[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 9th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 2889)
---------------------------------------
Vector Time (GMT): 2014/281/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1507243
38 A = 6795775
77 meter
Y = -5697804
17 meter E =
0010402
Z = 3375431
43 I = 51
29437
XDOT = 4661
629081 Wp = 96
63250
YDOT = 3970
418433 meter/sec RA = 257
49969 deg
ZDOT = 4607
126994 TA = 302
92473
MA = 303
02474
Ha = 226
381 n
mi
Hp = 221
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4945024
20 X = 1554448
47
Y = -18693583
23 feet Y = -5680684
79 meter
Z = 11074250
09 Z = 3382868
98
XDOT = 15294
058665 XDOT = 4594
504145
YDOT = 13026
307196 feet/sec YDOT = 4022
173112 meter/sec
ZDOT = 15115
246043 ZDOT = 4629
609323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9977428
77 X = -3041120
29
Y = 16541839
88 feet Y = 5041952
80 meter
Z = 11106789
90 Z = 3385349
56
XDOT = -9672
378943 XDOT = -2948
141102
YDOT = -16076
259952 feet/sec YDOT = -4900
044033 meter/sec
ZDOT = 15210
208796 ZDOT = 4636
071641
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 14281
46683544
00016717 00000-0 10270-3 0 9003
2 25544 51
6443 258
0782 0002489 238
7018 121
3890 15
50255564 28900
Satellite: ISS
Catalog Number: 25544
Epoch time: 14281
46683544 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 258
0782 deg
Eccentricity:
0002489
Arg of perigee: 238
7018 deg
Mean anomaly: 121
3890 deg
Mean motion: 15
50255564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2890
Checksum: 317
Coasting Arc #2 (Orbit 2904)
---------------------------------------
Vector Time (GMT): 2014/282/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1377670
54 A = 6794701
60 meter
Y = 5524264
66 meter E =
0003388
Z = -3711316
94 I = 51
29881
XDOT = -4872
418429 Wp = 91
28865
YDOT = -4081
677961 meter/sec RA = 252
51928 deg
ZDOT = -4270
332213 TA = 133
11665
MA = 133
08831
Ha = 226
291 n
mi
Hp = 221
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4519916
46 X = -1421312
99
Y = 18124227
90 feet Y = 5508614
18 meter
Z = -12176236
68 Z = -3718116
29
XDOT = -15985
624768 XDOT = -4805
669700
YDOT = -13391
331894 feet/sec YDOT = -4135
791813 meter/sec
ZDOT = -14010
276289 ZDOT = -4293
839582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9122947
42 X = 2780674
37
Y = -16277673
62 feet Y = -4961434
92 meter
Z = -12206031
02 Z = -3720398
25
XDOT = 10554
724872 XDOT = 3217
080141
YDOT = 16487
225042 feet/sec YDOT = 5025
306193 meter/sec
ZDOT = -14109
586102 ZDOT = -4300
601844
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 14282
43376526
00016717 00000-0 10270-3 0 9011
2 25544 51
6444 253
2855 0002533 242
1340 117
9554 15
50279891 29050
Satellite: ISS
Catalog Number: 25544
Epoch time: 14282
43376526 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 253
2855 deg
Eccentricity:
0002533
Arg of perigee: 242
1340 deg
Mean anomaly: 117
9554 deg
Mean motion: 15
50279891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2905
Checksum: 305
Coasting Arc #3 (Orbit 2920)
---------------------------------------
Vector Time (GMT): 2014/283/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1267419
37 A = 6793615
82 meter
Y = -5334340
89 meter E =
0008808
Z = 4006620
45 I = 51
30548
XDOT = 5110
296890 Wp = 110
75019
YDOT = 4159
893954 meter/sec RA = 247
53903 deg
ZDOT = 3911
797152 TA = 298
35806
MA = 298
44685
Ha = 226
144 n
mi
Hp = 221
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4158200
05 X = 1307511
71
Y = -17501118
41 feet Y = -5319943
20 meter
Z = 13145080
22 Z = 4012875
46
XDOT = 16766
065912 XDOT = 5044
397513
YDOT = 13647
946042 feet/sec YDOT = 4216
672544 meter/sec
ZDOT = 12833
980159 ZDOT = 3936
462289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8329390
84 X = -2538798
33
Y = 15921013
81 feet Y = 4852725
01 meter
Z = 13172527
26 Z = 4014986
31
XDOT = -11572
492924 XDOT = -3527
295843
YDOT = -16786
285596 feet/sec YDOT = -5116
459850 meter/sec
ZDOT = 12938
208434 ZDOT = 3943
565931
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 14283
46513810
00016717 00000-0 10270-3 0 9025
2 25544 51
6440 248
1734 0002567 247
8476 112
2402 15
50320830 29212
Satellite: ISS
Catalog Number: 25544
Epoch time: 14283
46513810 = yrday
fracday
Element set: 902
Inclination: 51
6440 deg
RA of node: 248
1734 deg
Eccentricity:
0002567
Arg of perigee: 247
8476 deg
Mean anomaly: 112
2402 deg
Mean motion: 15
50320830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2921
Checksum: 281
Coasting Arc #4 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2014/284/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1220599
57 A = 6792554
67 meter
Y = 5120071
61 meter E =
0005936
Z = -4299611
33 I = 51
31471
XDOT = -5347
565770 Wp = 69
41507
YDOT = -4213
829297 meter/sec RA = 242
55824 deg
ZDOT = -3501
715077 TA = 164
72443
MA = 164
70650
Ha = 226
129 n
mi
Hp = 221
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4004591
77 X = -1256876
11
Y = 16798135
21 feet Y = 5106218
88 meter
Z = -14106336
37 Z = -4305629
50
XDOT = -17544
507121 XDOT = -5283
037746
YDOT = -13824
899270 feet/sec YDOT = -4273
268740 meter/sec
ZDOT = -11488
566527 ZDOT = -3527
536244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7734658
88 X = 2357524
03
Y = -15415690
73 feet Y = -4698702
53 meter
Z = -14132740
67 Z = -4307659
36
XDOT = 12630
388941 XDOT = 3849
742549
YDOT = 16963
986228 feet/sec YDOT = 5170
623002 meter/sec
ZDOT = -11597
712330 ZDOT = -3534
982718
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 14284
43203245
00016717 00000-0 10270-3 0 9032
2 25544 51
6438 243
3805 0002495 250
8919 109
1962 15
50335723 29360
Satellite: ISS
Catalog Number: 25544
Epoch time: 14284
43203245 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 243
3805 deg
Eccentricity:
0002495
Arg of perigee: 250
8919 deg
Mean anomaly: 109
1962 deg
Mean motion: 15
50335723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 306
Coasting Arc #5 (Orbit 2951)
---------------------------------------
Vector Time (GMT): 2014/285/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1201724
04 A = 6791475
85 meter
Y = -4896634
03 meter E =
0006773
Z = 4547418
76 I = 51
32649
XDOT = 5600
812136 Wp = 126
56089
YDOT = 4233
300732 meter/sec RA = 237
57829 deg
ZDOT = 3071
137229 TA = 292
51675
MA = 292
58844
Ha = 225
940 n
mi
Hp = 221
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3942664
16 X = 1234299
70
Y = -16065072
28 feet Y = -4883013
11 meter
Z = 14919352
89 Z = 4553336
15
XDOT = 18375
367901 XDOT = 5538
139241
YDOT = 13888
781928 feet/sec YDOT = 4295
582431 meter/sec
ZDOT = 10075
909545 ZDOT = 3098
193164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7243747
74 X = -2207894
31
Y = 14845356
58 feet Y = 4524864
69 meter
Z = 14945291
75 Z = 4555324
92
XDOT = -13777
328757 XDOT = -4199
329805
YDOT = -17005
120212 feet/sec YDOT = -5183
160641 meter/sec
ZDOT = 10190
316179 ZDOT = 3106
008371
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 14285
46336593
00016717 00000-0 10270-3 0 9040
2 25544 51
6435 238
2686 0002625 256
8976 103
1882 15
50383064 29525
Satellite: ISS
Catalog Number: 25544
Epoch time: 14285
46336593 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 238
2686 deg
Eccentricity:
0002625
Arg of perigee: 256
8976 deg
Mean anomaly: 103
1882 deg
Mean motion: 15
50383064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2952
Checksum: 329
Coasting Arc #6 (Orbit 2966)
---------------------------------------
Vector Time (GMT): 2014/286/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1248209
16 A = 6790536
30 meter
Y = 4665541
56 meter E =
0008794
Z = -4781933
97 I = 51
34083
XDOT = -5837
279120 Wp = 69
42373
YDOT = -4218
758966 meter/sec RA = 232
59754 deg
ZDOT = -2593
248912 TA = 174
86952
MA = 174
86050
Ha = 225
977 n
mi
Hp = 221
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4095174
40 X = -1277058
08
Y = 15306894
87 feet Y = 4651421
67 meter
Z = -15688759
73 Z = -4788068
05
XDOT = -19151
178216 XDOT = -5777
072766
YDOT = -13841
072723 feet/sec YDOT = -4283
698732 meter/sec
ZDOT = -8508
034487 ZDOT = -2621
459533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6980143
40 X = 2127547
71
Y = -14195306
96 feet Y = -4326729
56 meter
Z = -15715582
21 Z = -4790109
46
XDOT = 14903
469972 XDOT = 4542
577647
YDOT = 16876
592746 feet/sec YDOT = 5143
985469 meter/sec
ZDOT = -8627
369554 ZDOT = -2629
622240
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 14286
43022332
00016717 00000-0 10270-3 0 9052
2 25544 51
6434 233
4753 0002499 259
9654 100
1215 15
50394808 29673
Satellite: ISS
Catalog Number: 25544
Epoch time: 14286
43022332 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 233
4753 deg
Eccentricity:
0002499
Arg of perigee: 259
9654 deg
Mean anomaly: 100
1215 deg
Mean motion: 15
50394808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2967
Checksum: 309
Coasting Arc #7 (Orbit 2982)
---------------------------------------
Vector Time (GMT): 2014/287/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1328255
90 A = 6789608
18 meter
Y = -4434391
06 meter E =
0004423
Z = 4965893
10 I = 51
35776
XDOT = 6076
104288 Wp = 144
43644
YDOT = 4172
332429 meter/sec RA = 227
61830 deg
ZDOT = 2096
080915 TA = 285
03901
MA = 285
08796
Ha = 225
778 n
mi
Hp = 221
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4357794
95 X = 1353620
54
Y = -14548527
10 feet Y = -4419395
50 meter
Z = 16292300
20 Z = 4972407
56
XDOT = 19934
725355 XDOT = 6018
814485
YDOT = 13688
754689 feet/sec YDOT = 4239
959173 meter/sec
ZDOT = 6876
905890 ZDOT = 2125
458734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6850284
45 X = -2087966
70
Y = 13520256
44 feet Y = 4120974
16 meter
Z = 16320702
55 Z = 4974550
14
XDOT = -16057
698727 XDOT = -4894
386572
YDOT = -16605
006941 feet/sec YDOT = -5061
206116 meter/sec
ZDOT = 7001
229866 ZDOT = 2133
974863
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 14287
46151668
00016717 00000-0 10270-3 0 9062
2 25544 51
6432 228
3634 0002660 265
6381 94
4465 15
50443852 29837
Satellite: ISS
Catalog Number: 25544
Epoch time: 14287
46151668 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 228
3634 deg
Eccentricity:
0002660
Arg of perigee: 265
6381 deg
Mean anomaly: 94
4465 deg
Mean motion: 15
50443852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2983
Checksum: 323
Coasting Arc #8 (Orbit 2997)
---------------------------------------
Vector Time (GMT): 2014/288/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1469498
41 A = 6788915
22 meter
Y = 4213839
52 meter E =
0011009
Z = -5125917
12 I = 51
37740
XDOT = -6280
007245 Wp = 75
68256
YDOT = -4087
927540 meter/sec RA = 222
63833 deg
ZDOT = -1560
348588 TA = 179
19295
MA = 179
19118
Ha = 225
835 n
mi
Hp = 221
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4821188
99 X = -1491608
98
Y = 13824932
82 feet Y = 4197282
64 meter
Z = -16817313
38 Z = -5133109
82
XDOT = -20603
698311 XDOT = -6226
248589
YDOT = -13411
835762 feet/sec YDOT = -4157
854180 meter/sec
ZDOT = -5119
253897 ZDOT = -1590
725437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6949926
49 X = 2118337
59
Y = -12845973
84 feet Y = -3915452
83 meter
Z = -16848564
86 Z = -5135442
57
XDOT = 17115
231790 XDOT = 5216
722650
YDOT = 16142
006938 feet/sec YDOT = 4920
083715 meter/sec
ZDOT = -5247
858726 ZDOT = -1599
547340
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
42833600
00016717 00000-0 10270-3 0 9073
2 25544 51
6433 223
5696 0002566 269
0002 91
0857 15
50456432 29988
Satellite: ISS
Catalog Number: 25544
Epoch time: 14288
42833600 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 223
5696 deg
Eccentricity:
0002566
Arg of perigee: 269
0002 deg
Mean anomaly: 91
0857 deg
Mean motion: 15
50456432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2998
Checksum: 315
Coasting Arc #9 (Orbit 3013)
---------------------------------------
Vector Time (GMT): 2014/289/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1645848
84 A = 6788284
64 meter
Y = -4003086
92 meter E =
0001872
Z = 5229363
94 I = 51
39960
XDOT = 6471
144028 Wp = 166
86915
YDOT = 3978
708988 meter/sec RA = 217
66052 deg
ZDOT = 1007
172834 TA = 273
43818
MA = 273
45959
Ha = 225
654 n
mi
Hp = 221
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5399766
54 X = 1665087
14
Y = -13133487
28 feet Y = -3984573
97 meter
Z = 17156705
84 Z = 5237406
38
XDOT = 21230
787493 XDOT = 6421
279658
YDOT = 13053
507178 feet/sec YDOT = 4050
794789 meter/sec
ZDOT = 3304
372816 ZDOT = 1038
487600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7194545
99 X = -2192897
62
Y = 12193770
36 feet Y = 3716661
20 meter
Z = 17191538
46 Z = 5239980
92
XDOT = -18131
419444 XDOT = -5526
456647
YDOT = -15552
147810 feet/sec YDOT = -4740
294652 meter/sec
ZDOT = 3437
002790 ZDOT = 1047
598450
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
45958881
00016717 00000-0 10270-3 0 9087
2 25544 51
6435 218
4574 0002692 274
0094 86
0749 15
50504147 30146
Satellite: ISS
Catalog Number: 25544
Epoch time: 14289
45958881 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 218
4574 deg
Eccentricity:
0002692
Arg of perigee: 274
0094 deg
Mean anomaly: 86
0749 deg
Mean motion: 15
50504147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3014
Checksum: 327
Coasting Arc #10 (Orbit 3028)
---------------------------------------
Vector Time (GMT): 2014/290/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1872436
85 A = 6787956
94 meter
Y = 3820673
62 meter E =
0012122
Z = -5299483
29 I = 51
42423
XDOT = -6610
033488 Wp = 84
29197
YDOT = -3834
489250 meter/sec RA = 212
68243 deg
ZDOT = -428
664674 TA = 181
59788
MA = 181
60176
Ha = 225
715 n
mi
Hp = 221
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6143165
52 X = -1889277
89
Y = 12535018
43 feet Y = 3799640
15 meter
Z = -17386756
21 Z = -5308620
69
XDOT = -21686
461576 XDOT = -6564
581729
YDOT = -12580
345308 feet/sec YDOT = -3908
152832 meter/sec
ZDOT = -1406
380163 ZDOT = -460
664842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7639884
64 X = 2328636
84
Y = -11624264
23 feet Y = -3543075
74 meter
Z = -17426218
90 Z = -5311511
52
XDOT = 18972
860560 XDOT = 5782
927899
YDOT = 14782
875294 feet/sec YDOT = 4505
820389 meter/sec
ZDOT = -1541
965843 ZDOT = -469
991189
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
42636958
00016717 00000-0 10270-3 0 9095
2 25544 51
6438 213
6634 0002672 277
5715 82
5132 15
50519572 30290
Satellite: ISS
Catalog Number: 25544
Epoch time: 14290
42636958 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 213
6634 deg
Eccentricity:
0002672
Arg of perigee: 277
5715 deg
Mean anomaly: 82
5132 deg
Mean motion: 15
50519572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 319
Coasting Arc #11 (Orbit 3044)
---------------------------------------
Vector Time (GMT): 2014/291/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2131011
12 A = 6787751
11 meter
Y = -3657006
23 meter E =
0000841
Z = 5306706
62 I = 51
45142
XDOT = 6720
946242 Wp = 342
95442
YDOT = 3677
274064 meter/sec RA = 207
70714 deg
ZDOT = -164
028725 TA = 108
61852
MA = 108
60939
Ha = 225
566 n
mi
Hp = 221
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6991506
31 X = 2145967
66
Y = -11998051
95 feet Y = -3633091
70 meter
Z = 17410454
80 Z = 5317095
60
XDOT = 22050
348564 XDOT = 6680
123400
YDOT = 12064
547455 feet/sec YDOT = 3752
203769 meter/sec
ZDOT = -538
151985 ZDOT = -131
478495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8219378
63 X = -2505266
61
Y = 11122747
42 feet Y = 3390213
41 meter
Z = 17455218
49 Z = 5320350
59
XDOT = -19703
506174 XDOT = -6005
628682
YDOT = -13928
270715 feet/sec YDOT = -4245
336914 meter/sec
ZDOT = -400
185608 ZDOT = -121
976573
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
45758190
00016717 00000-0 10270-3 0 9104
2 25544 51
6444 208
5511 0002730 281
9450 78
1395 15
50563703 30459
Satellite: ISS
Catalog Number: 25544
Epoch time: 14291
45758190 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 208
5511 deg
Eccentricity:
0002730
Arg of perigee: 281
9450 deg
Mean anomaly: 78
1395 deg
Mean motion: 15
50563703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 297
Coasting Arc #12 (Orbit 3059)
---------------------------------------
Vector Time (GMT): 2014/292/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2422309
25 A = 6787868
74 meter
Y = 3536405
93 meter E =
0011861
Z = -5273571
88 I = 51
48036
XDOT = -6766
314474 Wp = 93
69576
YDOT = -3495
063484 meter/sec RA = 202
73218 deg
ZDOT = 764
958454 TA = 183
63888
MA = 183
64751
Ha = 225
631 n
mi
Hp = 221
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7947208
82 X = -2436056
46
Y = 11602381
66 feet Y = 3509240
63 meter
Z = -17301745
00 Z = -5285373
06
XDOT = -22199
194467 XDOT = -6730
444944
YDOT = -11466
743715 feet/sec YDOT = -3570
528152 meter/sec
ZDOT = 2509
706215 ZDOT = 732
175741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8939709
21 X = 2724823
37
Y = -10774788
15 feet Y = -3284155
43 meter
Z = -17352501
49 Z = -5289042
45
XDOT = 20194
973663 XDOT = 6155
427973
YDOT = 12941
476859 feet/sec YDOT = 3944
562147 meter/sec
ZDOT = 2370
708363 ZDOT = 722
591909
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
42432435
00016717 00000-0 10270-3 0 9114
2 25544 51
6446 203
7569 0002767 285
5894 74
4951 15
50583569 30609
Satellite: ISS
Catalog Number: 25544
Epoch time: 14292
42432435 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 203
7569 deg
Eccentricity:
0002767
Arg of perigee: 285
5894 deg
Mean anomaly: 74
4951 deg
Mean motion: 15
50583569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 327
Coasting Arc #13 (Orbit 3075)
---------------------------------------
Vector Time (GMT): 2014/293/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2737858
70 A = 6788164
92 meter
Y = -3440659
12 meter E =
0003503
Z = 5171427
10 I = 51
51157
XDOT = 6770
229807 Wp = 15
94493
YDOT = 3316
115824 meter/sec RA = 197
76062 deg
ZDOT = -1374
496550 TA = 87
32245
MA = 87
28236
Ha = 225
517 n
mi
Hp = 221
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8982476
04 X = 2751007
92
Y = -11288251
69 feet Y = -3409968
46 meter
Z = 16966624
35 Z = 5184759
80
XDOT = 22212
040048 XDOT = 6739
322019
YDOT = 10879
645091 feet/sec YDOT = 3391
651941 meter/sec
ZDOT = -4509
503118 ZDOT = -1341
682671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9761511
58 X = -2975308
73
Y = 10529767
49 feet Y = 3209473
13 meter
Z = 17023887
12 Z = 5188880
79
XDOT = -20516
559087 XDOT = -6253
447210
YDOT = -11935
370649 feet/sec YDOT = -3637
900974 meter/sec
ZDOT = -4370
332741 ZDOT = -1332
077419
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
45549636
00016717 00000-0 10270-3 0 9121
2 25544 51
6453 198
6445 0002772 289
5077 70
5774 15
50622003 30769
Satellite: ISS
Catalog Number: 25544
Epoch time: 14293
45549636 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 198
6445 deg
Eccentricity:
0002772
Arg of perigee: 289
5077 deg
Mean anomaly: 70
5774 deg
Mean motion: 15
50622003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 324
Coasting Arc #14 (Orbit 3090)
---------------------------------------
Vector Time (GMT): 2014/294/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3063499
00 A = 6788738
20 meter
Y = 3397150
59 meter E =
0010134
Z = -5025345
04 I = 51
54393
XDOT = -6702
371861 Wp = 102
35287
YDOT = -3127
957177 meter/sec RA = 192
78999 deg
ZDOT = 1972
573777 TA = 186
85246
MA = 186
86632
Ha = 225
586 n
mi
Hp = 220
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10050849
74 X = -3076847
05
Y = 11145507
19 feet Y = 3362817
32 meter
Z = -16487352
48 Z = -5040260
20
XDOT = -21989
408993 XDOT = -6676
478497
YDOT = -10262
326697 feet/sec YDOT = -3202
762428 meter/sec
ZDOT = 6471
698742 ZDOT = 1940
077237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10638995
93 X = 3242765
96
Y = -10485195
92 feet Y = -3195887
72 meter
Z = -16551348
43 Z = -5044851
00
XDOT = 20563
869051 XDOT = 6267
867287
YDOT = 10873
722042 feet/sec YDOT = 3314
310478 meter/sec
ZDOT = 6333
839335 ZDOT = 1930
554229
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
42220095
00016717 00000-0 10270-3 0 9135
2 25544 51
6454 193
8502 0002824 293
2749 66
8105 15
50648513 30914
Satellite: ISS
Catalog Number: 25544
Epoch time: 14294
42220095 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 193
8502 deg
Eccentricity:
0002824
Arg of perigee: 293
2749 deg
Mean anomaly: 66
8105 deg
Mean motion: 15
50648513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3091
Checksum: 303
Coasting Arc #15 (Orbit 3106)
---------------------------------------
Vector Time (GMT): 2014/295/09:49:35
344
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3401847
76 A = 6789532
41 meter
Y = -3379890
39 meter E =
0006131
Z = 4805058
32 I = 51
57776
XDOT = 6583
336564 Wp = 38
58225
YDOT = 2962
609920 meter/sec RA = 187
82316 deg
ZDOT = -2570
450552 TA = 76
80157
MA = 76
73318
Ha = 225
509 n
mi
Hp = 221
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11160917
86 X = 3416047
68
Y = -11088879
24 feet Y = -3341768
78 meter
Z = 15764627
03 Z = 4821619
27
XDOT = 21598
873240 XDOT = 6562
205389
YDOT = 9719
848819 feet/sec YDOT = 3036
110614 meter/sec
ZDOT = -8433
236720 ZDOT = -2538
520565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11567798
25 X = -3525864
91
Y = 10558010
96 feet Y = 3218081
74 meter
Z = 15835632
09 Z = 4826700
66
XDOT = -20403
423480 XDOT = -6218
963477
YDOT = -9877
648723 feet/sec YDOT = -3010
707331 meter/sec
ZDOT = -8297
753654 ZDOT = -2529
155314
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
45333296
00016717 00000-0 10270-3 0 9148
2 25544 51
6456 188
7376 0002813 296
9441 63
1423 15
50679066 31073
Satellite: ISS
Catalog Number: 25544
Epoch time: 14295
45333296 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 188
7376 deg
Eccentricity:
0002813
Arg of perigee: 296
9441 deg
Mean anomaly: 63
1423 deg
Mean motion: 15
50679066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3107
Checksum: 325
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