[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 1st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
128/06:37:46
185 2
8 4
1 4
1
N/A -0
8 -0
4 223
9
000/00:13:32
371 2
9 0
1 222
8
137/01:53:25
082 -3
0 4
5 4
5
N/A -0
4 -0
2 226
1
000/00:14:50
163 -3
3 -0
1 223
7
Coasting Arc #1 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2013/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4004824
18 A = 6786428
72 meter
Y = -2595059
88 meter E =
0005075
Z = -4828937
81 I = 51
51276
XDOT = 5812
812699 Wp = 104
99301
YDOT = -4315
676505 meter/sec RA = 339
37655 deg
ZDOT = -2505
045251 TA = 140
33299
MA = 140
29586
Ha = 224
428 n
mi
Hp = 220
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13139186
93 X = -3952050
22
Y = -8513975
98 feet Y = -2639549
20 meter
Z = -15842971
82 Z = -4848264
84
XDOT = 19070
907804 XDOT = 5872
808389
YDOT = -14159
043652 feet/sec YDOT = -4250
338478 meter/sec
ZDOT = -8218
652399 ZDOT = -2476
661326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15499955
83 X = -4724386
54
Y = 1526261
38 feet Y = 465204
47 meter
Z = -15923180
32 Z = -4853385
36
XDOT = 6154
363324 XDOT = 1875
849941
YDOT = -21882
783924 feet/sec YDOT = -6669
872540 meter/sec
ZDOT = -8099
677231 ZDOT = -2468
781620
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 13121
52045618
00016717 00000-0 10270-3 0 9006
2 25544 51
6474 339
8036 0007949 232
0515 127
9918 15
51704712 27467
Satellite: ISS
Catalog Number: 25544
Epoch time: 13121
52045618 = yrday
fracday
Element set: 900
Inclination: 51
6474 deg
RA of node: 339
8036 deg
Eccentricity:
0007949
Arg of perigee: 232
0515 deg
Mean anomaly: 127
9918 deg
Mean motion: 15
51704712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 307
Coasting Arc #2 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2013/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3340505
15 A = 6785192
11 meter
Y = 2929180
05 meter E =
0007636
Z = 5132202
69 I = 51
48042
XDOT = -6148
075711 Wp = 199
53625
YDOT = 4304
533872 meter/sec RA = 334
39385 deg
ZDOT = 1538
551727 TA = 235
55474
MA = 235
62692
Ha = 224
291 n
mi
Hp = 220
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10959662
58 X = 3282571
20
Y = 9610170
77 feet Y = 2966211
77 meter
Z = 16837935
35 Z = 5148289
91
XDOT = -20170
852070 XDOT = -6203
226892
YDOT = 14122
486456 feet/sec YDOT = 4235
473851 meter/sec
ZDOT = 5047
741885 ZDOT = 1508
550828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14492067
83 X = 4417182
28
Y = 447808
31 feet Y = 136491
97 meter
Z = 16904587
86 Z = 5152518
38
XDOT = -6467
781590 XDOT = -1971
379829
YDOT = 22719
376166 feet/sec YDOT = 6924
865855 meter/sec
ZDOT = 4922
032426 ZDOT = 1500
235483
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 13122
55089255
00016717 00000-0 10270-3 0 9016
2 25544 51
6477 334
6856 0007857 235
4832 124
5578 15
51695553 27625
Satellite: ISS
Catalog Number: 25544
Epoch time: 13122
55089255 = yrday
fracday
Element set: 901
Inclination: 51
6477 deg
RA of node: 334
6856 deg
Eccentricity:
0007857
Arg of perigee: 235
4832 deg
Mean anomaly: 124
5578 deg
Mean motion: 15
51695553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2762
Checksum: 335
Coasting Arc #3 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2013/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2639482
98 A = 6784347
80 meter
Y = -3337345
86 meter E =
0008472
Z = -5290820
08 I = 51
44943
XDOT = 6363
149878 Wp = 111
08689
YDOT = -4232
681701 meter/sec RA = 329
40624 deg
ZDOT = -508
197978 TA = 154
06743
MA = 154
02495
Ha = 224
037 n
mi
Hp = 220
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8659721
06 X = -2576266
37
Y = -10949297
45 feet Y = -3366508
86 meter
Z = -17358333
58 Z = -5303488
90
XDOT = 20876
475977 XDOT = 6412
476410
YDOT = -13886
750987 feet/sec YDOT = -4161
249157 meter/sec
ZDOT = -1667
316202 ZDOT = -477
166303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13626464
26 X = -4153346
31
Y = -2716151
11 feet Y = -827882
86 meter
Z = -17410675
55 Z = -5306773
91
XDOT = 6565
259838 XDOT = 2001
091199
YDOT = -23158
839479 feet/sec YDOT = -7058
814273 meter/sec
ZDOT = -1537
327499 ZDOT = -468
577422
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 13123
51691179
00016717 00000-0 10270-3 0 9028
2 25544 51
6462 329
8863 0007937 239
5158 120
5210 15
51753003 27778
Satellite: ISS
Catalog Number: 25544
Epoch time: 13123
51691179 = yrday
fracday
Element set: 902
Inclination: 51
6462 deg
RA of node: 329
8863 deg
Eccentricity:
0007937
Arg of perigee: 239
5158 deg
Mean anomaly: 120
5210 deg
Mean motion: 15
51753003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 310
Coasting Arc #4 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2013/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1961933
38 A = 6784410
39 meter
Y = 3779598
67 meter E =
0005131
Z = 5285140
56 I = 51
42387
XDOT = -6454
352495 Wp = 240
82628
YDOT = 4093
697149 meter/sec RA = 324
41780 deg
ZDOT = -534
433747 TA = 214
27611
MA = 214
30923
Ha = 223
871 n
mi
Hp = 221
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6436789
32 X = 1893849
28
Y = 12400258
11 feet Y = 3801157
72 meter
Z = 17339700
01 Z = 5294506
06
XDOT = -21175
697161 XDOT = -6497
053234
YDOT = 13430
764925 feet/sec YDOT = 4021
281741 meter/sec
ZDOT = -1753
391560 ZDOT = -565
892516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12977809
01 X = 3955636
19
Y = 5043633
47 feet Y = 1537299
48 meter
Z = 17378207
30 Z = 5296877
58
XDOT = -6490
279740 XDOT = -1978
237265
YDOT = 23163
458009 feet/sec YDOT = 7060
222001 meter/sec
ZDOT = -1885
131988 ZDOT = -574
588230
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 13124
54732107
00016717 00000-0 10270-3 0 9030
2 25544 51
6465 324
7686 0007983 243
2966 116
7368 15
51743550 27933
Satellite: ISS
Catalog Number: 25544
Epoch time: 13124
54732107 = yrday
fracday
Element set: 903
Inclination: 51
6465 deg
RA of node: 324
7686 deg
Eccentricity:
0007983
Arg of perigee: 243
2966 deg
Mean anomaly: 116
7368 deg
Mean motion: 15
51743550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2793
Checksum: 327
Coasting Arc #5 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2013/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1298529
18 A = 6785033
55 meter
Y = -4267834
16 meter E =
0008419
Z = -5118914
56 I = 51
40054
XDOT = 6430
389202 Wp = 135
20162
YDOT = -3850
990101 meter/sec RA = 319
42572 deg
ZDOT = 1575
233404 TA = 150
08029
MA = 150
03215
Ha = 223
660 n
mi
Hp = 221
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4260266
34 X = -1225842
22
Y = -14002080
57 feet Y = -4281948
87 meter
Z = -16794339
12 Z = -5125046
10
XDOT = 21097
077435 XDOT = 6465
321723
YDOT = -12634
481960 feet/sec YDOT = -3778
886069 meter/sec
ZDOT = 5168
088595 ZDOT = 1606
557008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12552254
18 X = -3825927
07
Y = -7470620
28 feet Y = -2277045
06 meter
Z = -16819295
58 Z = -5126521
29
XDOT = 6364
564811 XDOT = 1939
919354
YDOT = -22655
957242 feet/sec YDOT = -6905
535767 meter/sec
ZDOT = 5299
222254 ZDOT = 1615
202943
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 13125
51331627
00016717 00000-0 10270-3 0 9041
2 25544 51
6451 319
9686 0007952 246
6793 113
3522 15
51790734 28083
Satellite: ISS
Catalog Number: 25544
Epoch time: 13125
51331627 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 319
9686 deg
Eccentricity:
0007952
Arg of perigee: 246
6793 deg
Mean anomaly: 113
3522 deg
Mean motion: 15
51790734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2808
Checksum: 318
Coasting Arc #6 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2013/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 692640
63 A = 6786411
97 meter
Y = 4758663
96 meter E =
0001424
Z = 4789932
78 I = 51
38257
XDOT = -6311
149548 Wp = 309
91000
YDOT = 3505
240118 meter/sec RA = 314
43547 deg
ZDOT = -2569
356900 TA = 165
50513
MA = 165
50105
Ha = 223
436 n
mi
Hp = 221
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2272443
02 X = 616108
18
Y = 15612414
58 feet Y = 4765981
70 meter
Z = 15715002
57 Z = 4793111
62
XDOT = -20705
871219 XDOT = -6337
395390
YDOT = 11500
131620 feet/sec YDOT = 3434
518057 meter/sec
ZDOT = -8429
648621 ZDOT = -2600
080220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12358857
70 X = 3766979
83
Y = 9786450
40 feet Y = 2982910
08 meter
Z = 15727581
41 Z = 4793766
81
XDOT = -6275
582791 XDOT = -1912
797635
YDOT = 21680
910036 feet/sec YDOT = 6608
341379 meter/sec
ZDOT = -8558
223428 ZDOT = -2608
546501
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 13126
54369826
00016717 00000-0 10270-3 0 9058
2 25544 51
6451 314
8506 0008052 250
9403 109
0876 15
51792203 28241
Satellite: ISS
Catalog Number: 25544
Epoch time: 13126
54369826 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 314
8506 deg
Eccentricity:
0008052
Arg of perigee: 250
9403 deg
Mean anomaly: 109
0876 deg
Mean motion: 15
51792203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 303
Coasting Arc #7 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2013/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -140419
21 A = 6788192
65 meter
Y = -5247685
54 meter E =
0005158
Z = -4307179
22 I = 51
36724
XDOT = 6107
419863 Wp = 176
32335
YDOT = -3032
456223 meter/sec RA = 309
44389 deg
ZDOT = 3490
691218 TA = 129
38510
MA = 129
33940
Ha = 223
236 n
mi
Hp = 221
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -460692
96 X = -60804
52
Y = -17216816
08 feet Y = -5248810
69 meter
Z = -14131165
40 Z = -4307667
94
XDOT = 20037
466741 XDOT = 6123
918363
YDOT = -9949
003355 feet/sec YDOT = -2964
066922 meter/sec
ZDOT = 11452
399010 ZDOT = 3520
401181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12372153
17 X = -3771032
29
Y = -11980157
19 feet Y = -3651551
91 meter
Z = -14132462
25 Z = -4307574
49
XDOT = 6328
430706 XDOT = 1928
905679
YDOT = -20210
633413 feet/sec YDOT = -6160
201064 meter/sec
ZDOT = 11576
677278 ZDOT = 3528
571234
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 13127
50966914
00016717 00000-0 10270-3 0 9067
2 25544 51
6444 310
0504 0007939 253
8637 106
1641 15
51825422 28397
Satellite: ISS
Catalog Number: 25544
Epoch time: 13127
50966914 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 310
0504 deg
Eccentricity:
0007939
Arg of perigee: 253
8637 deg
Mean anomaly: 106
1641 deg
Mean motion: 15
51825422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 308
Coasting Arc #8 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2013/128/06:44:32
371
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3385810
87 A = 6798081
88 meter
Y = -5832883
56 meter E =
0009673
Z = -799758
20 I = 51
38254
XDOT = 4519
181783 Wp = 341
51737
YDOT = 1810
069347 meter/sec RA = 305
56917 deg
ZDOT = 5920
034622 TA = 9
81436
MA = 9
79548
Ha = 223
928 n
mi
Hp = 222
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11108303
38 X = 3454668
87
Y = -19136757
10 feet Y = -5794636
28 meter
Z = -2623878
61 Z = -783142
66
XDOT = 14826
711888 XDOT = 4469
846807
YDOT = 5938
547725 feet/sec YDOT = 1860
329818 meter/sec
ZDOT = 19422
685767 ZDOT = 5941
869020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19824300
40 X = 6042446
76
Y = -9847327
92 feet Y = -3001465
55 meter
Z = -2553793
53 Z = -778396
27
XDOT = 8286
170585 XDOT = 2525
624794
YDOT = 11611
466283 feet/sec YDOT = 3539
174923 meter/sec
ZDOT = 19513
449034 ZDOT = 5947
699266
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 13128
28243693
00016717 00000-0 10270-3 0 9076
2 25544 51
6491 306
2145 0009710 277
4552 82
5495 15
51034481 28519
Satellite: ISS
Catalog Number: 25544
Epoch time: 13128
28243693 = yrday
fracday
Element set: 907
Inclination: 51
6491 deg
RA of node: 306
2145 deg
Eccentricity:
0009710
Arg of perigee: 277
4552 deg
Mean anomaly: 82
5495 deg
Mean motion: 15
51034481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 309
Coasting Arc #9 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2013/129/06:44:32
371
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3378806
21 A = 6798385
83 meter
Y = 5892990
87 meter E =
0006699
Z = 113575
91 I = 51
36650
XDOT = -4200
099283 Wp = 185
46434
YDOT = -2293
528038 meter/sec RA = 300
59392 deg
ZDOT = -5984
030568 TA = 353
30938
MA = 353
31832
Ha = 224
316 n
mi
Hp = 222
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11085322
22 X = -3445003
51
Y = 19333959
55 feet Y = 5854836
80 meter
Z = 372624
38 Z = 97000
96
XDOT = -13779
853291 XDOT = -4145
070981
YDOT = -7524
698288 feet/sec YDOT = -2340
188385 meter/sec
ZDOT = -19632
646220 ZDOT = -6004
301089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19726510
82 X = -6012640
50
Y = 10372962
54 feet Y = 3161678
98 meter
Z = 302702
03 Z = 92263
58
XDOT = -6735
814407 XDOT = -2053
076231
YDOT = -12238
499310 feet/sec YDOT = -3730
294590 meter/sec
ZDOT = -19716
822173 ZDOT = -6009
687398
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 13129
31332268
00016717 00000-0 10270-3 0 9089
2 25544 51
6492 301
0997 0009711 280
6859 79
3198 15
51016305 28671
Satellite: ISS
Catalog Number: 25544
Epoch time: 13129
31332268 = yrday
fracday
Element set: 908
Inclination: 51
6492 deg
RA of node: 301
0997 deg
Eccentricity:
0009711
Arg of perigee: 280
6859 deg
Mean anomaly: 79
3198 deg
Mean motion: 15
51016305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 324
Coasting Arc #10 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2013/130/06:44:32
371
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3339762
84 A = 6798073
37 meter
Y = -5883704
46 meter E =
0010811
Z = 584838
67 I = 51
35143
XDOT = 3925
285824 Wp = 3
77079
YDOT = 2819
135866 meter/sec RA = 295
61663 deg
ZDOT = 5950
273065 TA = 2
56032
MA = 2
55479
Ha = 224
582 n
mi
Hp = 222
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10957227
17 X = 3402466
42
Y = -19303492
31 feet Y = -5846006
55 meter
Z = 1918762
04 Z = 601215
35
XDOT = 12878
234332 XDOT = 3864
564492
YDOT = 9249
133418 feet/sec YDOT = 2862
691140 meter/sec
ZDOT = 19521
893259 ZDOT = 5969
194762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19407823
09 X = 5915504
48
Y = -10758816
15 feet Y = -3279287
16 meter
Z = 1987855
23 Z = 605898
28
XDOT = 5273
626293 XDOT = 1607
401294
YDOT = 13132
047230 feet/sec YDOT = 4002
647996 meter/sec
ZDOT = 19600
374310 ZDOT = 5974
194090
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 13130
34419333
00016717 00000-0 10270-3 0 9094
2 25544 51
6494 295
9839 0009848 285
8411 74
1655 15
51072985 28836
Satellite: ISS
Catalog Number: 25544
Epoch time: 13130
34419333 = yrday
fracday
Element set: 909
Inclination: 51
6494 deg
RA of node: 295
9839 deg
Eccentricity:
0009848
Arg of perigee: 285
8411 deg
Mean anomaly: 74
1655 deg
Mean motion: 15
51072985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 344
Coasting Arc #11 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2013/131/06:44:32
371
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3279309
34 A = 6797569
26 meter
Y = 5812386
34 meter E =
0005536
Z = -1274982
09 I = 51
33739
XDOT = -3697
723504 Wp = 225
30395
YDOT = -3362
488537 meter/sec RA = 290
63911 deg
ZDOT = -5806
433038 TA = 328
60163
MA = 328
63467
Ha = 224
871 n
mi
Hp = 222
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10758888
90 X = -3337867
33
Y = 19069509
00 feet Y = 5775387
69 meter
Z = -4183012
10 Z = -1291054
90
XDOT = -12131
638792 XDOT = -3631
641996
YDOT = -11031
786539 feet/sec YDOT = -3403
469015 meter/sec
ZDOT = -19049
977159 ZDOT = -5824
236257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18918168
49 X = -5766257
76
Y = 10996855
08 feet Y = 3351841
43 meter
Z = -4250827
34 Z = -1295652
17
XDOT = -3960
919855 XDOT = -1207
288372
YDOT = -14221
021049 feet/sec YDOT = -4334
567216 meter/sec
ZDOT = -19123
723004 ZDOT = -5828
910772
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 13131
31062428
00016717 00000-0 10270-3 0 9103
2 25544 51
6496 291
1890 0009902 288
5890 71
4186 15
51054370 28988
Satellite: ISS
Catalog Number: 25544
Epoch time: 13131
31062428 = yrday
fracday
Element set: 910
Inclination: 51
6496 deg
RA of node: 291
1890 deg
Eccentricity:
0009902
Arg of perigee: 288
5890 deg
Mean anomaly: 71
4186 deg
Mean motion: 15
51054370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 315
Coasting Arc #12 (Orbit 2913)
---------------------------------------
Vector Time (GMT): 2013/132/06:44:32
371
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3209093
93 A = 6796481
04 meter
Y = -5655670
47 meter E =
0009968
Z = 1953257
87 I = 51
32420
XDOT = 3525
665419 Wp = 21
81318
YDOT = 3921
972917 meter/sec RA = 285
65862 deg
ZDOT = 5563
537051 TA = 359
80944
MA = 359
80982
Ha = 225
051 n
mi
Hp = 222
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10528523
41 X = 3262609
79
Y = -18555349
31 feet Y = -5619485
26 meter
Z = 6408326
33 Z = 1968977
24
XDOT = 11567
143762 XDOT = 3454
520437
YDOT = 12867
365214 feet/sec YDOT = 3961
000979 meter/sec
ZDOT = 18253
074315 ZDOT = 5580
492140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18260632
82 X = 5565840
88
Y = -10992984
37 feet Y = -3350661
64 meter
Z = 6474644
62 Z = 1973471
68
XDOT = 2838
589699 XDOT = 865
202140
YDOT = 15507
398089 feet/sec YDOT = 4726
654938 meter/sec
ZDOT = 18323
211840 ZDOT = 5584
914969
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 13132
34146974
00016717 00000-0 10270-3 0 9117
2 25544 51
6494 286
0730 0010013 293
8724 66
1378 15
51107474 29149
Satellite: ISS
Catalog Number: 25544
Epoch time: 13132
34146974 = yrday
fracday
Element set: 911
Inclination: 51
6494 deg
RA of node: 286
0730 deg
Eccentricity:
0010013
Arg of perigee: 293
8724 deg
Mean anomaly: 66
1378 deg
Mean motion: 15
51107474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2914
Checksum: 300
Coasting Arc #13 (Orbit 2928)
---------------------------------------
Vector Time (GMT): 2013/133/06:44:32
371
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3141284
92 A = 6795240
71 meter
Y = 5436223
74 meter E =
0005205
Z = -2596988
28 I = 51
31241
XDOT = -3405
593362 Wp = 286
42547
YDOT = -4462
445575 meter/sec RA = 280
67761 deg
ZDOT = -5211
618419 TA = 282
89362
MA = 282
95175
Ha = 225
320 n
mi
Hp = 221
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10306052
88 X = -3189224
83
Y = 17835379
72 feet Y = 5400828
04 meter
Z = -8520302
76 Z = -2612364
64
XDOT = -11173
206567 XDOT = -3330
123247
YDOT = -14640
569473 feet/sec YDOT = -4500
106732 meter/sec
ZDOT = -17098
485627 ZDOT = -5227
979702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17518358
16 X = -5339595
57
Y = 10784861
61 feet Y = 3287225
82 meter
Z = -8585158
25 Z = -2616756
23
XDOT = -1957
190286 XDOT = -596
551599
YDOT = -16870
356286 feet/sec YDOT = -5142
084596 meter/sec
ZDOT = -17166
080044 ZDOT = -5232
221197
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 13133
30787606
00016717 00000-0 10270-3 0 9128
2 25544 51
6491 281
2781 0010093 296
7319 63
2798 15
51105106 29299
Satellite: ISS
Catalog Number: 25544
Epoch time: 13133
30787606 = yrday
fracday
Element set: 912
Inclination: 51
6491 deg
RA of node: 281
2781 deg
Eccentricity:
0010093
Arg of perigee: 296
7319 deg
Mean anomaly: 63
2798 deg
Mean motion: 15
51105106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2929
Checksum: 311
Coasting Arc #14 (Orbit 2944)
---------------------------------------
Vector Time (GMT): 2013/134/06:44:32
371
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3090159
65 A = 6793653
46 meter
Y = -5125774
27 meter E =
0007299
Z = 3203722
74 I = 51
30229
XDOT = 3338
625381 Wp = 33
95767
YDOT = 4990
588121 meter/sec RA = 275
69294 deg
ZDOT = 4765
048050 TA = 3
24759
MA = 3
24285
Ha = 225
477 n
mi
Hp = 221
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10138319
05 X = 3131684
50
Y = -16816844
70 feet Y = -5090986
19 meter
Z = 10510901
38 Z = 3218835
14
XDOT = 10953
495344 XDOT = 3259
423849
YDOT = 16373
320606 feet/sec YDOT = 5027
479573 meter/sec
ZDOT = 15633
359745 ZDOT = 4781
074928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16700157
05 X = 5090207
87
Y = -10264170
36 feet Y = -3128519
12 meter
Z = 10574610
55 Z = 3223141
30
XDOT = 1319
968038 XDOT = 402
326258
YDOT = 18319
706999 feet/sec YDOT = 5583
846693 meter/sec
ZDOT = 15699
496674 ZDOT = 4785
206586
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 13134
33869677
00016717 00000-0 10270-3 0 9132
2 25544 51
6487 276
1619 0010165 301
7637 58
2523 15
51135002 29453
Satellite: ISS
Catalog Number: 25544
Epoch time: 13134
33869677 = yrday
fracday
Element set: 913
Inclination: 51
6487 deg
RA of node: 276
1619 deg
Eccentricity:
0010165
Arg of perigee: 301
7637 deg
Mean anomaly: 58
2523 deg
Mean motion: 15
51135002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2945
Checksum: 309
Coasting Arc #15 (Orbit 2959)
---------------------------------------
Vector Time (GMT): 2013/135/06:44:32
371
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3064022
57 A = 6791985
17 meter
Y = 4765480
02 meter E =
0007572
Z = -3749969
77 I = 51
29382
XDOT = -3315
919480 Wp = 339
79611
YDOT = -5461
712499 meter/sec RA = 270
70737 deg
ZDOT = -4221
859807 TA = 245
21864
MA = 245
29744
Ha = 225
702 n
mi
Hp = 221
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10052567
47 X = -3098866
96
Y = 15634776
98 feet Y = 4731021
59 meter
Z = -12303050
42 Z = -3764938
99
XDOT = -10879
000918 XDOT = -3234
090157
YDOT = -17919
004262 feet/sec YDOT = -5498
335409 meter/sec
ZDOT = -13851
246086 ZDOT = -4237
769961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15906689
63 X = -4848359
00
Y = 9535301
01 feet Y = 2906359
75 meter
Z = -12366109
87 Z = -3769190
29
XDOT = -962
059454 XDOT = -293
235721
YDOT = -19693
721237 feet/sec YDOT = -6002
646233 meter/sec
ZDOT = -13916
843295 ZDOT = -4241
853836
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 13135
30507838
00016717 00000-0 10270-3 0 9149
2 25544 51
6477 271
3666 0010206 304
7946 55
2244 15
51157469 29608
Satellite: ISS
Catalog Number: 25544
Epoch time: 13135
30507838 = yrday
fracday
Element set: 914
Inclination: 51
6477 deg
RA of node: 271
3666 deg
Eccentricity:
0010206
Arg of perigee: 304
7946 deg
Mean anomaly: 55
2244 deg
Mean motion: 15
51157469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2960
Checksum: 311
Coasting Arc #16 (Orbit 2975)
---------------------------------------
Vector Time (GMT): 2013/136/06:44:32
371
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3079807
81 A = 6790328
84 meter
Y = -4319844
25 meter E =
0004035
Z = 4234347
62 I = 51
28862
XDOT = 3329
664989 Wp = 24
24089
YDOT = 5894
150379 meter/sec RA = 265
71829 deg
ZDOT = 3593
754271 TA = 28
83548
MA = 28
81319
Ha = 225
865 n
mi
Hp = 221
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10104356
32 X = 3107314
87
Y = -14172717
36 feet Y = -4285250
32 meter
Z = 13892216
61 Z = 4249375
75
XDOT = 10924
097734 XDOT = 3246
050248
YDOT = 19337
763709 feet/sec YDOT = 5930
917089 meter/sec
ZDOT = 11790
532385 ZDOT = 3609
726812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15147991
50 X = 4617107
81
Y = -8470015
71 feet Y = -2581660
79 meter
Z = 13955457
84 Z = 4253623
55
XDOT = 838
974462 XDOT = 255
719416
YDOT = 21022
456870 feet/sec YDOT = 6407
644854 meter/sec
ZDOT = 11856
343954 ZDOT = 3613
813637
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 13136
33587430
00016717 00000-0 10270-3 0 9150
2 25544 51
6474 266
2501 0010251 309
4803 50
5440 15
51157605 29765
Satellite: ISS
Catalog Number: 25544
Epoch time: 13136
33587430 = yrday
fracday
Element set: 915
Inclination: 51
6474 deg
RA of node: 266
2501 deg
Eccentricity:
0010251
Arg of perigee: 309
4803 deg
Mean anomaly: 50
5440 deg
Mean motion: 15
51157605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2976
Checksum: 289
Coasting Arc #17 (Orbit 2987)
---------------------------------------
Vector Time (GMT): 2013/137/02:00:50
163
Vector Time (MET): N/A
Weight (LBS) : 904105
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1957205
15 A = 6795562
47 meter
Y = 5540421
09 meter E =
0004547
Z = -3414055
83 I = 51
30080
XDOT = -4335
444669 Wp = 314
22649
YDOT = -4353
247552 meter/sec RA = 261
71545 deg
ZDOT = -4572
234803 TA = 265
84273
MA = 265
89470
Ha = 226
085 n
mi
Hp = 223
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6421276
74 X = -2002429
19
Y = 18177234
53 feet Y = 5518281
67 meter
Z = -11200970
57 Z = -3423673
43
XDOT = -14223
899834 XDOT = -4264
232660
YDOT = -14282
308240 feet/sec YDOT = -4401
330862 meter/sec
ZDOT = -15000
770352 ZDOT = -4593
123370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17460579
27 X = -5321984
56
Y = -8115188
64 feet Y = -2473509
50 meter
Z = -11241809
31 Z = -3426503
48
XDOT = 15016
844216 XDOT = 4577
134117
YDOT = -11378
689856 feet/sec YDOT = -3468
224668 meter/sec
ZDOT = -15087
295765 ZDOT = -4598
607749
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 13137
10897905
00016717 00000-0 10270-3 0 9168
2 25544 51
6482 262
4147 0008730 291
1333 68
8884 15
50288796 29884
Satellite: ISS
Catalog Number: 25544
Epoch time: 13137
10897905 = yrday
fracday
Element set: 916
Inclination: 51
6482 deg
RA of node: 262
4147 deg
Eccentricity:
0008730
Arg of perigee: 291
1333 deg
Mean anomaly: 68
8884 deg
Mean motion: 15
50288796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2988
Checksum: 346
Coasting Arc #18 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2013/138/02:00:50
163
Vector Time (MET): N/A
Weight (LBS) : 904105
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1811897
74 A = 6794572
44 meter
Y = -5371733
57 meter E =
0004378
Z = 3740060
28 I = 51
30238
XDOT = 4544
597087 Wp = 55
91264
YDOT = 4483
990027 meter/sec RA = 256
73534 deg
ZDOT = 4237
390331 TA = 348
96486
MA = 348
97446
Ha = 226
223 n
mi
Hp = 223
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5944546
40 X = 1853662
61
Y = -17623797
81 feet Y = -5351238
39 meter
Z = 12270538
98 Z = 3748963
66
XDOT = 14910
095430 XDOT = 4473
534120
YDOT = 14711
253371 feet/sec YDOT = 4534
413108 meter/sec
ZDOT = 13902
199248 ZDOT = 4259
295284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17085347
58 X = 5207613
94
Y = 7286763
74 feet Y = 2221005
59 meter
Z = 12308370
33 Z = 3751591
28
XDOT = -15341
280833 XDOT = -4676
022398
YDOT = 12328
339428 feet/sec YDOT = 3757
677858 meter/sec
ZDOT = 13992
956916 ZDOT = 4265
053268
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 13138
14036391
00016717 00000-0 10270-3 0 9178
2 25544 51
6477 257
3027 0008734 295
2582 64
7663 15
50288612 30040
Satellite: ISS
Catalog Number: 25544
Epoch time: 13138
14036391 = yrday
fracday
Element set: 917
Inclination: 51
6477 deg
RA of node: 257
3027 deg
Eccentricity:
0008734
Arg of perigee: 295
2582 deg
Mean anomaly: 64
7663 deg
Mean motion: 15
50288612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 312
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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