[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 20th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
239/08:38:29
119 -0
0 1
4 1
4
N/A 1
4 -0
2 228
6
000/00:02:58
237 -0
2 -0
0 220
2
Coasting Arc #1 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2014/232/13:58:55
677
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5840154
34 A = 6798413
67 meter
Y = -2371238
52 meter E =
0006513
Z = -2553244
34 I = 51
88852
XDOT = -65
240829 Wp = 87
69972
YDOT = 5527
844624 meter/sec RA = 139
37492 deg
ZDOT = -5294
434804 TA = 120
80075
MA = 120
73663
Ha = 228
603 n
mi
Hp = 220
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19160611
36 X = 5878638
68
Y = -7779653
94 feet Y = -2305714
99 meter
Z = -8376785
90 Z = -2524780
61
XDOT = -214
044714 XDOT = -101
331324
YDOT = 18135
973177 feet/sec YDOT = 5526
913215 meter/sec
ZDOT = -17370
192926 ZDOT = -5294
839443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19505926
26 X = -5945406
33
Y = 7013598
19 feet Y = 2137744
73 meter
Z = -8255353
80 Z = -2516231
84
XDOT = 1334
044188 XDOT = 406
616668
YDOT = -16693
711785 feet/sec YDOT = -5088
243352 meter/sec
ZDOT = -17372
764651 ZDOT = -5295
218666
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 14232
60982345
00016717 00000-0 10270-3 0 9006
2 25544 51
6469 140
2654 0004463 33
7179 326
4255 15
50092404 21327
Satellite: ISS
Catalog Number: 25544
Epoch time: 14232
60982345 = yrday
fracday
Element set: 900
Inclination: 51
6469 deg
RA of node: 140
2654 deg
Eccentricity:
0004463
Arg of perigee: 33
7179 deg
Mean anomaly: 326
4255 deg
Mean motion: 15
50092404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2132
Checksum: 287
Coasting Arc #2 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2014/233/13:58:55
677
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5615076
17 A = 6797599
25 meter
Y = 2516846
45 meter E =
0017039
Z = 2866771
30 I = 51
90913
XDOT = 37
034921 Wp = 69
68667
YDOT = -5735
501439 meter/sec RA = 134
43777 deg
ZDOT = 5089
256565 TA = 322
76444
MA = 322
88247
Ha = 228
738 n
mi
Hp = 219
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18422165
90 X = -5656728
42
Y = 8257370
24 feet Y = 2453822
21 meter
Z = 9405417
65 Z = 2839393
30
XDOT = 121
505646 XDOT = 76
446309
YDOT = -18817
261940 feet/sec YDOT = -5734
866833 meter/sec
ZDOT = 16697
035974 ZDOT = 5089
532307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18661328
44 X = 5687972
91
Y = -7842167
28 feet Y = -2390292
59 meter
Z = 9288566
86 Z = 2831155
18
XDOT = -1009
698852 XDOT = -307
756210
YDOT = 17449
926271 feet/sec YDOT = 5318
737527 meter/sec
ZDOT = 16699
095364 ZDOT = 5089
884267
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 14233
64131297
00016717 00000-0 10270-3 0 9014
2 25544 51
6468 135
1538 0004691 36
7208 323
4263 15
50128932 21488
Satellite: ISS
Catalog Number: 25544
Epoch time: 14233
64131297 = yrday
fracday
Element set: 901
Inclination: 51
6468 deg
RA of node: 135
1538 deg
Eccentricity:
0004691
Arg of perigee: 36
7208 deg
Mean anomaly: 323
4263 deg
Mean motion: 15
50128932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2148
Checksum: 296
Coasting Arc #3 (Orbit 2162)
---------------------------------------
Vector Time (GMT): 2014/234/13:58:55
677
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5402538
82 A = 6796671
52 meter
Y = -2600423
68 meter E =
0007675
Z = -3209930
26 I = 51
92719
XDOT = -1
672261 Wp = 71
19530
YDOT = 5941
900760 meter/sec RA = 129
50222 deg
ZDOT = -4823
485718 TA = 145
64223
MA = 145
59257
Ha = 228
581 n
mi
Hp = 219
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17724864
89 X = 5446808
35
Y = -8531573
74 feet Y = -2539761
58 meter
Z = -10531267
27 Z = -3183578
36
XDOT = -5
486419 XDOT = -44
685320
YDOT = 19494
425064 feet/sec YDOT = 5941
641404 meter/sec
ZDOT = -15825
084375 ZDOT = -4823
598506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17834908
50 X = -5436080
11
Y = 8439889
71 feet Y = 2572478
38 meter
Z = -10418756
01 Z = -3175636
83
XDOT = 622
639496 XDOT = 189
780518
YDOT = -18192
744462 feet/sec YDOT = -5545
148512 meter/sec
ZDOT = -15826
486117 ZDOT = -4823
912969
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 14234
60831811
00016717 00000-0 10270-3 0 9021
2 25544 51
6466 130
3624 0004446 39
2828 320
8645 15
50148542 21634
Satellite: ISS
Catalog Number: 25544
Epoch time: 14234
60831811 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node: 130
3624 deg
Eccentricity:
0004446
Arg of perigee: 39
2828 deg
Mean anomaly: 320
8645 deg
Mean motion: 15
50148542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2163
Checksum: 289
Coasting Arc #4 (Orbit 2178)
---------------------------------------
Vector Time (GMT): 2014/235/13:58:55
677
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5166611
35 A = 6795754
56 meter
Y = 2662585
97 meter E =
0015692
Z = 3504854
30 I = 51
94323
XDOT = -79
807235 Wp = 78
45512
YDOT = -6168
615141 meter/sec RA = 124
56651 deg
ZDOT = 4554
400042 TA = 322
52600
MA = 322
63530
Ha = 228
735 n
mi
Hp = 219
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16950824
65 X = -5213026
15
Y = 8735518
26 feet Y = 2604550
23 meter
Z = 11498865
80 Z = 3479643
23
XDOT = -261
834762 XDOT = -32
945833
YDOT = -20238
238650 feet/sec YDOT = -6169
245363 meter/sec
ZDOT = 14942
257355 ZDOT = 4554
126471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16916766
54 X = 5156230
44
Y = -8940218
10 feet Y = -2724978
48 meter
Z = 11391187
85 Z = 3472034
06
XDOT = -53
139063 XDOT = -16
196786
YDOT = 18997
632829 feet/sec YDOT = 5790
478486 meter/sec
ZDOT = 14942
054182 ZDOT = 4554
338115
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 14235
63977545
00016717 00000-0 10270-3 0 9031
2 25544 51
6463 125
2505 0004621 42
2377 317
9129 15
50174963 21797
Satellite: ISS
Catalog Number: 25544
Epoch time: 14235
63977545 = yrday
fracday
Element set: 903
Inclination: 51
6463 deg
RA of node: 125
2505 deg
Eccentricity:
0004621
Arg of perigee: 42
2377 deg
Mean anomaly: 317
9129 deg
Mean motion: 15
50174963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2179
Checksum: 312
Coasting Arc #5 (Orbit 2193)
---------------------------------------
Vector Time (GMT): 2014/236/13:58:55
677
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4955476
43 A = 6794706
45 meter
Y = -2664016
44 meter E =
0010034
Z = -3821299
60 I = 51
95603
XDOT = 174
808468 Wp = 63
76300
YDOT = 6378
001245 meter/sec RA = 119
63175 deg
ZDOT = -4224
010075 TA = 161
75219
MA = 161
71616
Ha = 228
556 n
mi
Hp = 219
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16258124
77 X = 5003460
09
Y = -8740211
41 feet Y = -2608333
05 meter
Z = -12537072
18 Z = -3797110
31
XDOT = 573
518595 XDOT = 123
993719
YDOT = 20925
200935 feet/sec YDOT = 6379
671676 meter/sec
ZDOT = -13858
300771 ZDOT = -4223
284724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16074483
98 X = -4899502
72
Y = 9214627
21 feet Y = 2808618
37 meter
Z = -12433732
57 Z = -3789801
69
XDOT = -599
556877 XDOT = -182
744936
YDOT = -19723
622481 feet/sec YDOT = -6011
760132 meter/sec
ZDOT = -13856
212042 ZDOT = -4223
373430
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 14236
60675013
00016717 00000-0 10270-3 0 9045
2 25544 51
6454 120
4586 0004436 45
4343 314
7169 15
50206028 21949
Satellite: ISS
Catalog Number: 25544
Epoch time: 14236
60675013 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 120
4586 deg
Eccentricity:
0004436
Arg of perigee: 45
4343 deg
Mean anomaly: 314
7169 deg
Mean motion: 15
50206028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2194
Checksum: 288
Coasting Arc #6 (Orbit 2209)
---------------------------------------
Vector Time (GMT): 2014/237/13:58:55
677
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4731803
67 A = 6793764
85 meter
Y = 2639625
10 meter E =
0013838
Z = 4086051
86 I = 51
96729
XDOT = -313
742175 Wp = 86
99529
YDOT = -6600
711765 meter/sec RA = 114
69657 deg
ZDOT = 3890
163664 TA = 322
86054
MA = 322
95620
Ha = 228
720 n
mi
Hp = 219
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15524290
26 X = -4780817
30
Y = 8660187
34 feet Y = 2586437
28 meter
Z = 13405681
96 Z = 4062946
54
XDOT = -1029
337846 XDOT = -258
805047
YDOT = -21655
878494 feet/sec YDOT = -6603
912755 meter/sec
ZDOT = 12763
004147 ZDOT = 3888
773529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15189744
39 X = 4629834
09
Y = -9376111
02 feet Y = -2857838
64 meter
Z = 13306951
16 Z = 4055958
71
XDOT = 1429
364612 XDOT = 435
670334
YDOT = 20472
336584 feet/sec YDOT = 6239
968191 meter/sec
ZDOT = 12758
126545 ZDOT = 3888
676971
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 14237
63817544
00016717 00000-0 10270-3 0 9057
2 25544 51
6450 115
3464 0004531 48
2900 311
8637 15
50218670 22102
Satellite: ISS
Catalog Number: 25544
Epoch time: 14237
63817544 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 115
3464 deg
Eccentricity:
0004531
Arg of perigee: 48
2900 deg
Mean anomaly: 311
8637 deg
Mean motion: 15
50218670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2210
Checksum: 283
Coasting Arc #7 (Orbit 2224)
---------------------------------------
Vector Time (GMT): 2014/238/13:58:55
677
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4545595
51 A = 6792687
62 meter
Y = -2560117
10 meter E =
0012853
Z = -4363606
70 I = 51
97493
XDOT = 467
717317 Wp = 63
91690
YDOT = 6788
114972 meter/sec RA = 109
76161 deg
ZDOT = -3497
848037 TA = 170
61714
MA = 170
59311
Ha = 228
536 n
mi
Hp = 219
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14913371
09 X = 4595082
21
Y = -8399334
31 feet Y = -2509009
01 meter
Z = -14316294
94 Z = -4341404
69
XDOT = 1534
505632 XDOT = 408
767492
YDOT = 22270
718411 feet/sec YDOT = 6793
015362 meter/sec
ZDOT = -11475
879388 ZDOT = -3495
719766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14438842
60 X = -4400959
22
Y = 9337288
38 feet Y = 2846005
50 meter
Z = -14221414
32 Z = -4334687
08
XDOT = -2338
229956 XDOT = -712
692491
YDOT = -21069
663847 feet/sec YDOT = -6422
033540 meter/sec
ZDOT = -11467
896673 ZDOT = -3495
414906
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 14238
60511990
00016717 00000-0 10270-3 0 9062
2 25544 51
6437 110
5537 0004426 52
4893 307
6659 15
50260985 22255
Satellite: ISS
Catalog Number: 25544
Epoch time: 14238
60511990 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 110
5537 deg
Eccentricity:
0004426
Arg of perigee: 52
4893 deg
Mean anomaly: 307
6659 deg
Mean motion: 15
50260985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2225
Checksum: 311
Coasting Arc #8 (Orbit 2236)
---------------------------------------
Vector Time (GMT): 2014/239/08:39:58
237
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4247159
46 A = 6789531
82 meter
Y = 240285
72 meter E =
0017601
Z = -5306927
23 I = 51
97188
XDOT = -1455
437537 Wp = 77
27535
YDOT = 7463
441469 meter/sec RA = 105
90459 deg
ZDOT = -825
406948 TA = 184
84193
MA = 184
85898
Ha = 228
584 n
mi
Hp = 220
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13934250
19 X = 4269935
95
Y = 788338
97 feet Y = 287907
03 meter
Z = -17411178
58 Z = -5286240
05
XDOT = -4775
057536 XDOT = -1534
777766
YDOT = 24486
356524 feet/sec YDOT = 7446
722127 meter/sec
ZDOT = -2708
028044 ZDOT = -832
670627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2795979
36 X = -852214
51
Y = -13784908
37 feet Y = -4201640
07 meter
Z = -17323185
24 Z = -5280106
86
XDOT = 23887
551407 XDOT = 7280
925669
YDOT = -1395
589177 feet/sec YDOT = -425
375581 meter/sec
ZDOT = -2740
125084 ZDOT = -835
190126
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 14239
37866840
00016717 00000-0 10270-3 0 9075
2 25544 51
6456 106
7202 0003596 50
5442 309
6026 15
50036465 22375
Satellite: ISS
Catalog Number: 25544
Epoch time: 14239
37866840 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 106
7202 deg
Eccentricity:
0003596
Arg of perigee: 50
5442 deg
Mean anomaly: 309
6026 deg
Mean motion: 15
50036465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2237
Checksum: 304
Coasting Arc #9 (Orbit 2252)
---------------------------------------
Vector Time (GMT): 2014/240/08:39:58
237
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4184450
04 A = 6789202
25 meter
Y = -321204
12 meter E =
0005398
Z = 5332105
32 I = 51
97860
XDOT = 1126
273629 Wp = 76
88132
YDOT = -7571
089385 meter/sec RA = 100
97057 deg
ZDOT = 428
608718 TA = 9
05394
MA = 9
04421
Ha = 228
619 n
mi
Hp = 219
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13728510
65 X = -4206448
75
Y = -1053819
30 feet Y = -368119
80 meter
Z = 17493783
87 Z = 5311724
60
XDOT = 3695
123455 XDOT = 1208
769558
YDOT = -24839
532102 feet/sec YDOT = -7558
033360 meter/sec
ZDOT = 1406
196582 ZDOT = 434
281107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2721675
33 X = 829566
64
Y = 13608826
19 feet Y = 4147970
22 meter
Z = 17407106
22 Z = 5305685
98
XDOT = -23920
116786 XDOT = -7290
851596
YDOT = 2956
256264 feet/sec YDOT = 901
066909 meter/sec
ZDOT = 1431
550390 ZDOT = 436
336559
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 14240
41021640
00016717 00000-0 10270-3 0 9084
2 25544 51
6452 101
6094 0003439 52
4930 307
6533 15
50085541 22531
Satellite: ISS
Catalog Number: 25544
Epoch time: 14240
41021640 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 101
6094 deg
Eccentricity:
0003439
Arg of perigee: 52
4930 deg
Mean anomaly: 307
6533 deg
Mean motion: 15
50085541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2253
Checksum: 269
Coasting Arc #10 (Orbit 2267)
---------------------------------------
Vector Time (GMT): 2014/241/08:39:58
237
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4168247
63 A = 6789154
78 meter
Y = 414449
10 meter E =
0017910
Z = -5358246
53 I = 51
98408
XDOT = -787
204668 Wp = 83
44902
YDOT = 7608
058786 meter/sec RA = 96
03613 deg
ZDOT = -21
988402 TA = 186
33058
MA = 186
35324
Ha = 228
541 n
mi
Hp = 220
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13675353
13 X = 4189331
92
Y = 1359741
14 feet Y = 461178
50 meter
Z = -17579548
97 Z = -5337946
67
XDOT = -2582
692479 XDOT = -872
114414
YDOT = 24960
822789 feet/sec YDOT = 7598
780995 meter/sec
ZDOT = -72
140425 ZDOT = -26
019514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2647194
68 X = -806864
94
Y = -13597205
34 feet Y = -4144428
19 meter
Z = -17493229
79 Z = -5331936
44
XDOT = 23663
118909 XDOT = 7212
518644
YDOT = -4482
278797 feet/sec YDOT = -1366
198577 meter/sec
ZDOT = -90
528706 ZDOT = -27
593150
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 14241
37728007
00016717 00000-0 10270-3 0 9092
2 25544 51
6459 96
8175 0003565 55
8814 304
2674 15
50086219 22689
Satellite: ISS
Catalog Number: 25544
Epoch time: 14241
37728007 = yrday
fracday
Element set: 909
Inclination: 51
6459 deg
RA of node: 96
8175 deg
Eccentricity:
0003565
Arg of perigee: 55
8814 deg
Mean anomaly: 304
2674 deg
Mean motion: 15
50086219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2268
Checksum: 325
Coasting Arc #11 (Orbit 2283)
---------------------------------------
Vector Time (GMT): 2014/242/08:39:58
237
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4160237
21 A = 6789043
48 meter
Y = -529686
71 meter E =
0006006
Z = 5334316
47 I = 51
98646
XDOT = 458
469938 Wp = 63
99571
YDOT = -7642
294747 meter/sec RA = 91
10196 deg
ZDOT = -398
393635 TA = 29
80326
MA = 29
76907
Ha = 228
572 n
mi
Hp = 219
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13649072
21 X = -4179917
31
Y = -1737817
30 feet Y = -576318
72 meter
Z = 17501038
29 Z = 5314058
89
XDOT = 1504
166464 XDOT = 545
829030
YDOT = -25073
145496 feet/sec YDOT = -7636
679423 meter/sec
ZDOT = -1307
065730 ZDOT = -395
953568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2512259
36 X = 765736
65
Y = 13638648
26 feet Y = 4157059
99 meter
Z = 17414917
42 Z = 5308066
83
XDOT = -23359
181453 XDOT = -7119
878507
YDOT = 5969
151554 feet/sec YDOT = 1819
397394 meter/sec
ZDOT = -1295
428155 ZDOT = -394
846502
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 14242
40879614
00016717 00000-0 10270-3 0 9100
2 25544 51
6457 91
7063 0003425 57
5822 302
5659 15
50136166 22849
Satellite: ISS
Catalog Number: 25544
Epoch time: 14242
40879614 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 91
7063 deg
Eccentricity:
0003425
Arg of perigee: 57
5822 deg
Mean anomaly: 302
5659 deg
Mean motion: 15
50136166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2284
Checksum: 303
Coasting Arc #12 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2014/243/08:39:58
237
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4201949
14 A = 6789228
40 meter
Y = 641982
26 meter E =
0017452
Z = -5308903
18 I = 51
98744
XDOT = -131
415117 Wp = 89
53086
YDOT = 7604
074613 meter/sec RA = 86
16763 deg
ZDOT = 817
973061 TA = 188
25553
MA = 188
28428
Ha = 228
474 n
mi
Hp = 219
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13785922
38 X = 4220247
01
Y = 2106241
02 feet Y = 689073
07 meter
Z = -17417661
34 Z = -5288446
29
XDOT = -431
151959 XDOT = -220
409317
YDOT = 24947
751355 feet/sec YDOT = 7602
107513 meter/sec
ZDOT = 2683
638652 ZDOT = 817
117906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2440852
00 X = -743971
69
Y = -13840214
94 feet Y = -4218497
51 meter
Z = -17330710
48 Z = -5282400
55
XDOT = 22776
586966 XDOT = 6942
303707
YDOT = -7361
022216 feet/sec YDOT = -2243
639571 meter/sec
ZDOT = 2678
736757 ZDOT = 816
478963
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 14243
37582954
00016717 00000-0 10270-3 0 9116
2 25544 51
6464 86
9144 0003497 60
4684 299
6815 15
50135907 22999
Satellite: ISS
Catalog Number: 25544
Epoch time: 14243
37582954 = yrday
fracday
Element set: 911
Inclination: 51
6464 deg
RA of node: 86
9144 deg
Eccentricity:
0003497
Arg of perigee: 60
4684 deg
Mean anomaly: 299
6815 deg
Mean motion: 15
50135907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 339
Coasting Arc #13 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2014/244/08:39:58
237
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4254992
68 A = 6789362
24 meter
Y = -772645
54 meter E =
0007524
Z = 5229079
10 I = 51
98561
XDOT = -174
292957 Wp = 58
39562
YDOT = -7561
149232 meter/sec RA = 81
23323 deg
ZDOT = -1253
895576 TA = 43
61573
MA = 43
55628
Ha = 228
504 n
mi
Hp = 219
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13959949
73 X = -4271437
74
Y = -2534926
31 feet Y = -820319
23 meter
Z = 17155771
34 Z = 5208369
04
XDOT = -571
827287 XDOT = -83
638465
YDOT = -24806
920054 feet/sec YDOT = -7562
591491 meter/sec
ZDOT = -4113
830630 ZDOT = -1254
521587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2332523
67 X = 710953
22
Y = 14102386
14 feet Y = 4298407
30 meter
Z = 17067764
26 Z = 5202254
55
XDOT = -22158
279488 XDOT = -6753
843588
YDOT = 8666
110746 feet/sec YDOT = 2641
430555 meter/sec
ZDOT = -4115
223920 ZDOT = -1254
320251
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 14244
40731342
00016717 00000-0 10270-3 0 9129
2 25544 51
6466 81
8031 0003389 62
0278 298
1215 15
50188336 23158
Satellite: ISS
Catalog Number: 25544
Epoch time: 14244
40731342 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 81
8031 deg
Eccentricity:
0003389
Arg of perigee: 62
0278 deg
Mean anomaly: 298
1215 deg
Mean motion: 15
50188336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 291
Coasting Arc #14 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2014/245/08:39:58
237
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4356805
23 A = 6789794
63 meter
Y = 884092
57 meter E =
0016201
Z = -5146324
93 I = 51
98159
XDOT = 466
201305 Wp = 95
10860
YDOT = 7449
034641 meter/sec RA = 76
29849 deg
ZDOT = 1677
496623 TA = 191
03525
MA = 191
07083
Ha = 228
394 n
mi
Hp = 219
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14293980
41 X = 4371594
46
Y = 2900566
18 feet Y = 932895
61 meter
Z = -16884268
14 Z = -5125124
33
XDOT = 1529
531839 XDOT = 374
721103
YDOT = 24439
090030 feet/sec YDOT = 7453
736597 meter/sec
ZDOT = 5503
597846 ZDOT = 1679
538778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2349295
69 X = -716065
33
Y = -14499848
96 feet Y = -4419553
96 meter
Z = -16794191
28 Z = -5118869
50
XDOT = 21295
979334 XDOT = 6491
014501
YDOT = -9821
467479 feet/sec YDOT = -2993
583288 meter/sec
ZDOT = 5511
022634 ZDOT = 1679
759699
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 14245
37431625
00016717 00000-0 10270-3 0 9138
2 25544 51
6469 77
0111 0003408 64
6716 295
4788 15
50185551 23302
Satellite: ISS
Catalog Number: 25544
Epoch time: 14245
37431625 = yrday
fracday
Element set: 913
Inclination: 51
6469 deg
RA of node: 77
0111 deg
Eccentricity:
0003408
Arg of perigee: 64
6716 deg
Mean anomaly: 295
4788 deg
Mean motion: 15
50185551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 304
Coasting Arc #15 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2014/246/08:39:58
237
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4470527
62 A = 6790183
87 meter
Y = -1009675
35 meter E =
0009511
Z = 5004567
93 I = 51
97538
XDOT = -724
311365 Wp = 60
09070
YDOT = -7332
140464 meter/sec RA = 71
36352 deg
ZDOT = -2118
660881 TA = 50
48877
MA = 50
40472
Ha = 228
420 n
mi
Hp = 219
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14667085
38 X = -4483215
43
Y = -3312583
16 feet Y = -1059738
40 meter
Z = 16419186
12 Z = 4982820
05
XDOT = -2376
349623 XDOT = -631
976116
YDOT = -24055
578950 feet/sec YDOT = -7339
723999 meter/sec
ZDOT = -6950
987143 ZDOT = -2121
954870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2351271
66 X = 716667
60
Y = 14953039
52 feet Y = 4557686
45 meter
Z = 16326800
18 Z = 4976408
70
XDOT = -20423
212022 XDOT = -6224
995024
YDOT = 10842
404957 feet/sec YDOT = 3304
765031 meter/sec
ZDOT = -6963
747453 ZDOT = -2122
550224
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 14246
40576732
00016717 00000-0 10270-3 0 9143
2 25544 51
6471 71
8997 0003333 66
1046 294
0454 15
50240493 23468
Satellite: ISS
Catalog Number: 25544
Epoch time: 14246
40576732 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 71
8997 deg
Eccentricity:
0003333
Arg of perigee: 66
1046 deg
Mean anomaly: 294
0454 deg
Mean motion: 15
50240493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 305
Coasting Arc #16 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2014/247/08:39:58
237
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4627604
06 A = 6790850
90 meter
Y = 1100219
53 meter E =
0014230
Z = -4859736
57 I = 51
96614
XDOT = 957
594721 Wp = 99
42198
YDOT = 7154
662274 meter/sec RA = 66
42759 deg
ZDOT = 2535
694307 TA = 195
44007
MA = 195
48353
Ha = 228
312 n
mi
Hp = 219
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15182428
00 X = 4638564
07
Y = 3609644
13 feet Y = 1152029
45 meter
Z = -15944017
62 Z = -4837229
92
XDOT = 3141
714965 XDOT = 865
200974
YDOT = 23473
301423 feet/sec YDOT = 7164
854229 meter/sec
ZDOT = 8319
207045 ZDOT = 2540
121389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2530304
68 X = -771236
87
Y = -15497503
11 feet Y = -4723638
95 meter
Z = -15848416
46 Z = -4830597
34
XDOT = 19362
960242 XDOT = 5901
830282
YDOT = -11673
298825 feet/sec YDOT = -3558
021482 meter/sec
ZDOT = 8336
811070 ZDOT = 2541
060014
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 14247
37273893
00016717 00000-0 10270-3 0 9153
2 25544 51
6465 67
1072 0003319 69
0977 291
0529 15
50235159 23612
Satellite: ISS
Catalog Number: 25544
Epoch time: 14247
37273893 = yrday
fracday
Element set: 915
Inclination: 51
6465 deg
RA of node: 67
1072 deg
Eccentricity:
0003319
Arg of perigee: 69
0977 deg
Mean anomaly: 291
0529 deg
Mean motion: 15
50235159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 319
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