[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 25th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19116 7 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
There are no maneuvers
Coasting Arc #1 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2013/175/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4308654
42 A = 6788779
79 meter
Y = 100121
97 meter E =
0011876
Z = 5235572
62 I = 51
96498
XDOT = -1626
758112 Wp = 79
86807
YDOT = -7401
025195 meter/sec RA = 70
52971 deg
ZDOT = -1192
891869 TA = 21
54388
MA = 21
49395
Ha = 230
134 n
mi
Hp = 217
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14136005
32 X = -4334886
51
Y = 328484
16 feet Y = 51792
37 meter
Z = 17177075
53 Z = 5214578
07
XDOT = -5337
132912 XDOT = -1538
082657
YDOT = -24281
578725 feet/sec YDOT = -7418
720627 meter/sec
ZDOT = -3913
687235 ZDOT = -1200
580237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12809274
74 X = 3904266
94
Y = 6234425
97 feet Y = 1900253
03 meter
Z = 17089203
76 Z = 5208789
31
XDOT = -5952
582823 XDOT = -1814
347244
YDOT = 23082
256112 feet/sec YDOT = 7035
471663 meter/sec
ZDOT = -3944
737569 ZDOT = -1202
356011
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 13175
71455703
00016717 00000-0 10270-3 0 9006
2 25544 51
6474 71
0334 0008360 91
5026 268
7082 15
50371183 35877
Satellite: ISS
Catalog Number: 25544
Epoch time: 13175
71455703 = yrday
fracday
Element set: 900
Inclination: 51
6474 deg
RA of node: 71
0334 deg
Eccentricity:
0008360
Arg of perigee: 91
5026 deg
Mean anomaly: 268
7082 deg
Mean motion: 15
50371183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 297
Coasting Arc #2 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2013/176/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4457026
55 A = 6789186
08 meter
Y = 87670
61 meter E =
0021715
Z = -5139973
56 I = 51
95433
XDOT = 1817
857557 Wp = 99
78077
YDOT = 7228
860661 meter/sec RA = 65
59001 deg
ZDOT = 1702
160595 TA = 186
62586
MA = 186
65462
Ha = 229
948 n
mi
Hp = 217
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14622790
53 X = 4480683
22
Y = 287633
25 feet Y = 137644
88 meter
Z = -16863430
33 Z = -5118264
54
XDOT = 5964
099595 XDOT = 1728
619239
YDOT = 23716
734451 feet/sec YDOT = 7248
689897 meter/sec
ZDOT = 5584
516387 ZDOT = 1710
775715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13076360
65 X = -3985674
73
Y = -6780334
49 feet Y = -2066645
95 meter
Z = -16772592
96 Z = -5112286
34
XDOT = 4695
750301 XDOT = 1431
264692
YDOT = -22936
295963 feet/sec YDOT = -6990
983009 meter/sec
ZDOT = 5619
467233 ZDOT = 1712
813613
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 13176
68141224
00016717 00000-0 10270-3 0 9014
2 25544 51
6462 66
2395 0008441 95
3752 264
8362 15
50408288 36028
Satellite: ISS
Catalog Number: 25544
Epoch time: 13176
68141224 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 66
2395 deg
Eccentricity:
0008441
Arg of perigee: 95
3752 deg
Mean anomaly: 264
8362 deg
Mean motion: 15
50408288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 306
Coasting Arc #3 (Orbit 3617)
---------------------------------------
Vector Time (GMT): 2013/177/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4613947
38 A = 6789842
96 meter
Y = -278997
73 meter E =
0013903
Z = 4962393
69 I = 51
94301
XDOT = -1975
434442 Wp = 81
02891
YDOT = -7070
015707 meter/sec RA = 60
65092 deg
ZDOT = -2226
797776 TA = 30
64473
MA = 30
56360
Ha = 230
046 n
mi
Hp = 217
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15137622
65 X = -4634590
30
Y = -915346
87 feet Y = -330709
79 meter
Z = 16280819
21 Z = 4939929
67
XDOT = -6481
084128 XDOT = -1885
412141
YDOT = -23195
589589 feet/sec YDOT = -7091
602664 meter/sec
ZDOT = -7305
766980 ZDOT = -2236
176284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13384850
58 X = 4079702
46
Y = 7340451
53 feet Y = 2237369
63 meter
Z = 16186849
59 Z = 4933751
75
XDOT = -3562
756135 XDOT = -1085
928070
YDOT = 22744
982640 feet/sec YDOT = 6932
670709 meter/sec
ZDOT = -7343
933030 ZDOT = -2238
430788
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 13177
71270986
00016717 00000-0 10270-3 0 9028
2 25544 51
6461 61
1272 0008345 99
2877 260
9218 15
50412602 36188
Satellite: ISS
Catalog Number: 25544
Epoch time: 13177
71270986 = yrday
fracday
Element set: 902
Inclination: 51
6461 deg
RA of node: 61
1272 deg
Eccentricity:
0008345
Arg of perigee: 99
2877 deg
Mean anomaly: 260
9218 deg
Mean motion: 15
50412602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3618
Checksum: 310
Coasting Arc #4 (Orbit 3632)
---------------------------------------
Vector Time (GMT): 2013/178/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4821530
38 A = 6790554
74 meter
Y = 423223
61 meter E =
0019440
Z = -4781393
48 I = 51
92962
XDOT = 2088
273885 Wp = 106
15176
YDOT = 6836
952493 meter/sec RA = 55
71011 deg
ZDOT = 2714
885319 TA = 190
63374
MA = 190
67491
Ha = 229
877 n
mi
Hp = 217
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15818669
24 X = 4839665
91
Y = 1388528
90 feet Y = 477242
87 meter
Z = -15686986
49 Z = -4757927
09
XDOT = 6851
292274 XDOT = 1998
478369
YDOT = 22430
946499 feet/sec YDOT = 6859
802556 meter/sec
ZDOT = 8907
104065 ZDOT = 2724
812399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13931462
97 X = -4246309
91
Y = -7819342
76 feet Y = -2383335
67 meter
Z = -15588844
48 Z = -4751479
80
XDOT = 2476
005278 XDOT = 754
686409
YDOT = -22223
835882 feet/sec YDOT = -6773
825177 meter/sec
ZDOT = 8947
596582 ZDOT = 2727
227438
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 13178
67953784
00016717 00000-0 10270-3 0 9039
2 25544 51
6459 56
3332 0008480 103
1439 257
0658 15
50449508 36334
Satellite: ISS
Catalog Number: 25544
Epoch time: 13178
67953784 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 56
3332 deg
Eccentricity:
0008480
Arg of perigee: 103
1439 deg
Mean anomaly: 257
0658 deg
Mean motion: 15
50449508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3633
Checksum: 327
Coasting Arc #5 (Orbit 3648)
---------------------------------------
Vector Time (GMT): 2013/179/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5029827
54 A = 6791524
34 meter
Y = -566233
39 meter E =
0016446
Z = 4514601
51 I = 51
91466
XDOT = -2152
223590 Wp = 86
67624
YDOT = -6622
976794 meter/sec RA = 50
76951 deg
ZDOT = -3217
503582 TA = 35
57852
MA = 35
46898
Ha = 229
959 n
mi
Hp = 217
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16502058
86 X = -5045052
50
Y = -1857721
09 feet Y = -622565
61 meter
Z = 14811684
75 Z = 4490130
23
XDOT = -7061
101016 XDOT = -2062
374439
YDOT = -21728
926490 feet/sec YDOT = -6646
541670 meter/sec
ZDOT = -10556
114113 ZDOT = -3227
741130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14500508
32 X = 4419754
94
Y = 8277983
93 feet Y = 2523129
50 meter
Z = 14709361
64 Z = 4483413
43
XDOT = -1581
046164 XDOT = -481
902871
YDOT = 21665
896521 feet/sec YDOT = 6603
765260 meter/sec
ZDOT = -10597
932044 ZDOT = -3230
249687
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
71080643
00016717 00000-0 10270-3 0 9041
2 25544 51
6457 51
2205 0008393 106
9947 253
2124 15
50453199 36497
Satellite: ISS
Catalog Number: 25544
Epoch time: 13179
71080643 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 51
2205 deg
Eccentricity:
0008393
Arg of perigee: 106
9947 deg
Mean anomaly: 253
2124 deg
Mean motion: 15
50453199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3649
Checksum: 312
Coasting Arc #6 (Orbit 3663)
---------------------------------------
Vector Time (GMT): 2013/180/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5273968
36 A = 6792441
30 meter
Y = 648116
12 meter E =
0016443
Z = -4248200
96 I = 51
89887
XDOT = 2166
360815 Wp = 109
92571
YDOT = 6354
090585 meter/sec RA = 45
82810 deg
ZDOT = 3664
929396 TA = 197
55707
MA = 197
61398
Ha = 229
788 n
mi
Hp = 217
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17303045
81 X = 5286965
52
Y = 2126365
23 feet Y = 707165
99 meter
Z = -13937667
20 Z = -4222549
00
XDOT = 7107
482990 XDOT = 2077
343843
YDOT = 20846
753889 feet/sec YDOT = 6377
818174 meter/sec
ZDOT = 12024
046575 ZDOT = 3675
237642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15274358
15 X = -4655624
36
Y = -8578395
83 feet Y = -2614695
05 meter
Z = -13830419
31 Z = -4215511
81
XDOT = 798
024443 XDOT = 243
237850
YDOT = -20842
076901 feet/sec YDOT = -6352
665039 meter/sec
ZDOT = 12066
193645 ZDOT = 3677
775823
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
67760738
00016717 00000-0 10270-3 0 9059
2 25544 51
6466 46
4270 0008522 110
6669 249
5396 15
50492730 36642
Satellite: ISS
Catalog Number: 25544
Epoch time: 13180
67760738 = yrday
fracday
Element set: 905
Inclination: 51
6466 deg
RA of node: 46
4270 deg
Eccentricity:
0008522
Arg of perigee: 110
6669 deg
Mean anomaly: 249
5396 deg
Mean motion: 15
50492730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3664
Checksum: 325
Coasting Arc #7 (Orbit 3679)
---------------------------------------
Vector Time (GMT): 2013/181/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5507073
03 A = 6793613
52 meter
Y = -727157
26 meter E =
0018957
Z = 3893376
69 I = 51
88030
XDOT = -2118
363843 Wp = 95
30062
YDOT = -6112
798933 meter/sec RA = 40
88615 deg
ZDOT = -4122
516599 TA = 37
85070
MA = 37
71756
Ha = 229
846 n
mi
Hp = 217
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18067824
92 X = -5517445
44
Y = -2385686
54 feet Y = -788799
17 meter
Z = 12773545
57 Z = 3866598
62
XDOT = -6950
012609 XDOT = -2029
825732
YDOT = -20055
114611 feet/sec YDOT = -6135
992404 meter/sec
ZDOT = -13525
316926 ZDOT = -4132
592890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16030642
91 X = 4886139
96
Y = 8831964
42 feet Y = 2691982
75 meter
Z = 12661601
65 Z = 3859256
18
XDOT = -268
590701 XDOT = -81
866446
YDOT = 20010
287999 feet/sec YDOT = 6099
135782 meter/sec
ZDOT = -13566
521736 ZDOT = -4135
075825
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
70884746
00016717 00000-0 10270-3 0 9061
2 25544 51
6462 41
3141 0008447 114
5300 245
6733 15
50494380 36803
Satellite: ISS
Catalog Number: 25544
Epoch time: 13181
70884746 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 41
3141 deg
Eccentricity:
0008447
Arg of perigee: 114
5300 deg
Mean anomaly: 245
6733 deg
Mean motion: 15
50494380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3680
Checksum: 298
Coasting Arc #8 (Orbit 3694)
---------------------------------------
Vector Time (GMT): 2013/182/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5758523
78 A = 6794599
25 meter
Y = 736748
17 meter E =
0013306
Z = -3545379
32 I = 51
86172
XDOT = 2022
984737 Wp = 108
60126
YDOT = 5839
918663 meter/sec RA = 35
94404 deg
ZDOT = 4509
111054 TA = 209
89611
MA = 209
97217
Ha = 229
663 n
mi
Hp = 217
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18892794
54 X = 5767079
80
Y = 2417152
77 feet Y = 801191
81 meter
Z = -11631821
91 Z = -3517384
07
XDOT = 6637
089032 XDOT = 1935
627114
YDOT = 19159
838132 feet/sec YDOT = 5862
052058 meter/sec
ZDOT = 14793
671437 ZDOT = 4518
726931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16935892
42 X = -5162060
01
Y = -8869315
17 feet Y = -2703367
26 meter
Z = -11514790
07 Z = -3509708
01
XDOT = -109
626127 XDOT = -33
414043
YDOT = -19005
992360 feet/sec YDOT = -5793
026471 meter/sec
ZDOT = 14832
983303 ZDOT = 4521
093311
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
67562145
00016717 00000-0 10270-3 0 9075
2 25544 51
6477 36
5213 0008513 117
9604 242
2409 15
50536674 36955
Satellite: ISS
Catalog Number: 25544
Epoch time: 13182
67562145 = yrday
fracday
Element set: 907
Inclination: 51
6477 deg
RA of node: 36
5213 deg
Eccentricity:
0008513
Arg of perigee: 117
9604 deg
Mean anomaly: 242
2409 deg
Mean motion: 15
50536674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3695
Checksum: 314
Coasting Arc #9 (Orbit 3710)
---------------------------------------
Vector Time (GMT): 2013/183/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5984429
77 A = 6795800
82 meter
Y = -746324
61 meter E =
0020931
Z = 3108339
63 I = 51
83968
XDOT = -1856
121822 Wp = 105
57481
YDOT = -5604
993942 meter/sec RA = 31
00056 deg
ZDOT = -4897
420033 TA = 38
78710
MA = 38
63704
Ha = 229
680 n
mi
Hp = 217
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19633955
94 X = -5990738
90
Y = -2448571
55 feet Y = -813281
91 meter
Z = 10197964
67 Z = 3079252
39
XDOT = -6089
638523 XDOT = -1769
517270
YDOT = -18389
087737 feet/sec YDOT = -5625
265473 meter/sec
ZDOT = -16067
651028 ZDOT = -4906
227195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17766197
56 X = 5415137
02
Y = 8849589
80 feet Y = 2697354
97 meter
Z = 10076368
21 Z = 3071277
03
XDOT = 188
527815 XDOT = 57
463278
YDOT = 18040
362896 feet/sec YDOT = 5498
702611 meter/sec
ZDOT = -16103
607614 ZDOT = -4908
379601
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
70683313
00016717 00000-0 10270-3 0 9082
2 25544 51
6471 31
4082 0008443 121
8983 238
2991 15
50538441 37117
Satellite: ISS
Catalog Number: 25544
Epoch time: 13183
70683313 = yrday
fracday
Element set: 908
Inclination: 51
6471 deg
RA of node: 31
4082 deg
Eccentricity:
0008443
Arg of perigee: 121
8983 deg
Mean anomaly: 238
2991 deg
Mean motion: 15
50538441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3711
Checksum: 303
Coasting Arc #10 (Orbit 3725)
---------------------------------------
Vector Time (GMT): 2013/184/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6210695
47 A = 6796702
65 meter
Y = 684799
87 meter E =
0011100
Z = -2686791
98 I = 51
81781
XDOT = 1652
444634 Wp = 99
46437
YDOT = 5362
816695 meter/sec RA = 26
05698 deg
ZDOT = 5203
162257 TA = 230
36680
MA = 230
46481
Ha = 229
496 n
mi
Hp = 217
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20376297
46 X = 6215627
99
Y = 2246718
74 feet Y = 754279
72 meter
Z = -8814934
30 Z = -2656608
92
XDOT = 5421
406280 XDOT = 1567
078110
YDOT = 17594
542963 feet/sec YDOT = 5380
817396 meter/sec
ZDOT = 17070
742313 ZDOT = 5210
983016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18675719
88 X = -5692359
42
Y = -8582977
75 feet Y = -2616091
62 meter
Z = -8688745
01 Z = -2648329
48
XDOT = -112
721708 XDOT = -34
357577
YDOT = -17012
242821 feet/sec YDOT = -5185
331612 meter/sec
ZDOT = 17102
602975 ZDOT = 5212
873387
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
67358017
00016717 00000-0 10270-3 0 9090
2 25544 51
6485 26
6156 0008425 125
0737 235
1205 15
50579223 37266
Satellite: ISS
Catalog Number: 25544
Epoch time: 13184
67358017 = yrday
fracday
Element set: 909
Inclination: 51
6485 deg
RA of node: 26
6156 deg
Eccentricity:
0008425
Arg of perigee: 125
0737 deg
Mean anomaly: 235
1205 deg
Mean motion: 15
50579223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3726
Checksum: 310
Coasting Arc #11 (Orbit 3741)
---------------------------------------
Vector Time (GMT): 2013/185/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6395926
94 A = 6797718
97 meter
Y = -631404
68 meter E =
0021948
Z = 2178408
93 I = 51
79269
XDOT = -1373
569939 Wp = 116
56732
YDOT = -5169
351243 meter/sec RA = 21
11154 deg
ZDOT = -5498
019180 TA = 39
32067
MA = 39
16151
Ha = 229
457 n
mi
Hp = 217
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20984012
26 X = -6398973
16
Y = -2071537
67 feet Y = -702945
31 meter
Z = 7147010
94 Z = 2147330
69
XDOT = -4506
463054 XDOT = -1288
955235
YDOT = -16959
813788 feet/sec YDOT = -5184
237501 meter/sec
ZDOT = -18038
120669 ZDOT = -5504
487032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19442977
67 X = 5926219
59
Y = 8272313
61 feet Y = 2521401
19 meter
Z = 7017068
56 Z = 2138802
50
XDOT = -282
435047 XDOT = -86
086202
YDOT = 16081
118503 feet/sec YDOT = 4901
524920 meter/sec
ZDOT = -18064
345925 ZDOT = -5506
012638
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
70476324
00016717 00000-0 10270-3 0 9109
2 25544 51
6479 21
5023 0008363 129
1008 231
0887 15
50586426 37425
Satellite: ISS
Catalog Number: 25544
Epoch time: 13185
70476324 = yrday
fracday
Element set: 910
Inclination: 51
6479 deg
RA of node: 21
5023 deg
Eccentricity:
0008363
Arg of perigee: 129
1008 deg
Mean anomaly: 231
0887 deg
Mean motion: 15
50586426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3742
Checksum: 298
Coasting Arc #12 (Orbit 3756)
---------------------------------------
Vector Time (GMT): 2013/186/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6565473
28 A = 6798384
00 meter
Y = 511964
80 meter E =
0010975
Z = -1696002
65 I = 51
76747
XDOT = 1075
870171 Wp = 86
36510
YDOT = 4990
646539 meter/sec RA = 16
16544 deg
ZDOT = 5703
921695 TA = 255
12283
MA = 255
24441
Ha = 229
296 n
mi
Hp = 217
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21540266
67 X = 6567499
09
Y = 1679674
53 feet Y = 585395
64 meter
Z = -5564313
16 Z = -1664103
35
XDOT = 3529
757778 XDOT = 992
275767
YDOT = 16373
512267 feet/sec YDOT = 5002
209377 meter/sec
ZDOT = 18713
653856 ZDOT = 5708
945818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20217355
83 X = -6162250
06
Y = -7715545
81 feet Y = -2351698
36 meter
Z = -5430916
30 Z = -1655343
29
XDOT = 796
795434 XDOT = 242
863248
YDOT = -15197
447876 feet/sec YDOT = -4632
182113 meter/sec
ZDOT = 18733
863299 ZDOT = 5710
081533
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
67148336
00016717 00000-0 10270-3 0 9116
2 25544 51
6490 16
7095 0008277 131
9996 228
1861 15
50619317 37575
Satellite: ISS
Catalog Number: 25544
Epoch time: 13186
67148336 = yrday
fracday
Element set: 911
Inclination: 51
6490 deg
RA of node: 16
7095 deg
Eccentricity:
0008277
Arg of perigee: 131
9996 deg
Mean anomaly: 228
1861 deg
Mean motion: 15
50619317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3757
Checksum: 335
Coasting Arc #13 (Orbit 3772)
---------------------------------------
Vector Time (GMT): 2013/187/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6679750
60 A = 6799004
62 meter
Y = -414260
45 meter E =
0021711
Z = 1132457
56 I = 51
73967
XDOT = -706
246170 Wp = 127
51412
YDOT = -4869
788082 meter/sec RA = 11
21747 deg
ZDOT = -5882
825866 TA = 40
21825
MA = 40
05781
Ha = 229
196 n
mi
Hp = 217
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21915192
24 X = -6680122
92
Y = -1359122
20 feet Y = -488959
88 meter
Z = 3715411
95 Z = 1100007
24
XDOT = -2317
080610 XDOT = -623
161726
YDOT = -15976
995019 feet/sec YDOT = -4877
220377 meter/sec
ZDOT = -19300
609796 ZDOT = -5886
055610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20782778
25 X = 6334590
81
Y = 7154653
86 feet Y = 2180738
50 meter
Z = 3579693
64 Z = 1091090
62
XDOT = -1617
419744 XDOT = -492
989538
YDOT = 14470
932774 feet/sec YDOT = 4410
740310 meter/sec
ZDOT = -19313
328649 ZDOT = -5886
702572
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
70263759
00016717 00000-0 10270-3 0 9129
2 25544 51
6488 11
5961 0008238 136
1223 224
0584 15
50636212 37732
Satellite: ISS
Catalog Number: 25544
Epoch time: 13187
70263759 = yrday
fracday
Element set: 912
Inclination: 51
6488 deg
RA of node: 11
5961 deg
Eccentricity:
0008238
Arg of perigee: 136
1223 deg
Mean anomaly: 224
0584 deg
Mean motion: 15
50636212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3773
Checksum: 305
Coasting Arc #14 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2013/188/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6766606
58 A = 6799289
76 meter
Y = 261378
09 meter E =
0012668
Z = -606709
77 I = 51
71153
XDOT = 341
086281 Wp = 80
13670
YDOT = 4780
290506 meter/sec RA = 6
26796 deg
ZDOT = 5972
032793 TA = 273
33503
MA = 273
47994
Ha = 229
074 n
mi
Hp = 217
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22200152
81 X = 6766128
08
Y = 857539
68 feet Y = 337043
97 meter
Z = -1990517
63 Z = -573839
71
XDOT = 1119
049478 XDOT = 258
596503
YDOT = 15683
367803 feet/sec YDOT = 4783
642695 meter/sec
ZDOT = 19593
283442 ZDOT = 5973
490041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21293615
63 X = -6490294
04
Y = -6379073
33 feet Y = -1944341
55 meter
Z = -1853018
21 Z = -564799
95
XDOT = 2487
112506 XDOT = 758
071892
YDOT = -13884
083019 feet/sec YDOT = -4231
868504 meter/sec
ZDOT = 19598
599900 ZDOT = 5973
653249
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
66933077
00016717 00000-0 10270-3 0 9133
2 25544 51
6497 6
8029 0008115 138
7518 221
4247 15
50659271 37886
Satellite: ISS
Catalog Number: 25544
Epoch time: 13188
66933077 = yrday
fracday
Element set: 913
Inclination: 51
6497 deg
RA of node: 6
8029 deg
Eccentricity:
0008115
Arg of perigee: 138
7518 deg
Mean anomaly: 221
4247 deg
Mean motion: 15
50659271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 333
Coasting Arc #15 (Orbit 3803)
---------------------------------------
Vector Time (GMT): 2013/189/16:02:15
734
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6787638
15 A = 6799365
85 meter
Y = -148487
96 meter E =
0020076
Z = 9527
13 I = 51
68137
XDOT = 85
186290 Wp = 137
52498
YDOT = -4753
670694 meter/sec RA = 1
31676 deg
ZDOT = -6016
056506 TA = 42
37255
MA = 42
21767
Ha = 228
924 n
mi
Hp = 217
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22269154
03 X = -6785519
53
Y = -487165
23 feet Y = -224379
77 meter
Z = 31256
98 Z = -23441
03
XDOT = 279
482580 XDOT = 167
560501
YDOT = -15596
032460 feet/sec YDOT = -4752
256733 meter/sec
ZDOT = -19737
718195 ZDOT = -6015
443215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21541795
02 X = 6565939
12
Y = 5665087
54 feet Y = 1726718
68 meter
Z = -106670
39 Z = -32513
13
XDOT = -3613
699718 XDOT = -1101
455674
YDOT = 13503
333714 feet/sec YDOT = 4115
816116 meter/sec
ZDOT = -19734
376472 ZDOT = -6015
037949
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
70045603
00016717 00000-0 10270-3 0 9149
2 25544 51
6496 1
6896 0008103 143
0126 217
1585 15
50683641 38045
Satellite: ISS
Catalog Number: 25544
Epoch time: 13189
70045603 = yrday
fracday
Element set: 914
Inclination: 51
6496 deg
RA of node: 1
6896 deg
Eccentricity:
0008103
Arg of perigee: 143
0126 deg
Mean anomaly: 217
1585 deg
Mean motion: 15
50683641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3804
Checksum: 298
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