[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 27th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 26909 78 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
087/22:41:40
084 -1
4 3
3 3
3
N/A 2
8 -0
2 226
2
000/00:07:20
169 -1
0 -0
1 221
2
087/22:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
2
000/00:00:00
000 0
0 0
0 221
2
Coasting Arc #1 (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 = 3197772
25 A = 6786768
91 meter
Y = 2885997
58 meter E =
0014523
Z = -5257001
10 I = 51
81265
XDOT = -5970
391854 Wp = 66
99280
YDOT = 4667
261607 meter/sec RA = 148
33822 deg
ZDOT = -1066
295601 TA = 192
77796
MA = 192
81481
Ha = 226
085 n
mi
Hp = 219
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10491378
78 X = 3190799
32
Y = 9468496
00 feet Y = 2921717
54 meter
Z = -17247378
93 Z = -5241484
17
XDOT = -19587
899782 XDOT = -6016
958815
YDOT = 15312
538081 feet/sec YDOT = 4600
236365 meter/sec
ZDOT = -3498
345149 ZDOT = -1095
412304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11085091
10 X = 3378735
77
Y = 8893106
57 feet Y = 2710618
88 meter
Z = -17182169
13 Z = -5237125
15
XDOT = -18079
655004 XDOT = -5510
678845
YDOT = 15517
560899 feet/sec YDOT = 4729
752562 meter/sec
ZDOT = -3622
081328 ZDOT = -1104
010389
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
51802249
00016717 00000-0 10270-3 0 9006
2 25544 51
6477 149
3056 0003741 348
7710 11
3357 15
51039994 38507
Satellite: ISS
Catalog Number: 25544
Epoch time: 14085
51802249 = yrday
fracday
Element set: 900
Inclination: 51
6477 deg
RA of node: 149
3056 deg
Eccentricity:
0003741
Arg of perigee: 348
7710 deg
Mean anomaly: 11
3357 deg
Mean motion: 15
51039994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3850
Checksum: 307
Coasting Arc #2 (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 = -2744536
15 A = 6786153
99 meter
Y = -3178100
24 meter E =
0003737
Z = 5329077
65 I = 51
83778
XDOT = 6017
620522 Wp = 32
95693
YDOT = -4740
843923 meter/sec RA = 143
38344 deg
ZDOT = 274
814457 TA = 54
44717
MA = 54
41234
Ha = 226
135 n
mi
Hp = 219
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9004383
69 X = -2734680
69
Y = -10426838
06 feet Y = -3208735
60 meter
Z = 17483850
56 Z = 5315769
54
XDOT = 19742
849481 XDOT = 6068
851514
YDOT = -15553
949880 feet/sec YDOT = -4673
264545 meter/sec
ZDOT = 901
622234 ZDOT = 304
172039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9821745
23 X = -2993667
95
Y = -9761174
03 feet Y = -2975205
84 meter
Z = 17428015
09 Z = 5312059
00
XDOT = 17886
598042 XDOT = 5451
835083
YDOT = -16182
444567 feet/sec YDOT = -4932
409104 meter/sec
ZDOT = 1026
399409 ZDOT = 312
846540
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
54887749
00016717 00000-0 10270-3 0 9019
2 25544 51
6481 144
1907 0003801 353
2566 6
8533 15
51118378 38663
Satellite: ISS
Catalog Number: 25544
Epoch time: 14086
54887749 = yrday
fracday
Element set: 901
Inclination: 51
6481 deg
RA of node: 144
1907 deg
Eccentricity:
0003801
Arg of perigee: 353
2566 deg
Mean anomaly: 6
8533 deg
Mean motion: 15
51118378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3866
Checksum: 326
Coasting Arc #3 (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 = 2328833
73 A = 6786206
87 meter
Y = 3522691
89 meter E =
0014881
Z = -5324620
86 I = 51
86199
XDOT = -5979
270063 Wp = 78
98382
YDOT = 4747
311530 meter/sec RA = 138
42949 deg
ZDOT = 529
616437 TA = 196
04035
MA = 196
08752
Ha = 226
205 n
mi
Hp = 219
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7640530
62 X = 2315134
29
Y = 11557388
09 feet Y = 3548657
03 meter
Z = -17469228
54 Z = -5313341
55
XDOT = -19617
027765 XDOT = -6034
483873
YDOT = 15575
169061 feet/sec YDOT = 4680
138854 meter/sec
ZDOT = 1737
586734 ZDOT = 500
435326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8728087
83 X = 2660321
17
Y = 10835989
94 feet Y = 3302809
73 meter
Z = -17422017
06 Z = -5310230
80
XDOT = -17404
031618 XDOT = -5304
748837
YDOT = 16591
430227 feet/sec YDOT = 5057
067933 meter/sec
ZDOT = 1613
543487 ZDOT = 491
808055
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
51528082
00016717 00000-0 10270-3 0 9020
2 25544 51
6478 139
3950 0003910 358
4763 1
6375 15
51120547 38815
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
51528082 = yrday
fracday
Element set: 902
Inclination: 51
6478 deg
RA of node: 139
3950 deg
Eccentricity:
0003910
Arg of perigee: 358
4763 deg
Mean anomaly: 1
6375 deg
Mean motion: 15
51120547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3881
Checksum: 309
Coasting Arc #4 (Orbit 3887)
---------------------------------------
Vector Time (GMT): 2014/087/22:45:20
169
Vector Time (MET): N/A
Weight (LBS) : 900592
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3769356
30 A = 6788220
71 meter
Y = 2097362
62 meter E =
0012735
Z = -5252365
86 I = 51
87468
XDOT = -4818
941127 Wp = 66
13390
YDOT = 5838
522632 meter/sec RA = 136
22693 deg
ZDOT = -1124
024012 TA = 193
08952
MA = 193
12261
Ha = 226
225 n
mi
Hp = 221
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12366654
54 X = 3771137
21
Y = 6881110
95 feet Y = 2139523
15 meter
Z = -17232171
47 Z = -5234050
90
XDOT = -15810
174300 XDOT = -4878
410515
YDOT = 19155
257978 feet/sec YDOT = 5784
301460 meter/sec
ZDOT = -3687
742822 ZDOT = -1147
578997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10570255
09 X = -3221813
75
Y = -9550225
12 feet Y = -2910908
62 meter
Z = -17155013
07 Z = -5228847
98
XDOT = 19052
690066 XDOT = 5807
259932
YDOT = -14266
085990 feet/sec YDOT = -4348
303010 meter/sec
ZDOT = -3788
150398 ZDOT = -1154
628241
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
96626320
00016717 00000-0 10270-3 0 9034
2 25544 51
6490 137
1574 0003854 322
1148 37
9731 15
50555488 38889
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
96626320 = yrday
fracday
Element set: 903
Inclination: 51
6490 deg
RA of node: 137
1574 deg
Eccentricity:
0003854
Arg of perigee: 322
1148 deg
Mean anomaly: 37
9731 deg
Mean motion: 15
50555488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3888
Checksum: 327
Coasting Arc #5 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2014/088/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3339622
93 A = 6787704
08 meter
Y = -2538699
38 meter E =
0002589
Z = 5335831
33 I = 51
89483
XDOT = 4895
231891 Wp = 6
54919
YDOT = -5890
314794 meter/sec RA = 131
27686 deg
ZDOT = 263
836639 TA = 80
95783
MA = 80
92853
Ha = 226
343 n
mi
Hp = 220
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10956768
13 X = -3336906
22
Y = -8329066
20 feet Y = -2576029
18 meter
Z = 17506008
30 Z = 5319614
87
XDOT = 16060
472084 XDOT = 4959
453258
YDOT = -19325
179771 feet/sec YDOT = -5835
214047 meter/sec
ZDOT = 865
605770 ZDOT = 287
773913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9080372
71 X = 2767697
60
Y = 10457292
41 feet Y = 3187382
73 meter
Z = 17437783
84 Z = 5315036
51
XDOT = -18977
836229 XDOT = -5784
444483
YDOT = 14879
119920 feet/sec YDOT = 4535
155752 meter/sec
ZDOT = 967
648946 ZDOT = 294
939399
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 14088
99747084
00016717 00000-0 10270-3 0 9040
2 25544 51
6487 132
0445 0003843 325
5610 34
5291 15
50587130 39047
Satellite: ISS
Catalog Number: 25544
Epoch time: 14088
99747084 = yrday
fracday
Element set: 904
Inclination: 51
6487 deg
RA of node: 132
0445 deg
Eccentricity:
0003843
Arg of perigee: 325
5610 deg
Mean anomaly: 34
5291 deg
Mean motion: 15
50587130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 311
Coasting Arc #6 (Orbit 3918)
---------------------------------------
Vector Time (GMT): 2014/089/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3145124
09 A = 6787586
53 meter
Y = 2788056
84 meter E =
0013069
Z = -5340649
48 I = 51
91383
XDOT = -4742
602496 Wp = 78
03389
YDOT = 5997
354196 meter/sec RA = 126
33156 deg
ZDOT = 341
293674 TA = 195
19433
MA = 195
23362
Ha = 226
308 n
mi
Hp = 220
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10318648
60 X = 3139656
99
Y = 9147168
11 feet Y = 2823196
28 meter
Z = -17521815
86 Z = -5325384
50
XDOT = -15559
719476 XDOT = -4810
971687
YDOT = 19676
358912 feet/sec YDOT = 5943
937148 meter/sec
ZDOT = 1119
729901 ZDOT = 318
087689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8475538
22 X = -2583344
05
Y = -10979749
21 feet Y = -3346627
56 meter
Z = -17457651
15 Z = -5321092
07
XDOT = 18257
810817 XDOT = 5564
980737
YDOT = -15699
143653 feet/sec YDOT = -4785
098985 meter/sec
ZDOT = 1020
750305 ZDOT = 311
124693
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 14089
96420340
00016717 00000-0 10270-3 0 9052
2 25544 51
6480 127
2504 0003946 329
3255 30
7665 15
50631644 39192
Satellite: ISS
Catalog Number: 25544
Epoch time: 14089
96420340 = yrday
fracday
Element set: 905
Inclination: 51
6480 deg
RA of node: 127
2504 deg
Eccentricity:
0003946
Arg of perigee: 329
3255 deg
Mean anomaly: 30
7665 deg
Mean motion: 15
50631644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3919
Checksum: 308
Coasting Arc #7 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2014/090/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2957305
76 A = 6787722
41 meter
Y = -3083654
21 meter E =
0005439
Z = 5274053
21 I = 51
93229
XDOT = 4586
523756 Wp = 12
61162
YDOT = -6062
603479 meter/sec RA = 121
38766 deg
ZDOT = -967
562642 TA = 86
64796
MA = 86
58574
Ha = 226
382 n
mi
Hp = 220
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9702446
71 X = -2948223
75
Y = -10116975
74 feet Y = -3116673
21 meter
Z = 17303324
16 Z = 5259709
37
XDOT = 15047
650117 XDOT = 4658
676427
YDOT = -19890
431360 feet/sec YDOT = -6010
910728 meter/sec
ZDOT = -3174
418117 ZDOT = -945
105675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7885131
57 X = 2403388
10
Y = 11678866
23 feet Y = 3559718
43 meter
Z = 17243099
52 Z = 5255696
73
XDOT = -17469
422526 XDOT = -5324
679986
YDOT = 16366
055109 feet/sec YDOT = 4988
373597 meter/sec
ZDOT = -3078
580547 ZDOT = -938
351351
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 14090
99535805
00016717 00000-0 10270-3 0 9061
2 25544 51
6479 122
1371 0003944 332
7189 27
3755 15
50671882 39356
Satellite: ISS
Catalog Number: 25544
Epoch time: 14090
99535805 = yrday
fracday
Element set: 906
Inclination: 51
6479 deg
RA of node: 122
1371 deg
Eccentricity:
0003944
Arg of perigee: 332
7189 deg
Mean anomaly: 27
3755 deg
Mean motion: 15
50671882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 331
Coasting Arc #8 (Orbit 3949)
---------------------------------------
Vector Time (GMT): 2014/091/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2823970
10 A = 6788137
20 meter
Y = 3397814
26 meter E =
0011738
Z = -5163428
95 I = 51
94833
XDOT = -4399
682875 Wp = 85
93294
YDOT = 6059
701634 meter/sec RA = 116
44383 deg
ZDOT = 1585
257275 TA = 199
29316
MA = 199
33764
Ha = 226
382 n
mi
Hp = 220
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9264993
76 X = 2810847
65
Y = 11147684
59 feet Y = 3429319
74 meter
Z = -16940383
69 Z = -5149742
62
XDOT = -14434
655103 XDOT = -4474
817586
YDOT = 19880
910873 feet/sec YDOT = 6010
081639 meter/sec
ZDOT = 5200
975312 ZDOT = 1563
700798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7487467
24 X = -2282180
01
Y = -12489599
97 feet Y = -3806830
07 meter
Z = -16882988
71 Z = -5145934
96
XDOT = 16521
975151 XDOT = 5035
898026
YDOT = -16793
519806 feet/sec YDOT = -5118
664837 meter/sec
ZDOT = 5108
928370 ZDOT = 1557
201367
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 14091
96204129
00016717 00000-0 10270-3 0 9072
2 25544 51
6469 117
3422 0003988 336
3467 23
7500 15
50705973 39509
Satellite: ISS
Catalog Number: 25544
Epoch time: 14091
96204129 = yrday
fracday
Element set: 907
Inclination: 51
6469 deg
RA of node: 117
3422 deg
Eccentricity:
0003988
Arg of perigee: 336
3467 deg
Mean anomaly: 23
7500 deg
Mean motion: 15
50705973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3950
Checksum: 315
Coasting Arc #9 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2014/092/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2703551
54 A = 6788777
54 meter
Y = -3748392
81 meter E =
0008180
Z = 4971706
62 I = 51
96428
XDOT = 4225
321094 Wp = 29
15019
YDOT = -5997
176503 meter/sec RA = 111
50217 deg
ZDOT = -2215
380718 TA = 82
42914
MA = 82
33623
Ha = 226
409 n
mi
Hp = 220
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8869919
76 X = -2685586
45
Y = -12297876
66 feet Y = -3778524
73 meter
Z = 16311373
42 Z = 4958617
00
XDOT = 13862
602013 XDOT = 4302
830562
YDOT = -19675
775930 feet/sec YDOT = -5949
493085 meter/sec
ZDOT = -7268
309441 ZDOT = -2194
665640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7143617
74 X = 2177374
69
Y = 13441250
03 feet Y = 4096893
01 meter
Z = 16256557
85 Z = 4954998
83
XDOT = -15569
274958 XDOT = -4745
515007
YDOT = 16992
017533 feet/sec YDOT = 5179
166944 meter/sec
ZDOT = -7179
811367 ZDOT = -2188
406505
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 14092
99314252
00016717 00000-0 10270-3 0 9086
2 25544 51
6472 112
2286 0004006 339
3840 20
7149 15
50755615 39666
Satellite: ISS
Catalog Number: 25544
Epoch time: 14092
99314252 = yrday
fracday
Element set: 908
Inclination: 51
6472 deg
RA of node: 112
2286 deg
Eccentricity:
0004006
Arg of perigee: 339
3840 deg
Mean anomaly: 20
7149 deg
Mean motion: 15
50755615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 306
Coasting Arc #10 (Orbit 3980)
---------------------------------------
Vector Time (GMT): 2014/093/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2645824
11 A = 6789686
42 meter
Y = 4092744
77 meter E =
0009102
Z = -4735211
60 I = 51
97694
XDOT = -4039
672213 Wp = 88
68464
YDOT = 5862
665361 meter/sec RA = 106
56058 deg
ZDOT = 2814
908559 TA = 209
11251
MA = 209
16328
Ha = 226
440 n
mi
Hp = 220
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8680525
28 X = 2622863
81
Y = 13427640
31 feet Y = 4122203
32 meter
Z = -15535471
12 Z = -4722414
54
XDOT = -13253
517758 XDOT = -4118
603667
YDOT = 19234
466406 feet/sec YDOT = 5817
050047 meter/sec
ZDOT = 9235
264301 ZDOT = 2795
092038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7040594
75 X = -2145973
28
Y = -14413299
15 feet Y = -4393173
58 meter
Z = -15481948
83 Z = -4718898
00
XDOT = 14547
729027 XDOT = 4434
147807
YDOT = -16918
063755 feet/sec YDOT = -5156
625833 meter/sec
ZDOT = 9150
568336 ZDOT = 2789
093229
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 14093
95977592
00016717 00000-0 10270-3 0 9096
2 25544 51
6461 107
4332 0003953 343
5230 16
5792 15
50781209 39814
Satellite: ISS
Catalog Number: 25544
Epoch time: 14093
95977592 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 107
4332 deg
Eccentricity:
0003953
Arg of perigee: 343
5230 deg
Mean anomaly: 16
5792 deg
Mean motion: 15
50781209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3981
Checksum: 324
Coasting Arc #11 (Orbit 3996)
---------------------------------------
Vector Time (GMT): 2014/094/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2601700
54 A = 6790755
39 meter
Y = -4458328
20 meter E =
0010570
Z = 4409640
69 I = 51
98957
XDOT = 3886
107593 Wp = 48
60453
YDOT = -5655
094674 meter/sec RA = 101
62159 deg
ZDOT = -3412
628817 TA = 75
86983
MA = 75
75240
Ha = 226
419 n
mi
Hp = 220
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8535762
91 X = -2573073
90
Y = -14627061
01 feet Y = -4487261
71 meter
Z = 14467325
10 Z = 4397071
76
XDOT = 12749
696829 XDOT = 3965
632878
YDOT = -18553
460217 feet/sec YDOT = -5611
193312 meter/sec
ZDOT = -11196
288770 ZDOT = -3393
556973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7008310
19 X = 2136132
94
Y = 15466414
85 feet Y = 4714163
24 meter
Z = 14414827
72 Z = 4393639
49
XDOT = -13607
082891 XDOT = -4147
438865
YDOT = 16561
939049 feet/sec YDOT = 5048
079022 meter/sec
ZDOT = -11114
756958 ZDOT = -3387
777921
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 14094
99082280
00016717 00000-0 10270-3 0 9104
2 25544 51
6466 102
3194 0003997 345
9316 14
1723 15
50838646 39971
Satellite: ISS
Catalog Number: 25544
Epoch time: 14094
99082280 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 102
3194 deg
Eccentricity:
0003997
Arg of perigee: 345
9316 deg
Mean anomaly: 14
1723 deg
Mean motion: 15
50838646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3997
Checksum: 329
Coasting Arc #12 (Orbit 4011)
---------------------------------------
Vector Time (GMT): 2014/095/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2619575
87 A = 6792001
64 meter
Y = 4790858
57 meter E =
0006306
Z = -4043424
40 I = 51
99803
XDOT = -3744
061926 Wp = 74
93681
YDOT = 5381
800390 meter/sec RA = 96
68268 deg
ZDOT = 3957
735933 TA = 236
01789
MA = 236
07782
Ha = 226
476 n
mi
Hp = 219
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8594409
03 X = 2585450
46
Y = 15718039
93 feet Y = 4819961
27 meter
Z = -13265828
10 Z = -4030782
04
XDOT = -12283
667737 XDOT = -3823
189654
YDOT = 17656
825425 feet/sec YDOT = 5339
489730 meter/sec
ZDOT = 12984
697943 ZDOT = 3939
355169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7225936
36 X = -2202465
40
Y = -16434820
19 feet Y = -5009333
19 meter
Z = -13213075
72 Z = -4027345
48
XDOT = 12706
862724 XDOT = 3873
051758
YDOT = -15945
140933 feet/sec YDOT = -4860
078956 meter/sec
ZDOT = 12906
116256 ZDOT = 3933
784235
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 14095
95740525
00016717 00000-0 10270-3 0 9115
2 25544 51
6454 97
5237 0003846 351
1167 8
9915 15
50859603 40126
Satellite: ISS
Catalog Number: 25544
Epoch time: 14095
95740525 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 97
5237 deg
Eccentricity:
0003846
Arg of perigee: 351
1167 deg
Mean anomaly: 8
9915 deg
Mean motion: 15
50859603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4012
Checksum: 315
Coasting Arc #13 (Orbit 4027)
---------------------------------------
Vector Time (GMT): 2014/096/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2644136
70 A = 6793287
44 meter
Y = -5125897
53 meter E =
0012382
Z = 3583501
62 I = 52
00612
XDOT = 3654
805399 Wp = 68
91463
YDOT = -5029
380654 meter/sec RA = 91
74637 deg
ZDOT = -4480
573216 TA = 69
04480
MA = 68
91234
Ha = 226
413 n
mi
Hp = 219
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8674989
16 X = -2604028
77
Y = -16817249
11 feet Y = -5155241
44 meter
Z = 11756895
07 Z = 3570754
55
XDOT = 11990
831362 XDOT = 3732
538666
YDOT = -16500
592697 feet/sec YDOT = -4988
075975 meter/sec
ZDOT = -14700
043359 ZDOT = -4462
629470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7498319
12 X = 2285487
67
Y = 17409686
44 feet Y = 5306472
43 meter
Z = 11703756
43 Z = 3567304
96
XDOT = -11984
697234 XDOT = -3652
935717
YDOT = 15029
599492 feet/sec YDOT = 4581
021925 meter/sec
ZDOT = -14623
352151 ZDOT = -4457
197736
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 14096
98839629
00016717 00000-0 10270-3 0 9124
2 25544 51
6459 92
4095 0003919 352
8410 7
2684 15
50924105 40289
Satellite: ISS
Catalog Number: 25544
Epoch time: 14096
98839629 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 92
4095 deg
Eccentricity:
0003919
Arg of perigee: 352
8410 deg
Mean anomaly: 7
2684 deg
Mean motion: 15
50924105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4028
Checksum: 327
Coasting Arc #14 (Orbit 4042)
---------------------------------------
Vector Time (GMT): 2014/097/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2720144
86 A = 6794610
38 meter
Y = 5402688
75 meter E =
0006586
Z = -3092497
78 I = 52
00963
XDOT = -3598
938444 Wp = 40
51755
YDOT = 4628
140620 meter/sec RA = 86
81002 deg
ZDOT = 4930
639011 TA = 284
20064
MA = 284
27379
Ha = 226
492 n
mi
Hp = 219
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8924359
77 X = 2674550
98
Y = 17725356
78 feet Y = 5432851
96 meter
Z = -10145990
10 Z = -3079394
88
XDOT = -11807
540826 XDOT = -3674
375358
YDOT = 15184
188387 feet/sec YDOT = 4587
473598 meter/sec
ZDOT = 16176
637176 ZDOT = 4912
972247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7984926
90 X = -2433805
72
Y = -18198304
46 feet Y = -5546843
20 meter
Z = -10091394
48 Z = -3075857
04
XDOT = 11410
095089 XDOT = 3477
796983
YDOT = -13915
276949 feet/sec YDOT = -4241
376414 meter/sec
ZDOT = 16101
169972 ZDOT = 4907
636607
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 14097
95492622
00016717 00000-0 10270-3 0 9131
2 25544 51
6448 87
6136 0003698 359
3944
7202 15
50941487 40430
Satellite: ISS
Catalog Number: 25544
Epoch time: 14097
95492622 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 87
6136 deg
Eccentricity:
0003698
Arg of perigee: 359
3944 deg
Mean anomaly:
7202 deg
Mean motion: 15
50941487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4043
Checksum: 325
Coasting Arc #15 (Orbit 4058)
---------------------------------------
Vector Time (GMT): 2014/098/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2787256
99 A = 6795772
49 meter
Y = -5662694
80 meter E =
0013274
Z = 2508525
18 I = 52
01177
XDOT = 3613
609800 Wp = 88
60257
YDOT = -4151
599173 meter/sec RA = 81
87589 deg
ZDOT = -5331
984330 TA = 63
45160
MA = 63
31559
Ha = 226
395 n
mi
Hp = 219
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9144543
92 X = -2735913
92
Y = -18578395
02 feet Y = -5693576
39 meter
Z = 8230069
49 Z = 2495110
31
XDOT = 11855
675197 XDOT = 3685
666432
YDOT = -13620
732196 feet/sec YDOT = -4110
787075 meter/sec
ZDOT = -17493
386910 ZDOT = -5314
254506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8471880
22 X = 2582229
09
Y = 18918857
72 feet Y = 5766467
83 meter
Z = 8174200
70 Z = 2491496
37
XDOT = -11102
277219 XDOT = -3383
974096
YDOT = 12532
358620 feet/sec YDOT = 3819
862907 meter/sec
ZDOT = -17417
719642 ZDOT = -5308
920947
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 14098
98585964
00016717 00000-0 10270-3 0 9148
2 25544 51
6450 82
4987 0003807
6931 359
4225 15
51016189 40593
Satellite: ISS
Catalog Number: 25544
Epoch time: 14098
98585964 = yrday
fracday
Element set: 914
Inclination: 51
6450 deg
RA of node: 82
4987 deg
Eccentricity:
0003807
Arg of perigee:
6931 deg
Mean anomaly: 359
4225 deg
Mean motion: 15
51016189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4059
Checksum: 335
Coasting Arc #16 (Orbit 4073)
---------------------------------------
Vector Time (GMT): 2014/099/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2886037
73 A = 6796843
34 meter
Y = 5844930
87 meter E =
0010284
Z = -1908754
99 I = 52
00972
XDOT = -3678
018735 Wp = 28
96151
YDOT = 3652
265378 meter/sec RA = 76
94145 deg
ZDOT = 5644
111948 TA = 310
14895
MA = 310
23899
Ha = 226
488 n
mi
Hp = 219
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9468627
71 X = 2829736
03
Y = 19176282
39 feet Y = 5876889
40 meter
Z = -6262319
53 Z = -1894872
37
XDOT = -12066
990602 XDOT = -3746
003155
YDOT = 11982
497959 feet/sec YDOT = 3610
755876 meter/sec
ZDOT = 18517
427652 ZDOT = 5626
079120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9094944
06 X = -2772138
95
Y = -19374917
89 feet Y = -5905474
97 meter
Z = -6204507
42 Z = -1891133
86
XDOT = 11023
578106 XDOT = 3359
986607
YDOT = -11057
246247 feet/sec YDOT = -3370
248656 meter/sec
ZDOT = 18440
551365 ZDOT = 5620
680056
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 14099
95233530
00016717 00000-0 10270-3 0 9156
2 25544 51
6445 77
7026 0003547 8
5097 351
6113 15
51027686 40740
Satellite: ISS
Catalog Number: 25544
Epoch time: 14099
95233530 = yrday
fracday
Element set: 915
Inclination: 51
6445 deg
RA of node: 77
7026 deg
Eccentricity:
0003547
Arg of perigee: 8
5097 deg
Mean anomaly: 351
6113 deg
Mean motion: 15
51027686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4074
Checksum: 310
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