[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 3rd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20182 33 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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 3011)
---------------------------------------
Vector Time (GMT): 2014/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4617543
57 A = 6791208
89 meter
Y = -111421
17 meter E =
0015916
Z = -4993083
26 I = 51
93497
XDOT = 2518
545060 Wp = 100
74680
YDOT = 6886
320524 meter/sec RA = 56
45702 deg
ZDOT = 2178
462261 TA = 190
44329
MA = 190
47639
Ha = 229
004 n
mi
Hp = 220
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15149421
16 X = 4642700
46
Y = -365555
01 feet Y = -59644
30 meter
Z = -16381506
76 Z = -4970591
38
XDOT = 8262
943109 XDOT = 2430
771517
YDOT = 22592
915104 feet/sec YDOT = 6913
993786 meter/sec
ZDOT = 7147
185897 ZDOT = 2190
483315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10046402
05 X = 3062143
35
Y = 11480913
65 feet Y = 3499382
48 meter
Z = -16286521
53 Z = -4964131
76
XDOT = -11257
060311 XDOT = -3431
151983
YDOT = 20045
599265 feet/sec YDOT = 6109
898656 meter/sec
ZDOT = 7196
789223 ZDOT = 2193
581355
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 14031
51229940
00016717 00000-0 10270-3 0 9008
2 25544 51
6489 57
0815 0003780 84
2808 275
8773 15
49927112 30125
Satellite: ISS
Catalog Number: 25544
Epoch time: 14031
51229940 = yrday
fracday
Element set: 900
Inclination: 51
6489 deg
RA of node: 57
0815 deg
Eccentricity:
0003780
Arg of perigee: 84
2808 deg
Mean anomaly: 275
8773 deg
Mean motion: 15
49927112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3012
Checksum: 307
Coasting Arc #2 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2014/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4746269
08 A = 6791583
89 meter
Y = 134858
82 meter E =
0010879
Z = 4848650
48 I = 51
91753
XDOT = -2780
968794 Wp = 69
77147
YDOT = -6682
479263 meter/sec RA = 51
52037 deg
ZDOT = -2528
128972 TA = 45
03948
MA = 44
95132
Ha = 229
093 n
mi
Hp = 219
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15571748
95 X = -4770976
95
Y = 442450
19 feet Y = 81645
08 meter
Z = 15907645
94 Z = 4825534
33
XDOT = -9123
913366 XDOT = -2693
756596
YDOT = -21924
144564 feet/sec YDOT = -6713
090323 meter/sec
ZDOT = -8294
386391 ZDOT = -2541
426046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10574576
58 X = -3223130
94
Y = -11573670
38 feet Y = -3527654
73 meter
Z = 15810022
49 Z = 4818894
85
XDOT = 9827
046001 XDOT = 2995
283621
YDOT = -20421
521867 feet/sec YDOT = -6224
479865 meter/sec
ZDOT = -8349
407984 ZDOT = -2544
899554
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 14032
54390344
00016717 00000-0 10270-3 0 9010
2 25544 51
6475 51
9706 0003894 87
8687 272
2910 15
49984937 30281
Satellite: ISS
Catalog Number: 25544
Epoch time: 14032
54390344 = yrday
fracday
Element set: 901
Inclination: 51
6475 deg
RA of node: 51
9706 deg
Eccentricity:
0003894
Arg of perigee: 87
8687 deg
Mean anomaly: 272
2910 deg
Mean motion: 15
49984937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 335
Coasting Arc #3 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2014/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4898557
46 A = 6792221
58 meter
Y = -201221
52 meter E =
0014238
Z = -4714381
98 I = 51
90038
XDOT = 3005
621230 Wp = 104
14279
YDOT = 6430
635880 meter/sec RA = 46
58351 deg
ZDOT = 2852
404207 TA = 194
11934
MA = 194
15919
Ha = 228
961 n
mi
Hp = 219
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16071382
74 X = 4923343
97
Y = -660175
58 feet Y = -146304
42 meter
Z = -15467132
48 Z = -4690525
76
XDOT = 9860
962041 XDOT = 2919
633264
YDOT = 21097
886744 feet/sec YDOT = 6463
766050 meter/sec
ZDOT = 9358
281519 ZDOT = 2866
795530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11265481
36 X = 3433718
72
Y = 11615539
70 feet Y = 3540416
50 meter
Z = -15366376
59 Z = -4683671
58
XDOT = -8355
153245 XDOT = -2546
650709
YDOT = 20545
747142 feet/sec YDOT = 6262
343729 meter/sec
ZDOT = 9417
959542 ZDOT = 2870
594069
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 14033
51101964
00016717 00000-0 10270-3 0 9027
2 25544 51
6483 47
1799 0003820 90
3135 269
8454 15
49968474 30435
Satellite: ISS
Catalog Number: 25544
Epoch time: 14033
51101964 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 47
1799 deg
Eccentricity:
0003820
Arg of perigee: 90
3135 deg
Mean anomaly: 269
8454 deg
Mean motion: 15
49968474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 316
Coasting Arc #4 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2014/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5051791
26 A = 6792746
76 meter
Y = 258992
83 meter E =
0012583
Z = 4524800
96 I = 51
87975
XDOT = -3190
906889 Wp = 75
52342
YDOT = -6194
871995 meter/sec RA = 41
64434 deg
ZDOT = -3197
462737 TA = 46
54163
MA = 46
43704
Ha = 229
005 n
mi
Hp = 219
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16574118
30 X = -5076291
57
Y = 849714
02 feet Y = 202363
78 meter
Z = 14845147
50 Z = 4500200
96
XDOT = -10468
854622 XDOT = -3105
865305
YDOT = -20324
383186 feet/sec YDOT = -6230
079472 meter/sec
ZDOT = -10490
363309 ZDOT = -3212
756486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11941442
89 X = -3639751
79
Y = -11657590
83 feet Y = -3553233
69 meter
Z = 14741245
99 Z = 4493131
78
XDOT = 7007
443026 XDOT = 2135
868634
YDOT = -20567
499746 feet/sec YDOT = -6268
973923 meter/sec
ZDOT = -10553
882961 ZDOT = -3216
823527
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 14034
54259510
00016717 00000-0 10270-3 0 9033
2 25544 51
6473 42
0686 0003858 93
7366 266
4226 15
50026597 30597
Satellite: ISS
Catalog Number: 25544
Epoch time: 14034
54259510 = yrday
fracday
Element set: 903
Inclination: 51
6473 deg
RA of node: 42
0686 deg
Eccentricity:
0003858
Arg of perigee: 93
7366 deg
Mean anomaly: 266
4226 deg
Mean motion: 15
50026597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 314
Coasting Arc #5 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2014/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5218309
45 A = 6793495
11 meter
Y = -366927
14 meter E =
0012210
Z = -4346503
59 I = 51
85875
XDOT = 3335
584833 Wp = 105
58391
YDOT = 5924
232994 meter/sec RA = 36
70527 deg
ZDOT = 3509
529151 TA = 200
06926
MA = 200
11732
Ha = 228
904 n
mi
Hp = 219
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17120437
83 X = 5243138
31
Y = -1203829
21 feet Y = -308434
10 meter
Z = -14260182
38 Z = -4321093
80
XDOT = 10943
519793 XDOT = 3252
042895
YDOT = 19436
459955 feet/sec YDOT = 5961
066737 meter/sec
ZDOT = 11514
203252 ZDOT = 3525
529460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12771226
13 X = 3892669
72
Y = 11597588
89 feet Y = 3534945
09 meter
Z = -14152848
23 Z = -4313788
14
XDOT = -5676
749045 XDOT = -1730
273109
YDOT = 20363
247117 feet/sec YDOT = 6206
717721 meter/sec
ZDOT = 11580
742356 ZDOT = 3529
810270
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 14035
50968427
00016717 00000-0 10270-3 0 9045
2 25544 51
6477 37
2782 0003844 96
3097 263
8491 15
50010118 30743
Satellite: ISS
Catalog Number: 25544
Epoch time: 14035
50968427 = yrday
fracday
Element set: 904
Inclination: 51
6477 deg
RA of node: 37
2782 deg
Eccentricity:
0003844
Arg of perigee: 96
3097 deg
Mean anomaly: 263
8491 deg
Mean motion: 15
50010118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 312
Coasting Arc #6 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2014/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5381949
21 A = 6794139
38 meter
Y = 466438
51 meter E =
0014195
Z = 4109467
94 I = 51
83544
XDOT = -3434
893787 Wp = 82
77844
YDOT = -5677
197920 meter/sec RA = 31
76355 deg
ZDOT = -3841
009727 TA = 46
86324
MA = 46
74462
Ha = 228
889 n
mi
Hp = 219
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17657313
69 X = -5406727
27
Y = 1530310
09 feet Y = 406115
77 meter
Z = 13482506
36 Z = 4083263
29
XDOT = -11269
336571 XDOT = -3352
496632
YDOT = -18625
977428 feet/sec YDOT = -5715
148575 meter/sec
ZDOT = -12601
737950 ZDOT = -3857
495350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13575157
48 X = -4137708
00
Y = -11524344
69 feet Y = -3512620
26 meter
Z = 13371803
62 Z = 4075725
74
XDOT = 4514
636969 XDOT = 1376
061348
YDOT = -20069
872835 feet/sec YDOT = -6117
297240 meter/sec
ZDOT = -12670
358606 ZDOT = -3861
925303
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 14036
54123047
00016717 00000-0 10270-3 0 9052
2 25544 51
6471 32
1669 0003779 99
5962 260
5616 15
50068279 30900
Satellite: ISS
Catalog Number: 25544
Epoch time: 14036
54123047 = yrday
fracday
Element set: 905
Inclination: 51
6471 deg
RA of node: 32
1669 deg
Eccentricity:
0003779
Arg of perigee: 99
5962 deg
Mean anomaly: 260
5616 deg
Mean motion: 15
50068279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 316
Coasting Arc #7 (Orbit 3104)
---------------------------------------
Vector Time (GMT): 2014/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5547037
12 A = 6794950
18 meter
Y = -620229
79 meter E =
0010077
Z = -3885558
74 I = 51
81123
XDOT = 3494
963544 Wp = 103
28168
YDOT = 5409
752876 meter/sec RA = 26
82156 deg
ZDOT = 4132
666700 TA = 210
09066
MA = 210
14860
Ha = 228
827 n
mi
Hp = 219
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18198940
69 X = 5572434
98
Y = -2034874
64 feet Y = -558057
40 meter
Z = -12747896
12 Z = -3858550
61
XDOT = 11466
415827 XDOT = 3414
135789
YDOT = 17748
533057 feet/sec YDOT = 5448
384004 meter/sec
ZDOT = 13558
617781 ZDOT = 4149
448031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14508090
68 X = 4422066
04
Y = 11302829
94 feet Y = 3445102
56 meter
Z = -12633778
24 Z = -3850775
61
XDOT = -3418
412223 XDOT = -1041
932046
YDOT = 19596
076417 feet/sec YDOT = 5972
884092 meter/sec
ZDOT = 13628
524308 ZDOT = 4153
974209
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 14037
50829194
00016717 00000-0 10270-3 0 9066
2 25544 51
6470 27
3763 0003852 102
3035 257
8547 15
50054969 31056
Satellite: ISS
Catalog Number: 25544
Epoch time: 14037
50829194 = yrday
fracday
Element set: 906
Inclination: 51
6470 deg
RA of node: 27
3763 deg
Eccentricity:
0003852
Arg of perigee: 102
3035 deg
Mean anomaly: 257
8547 deg
Mean motion: 15
50054969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 306
Coasting Arc #8 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2014/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5704328
49 A = 6795672
02 meter
Y = 763726
07 meter E =
0015636
Z = 3599843
53 I = 51
78577
XDOT = -3505
311365 Wp = 91
14189
YDOT = -5174
761911 meter/sec RA = 21
87698 deg
ZDOT = -4440
322979 TA = 46
40904
MA = 46
27937
Ha = 228
764 n
mi
Hp = 219
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18714988
47 X = -5729931
35
Y = 2505662
96 feet Y = 699793
55 meter
Z = 11810510
28 Z = 3572070
85
XDOT = -11500
365370 XDOT = -3425
616109
YDOT = -16977
565326 feet/sec YDOT = -5213
515049 meter/sec
ZDOT = -14567
988777 ZDOT = -4457
157376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15394489
80 X = -4692240
49
Y = -11058815
27 feet Y = -3370726
89 meter
Z = 11693142
52 Z = 3564069
84
XDOT = 2531
584404 XDOT = 771
626926
YDOT = -19059
205203 feet/sec YDOT = -5809
245746 meter/sec
ZDOT = -14638
153197 ZDOT = -4461
709095
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 14038
53980809
00016717 00000-0 10270-3 0 9072
2 25544 51
6467 22
2650 0003716 105
5780 254
5781 15
50109996 31215
Satellite: ISS
Catalog Number: 25544
Epoch time: 14038
53980809 = yrday
fracday
Element set: 907
Inclination: 51
6467 deg
RA of node: 22
2650 deg
Eccentricity:
0003716
Arg of perigee: 105
5780 deg
Mean anomaly: 254
5781 deg
Mean motion: 15
50109996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 311
Coasting Arc #9 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2014/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5850706
70 A = 6796477
87 meter
Y = -962009
40 meter E =
0008292
Z = -3329909
99 I = 51
75937
XDOT = 3482
241962 Wp = 94
63181
YDOT = 4933
843553 meter/sec RA = 16
93157 deg
ZDOT = 4702
424732 TA = 226
79971
MA = 226
86900
Ha = 228
721 n
mi
Hp = 219
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19195231
95 X = 5877204
66
Y = -3156198
80 feet Y = -896434
95 meter
Z = -10924901
55 Z = -3301424
13
XDOT = 11424
678352 XDOT = 3403
969284
YDOT = 16187
150766 feet/sec YDOT = 4972
346644 meter/sec
ZDOT = 15427
902665 ZDOT = 4719
150519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16371329
76 X = 4989981
31
Y = 10630829
57 feet Y = 3240276
85 meter
Z = -10804490
68 Z = -3293208
76
XDOT = -1743
129959 XDOT = -531
306011
YDOT = 18403
332469 feet/sec YDOT = 5609
335736 meter/sec
ZDOT = 15497
645676 ZDOT = 4723
682402
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 14039
50684081
00016717 00000-0 10270-3 0 9084
2 25544 51
6467 17
4739 0003828 108
5178 251
6388 15
50104684 31363
Satellite: ISS
Catalog Number: 25544
Epoch time: 14039
50684081 = yrday
fracday
Element set: 908
Inclination: 51
6467 deg
RA of node: 17
4739 deg
Eccentricity:
0003828
Arg of perigee: 108
5178 deg
Mean anomaly: 251
6388 deg
Mean motion: 15
50104684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 321
Coasting Arc #10 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2014/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5983773
06 A = 6797222
40 meter
Y = 1145764
31 meter E =
0016775
Z = 2995871
46 I = 51
73249
XDOT = -3407
704472 Wp = 100
27914
YDOT = -4734
955201 meter/sec RA = 11
98384 deg
ZDOT = -4974
697681 TA = 45
52426
MA = 45
38722
Ha = 228
636 n
mi
Hp = 219
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19631801
37 X = -6010693
25
Y = 3759069
26 feet Y = 1078699
46 meter
Z = 9828974
60 Z = 2966738
24
XDOT = -11180
132782 XDOT = -3330
338820
YDOT = -15534
629926 feet/sec YDOT = -4772
629839 meter/sec
ZDOT = -16321
186619 ZDOT = -4991
063545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17272496
92 X = -5264657
06
Y = -10178666
27 feet Y = -3102457
48 meter
Z = 9705800
92 Z = 2958328
12
XDOT = 1195
699972 XDOT = 364
449352
YDOT = -17722
877390 feet/sec YDOT = -5401
933028 meter/sec
ZDOT = -16389
442116 ZDOT = -4995
501957
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 14040
53832620
00016717 00000-0 10270-3 0 9094
2 25544 51
6467 12
3624 0003685 111
9534 248
2008 15
50151446 31522
Satellite: ISS
Catalog Number: 25544
Epoch time: 14040
53832620 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 12
3624 deg
Eccentricity:
0003685
Arg of perigee: 111
9534 deg
Mean anomaly: 248
2008 deg
Mean motion: 15
50151446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 280
Coasting Arc #11 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2014/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6094257
18 A = 6797945
50 meter
Y = -1381017
94 meter E =
0007560
Z = -2681056
23 I = 51
70470
XDOT = 3309
822337 Wp = 79
25572
YDOT = 4543
288293 meter/sec RA = 7
03494 deg
ZDOT = 5197
082177 TA = 250
58570
MA = 250
66742
Ha = 228
580 n
mi
Hp = 219
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19994282
08 X = 6122270
54
Y = -4530898
75 feet Y = -1312711
48 meter
Z = -8796116
25 Z = -2651383
72
XDOT = 10858
997169 XDOT = 3233
527038
YDOT = 14905
801487 feet/sec YDOT = 4579
874364 meter/sec
ZDOT = 17050
794545 ZDOT = 5212
975089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18215925
53 X = 5552214
10
Y = 9522200
23 feet Y = 2902366
63 meter
Z = -8670627
44 Z = -2642807
24
XDOT = -758
061968 XDOT = -231
057288
YDOT = 16994
504973 feet/sec YDOT = 5179
925116 meter/sec
ZDOT = 17117
085894 ZDOT = 5217
287780
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 14041
50532921
00016717 00000-0 10270-3 0 9105
2 25544 51
6469 7
5711 0003758 115
2670 244
8871 15
50158019 31675
Satellite: ISS
Catalog Number: 25544
Epoch time: 14041
50532921 = yrday
fracday
Element set: 910
Inclination: 51
6469 deg
RA of node: 7
5711 deg
Eccentricity:
0003758
Arg of perigee: 115
2670 deg
Mean anomaly: 244
8871 deg
Mean motion: 15
50158019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 294
Coasting Arc #12 (Orbit 3182)
---------------------------------------
Vector Time (GMT): 2014/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6186068
78 A = 6798638
30 meter
Y = 1594926
53 meter E =
0017438
Z = 2301142
09 I = 51
67715
XDOT = -3162
132225 Wp = 109
87889
YDOT = -4402
920698 meter/sec RA = 2
08397 deg
ZDOT = -5421
330331 TA = 44
52848
MA = 44
38848
Ha = 228
495 n
mi
Hp = 219
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20295501
23 X = -6214621
80
Y = 5232698
58 feet Y = 1525590
37 meter
Z = 7549678
78 Z = 2271022
32
XDOT = -10374
449558 XDOT = -3086
328282
YDOT = -14445
277882 feet/sec YDOT = -4437
858010 meter/sec
ZDOT = -17786
516833 ZDOT = -5436
506918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19048834
58 X = -5806084
78
Y = -8850875
19 feet Y = -2697746
76 meter
Z = 7422268
12 Z = 2262307
32
XDOT = 577
924394 XDOT = 176
151355
YDOT = -16289
828124 feet/sec YDOT = -4965
139612 meter/sec
ZDOT = -17849
809141 ZDOT = -5440
621826
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 14042
53678325
00016717 00000-0 10270-3 0 9119
2 25544 51
6475 2
4595 0003666 118
9591 241
1927 15
50192647 31831
Satellite: ISS
Catalog Number: 25544
Epoch time: 14042
53678325 = yrday
fracday
Element set: 911
Inclination: 51
6475 deg
RA of node: 2
4595 deg
Eccentricity:
0003666
Arg of perigee: 118
9591 deg
Mean anomaly: 241
1927 deg
Mean motion: 15
50192647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3183
Checksum: 314
Coasting Arc #13 (Orbit 3197)
---------------------------------------
Vector Time (GMT): 2014/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6245565
20 A = 6799202
07 meter
Y = -1853475
48 meter E =
0008298
Z = -1944627
59 I = 51
64844
XDOT = 3004
784760 Wp = 64
83280
YDOT = 4280
266012 meter/sec RA = 357
13165 deg
ZDOT = 5593
004593 TA = 273
77655
MA = 273
87142
Ha = 228
411 n
mi
Hp = 219
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20490699
48 X = 6275273
15
Y = -6080956
32 feet Y = -1783467
56 meter
Z = -6380011
78 Z = -1914216
01
XDOT = 9858
217717 XDOT = 2929
530185
YDOT = 14042
867494 feet/sec YDOT = 4313
446918 meter/sec
ZDOT = 18349
752603 ZDOT = 5607
418083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19871988
55 X = 6056982
11
Y = 7973474
67 feet Y = 2430315
08 meter
Z = -6251329
27 Z = -1905405
16
XDOT = -495
427230 XDOT = -151
006220
YDOT = 15610
159392 feet/sec YDOT = 4757
976583 meter/sec
ZDOT = 18409
846307 ZDOT = 5611
321154
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 14043
50375603
00016717 00000-0 10270-3 0 9121
2 25544 51
6477 357
6681 0003658 122
6078 237
5426 15
50211343 31981
Satellite: ISS
Catalog Number: 25544
Epoch time: 14043
50375603 = yrday
fracday
Element set: 912
Inclination: 51
6477 deg
RA of node: 357
6681 deg
Eccentricity:
0003658
Arg of perigee: 122
6078 deg
Mean anomaly: 237
5426 deg
Mean motion: 15
50211343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 306
Coasting Arc #14 (Orbit 3213)
---------------------------------------
Vector Time (GMT): 2014/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6282228
38 A = 6799746
28 meter
Y = 2081255
86 meter E =
0017456
Z = 1523780
05 I = 51
62068
XDOT = -2803
046850 Wp = 119
59657
YDOT = -4216
521263 meter/sec RA = 352
17741 deg
ZDOT = -5756
035528 TA = 43
77135
MA = 43
63310
Ha = 228
333 n
mi
Hp = 219
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20610985
51 X = -6312436
40
Y = 6828267
25 feet Y = 2010835
15 meter
Z = 4999278
37 Z = 1493189
13
XDOT = -9196
347933 XDOT = -2727
728158
YDOT = -13833
731179 feet/sec YDOT = -4247
445951 meter/sec
ZDOT = -18884
630999 ZDOT = -5769
468797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20548526
42 X = -6263190
85
Y = -7104491
04 feet Y = -2165448
87 meter
Z = 4869806
01 Z = 1484316
87
XDOT = 666
864859 XDOT = 203
260409
YDOT = -15006
844393 feet/sec YDOT = -4574
086171 meter/sec
ZDOT = -18940
600068 ZDOT = -5773
094901
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 14044
53517829
00016717 00000-0 10270-3 0 9134
2 25544 51
6487 352
5566 0003640 126
5141 233
6345 15
50234789 32148
Satellite: ISS
Catalog Number: 25544
Epoch time: 14044
53517829 = yrday
fracday
Element set: 913
Inclination: 51
6487 deg
RA of node: 352
5566 deg
Eccentricity:
0003640
Arg of perigee: 126
5141 deg
Mean anomaly: 233
6345 deg
Mean motion: 15
50234789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 306
Coasting Arc #15 (Orbit 3228)
---------------------------------------
Vector Time (GMT): 2014/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6279913
61 A = 6800084
85 meter
Y = -2343924
40 meter E =
0010015
Z = -1131223
64 I = 51
59145
XDOT = 2607
836579 Wp = 58
76571
YDOT = 4177
141562 meter/sec RA = 347
22157 deg
ZDOT = 5865
660732 TA = 288
97336
MA = 289
08186
Ha = 228
234 n
mi
Hp = 219
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20603391
10 X = 6311152
15
Y = -7690040
70 feet Y = -2273523
82 meter
Z = -3711363
66 Z = -1100641
39
XDOT = 8555
894287 XDOT = 2532
440217
YDOT = 13704
532684 feet/sec YDOT = 4205
882960 meter/sec
ZDOT = 19244
293740 ZDOT = 5878
145469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21166332
21 X = 6451498
06
Y = 6047074
42 feet Y = 1843148
28 meter
Z = -3581890
95 Z = -1091760
36
XDOT = -900
598896 XDOT = -274
502544
YDOT = 14494
439334 feet/sec YDOT = 4417
905109 meter/sec
ZDOT = 19296
268116 ZDOT = 5881
502522
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 14045
50212073
00016717 00000-0 10270-3 0 9146
2 25544 51
6486 347
7652 0003564 130
1872 229
9591 15
50261369 32297
Satellite: ISS
Catalog Number: 25544
Epoch time: 14045
50212073 = yrday
fracday
Element set: 914
Inclination: 51
6486 deg
RA of node: 347
7652 deg
Eccentricity:
0003564
Arg of perigee: 130
1872 deg
Mean anomaly: 229
9591 deg
Mean motion: 15
50261369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3229
Checksum: 307
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