[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 24th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18460 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
269/02:47:15
000 0
0 0
0 0
0
N/A 0
0 0
0 227
7
000/00:00:00
000 0
0 0
0 219
4
271/11:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
7
000/00:00:00
000 0
0 0
0 219
1
275/19:19:29
198 2
8 6
3 6
3
N/A -5
7 -0
0 227
7
000/00:14:58
396 0
2 0
3 222
9
Coasting Arc #1 (Orbit 995)
---------------------------------------
Vector Time (GMT): 2013/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3423418
23 A = 6793851
36 meter
Y = 4435565
17 meter E =
0014111
Z = 3832051
45 I = 51
53512
XDOT = -6315
938767 Wp = 80
47293
YDOT = -1272
160398 meter/sec RA = 340
57221 deg
ZDOT = -4154
551079 TA = 53
39131
MA = 53
26159
Ha = 227
779 n
mi
Hp = 219
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11231687
11 X = -3491378
54
Y = 14552379
18 feet Y = 4396902
73 meter
Z = 12572347
27 Z = 3815255
09
XDOT = -20721
583881 XDOT = -6281
061852
YDOT = -4173
754586 feet/sec YDOT = -1342
594640 meter/sec
ZDOT = -13630
416927 ZDOT = -4185
148851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10878062
70 X = 3315633
51
Y = -14878630
47 feet Y = -4535006
57 meter
Z = 12501222
27 Z = 3810372
55
XDOT = 19665
064137 XDOT = 5993
911549
YDOT = 2774
789111 feet/sec YDOT = 845
755721 meter/sec
ZDOT = -13758
557592 ZDOT = -4193
608354
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 13266
54045531
00016717 00000-0 10270-3 0 9002
2 25544 51
6507 340
9464 0002705 73
3387 286
8061 15
50470256 9961
Satellite: ISS
Catalog Number: 25544
Epoch time: 13266
54045531 = yrday
fracday
Element set: 900
Inclination: 51
6507 deg
RA of node: 340
9464 deg
Eccentricity:
0002705
Arg of perigee: 73
3387 deg
Mean anomaly: 286
8061 deg
Mean motion: 15
50470256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 996
Checksum: 307
Coasting Arc #2 (Orbit 1010)
---------------------------------------
Vector Time (GMT): 2013/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3528165
26 A = 6794874
38 meter
Y = -4646520
65 meter E =
0007671
Z = -3489333
22 I = 51
50907
XDOT = 6055
378052 Wp = 86
65735
YDOT = 1205
850182 meter/sec RA = 335
60703 deg
ZDOT = 4526
078833 TA = 232
36376
MA = 232
43340
Ha = 227
748 n
mi
Hp = 219
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11575345
34 X = 3596811
86
Y = -15244490
31 feet Y = -4606682
93 meter
Z = -11447943
65 Z = -3472026
40
XDOT = 19866
725893 XDOT = 6019
457223
YDOT = 3956
201384 feet/sec YDOT = 1273
364807 meter/sec
ZDOT = 14849
340002 ZDOT = 4555
408261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10924642
79 X = -3329831
12
Y = 15770481
49 feet Y = 4806842
76 meter
Z = -11374647
77 Z = -3466992
64
XDOT = -18786
737617 XDOT = -5726
197626
YDOT = -2236
820779 feet/sec YDOT = -681
782973 meter/sec
ZDOT = 14972
166941 ZDOT = 4563
516484
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 13267
50727206
00016717 00000-0 10270-3 0 9016
2 25544 51
6498 336
1542 0002750 77
9445 282
2014 15
50483448 10113
Satellite: ISS
Catalog Number: 25544
Epoch time: 13267
50727206 = yrday
fracday
Element set: 901
Inclination: 51
6498 deg
RA of node: 336
1542 deg
Eccentricity:
0002750
Arg of perigee: 77
9445 deg
Mean anomaly: 282
2014 deg
Mean motion: 15
50483448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1011
Checksum: 293
Coasting Arc #3 (Orbit 1026)
---------------------------------------
Vector Time (GMT): 2013/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3628589
04 A = 6795920
29 meter
Y = 4846675
00 meter E =
0015695
Z = 3072261
77 I = 51
48556
XDOT = -5778
399510 Wp = 92
40208
YDOT = -1213
702328 meter/sec RA = 330
63981 deg
ZDOT = -4889
061452 TA = 52
26523
MA = 52
12309
Ha = 227
720 n
mi
Hp = 219
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11904819
69 X = -3697440
28
Y = 15901164
71 feet Y = 4805713
08 meter
Z = 10079598
97 Z = 3054466
65
XDOT = -18958
003641 XDOT = -5740
648221
YDOT = -3981
963017 feet/sec YDOT = -1278
109362 meter/sec
ZDOT = -16040
227861 ZDOT = -4917
040836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10930260
36 X = 3331543
36
Y = -16631744
49 feet Y = -5069355
72 meter
Z = 10004227
61 Z = 3049288
57
XDOT = 17860
562194 XDOT = 5443
899357
YDOT = 1977
164662 feet/sec YDOT = 602
639789 meter/sec
ZDOT = -16157
388939 ZDOT = -4924
772149
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 13268
53852830
00016717 00000-0 10270-3 0 9023
2 25544 51
6501 331
0415 0002776 76
8831 283
2629 15
50518181 10279
Satellite: ISS
Catalog Number: 25544
Epoch time: 13268
53852830 = yrday
fracday
Element set: 902
Inclination: 51
6501 deg
RA of node: 331
0415 deg
Eccentricity:
0002776
Arg of perigee: 76
8831 deg
Mean anomaly: 283
2629 deg
Mean motion: 15
50518181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1027
Checksum: 296
Coasting Arc #4 (Orbit 1035)
---------------------------------------
Vector Time (GMT): 2013/269/02:47:15
000
Vector Time (MET): N/A
Weight (LBS) : 929266
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5011892
12 A = 6799240
52 meter
Y = -4402577
85 meter E =
0011308
Z = -1294373
39 I = 51
47784
XDOT = 4049
588765 Wp = 45
80594
YDOT = 2912
042811 meter/sec RA = 327
58866 deg
ZDOT = 5814
789559 TA = 300
10297
MA = 300
21503
Ha = 227
727 n
mi
Hp = 219
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16443215
63 X = 5067037
98
Y = -14444153
06 feet Y = -4346223
45 meter
Z = -4246631
87 Z = -1269891
62
XDOT = 13286
052378 XDOT = 3988
477814
YDOT = 9553
946231 feet/sec YDOT = 2956
986638 meter/sec
ZDOT = 19077
393565 ZDOT = 5834
313572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1022951
92 X = 311795
75
Y = -21882265
06 feet Y = -6669714
39 meter
Z = -4143286
76 Z = -1262873
80
XDOT = 14421
147903 XDOT = 4395
565881
YDOT = -2928
421577 feet/sec YDOT = -892
582897 meter/sec
ZDOT = 19158
833983 ZDOT = 5839
612598
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 13269
11860365
00016717 00000-0 10270-3 0 9031
2 25544 51
6479 328
1647 0002746 74
3775 285
7678 15
50492835 10362
Satellite: ISS
Catalog Number: 25544
Epoch time: 13269
11860365 = yrday
fracday
Element set: 903
Inclination: 51
6479 deg
RA of node: 328
1647 deg
Eccentricity:
0002746
Arg of perigee: 74
3775 deg
Mean anomaly: 285
7678 deg
Mean motion: 15
50492835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1036
Checksum: 337
Coasting Arc #5 (Orbit 1051)
---------------------------------------
Vector Time (GMT): 2013/270/02:47:15
000
Vector Time (MET): N/A
Weight (LBS) : 929266
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4972242
59 A = 6799501
19 meter
Y = 4565283
90 meter E =
0015124
Z = 764736
29 I = 51
45416
XDOT = -3752
120066 Wp = 118
27414
YDOT = -3079
378664 meter/sec RA = 322
62207 deg
ZDOT = -5930
171253 TA = 53
45040
MA = 53
31126
Ha = 227
622 n
mi
Hp = 219
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16313131
87 X = -5026637
95
Y = 14977965
56 feet Y = 4509377
05 meter
Z = 2508977
34 Z = 740448
99
XDOT = -12310
105205 XDOT = -3688
599600
YDOT = -10102
948372 feet/sec YDOT = -3120
982558 meter/sec
ZDOT = -19455
942431 ZDOT = -5948
244271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -159753
62 X = -48692
90
Y = 22157081
79 feet Y = 6753478
53 meter
Z = 2406428
14 Z = 733479
30
XDOT = -14085
071292 XDOT = -4293
129730
YDOT = 2050
391977 feet/sec YDOT = 624
959475 meter/sec
ZDOT = -19531
273282 ZDOT = -5953
132096
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 13270
14983738
00016717 00000-0 10270-3 0 9047
2 25544 51
6482 323
0521 0002817 74
9805 285
1657 15
50558482 10520
Satellite: ISS
Catalog Number: 25544
Epoch time: 13270
14983738 = yrday
fracday
Element set: 904
Inclination: 51
6482 deg
RA of node: 323
0521 deg
Eccentricity:
0002817
Arg of perigee: 74
9805 deg
Mean anomaly: 285
1657 deg
Mean motion: 15
50558482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1052
Checksum: 311
Coasting Arc #6 (Orbit 1066)
---------------------------------------
Vector Time (GMT): 2013/271/02:47:15
000
Vector Time (MET): N/A
Weight (LBS) : 929266
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4870432
67 A = 6799772
74 meter
Y = -4729371
51 meter E =
0013902
Z = -268981
51 I = 51
42988
XDOT = 3494
733503 Wp = 50
63386
YDOT = 3270
946889 meter/sec RA = 317
65244 deg
ZDOT = 5983
689381 TA = 306
46362
MA = 306
59167
Ha = 227
695 n
mi
Hp = 219
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15979109
80 X = 4924262
20
Y = -15516310
74 feet Y = -4674606
28 meter
Z = -882485
25 Z = -245190
15
XDOT = 11465
661098 XDOT = 3428
830075
YDOT = 10731
453048 feet/sec YDOT = 3309
659244 meter/sec
ZDOT = 19631
526840 ZDOT = 6000
506180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -851715
44 X = -259602
87
Y = -22260496
17 feet Y = -6784999
23 meter
Z = -781997
71 Z = -238352
90
XDOT = 13942
223375 XDOT = 4249
589685
YDOT = -1197
428320 feet/sec YDOT = -364
976152 meter/sec
ZDOT = 19701
562853 ZDOT = 6005
036358
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 13271
11660781
00016717 00000-0 10270-3 0 9056
2 25544 51
6471 318
2580 0002824 82
8234 277
3238 15
50533831 10676
Satellite: ISS
Catalog Number: 25544
Epoch time: 13271
11660781 = yrday
fracday
Element set: 905
Inclination: 51
6471 deg
RA of node: 318
2580 deg
Eccentricity:
0002824
Arg of perigee: 82
8234 deg
Mean anomaly: 277
3238 deg
Mean motion: 15
50533831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1067
Checksum: 296
Coasting Arc #7 (Orbit 1072)
---------------------------------------
Vector Time (GMT): 2013/271/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5676695
83 A = 6797423
53 meter
Y = 2946662
50 meter E =
0008076
Z = -2300840
32 I = 51
41688
XDOT = -620
672834 Wp = 118
22883
YDOT = -5396
369419 meter/sec RA = 315
88862 deg
ZDOT = -5397
985133 TA = 87
43103
MA = 87
33858
Ha = 227
688 n
mi
Hp = 219
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18624330
14 X = -5698047
25
Y = 9667527
89 feet Y = 2883062
49 meter
Z = -7548688
70 Z = -2328469
39
XDOT = -2036
328194 XDOT = -534
061285
YDOT = -17704
624079 feet/sec YDOT = -5402
826383 meter/sec
ZDOT = -17709
924976 ZDOT = -5400
789459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18929151
28 X = 5769605
31
Y = -8957926
84 feet Y = -2730376
10 meter
Z = -7665001
52 Z = -2336292
46
XDOT = 602
469556 XDOT = 183
632721
YDOT = 16385
798275 feet/sec YDOT = 4994
391314 meter/sec
ZDOT = -17720
878003 ZDOT = -5401
323615
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 13271
50331317
00016717 00000-0 10270-3 0 9060
2 25544 51
6497 316
3430 0003011 86
5702 273
5793 15
50556816 10736
Satellite: ISS
Catalog Number: 25544
Epoch time: 13271
50331317 = yrday
fracday
Element set: 906
Inclination: 51
6497 deg
RA of node: 316
3430 deg
Eccentricity:
0003011
Arg of perigee: 86
5702 deg
Mean anomaly: 273
5793 deg
Mean motion: 15
50556816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1073
Checksum: 290
Coasting Arc #8 (Orbit 1088)
---------------------------------------
Vector Time (GMT): 2013/272/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5461626
49 A = 6796469
00 meter
Y = -2953613
53 meter E =
0016487
Z = 2745956
30 I = 51
39173
XDOT = 486
447567 Wp = 80
91457
YDOT = 5683
513994 meter/sec RA = 310
91599 deg
ZDOT = 5121
964235 TA = 310
25598
MA = 310
40005
Ha = 227
693 n
mi
Hp = 219
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17918722
09 X = 5480909
38
Y = -9690333
10 feet Y = -2892430
06 meter
Z = 9009042
97 Z = 2772535
58
XDOT = 1595
956586 XDOT = 397
975934
YDOT = 18646
699457 feet/sec YDOT = 5688
459601 meter/sec
ZDOT = 16804
344602 ZDOT = 5124
111895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18058211
66 X = -5504142
91
Y = 9319619
54 feet Y = 2840620
04 meter
Z = 9120948
16 Z = 2780065
00
XDOT = -427
457145 XDOT = -130
288938
YDOT = -17357
929050 feet/sec YDOT = -5290
696774 meter/sec
ZDOT = 16812
508589 ZDOT = 5124
452618
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 13272
53451508
00016717 00000-0 10270-3 0 9070
2 25544 51
6492 311
2305 0003108 88
5940 271
5567 15
50557680 10893
Satellite: ISS
Catalog Number: 25544
Epoch time: 13272
53451508 = yrday
fracday
Element set: 907
Inclination: 51
6492 deg
RA of node: 311
2305 deg
Eccentricity:
0003108
Arg of perigee: 88
5940 deg
Mean anomaly: 271
5567 deg
Mean motion: 15
50557680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1089
Checksum: 307
Coasting Arc #9 (Orbit 1103)
---------------------------------------
Vector Time (GMT): 2013/273/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5255629
53 A = 6795159
30 meter
Y = 2877119
92 meter E =
0007708
Z = -3211288
97 I = 51
36911
XDOT = -368
499976 Wp = 95
24553
YDOT = -5980
395739 meter/sec RA = 305
94066 deg
ZDOT = -4765
582366 TA = 121
96267
MA = 121
88772
Ha = 227
664 n
mi
Hp = 218
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17242879
04 X = -5271811
89
Y = 9439369
81 feet Y = 2818257
28 meter
Z = -10535724
96 Z = -3236860
05
XDOT = -1208
989424 XDOT = -278
448514
YDOT = -19620
720929 feet/sec YDOT = -5984
013581 meter/sec
ZDOT = -15635
112748 ZDOT = -4767
153092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17209062
94 X = 5245322
38
Y = -9380117
90 feet Y = -2859059
94 meter
Z = -10643383
93 Z = -3244103
42
XDOT = 361
107074 XDOT = 110
065436
YDOT = 18370
678167 feet/sec YDOT = 5599
382705 meter/sec
ZDOT = -15640
822420 ZDOT = -4767
322673
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 13273
50125329
00016717 00000-0 10270-3 0 9088
2 25544 51
6499 306
4372 0003123 91
4802 268
6707 15
50601580 11047
Satellite: ISS
Catalog Number: 25544
Epoch time: 13273
50125329 = yrday
fracday
Element set: 908
Inclination: 51
6499 deg
RA of node: 306
4372 deg
Eccentricity:
0003123
Arg of perigee: 91
4802 deg
Mean anomaly: 268
6707 deg
Mean motion: 15
50601580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1104
Checksum: 289
Coasting Arc #10 (Orbit 1119)
---------------------------------------
Vector Time (GMT): 2013/274/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5032763
94 A = 6793999
22 meter
Y = -2778924
21 meter E =
0015128
Z = 3608180
28 I = 51
34667
XDOT = 316
434663 Wp = 93
71081
YDOT = 6283
770707 meter/sec RA = 300
96306 deg
ZDOT = 4381
328575 TA = 309
18823
MA = 309
32250
Ha = 227
643 n
mi
Hp = 219
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16511692
72 X = 5045936
79
Y = -9117205
41 feet Y = -2722570
52 meter
Z = 11837861
80 Z = 3632661
45
XDOT = 1038
171465 XDOT = 224
861238
YDOT = 20616
045626 feet/sec YDOT = 6286
797837 meter/sec
ZDOT = 14374
437583 ZDOT = 4382
642543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16310420
45 X = -4971416
15
Y = 9342313
07 feet Y = 2847537
02 meter
Z = 11940928
53 Z = 3639595
02
XDOT = -552
065043 XDOT = -168
269425
YDOT = -19412
708853 feet/sec YDOT = -5916
993658 meter/sec
ZDOT = 14379
036036 ZDOT = 4382
730184
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 13274
53242741
00016717 00000-0 10270-3 0 9091
2 25544 51
6487 301
3244 0003243 93
7267 266
4255 15
50603705 11202
Satellite: ISS
Catalog Number: 25544
Epoch time: 13274
53242741 = yrday
fracday
Element set: 909
Inclination: 51
6487 deg
RA of node: 301
3244 deg
Eccentricity:
0003243
Arg of perigee: 93
7267 deg
Mean anomaly: 266
4255 deg
Mean motion: 15
50603705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1120
Checksum: 287
Coasting Arc #11 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2013/275/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4836331
25 A = 6792602
58 meter
Y = 2598126
09 meter E =
0010042
Z = -4009864
64 I = 51
32832
XDOT = -286
369610 Wp = 79
48528
YDOT = -6568
977328 meter/sec RA = 295
98287 deg
ZDOT = -3917
472392 TA = 149
58032
MA = 149
52202
Ha = 227
623 n
mi
Hp = 218
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15867228
52 X = -4845545
65
Y = 8524035
72 feet Y = 2543991
06 meter
Z = -13155723
89 Z = -4033382
02
XDOT = -939
532840 XDOT = -193
862421
YDOT = -21551
762887 feet/sec YDOT = -6571
663021 meter/sec
ZDOT = -12852
599711 ZDOT = -3918
637918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15513371
11 X = 4728475
51
Y = -9008275
45 feet Y = -2745722
36 meter
Z = -13254715
66 Z = -4040037
33
XDOT = 870
490032 XDOT = 265
325362
YDOT = 20384
482952 feet/sec YDOT = 6213
190404 meter/sec
ZDOT = -12856
544435 ZDOT = -3918
674744
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 13275
49913910
00016717 00000-0 10270-3 0 9102
2 25544 51
6496 296
5309 0003182 97
1280 263
0233 15
50642275 11354
Satellite: ISS
Catalog Number: 25544
Epoch time: 13275
49913910 = yrday
fracday
Element set: 910
Inclination: 51
6496 deg
RA of node: 296
5309 deg
Eccentricity:
0003182
Arg of perigee: 97
1280 deg
Mean anomaly: 263
0233 deg
Mean motion: 15
50642275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1135
Checksum: 300
Coasting Arc #12 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2013/275/19:26:58
396
Vector Time (MET): N/A
Weight (LBS) : 938816
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2063883
38 A = 6793997
65 meter
Y = -4500906
70 meter E =
0008465
Z = -4660329
49 I = 51
31607
XDOT = 4849
289803 Wp = 115
17662
YDOT = -5184
209462 meter/sec RA = 294
26944 deg
ZDOT = 2859
863469 TA = 183
42179
MA = 183
42758
Ha = 227
655 n
mi
Hp = 222
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6771270
92 X = -1990761
05
Y = -14766754
27 feet Y = -4523578
19 meter
Z = -15289794
92 Z = -4670177
46
XDOT = 15909
743447 XDOT = 4893
007802
YDOT = -17008
561227 feet/sec YDOT = -5129
736759 meter/sec
ZDOT = 9382
754165 ZDOT = 2883
528019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8844442
46 X = 2695786
06
Y = -13580801
94 feet Y = -4139428
43 meter
Z = -15330447
69 Z = -4672720
46
XDOT = 21878
070689 XDOT = 6668
435946
YDOT = 3545
678509 feet/sec YDOT = 1080
722810 meter/sec
ZDOT = 9482
730627 ZDOT = 2890
336295
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 13275
82137641
00016717 00000-0 10270-3 0 9119
2 25544 51
6497 294
9336 0002259 267
4743 92
6148 15
49373763 11405
Satellite: ISS
Catalog Number: 25544
Epoch time: 13275
82137641 = yrday
fracday
Element set: 911
Inclination: 51
6497 deg
RA of node: 294
9336 deg
Eccentricity:
0002259
Arg of perigee: 267
4743 deg
Mean anomaly: 92
6148 deg
Mean motion: 15
49373763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 328
Coasting Arc #13 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2013/276/19:26:58
396
Vector Time (MET): N/A
Weight (LBS) : 938816
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2337031
14 A = 6794173
45 meter
Y = 4434630
44 meter E =
0006555
Z = 4583213
88 I = 51
30473
XDOT = -4459
307569 Wp = 56
93120
YDOT = 5459
442950 meter/sec RA = 289
29705 deg
ZDOT = -3001
959085 TA = 63
23543
MA = 63
16837
Ha = 227
534 n
mi
Hp = 222
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7667425
01 X = 2265004
15
Y = 14549312
47 feet Y = 4460362
57 meter
Z = 15036790
93 Z = 4594391
48
XDOT = -14630
274175 XDOT = -4505
441949
YDOT = 17911
558235 feet/sec YDOT = 5409
317736 meter/sec
ZDOT = -9848
947130 ZDOT = -3023
735130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7931775
24 X = -2417605
09
Y = 14358482
72 feet Y = 4376465
53 meter
Z = 15083033
40 Z = 4597308
58
XDOT = -21932
923614 XDOT = -6685
155118
YDOT = -1650
474414 feet/sec YDOT = -503
064601 meter/sec
ZDOT = -9941
033702 ZDOT = -3030
027072
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 13276
85336379
00016717 00000-0 10270-3 0 9123
2 25544 51
6492 289
8262 0002272 272
8223 87
2667 15
49406909 11561
Satellite: ISS
Catalog Number: 25544
Epoch time: 13276
85336379 = yrday
fracday
Element set: 912
Inclination: 51
6492 deg
RA of node: 289
8262 deg
Eccentricity:
0002272
Arg of perigee: 272
8223 deg
Mean anomaly: 87
2667 deg
Mean motion: 15
49406909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 338
Coasting Arc #14 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2013/277/19:26:58
396
Vector Time (MET): N/A
Weight (LBS) : 938816
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2623318
39 A = 6794417
08 meter
Y = -4353420
86 meter E =
0007454
Z = -4516452
12 I = 51
29692
XDOT = 4045
900016 Wp = 114
50397
YDOT = -5690
076986 meter/sec RA = 284
32298 deg
ZDOT = 3135
747494 TA = 187
15850
MA = 187
16915
Ha = 227
570 n
mi
Hp = 222
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8606687
64 X = -2552502
45
Y = -14282876
84 feet Y = -4382361
16 meter
Z = -14817756
31 Z = -4529023
54
XDOT = 13273
950183 XDOT = 4093
994144
YDOT = -18668
231580 feet/sec YDOT = -5644
563803 meter/sec
ZDOT = 10287
885478 ZDOT = 3155
520053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6930491
11 X = 2112413
69
Y = -15116122
19 feet Y = -4607394
04 meter
Z = -14869858
36 Z = -4532332
83
XDOT = 21764
504730 XDOT = 6633
821042
YDOT = -220
518036 feet/sec YDOT = -67
213897 meter/sec
ZDOT = 10371
595402 ZDOT = 3161
262279
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 13277
82083925
00016717 00000-0 10270-3 0 9138
2 25544 51
6497 285
0372 0002314 276
4827 83
6060 15
49415565 11715
Satellite: ISS
Catalog Number: 25544
Epoch time: 13277
82083925 = yrday
fracday
Element set: 913
Inclination: 51
6497 deg
RA of node: 285
0372 deg
Eccentricity:
0002314
Arg of perigee: 276
4827 deg
Mean anomaly: 83
6060 deg
Mean motion: 15
49415565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 317
Coasting Arc #15 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2013/278/19:26:58
396
Vector Time (MET): N/A
Weight (LBS) : 938816
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2891966
65 A = 6794607
64 meter
Y = 4265044
99 meter E =
0007362
Z = 4425210
11 I = 51
29118
XDOT = -3639
159848 Wp = 59
67254
YDOT = 5886
559616 meter/sec RA = 279
34871 deg
ZDOT = -3287
475690 TA = 63
72279
MA = 63
64716
Ha = 227
451 n
mi
Hp = 222
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9488079
57 X = 2822562
14
Y = 13992929
76 feet Y = 4296997
30 meter
Z = 14518405
87 Z = 4439090
17
XDOT = -11939
500813 XDOT = -3688
744196
YDOT = 19312
859631 feet/sec YDOT = 5845
586555 meter/sec
ZDOT = -10785
681398 ZDOT = -3305
275934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5919941
96 X = -1804398
31
Y = 15783030
43 feet Y = 4810667
68 meter
Z = 14576010
55 Z = 4442768
02
XDOT = -21464
015908 XDOT = -6542
232049
YDOT = 2003
167866 feet/sec YDOT = 610
565566 meter/sec
ZDOT = -10861
142890 ZDOT = -3310
476353
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 13278
85279881
00016717 00000-0 10270-3 0 9141
2 25544 51
6496 279
9293 0002338 282
2503 77
8385 15
49460205 11873
Satellite: ISS
Catalog Number: 25544
Epoch time: 13278
85279881 = yrday
fracday
Element set: 914
Inclination: 51
6496 deg
RA of node: 279
9293 deg
Eccentricity:
0002338
Arg of perigee: 282
2503 deg
Mean anomaly: 77
8385 deg
Mean motion: 15
49460205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 348
Coasting Arc #16 (Orbit 1201)
---------------------------------------
Vector Time (GMT): 2013/279/19:26:58
396
Vector Time (MET): N/A
Weight (LBS) : 938816
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3174092
50 A = 6794919
01 meter
Y = -4156965
66 meter E =
0006331
Z = -4344282
65 I = 51
28856
XDOT = 3218
282724 Wp = 112
55472
YDOT = -6039
278795 meter/sec RA = 274
37350 deg
ZDOT = 3429
120678 TA = 192
47611
MA = 192
49179
Ha = 227
500 n
mi
Hp = 222
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10413689
31 X = -3106268
68
Y = -13638338
79 feet Y = -4192081
63 meter
Z = -14252895
84 Z = -4359537
25
XDOT = 10558
670353 XDOT = 3268
917969
YDOT = -19813
906809 feet/sec YDOT = -6003
006423 meter/sec
ZDOT = 11250
395925 ZDOT = 3444
878789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4810586
86 X = 1466266
87
Y = -16416350
55 feet Y = -5003703
65 meter
Z = -14316282
29 Z = -4363602
84
XDOT = 20966
107053 XDOT = 6390
469430
YDOT = -3721
040115 feet/sec YDOT = -1134
173027 meter/sec
ZDOT = 11317
312330 ZDOT = 3449
516798
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 13279
82024825
00016717 00000-0 10270-3 0 9156
2 25544 51
6500 275
1401 0002409 284
8872 75
2011 15
49459211 12025
Satellite: ISS
Catalog Number: 25544
Epoch time: 13279
82024825 = yrday
fracday
Element set: 915
Inclination: 51
6500 deg
RA of node: 275
1401 deg
Eccentricity:
0002409
Arg of perigee: 284
8872 deg
Mean anomaly: 75
2011 deg
Mean motion: 15
49459211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1202
Checksum: 285
Coasting Arc #17 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2013/280/19:26:58
396
Vector Time (MET): N/A
Weight (LBS) : 938816
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3438403
30 A = 6795131
27 meter
Y = 4045571
32 meter E =
0008162
Z = 4236866
20 I = 51
28864
XDOT = -2811
820744 Wp = 63
29240
YDOT = 6157
666707 meter/sec RA = 269
39858 deg
ZDOT = -3588
751801 TA = 63
63911
MA = 63
55533
Ha = 227
393 n
mi
Hp = 222
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11280850
71 X = 3372327
27
Y = 13272871
80 feet Y = 4083652
65 meter
Z = 13900479
65 Z = 4253409
17
XDOT = -9225
133673 XDOT = -2863
034569
YDOT = 20202
318592 feet/sec YDOT = 6125
936473 meter/sec
ZDOT = -11774
120082 ZDOT = -3602
536611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3708087
35 X = -1130225
03
Y = 16963464
52 feet Y = 5170463
99 meter
Z = 13969288
19 Z = 4257839
04
XDOT = -20358
672422 XDOT = -6205
323354
YDOT = 5318
090718 feet/sec YDOT = 1620
954051 meter/sec
ZDOT = -11832
776618 ZDOT = -3606
630313
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 13280
85217920
00016717 00000-0 10270-3 0 9162
2 25544 51
6502 270
0321 0002443 290
7949 69
2940 15
49513514 12189
Satellite: ISS
Catalog Number: 25544
Epoch time: 13280
85217920 = yrday
fracday
Element set: 916
Inclination: 51
6502 deg
RA of node: 270
0321 deg
Eccentricity:
0002443
Arg of perigee: 290
7949 deg
Mean anomaly: 69
2940 deg
Mean motion: 15
49513514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 295
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