean anomaly: 324
1715 deg
Mean motion: 15
54391703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 325
Coasting Arc #16 (Orbit 667)
---------------------------------------
Vector Time (GMT): 2015/287/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4599410
68 A = 6779508
52 meter
Y = -1889416
72 meter E =
0014258
Z = 4602379
66 I = 51
47270
XDOT = 5030
326408 Wp = 54
65982
YDOT = 4973
604572 meter/sec RA = 205
14117 deg
ZDOT = -2970
669283 TA = 65
07931
MA = 64
93120
Ha = 222
454 n
mi
Hp = 212
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15089930
06 X = 4597839
60
Y = -6198873
74 feet Y = -1837991
37 meter
Z = 15099670
79 Z = 4624719
60
XDOT = 16503
695564 XDOT = 4988
767219
YDOT = 16317
600301 feet/sec YDOT = 5029
624314 meter/sec
ZDOT = -9746
290298 ZDOT = -2946
333840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14268008
45 X = 4348888
97
Y = -7721913
62 feet Y = -2353639
27 meter
Z = 15196317
58 Z = 4631837
60
XDOT = 17608
343518 XDOT = 5367
023104
YDOT = 13466
609724 feet/sec YDOT = 4104
622644 meter/sec
ZDOT = -9642
132276 ZDOT = -2938
921918
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 15287
99759510
00016717 00000-0 10270-3 0 9151
2 25544 51
6440 206
0517 0006301 40
2997 319
8622 15
54372139 6685
Satellite: ISS
Catalog Number: 25544
Epoch time: 15287
99759510 = yrday
fracday
Element set: 915
Inclination: 51
6440 deg
RA of node: 206
0517 deg
Eccentricity:
0006301
Arg of perigee: 40
2997 deg
Mean anomaly: 319
8622 deg
Mean motion: 15
54372139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 668
Checksum: 320
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