[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 28th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19870 18 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
191/05:40:05
466 4
2 4
6 4
7
N/A 0
3 -0
7 228
7
000/00:10:10
932 2
0 -0
1 221
0
Coasting Arc #1 (Orbit 3646)
---------------------------------------
Vector Time (GMT): 2013/179/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4008637
66 A = 6799921
89 meter
Y = 5475811
27 meter E =
0018678
Z = 340368
34 I = 51
94966
XDOT = -4001
471898 Wp = 70
04466
YDOT = 2538
829444 meter/sec RA = 51
54371 deg
ZDOT = 6020
719598 TA = 293
60249
MA = 293
79850
Ha = 229
753 n
mi
Hp = 217
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13151698
37 X = 3945454
62
Y = 17965260
06 feet Y = 5520285
08 meter
Z = 1116694
02 Z = 359688
78
XDOT = -13128
188641 XDOT = -4058
811010
YDOT = 8329
492926 feet/sec YDOT = 2493
761340 meter/sec
ZDOT = 19753
017053 ZDOT = 6001
141919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14699231
82 X = 4480325
86
Y = -16717213
66 feet Y = -5095406
72 meter
Z = 1196702
09 Z = 364754
80
XDOT = 9779
250284 XDOT = 2980
715487
YDOT = 10064
226234 feet/sec YDOT = 3067
576156 meter/sec
ZDOT = 19670
692545 ZDOT = 5995
627088
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 13179
58190444
00016717 00000-0 10270-3 0 9003
2 25544 51
6495 51
8664 0008231 104
6164 255
5900 15
50472712 36478
Satellite: ISS
Catalog Number: 25544
Epoch time: 13179
58190444 = yrday
fracday
Element set: 900
Inclination: 51
6495 deg
RA of node: 51
8664 deg
Eccentricity:
0008231
Arg of perigee: 104
6164 deg
Mean anomaly: 255
5900 deg
Mean motion: 15
50472712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3647
Checksum: 305
Coasting Arc #2 (Orbit 3661)
---------------------------------------
Vector Time (GMT): 2013/180/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110648
05 A = 6799731
80 meter
Y = -5339493
67 meter E =
0017507
Z = -869247
01 I = 51
92875
XDOT = 4236
138529 Wp = 126
13431
YDOT = -2307
236560 meter/sec RA = 46
60969 deg
ZDOT = -5953
543925 TA = 63
21842
MA = 63
03944
Ha = 229
739 n
mi
Hp = 217
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13486378
13 X = -4046412
62
Y = -17518023
87 feet Y = -5385102
31 meter
Z = -2851860
28 Z = -889060
48
XDOT = 13898
092288 XDOT = 4290
544256
YDOT = -7569
673752 feet/sec YDOT = -2259
560690 meter/sec
ZDOT = -19532
624426 ZDOT = -5932
833296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13899245
02 X = -4236489
88
Y = 17178463
80 feet Y = 5235995
77 meter
Z = -2933944
72 Z = -894266
35
XDOT = -9375
617201 XDOT = -2857
688123
YDOT = -10856
103768 feet/sec YDOT = -3308
940429 meter/sec
ZDOT = -19445
594128 ZDOT = -5927
017090
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 13180
54871876
00016717 00000-0 10270-3 0 9017
2 25544 51
6493 47
0735 0008188 108
9180 251
2859 15
50440158 36620
Satellite: ISS
Catalog Number: 25544
Epoch time: 13180
54871876 = yrday
fracday
Element set: 901
Inclination: 51
6493 deg
RA of node: 47
0735 deg
Eccentricity:
0008188
Arg of perigee: 108
9180 deg
Mean anomaly: 251
2859 deg
Mean motion: 15
50440158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3662
Checksum: 321
Coasting Arc #3 (Orbit 3677)
---------------------------------------
Vector Time (GMT): 2013/181/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4222999
32 A = 6799070
86 meter
Y = 5152645
98 meter E =
0019811
Z = 1327920
22 I = 51
90507
XDOT = -4475
358060 Wp = 78
39640
YDOT = 2145
038256 meter/sec RA = 41
67268 deg
ZDOT = 5839
346522 TA = 295
98579
MA = 296
18972
Ha = 229
564 n
mi
Hp = 217
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13854984
64 X = 4158616
79
Y = 16905006
49 feet Y = 5199510
12 meter
Z = 4356693
63 Z = 1348279
19
XDOT = -14682
933269 XDOT = -4527
377618
YDOT = 7037
527088 feet/sec YDOT = 2094
700605 meter/sec
ZDOT = 19157
961030 ZDOT = 5817
479521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12918515
70 X = 3937563
59
Y = -17609922
64 feet Y = -5367504
42 meter
Z = 4441080
93 Z = 1353641
47
XDOT = 9226
757512 XDOT = 2812
315690
YDOT = 11633
622148 feet/sec YDOT = 3545
928031 meter/sec
ZDOT = 19066
116682 ZDOT = 5811
352365
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 13181
57996931
00016717 00000-0 10270-3 0 9022
2 25544 51
6488 41
9604 0008074 112
1823 248
0185 15
50519728 36780
Satellite: ISS
Catalog Number: 25544
Epoch time: 13181
57996931 = yrday
fracday
Element set: 902
Inclination: 51
6488 deg
RA of node: 41
9604 deg
Eccentricity:
0008074
Arg of perigee: 112
1823 deg
Mean anomaly: 248
0185 deg
Mean motion: 15
50519728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3678
Checksum: 326
Coasting Arc #4 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2013/182/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4241472
55 A = 6798408
08 meter
Y = -4976643
68 meter E =
0014783
Z = -1849706
85 I = 51
87872
XDOT = 4771
129220 Wp = 127
12724
YDOT = -1978
445471 meter/sec RA = 36
73483 deg
ZDOT = -5657
221182 TA = 73
11535
MA = 72
95331
Ha = 229
526 n
mi
Hp = 217
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13915592
36 X = -4176522
04
Y = -16327571
12 feet Y = -5023711
16 meter
Z = -6068592
02 Z = -1870154
26
XDOT = 15653
311090 XDOT = 4820
379260
YDOT = -6490
962830 feet/sec YDOT = -1924
815759 meter/sec
ZDOT = -18560
436948 ZDOT = -5633
924041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12043913
48 X = -3670984
83
Y = 17724031
99 feet Y = 5402284
95 meter
Z = -6153367
90 Z = -1875546
54
XDOT = -9163
683127 XDOT = -2793
090617
YDOT = -12592
039163 feet/sec YDOT = -3838
053537 meter/sec
ZDOT = -18462
633907 ZDOT = -5627
410815
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 13182
54675571
00016717 00000-0 10270-3 0 9035
2 25544 51
6484 37
1674 0008026 115
7214 244
4766 15
50499663 36937
Satellite: ISS
Catalog Number: 25544
Epoch time: 13182
54675571 = yrday
fracday
Element set: 903
Inclination: 51
6484 deg
RA of node: 37
1674 deg
Eccentricity:
0008026
Arg of perigee: 115
7214 deg
Mean anomaly: 244
4766 deg
Mean motion: 15
50499663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 326
Coasting Arc #5 (Orbit 3708)
---------------------------------------
Vector Time (GMT): 2013/183/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4262476
62 A = 6797444
33 meter
Y = 4763106
62 meter E =
0020093
Z = 2294973
66 I = 51
85047
XDOT = -5060
346670 Wp = 89
17695
YDOT = 1888
723199 meter/sec RA = 31
79344 deg
ZDOT = 5437
846979 TA = 296
27222
MA = 296
47855
Ha = 229
373 n
mi
Hp = 217
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13984503
34 X = 4197749
37
Y = 15626990
23 feet Y = 4810410
16 meter
Z = 7529441
13 Z = 2315523
71
XDOT = -16602
187238 XDOT = -5107
506278
YDOT = 6196
598423 feet/sec YDOT = 1831
870910 meter/sec
ZDOT = 17840
705312 ZDOT = 5413
149924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11048451
94 X = 3367568
15
Y = -17787920
66 feet Y = -5421758
22 meter
Z = 7614671
99 Z = 2320952
02
XDOT = 9373
842199 XDOT = 2857
147102
YDOT = 13471
891818 feet/sec YDOT = 4106
232626 meter/sec
ZDOT = 17737
057957 ZDOT = 5406
255265
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 13183
57797732
00016717 00000-0 10270-3 0 9044
2 25544 51
6479 32
0540 0007959 119
8880 240
3062 15
50563310 37098
Satellite: ISS
Catalog Number: 25544
Epoch time: 13183
57797732 = yrday
fracday
Element set: 904
Inclination: 51
6479 deg
RA of node: 32
0540 deg
Eccentricity:
0007959
Arg of perigee: 119
8880 deg
Mean anomaly: 240
3062 deg
Mean motion: 15
50563310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3709
Checksum: 316
Coasting Arc #6 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2013/184/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4182210
19 A = 6796372
61 meter
Y = -4574621
03 meter E =
0012663
Z = -2788125
27 I = 51
81965
XDOT = 5383
618059 Wp = 120
89533
YDOT = -1804
097723 meter/sec RA = 26
85028 deg
ZDOT = -5139
031366 TA = 90
56305
MA = 90
41795
Ha = 229
337 n
mi
Hp = 217
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13721162
03 X = -4117201
00
Y = -15008599
18 feet Y = -4621025
31 meter
Z = -9147392
61 Z = -2808284
74
XDOT = 17662
788908 XDOT = 5428
355755
YDOT = -5918
955783 feet/sec YDOT = -1743
643914 meter/sec
ZDOT = -16860
339126 ZDOT = -5112
769805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10232708
28 X = -3118929
48
Y = 17529495
78 feet Y = 5342990
32 meter
Z = -9231012
24 Z = -2813612
53
XDOT = -9687
260059 XDOT = -2952
676866
YDOT = -14435
009028 feet/sec YDOT = -4399
790752 meter/sec
ZDOT = -16750
157805 ZDOT = -5105
448099
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 13184
54473596
00016717 00000-0 10270-3 0 9052
2 25544 51
6472 27
2607 0007961 122
4981 237
6940 15
50561189 37249
Satellite: ISS
Catalog Number: 25544
Epoch time: 13184
54473596 = yrday
fracday
Element set: 905
Inclination: 51
6472 deg
RA of node: 27
2607 deg
Eccentricity:
0007961
Arg of perigee: 122
4981 deg
Mean anomaly: 237
6940 deg
Mean motion: 15
50561189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 325
Coasting Arc #7 (Orbit 3739)
---------------------------------------
Vector Time (GMT): 2013/185/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4101229
51 A = 6795207
90 meter
Y = 4363691
69 meter E =
0019472
Z = 3199378
98 I = 51
78794
XDOT = -5688
793667 Wp = 101
60939
YDOT = 1796
736908 meter/sec RA = 21
90347 deg
ZDOT = 4813
138451 TA = 295
24095
MA = 295
44265
Ha = 229
194 n
mi
Hp = 217
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13455477
39 X = 4036587
27
Y = 14316573
80 feet Y = 4409192
36 meter
Z = 10496650
20 Z = 3219145
93
XDOT = -18664
021216 XDOT = -5731
843227
YDOT = 5894
806127 feet/sec YDOT = 1732
879861 meter/sec
ZDOT = 15791
136651 ZDOT = 4785
398547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9359598
81 X = 2852805
72
Y = -17224510
65 feet Y = -5250030
84 meter
Z = 10578656
13 Z = 3224374
39
XDOT = 10259
922174 XDOT = 3127
224279
YDOT = 15259
220215 feet/sec YDOT = 4651
010322 meter/sec
ZDOT = 15674
769343 ZDOT = 4777
669696
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 13185
57592846
00016717 00000-0 10270-3 0 9067
2 25544 51
6468 22
1470 0007913 127
4361 232
7511 15
50604097 37404
Satellite: ISS
Catalog Number: 25544
Epoch time: 13185
57592846 = yrday
fracday
Element set: 906
Inclination: 51
6468 deg
RA of node: 22
1470 deg
Eccentricity:
0007913
Arg of perigee: 127
4361 deg
Mean anomaly: 232
7511 deg
Mean motion: 15
50604097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3740
Checksum: 305
Coasting Arc #8 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2013/186/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3918030
47 A = 6793889
75 meter
Y = -4194671
32 meter E =
0012361
Z = -3640978
25 I = 51
75445
XDOT = 6000
340109 Wp = 109
16286
YDOT = -1797
925742 meter/sec RA = 16
95397 deg
ZDOT = -4401
749172 TA = 113
84063
MA = 113
71103
Ha = 229
182 n
mi
Hp = 217
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12854430
69 X = -3853146
76
Y = -13762045
00 feet Y = -4238121
90 meter
Z = -11945466
71 Z = -3659854
60
XDOT = 19686
155214 XDOT = 6041
381340
YDOT = -5898
706503 feet/sec YDOT = -1730
596046 meter/sec
ZDOT = -14441
434291 ZDOT = -4372
500773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8741392
59 X = -2664376
46
Y = 16623521
16 feet Y = 5066849
25 meter
Z = -12023770
02 Z = -3664845
10
XDOT = -10916
291124 XDOT = -3327
285535
YDOT = -16058
894104 feet/sec YDOT = -4894
750923 meter/sec
ZDOT = -14318
753467 ZDOT = -4364
356057
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 13186
54265932
00016717 00000-0 10270-3 0 9079
2 25544 51
6463 17
3532 0007990 129
4284 230
7575 15
50616327 37558
Satellite: ISS
Catalog Number: 25544
Epoch time: 13186
54265932 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 17
3532 deg
Eccentricity:
0007990
Arg of perigee: 129
4284 deg
Mean anomaly: 230
7575 deg
Mean motion: 15
50616327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 321
Coasting Arc #9 (Orbit 3770)
---------------------------------------
Vector Time (GMT): 2013/187/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3735846
38 A = 6792655
24 meter
Y = 4018310
69 meter E =
0017982
Z = 3996223
10 I = 51
72054
XDOT = -6283
808518 Wp = 114
86165
YDOT = 1869
646973 meter/sec RA = 12
00093 deg
ZDOT = 3972
983024 TA = 293
72808
MA = 293
91661
Ha = 229
024 n
mi
Hp = 217
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12256713
84 X = 3671222
69
Y = 13183434
02 feet Y = 4059725
38 meter
Z = 13110968
18 Z = 4014214
97
XDOT = -20616
169678 XDOT = -6323
547806
YDOT = 6134
012377 feet/sec YDOT = 1799
154691 meter/sec
ZDOT = 13034
721206 ZDOT = 3942
360833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8122359
21 X = 2475695
09
Y = -16002960
77 feet Y = -4877702
44 meter
Z = 13185597
47 Z = 4018970
11
XDOT = 11788
099702 XDOT = 3593
012789
YDOT = 16674
759049 feet/sec YDOT = 5082
466558 meter/sec
ZDOT = 12906
279385 ZDOT = 3933
833956
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 13187
57382228
00016717 00000-0 10270-3 0 9082
2 25544 51
6459 12
2393 0007924 134
6503 225
5295 15
50643999 37715
Satellite: ISS
Catalog Number: 25544
Epoch time: 13187
57382228 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 12
2393 deg
Eccentricity:
0007924
Arg of perigee: 134
6503 deg
Mean anomaly: 225
5295 deg
Mean motion: 15
50643999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3771
Checksum: 331
Coasting Arc #10 (Orbit 3785)
---------------------------------------
Vector Time (GMT): 2013/188/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3458323
84 A = 6791317
98 meter
Y = -3900926
50 meter E =
0014093
Z = -4362945
46 I = 51
68644
XDOT = 6543
959274 Wp = 100
71633
YDOT = -1945
638770 meter/sec RA = 7
04489 deg
ZDOT = -3459
586245 TA = 134
16536
MA = 134
04943
Ha = 229
034 n
mi
Hp = 217
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11346206
82 X = -3393252
03
Y = -12798315
28 feet Y = -3939235
21 meter
Z = -14314125
51 Z = -4379587
99
XDOT = 21469
682659 XDOT = 6582
035013
YDOT = -6383
329299 feet/sec YDOT = -1872
246709 meter/sec
ZDOT = -11350
348572 ZDOT = -3427
704413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7821550
48 X = -2384008
59
Y = 15145179
69 feet Y = 4616250
77 meter
Z = -14383127
36 Z = -4383977
22
XDOT = -12684
814862 XDOT = -3866
331570
YDOT = -17165
747410 feet/sec YDOT = -5232
119810 meter/sec
ZDOT = -11216
623518 ZDOT = -3418
826848
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 13188
54052507
00016717 00000-0 10270-3 0 9095
2 25544 51
6463 7
4453 0008044 136
5302 223
6484 15
50663986 37868
Satellite: ISS
Catalog Number: 25544
Epoch time: 13188
54052507 = yrday
fracday
Element set: 909
Inclination: 51
6463 deg
RA of node: 7
4453 deg
Eccentricity:
0008044
Arg of perigee: 136
5302 deg
Mean anomaly: 223
6484 deg
Mean motion: 15
50663986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3786
Checksum: 317
Coasting Arc #11 (Orbit 3801)
---------------------------------------
Vector Time (GMT): 2013/189/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3188162
03 A = 6790185
69 meter
Y = 3789166
81 meter E =
0015705
Z = 4639827
60 I = 51
65182
XDOT = -6769
344564 Wp = 127
80089
YDOT = 2078
921120 meter/sec RA = 2
08522 deg
ZDOT = 2937
426757 TA = 292
87044
MA = 293
03618
Ha = 228
852 n
mi
Hp = 217
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10459849
17 X = 3123015
07
Y = 12431649
64 feet Y = 3824453
99 meter
Z = 15222531
51 Z = 4655157
46
XDOT = -22209
135708 XDOT = -6806
357427
YDOT = 6820
607350 feet/sec YDOT = 2003
014700 meter/sec
ZDOT = 9637
226893 ZDOT = 2904
452700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7559835
17 X = 2304237
76
Y = -14313109
49 feet Y = -4362635
77 meter
Z = 15286059
40 Z = 4659190
90
XDOT = 13729
895357 XDOT = 4184
872105
YDOT = 17452
984929 feet/sec YDOT = 5319
669806 meter/sec
ZDOT = 9498
911127 ZDOT = 2895
268111
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 13189
57165826
00016717 00000-0 10270-3 0 9100
2 25544 51
6459 2
3311 0007940 141
5569 218
6149 15
50683271 38025
Satellite: ISS
Catalog Number: 25544
Epoch time: 13189
57165826 = yrday
fracday
Element set: 910
Inclination: 51
6459 deg
RA of node: 2
3311 deg
Eccentricity:
0007940
Arg of perigee: 141
5569 deg
Mean anomaly: 218
6149 deg
Mean motion: 15
50683271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3802
Checksum: 309
Coasting Arc #12 (Orbit 3816)
---------------------------------------
Vector Time (GMT): 2013/190/12:26:08
222
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2837750
55 A = 6789066
80 meter
Y = -3750660
45 meter E =
0016659
Z = -4909192
56 I = 51
61876
XDOT = 6943
823063 Wp = 99
94531
YDOT = -2204
232253 meter/sec RA = 357
12310 deg
ZDOT = -2339
403864 TA = 147
15063
MA = 147
04697
Ha = 228
858 n
mi
Hp = 217
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9310205
23 X = -2771751
79
Y = -12305316
43 feet Y = -3782024
37 meter
Z = -16106274
80 Z = -4922818
02
XDOT = 22781
571729 XDOT = 6979
319202
YDOT = -7231
733114 feet/sec YDOT = -2126
383294 meter/sec
ZDOT = -7675
209529 ZDOT = -2305
585947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7653934
10 X = -2332919
11
Y = 13330339
14 feet Y = 4063087
37 meter
Z = -16162678
40 Z = -4926384
38
XDOT = -14708
294984 XDOT = -4483
088311
YDOT = -17541
089353 feet/sec YDOT = -5346
524035 meter/sec
ZDOT = -7533
345412 ZDOT = -2296
163681
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 13190
53833255
00016717 00000-0 10270-3 0 9117
2 25544 51
6471 357
5376 0008051 143
7147 216
4551 15
50709329 38177
Satellite: ISS
Catalog Number: 25544
Epoch time: 13190
53833255 = yrday
fracday
Element set: 911
Inclination: 51
6471 deg
RA of node: 357
5376 deg
Eccentricity:
0008051
Arg of perigee: 143
7147 deg
Mean anomaly: 216
4551 deg
Mean motion: 15
50709329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3817
Checksum: 308
Coasting Arc #13 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2013/191/05:45:10
932
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4679054
24 A = 6796500
13 meter
Y = -3392272
08 meter E =
0007948
Z = -3586624
74 I = 51
61686
XDOT = 5511
622261 Wp = 128
59076
YDOT = 2911
085298 meter/sec RA = 353
50254 deg
ZDOT = 4438
869305 TA = 189
13452
MA = 189
14898
Ha = 228
680 n
mi
Hp = 220
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15351227
82 X = 4734062
18
Y = -11129501
58 feet Y = -3339640
00 meter
Z = -11767141
55 Z = -3563761
42
XDOT = 18082
750201 XDOT = 5457
097756
YDOT = 9550
804783 feet/sec YDOT = 2972
414411 meter/sec
ZDOT = 14563
219506 ZDOT = 4465
511720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12324146
38 X = 3756399
82
Y = -14487806
58 feet Y = -4415883
44 meter
Z = -11670925
31 Z = -3557298
04
XDOT = 18694
635465 XDOT = 5698
124890
YDOT = 4086
496036 feet/sec YDOT = 1245
563992 meter/sec
ZDOT = 14674
226731 ZDOT = 4472
704308
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 13191
24721725
00016717 00000-0 10270-3 0 9125
2 25544 51
6512 354
0246 0004601 167
5218 192
6047 15
49838178 38281
Satellite: ISS
Catalog Number: 25544
Epoch time: 13191
24721725 = yrday
fracday
Element set: 912
Inclination: 51
6512 deg
RA of node: 354
0246 deg
Eccentricity:
0004601
Arg of perigee: 167
5218 deg
Mean anomaly: 192
6047 deg
Mean motion: 15
49838178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 310
Coasting Arc #14 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2013/192/05:45:10
932
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4639295
50 A = 6797142
40 meter
Y = 3651420
67 meter E =
0014172
Z = 3351632
73 I = 51
58864
XDOT = -5472
870468 Wp = 109
55208
YDOT = -2663
312630 meter/sec RA = 348
54740 deg
ZDOT = -4662
505948 TA = 31
39379
MA = 31
30926
Ha = 228
659 n
mi
Hp = 220
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15220785
75 X = -4696062
74
Y = 11979726
62 feet Y = 3599223
45 meter
Z = 10996170
36 Z = 3328958
23
XDOT = -17955
611772 XDOT = -5420
033137
YDOT = -8737
902331 feet/sec YDOT = -2724
217891 meter/sec
ZDOT = -15296
935526 ZDOT = -4688
964142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11725440
49 X = -3573914
26
Y = 15485171
52 feet Y = 4719880
28 meter
Z = 10900708
23 Z = 3322535
87
XDOT = -18369
995528 XDOT = -5599
174637
YDOT = -3037
334574 feet/sec YDOT = -925
779578 meter/sec
ZDOT = -15407
211109 ZDOT = -4696
117946
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 13192
27889863
00016717 00000-0 10270-3 0 9138
2 25544 51
6511 348
9154 0004558 170
6766 189
4470 15
49847217 38440
Satellite: ISS
Catalog Number: 25544
Epoch time: 13192
27889863 = yrday
fracday
Element set: 913
Inclination: 51
6511 deg
RA of node: 348
9154 deg
Eccentricity:
0004558
Arg of perigee: 170
6766 deg
Mean anomaly: 189
4470 deg
Mean motion: 15
49847217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 352
Coasting Arc #15 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2013/193/05:45:10
932
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4579928
18 A = 6797664
97 meter
Y = -3936759
71 meter E =
0005602
Z = -3127791
38 I = 51
56138
XDOT = 5397
692689 Wp = 124
00648
YDOT = 2425
998924 meter/sec RA = 343
58966 deg
ZDOT = 4853
414570 TA = 200
03979
MA = 200
06180
Ha = 228
384 n
mi
Hp = 221
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15026011
09 X = 4638803
24
Y = -12915878
32 feet Y = -3885214
65 meter
Z = -10261782
73 Z = -3105400
09
XDOT = 17708
965514 XDOT = 5346
587237
YDOT = 7959
314056 feet/sec YDOT = 2486
073246 meter/sec
ZDOT = 15923
276149 ZDOT = 4879
511744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11011126
66 X = 3356191
40
Y = -16531267
78 feet Y = -5038730
42 meter
Z = -10167466
86 Z = -3099043
90
XDOT = 17905
105716 XDOT = 5457
476222
YDOT = 2072
278483 feet/sec YDOT = 631
630481 meter/sec
ZDOT = 16032
077448 ZDOT = 4886
577206
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 13193
24608490
00016717 00000-0 10270-3 0 9142
2 25544 51
6516 344
1250 0004407 176
4228 183
6955 15
49877881 38590
Satellite: ISS
Catalog Number: 25544
Epoch time: 13193
24608490 = yrday
fracday
Element set: 914
Inclination: 51
6516 deg
RA of node: 344
1250 deg
Eccentricity:
0004407
Arg of perigee: 176
4228 deg
Mean anomaly: 183
6955 deg
Mean motion: 15
49877881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 336
Coasting Arc #16 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2013/194/05:45:10
932
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4500948
16 A = 6798281
15 meter
Y = 4201879
62 meter E =
0014786
Z = 2861047
42 I = 51
53435
XDOT = -5310
996356 Wp = 116
10034
YDOT = -2236
155693 meter/sec RA = 338
63091 deg
ZDOT = -5057
057340 TA = 31
34016
MA = 31
25212
Ha = 228
338 n
mi
Hp = 221
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14766890
30 X = -4561498
00
Y = 13785694
30 feet Y = 4151208
45 meter
Z = 9386638
51 Z = 2839035
65
XDOT = -17424
528726 XDOT = -5261
030927
YDOT = -7336
468808 feet/sec YDOT = -2295
266942 meter/sec
ZDOT = -16591
395472 ZDOT = -5082
736149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10221102
95 X = -3115392
18
Y = 17474791
08 feet Y = 5326316
32 meter
Z = 9293875
95 Z = 2832773
39
XDOT = -17427
072396 XDOT = -5311
771666
YDOT = -1287
569035 feet/sec YDOT = -392
451042 meter/sec
ZDOT = -16698
473895 ZDOT = -5089
694843
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 13194
27773756
00016717 00000-0 10270-3 0 9155
2 25544 51
6516 339
0158 0004373 179
1166 180
9993 15
49893907 38750
Satellite: ISS
Catalog Number: 25544
Epoch time: 13194
27773756 = yrday
fracday
Element set: 915
Inclination: 51
6516 deg
RA of node: 339
0158 deg
Eccentricity:
0004373
Arg of perigee: 179
1166 deg
Mean anomaly: 180
9993 deg
Mean motion: 15
49893907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 359
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