[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 15th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
263/11:28:05
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 219
9
Coasting Arc #1 (Orbit 2533)
---------------------------------------
Vector Time (GMT): 2014/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4075211
09 A = 6794314
86 meter
Y = -3888849
00 meter E =
0007808
Z = -3806384
17 I = 51
72174
XDOT = 6007
899973 Wp = 84
08893
YDOT = -2177
632861 meter/sec RA = 11
43457 deg
ZDOT = -4214
060961 TA = 141
40893
MA = 141
35310
Ha = 227
694 n
mi
Hp = 219
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13370115
11 X = -4012931
98
Y = -12758690
95 feet Y = -3934072
71 meter
Z = -12488137
05 Z = -3826029
44
XDOT = 19710
957918 XDOT = 6052
274834
YDOT = -7144
464767 feet/sec YDOT = -2110
200845 meter/sec
ZDOT = -13825
659321 ZDOT = -4184
767435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11772080
74 X = 3588130
21
Y = 14173414
10 feet Y = 4320056
62 meter
Z = -12571005
83 Z = -3831642
58
XDOT = -19442
052595 XDOT = -5925
937631
YDOT = 4015
663471 feet/sec YDOT = 1223
974226 meter/sec
ZDOT = -13700
631762 ZDOT = -4175
952561
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 14258
52404156
00016717 00000-0 10270-3 0 9004
2 25544 51
6469 11
8400 0001959 112
9946 247
1411 15
50292224 25349
Satellite: ISS
Catalog Number: 25544
Epoch time: 14258
52404156 = yrday
fracday
Element set: 900
Inclination: 51
6469 deg
RA of node: 11
8400 deg
Eccentricity:
0001959
Arg of perigee: 112
9946 deg
Mean anomaly: 247
1411 deg
Mean motion: 15
50292224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2534
Checksum: 287
Coasting Arc #2 (Orbit 2549)
---------------------------------------
Vector Time (GMT): 2014/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3957040
96 A = 6793153
69 meter
Y = 3701279
93 meter E =
0012430
Z = 4089303
90 I = 51
68820
XDOT = -6195
902364 Wp = 104
53153
YDOT = 2356
936828 meter/sec RA = 6
48199 deg
ZDOT = 3849
363299 TA = 305
62039
MA = 305
73611
Ha = 227
534 n
mi
Hp = 219
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12982417
86 X = 3895493
79
Y = 12143306
85 feet Y = 3745186
30 meter
Z = 13416351
36 Z = 4108376
85
XDOT = -20327
763663 XDOT = -6240
496637
YDOT = 7732
732375 feet/sec YDOT = 2287
401196 meter/sec
ZDOT = 12629
144683 ZDOT = 3819
156010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11681056
93 X = -3560386
15
Y = -13318799
87 feet Y = -4059570
20 meter
Z = 13496815
84 Z = 4113829
47
XDOT = 20080
063010 XDOT = 6120
403205
YDOT = -4901
186638 feet/sec YDOT = -1493
881687 meter/sec
ZDOT = 12500
200014 ZDOT = 3810
060964
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 14259
55540441
00016717 00000-0 10270-3 0 9017
2 25544 51
6474 6
7281 0001962 114
0110 246
1246 15
50361194 25501
Satellite: ISS
Catalog Number: 25544
Epoch time: 14259
55540441 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 6
7281 deg
Eccentricity:
0001962
Arg of perigee: 114
0110 deg
Mean anomaly: 246
1246 deg
Mean motion: 15
50361194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2550
Checksum: 272
Coasting Arc #3 (Orbit 2564)
---------------------------------------
Vector Time (GMT): 2014/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3782469
92 A = 6792175
54 meter
Y = -3567365
88 meter E =
0010349
Z = -4380576
17 I = 51
65371
XDOT = 6355
837478 Wp = 76
56845
YDOT = -2540
118463 meter/sec RA = 1
52675 deg
ZDOT = -3423
941333 TA = 158
67205
MA = 158
62889
Ha = 227
579 n
mi
Hp = 219
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12409678
22 X = -3721018
32
Y = -11703956
29 feet Y = -3609320
67 meter
Z = -14371969
07 Z = -4398801
26
XDOT = 20852
485163 XDOT = 6400
401644
YDOT = -8333
721991 feet/sec YDOT = -2468
794491 meter/sec
ZDOT = -11233
403324 ZDOT = -3392
957215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11365803
22 X = 3464296
82
Y = 12632715
29 feet Y = 3850451
62 meter
Z = -14448848
50 Z = -4404009
02
XDOT = -20589
352176 XDOT = -6275
634543
YDOT = 5844
117124 feet/sec YDOT = 1781
286899 meter/sec
ZDOT = -11101
124740 ZDOT = -3383
622821
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 14260
52229171
00016717 00000-0 10270-3 0 9021
2 25544 51
6474 1
9361 0001887 115
7289 244
4057 15
50346519 25659
Satellite: ISS
Catalog Number: 25544
Epoch time: 14260
52229171 = yrday
fracday
Element set: 902
Inclination: 51
6474 deg
RA of node: 1
9361 deg
Eccentricity:
0001887
Arg of perigee: 115
7289 deg
Mean anomaly: 244
4057 deg
Mean motion: 15
50346519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2565
Checksum: 304
Coasting Arc #4 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2014/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3591967
63 A = 6791058
87 meter
Y = 3445608
02 meter E =
0010202
Z = 4614042
76 I = 51
61970
XDOT = -6497
631853 Wp = 114
67324
YDOT = 2760
268384 meter/sec RA = 356
56790 deg
ZDOT = 2987
678567 TA = 305
46572
MA = 305
56089
Ha = 227
409 n
mi
Hp = 219
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11784670
69 X = 3530757
64
Y = 11304488
27 feet Y = 3485433
92 meter
Z = 15137935
58 Z = 4631342
95
XDOT = -21317
689807 XDOT = -6542
528010
YDOT = 9055
998634 feet/sec YDOT = 2687
356914 meter/sec
ZDOT = 9802
095037 ZDOT = 2956
004826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10977152
90 X = -3345836
20
Y = -11998233
95 feet Y = -3657061
71 meter
Z = 15210900
96 Z = 4636282
61
XDOT = 21017
067177 XDOT = 6406
002075
YDOT = -6934
440734 feet/sec YDOT = -2113
617536 meter/sec
ZDOT = 9666
848615 ZDOT = 2946
455458
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 14261
55361679
00016717 00000-0 10270-3 0 9036
2 25544 51
6477 356
8238 0001906 115
9913 244
1434 15
50415499 25813
Satellite: ISS
Catalog Number: 25544
Epoch time: 14261
55361679 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 356
8238 deg
Eccentricity:
0001906
Arg of perigee: 115
9913 deg
Mean anomaly: 244
1434 deg
Mean motion: 15
50415499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 323
Coasting Arc #5 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2014/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3359926
43 A = 6790225
30 meter
Y = -3387087
48 meter E =
0013066
Z = -4843915
54 I = 51
58544
XDOT = 6593
404371 Wp = 77
62655
YDOT = -2974
182748 meter/sec RA = 351
60679 deg
ZDOT = -2496
728700 TA = 167
78002
MA = 167
74829
Ha = 227
469 n
mi
Hp = 219
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11023380
67 X = -3298271
45
Y = -11112491
75 feet Y = -3424316
14 meter
Z = -15892111
36 Z = -4860087
39
XDOT = 21631
904103 XDOT = 6638
300579
YDOT = -9757
817414 feet/sec YDOT = -2900
200272 meter/sec
ZDOT = -8191
367125 ZDOT = -2464
589665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10425042
21 X = 3177552
86
Y = 11582286
23 feet Y = 3530280
84 meter
Z = -15960286
28 Z = -4864695
26
XDOT = -21245
658567 XDOT = -6475
676731
YDOT = 8037
795556 feet/sec YDOT = 2449
920085 meter/sec
ZDOT = -8054
110465 ZDOT = -2454
892870
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 14262
52046843
00016717 00000-0 10270-3 0 9048
2 25544 51
6475 352
0319 0001818 117
6760 242
4575 15
50400458 25962
Satellite: ISS
Catalog Number: 25544
Epoch time: 14262
52046843 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 352
0319 deg
Eccentricity:
0001818
Arg of perigee: 117
6760 deg
Mean anomaly: 242
4575 deg
Mean motion: 15
50400458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 304
Coasting Arc #6 (Orbit 2610)
---------------------------------------
Vector Time (GMT): 2014/263/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3181700
87 A = 6792410
08 meter
Y = -4230684
62 meter E =
0009981
Z = -4266565
69 I = 51
56328
XDOT = 6620
605078 Wp = 110
96947
YDOT = 1363
031805 meter/sec RA = 346
71168 deg
ZDOT = 3588
922559 TA = 195
79076
MA = 195
82191
Ha = 227
415 n
mi
Hp = 219
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10438651
15 X = 3249498
41
Y = -13880198
89 feet Y = -4194726
22 meter
Z = -13997918
92 Z = -4250944
32
XDOT = 21721
145270 XDOT = 6587
437523
YDOT = 4471
889125 feet/sec YDOT = 1436
882678 meter/sec
ZDOT = 11774
680312 ZDOT = 3621
003658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12679483
78 X = -3864706
66
Y = 11947103
44 feet Y = 3641477
13 meter
Z = -13930703
63 Z = -4246078
47
XDOT = -19736
129644 XDOT = -6015
572315
YDOT = -7070
256330 feet/sec YDOT = -2155
014129 meter/sec
ZDOT = 11910
893317 ZDOT = 3630
440283
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 14263
48730189
00016717 00000-0 10270-3 0 9058
2 25544 51
6477 347
2391 0001899 117
4348 242
6996 15
50462957 26118
Satellite: ISS
Catalog Number: 25544
Epoch time: 14263
48730189 = yrday
fracday
Element set: 905
Inclination: 51
6477 deg
RA of node: 347
2391 deg
Eccentricity:
0001899
Arg of perigee: 117
4348 deg
Mean anomaly: 242
6996 deg
Mean motion: 15
50462957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2611
Checksum: 340
Coasting Arc #7 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2014/264/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3355119
79 A = 6793492
42 meter
Y = 4397374
29 meter E =
0012742
Z = 3934163
59 I = 51
53677
XDOT = -6397
262279 Wp = 85
18685
YDOT = -1262
760360 meter/sec RA = 341
74716 deg
ZDOT = -4031
924474 TA = 47
06153
MA = 46
95470
Ha = 227
451 n
mi
Hp = 219
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11007610
85 X = -3423153
74
Y = 14427081
00 feet Y = 4359475
29 meter
Z = 12907360
85 Z = 3917699
09
XDOT = -20988
393303 XDOT = -6363
080595
YDOT = -4142
914567 feet/sec YDOT = -1334
108106 meter/sec
ZDOT = -13228
098668 ZDOT = -4062
918195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13109177
85 X = 3995677
41
Y = -12620653
37 feet Y = -3846775
15 meter
Z = 12836537
35 Z = 3912576
59
XDOT = 19136
682243 XDOT = 5832
860748
YDOT = 6247
842688 feet/sec YDOT = 1904
342451 meter/sec
ZDOT = -13359
697430 ZDOT = -4072
035777
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 14264
51857252
00016717 00000-0 10270-3 0 9065
2 25544 51
6476 342
1268 0001899 115
8653 244
2693 15
50478263 26271
Satellite: ISS
Catalog Number: 25544
Epoch time: 14264
51857252 = yrday
fracday
Element set: 906
Inclination: 51
6476 deg
RA of node: 342
1268 deg
Eccentricity:
0001899
Arg of perigee: 115
8653 deg
Mean anomaly: 244
2693 deg
Mean motion: 15
50478263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 330
Coasting Arc #8 (Orbit 2641)
---------------------------------------
Vector Time (GMT): 2014/265/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3484288
17 A = 6794498
70 meter
Y = -4602008
43 meter E =
0006953
Z = -3591452
77 I = 51
51074
XDOT = 6132
458699 Wp = 101
75346
YDOT = 1195
988846 meter/sec RA = 336
78184 deg
ZDOT = 4422
856013 TA = 215
79781
MA = 215
84444
Ha = 227
312 n
mi
Hp = 219
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11431391
65 X = 3552936
06
Y = -15098452
86 feet Y = -4562661
55 meter
Z = -11782981
51 Z = -3574359
18
XDOT = 20119
615153 XDOT = 6097
144276
YDOT = 3923
847921 feet/sec YDOT = 1264
369155 meter/sec
ZDOT = 14510
682458 ZDOT = 4452
560684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13391511
10 X = -4081732
58
Y = 13454915
51 feet Y = 4101058
25 meter
Z = -11709454
56 Z = -3569041
75
XDOT = -18356
371657 XDOT = -5595
022081
YDOT = -5548
790837 feet/sec YDOT = -1691
271447 meter/sec
ZDOT = 14636
802893 ZDOT = 4461
297522
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 14265
48537084
00016717 00000-0 10270-3 0 9071
2 25544 51
6473 337
3344 0001824 119
6787 240
4545 15
50509020 26424
Satellite: ISS
Catalog Number: 25544
Epoch time: 14265
48537084 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 337
3344 deg
Eccentricity:
0001824
Arg of perigee: 119
6787 deg
Mean anomaly: 240
4545 deg
Mean motion: 15
50509020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2642
Checksum: 309
Coasting Arc #9 (Orbit 2657)
---------------------------------------
Vector Time (GMT): 2014/266/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3602295
09 A = 6795572
65 meter
Y = 4798144
33 meter E =
0014557
Z = 3176232
57 I = 51
48612
XDOT = -5852
150908 Wp = 96
79375
YDOT = -1201
836138 meter/sec RA = 331
81466 deg
ZDOT = -4804
340754 TA = 46
48335
MA = 46
36247
Ha = 227
287 n
mi
Hp = 219
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11818553
44 X = -3671110
49
Y = 15741943
33 feet Y = 4757476
84 meter
Z = 10420710
53 Z = 3158565
19
XDOT = -19199
970169 XDOT = -5814
938721
YDOT = -3943
031950 feet/sec YDOT = -1267
071342 meter/sec
ZDOT = -15762
272816 ZDOT = -4832
679207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13607813
90 X = 4147661
68
Y = -14279090
03 feet Y = -4352266
64 meter
Z = 10344717
60 Z = 3153069
92
XDOT = 17482
031823 XDOT = 5328
523300
YDOT = 5112
418748 feet/sec YDOT = 1558
265234 meter/sec
ZDOT = -15882
573973 ZDOT = -4841
008547
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 14266
51660423
00016717 00000-0 10270-3 0 9081
2 25544 51
6471 332
2217 0001797 117
3655 242
7678 15
50543619 26584
Satellite: ISS
Catalog Number: 25544
Epoch time: 14266
51660423 = yrday
fracday
Element set: 908
Inclination: 51
6471 deg
RA of node: 332
2217 deg
Eccentricity:
0001797
Arg of perigee: 117
3655 deg
Mean anomaly: 242
7678 deg
Mean motion: 15
50543619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2658
Checksum: 319
Coasting Arc #10 (Orbit 2672)
---------------------------------------
Vector Time (GMT): 2014/267/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3664186
33 A = 6796593
76 meter
Y = -5017395
76 meter E =
0005829
Z = -2757871
49 I = 51
46172
XDOT = 5553
365883 Wp = 72
41677
YDOT = 1245
897142 meter/sec RA = 326
84649 deg
ZDOT = 5122
389908 TA = 256
33867
MA = 256
40358
Ha = 227
222 n
mi
Hp = 219
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12021608
69 X = 3733416
63
Y = -16461272
17 feet Y = -4976033
78 meter
Z = -9048134
81 Z = -2739902
34
XDOT = 18219
704342 XDOT = 5514
138125
YDOT = 4087
589048 feet/sec YDOT = 1307
779922 meter/sec
ZDOT = 16805
741169 ZDOT = 5149
272096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13623682
77 X = -4152498
51
Y = 15207919
02 feet Y = 4635373
72 meter
Z = -8970828
66 Z = -2734308
57
XDOT = -16520
355204 XDOT = -5035
404266
YDOT = -4839
617877 feet/sec YDOT = -1475
115529 meter/sec
ZDOT = 16919
834176 ZDOT = 5157
165457
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 14267
48336835
00016717 00000-0 10270-3 0 9096
2 25544 51
6462 327
4288 0001750 120
5729 239
5594 15
50549718 26739
Satellite: ISS
Catalog Number: 25544
Epoch time: 14267
48336835 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 327
4288 deg
Eccentricity:
0001750
Arg of perigee: 120
5729 deg
Mean anomaly: 239
5594 deg
Mean motion: 15
50549718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2673
Checksum: 339
Coasting Arc #11 (Orbit 2688)
---------------------------------------
Vector Time (GMT): 2014/268/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3713765
30 A = 6797462
28 meter
Y = 5212462
13 meter E =
0015552
Z = 2267863
50 I = 51
43951
XDOT = -5247
971797 Wp = 109
03505
YDOT = -1371
006984 meter/sec RA = 321
87676 deg
ZDOT = -5417
238956 TA = 45
67918
MA = 45
55178
Ha = 227
142 n
mi
Hp = 219
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12184269
37 X = -3782792
91
Y = 17101253
71 feet Y = 5170546
78 meter
Z = 7440497
06 Z = 2249653
93
XDOT = -17217
755241 XDOT = -5205
935345
YDOT = -4498
054408 feet/sec YDOT = -1429
458960 meter/sec
ZDOT = -17773
093688 ZDOT = -5442
630826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13563439
63 X = 4134136
40
Y = -16065561
31 feet Y = -4896783
09 meter
Z = 7362142
35 Z = 2243980
99
XDOT = 15517
833595 XDOT = 4729
835680
YDOT = 4868
258437 feet/sec YDOT = 1483
845172 meter/sec
ZDOT = -17880
820789 ZDOT = -5450
074177
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 14268
51456458
00016717 00000-0 10270-3 0 9107
2 25544 51
6462 322
3155 0001739 117
9214 242
2113 15
50607022 26890
Satellite: ISS
Catalog Number: 25544
Epoch time: 14268
51456458 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 322
3155 deg
Eccentricity:
0001739
Arg of perigee: 117
9214 deg
Mean anomaly: 242
2113 deg
Mean motion: 15
50607022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2689
Checksum: 291
Coasting Arc #12 (Orbit 2703)
---------------------------------------
Vector Time (GMT): 2014/269/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3701969
32 A = 6798323
48 meter
Y = -5413213
91 meter E =
0007922
Z = -1784574
70 I = 51
41742
XDOT = 4949
347022 Wp = 50
42290
YDOT = 1532
253967 meter/sec RA = 316
90585 deg
ZDOT = 5640
933410 TA = 289
95007
MA = 290
03538
Ha = 227
151 n
mi
Hp = 219
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12145568
63 X = 3770895
00
Y = -17759888
16 feet Y = -5371430
95 meter
Z = -5854903
86 Z = -1766422
66
XDOT = 16238
015163 XDOT = 4904
442937
YDOT = 5027
079944 feet/sec YDOT = 1587
350464 meter/sec
ZDOT = 18506
999378 ZDOT = 5664
867685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13278021
12 X = -4047140
84
Y = 16956753
78 feet Y = 5168418
55 meter
Z = -5776765
54 Z = -1760758
14
XDOT = -14535
378898 XDOT = -4430
383488
YDOT = -5067
084613 feet/sec YDOT = -1544
447390 meter/sec
ZDOT = 18608
495230 ZDOT = 5671
869346
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 14269
48129438
00016717 00000-0 10270-3 0 9110
2 25544 51
6454 317
5219 0001715 119
6624 240
4698 15
50589065 27048
Satellite: ISS
Catalog Number: 25544
Epoch time: 14269
48129438 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 317
5219 deg
Eccentricity:
0001715
Arg of perigee: 119
6624 deg
Mean anomaly: 240
4698 deg
Mean motion: 15
50589065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2704
Checksum: 322
Coasting Arc #13 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2014/270/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3681520
36 A = 6798808
39 meter
Y = 5572073
62 meter E =
0015464
Z = 1233666
39 I = 51
39792
XDOT = -4655
489481 Wp = 121
06242
YDOT = -1776
025690 meter/sec RA = 311
93367 deg
ZDOT = -5824
735643 TA = 45
49688
MA = 45
37060
Ha = 227
039 n
mi
Hp = 219
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12078478
88 X = -3749547
80
Y = 18281081
44 feet Y = 5530524
27 meter
Z = 4047461
90 Z = 1215615
90
XDOT = -15273
915621 XDOT = -4606
988409
YDOT = -5826
855937 feet/sec YDOT = -1827
815907 meter/sec
ZDOT = -19110
025077 ZDOT = -5847
233678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12929896
42 X = 3941032
43
Y = -17706736
96 feet Y = -5397013
43 meter
Z = 3969733
39 Z = 1209974
74
XDOT = 13578
606870 XDOT = 4138
759374
YDOT = 5574
852587 feet/sec YDOT = 1699
215068 meter/sec
ZDOT = -19205
368114 ZDOT = -5853
796201
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 14270
51245351
00016717 00000-0 10270-3 0 9120
2 25544 51
6457 312
4081 0001773 118
8675 241
2654 15
50662512 27201
Satellite: ISS
Catalog Number: 25544
Epoch time: 14270
51245351 = yrday
fracday
Element set: 912
Inclination: 51
6457 deg
RA of node: 312
4081 deg
Eccentricity:
0001773
Arg of perigee: 118
8675 deg
Mean anomaly: 241
2654 deg
Mean motion: 15
50662512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 285
Coasting Arc #14 (Orbit 2734)
---------------------------------------
Vector Time (GMT): 2014/271/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3601966
05 A = 6799304
80 meter
Y = -5719074
12 meter E =
0011071
Z = -701604
28 I = 51
37866
XDOT = 4392
513250 Wp = 49
06010
YDOT = 2046
931443 meter/sec RA = 306
96040 deg
ZDOT = 5933
896545 TA = 303
34580
MA = 303
45173
Ha = 227
091 n
mi
Hp = 219
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11817473
92 X = 3669058
58
Y = -18763366
54 feet Y = -5678419
54 meter
Z = -2301851
30 Z = -683942
59
XDOT = 14411
132710 XDOT = 4340
472102
YDOT = 6715
654340 feet/sec YDOT = 2095
761011 meter/sec
ZDOT = 19468
164517 ZDOT = 5955
108471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12365356
67 X = -3768960
71
Y = 18416272
74 feet Y = 5613279
93 meter
Z = -2225755
14 Z = -678410
17
XDOT = -12746
602821 XDOT = -3885
164540
YDOT = -6222
915586 feet/sec YDOT = -1896
744670 meter/sec
ZDOT = 19557
990669 ZDOT = 5961
275556
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 14271
47914852
00016717 00000-0 10270-3 0 9136
2 25544 51
6452 307
6141 0001756 118
5584 241
5744 15
50635134 27355
Satellite: ISS
Catalog Number: 25544
Epoch time: 14271
47914852 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 307
6141 deg
Eccentricity:
0001756
Arg of perigee: 118
5584 deg
Mean anomaly: 241
5744 deg
Mean motion: 15
50635134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2735
Checksum: 305
Coasting Arc #15 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2014/272/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3522893
58 A = 6799287
06 meter
Y = 5806771
01 meter E =
0014080
Z = 109913
26 I = 51
36186
XDOT = -4146
181409 Wp = 131
82174
YDOT = -2392
927169 meter/sec RA = 301
98588 deg
ZDOT = -5984
964906 TA = 46
99127
MA = 46
87337
Ha = 226
967 n
mi
Hp = 219
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11558049
82 X = -3588098
34
Y = 19051085
98 feet Y = 5767011
16 meter
Z = 360607
80 Z = 92640
39
XDOT = -13602
957380 XDOT = -4090
041522
YDOT = -7850
810923 feet/sec YDOT = -2438
979093 meter/sec
ZDOT = -19635
711634 ZDOT = -6004
970189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11778419
42 X = 3590062
24
Y = -18916907
32 feet Y = -5765873
35 meter
Z = 286154
08 Z = 87219
76
XDOT = 12008
343531 XDOT = 3660
143108
YDOT = 7148
095198 feet/sec YDOT = 2178
739416 meter/sec
ZDOT = -19720
348051 ZDOT = -6010
762086
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 14272
51027041
00016717 00000-0 10270-3 0 9148
2 25544 51
6457 302
4999 0001864 122
1334 237
9998 15
50708337 27512
Satellite: ISS
Catalog Number: 25544
Epoch time: 14272
51027041 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 302
4999 deg
Eccentricity:
0001864
Arg of perigee: 122
1334 deg
Mean anomaly: 237
9998 deg
Mean motion: 15
50708337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 314
Coasting Arc #16 (Orbit 2765)
---------------------------------------
Vector Time (GMT): 2014/273/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3394440
91 A = 6799233
83 meter
Y = -5867577
24 meter E =
0013619
Z = 449345
29 I = 51
34546
XDOT = 3950
198358 Wp = 57
21617
YDOT = 2751
374038 meter/sec RA = 297
01046 deg
ZDOT = 5962
210904 TA = 307
64248
MA = 307
76598
Ha = 227
004 n
mi
Hp = 219
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11136617
16 X = 3457618
43
Y = -19250581
50 feet Y = -5829265
12 meter
Z = 1474229
94 Z = 465989
12
XDOT = 12959
968366 XDOT = 3890
175411
YDOT = 9026
817710 feet/sec YDOT = 2795
212574 meter/sec
ZDOT = 19561
059395 ZDOT = 5981
254631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11017167
07 X = -3358032
52
Y = 19313579
47 feet Y = 5886779
02 meter
Z = 1546014
72 Z = 471225
29
XDOT = -11479
371891 XDOT = -3498
912552
YDOT = -8151
780762 feet/sec YDOT = -2484
662776 meter/sec
ZDOT = 19641
548474 ZDOT = 5986
743975
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 14273
54137451
00016717 00000-0 10270-3 0 9150
2 25544 51
6454 297
3863 0001838 120
5404 239
5928 15
50695802 27661
Satellite: ISS
Catalog Number: 25544
Epoch time: 14273
54137451 = yrday
fracday
Element set: 915
Inclination: 51
6454 deg
RA of node: 297
3863 deg
Eccentricity:
0001838
Arg of perigee: 120
5404 deg
Mean anomaly: 239
5928 deg
Mean motion: 15
50695802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2766
Checksum: 325
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