[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 16th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 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
176/10:51:32
563 1
4 3
3 3
3
N/A 3
0 -0
0 227
2
000/00:01:05
126 0
5 -0
0 220
9
Coasting Arc #1 (Orbit 1121)
---------------------------------------
Vector Time (GMT): 2014/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2270039
09 A = 6792038
08 meter
Y = 4885549
52 meter E =
0011468
Z = -4148268
24 I = 51
99233
XDOT = -4156
627709 Wp = 107
09020
YDOT = 5168
211989 meter/sec RA = 102
07560 deg
ZDOT = 3817
589451 TA = 202
16660
MA = 202
21622
Ha = 227
794 n
mi
Hp = 218
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7447634
82 X = 2235389
86
Y = 16028705
76 feet Y = 4910741
31 meter
Z = -13609803
93 Z = -4137324
36
XDOT = -13637
230016 XDOT = -4232
655390
YDOT = 16956
076080 feet/sec YDOT = 5121
304354 meter/sec
ZDOT = 12524
899773 ZDOT = 3797
213235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16741995
70 X = 5102960
29
Y = -5773314
52 feet Y = -1759706
27 meter
Z = -13564212
29 Z = -4134371
91
XDOT = 14969
969850 XDOT = 4562
846810
YDOT = 14231
690567 feet/sec YDOT = 4337
819285 meter/sec
ZDOT = 12437
561903 ZDOT = 3790
968868
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 14167
50911759
00016717 00000-0 10270-3 0 9003
2 25544 51
6458 102
9444 0003960 102
9396 257
2197 15
50725128 11228
Satellite: ISS
Catalog Number: 25544
Epoch time: 14167
50911759 = yrday
fracday
Element set: 900
Inclination: 51
6458 deg
RA of node: 102
9444 deg
Eccentricity:
0003960
Arg of perigee: 102
9396 deg
Mean anomaly: 257
2197 deg
Mean motion: 15
50725128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1122
Checksum: 305
Coasting Arc #2 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2014/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2288995
22 A = 6793339
50 meter
Y = -5184663
44 meter E =
0015430
Z = 3732249
86 I = 52
00288
XDOT = 4016
981264 Wp = 90
04852
YDOT = -4896
588087 meter/sec RA = 97
13980 deg
ZDOT = -4323
107600 TA = 45
69093
MA = 45
56451
Ha = 227
809 n
mi
Hp = 218
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7509826
83 X = -2248978
95
Y = -17010050
66 feet Y = -5210037
09 meter
Z = 12244914
23 Z = 3721226
99
XDOT = 13179
072387 XDOT = 4092
437596
YDOT = -16064
921546 feet/sec YDOT = -4851
245288 meter/sec
ZDOT = -14183
423884 ZDOT = -4303
411015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17622522
25 X = -5371344
78
Y = 6025557
93 feet Y = 1836590
06 meter
Z = 12199041
29 Z = 3718267
79
XDOT = -14367
987139 XDOT = -4379
362480
YDOT = -13374
370975 feet/sec YDOT = -4076
508273 meter/sec
ZDOT = -14099
006050 ZDOT = -4297
377044
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 14168
54020268
00016717 00000-0 10270-3 0 9015
2 25544 51
6462 97
8308 0003965 106
6297 253
5290 15
50744641 11381
Satellite: ISS
Catalog Number: 25544
Epoch time: 14168
54020268 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 97
8308 deg
Eccentricity:
0003965
Arg of perigee: 106
6297 deg
Mean anomaly: 253
5290 deg
Mean motion: 15
50744641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 310
Coasting Arc #3 (Orbit 1152)
---------------------------------------
Vector Time (GMT): 2014/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2373918
49 A = 6794564
81 meter
Y = 5445845
75 meter E =
0008355
Z = -3305592
05 I = 52
01005
XDOT = -3888
729729 Wp = 95
89087
YDOT = 4572
744125 meter/sec RA = 92
20488 deg
ZDOT = 4750
203332 TA = 226
01598
MA = 226
08489
Ha = 227
699 n
mi
Hp = 218
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7788446
47 X = 2328902
79
Y = 17866948
01 feet Y = 5472141
02 meter
Z = -10845118
28 Z = -3294168
82
XDOT = -12758
299636 XDOT = -3962
649025
YDOT = 15002
441356 feet/sec YDOT = 4528
844141 meter/sec
ZDOT = 15584
656602 ZDOT = 4731
133362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18390663
43 X = 5605474
21
Y = -6534503
15 feet Y = -1991716
56 meter
Z = -10797596
38 Z = -3291107
38
XDOT = 13551
307322 XDOT = 4130
438472
YDOT = 12573
248214 feet/sec YDOT = 3832
326056 meter/sec
ZDOT = 15502
944747 ZDOT = 4725
297559
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 14169
50683518
00016717 00000-0 10270-3 0 9026
2 25544 51
6461 93
0364 0003921 110
0268 250
1306 15
50760925 11530
Satellite: ISS
Catalog Number: 25544
Epoch time: 14169
50683518 = yrday
fracday
Element set: 902
Inclination: 51
6461 deg
RA of node: 93
0364 deg
Eccentricity:
0003921
Arg of perigee: 110
0268 deg
Mean anomaly: 250
1306 deg
Mean motion: 15
50760925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1153
Checksum: 280
Coasting Arc #4 (Orbit 1168)
---------------------------------------
Vector Time (GMT): 2014/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2453654
95 A = 6795856
02 meter
Y = -5679165
83 meter E =
0017268
Z = 2792434
02 I = 52
01495
XDOT = 3826
855487 Wp = 103
41962
YDOT = -4197
368408 meter/sec RA = 87
27139 deg
ZDOT = -5151
121822 TA = 45
11567
MA = 44
97560
Ha = 227
711 n
mi
Hp = 218
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8050049
03 X = -2403531
58
Y = -18632433
83 feet Y = -5706324
14 meter
Z = 9161528
94 Z = 2780635
83
XDOT = 12555
300153 XDOT = 3898
529451
YDOT = -13770
893728 feet/sec YDOT = -4154
172896 meter/sec
ZDOT = -16900
005977 ZDOT = -5132
357759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19053959
37 X = -5807646
81
Y = 7057912
35 feet Y = 2151251
68 meter
Z = 9112463
90 Z = 2777479
00
XDOT = -12531
723537 XDOT = -3819
669334
YDOT = -12018
555788 feet/sec YDOT = -3663
255804 meter/sec
ZDOT = -16819
649334 ZDOT = -5126
629117
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 14170
53789984
00016717 00000-0 10270-3 0 9036
2 25544 51
6463 87
9224 0003936 113
7057 246
4503 15
50769120 11691
Satellite: ISS
Catalog Number: 25544
Epoch time: 14170
53789984 = yrday
fracday
Element set: 903
Inclination: 51
6463 deg
RA of node: 87
9224 deg
Eccentricity:
0003936
Arg of perigee: 113
7057 deg
Mean anomaly: 246
4503 deg
Mean motion: 15
50769120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1169
Checksum: 321
Coasting Arc #5 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2014/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2586500
72 A = 6796861
50 meter
Y = 5856965
88 meter E =
0007974
Z = -2282947
29 I = 52
01660
XDOT = -3792
570612 Wp = 71
49442
YDOT = 3796
833329 meter/sec RA = 82
33860 deg
ZDOT = 5462
088570 TA = 263
28494
MA = 263
37569
Ha = 227
588 n
mi
Hp = 218
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8485894
77 X = 2531904
41
Y = 19215767
33 feet Y = 5885584
72 meter
Z = -7489984
55 Z = -2270514
54
XDOT = -12442
816968 XDOT = -3861
278915
YDOT = 12456
802261 feet/sec YDOT = 3754
037752 meter/sec
ZDOT = 17920
238090 ZDOT = 5443
498178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19529147
12 X = 5952484
04
Y = -7787206
01 feet Y = -2373540
39 meter
Z = -7438267
82 Z = -2267184
03
XDOT = 11398
300735 XDOT = 3474
202064
YDOT = 11600
959155 feet/sec YDOT = 3535
972350 meter/sec
ZDOT = 17840
680683 ZDOT = 5437
839472
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 14171
50451310
00016717 00000-0 10270-3 0 9044
2 25544 51
6467 83
1278 0003863 117
1295 243
0250 15
50794904 11840
Satellite: ISS
Catalog Number: 25544
Epoch time: 14171
50451310 = yrday
fracday
Element set: 904
Inclination: 51
6467 deg
RA of node: 83
1278 deg
Eccentricity:
0003863
Arg of perigee: 117
1295 deg
Mean anomaly: 243
0250 deg
Mean motion: 15
50794904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1184
Checksum: 288
Coasting Arc #6 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2014/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2695071
01 A = 6797875
03 meter
Y = -5996723
32 meter E =
0017801
Z = 1694020
24 I = 52
01520
XDOT = 3835
390072 Wp = 116
98964
YDOT = -3353
174382 meter/sec RA = 77
40685 deg
ZDOT = -5729
851187 TA = 44
55450
MA = 44
41153
Ha = 227
605 n
mi
Hp = 218
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8842096
48 X = -2636043
02
Y = -19674289
12 feet Y = -6026531
45 meter
Z = 5557809
20 Z = 1681070
73
XDOT = 12583
300761 XDOT = 3900
434878
YDOT = -11001
228289 feet/sec YDOT = -3309
920368 meter/sec
ZDOT = -18798
724367 ZDOT = -5711
061634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19858216
06 X = -6052784
26
Y = 8456211
35 feet Y = 2577453
22 meter
Z = 5503935
87 Z = 1677599
65
XDOT = -10113
522775 XDOT = -3082
601742
YDOT = -11484
200236 feet/sec YDOT = -3500
384232 meter/sec
ZDOT = -18718
392639 ZDOT = -5705
366076
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 14172
53555796
00016717 00000-0 10270-3 0 9052
2 25544 51
6471 78
0136 0003904 121
2495 238
9039 15
50787406 12001
Satellite: ISS
Catalog Number: 25544
Epoch time: 14172
53555796 = yrday
fracday
Element set: 905
Inclination: 51
6471 deg
RA of node: 78
0136 deg
Eccentricity:
0003904
Arg of perigee: 121
2495 deg
Mean anomaly: 238
9039 deg
Mean motion: 15
50787406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 307
Coasting Arc #7 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2014/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2838716
22 A = 6798420
50 meter
Y = 6071543
98 meter E =
0010399
Z = -1125123
39 I = 52
01046
XDOT = -3914
179634 Wp = 59
32672
YDOT = 2915
549686 meter/sec RA = 72
47524 deg
ZDOT = 5903
307954 TA = 288
54744
MA = 288
66040
Ha = 227
453 n
mi
Hp = 218
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9313373
44 X = 2776077
37
Y = 19919763
70 feet Y = 6102938
21 meter
Z = -3691349
69 Z = -1111484
71
XDOT = -12841
796701 XDOT = -3975
167598
YDOT = 9565
451725 feet/sec YDOT = 2871
437171 meter/sec
ZDOT = 19367
808249 ZDOT = 5884
145488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19957330
23 X = 6082994
26
Y = -9255095
30 feet Y = -2820953
05 meter
Z = -3634577
58 Z = -1107819
25
XDOT = 8839
352759 XDOT = 2694
234721
YDOT = 11546
700048 feet/sec YDOT = 3519
434175 meter/sec
ZDOT = 19285
964949 ZDOT = 5878
362116
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 14173
50215205
00016717 00000-0 10270-3 0 9069
2 25544 51
6478 73
2192 0003762 124
2062 235
9446 15
50826502 12158
Satellite: ISS
Catalog Number: 25544
Epoch time: 14173
50215205 = yrday
fracday
Element set: 906
Inclination: 51
6478 deg
RA of node: 73
2192 deg
Eccentricity:
0003762
Arg of perigee: 124
2062 deg
Mean anomaly: 235
9446 deg
Mean motion: 15
50826502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1215
Checksum: 281
Coasting Arc #8 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2014/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2935731
76 A = 6798919
18 meter
Y = -6104042
04 meter E =
0016710
Z = 488392
60 I = 52
00205
XDOT = 4072
144696 Wp = 129
56395
YDOT = -2449
868565 meter/sec RA = 67
54405 deg
ZDOT = -6015
083834 TA = 45
19975
MA = 45
06400
Ha = 227
465 n
mi
Hp = 218
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9631665
89 X = -2869629
25
Y = -20026384
65 feet Y = -6136501
74 meter
Z = 1602337
93 Z = 474290
96
XDOT = 13360
054777 XDOT = 4128
456523
YDOT = -8037
626527 feet/sec YDOT = -2404
015622 meter/sec
ZDOT = -19734
527015 ZDOT = -5995
165350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19897968
59 X = -6064900
83
Y = 9903567
20 feet Y = 3018607
28 meter
Z = 1543618
98 Z = 470495
07
XDOT = -7493
484546 XDOT = -2284
014090
YDOT = -11926
012052 feet/sec YDOT = -3635
048474 meter/sec
ZDOT = -19649
553009 ZDOT = -5989
183757
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 14174
53317735
00016717 00000-0 10270-3 0 9075
2 25544 51
6482 68
1052 0003826 129
3833 230
7657 15
50804324 12317
Satellite: ISS
Catalog Number: 25544
Epoch time: 14174
53317735 = yrday
fracday
Element set: 907
Inclination: 51
6482 deg
RA of node: 68
1052 deg
Eccentricity:
0003826
Arg of perigee: 129
3833 deg
Mean anomaly: 230
7657 deg
Mean motion: 15
50804324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 296
Coasting Arc #9 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2014/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3047690
12 A = 6798846
41 meter
Y = 6071650
29 meter E =
0013165
Z = 111288
12 I = 51
98998
XDOT = -4265
564043 Wp = 62
47897
YDOT = 2020
603252 meter/sec RA = 62
61187 deg
ZDOT = 6035
244514 TA = 298
71219
MA = 298
84444
Ha = 227
289 n
mi
Hp = 218
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9998983
33 X = 2979028
43
Y = 19920112
50 feet Y = 6105347
60 meter
Z = 365118
50 Z = 125927
48
XDOT = -13994
632688 XDOT = -4317
159227
YDOT = 6629
275760 feet/sec YDOT = 1972
613659 meter/sec
ZDOT = 19800
670979 ZDOT = 6014
397893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19607857
96 X = 5976475
11
Y = -10595951
76 feet Y = -3229646
10 meter
Z = 426114
56 Z = 129879
72
XDOT = 6283
442386 XDOT = 1915
193239
YDOT = 12481
269799 feet/sec YDOT = 3804
291035 meter/sec
ZDOT = 19711
830817 ZDOT = 6008
166033
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 14175
56419060
00016717 00000-0 10270-3 0 9084
2 25544 51
6485 62
9912 0003617 131
7311 228
4150 15
50857569 12471
Satellite: ISS
Catalog Number: 25544
Epoch time: 14175
56419060 = yrday
fracday
Element set: 908
Inclination: 51
6485 deg
RA of node: 62
9912 deg
Eccentricity:
0003617
Arg of perigee: 131
7311 deg
Mean anomaly: 228
4150 deg
Mean motion: 15
50857569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 309
Coasting Arc #10 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2014/176/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4345788
91 A = 6789436
85 meter
Y = -706718
35 meter E =
0014144
Z = -5180847
49 I = 51
93818
XDOT = 2930
799890 Wp = 109
22970
YDOT = 6903
414371 meter/sec RA = 57
89225 deg
ZDOT = 1515
561218 TA = 175
34763
MA = 175
33447
Ha = 227
228 n
mi
Hp = 220
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14257837
63 X = 4378535
50
Y = -2318629
74 feet Y = -657937
09 meter
Z = -16997531
12 Z = -5159656
81
XDOT = 9615
485202 XDOT = 2846
024402
YDOT = 22648
997280 feet/sec YDOT = 6935
714232 meter/sec
ZDOT = 4972
313706 ZDOT = 1529
593728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1300174
98 X = 396293
33
Y = -14492239
28 feet Y = -4417234
53 meter
Z = -16907471
36 Z = -5153397
27
XDOT = 23258
252940 XDOT = 7089
115496
YDOT = -3786
768079 feet/sec YDOT = -1154
206910 meter/sec
ZDOT = 5030
569907 ZDOT = 1533
317708
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 14176
46632088
00016717 00000-0 10270-3 0 9092
2 25544 51
6484 58
5164 0001968 180
2854 179
8296 15
50255088 12612
Satellite: ISS
Catalog Number: 25544
Epoch time: 14176
46632088 = yrday
fracday
Element set: 909
Inclination: 51
6484 deg
RA of node: 58
5164 deg
Eccentricity:
0001968
Arg of perigee: 180
2854 deg
Mean anomaly: 179
8296 deg
Mean motion: 15
50255088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 338
Coasting Arc #11 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2014/177/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4498254
38 A = 6789833
96 meter
Y = 603377
06 meter E =
0004843
Z = 5046527
52 I = 51
92250
XDOT = -3124
497950 Wp = 72
99462
YDOT = -6713
484724 meter/sec RA = 52
95362 deg
ZDOT = -1979
412242 TA = 36
17287
MA = 36
14013
Ha = 227
198 n
mi
Hp = 220
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14758052
42 X = -4529181
49
Y = 1979583
54 feet Y = 552901
02 meter
Z = 16556848
81 Z = 5024600
66
XDOT = -10250
977525 XDOT = -3039
578694
YDOT = -22025
868517 feet/sec YDOT = -6747
949764 meter/sec
ZDOT = -6494
134652 ZDOT = -1994
385305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1495239
04 X = -455748
86
Y = 14918430
86 feet Y = 4547137
73 meter
Z = 16463680
80 Z = 5018129
91
XDOT = -22697
993389 XDOT = -6918
348385
YDOT = 4971
281520 feet/sec YDOT = 1515
246607 meter/sec
ZDOT = -6556
409568 ZDOT = -1998
393636
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 14177
49772564
00016717 00000-0 10270-3 0 9102
2 25544 51
6482 53
4051 0001889 188
3166 171
7954 15
50301090 12770
Satellite: ISS
Catalog Number: 25544
Epoch time: 14177
49772564 = yrday
fracday
Element set: 910
Inclination: 51
6482 deg
RA of node: 53
4051 deg
Eccentricity:
0001889
Arg of perigee: 188
3166 deg
Mean anomaly: 171
7954 deg
Mean motion: 15
50301090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 316
Coasting Arc #12 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2014/178/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4686337
93 A = 6790554
93 meter
Y = -531387
49 meter E =
0012065
Z = -4896808
21 I = 51
90542
XDOT = 3270
934015 Wp = 116
21009
YDOT = 6478
399367 meter/sec RA = 48
01349 deg
ZDOT = 2426
781270 TA = 177
55649
MA = 177
55059
Ha = 227
032 n
mi
Hp = 220
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15375124
43 X = 4715718
70
Y = -1743397
28 feet Y = -478816
86 meter
Z = -16065643
73 Z = -4873971
48
XDOT = 10731
410811 XDOT = 3186
459523
YDOT = 21254
591098 feet/sec YDOT = 6514
504377 meter/sec
ZDOT = 7961
880808 ZDOT = 2442
466673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1600299
35 X = 487771
24
Y = -15491315
10 feet Y = -4721752
84 meter
Z = -15968625
24 Z = -4867236
97
XDOT = 21916
330952 XDOT = 6680
097674
YDOT = -6012
386253 feet/sec YDOT = -1832
575330 meter/sec
ZDOT = 8027
217024 ZDOT = 2446
695749
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 14178
46466070
00016717 00000-0 10270-3 0 9113
2 25544 51
6484 48
6127 0001891 192
1181 167
9925 15
50284067 12921
Satellite: ISS
Catalog Number: 25544
Epoch time: 14178
46466070 = yrday
fracday
Element set: 911
Inclination: 51
6484 deg
RA of node: 48
6127 deg
Eccentricity:
0001891
Arg of perigee: 192
1181 deg
Mean anomaly: 167
9925 deg
Mean motion: 15
50284067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1292
Checksum: 318
Coasting Arc #13 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2014/179/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4879987
25 A = 6791200
41 meter
Y = 478383
13 meter E =
0007001
Z = 4693695
10 I = 51
88647
XDOT = -3382
414804 Wp = 74
54622
YDOT = -6249
011120 meter/sec RA = 43
07262 deg
ZDOT = -2874
378214 TA = 43
94638
MA = 43
89073
Ha = 227
009 n
mi
Hp = 220
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16010456
86 X = -4907774
21
Y = 1569498
45 feet Y = 423655
96 meter
Z = 15399262
13 Z = 4669921
58
XDOT = -11097
161432 XDOT = -3298
322867
YDOT = -20502
004988 feet/sec YDOT = -6286
364879 meter/sec
ZDOT = -9430
374717 ZDOT = -2890
605970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1628307
58 X = -496308
15
Y = 16101139
21 feet Y = 4907627
23 meter
Z = 15298276
34 Z = 4662914
63
XDOT = -21099
418081 XDOT = -6431
102631
YDOT = 6907
550010 feet/sec YDOT = 2105
421243 meter/sec
ZDOT = -9498
051695 ZDOT = -2895
006157
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 14179
49604697
00016717 00000-0 10270-3 0 9127
2 25544 51
6483 43
5010 0001802 199
6089 160
4993 15
50331514 13087
Satellite: ISS
Catalog Number: 25544
Epoch time: 14179
49604697 = yrday
fracday
Element set: 912
Inclination: 51
6483 deg
RA of node: 43
5010 deg
Eccentricity:
0001802
Arg of perigee: 199
6089 deg
Mean anomaly: 160
4993 deg
Mean motion: 15
50331514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 308
Coasting Arc #14 (Orbit 1322)
---------------------------------------
Vector Time (GMT): 2014/180/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5095372
31 A = 6792128
59 meter
Y = -467845
88 meter E =
0009236
Z = -4476219
40 I = 51
86563
XDOT = 3443
020225 Wp = 121
69500
YDOT = 5989
641469 meter/sec RA = 38
13003 deg
ZDOT = 3293
510567 TA = 181
47131
MA = 181
47403
Ha = 226
840 n
mi
Hp = 221
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16717100
75 X = 5121968
97
Y = -1534927
43 feet Y = -410716
89 meter
Z = -14685759
18 Z = -4451402
51
XDOT = 11295
998115 XDOT = 3359
788152
YDOT = 19651
054688 feet/sec YDOT = 6027
677749 meter/sec
ZDOT = 10805
480864 ZDOT = 3310
034681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1511440
27 X = 460686
99
Y = -16811246
60 feet Y = -5124067
96 meter
Z = -14580346
99 Z = -4444089
76
XDOT = 20124
805179 XDOT = 6134
040619
YDOT = -7621
248465 feet/sec YDOT = -2322
956532 meter/sec
ZDOT = 10874
461526 ZDOT = 3314
535873
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 14180
46296459
00016717 00000-0 10270-3 0 9130
2 25544 51
6479 38
7082 0001851 204
5680 155
5383 15
50311547 13233
Satellite: ISS
Catalog Number: 25544
Epoch time: 14180
46296459 = yrday
fracday
Element set: 913
Inclination: 51
6479 deg
RA of node: 38
7082 deg
Eccentricity:
0001851
Arg of perigee: 204
5680 deg
Mean anomaly: 155
5383 deg
Mean motion: 15
50311547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1323
Checksum: 307
Coasting Arc #15 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2014/181/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5308154
05 A = 6792953
72 meter
Y = 475885
76 meter E =
0009103
Z = 4205016
67 I = 51
84398
XDOT = -3460
328069 Wp = 82
70432
YDOT = -5746
056617 meter/sec RA = 33
18691 deg
ZDOT = -3709
813874 TA = 45
32106
MA = 45
24693
Ha = 226
813 n
mi
Hp = 220
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17415203
58 X = -5333507
39
Y = 1561305
00 feet Y = 416384
35 meter
Z = 13795986
44 Z = 4179169
16
XDOT = -11352
782378 XDOT = -3377
796298
YDOT = -18851
891789 feet/sec YDOT = -5784
290362 meter/sec
ZDOT = -12171
305361 ZDOT = -3726
423640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1308887
02 X = -398948
76
Y = 17522299
39 feet Y = 5340796
85 meter
Z = 13686199
98 Z = 4171553
75
XDOT = -19160
073083 XDOT = -5839
990276
YDOT = 8150
328739 feet/sec YDOT = 2484
220200 meter/sec
ZDOT = -12240
692943 ZDOT = -3730
963209
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 14181
49433256
00016717 00000-0 10270-3 0 9143
2 25544 51
6480 33
5963 0001754 212
0146 148
0899 15
50360111 13396
Satellite: ISS
Catalog Number: 25544
Epoch time: 14181
49433256 = yrday
fracday
Element set: 914
Inclination: 51
6480 deg
RA of node: 33
5963 deg
Eccentricity:
0001754
Arg of perigee: 212
0146 deg
Mean anomaly: 148
0899 deg
Mean motion: 15
50360111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 293
Coasting Arc #16 (Orbit 1353)
---------------------------------------
Vector Time (GMT): 2014/182/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5526660
20 A = 6794002
11 meter
Y = -532630
40 meter E =
0005983
Z = -3922376
47 I = 51
81991
XDOT = 3428
745205 Wp = 121
80924
YDOT = 5489
950849 meter/sec RA = 28
24172 deg
ZDOT = 4087
145051 TA = 190
96651
MA = 190
97955
Ha = 226
668 n
mi
Hp = 221
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18132087
27 X = 5551258
87
Y = -1747475
07 feet Y = -470689
82 meter
Z = -12868689
19 Z = -3895469
32
XDOT = 11249
164060 XDOT = 3347
246675
YDOT = 18011
649766 feet/sec YDOT = 5527
837209 meter/sec
ZDOT = 13409
268539 ZDOT = 4103
603801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 926918
26 X = 282524
69
Y = -18272809
93 feet Y = -5569552
47 meter
Z = -12754397
65 Z = -3887540
40
XDOT = 18116
369512 XDOT = 5521
869427
YDOT = -8485
195358 feet/sec YDOT = -2586
287545 meter/sec
ZDOT = 13478
060978 ZDOT = 4108
112986
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 14182
46123308
00016717 00000-0 10270-3 0 9156
2 25544 51
6472 28
8030 0001853 216
2748 143
8278 15
50337163 13545
Satellite: ISS
Catalog Number: 25544
Epoch time: 14182
46123308 = yrday
fracday
Element set: 915
Inclination: 51
6472 deg
RA of node: 28
8030 deg
Eccentricity:
0001853
Arg of perigee: 216
2748 deg
Mean anomaly: 143
8278 deg
Mean motion: 15
50337163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1354
Checksum: 295
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