[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 22nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 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 3353)
---------------------------------------
Vector Time (GMT): 2015/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3588560
26 A = 6778535
81 meter
Y = 3927598
13 meter E =
0008609
Z = 4195950
94 I = 51
27290
XDOT = -2573
117501 Wp = 66
74963
YDOT = 6245
725360 meter/sec RA = 266
81570 deg
ZDOT = -3636
338713 TA = 60
70882
MA = 60
62280
Ha = 218
518 n
mi
Hp = 213
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11773491
68 X = 3523992
06
Y = 12885820
65 feet Y = 3967366
63 meter
Z = 13766243
24 Z = 4213226
57
XDOT = -8441
986552 XDOT = -2625
103679
YDOT = 20491
224934 feet/sec YDOT = 6216
660505 meter/sec
ZDOT = -11930
245123 ZDOT = -3648
964377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5582104
63 X = 1701425
49
Y = -16476319
97 feet Y = -5021982
33 meter
Z = 13839794
84 Z = 4218369
47
XDOT = 20771
571401 XDOT = 6331
174963
YDOT = -3055
929541 feet/sec YDOT = -931
447324 meter/sec
ZDOT = -11985
699583 ZDOT = -3653
241233
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 15203
54153793
00016717 00000-0 10270-3 0 9005
2 25544 51
6431 267
4847 0001943 289
9116 70
1828 15
55241153 33546
Satellite: ISS
Catalog Number: 25544
Epoch time: 15203
54153793 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 267
4847 deg
Eccentricity:
0001943
Arg of perigee: 289
9116 deg
Mean anomaly: 70
1828 deg
Mean motion: 15
55241153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3354
Checksum: 305
Coasting Arc #2 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2015/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2944471
80 A = 6783114
43 meter
Y = -5501080
03 meter E =
0004307
Z = -2657340
45 I = 51
28986
XDOT = 3556
299356 Wp = 33
85803
YDOT = -4399
711891 meter/sec RA = 261
79949 deg
ZDOT = 5175
050216 TA = 296
00008
MA = 296
04443
Ha = 218
676 n
mi
Hp = 213
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9660340
54 X = -2869830
29
Y = -18048162
82 feet Y = -5533589
61 meter
Z = -8718308
56 Z = -2671462
89
XDOT = 11667
648805 XDOT = 3580
095426
YDOT = -14434
750299 feet/sec YDOT = -4359
810132 meter/sec
ZDOT = 16978
511208 ZDOT = 5192
383549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10807706
97 X = -3294189
08
Y = 17355319
48 feet Y = 5289901
38 meter
Z = -8778019
17 Z = -2675540
24
XDOT = -17016
876237 XDOT = -5186
743877
YDOT = -1983
884552 feet/sec YDOT = -604
688012 meter/sec
ZDOT = 17053
858666 ZDOT = 5198
016121
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 15204
50539659
00016717 00000-0 10270-3 0 9012
2 25544 51
6423 262
6719 0001814 294
7421 65
3543 15
55220453 33698
Satellite: ISS
Catalog Number: 25544
Epoch time: 15204
50539659 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 262
6719 deg
Eccentricity:
0001814
Arg of perigee: 294
7421 deg
Mean anomaly: 65
3543 deg
Mean motion: 15
55220453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3369
Checksum: 304
Coasting Arc #3 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2015/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2069553
94 A = 6785873
72 meter
Y = 6420388
66 meter E =
0011414
Z = 684582
48 I = 51
30534
XDOT = -4400
810197 Wp = 128
05320
YDOT = 2057
946387 meter/sec RA = 256
79639 deg
ZDOT = -5935
761301 TA = 44
51407
MA = 44
42243
Ha = 218
739 n
mi
Hp = 213
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6789875
13 X = 1994280
37
Y = 21064267
25 feet Y = 6443110
86 meter
Z = 2246005
52 Z = 694453
34
XDOT = -14438
353665 XDOT = -4394
662047
YDOT = 6751
792608 feet/sec YDOT = 2008
768255 meter/sec
ZDOT = -19474
282485 ZDOT = -5957
124436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14550317
95 X = 4434936
91
Y = -16670540
40 feet Y = -5081180
72 meter
Z = 2287275
72 Z = 697161
64
XDOT = 11950
821211 XDOT = 3642
610305
YDOT = 7719
402328 feet/sec YDOT = 2352
873830 meter/sec
ZDOT = -19566
526225 ZDOT = -5963
877194
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 15205
53350525
00016717 00000-0 10270-3 0 9020
2 25544 51
6429 257
5377 0001818 305
0641 55
0342 15
55247230 33854
Satellite: ISS
Catalog Number: 25544
Epoch time: 15205
53350525 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 257
5377 deg
Eccentricity:
0001818
Arg of perigee: 305
0641 deg
Mean anomaly: 55
0342 deg
Mean motion: 15
55247230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3385
Checksum: 288
Coasting Arc #4 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2015/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1004122
03 A = 6785440
07 meter
Y = -6562243
07 meter E =
0013465
Z = 1368558
13 I = 51
31091
XDOT = 5021
924330 Wp = 52
81578
YDOT = 444
306458 meter/sec RA = 251
79769 deg
ZDOT = 5783
732329 TA = 322
17542
MA = 322
26997
Ha = 218
903 n
mi
Hp = 213
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3294363
61 X = -937314
72
Y = -21529668
86 feet Y = -6573098
35 meter
Z = 4490020
11 Z = 1363842
25
XDOT = 16476
129692 XDOT = 4988
487705
YDOT = 1457
698353 feet/sec YDOT = 500
277649 meter/sec
ZDOT = 18975
499767 ZDOT = 5808
046535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16486992
20 X = -5025235
22
Y = 14238314
46 feet Y = 4339838
25 meter
Z = 4470933
14 Z = 1362740
42
XDOT = -6401
043511 XDOT = -1951
038062
YDOT = -13435
651247 feet/sec YDOT = -4095
186500 meter/sec
ZDOT = 19079
981918 ZDOT = 5815
578489
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 15206
56160991
00016717 00000-0 10270-3 0 9031
2 25544 51
6422 252
4038 0001806 315
0003 45
1004 15
55197246 34010
Satellite: ISS
Catalog Number: 25544
Epoch time: 15206
56160991 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 252
4038 deg
Eccentricity:
0001806
Arg of perigee: 315
0003 deg
Mean anomaly: 45
1004 deg
Mean motion: 15
55197246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 265
Coasting Arc #5 (Orbit 3415)
---------------------------------------
Vector Time (GMT): 2015/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -271759
76 A = 6781592
28 meter
Y = 5952768
68 meter E =
0003406
Z = -3240987
17 I = 51
31031
XDOT = -5331
047507 Wp = 79
65661
YDOT = -2817
536180 meter/sec RA = 246
79216 deg
ZDOT = -4731
647790 TA = 138
08657
MA = 138
06049
Ha = 218
854 n
mi
Hp = 213
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -891600
27 X = -322561
46
Y = 19530080
98 feet Y = 5949445
86 meter
Z = -10633160
01 Z = -3242430
31
XDOT = -17490
313343 XDOT = -5276
160506
YDOT = -9243
885104 feet/sec YDOT = -2876
844239 meter/sec
ZDOT = -15523
778839 ZDOT = -4757
411690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16822680
93 X = 5127553
15
Y = -9952965
37 feet Y = -3033663
84 meter
Z = -10640441
38 Z = -3243206
53
XDOT = 1001
078600 XDOT = 305
128757
YDOT = 18393
204533 feet/sec YDOT = 5606
248742 meter/sec
ZDOT = -15634
076034 ZDOT = -4765
266375
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 15207
52544930
00016717 00000-0 10270-3 0 9048
2 25544 51
6431 247
5907 0001752 316
4443 43
6572 15
55254845 34161
Satellite: ISS
Catalog Number: 25544
Epoch time: 15207
52544930 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 247
5907 deg
Eccentricity:
0001752
Arg of perigee: 316
4443 deg
Mean anomaly: 43
6572 deg
Mean motion: 15
55254845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3416
Checksum: 303
Coasting Arc #6 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2015/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1654513
38 A = 6777043
11 meter
Y = -4695918
23 meter E =
0006950
Z = 4593058
60 I = 51
30722
XDOT = 5244
796545 Wp = 107
90758
YDOT = 4752
048819 meter/sec RA = 241
77276 deg
ZDOT = 2963
382085 TA = 312
40441
MA = 312
46319
Ha = 218
854 n
mi
Hp = 213
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5428193
51 X = 1684590
15
Y = -15406555
87 feet Y = -4677248
57 meter
Z = 15069089
89 Z = 4601168
51
XDOT = 17207
337746 XDOT = 5176
873319
YDOT = 15590
711347 feet/sec YDOT = 4810
319557 meter/sec
ZDOT = 9722
382170 ZDOT = 2988
695462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15752253
62 X = -4801286
90
Y = 4197121
60 feet Y = 1279282
66 meter
Z = 15104813
64 Z = 4603947
20
XDOT = 3640
172125 XDOT = 1109
524464
YDOT = -21784
583006 feet/sec YDOT = -6639
940900 meter/sec
ZDOT = 9830
409457 ZDOT = 2996
308803
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 15208
55354016
00016717 00000-0 10270-3 0 9057
2 25544 51
6418 242
4567 0001738 322
8873 37
2160 15
55255425 34329
Satellite: ISS
Catalog Number: 25544
Epoch time: 15208
55354016 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 242
4567 deg
Eccentricity:
0001738
Arg of perigee: 322
8873 deg
Mean anomaly: 37
2160 deg
Mean motion: 15
55255425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 300
Coasting Arc #7 (Orbit 3446)
---------------------------------------
Vector Time (GMT): 2015/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3067596
69 A = 6774285
30 meter
Y = 2996820
64 meter E =
0013761
Z = -5256017
16 I = 51
31470
XDOT = -4655
617826 Wp = 77
78995
YDOT = -6039
738820 meter/sec RA = 236
74132 deg
ZDOT = -725
248991 TA = 185
23634
MA = 185
25075
Ha = 218
936 n
mi
Hp = 213
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10064293
60 X = -3075348
43
Y = 9832088
72 feet Y = 2962473
86 meter
Z = -17244150
79 Z = -5270937
34
XDOT = -15274
336699 XDOT = -4584
211055
YDOT = -19815
416077 feet/sec YDOT = -6091
401672 meter/sec
ZDOT = -2379
425823 ZDOT = -747
691867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13762005
07 X = 4194659
14
Y = 2516171
52 feet Y = 766929
08 meter
Z = -17308865
01 Z = -5275742
06
XDOT = -7297
674162 XDOT = -2224
331085
YDOT = 22861
180301 feet/sec YDOT = 6968
087756 meter/sec
ZDOT = -2474
895712 ZDOT = -754
348213
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 15209
51737005
00016717 00000-0 10270-3 0 9068
2 25544 51
6427 237
6437 0001835 324
0552 36
0477 15
55248626 34476
Satellite: ISS
Catalog Number: 25544
Epoch time: 15209
51737005 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 237
6437 deg
Eccentricity:
0001835
Arg of perigee: 324
0552 deg
Mean anomaly: 36
0477 deg
Mean motion: 15
55248626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3447
Checksum: 308
Coasting Arc #8 (Orbit 3462)
---------------------------------------
Vector Time (GMT): 2015/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4338900
31 A = 6774839
61 meter
Y = -1075940
33 meter E =
0005505
Z = 5088956
50 I = 51
33355
XDOT = 3552
749419 Wp = 35
75686
YDOT = 6601
903025 meter/sec RA = 231
70688 deg
ZDOT = -1628
013372 TA = 70
04305
MA = 69
98377
Ha = 218
838 n
mi
Hp = 213
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14235237
24 X = 4325889
43
Y = -3529987
97 feet Y = -1027493
06 meter
Z = 16696051
52 Z = 5110002
00
XDOT = 11656
002030 XDOT = 3486
569449
YDOT = 21659
786828 feet/sec YDOT = 6641
262294 meter/sec
ZDOT = -5341
251219 ZDOT = -1610
915312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11156253
53 X = -3400426
07
Y = -9359640
08 feet Y = -2852818
30 meter
Z = 16786782
77 Z = 5116611
39
XDOT = 9975
859355 XDOT = 3040
641932
YDOT = -21371
511961 feet/sec YDOT = -6514
036846 meter/sec
ZDOT = -5268
852498 ZDOT = -1605
946241
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 15210
54544864
00016717 00000-0 10270-3 0 9073
2 25544 51
6410 232
5094 0001846 332
4887 27
6169 15
55284383 34639
Satellite: ISS
Catalog Number: 25544
Epoch time: 15210
54544864 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 232
5094 deg
Eccentricity:
0001846
Arg of perigee: 332
4887 deg
Mean anomaly: 27
6169 deg
Mean motion: 15
55284383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3463
Checksum: 316
Coasting Arc #9 (Orbit 3477)
---------------------------------------
Vector Time (GMT): 2015/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5305830
29 A = 6778589
21 meter
Y = -792269
52 meter E =
0006633
Z = -4149949
08 I = 51
36710
XDOT = -1952
098224 Wp = 97
58545
YDOT = -6407
920963 meter/sec RA = 226
68204 deg
ZDOT = 3723
417580 TA = 210
85299
MA = 210
89198
Ha = 218
996 n
mi
Hp = 213
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17407579
69 X = -5276418
12
Y = -2599309
43 feet Y = -851438
07 meter
Z = -13615318
51 Z = -4175651
86
XDOT = -6404
521733 XDOT = -1898
384821
YDOT = -21023
362738 feet/sec YDOT = -6429
450515 meter/sec
ZDOT = 12215
936943 ZDOT = 3714
064910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8338235
83 X = 2541494
28
Y = 15402406
30 feet Y = 4694653
44 meter
Z = -13725772
91 Z = -4183615
58
XDOT = -11774
702694 XDOT = -3588
929381
YDOT = 17213
280171 feet/sec YDOT = 5246
607796 meter/sec
ZDOT = 12176
808761 ZDOT = 3711
491310
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 15211
50926732
00016717 00000-0 10270-3 0 9089
2 25544 51
6417 227
6963 0001973 336
0733 24
0328 15
55269342 34789
Satellite: ISS
Catalog Number: 25544
Epoch time: 15211
50926732 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 227
6963 deg
Eccentricity:
0001973
Arg of perigee: 336
0733 deg
Mean anomaly: 24
0328 deg
Mean motion: 15
55269342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3478
Checksum: 312
Coasting Arc #10 (Orbit 3493)
---------------------------------------
Vector Time (GMT): 2015/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5791019
81 A = 6783089
78 meter
Y = 2442740
76 meter E =
0012725
Z = 2537829
86 I = 51
40345
XDOT = -41
029192 Wp = 96
13374
YDOT = 5584
077635 meter/sec RA = 221
67259 deg
ZDOT = -5259
821392 TA = 55
24228
MA = 55
12254
Ha = 219
015 n
mi
Hp = 212
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18999408
82 X = 5750946
55
Y = 8014241
32 feet Y = 2507275
57 meter
Z = 8326213
44 Z = 2565863
63
XDOT = -134
610209 XDOT = -77
918990
YDOT = 18320
464682 feet/sec YDOT = 5583
412783 meter/sec
ZDOT = -17256
631863 ZDOT = -5260
110059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5332354
26 X = -1625301
58
Y = -19868448
60 feet Y = -6055903
13 meter
Z = 8446429
90 Z = 2574471
83
XDOT = 13010
843474 XDOT = 3965
705091
YDOT = -10858
354535 feet/sec YDOT = -3309
626462 meter/sec
ZDOT = -17258
832849 ZDOT = -5260
492252
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 15212
53733415
00016717 00000-0 10270-3 0 9098
2 25544 51
6401 222
5613 0002002 342
3872 17
7211 15
55308289 34948
Satellite: ISS
Catalog Number: 25544
Epoch time: 15212
53733415 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 222
5613 deg
Eccentricity:
0002002
Arg of perigee: 342
3872 deg
Mean anomaly: 17
7211 deg
Mean motion: 15
55308289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3494
Checksum: 280
Coasting Arc #11 (Orbit 3508)
---------------------------------------
Vector Time (GMT): 2015/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5671485
53 A = 6785650
20 meter
Y = -3672475
39 meter E =
0011913
Z = -554929
28 I = 51
43708
XDOT = 2201
617763 Wp = 33
81156
YDOT = -4290
693385 meter/sec RA = 216
67863 deg
ZDOT = 5965
919621 TA = 320
17949
MA = 320
26685
Ha = 218
976 n
mi
Hp = 212
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18607235
98 X = -5627301
93
Y = -12048803
77 feet Y = -3735650
61 meter
Z = -1820634
12 Z = -582372
37
XDOT = 7223
155392 XDOT = 2220
454177
YDOT = -14077
078036 feet/sec YDOT = -4265
968247 meter/sec
ZDOT = 19573
227104 ZDOT = 5976
660070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2315263
26 X = 705692
24
Y = 22036353
31 feet Y = 6716680
49 meter
Z = -1938117
88 Z = -590738
33
XDOT = -13802
199265 XDOT = -4206
910336
YDOT = 3156
386693 feet/sec YDOT = 962
066664 meter/sec
ZDOT = 19620
178410 ZDOT = 5980
230379
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 15213
50114145
00016717 00000-0 10270-3 0 9101
2 25544 51
6406 217
7482 0001834 343
5959 16
5135 15
55343554 35097
Satellite: ISS
Catalog Number: 25544
Epoch time: 15213
50114145 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 217
7482 deg
Eccentricity:
0001834
Arg of perigee: 343
5959 deg
Mean anomaly: 16
5135 deg
Mean motion: 15
55343554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3509
Checksum: 292
Coasting Arc #12 (Orbit 3524)
---------------------------------------
Vector Time (GMT): 2015/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4870555
93 A = 6784939
89 meter
Y = 4458694
59 meter E =
0006471
Z = -1550946
75 I = 51
45944
XDOT = -4303
823996 Wp = 134
67801
YDOT = 2712
831678 meter/sec RA = 211
68848 deg
ZDOT = -5735
927217 TA = 62
31984
MA = 62
25419
Ha = 219
176 n
mi
Hp = 212
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15979514
21 X = 4827869
50
Y = 14628263
09 feet Y = 4512921
67 meter
Z = -5088407
97 Z = -1527390
72
XDOT = -14120
157467 XDOT = -4305
977277
YDOT = 8900
366397 feet/sec YDOT = 2664
691448 meter/sec
ZDOT = -18818
658849 ZDOT = -5756
839143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 941811
31 X = 287064
09
Y = -21666979
73 feet Y = -6604095
42 meter
Z = -4987768
24 Z = -1520271
76
XDOT = 14229
158117 XDOT = 4337
047394
YDOT = 4956
613161 feet/sec YDOT = 1510
775692 meter/sec
ZDOT = -18909
120967 ZDOT = -5763
500071
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 15214
52919676
00016717 00000-0 10270-3 0 9117
2 25544 51
6397 212
6127 0002036 349
0564 11
0545 15
55300302 35251
Satellite: ISS
Catalog Number: 25544
Epoch time: 15214
52919676 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 212
6127 deg
Eccentricity:
0002036
Arg of perigee: 349
0564 deg
Mean anomaly: 11
0545 deg
Mean motion: 15
55300302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3525
Checksum: 282
Coasting Arc #13 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2015/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3444401
50 A = 6781009
40 meter
Y = -4749922
66 meter E =
0012270
Z = 3386785
68 I = 51
47413
XDOT = 6035
966142 Wp = 79
99619
YDOT = -1077
759473 meter/sec RA = 206
69276 deg
ZDOT = 4614
940771 TA = 319
72233
MA = 319
81317
Ha = 219
137 n
mi
Hp = 212
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11300529
85 X = -3407482
16
Y = -15583735
76 feet Y = -4788233
74 meter
Z = 11111501
56 Z = 3370143
48
XDOT = 19803
038522 XDOT = 6025
152051
YDOT = -3535
956276 feet/sec YDOT = -1010
321735 meter/sec
ZDOT = 15140
881794 ZDOT = 4644
235547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4329601
62 X = -1319662
57
Y = 18798370
81 feet Y = 5729743
42 meter
Z = 11040655
17 Z = 3365191
69
XDOT = -14205
537271 XDOT = -4329
847760
YDOT = -12262
086643 feet/sec YDOT = -3737
484009 meter/sec
ZDOT = 15267
159786 ZDOT = 4653
430303
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 15215
55724431
00016717 00000-0 10270-3 0 9125
2 25544 51
6397 207
4784 0002104 347
9850 12
1253 15
55336198 35411
Satellite: ISS
Catalog Number: 25544
Epoch time: 15215
55724431 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 207
4784 deg
Eccentricity:
0002104
Arg of perigee: 347
9850 deg
Mean anomaly: 12
1253 deg
Mean motion: 15
55336198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 300
Coasting Arc #14 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2015/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1504489
00 A = 6776491
26 meter
Y = 4637983
38 meter E =
0011570
Z = -4717278
43 I = 51
48762
XDOT = -7134
104273 Wp = 60
68251
YDOT = -482
295881 meter/sec RA = 201
68277 deg
ZDOT = -2749
030484 TA = 182
01757
MA = 182
02225
Ha = 219
237 n
mi
Hp = 212
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4935987
55 X = 1475428
59
Y = 15216480
89 feet Y = 4654644
99 meter
Z = -15476635
26 Z = -4710040
68
XDOT = -23405
853913 XDOT = -7114
827329
YDOT = -1582
335568 feet/sec YDOT = -561
966387 meter/sec
ZDOT = -9019
128884 ZDOT = -2783
639264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7963404
37 X = 2427245
65
Y = -13907883
94 feet Y = -4239123
03 meter
Z = -15446244
13 Z = -4708015
21
XDOT = 13398
717651 XDOT = 4083
929140
YDOT = 17855
622662 feet/sec YDOT = 5442
393787 meter/sec
ZDOT = -9168
035000 ZDOT = -2794
417068
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 15216
52103522
00016717 00000-0 10270-3 0 9136
2 25544 51
6397 202
6641 0002178 355
4315 4
6818 15
55314998 35564
Satellite: ISS
Catalog Number: 25544
Epoch time: 15216
52103522 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 202
6641 deg
Eccentricity:
0002178
Arg of perigee: 355
4315 deg
Mean anomaly: 4
6818 deg
Mean motion: 15
55314998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 304
Coasting Arc #15 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2015/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 710944
15 A = 6773946
62 meter
Y = -4174145
94 meter E =
0002755
Z = 5285275
28 I = 51
50914
XDOT = 7433
708125 Wp = 62
70615
YDOT = 1844
781201 meter/sec RA = 196
66302 deg
ZDOT = 458
066800 TA = 22
92563
MA = 22
91334
Ha = 219
212 n
mi
Hp = 212
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2332493
95 X = 731894
00
Y = -13694704
53 feet Y = -4166078
49 meter
Z = 17340142
00 Z = 5288779
81
XDOT = 24388
806185 XDOT = 7410
301755
YDOT = 6052
431763 feet/sec YDOT = 1927
778940 meter/sec
ZDOT = 1502
843833 ZDOT = 494
121057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11545706
83 X = -3519131
44
Y = 7689913
78 feet Y = 2343885
72 meter
Z = 17355917
28 Z = 5290083
59
XDOT = -11593
628147 XDOT = -3533
737859
YDOT = -21140
500197 feet/sec YDOT = -6443
624460 meter/sec
ZDOT = 1657
762895 ZDOT = 505
286130
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 15217
54907157
00016717 00000-0 10270-3 0 9146
2 25544 51
6396 197
5298 0002293 356
8692 3
2446 15
55325395 35727
Satellite: ISS
Catalog Number: 25544
Epoch time: 15217
54907157 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 197
5298 deg
Eccentricity:
0002293
Arg of perigee: 356
8692 deg
Mean anomaly: 3
2446 deg
Mean motion: 15
55325395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 337
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