[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 15th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3663)
---------------------------------------
Vector Time (GMT): 2014/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6046784
33 A = 6798901
65 meter
Y = 3096433
26 meter E =
0008290
Z = 106821
73 I = 51
49439
XDOT = -2087
333818 Wp = 143
04166
YDOT = 4291
144237 meter/sec RA = 207
83284 deg
ZDOT = -5994
600712 TA = 35
80713
MA = 35
75159
Ha = 224
998 n
mi
Hp = 221
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19838531
28 X = 6011191
01
Y = 10158901
76 feet Y = 3163853
28 meter
Z = 350465
00 Z = 136108
88
XDOT = -6848
208063 XDOT = -2106
043732
YDOT = 14078
557209 feet/sec YDOT = 4267
696835 meter/sec
ZDOT = -19667
325169 ZDOT = -6004
786636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18049471
36 X = 5501478
87
Y = 13072322
01 feet Y = 3984443
75 meter
Z = 473724
13 Z = 144391
12
XDOT = -7845
041487 XDOT = -2391
168645
YDOT = 11567
032070 feet/sec YDOT = 3525
631375 meter/sec
ZDOT = -19710
913960 ZDOT = -6007
886575
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14073
53251938
00016717 00000-0 10270-3 0 9008
2 25544 51
6466 208
7448 0004398 294
9335 65
1359 15
50837761 36643
Satellite: ISS
Catalog Number: 25544
Epoch time: 14073
53251938 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 208
7448 deg
Eccentricity:
0004398
Arg of perigee: 294
9335 deg
Mean anomaly: 65
1359 deg
Mean motion: 15
50837761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3664
Checksum: 335
Coasting Arc #2 (Orbit 3679)
---------------------------------------
Vector Time (GMT): 2014/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6071562
57 A = 6798745
04 meter
Y = -2999842
22 meter E =
0012066
Z = 509078
76 I = 51
52359
XDOT = 2524
670995 Wp = 30
76074
YDOT = -4087
275432 meter/sec RA = 202
86799 deg
ZDOT = 5973
014364 TA = 334
73381
MA = 334
79278
Ha = 225
075 n
mi
Hp = 221
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19919824
71 X = -6040039
33
Y = -9842002
02 feet Y = -3067561
99 meter
Z = 1670205
92 Z = 479661
29
XDOT = 8283
041322 XDOT = 2541
173470
YDOT = -13409
696298 feet/sec YDOT = -4058
949725 meter/sec
ZDOT = 19596
503820 ZDOT = 5985
319474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18407802
63 X = -5610698
24
Y = -12458553
13 feet Y = -3797366
99 meter
Z = 1546371
34 Z = 471333
99
XDOT = 8997
945333 XDOT = 2742
573737
YDOT = -10832
674734 feet/sec YDOT = -3301
799259 meter/sec
ZDOT = 19649
013635 ZDOT = 5989
019356
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14074
56353204
00016717 00000-0 10270-3 0 9012
2 25544 51
6483 203
6309 0004362 299
8172 60
2545 15
50863899 36808
Satellite: ISS
Catalog Number: 25544
Epoch time: 14074
56353204 = yrday
fracday
Element set: 901
Inclination: 51
6483 deg
RA of node: 203
6309 deg
Eccentricity:
0004362
Arg of perigee: 299
8172 deg
Mean anomaly: 60
2545 deg
Mean motion: 15
50863899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3680
Checksum: 314
Coasting Arc #3 (Orbit 3694)
---------------------------------------
Vector Time (GMT): 2014/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6033127
77 A = 6798184
70 meter
Y = 2907963
49 meter E =
0005351
Z = -1149040
26 I = 51
55106
XDOT = -3001
711853 Wp = 156
71906
YDOT = 3918
371099 meter/sec RA = 197
90486 deg
ZDOT = -5858
365444 TA = 35
75004
MA = 35
71423
Ha = 225
160 n
mi
Hp = 221
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19793726
27 X = 6005743
51
Y = 9540562
62 feet Y = 2975276
49 meter
Z = -3769817
13 Z = -1119799
33
XDOT = -9848
136000 XDOT = -3016
846963
YDOT = 12855
548226 feet/sec YDOT = 3884
718449 meter/sec
ZDOT = -19220
359068 ZDOT = -5872
984655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18543054
66 X = 5651923
06
Y = 11827177
21 feet Y = 3604923
61 meter
Z = -3646705
24 Z = -1111515
76
XDOT = -10323
572757 XDOT = -3146
624976
YDOT = 10254
994227 feet/sec YDOT = 3125
722240 meter/sec
ZDOT = -19282
620548 ZDOT = -5877
342743
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14075
53008466
00016717 00000-0 10270-3 0 9028
2 25544 51
6483 198
8366 0004446 304
2175 55
8554 15
50907087 36957
Satellite: ISS
Catalog Number: 25544
Epoch time: 14075
53008466 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 198
8366 deg
Eccentricity:
0004446
Arg of perigee: 304
2175 deg
Mean anomaly: 55
8554 deg
Mean motion: 15
50907087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3695
Checksum: 329
Coasting Arc #4 (Orbit 3710)
---------------------------------------
Vector Time (GMT): 2014/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5929243
94 A = 6797356
12 meter
Y = -2798510
53 meter E =
0012646
Z = 1764265
91 I = 51
57942
XDOT = 3488
540887 Wp = 46
66402
YDOT = -3808
918610 meter/sec RA = 192
94297 deg
ZDOT = 5665
222943 TA = 332
70539
MA = 332
77179
Ha = 225
286 n
mi
Hp = 220
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19452900
08 X = -5906079
92
Y = -9181464
99 feet Y = -2864685
34 meter
Z = 5788273
99 Z = 1735519
25
XDOT = 11445
344116 XDOT = 3503
354003
YDOT = -12496
452134 feet/sec YDOT = -3769
823771 meter/sec
ZDOT = 18586
689444 ZDOT = 5682
206346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18453804
43 X = -5624719
59
Y = -11115682
28 feet Y = -3388059
96 meter
Z = 5667225
64 Z = 1727370
38
XDOT = 11730
457883 XDOT = 3575
443563
YDOT = -9932
156018 feet/sec YDOT = -3027
321154 meter/sec
ZDOT = 18658
925036 ZDOT = 5687
240351
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14076
56105117
00016717 00000-0 10270-3 0 9034
2 25544 51
6493 193
7226 0004443 309
2783 50
7973 15
50940244 37114
Satellite: ISS
Catalog Number: 25544
Epoch time: 14076
56105117 = yrday
fracday
Element set: 903
Inclination: 51
6493 deg
RA of node: 193
7226 deg
Eccentricity:
0004443
Arg of perigee: 309
2783 deg
Mean anomaly: 50
7973 deg
Mean motion: 15
50940244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3711
Checksum: 302
Coasting Arc #5 (Orbit 3725)
---------------------------------------
Vector Time (GMT): 2014/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5757158
80 A = 6796199
69 meter
Y = 2713579
70 meter E =
0001209
Z = -2382319
99 I = 51
60625
XDOT = -3982
418950 Wp = 140
27257
YDOT = 3737
658017 meter/sec RA = 187
98255 deg
ZDOT = -5369
028974 TA = 66
29619
MA = 66
28351
Ha = 225
333 n
mi
Hp = 220
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18888316
29 X = 5737959
63
Y = 8902820
54 feet Y = 2777852
23 meter
Z = -7816010
47 Z = -2354399
52
XDOT = -13065
678969 XDOT = -3997
837227
YDOT = 12262
657535 feet/sec YDOT = 3693
037030 meter/sec
ZDOT = -17614
924455 ZDOT = -5388
413056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18115951
16 X = 5521741
91
Y = 10472114
71 feet Y = 3191900
56 meter
Z = -7698431
82 Z = -2346482
02
XDOT = -13182
320999 XDOT = -4017
971440
YDOT = 9800
393837 feet/sec YDOT = 2987
160041 meter/sec
ZDOT = -17697
296613 ZDOT = -5394
136008
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14077
52756137
00016717 00000-0 10270-3 0 9046
2 25544 51
6493 188
9285 0004520 313
1856 46
8917 15
50969790 37263
Satellite: ISS
Catalog Number: 25544
Epoch time: 14077
52756137 = yrday
fracday
Element set: 904
Inclination: 51
6493 deg
RA of node: 188
9285 deg
Eccentricity:
0004520
Arg of perigee: 313
1856 deg
Mean anomaly: 46
8917 deg
Mean motion: 15
50969790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3726
Checksum: 343
Coasting Arc #6 (Orbit 3741)
---------------------------------------
Vector Time (GMT): 2014/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5513737
20 A = 6794780
31 meter
Y = -2634293
58 meter E =
0011361
Z = 2955766
15 I = 51
63303
XDOT = 4464
038936 Wp = 62
78776
YDOT = -3725
757358 meter/sec RA = 183
02211 deg
ZDOT = 4997
052064 TA = 330
94838
MA = 331
01155
Ha = 225
490 n
mi
Hp = 220
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18089688
97 X = -5498228
37
Y = -8642695
46 feet Y = -2695864
60 meter
Z = 9697395
52 Z = 2929019
11
XDOT = 14645
797035 XDOT = 4481
095227
YDOT = -12223
613379 feet/sec YDOT = -3675
741559 meter/sec
ZDOT = 16394
527770 ZDOT = 5018
779773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17525905
21 X = -5341895
91
Y = -9846199
22 feet Y = -3001121
52 meter
Z = 9584754
52 Z = 2921433
18
XDOT = 14616
075608 XDOT = 4454
979845
YDOT = -9935
735704 feet/sec YDOT = -3028
412242 meter/sec
ZDOT = 16486
806949 ZDOT = 5025
178758
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14078
55848158
00016717 00000-0 10270-3 0 9056
2 25544 51
6495 183
8140 0004546 318
3082 41
7722 15
51018187 37427
Satellite: ISS
Catalog Number: 25544
Epoch time: 14078
55848158 = yrday
fracday
Element set: 905
Inclination: 51
6495 deg
RA of node: 183
8140 deg
Eccentricity:
0004546
Arg of perigee: 318
3082 deg
Mean anomaly: 41
7722 deg
Mean motion: 15
51018187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3742
Checksum: 317
Coasting Arc #7 (Orbit 3756)
---------------------------------------
Vector Time (GMT): 2014/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5208395
18 A = 6793256
09 meter
Y = 2599624
97 meter E =
0004412
Z = -3507531
29 I = 51
65871
XDOT = -4915
008146 Wp = 29
38293
YDOT = 3744
601340 meter/sec RA = 178
06298 deg
ZDOT = -4521
716321 TA = 191
76592
MA = 191
77624
Ha = 225
517 n
mi
Hp = 220
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17087910
69 X = 5195977
05
Y = 8528953
32 feet Y = 2657798
73 meter
Z = -11507648
60 Z = -3482259
97
XDOT = -16125
354809 XDOT = -4934
550649
YDOT = 12285
437467 feet/sec YDOT = 3689
528757 meter/sec
ZDOT = -14835
027299 ZDOT = -4545
640790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16709222
35 X = 5092970
97
Y = 9379743
71 feet Y = 2858945
88 meter
Z = -11401228
43 Z = -3475094
42
XDOT = -15945
442815 XDOT = -4860
170970
YDOT = 10244
408997 feet/sec YDOT = 3122
495862 meter/sec
ZDOT = -14936
600970 ZDOT = -4552
675976
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14079
52494936
00016717 00000-0 10270-3 0 9066
2 25544 51
6492 179
0200 0004630 321
9990 38
0834 15
51029877 37577
Satellite: ISS
Catalog Number: 25544
Epoch time: 14079
52494936 = yrday
fracday
Element set: 906
Inclination: 51
6492 deg
RA of node: 179
0200 deg
Eccentricity:
0004630
Arg of perigee: 321
9990 deg
Mean anomaly: 38
0834 deg
Mean motion: 15
51029877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3757
Checksum: 327
Coasting Arc #8 (Orbit 3772)
---------------------------------------
Vector Time (GMT): 2014/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4835007
48 A = 6791530
83 meter
Y = -2593991
03 meter E =
0008472
Z = 3993764
24 I = 51
68438
XDOT = 5333
406582 Wp = 77
12195
YDOT = -3810
405383 meter/sec RA = 173
10272 deg
ZDOT = 3976
666396 TA = 331
47209
MA = 331
51843
Ha = 225
678 n
mi
Hp = 220
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15862885
44 X = -4825042
07
Y = -8510469
26 feet Y = -2648003
06 meter
Z = 13102901
05 Z = 3970300
80
XDOT = 17498
053092 XDOT = 5356
301530
YDOT = -12501
329998 feet/sec YDOT = -3750
635392 meter/sec
ZDOT = 13046
805760 ZDOT = 4002
631467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15654354
73 X = -4771447
32
Y = -9032140
41 feet Y = -2752996
40 meter
Z = 13004109
16 Z = 3963652
47
XDOT = 17161
396270 XDOT = 5230
793583
YDOT = -10775
827142 feet/sec YDOT = -3284
472113 meter/sec
ZDOT = 13157
024216 ZDOT = 4010
260981
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14080
55582377
00016717 00000-0 10270-3 0 9079
2 25544 51
6490 173
9047 0004686 327
0010 33
0848 15
51090550 37732
Satellite: ISS
Catalog Number: 25544
Epoch time: 14080
55582377 = yrday
fracday
Element set: 907
Inclination: 51
6490 deg
RA of node: 173
9047 deg
Eccentricity:
0004686
Arg of perigee: 327
0010 deg
Mean anomaly: 33
0848 deg
Mean motion: 15
51090550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3773
Checksum: 305
Coasting Arc #9 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2014/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4418420
27 A = 6789994
07 meter
Y = 2648503
31 meter E =
0009502
Z = -4432972
37 I = 51
70923
XDOT = -5685
145205 Wp = 40
15339
YDOT = 3888
192026 meter/sec RA = 168
14381 deg
ZDOT = -3340
374686 TA = 196
05355
MA = 196
08368
Ha = 225
711 n
mi
Hp = 220
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14496129
48 X = 4410009
74
Y = 8689315
34 feet Y = 2697865
51 meter
Z = -14543872
61 Z = -4411528
91
XDOT = -18652
051197 XDOT = -5711
974794
YDOT = 12756
535517 feet/sec YDOT = 3824
466780 meter/sec
ZDOT = -10959
234533 ZDOT = -3368
057907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14447025
09 X = 4403453
25
Y = 8918672
13 feet Y = 2718411
26 meter
Z = -14453613
91 Z = -4405461
52
XDOT = -18132
978530 XDOT = -5526
931856
YDOT = 11405
441222 feet/sec YDOT = 3476
378484 meter/sec
ZDOT = -11076
740221 ZDOT = -3376
190419
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14081
52224928
00016717 00000-0 10270-3 0 9083
2 25544 51
6483 169
1104 0004772 330
8322 29
2562 15
51090224 37883
Satellite: ISS
Catalog Number: 25544
Epoch time: 14081
52224928 = yrday
fracday
Element set: 908
Inclination: 51
6483 deg
RA of node: 169
1104 deg
Eccentricity:
0004772
Arg of perigee: 330
8322 deg
Mean anomaly: 29
2562 deg
Mean motion: 15
51090224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 300
Coasting Arc #10 (Orbit 3803)
---------------------------------------
Vector Time (GMT): 2014/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3945759
59 A = 6788391
87 meter
Y = -2750930
20 meter E =
0004769
Z = 4785759
38 I = 51
73495
XDOT = 5989
332726 Wp = 80
43654
YDOT = -3988
694145 meter/sec RA = 163
18351 deg
ZDOT = 2643
844918 TA = 343
50063
MA = 343
51614
Ha = 225
847 n
mi
Hp = 219
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12945405
47 X = -3937952
47
Y = -9025361
55 feet Y = -2795010
17 meter
Z = 15701310
30 Z = 4766610
64
XDOT = 19650
041751 XDOT = 6020
647119
YDOT = -13086
266880 feet/sec YDOT = -3921
542284 meter/sec
ZDOT = 8674
031884 ZDOT = 2673
016614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13055297
97 X = -3979254
82
Y = -9006834
58 feet Y = -2745283
18 meter
Z = 15620753
65 Z = 4761205
71
XDOT = 18921
286811 XDOT = 5767
208220
YDOT = -12159
437062 feet/sec YDOT = -3706
196417 meter/sec
ZDOT = 8797
859588 ZDOT = 2681
587602
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14082
55307875
00016717 00000-0 10270-3 0 9091
2 25544 51
6486 163
9946 0004844 335
4913 24
6008 15
51156273 38049
Satellite: ISS
Catalog Number: 25544
Epoch time: 14082
55307875 = yrday
fracday
Element set: 909
Inclination: 51
6486 deg
RA of node: 163
9946 deg
Eccentricity:
0004844
Arg of perigee: 335
4913 deg
Mean anomaly: 24
6008 deg
Mean motion: 15
51156273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3804
Checksum: 324
Coasting Arc #11 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2014/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3459588
31 A = 6787264
16 meter
Y = 2919432
87 meter E =
0013347
Z = -5068791
81 I = 51
75975
XDOT = -6200
300005 Wp = 54
54068
YDOT = 4073
583994 meter/sec RA = 158
22469 deg
ZDOT = -1881
588374 TA = 197
19617
MA = 197
24143
Ha = 225
911 n
mi
Hp = 219
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11350355
35 X = 3451307
88
Y = 9578191
84 feet Y = 2958073
49 meter
Z = -16629894
40 Z = -5052006
05
XDOT = -20342
191619 XDOT = -6236
250807
YDOT = 13364
776884 feet/sec YDOT = 4004
047095 meter/sec
ZDOT = -6173
190203 ZDOT = -1911
796081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11629603
17 X = 3544703
05
Y = 9363029
48 feet Y = 2853851
39 meter
Z = -16559339
43 Z = -5047286
66
XDOT = -19369
376970 XDOT = -5903
786101
YDOT = 12890
005665 feet/sec YDOT = 3928
873727 meter/sec
ZDOT = -6301
426442 ZDOT = -1920
674780
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14083
51946255
00016717 00000-0 10270-3 0 9101
2 25544 51
6478 159
1997 0004933 339
7143 20
3811 15
51150976 38199
Satellite: ISS
Catalog Number: 25544
Epoch time: 14083
51946255 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 159
1997 deg
Eccentricity:
0004933
Arg of perigee: 339
7143 deg
Mean anomaly: 20
3811 deg
Mean motion: 15
51150976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3819
Checksum: 324
Coasting Arc #12 (Orbit 3834)
---------------------------------------
Vector Time (GMT): 2014/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2935623
04 A = 6786228
52 meter
Y = -3145743
39 meter E =
0003242
Z = 5245794
55 I = 51
78621
XDOT = 6356
950468 Wp = 34
31543
YDOT = -4147
553931 meter/sec RA = 153
26536 deg
ZDOT = 1072
569718 TA = 45
43996
MA = 45
41349
Ha = 225
990 n
mi
Hp = 219
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9631309
20 X = -2925710
65
Y = -10320680
41 feet Y = -3178515
49 meter
Z = 17210612
03 Z = 5231558
19
XDOT = 20856
136705 XDOT = 6397
646727
YDOT = -13607
460402 feet/sec YDOT = -4076
238786 meter/sec
ZDOT = 3518
929520 ZDOT = 1103
549897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10101178
78 X = -3078839
29
Y = -9964838
55 feet Y = -3037282
79 meter
Z = 17150857
34 Z = 5227581
32
XDOT = 19607
737876 XDOT = 5976
438504
YDOT = -13606
046412 feet/sec YDOT = -4147
122946 meter/sec
ZDOT = 3650
458293 ZDOT = 1112
659688
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14084
55024782
00016717 00000-0 10270-3 0 9119
2 25544 51
6485 154
0838 0004997 343
9617 16
1376 15
51221735 38357
Satellite: ISS
Catalog Number: 25544
Epoch time: 14084
55024782 = yrday
fracday
Element set: 911
Inclination: 51
6485 deg
RA of node: 154
0838 deg
Eccentricity:
0004997
Arg of perigee: 343
9617 deg
Mean anomaly: 16
1376 deg
Mean motion: 15
51221735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3835
Checksum: 320
Coasting Arc #13 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2014/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2434270
99 A = 6785882
08 meter
Y = 3430684
53 meter E =
0014881
Z = -5336885
61 I = 51
81157
XDOT = -6410
019501 Wp = 68
43841
YDOT = 4175
083574 meter/sec RA = 148
30755 deg
ZDOT = -235
103762 TA = 199
29350
MA = 199
34990
Ha = 226
106 n
mi
Hp = 219
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7986453
39 X = 2421652
04
Y = 11255526
66 feet Y = 3457834
95 meter
Z = -17509467
23 Z = -5325091
41
XDOT = -21030
247708 XDOT = -6455
087771
YDOT = 13697
780756 feet/sec YDOT = 4103
150607 meter/sec
ZDOT = -771
337802 ZDOT = -266
352399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8679899
83 X = 2645633
47
Y = 10810043
12 feet Y = 3294901
14 meter
Z = -17460070
66 Z = -5321829
54
XDOT = -19482
623491 XDOT = -5938
303640
YDOT = 14157
882142 feet/sec YDOT = 4315
322477 meter/sec
ZDOT = -904
020470 ZDOT = -275
545439
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14085
51659064
00016717 00000-0 10270-3 0 9124
2 25544 51
6478 149
2883 0005105 348
7412 11
3625 15
51213468 38508
Satellite: ISS
Catalog Number: 25544
Epoch time: 14085
51659064 = yrday
fracday
Element set: 912
Inclination: 51
6478 deg
RA of node: 149
2883 deg
Eccentricity:
0005105
Arg of perigee: 348
7412 deg
Mean anomaly: 11
3625 deg
Mean motion: 15
51213468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3850
Checksum: 306
Coasting Arc #14 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2014/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1915789
40 A = 6785735
16 meter
Y = -3770883
11 meter E =
0006581
Z = 5305089
82 I = 51
83827
XDOT = 6411
826551 Wp = 17
82473
YDOT = -4153
078911 meter/sec RA = 143
35073 deg
ZDOT = -630
256517 TA = 78
21470
MA = 78
14089
Ha = 226
121 n
mi
Hp = 219
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6285398
29 X = -1899250
38
Y = -12371663
75 feet Y = -3792213
53 meter
Z = 17405150
33 Z = 5295823
92
XDOT = 21036
176348 XDOT = 6460
852235
YDOT = -13625
586978 feet/sec YDOT = -4081
103717 meter/sec
ZDOT = -2067
770726 ZDOT = -598
989387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7245286
17 X = -2208363
22
Y = -11891783
18 feet Y = -3624615
51 meter
Z = 17366487
12 Z = 5293305
27
XDOT = 19174
997748 XDOT = 5844
539314
YDOT = -14538
868157 feet/sec YDOT = -4431
447014 meter/sec
ZDOT = -1934
999764 ZDOT = -589
787928
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14086
54733213
00016717 00000-0 10270-3 0 9138
2 25544 51
6482 144
1726 0005149 352
7729 7
3348 15
51291153 38668
Satellite: ISS
Catalog Number: 25544
Epoch time: 14086
54733213 = yrday
fracday
Element set: 913
Inclination: 51
6482 deg
RA of node: 144
1726 deg
Eccentricity:
0005149
Arg of perigee: 352
7729 deg
Mean anomaly: 7
3348 deg
Mean motion: 15
51291153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3866
Checksum: 310
Coasting Arc #15 (Orbit 3880)
---------------------------------------
Vector Time (GMT): 2014/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1455532
34 A = 6786336
11 meter
Y = 4147711
77 meter E =
0013606
Z = -5181292
39 I = 51
86416
XDOT = -6319
313248 Wp = 79
07898
YDOT = 4058
239123 meter/sec RA = 138
39557 deg
ZDOT = 1479
266041 TA = 205
11107
MA = 205
17730
Ha = 226
281 n
mi
Hp = 218
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4775368
55 X = 1434212
45
Y = 13607978
23 feet Y = 4163868
51 meter
Z = -16998990
79 Z = -5174274
04
XDOT = -20732
655014 XDOT = -6371
409495
YDOT = 13314
432819 feet/sec YDOT = 3987
281435 meter/sec
ZDOT = 4853
235044 ZDOT = 1448
440729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6049829
76 X = 1843988
11
Y = 13128958
58 feet Y = 4001706
58 meter
Z = -16969882
46 Z = -5172420
17
XDOT = -18564
763941 XDOT = -5658
540049
YDOT = 14633
868593 feet/sec YDOT = 4460
403147 meter/sec
ZDOT = 4722
333699 ZDOT = 1439
367311
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 14087
51363422
00016717 00000-0 10270-3 0 9148
2 25544 51
6479 139
3763 0005276 357
9827 2
1302 15
51282218 38810
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
51363422 = yrday
fracday
Element set: 914
Inclination: 51
6479 deg
RA of node: 139
3763 deg
Eccentricity:
0005276
Arg of perigee: 357
9827 deg
Mean anomaly: 2
1302 deg
Mean motion: 15
51282218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3881
Checksum: 312
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