[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 12th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 35520 9 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 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
072/04:10:55
320 -0
1 3
4 3
5
N/A -2
2 -0
3 225
0
000/00:07:50
640 2
7 0
3 221
4
Coasting Arc #1 (Orbit 3632)
---------------------------------------
Vector Time (GMT): 2014/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5871853
88 A = 6796278
42 meter
Y = 3082401
70 meter E =
0012119
Z = 1454985
06 I = 51
43862
XDOT = -1149
525632 Wp = 129
85773
YDOT = 4921
951324 meter/sec RA = 217
76989 deg
ZDOT = -5763
724525 TA = 34
23614
MA = 34
15807
Ha = 224
259 n
mi
Hp = 219
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19264612
48 X = 5829881
62
Y = 10112866
47 feet Y = 3147830
03 meter
Z = 4773573
03 Z = 1483406
96
XDOT = -3771
409554 XDOT = -1176
480656
YDOT = 16148
134264 feet/sec YDOT = 4908
945190 meter/sec
ZDOT = -18909
857364 ZDOT = -5769
374732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17006682
54 X = 5183636
84
Y = 13528199
10 feet Y = 4123395
09 meter
Z = 4893152
33 Z = 1491432
83
XDOT = -5618
423399 XDOT = -1712
495452
YDOT = 13939
858380 feet/sec YDOT = 4248
868834 meter/sec
ZDOT = -18934
386992 ZDOT = -5771
201155
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 14071
53514391
00016717 00000-0 10270-3 0 9001
2 25544 51
6455 218
6538 0003067 248
3474 111
7351 15
51419247 36332
Satellite: ISS
Catalog Number: 25544
Epoch time: 14071
53514391 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 218
6538 deg
Eccentricity:
0003067
Arg of perigee: 248
3474 deg
Mean anomaly: 111
7351 deg
Mean motion: 15
51419247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3633
Checksum: 297
Coasting Arc #2 (Orbit 3642)
---------------------------------------
Vector Time (GMT): 2014/072/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5988608
98 A = 6798391
91 meter
Y = -2992406
59 meter E =
0009443
Z = -1148718
21 I = 51
46054
XDOT = 1269
630765 Wp = 9
97843
YDOT = -4781
494753 meter/sec RA = 214
40633 deg
ZDOT = 5853
152173 TA = 337
53491
MA = 337
57624
Ha = 224
998 n
mi
Hp = 221
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19647667
27 X = -5949122
11
Y = -9817606
93 feet Y = -3059154
42 meter
Z = -3768760
52 Z = -1177713
30
XDOT = 4165
455267 XDOT = 1294
571831
YDOT = -15687
318743 feet/sec YDOT = -4767
156720 meter/sec
ZDOT = 19203
255160 ZDOT = 5859
380965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19545333
33 X = 5957417
60
Y = -9973041
12 feet Y = -3039782
93 meter
Z = -3890782
27 Z = -1185910
44
XDOT = 9500
276216 XDOT = 2895
684191
YDOT = 11136
777902 feet/sec YDOT = 3394
489904 meter/sec
ZDOT = 19230
205140 ZDOT = 5861
366527
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 14072
17928006
00016717 00000-0 10270-3 0 9015
2 25544 51
6495 215
4606 0004588 296
7355 63
3326 15
50811894 36439
Satellite: ISS
Catalog Number: 25544
Epoch time: 14072
17928006 = yrday
fracday
Element set: 901
Inclination: 51
6495 deg
RA of node: 215
4606 deg
Eccentricity:
0004588
Arg of perigee: 296
7355 deg
Mean anomaly: 63
3326 deg
Mean motion: 15
50811894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3643
Checksum: 318
Coasting Arc #3 (Orbit 3658)
---------------------------------------
Vector Time (GMT): 2014/073/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6093719
07 A = 6798813
40 meter
Y = 2958705
20 meter E =
0008532
Z = 525725
95 I = 51
48843
XDOT = -1669
734427 Wp = 133
98136
YDOT = 4508
689253 meter/sec RA = 209
43890 deg
ZDOT = -5965
569284 TA = 40
34362
MA = 40
28036
Ha = 225
158 n
mi
Hp = 221
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19992516
62 X = 6057627
49
Y = 9707038
05 feet Y = 3026647
35 meter
Z = 1724822
68 Z = 555239
90
XDOT = -5478
131321 XDOT = -1691
049061
YDOT = 14792
287574 feet/sec YDOT = 4489
897181 meter/sec
ZDOT = -19572
077703 ZDOT = -5973
732928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19487808
75 X = -5939884
11
Y = 10663424
97 feet Y = 3250211
93 meter
Z = 1849053
78 Z = 563591
59
XDOT = -8175
839250 XDOT = -2491
995803
YDOT = -11512
736400 feet/sec YDOT = -3509
082055 meter/sec
ZDOT = -19607
156888 ZDOT = -5976
261419
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 14073
21030414
00016717 00000-0 10270-3 0 9029
2 25544 51
6498 210
3468 0004564 300
2939 59
7760 15
50825166 36590
Satellite: ISS
Catalog Number: 25544
Epoch time: 14073
21030414 = yrday
fracday
Element set: 902
Inclination: 51
6498 deg
RA of node: 210
3468 deg
Eccentricity:
0004564
Arg of perigee: 300
2939 deg
Mean anomaly: 59
7760 deg
Mean motion: 15
50825166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3659
Checksum: 303
Coasting Arc #4 (Orbit 3674)
---------------------------------------
Vector Time (GMT): 2014/074/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6146344
26 A = 6798691
52 meter
Y = -2886108
44 meter E =
0012311
Z = 101428
61 I = 51
51680
XDOT = 2112
201204 Wp = 24
06274
YDOT = -4278
709052 meter/sec RA = 204
47273 deg
ZDOT = 5999
447410 TA = 337
03054
MA = 337
08554
Ha = 225
173 n
mi
Hp = 221
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20165171
47 X = -6114107
04
Y = -9468859
72 feet Y = -2954660
54 meter
Z = 332771
03 Z = 71649
60
XDOT = 6929
793976 XDOT = 2130
746618
YDOT = -14037
759356 feet/sec YDOT = -4254
984438 meter/sec
ZDOT = 19683
226410 ZDOT = 6009
753787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19209735
38 X = 5855127
34
Y = -11284823
16 feet Y = -3439614
10 meter
Z = 207398
28 Z = 63215
00
XDOT = 6909
148250 XDOT = 2105
908387
YDOT = 12147
573988 feet/sec YDOT = 3702
580551 meter/sec
ZDOT = 19727
321120 ZDOT = 6012
887477
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 14074
24129179
00016717 00000-0 10270-3 0 9031
2 25544 51
6503 205
2322 0004791 306
4011 53
6698 15
50913863 36753
Satellite: ISS
Catalog Number: 25544
Epoch time: 14074
24129179 = yrday
fracday
Element set: 903
Inclination: 51
6503 deg
RA of node: 205
2322 deg
Eccentricity:
0004791
Arg of perigee: 306
4011 deg
Mean anomaly: 53
6698 deg
Mean motion: 15
50913863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3675
Checksum: 298
Coasting Arc #5 (Orbit 3689)
---------------------------------------
Vector Time (GMT): 2014/075/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6136221
50 A = 6798442
13 meter
Y = 2817777
12 meter E =
0005834
Z = -764028
60 I = 51
54494
XDOT = -2608
733690 Wp = 149
38831
YDOT = 4077
923225 meter/sec RA = 199
50923 deg
ZDOT = -5937
131605 TA = 38
86653
MA = 38
82459
Ha = 225
285 n
mi
Hp = 221
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20131960
30 X = 6107967
80
Y = 9244675
58 feet Y = 2886238
18 meter
Z = -2506655
51 Z = -734288
99
XDOT = -8558
837564 XDOT = -2625
299572
YDOT = 13379
013205 feet/sec YDOT = 4048
657101 meter/sec
ZDOT = -19478
778231 ZDOT = -5949
845277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18814734
28 X = -5734731
01
Y = 11720825
23 feet Y = 3572507
53 meter
Z = -2381428
90 Z = -725859
53
XDOT = -5661
339996 XDOT = -1725
576431
YDOT = -13039
017292 feet/sec YDOT = -3974
292471 meter/sec
ZDOT = -19533
012537 ZDOT = -5953
662221
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 14075
20781337
00016717 00000-0 10270-3 0 9049
2 25544 51
6506 200
4380 0004783 308
9134 51
1590 15
50921365 36908
Satellite: ISS
Catalog Number: 25544
Epoch time: 14075
20781337 = yrday
fracday
Element set: 904
Inclination: 51
6506 deg
RA of node: 200
4380 deg
Eccentricity:
0004783
Arg of perigee: 308
9134 deg
Mean anomaly: 51
1590 deg
Mean motion: 15
50921365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3690
Checksum: 291
Coasting Arc #6 (Orbit 3705)
---------------------------------------
Vector Time (GMT): 2014/076/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6054525
75 A = 6797603
65 meter
Y = -2728304
04 meter E =
0013384
Z = 1411956
21 I = 51
57249
XDOT = 3127
704577 Wp = 39
48930
YDOT = -3934
067531 meter/sec RA = 194
54606 deg
ZDOT = 5789
860132 TA = 335
90559
MA = 335
96814
Ha = 225
381 n
mi
Hp = 220
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19863929
62 X = -6030426
06
Y = -8951128
76 feet Y = -2795874
66 meter
Z = 4632402
25 Z = 1382603
24
XDOT = 10261
497955 XDOT = 3143
338543
YDOT = -12907
045704 feet/sec YDOT = -3899
003175 meter/sec
ZDOT = 18995
604108 ZDOT = 5805
092647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18225805
81 X = 5555225
61
Y = -11985341
05 feet Y = -3653131
95 meter
Z = 4508786
83 Z = 1374278
23
XDOT = 4575
641672 XDOT = 1394
655582
YDOT = 14153
962907 feet/sec YDOT = 4314
127894 meter/sec
ZDOT = 19060
459783 ZDOT = 5809
628142
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 14076
23873406
00016717 00000-0 10270-3 0 9053
2 25544 51
6505 195
3230 0005019 315
2348 44
8398 15
51014193 37060
Satellite: ISS
Catalog Number: 25544
Epoch time: 14076
23873406 = yrday
fracday
Element set: 905
Inclination: 51
6505 deg
RA of node: 195
3230 deg
Eccentricity:
0005019
Arg of perigee: 315
2348 deg
Mean anomaly: 44
8398 deg
Mean motion: 15
51014193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3706
Checksum: 297
Coasting Arc #7 (Orbit 3720)
---------------------------------------
Vector Time (GMT): 2014/077/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5899682
79 A = 6796594
79 meter
Y = 2661906
25 meter E =
0001594
Z = -2072115
00 I = 51
59934
XDOT = -3666
996182 Wp = 145
96210
YDOT = 3825
554684 meter/sec RA = 189
58508 deg
ZDOT = -5529
519560 TA = 56
93400
MA = 56
91869
Ha = 225
422 n
mi
Hp = 220
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19355914
68 X = 5879543
96
Y = 8733288
23 feet Y = 2727767
36 meter
Z = -6798277
56 Z = -2043504
48
XDOT = -12030
827368 XDOT = -3682
641198
YDOT = 12551
032428 feet/sec YDOT = 3784
459645 meter/sec
ZDOT = -18141
468373 ZDOT = -5547
371919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17572919
34 X = -5356225
81
Y = 11989082
20 feet Y = 3654272
25 meter
Z = -6677780
18 Z = -2035387
40
XDOT = -3611
085373 XDOT = -1100
658822
YDOT = -15433
551557 feet/sec YDOT = -4704
146515 meter/sec
ZDOT = -18217
380026 ZDOT = -5552
657432
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 14077
20519213
00016717 00000-0 10270-3 0 9065
2 25544 51
6503 190
5286 0005048 317
6820 42
3941 15
51031352 37219
Satellite: ISS
Catalog Number: 25544
Epoch time: 14077
20519213 = yrday
fracday
Element set: 906
Inclination: 51
6503 deg
RA of node: 190
5286 deg
Eccentricity:
0005048
Arg of perigee: 317
6820 deg
Mean anomaly: 42
3941 deg
Mean motion: 15
51031352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 278
Coasting Arc #8 (Orbit 3736)
---------------------------------------
Vector Time (GMT): 2014/078/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5661941
82 A = 6795136
10 meter
Y = -2598554
04 meter E =
0012342
Z = 2694537
48 I = 51
62537
XDOT = 4204
209398 Wp = 55
41580
YDOT = -3776
773488 meter/sec RA = 184
62330 deg
ZDOT = 5181
865060 TA = 335
00698
MA = 335
06669
Ha = 225
592 n
mi
Hp = 220
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18575924
59 X = -5645552
64
Y = -8525439
75 feet Y = -2661777
48 meter
Z = 8840346
07 Z = 2667072
64
XDOT = 13793
337919 XDOT = 4220
957725
YDOT = -12390
989133 feet/sec YDOT = -3729
664939 meter/sec
ZDOT = 17000
869621 ZDOT = 5202
329812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16795726
59 X = 5119337
46
Y = -11733861
29 feet Y = -3576480
92 meter
Z = 8724670
98 Z = 2659279
71
XDOT = 2881
240042 XDOT = 878
201965
YDOT = 16854
631381 feet/sec YDOT = 5137
291645 meter/sec
ZDOT = 17087
817323 ZDOT = 5208
366720
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 14078
23604622
00016717 00000-0 10270-3 0 9079
2 25544 51
6498 185
4129 0005239 323
6284 36
4511 15
51108261 37372
Satellite: ISS
Catalog Number: 25544
Epoch time: 14078
23604622 = yrday
fracday
Element set: 907
Inclination: 51
6498 deg
RA of node: 185
4129 deg
Eccentricity:
0005239
Arg of perigee: 323
6284 deg
Mean anomaly: 36
4511 deg
Mean motion: 15
51108261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3737
Checksum: 305
Coasting Arc #9 (Orbit 3751)
---------------------------------------
Vector Time (GMT): 2014/079/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5352366
58 A = 6793504
15 meter
Y = 2579234
69 meter E =
0004170
Z = -3299815
66 I = 51
65030
XDOT = -4719
004773 Wp = 24
30989
YDOT = 3758
281886 meter/sec RA = 179
66282 deg
ZDOT = -4715
148827 TA = 193
94171
MA = 193
95323
Ha = 225
565 n
mi
Hp = 220
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17560257
79 X = 5339156
73
Y = 8462056
08 feet Y = 2639014
01 meter
Z = -10826166
86 Z = -3273846
88
XDOT = -15482
299123 XDOT = -4737
775189
YDOT = 12330
321147 feet/sec YDOT = 3705
405405 meter/sec
ZDOT = -15469
648382 ZDOT = -4738
119277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16042253
38 X = -4889678
83
Y = 11179053
29 feet Y = 3407375
44 meter
Z = -10716800
36 Z = -3266480
75
XDOT = -2343
344251 XDOT = -714
251328
YDOT = -18291
287966 feet/sec YDOT = -5575
184572 meter/sec
ZDOT = -15567
189357 ZDOT = -4744
879316
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 14079
20244059
00016717 00000-0 10270-3 0 9082
2 25544 51
6488 180
6177 0005262 326
6610 33
4209 15
51147889 37520
Satellite: ISS
Catalog Number: 25544
Epoch time: 14079
20244059 = yrday
fracday
Element set: 908
Inclination: 51
6488 deg
RA of node: 180
6177 deg
Eccentricity:
0005262
Arg of perigee: 326
6610 deg
Mean anomaly: 33
4209 deg
Mean motion: 15
51147889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3752
Checksum: 316
Coasting Arc #10 (Orbit 3767)
---------------------------------------
Vector Time (GMT): 2014/080/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4959116
32 A = 6791733
54 meter
Y = -2589081
98 meter E =
0009392
Z = 3840851
54 I = 51
67531
XDOT = 5206
315594 Wp = 69
87187
YDOT = -3788
076040 meter/sec RA = 174
70097 deg
ZDOT = 4163
520184 TA = 336
30470
MA = 336
34792
Ha = 225
785 n
mi
Hp = 220
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16270066
65 X = -4948453
77
Y = -8494363
44 feet Y = -2644477
96 meter
Z = 12601218
95 Z = 3816786
89
XDOT = 17081
087907 XDOT = 5228
062607
YDOT = -12428
070998 feet/sec YDOT = -3729
733638 meter/sec
ZDOT = 13659
843123 ZDOT = 4188
865102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15265476
73 X = 4652917
31
Y = -10313970
51 feet Y = -3143698
21 meter
Z = 12499889
23 Z = 3809966
24
XDOT = 2058
412637 XDOT = 627
404172
YDOT = 19752
359709 feet/sec YDOT = 6020
519239 meter/sec
ZDOT = 13767
433393 ZDOT = 4196
313698
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 14080
23322849
00016717 00000-0 10270-3 0 9092
2 25544 51
6482 175
5013 0005398 331
9848 28
1012 15
51193853 37680
Satellite: ISS
Catalog Number: 25544
Epoch time: 14080
23322849 = yrday
fracday
Element set: 909
Inclination: 51
6482 deg
RA of node: 175
5013 deg
Eccentricity:
0005398
Arg of perigee: 331
9848 deg
Mean anomaly: 28
1012 deg
Mean motion: 15
51193853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3768
Checksum: 316
Coasting Arc #11 (Orbit 3782)
---------------------------------------
Vector Time (GMT): 2014/081/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4509957
85 A = 6789877
43 meter
Y = 2660694
45 meter E =
0009635
Z = -4332206
72 I = 51
69916
XDOT = -5627
115156 Wp = 36
46913
YDOT = 3829
671242 meter/sec RA = 169
73952 deg
ZDOT = -3502
392377 TA = 197
85063
MA = 197
88450
Ha = 225
697 n
mi
Hp = 219
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14796449
63 X = 4500914
72
Y = 8729312
50 feet Y = 2711076
73 meter
Z = -14213276
65 Z = -4310320
11
XDOT = -18461
663897 XDOT = -5652
507617
YDOT = 12564
538197 feet/sec YDOT = 3766
602933 meter/sec
ZDOT = -11490
788638 ZDOT = -3529
790241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14617894
88 X = -4455534
36
Y = 9168605
26 feet Y = 2794590
88 meter
Z = -14121150
03 Z = -4304126
53
XDOT = -1977
513907 XDOT = -602
746239
YDOT = -21047
681123 feet/sec YDOT = -6415
333206 meter/sec
ZDOT = -11607
075016 ZDOT = -3537
836465
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 14081
19955963
00016717 00000-0 10270-3 0 9109
2 25544 51
6468 170
7052 0005356 335
5283 24
5614 15
51257410 37836
Satellite: ISS
Catalog Number: 25544
Epoch time: 14081
19955963 = yrday
fracday
Element set: 910
Inclination: 51
6468 deg
RA of node: 170
7052 deg
Eccentricity:
0005356
Arg of perigee: 335
5283 deg
Mean anomaly: 24
5614 deg
Mean motion: 15
51257410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3783
Checksum: 309
Coasting Arc #12 (Orbit 3798)
---------------------------------------
Vector Time (GMT): 2014/082/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3987839
70 A = 6788261
35 meter
Y = -2783463
54 meter E =
0005472
Z = 4730801
28 I = 51
72430
XDOT = 5998
502307 Wp = 73
71824
YDOT = -3893
169403 meter/sec RA = 164
77705 deg
ZDOT = 2764
671047 TA = 348
93157
MA = 348
94360
Ha = 225
928 n
mi
Hp = 219
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13083463
58 X = -3979398
72
Y = -9132098
22 feet Y = -2828010
53 meter
Z = 15521001
58 Z = 4711449
64
XDOT = 19680
125680 XDOT = 6028
160889
YDOT = -12772
865494 feet/sec YDOT = -3825
924246 meter/sec
ZDOT = 9070
443069 ZDOT = 2793
883299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14056784
39 X = 4284507
88
Y = -7713588
96 feet Y = -2351101
92 meter
Z = 15439594
72 Z = 4705988
47
XDOT = 2099
142677 XDOT = 639
818688
YDOT = 22236
620424 feet/sec YDOT = 6777
721905 meter/sec
ZDOT = 9194
423315 ZDOT = 2802
460226
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 14082
23028173
00016717 00000-0 10270-3 0 9110
2 25544 51
6468 165
5883 0005450 340
5145 19
5797 15
51275929 37996
Satellite: ISS
Catalog Number: 25544
Epoch time: 14082
23028173 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 165
5883 deg
Eccentricity:
0005450
Arg of perigee: 340
5145 deg
Mean anomaly: 19
5797 deg
Mean motion: 15
51275929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 330
Coasting Arc #13 (Orbit 3813)
---------------------------------------
Vector Time (GMT): 2014/083/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3440084
58 A = 6786741
97 meter
Y = 2976033
21 meter E =
0013788
Z = -5048722
29 I = 51
74872
XDOT = -6267
942956 Wp = 52
83534
YDOT = 3938
071572 meter/sec RA = 159
81476 deg
ZDOT = -1945
031438 TA = 198
25860
MA = 198
30815
Ha = 225
806 n
mi
Hp = 219
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11286366
73 X = 3431075
22
Y = 9763888
50 feet Y = 3014451
66 meter
Z = -16564049
51 Z = -5032033
03
XDOT = -20564
117310 XDOT = -6302
065204
YDOT = 12920
182323 feet/sec YDOT = 3867
788468 meter/sec
ZDOT = -6381
336738 ZDOT = -1975
563319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13719827
45 X = -4181803
41
Y = 6066342
43 feet Y = 1849021
17 meter
Z = -16493912
61 Z = -5027344
56
XDOT = -2363
656849 XDOT = -720
442608
YDOT = -23088
321568 feet/sec YDOT = -7037
320414 meter/sec
ZDOT = -6510
918967 ZDOT = -1984
528101
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 14083
19655060
00016717 00000-0 10270-3 0 9128
2 25544 51
6458 160
7913 0005355 344
3104 15
7881 15
51358540 38148
Satellite: ISS
Catalog Number: 25544
Epoch time: 14083
19655060 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 160
7913 deg
Eccentricity:
0005355
Arg of perigee: 344
3104 deg
Mean anomaly: 15
7881 deg
Mean motion: 15
51358540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3814
Checksum: 300
Coasting Arc #14 (Orbit 3829)
---------------------------------------
Vector Time (GMT): 2014/084/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2839956
46 A = 6785809
10 meter
Y = -3231073
59 meter E =
0003870
Z = 5245666
07 I = 51
77483
XDOT = 6473
872977 Wp = 34
37055
YDOT = -3965
745408 meter/sec RA = 154
85238 deg
ZDOT = 1064
925775 TA = 45
46046
MA = 45
42886
Ha = 226
001 n
mi
Hp = 219
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9317442
46 X = -2829096
39
Y = -10600635
13 feet Y = -3262770
61 meter
Z = 17210190
52 Z = 5231896
73
XDOT = 21239
740739 XDOT = 6512
564650
YDOT = -13010
975747 feet/sec YDOT = -3893
133975 meter/sec
ZDOT = 3493
850968 ZDOT = 1096
469064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13557751
70 X = 4132402
72
Y = -4166604
10 feet Y = -1269980
93 meter
Z = 17152423
62 Z = 5228058
72
XDOT = 2710
597871 XDOT = 826
190231
YDOT = 23717
057916 feet/sec YDOT = 7228
959253 meter/sec
ZDOT = 3627
730072 ZDOT = 1105
732126
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 14084
22720730
00016717 00000-0 10270-3 0 9131
2 25544 51
6461 155
6742 0005406 349
1656 10
9378 15
51363648 38308
Satellite: ISS
Catalog Number: 25544
Epoch time: 14084
22720730 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 155
6742 deg
Eccentricity:
0005406
Arg of perigee: 349
1656 deg
Mean anomaly: 10
9378 deg
Mean motion: 15
51363648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3830
Checksum: 303
Coasting Arc #15 (Orbit 3844)
---------------------------------------
Vector Time (GMT): 2014/085/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2254375
73 A = 6785157
81 meter
Y = 3548509
97 meter E =
0015292
Z = -5338229
62 I = 51
80102
XDOT = -6560
712680 Wp = 68
66482
YDOT = 3938
606011 meter/sec RA = 149
89094 deg
ZDOT = -147
430946 TA = 199
90076
MA = 199
96047
Ha = 225
893 n
mi
Hp = 218
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7396245
82 X = 2240459
13
Y = 11642093
08 feet Y = 3573641
47 meter
Z = -17513876
71 Z = -5327312
46
XDOT = -21524
647900 XDOT = -6603
551287
YDOT = 12921
935733 feet/sec YDOT = 3865
000374 meter/sec
ZDOT = -483
697328 ZDOT = -179
406162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13670991
78 X = -4166918
29
Y = 2223610
72 feet Y = 677756
55 meter
Z = -17468205
41 Z = -5324309
01
XDOT = -3073
947192 XDOT = -936
939104
YDOT = -23896
164148 feet/sec YDOT = -7283
550832 meter/sec
ZDOT = -619
414916 ZDOT = -188
797666
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 14085
19341507
00016717 00000-0 10270-3 0 9140
2 25544 51
6459 150
8770 0005315 353
2826 6
8253 15
51457119 38456
Satellite: ISS
Catalog Number: 25544
Epoch time: 14085
19341507 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 150
8770 deg
Eccentricity:
0005315
Arg of perigee: 353
2826 deg
Mean anomaly: 6
8253 deg
Mean motion: 15
51457119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3845
Checksum: 310
Coasting Arc #16 (Orbit 3860)
---------------------------------------
Vector Time (GMT): 2014/086/04:14:50
640
Vector Time (MET): N/A
Weight (LBS) : 886041
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1642505
67 A = 6785305
71 meter
Y = -3923433
50 meter E =
0007286
Z = 5285241
93 I = 51
82802
XDOT = 6581
219925 Wp = 20
97030
YDOT = -3847
770645 meter/sec RA = 144
93054 deg
ZDOT = -804
108037 TA = 76
73805
MA = 76
65679
Ha = 226
011 n
mi
Hp = 218
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5388798
14 X = -1624184
68
Y = -12872157
14 feet Y = -3941697
95 meter
Z = 17340032
59 Z = 5277307
93
XDOT = 21591
928888 XDOT = 6627
663500
YDOT = -12623
919438 feet/sec YDOT = -3773
915641 meter/sec
ZDOT = -2638
149727 ZDOT = -772
024375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13994927
24 X = 4265653
82
Y = -131534
80 feet Y = -40091
81 meter
Z = 17307022
14 Z = 5275180
35
XDOT = 3345
953348 XDOT = 1019
846580
YDOT = 23778
970212 feet/sec YDOT = 7247
830121 meter/sec
ZDOT = -2501
972018 ZDOT = -762
601071
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 14086
22400650
00016717 00000-0 10270-3 0 9151
2 25544 51
6458 145
7597 0005328 357
7238 2
3888 15
51465156 38618
Satellite: ISS
Catalog Number: 25544
Epoch time: 14086
22400650 = yrday
fracday
Element set: 915
Inclination: 51
6458 deg
RA of node: 145
7597 deg
Eccentricity:
0005328
Arg of perigee: 357
7238 deg
Mean anomaly: 2
3888 deg
Mean motion: 15
51465156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3861
Checksum: 323
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