[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 16th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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
294/15:33:44
000 0
0 0
0 0
0
N/A 0
0 0
0 225
5
000/00:00:00
000 0
0 0
0 221
2
300/05:39:30
000 0
0 0
0 0
0
N/A 0
0 0
0 225
5
000/00:00:00
000 0
0 0
0 220
7
Coasting Arc #1 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2014/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1948829
22 A = 6794907
68 meter
Y = -5504129
22 meter E =
0009589
Z = 3467356
23 I = 51
40077
XDOT = 6142
080224 Wp = 92
55584
YDOT = 687
036089 meter/sec RA = 222
20599 deg
ZDOT = 4531
471951 TA = 308
23677
MA = 308
32304
Ha = 225
758 n
mi
Hp = 221
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6393796
67 X = -1903979
42
Y = -18058166
74 feet Y = -5525671
27 meter
Z = 11375840
65 Z = 3457998
33
XDOT = 20151
181838 XDOT = 6111
928455
YDOT = 2254
055409 feet/sec YDOT = 755
552554 meter/sec
ZDOT = 14867
033959 ZDOT = 4561
236346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13034411
28 X = 3972888
56
Y = 14070078
63 feet Y = 4288559
97 meter
Z = 11336877
09 Z = 3455480
14
XDOT = -18306
576883 XDOT = -5579
844634
YDOT = 4848
135915 feet/sec YDOT = 1477
711827 meter/sec
ZDOT = 14993
559416 ZDOT = 4570
036910
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 14288
55721382
00016717 00000-0 10270-3 0 9003
2 25544 51
6445 222
9368 0002737 265
6122 94
4716 15
50482796 30003
Satellite: ISS
Catalog Number: 25544
Epoch time: 14288
55721382 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 222
9368 deg
Eccentricity:
0002737
Arg of perigee: 265
6122 deg
Mean anomaly: 94
4716 deg
Mean motion: 15
50482796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 310
Coasting Arc #2 (Orbit 3014)
---------------------------------------
Vector Time (GMT): 2014/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1875431
99 A = 6793627
77 meter
Y = 5279206
30 meter E =
0003625
Z = -3846801
22 I = 51
42106
XDOT = -6406
774308 Wp = 64
74550
YDOT = -731
695038 meter/sec RA = 217
23196 deg
ZDOT = -4129
192040 TA = 161
64608
MA = 161
63300
Ha = 225
684 n
mi
Hp = 221
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6152992
11 X = 1834946
01
Y = 17320230
63 feet Y = 5299951
90 meter
Z = -12620738
91 Z = -3837789
33
XDOT = -21019
600748 XDOT = -6378
057667
YDOT = -2400
574273 feet/sec YDOT = -803
179524 meter/sec
ZDOT = -13547
217980 ZDOT = -4160
245741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12760521
73 X = -3889407
02
Y = -13265174
34 feet Y = -4043225
14 meter
Z = -12583202
55 Z = -3835360
14
XDOT = 19122
756056 XDOT = 5828
616046
YDOT = -5424
106147 feet/sec YDOT = -1653
267554 meter/sec
ZDOT = -13679
235742 ZDOT = -4169
431054
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 14289
52400658
00016717 00000-0 10270-3 0 9012
2 25544 51
6449 218
1433 0002716 271
0420 89
0420 15
50522297 30155
Satellite: ISS
Catalog Number: 25544
Epoch time: 14289
52400658 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 218
1433 deg
Eccentricity:
0002716
Arg of perigee: 271
0420 deg
Mean anomaly: 89
0420 deg
Mean motion: 15
50522297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3015
Checksum: 281
Coasting Arc #3 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2014/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1763216
54 A = 6792422
44 meter
Y = -5052092
93 meter E =
0007633
Z = 4179251
57 I = 51
44262
XDOT = 6675
060894 Wp = 109
02128
YDOT = 732
061392 meter/sec RA = 212
25892 deg
ZDOT = 3693
170314 TA = 302
89844
MA = 302
97185
Ha = 225
655 n
mi
Hp = 221
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5784831
16 X = -1726893
48
Y = -16575108
02 feet Y = -5071606
86 meter
Z = 13711455
30 Z = 4170774
74
XDOT = 21899
806082 XDOT = 6648
438287
YDOT = 2401
776219 feet/sec YDOT = 806
557745 meter/sec
ZDOT = 12116
700506 ZDOT = 3725
532410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12343685
66 X = 3762355
39
Y = 12521932
29 feet Y = 3816684
96 meter
Z = 13676151
50 Z = 4168490
98
XDOT = -19870
476214 XDOT = -6056
521150
YDOT = 6175
123524 feet/sec YDOT = 1882
177650 meter/sec
ZDOT = 12254
299037 ZDOT = 3735
110347
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 14290
55523040
00016717 00000-0 10270-3 0 9029
2 25544 51
6448 213
0304 0002752 273
0716 87
0120 15
50546741 30318
Satellite: ISS
Catalog Number: 25544
Epoch time: 14290
55523040 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 213
0304 deg
Eccentricity:
0002752
Arg of perigee: 273
0716 deg
Mean anomaly: 87
0120 deg
Mean motion: 15
50546741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3031
Checksum: 261
Coasting Arc #4 (Orbit 3045)
---------------------------------------
Vector Time (GMT): 2014/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1584478
83 A = 6791150
38 meter
Y = 4844950
53 meter E =
0007152
Z = -4494616
37 I = 51
46652
XDOT = -6920
014718 Wp = 59
31345
YDOT = -703
635439 meter/sec RA = 207
28606 deg
ZDOT = -3198
210660 TA = 178
40852
MA = 178
40624
Ha = 225
586 n
mi
Hp = 221
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5198421
37 X = 1552017
36
Y = 15895506
98 feet Y = 4862487
22 meter
Z = -14746116
70 Z = -4486998
47
XDOT = -22703
460362 XDOT = -6896
096131
YDOT = -2308
515219 feet/sec YDOT = -780
886130 meter/sec
ZDOT = -10492
817127 ZDOT = -3231
769325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11737682
11 X = -3577645
51
Y = -11952033
13 feet Y = -3642979
70 meter
Z = -14714428
55 Z = -4484957
82
XDOT = 20477
286095 XDOT = 6241
476802
YDOT = -7017
327780 feet/sec YDOT = -2138
881507 meter/sec
ZDOT = -10635
525029 ZDOT = -3241
708029
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 14291
52198262
00016717 00000-0 10270-3 0 9032
2 25544 51
6456 208
2367 0002732 278
4617 81
6224 15
50591725 30462
Satellite: ISS
Catalog Number: 25544
Epoch time: 14291
52198262 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 208
2367 deg
Eccentricity:
0002732
Arg of perigee: 278
4617 deg
Mean anomaly: 81
6224 deg
Mean motion: 15
50591725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3046
Checksum: 308
Coasting Arc #5 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2014/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1365113
50 A = 6790044
39 meter
Y = -4649415
16 meter E =
0005114
Z = 4754294
03 I = 51
49117
XDOT = 7154
092203 Wp = 127
36329
YDOT = 637
500163 meter/sec RA = 202
31422 deg
ZDOT = 2672
588966 TA = 296
14440
MA = 296
19700
Ha = 225
559 n
mi
Hp = 221
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4478718
83 X = -1336116
35
Y = -15253986
74 feet Y = -4664518
06 meter
Z = 15598077
51 Z = 4747733
37
XDOT = 23471
431111 XDOT = 7133
449060
YDOT = 2091
535968 feet/sec YDOT = 717
386743 meter/sec
ZDOT = 8768
336502 ZDOT = 2707
292791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11013564
11 X = 3356934
34
Y = 11501869
34 feet Y = 3505769
77 meter
Z = 15570853
00 Z = 4745995
99
XDOT = -20966
368833 XDOT = -6390
549220
YDOT = 7983
801112 feet/sec YDOT = 2433
462579 meter/sec
ZDOT = 8915
940585 ZDOT = 2717
578690
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 14292
55316326
00016717 00000-0 10270-3 0 9040
2 25544 51
6455 203
1235 0002791 280
3732 79
7105 15
50615309 30623
Satellite: ISS
Catalog Number: 25544
Epoch time: 14292
55316326 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 203
1235 deg
Eccentricity:
0002791
Arg of perigee: 280
3732 deg
Mean anomaly: 79
7105 deg
Mean motion: 15
50615309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 287
Coasting Arc #6 (Orbit 3076)
---------------------------------------
Vector Time (GMT): 2014/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1090325
91 A = 6788993
79 meter
Y = 4490368
60 meter E =
0010183
Z = -4983171
59 I = 51
51826
XDOT = -7341
368707 Wp = 66
43374
YDOT = -545
830759 meter/sec RA = 197
34316 deg
ZDOT = -2097
584566 TA = 183
07225
MA = 183
07851
Ha = 225
507 n
mi
Hp = 221
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3577184
76 X = 1064239
58
Y = 14732180
43 feet Y = 4502414
87 meter
Z = -16348988
15 Z = -4977938
76
XDOT = -24085
855337 XDOT = -7324
529908
YDOT = -1790
783330 feet/sec YDOT = -627
832803 meter/sec
ZDOT = -6881
839127 ZDOT = -2133
207518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10172939
28 X = -3100711
89
Y = -11271670
31 feet Y = -3435605
11 meter
Z = -16327386
79 Z = -4976587
49
XDOT = 21240
114238 XDOT = 6473
986820
YDOT = -8978
888148 feet/sec YDOT = -2736
765107 meter/sec
ZDOT = -7033
381130 ZDOT = -2143
774568
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 14293
51987527
00016717 00000-0 10270-3 0 9055
2 25544 51
6464 198
3298 0002796 285
8416 74
2427 15
50660178 30778
Satellite: ISS
Catalog Number: 25544
Epoch time: 14293
51987527 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 198
3298 deg
Eccentricity:
0002796
Arg of perigee: 285
8416 deg
Mean anomaly: 74
2427 deg
Mean motion: 15
50660178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3077
Checksum: 347
Coasting Arc #7 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2014/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -778303
18 A = 6788176
34 meter
Y = -4355657
63 meter E =
0002231
Z = 5147399
06 I = 51
54579
XDOT = 7503
643697 Wp = 148
27247
YDOT = 429
764662 meter/sec RA = 192
37320 deg
ZDOT = 1496
082979 TA = 287
27951
MA = 287
30392
Ha = 225
466 n
mi
Hp = 221
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2553488
12 X = -754544
27
Y = -14290215
31 feet Y = -4364227
66 meter
Z = 16887792
21 Z = 5143676
34
XDOT = 24618
253598 XDOT = 7491
012640
YDOT = 1409
989048 feet/sec YDOT = 513
604824 meter/sec
ZDOT = 4908
408724 ZDOT = 1532
504611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9258721
54 X = 2822058
33
Y = 11203555
50 feet Y = 3414843
72 meter
Z = 16872596
14 Z = 5142767
30
XDOT = -21366
163404 XDOT = -6512
406605
YDOT = 10021
079110 feet/sec YDOT = 3054
424913 meter/sec
ZDOT = 5063
379816 ZDOT = 1543
318168
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 14294
55101302
00016717 00000-0 10270-3 0 9060
2 25544 51
6462 193
2163 0002876 287
7888 72
2949 15
50686466 30937
Satellite: ISS
Catalog Number: 25544
Epoch time: 14294
55101302 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 193
2163 deg
Eccentricity:
0002876
Arg of perigee: 287
7888 deg
Mean anomaly: 72
2949 deg
Mean motion: 15
50686466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 331
Coasting Arc #8 (Orbit 3094)
---------------------------------------
Vector Time (GMT): 2014/294/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6561521
55 A = 6799348
54 meter
Y = 1707992
62 meter E =
0008746
Z = -441992
62 I = 51
58596
XDOT = -1575
390703 Wp = 148
22539
YDOT = 4519
694341 meter/sec RA = 191
62737 deg
ZDOT = -5983
004970 TA = 36
53688
MA = 36
47724
Ha = 225
457 n
mi
Hp = 221
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21527301
68 X = 6544081
81
Y = 5603650
32 feet Y = 1781270
24 meter
Z = -1450107
02 Z = -410159
59
XDOT = -5168
604670 XDOT = -1596
749775
YDOT = 14828
393506 feet/sec YDOT = 4501
957161 meter/sec
ZDOT = -19629
281396 ZDOT = -5990
710571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8328744
44 X = -2538601
31
Y = 20635687
32 feet Y = 6289757
49 meter
Z = -1314857
39 Z = -400768
53
XDOT = -12549
306445 XDOT = -3825
028605
YDOT = -6303
744904 feet/sec YDOT = -1921
381447 meter/sec
ZDOT = -19662
756860 ZDOT = -5993
208291
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 14294
67990278
00016717 00000-0 10270-3 0 9072
2 25544 51
6448 192
5767 0003042 287
5821 72
4998 15
50664298 30951
Satellite: ISS
Catalog Number: 25544
Epoch time: 14294
67990278 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 192
5767 deg
Eccentricity:
0003042
Arg of perigee: 287
5821 deg
Mean anomaly: 72
4998 deg
Mean motion: 15
50664298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3095
Checksum: 357
Coasting Arc #9 (Orbit 3110)
---------------------------------------
Vector Time (GMT): 2014/295/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6533914
76 A = 6798884
02 meter
Y = -1561699
93 meter E =
0011987
Z = 1000368
88 I = 51
61460
XDOT = 1977
985552 Wp = 43
63418
YDOT = -4474
545282 meter/sec RA = 186
66779 deg
ZDOT = 5900
142887 TA = 327
19607
MA = 327
27043
Ha = 225
390 n
mi
Hp = 221
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21436728
22 X = -6520825
44
Y = -5123687
43 feet Y = -1634693
10 meter
Z = 3282050
14 Z = 968659
26
XDOT = 6489
453910 XDOT = 1999
212265
YDOT = -14680
266673 feet/sec YDOT = -4452
306827 meter/sec
ZDOT = 19357
424169 ZDOT = 5909
803943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7486608
48 X = 2281918
26
Y = -20750965
79 feet Y = -6324894
37 meter
Z = 3147293
28 Z = 959294
99
XDOT = 12362
886667 XDOT = 3768
207856
YDOT = 7420
119966 feet/sec YDOT = 2261
652566 meter/sec
ZDOT = 19399
221128 ZDOT = 5912
882600
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 14295
71101548
00016717 00000-0 10270-3 0 9083
2 25544 51
6437 187
4617 0003088 290
7430 69
3390 15
50715159 31111
Satellite: ISS
Catalog Number: 25544
Epoch time: 14295
71101548 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 187
4617 deg
Eccentricity:
0003088
Arg of perigee: 290
7430 deg
Mean anomaly: 69
3390 deg
Mean motion: 15
50715159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3111
Checksum: 308
Coasting Arc #10 (Orbit 3125)
---------------------------------------
Vector Time (GMT): 2014/296/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6449037
64 A = 6798185
26 meter
Y = 1444358
47 meter E =
0005586
Z = -1580948
87 I = 51
64313
XDOT = -2404
790190 Wp = 157
44376
YDOT = 4470
430053 meter/sec RA = 181
71144 deg
ZDOT = -5737
245355 TA = 39
81528
MA = 39
77430
Ha = 225
423 n
mi
Hp = 221
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21158259
98 X = 6440087
12
Y = 4738708
90 feet Y = 1516425
60 meter
Z = -5186840
14 Z = -1549641
42
XDOT = -7889
731595 XDOT = -2426
730415
YDOT = 14666
765267 feet/sec YDOT = 4443
414910 meter/sec
ZDOT = -18822
983447 ZDOT = -5748
981511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6719951
17 X = -2048241
12
Y = 20647816
75 feet Y = 6293454
54 meter
Z = -5053766
72 Z = -1540388
10
XDOT = -12359
315168 XDOT = -3767
119263
YDOT = -8632
221397 feet/sec YDOT = -2631
101082 meter/sec
ZDOT = -18873
620693 ZDOT = -5752
679587
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 14296
67766448
00016717 00000-0 10270-3 0 9096
2 25544 51
6432 182
6678 0003094 295
0677 65
0152 15
50742417 31260
Satellite: ISS
Catalog Number: 25544
Epoch time: 14296
67766448 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 182
6678 deg
Eccentricity:
0003094
Arg of perigee: 295
0677 deg
Mean anomaly: 65
0152 deg
Mean motion: 15
50742417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3126
Checksum: 330
Coasting Arc #11 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2014/297/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6309719
27 A = 6797230
05 meter
Y = -1328507
71 meter E =
0011986
Z = 2129538
19 I = 51
67054
XDOT = 2817
688987 Wp = 59
29234
YDOT = -4522
897538 meter/sec RA = 176
75460 deg
ZDOT = 5509
985788 TA = 324
27127
MA = 324
35142
Ha = 225
413 n
mi
Hp = 220
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20701178
69 X = -6304739
53
Y = -4358621
09 feet Y = -1399039
07 meter
Z = 6986673
87 Z = 2098897
81
XDOT = 9244
386439 XDOT = 2841
289171
YDOT = -14838
902684 feet/sec YDOT = -4491
255938 meter/sec
ZDOT = 18077
381193 ZDOT = 5523
731772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5950190
80 X = 1813618
16
Y = -20345388
74 feet Y = -6201274
49 meter
Z = 6856411
27 Z = 2089834
15
XDOT = 12602
728154 XDOT = 3841
311541
YDOT = 9817
082072 feet/sec YDOT = 2992
246616 meter/sec
ZDOT = 18136
592814 ZDOT = 5528
033490
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 14297
70873475
00016717 00000-0 10270-3 0 9102
2 25544 51
6421 177
5525 0003065 296
1287 63
9548 15
50783069 31421
Satellite: ISS
Catalog Number: 25544
Epoch time: 14297
70873475 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 177
5525 deg
Eccentricity:
0003065
Arg of perigee: 296
1287 deg
Mean anomaly: 63
9548 deg
Mean motion: 15
50783069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3142
Checksum: 327
Coasting Arc #12 (Orbit 3156)
---------------------------------------
Vector Time (GMT): 2014/298/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6115427
75 A = 6796015
63 meter
Y = 1259548
39 meter E =
0001974
Z = -2682751
72 I = 51
69755
XDOT = -3226
894268 Wp = 132
06677
YDOT = 4610
469564 meter/sec RA = 171
80012 deg
ZDOT = -5194
958854 TA = 78
13533
MA = 78
11319
Ha = 225
434 n
mi
Hp = 220
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20063739
35 X = 6113920
99
Y = 4132376
60 feet Y = 1327926
49 meter
Z = -8801678
86 Z = -2653046
74
XDOT = -10586
923453 XDOT = -3252
973630
YDOT = 15126
212480 feet/sec YDOT = 4574
238228 meter/sec
ZDOT = -17043
828261 ZDOT = -5210
698697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5335652
44 X = -1626306
87
Y = 19833516
87 feet Y = 6045255
94 meter
Z = -8675375
83 Z = -2644254
55
XDOT = -13019
937429 XDOT = -3968
476928
YDOT = -10981
955284 feet/sec YDOT = -3347
299970 meter/sec
ZDOT = -17111
555062 ZDOT = -5215
601983
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 14298
67534401
00016717 00000-0 10270-3 0 9113
2 25544 51
6417 172
7579 0003037 302
6543 57
4315 15
50818104 31574
Satellite: ISS
Catalog Number: 25544
Epoch time: 14298
67534401 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 172
7579 deg
Eccentricity:
0003037
Arg of perigee: 302
6543 deg
Mean anomaly: 57
4315 deg
Mean motion: 15
50818104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3157
Checksum: 301
Coasting Arc #13 (Orbit 3172)
---------------------------------------
Vector Time (GMT): 2014/299/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5869767
90 A = 6794678
55 meter
Y = -1212185
20 meter E =
0010624
Z = 3188798
55 I = 51
72341
XDOT = 3604
584347 Wp = 76
29711
YDOT = -4747
780454 meter/sec RA = 166
84507 deg
ZDOT = 4819
278863 TA = 320
45204
MA = 320
52951
Ha = 225
461 n
mi
Hp = 220
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19257768
71 X = -5871267
28
Y = -3976985
56 feet Y = -1277833
00 meter
Z = 10461937
51 Z = 3160279
70
XDOT = 11826
064132 XDOT = 3633
996097
YDOT = -15576
707526 feet/sec YDOT = -4707
307013 meter/sec
ZDOT = 15811
282359 ZDOT = 4836
861521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4804067
76 X = 1464279
85
Y = -19134309
41 feet Y = -5832137
51 meter
Z = 10340664
53 Z = 3151834
55
XDOT = 13660
896326 XDOT = 4163
841200
YDOT = 12035
318659 feet/sec YDOT = 3668
365127 meter/sec
ZDOT = 15886
891993 ZDOT = 4842
324680
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 14299
70637196
00016717 00000-0 10270-3 0 9124
2 25544 51
6409 167
6423 0003002 302
1779 57
9081 15
50850781 31734
Satellite: ISS
Catalog Number: 25544
Epoch time: 14299
70637196 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 167
6423 deg
Eccentricity:
0003002
Arg of perigee: 302
1779 deg
Mean anomaly: 57
9081 deg
Mean motion: 15
50850781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3173
Checksum: 312
Coasting Arc #14 (Orbit 3181)
---------------------------------------
Vector Time (GMT): 2014/300/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2483687
15 A = 6787408
14 meter
Y = -3565974
23 meter E =
0001095
Z = 5213020
65 I = 51
71836
XDOT = 6935
266759 Wp = 111
20033
YDOT = -3016
956773 meter/sec RA = 163
92427 deg
ZDOT = 1239
882563 TA = 326
90262
MA = 326
90947
Ha = 225
516 n
mi
Hp = 220
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8148579
89 X = -2468950
82
Y = -11699390
50 feet Y = -3593665
86 meter
Z = 17103086
11 Z = 5200990
85
XDOT = 22753
499864 XDOT = 6962
464517
YDOT = -9898
152141 feet/sec YDOT = -2939
250016 meter/sec
ZDOT = 4067
856178 ZDOT = 1273
640115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6103599
32 X = -1860377
07
Y = 12951929
53 feet Y = 3947748
12 meter
Z = 17052397
01 Z = 5197570
61
XDOT = -18875
616571 XDOT = -5753
287931
YDOT = -14443
337336 feet/sec YDOT = -4402
329220 meter/sec
ZDOT = 4212
100927 ZDOT = 1283
848363
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 14300
28631706
00016717 00000-0 10270-3 0 9132
2 25544 51
6421 164
7685 0003157 309
3745 50
7126 15
50866167 31825
Satellite: ISS
Catalog Number: 25544
Epoch time: 14300
28631706 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 164
7685 deg
Eccentricity:
0003157
Arg of perigee: 309
3745 deg
Mean anomaly: 50
7126 deg
Mean motion: 15
50866167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3182
Checksum: 301
Coasting Arc #15 (Orbit 3196)
---------------------------------------
Vector Time (GMT): 2014/301/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2067796
05 A = 6786948
39 meter
Y = 3694692
06 meter E =
0012775
Z = -5315284
90 I = 51
74690
XDOT = -6964
965070 Wp = 75
31811
YDOT = 3128
595325 meter/sec RA = 158
96451 deg
ZDOT = -532
775586 TA = 189
58427
MA = 189
60867
Ha = 225
526 n
mi
Hp = 220
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6784107
77 X = 2052147
97
Y = 12121693
12 feet Y = 3717727
88 meter
Z = -17438598
74 Z = -5305277
71
XDOT = -22850
935270 XDOT = -6996
843984
YDOT = 10264
420357 feet/sec YDOT = 3050
530316 meter/sec
ZDOT = -1747
951396 ZDOT = -566
688642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6935836
93 X = 2114043
10
Y = -12096229
93 feet Y = -3686930
88 meter
Z = -17396542
07 Z = -5302466
02
XDOT = 19563
758639 XDOT = 5963
033633
YDOT = 13949
814041 feet/sec YDOT = 4251
903320 meter/sec
ZDOT = -1892
898450 ZDOT = -576
955447
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 14301
25287523
00016717 00000-0 10270-3 0 9145
2 25544 51
6423 159
9728 0003171 313
6277 46
4611 15
50877845 31977
Satellite: ISS
Catalog Number: 25544
Epoch time: 14301
25287523 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 159
9728 deg
Eccentricity:
0003171
Arg of perigee: 313
6277 deg
Mean anomaly: 46
4611 deg
Mean motion: 15
50877845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3197
Checksum: 316
Coasting Arc #16 (Orbit 3212)
---------------------------------------
Vector Time (GMT): 2014/302/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1638748
93 A = 6786700
66 meter
Y = -3870123
43 meter E =
0002716
Z = 5328661
92 I = 51
77604
XDOT = 6952
736605 Wp = 4
88057
YDOT = -3217
951062 meter/sec RA = 154
00751 deg
ZDOT = -196
291928 TA = 87
00331
MA = 86
97223
Ha = 225
557 n
mi
Hp = 220
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5376472
86 X = -1621235
90
Y = -12697255
34 feet Y = -3888350
94 meter
Z = 17482486
62 Z = 5320743
59
XDOT = 22810
815633 XDOT = 6989
157273
YDOT = -10557
582226 feet/sec YDOT = -3139
997422 meter/sec
ZDOT = -644
002390 ZDOT = -162
427379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7953199
16 X = -2424135
10
Y = 11315068
00 feet Y = 3448832
73 meter
Z = 17449353
89 Z = 5318563
07
XDOT = -20103
334931 XDOT = -6127
496487
YDOT = -13347
055097 feet/sec YDOT = -4068
182394 meter/sec
ZDOT = -499
225792 ZDOT = -152
164021
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 14302
28384906
00016717 00000-0 10270-3 0 9153
2 25544 51
6429 154
8587 0003266 317
4731 42
6166 15
50924193 32133
Satellite: ISS
Catalog Number: 25544
Epoch time: 14302
28384906 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 154
8587 deg
Eccentricity:
0003266
Arg of perigee: 317
4731 deg
Mean anomaly: 42
6166 deg
Mean motion: 15
50924193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3213
Checksum: 310
Coasting Arc #17 (Orbit 3227)
---------------------------------------
Vector Time (GMT): 2014/303/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1237249
42 A = 6786900
35 meter
Y = 4098767
40 meter E =
0012276
Z = -5276531
10 I = 51
80487
XDOT = -6861
622573 Wp = 86
30295
YDOT = 3262
922887 meter/sec RA = 149
05103 deg
ZDOT = 928
322732 TA = 192
55892
MA = 192
58954
Ha = 225
577 n
mi
Hp = 220
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4059217
26 X = 1216956
16
Y = 13447399
61 feet Y = 4112489
50 meter
Z = -17311453
75 Z = -5270570
05
XDOT = -22511
885083 XDOT = -6902
108918
YDOT = 10705
127581 feet/sec YDOT = 3185
965433 meter/sec
ZDOT = 3045
678253 ZDOT = 894
891022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9098520
20 X = 2773228
96
Y = -10741663
74 feet Y = -3274059
11 meter
Z = -17286694
95 Z = -5268984
62
XDOT = 20353
697838 XDOT = 6203
807101
YDOT = 12582
757554 feet/sec YDOT = 3835
224503 meter/sec
ZDOT = 2902
718109 ZDOT = 884
748480
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 14303
25036729
00016717 00000-0 10270-3 0 9169
2 25544 51
6432 150
0629 0003334 321
0476 39
0434 15
50944360 32287
Satellite: ISS
Catalog Number: 25544
Epoch time: 14303
25036729 = yrday
fracday
Element set: 916
Inclination: 51
6432 deg
RA of node: 150
0629 deg
Eccentricity:
0003334
Arg of perigee: 321
0476 deg
Mean anomaly: 39
0434 deg
Mean motion: 15
50944360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3228
Checksum: 280
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