Date:
May 28th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6673 62 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 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
143/23:31:13
309 0
3 1
6 1
6
N/A -1
0 -0
0 183
9
000/00:02:26
618 1
1 0
0 179
7
Coasting Arc #1 (Orbit 686)
---------------------------------------
Vector Time (GMT): 2007/143/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3314328
35 A = 6719596
31 meter
Y = -5704934
56 meter E =
0006174
Z = 1268247
51 I = 51
40231
XDOT = 4797
659009 Wp = 90
02816
YDOT = -1483
271402 meter/sec RA = 231
01907 deg
ZDOT = 5841
165262 TA = 283
94871
MA = 284
01737
Ha = 184
275 n
mi
Hp = 178
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10873780
66 X = -3256449
51
Y = -18716976
92 feet Y = -5741673
76 meter
Z = 4160917
03 Z = 1252286
50
XDOT = 15740
351078 XDOT = 4785
513321
YDOT = -4866
375990 feet/sec YDOT = -1429
689836 meter/sec
ZDOT = 19163
928025 ZDOT = 5864
442587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18777644
68 X = -5723426
10
Y = -10792005
82 feet Y = -3289403
37 meter
Z = 4100028
30 Z = 1249688
63
XDOT = 10338
298802 XDOT = 3151
113475
YDOT = -10643
376883 feet/sec YDOT = -3244
101274 meter/sec
ZDOT = 19251
514075 ZDOT = 5867
861490
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 07143
47757285
00020000 00000-0 20000-3 0 9009
2 25544 51
6331 231
5873 0009243 218
7685 141
2818 15
78192396 6872
Satellite: ISS
Catalog Number: 25544
Epoch time: 07143
47757285 = yrday
fracday
Element set: 900
Inclination: 51
6331 deg
RA of node: 231
5873 deg
Eccentricity:
0009243
Arg of perigee: 218
7685 deg
Mean anomaly: 141
2818 deg
Mean motion: 15
78192396 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 687
Checksum: 313
Coasting Arc #2 (Orbit 694)
---------------------------------------
Vector Time (GMT): 2007/143/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5241521
98 A = 6719844
95 meter
Y = -3866701
41 meter E =
0002011
Z = -1648707
57 I = 51
41090
XDOT = 1776
904430 Wp = 298
08782
YDOT = -4847
859092 meter/sec RA = 228
06961 deg
ZDOT = 5716
212599 TA = 43
61557
MA = 43
59968
Ha = 183
927 n
mi
Hp = 179
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17196594
43 X = -5189885
28
Y = -12686028
26 feet Y = -3925026
17 meter
Z = -5409145
57 Z = -1674045
83
XDOT = 5829
738944 XDOT = 1803
213521
YDOT = -15905
049513 feet/sec YDOT = -4827
842220 meter/sec
ZDOT = 18753
978344 ZDOT = 5724
908218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20400614
28 X = 6218107
23
Y = -6278938
35 feet Y = -1913820
41 meter
Z = -5505170
22 Z = -1677975
88
XDOT = 8940
034937 XDOT = 2724
922649
YDOT = 12563
257200 feet/sec YDOT = 3829
280795 meter/sec
ZDOT = 18786
164686 ZDOT = 5726
022996
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 07143
98413819
00020000 00000-0 20000-3 0 9018
2 25544 51
6329 228
9735 0008366 231
2181 128
8237 15
77907383 6956
Satellite: ISS
Catalog Number: 25544
Epoch time: 07143
98413819 = yrday
fracday
Element set: 901
Inclination: 51
6329 deg
RA of node: 228
9735 deg
Eccentricity:
0008366
Arg of perigee: 231
2181 deg
Mean anomaly: 128
8237 deg
Mean motion: 15
77907383 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 695
Checksum: 316
Coasting Arc #3 (Orbit 710)
---------------------------------------
Vector Time (GMT): 2007/144/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2516447
60 A = 6708896
64 meter
Y = 3367614
79 meter E =
0009015
Z = -5235152
28 I = 51
39529
XDOT = -5849
077922 Wp = 115
34380
YDOT = -4994
409655 meter/sec RA = 222
90618 deg
ZDOT = -405
546690 TA = 150
81792
MA = 150
76752
Ha = 183
566 n
mi
Hp = 179
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8256061
68 X = -2528486
23
Y = 11048604
96 feet Y = 3339407
62 meter
Z = -17175696
47 Z = -5247406
16
XDOT = -19189
888195 XDOT = -5790
824911
YDOT = -16385
858448 feet/sec YDOT = -5059
491579 meter/sec
ZDOT = -1330
533761 ZDOT = -433
820547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4269580
84 X = -1301368
24
Y = -13054881
66 feet Y = -3979127
93 meter
Z = -17221484
24 Z = -5249108
40
XDOT = 23520
951085 XDOT = 7169
185891
YDOT = -5814
591677 feet/sec YDOT = -1772
287543 meter/sec
ZDOT = -1437
777557 ZDOT = -438
234599
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 07144
99744024
00020000 00000-0 20000-3 0 9026
2 25544 51
6336 223
7383 0008264 235
3637 124
6749 15
77960413 7118
Satellite: ISS
Catalog Number: 25544
Epoch time: 07144
99744024 = yrday
fracday
Element set: 902
Inclination: 51
6336 deg
RA of node: 223
7383 deg
Eccentricity:
0008264
Arg of perigee: 235
3637 deg
Mean anomaly: 124
6749 deg
Mean motion: 15
77960413 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 711
Checksum: 296
Coasting Arc #4 (Orbit 726)
---------------------------------------
Vector Time (GMT): 2007/145/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4743684
96 A = 6720577
26 meter
Y = 4648735
10 meter E =
0012195
Z = -971253
24 I = 51
45687
XDOT = -4016
919729 Wp = 184
90479
YDOT = 2862
034532 meter/sec RA = 217
73069 deg
ZDOT = -5926
862383 TA = 5
75627
MA = 5
74227
Ha = 183
498 n
mi
Hp = 180
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15563270
88 X = 4696067
77
Y = 15251755
59 feet Y = 4701515
49 meter
Z = -3186526
37 Z = -948323
50
XDOT = -13178
870502 XDOT = -4019
833041
YDOT = 9389
877074 feet/sec YDOT = 2817
099316 meter/sec
ZDOT = -19445
086558 ZDOT = -5946
383543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21391260
60 X = -6520056
23
Y = 4218132
67 feet Y = 1285686
84 meter
Z = -3099471
90 Z = -944719
03
XDOT = -40
205482 XDOT = -12
254631
YDOT = -14529
781797 feet/sec YDOT = -4428
677492 meter/sec
ZDOT = -19518
344723 ZDOT = -5949
191471
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 07146
01072009
00020000 00000-0 20000-3 0 9039
2 25544 51
6339 218
5032 0008384 239
1834 120
8507 15
77949174 7276
Satellite: ISS
Catalog Number: 25544
Epoch time: 07146
01072009 = yrday
fracday
Element set: 903
Inclination: 51
6339 deg
RA of node: 218
5032 deg
Eccentricity:
0008384
Arg of perigee: 239
1834 deg
Mean anomaly: 120
8507 deg
Mean motion: 15
77949174 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 727
Checksum: 287
Coasting Arc #5 (Orbit 742)
---------------------------------------
Vector Time (GMT): 2007/146/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4449359
94 A = 6710726
92 meter
Y = -1648953
15 meter E =
0001165
Z = 4746354
88 I = 51
44823
XDOT = 4773
426295 Wp = 275
61810
YDOT = 5475
283643 meter/sec RA = 212
52151 deg
ZDOT = -2572
970614 TA = 199
65314
MA = 199
65763
Ha = 182
971 n
mi
Hp = 180
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14597637
60 X = 4444410
89
Y = -5409951
27 feet Y = -1599226
03 meter
Z = 15572030
46 Z = 4767957
94
XDOT = 15660
847424 XDOT = 4724
345270
YDOT = 17963
529012 feet/sec YDOT = 5528
388592 meter/sec
ZDOT = -8441
504640 ZDOT = -2549
899743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3489815
80 X = -1063695
86
Y = 15087817
29 feet Y = 4598766
71 meter
Z = 15653296
26 Z = 4771124
70
XDOT = -22547
411848 XDOT = -6872
451131
YDOT = 3450
235936 feet/sec YDOT = 1051
631913 meter/sec
ZDOT = -8353
809327 ZDOT = -2546
241083
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 07147
02397526
00020000 00000-0 20000-3 0 9046
2 25544 51
6338 213
2681 0008290 244
9762 115
0543 15
78049709 7437
Satellite: ISS
Catalog Number: 25544
Epoch time: 07147
02397526 = yrday
fracday
Element set: 904
Inclination: 51
6338 deg
RA of node: 213
2681 deg
Eccentricity:
0008290
Arg of perigee: 244
9762 deg
Mean anomaly: 115
0543 deg
Mean motion: 15
78049709 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 743
Checksum: 295
Coasting Arc #6 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2007/147/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3328617
65 A = 6715785
93 meter
Y = -4753140
51 meter E =
0005780
Z = 3379509
16 I = 51
49020
XDOT = 6091
991061 Wp = 120
49968
YDOT = -979
106892 meter/sec RA = 207
38836 deg
ZDOT = 4614
453554 TA = 279
52754
MA = 279
59285
Ha = 182
856 n
mi
Hp = 180
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10920661
57 X = -3291637
23
Y = -15594293
01 feet Y = -4790156
58 meter
Z = 11087628
49 Z = 3363427
80
XDOT = 19986
847312 XDOT = 6080
070291
YDOT = -3212
292952 feet/sec YDOT = -911
049989 meter/sec
ZDOT = 15139
283313 ZDOT = 4644
019827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19052760
97 X = 5807281
54
Y = -888562
41 feet Y = -270833
82 meter
Z = 11026381
34 Z = 3360841
03
XDOT = -8044
057948 XDOT = -2451
828863
YDOT = 17123
866240 feet/sec YDOT = 5219
354430 meter/sec
ZDOT = 15250
672279 ZDOT = 4648
404911
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 07148
03721086
00020000 00000-0 20000-3 0 9051
2 25544 51
6340 208
0321 0008178 248
9582 111
0708 15
78036990 7596
Satellite: ISS
Catalog Number: 25544
Epoch time: 07148
03721086 = yrday
fracday
Element set: 905
Inclination: 51
6340 deg
RA of node: 208
0321 deg
Eccentricity:
0008178
Arg of perigee: 248
9582 deg
Mean anomaly: 111
0708 deg
Mean motion: 15
78036990 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 759
Checksum: 289
Coasting Arc #7 (Orbit 773)
---------------------------------------
Vector Time (GMT): 2007/148/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5998400
21 A = 6716518
75 meter
Y = 145735
28 meter E =
0003792
Z = -3016363
82 I = 51
51948
XDOT = -2615
359021 Wp = 253
94931
YDOT = -5303
926946 meter/sec RA = 202
16122 deg
ZDOT = 4938
543881 TA = 71
03775
MA = 70
99666
Ha = 182
552 n
mi
Hp = 180
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19679790
72 X = -5984930
83
Y = 478134
11 feet Y = 78733
50 meter
Z = -9896206
74 Z = -3045471
82
XDOT = -8580
574217 XDOT = -2579
846323
YDOT = -17401
335126 feet/sec YDOT = -5332
975429 meter/sec
ZDOT = 16202
571788 ZDOT = 4925
923827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9845785
90 X = 3000995
54
Y = -16982301
11 feet Y = -5176205
38 meter
Z = -10005979
81 Z = -3049822
65
XDOT = 18129
339716 XDOT = 5525
822745
YDOT = 980
913504 feet/sec YDOT = 298
982436 meter/sec
ZDOT = 16154
309637 ZDOT = 4923
833577
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 07148
98709696
00020000 00000-0 20000-3 0 9069
2 25544 51
6339 203
1238 0008312 253
4047 106
6205 15
78082032 7741
Satellite: ISS
Catalog Number: 25544
Epoch time: 07148
98709696 = yrday
fracday
Element set: 906
Inclination: 51
6339 deg
RA of node: 203
1238 deg
Eccentricity:
0008312
Arg of perigee: 253
4047 deg
Mean anomaly: 106
6205 deg
Mean motion: 15
78082032 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 774
Checksum: 292
Coasting Arc #8 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2007/149/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1046324
44 A = 6709806
47 meter
Y = 4425070
24 meter E =
0004479
Z = -4938196
82 I = 51
52361
XDOT = -7402
126383 Wp = 68
69764
YDOT = -552
137972 meter/sec RA = 197
02752 deg
ZDOT = -2063
050539 TA = 181
29929
MA = 181
30045
Ha = 182
245 n
mi
Hp = 180
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3432822
96 X = 1020754
19
Y = 14517946
97 feet Y = 4436628
59 meter
Z = -16201433
12 Z = -4933175
13
XDOT = -24285
191545 XDOT = -7385
380044
YDOT = -1811
476286 feet/sec YDOT = -634
818757 meter/sec
ZDOT = -6768
538515 ZDOT = -2098
970131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14296284
15 X = -4357507
41
Y = -4336185
68 feet Y = -1321669
40 meter
Z = -16181941
98 Z = -4932255
91
XDOT = 13555
756211 XDOT = 4131
794493
YDOT = -18926
657130 feet/sec YDOT = -5768
845093 meter/sec
ZDOT = -6904
102577 ZDOT = -2104
370465
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 07150
00028806
00020000 00000-0 20000-3 0 9073
2 25544 51
6332 197
8880 0008328 257
8268 102
1964 15
78133875 7909
Satellite: ISS
Catalog Number: 25544
Epoch time: 07150
00028806 = yrday
fracday
Element set: 907
Inclination: 51
6332 deg
RA of node: 197
8880 deg
Eccentricity:
0008328
Arg of perigee: 257
8268 deg
Mean anomaly: 102
1964 deg
Mean motion: 15
78133875 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 790
Checksum: 304
Coasting Arc #9 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2007/150/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6619959
09 A = 6720402
94 meter
Y = 1024545
35 meter E =
0010034
Z = 447330
10 I = 51
58700
XDOT = -336
294108 Wp = 169
52134
YDOT = 4805
649611 meter/sec RA = 191
83300 deg
ZDOT = -6018
574130 TA = 5
60061
MA = 5
58940
Ha = 182
077 n
mi
Hp = 180
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21719025
88 X = 6605837
37
Y = 3361369
25 feet Y = 1098494
41 meter
Z = 1467618
43 Z = 479456
29
XDOT = -1103
327127 XDOT = -360
768949
YDOT = 15766
566964 feet/sec YDOT = 4801
753163 meter/sec
ZDOT = -19745
978116 ZDOT = -6020
266505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13624874
77 X = -4152861
83
Y = 17233886
31 feet Y = 5252888
55 meter
Z = 1588943
69 Z = 484310
04
XDOT = -11972
624549 XDOT = -3649
255963
YDOT = -7641
141101 feet/sec YDOT = -2329
019808 meter/sec
ZDOT = -19751
770837 ZDOT = -6020
339751
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 07151
01345923
00020000 00000-0 20000-3 0 9088
2 25544 51
6330 192
6525 0008287 260
3076 99
7154 15
78111990 8060
Satellite: ISS
Catalog Number: 25544
Epoch time: 07151
01345923 = yrday
fracday
Element set: 908
Inclination: 51
6330 deg
RA of node: 192
6525 deg
Eccentricity:
0008287
Arg of perigee: 260
3076 deg
Mean anomaly: 99
7154 deg
Mean motion: 15
78111990 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 806
Checksum: 290
Coasting Arc #10 (Orbit 821)
---------------------------------------
Vector Time (GMT): 2007/151/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1675172
45 A = 6708527
25 meter
Y = -3935756
87 meter E =
0005426
Z = 5172682
41 I = 51
57564
XDOT = 7427
497027 Wp = 284
98205
YDOT = 1733
878496 meter/sec RA = 186
65617 deg
ZDOT = -1085
694856 TA = 175
38333
MA = 175
37833
Ha = 181
645 n
mi
Hp = 181
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5495972
60 X = 1693929
84
Y = -12912588
17 feet Y = -3916920
26 meter
Z = 16970742
82 Z = 5180865
33
XDOT = 24368
428565 XDOT = 7412
830698
YDOT = 5688
577743 feet/sec YDOT = 1816
855132 meter/sec
ZDOT = -3561
990999 ZDOT = -1049
646848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8762546
89 X = 2670824
29
Y = 10914482
39 feet Y = 3326734
23 meter
Z = 17001135
44 Z = 5181946
08
XDOT = -15854
224585 XDOT = -4832
367653
YDOT = 18066
788485 feet/sec YDOT = 5506
757130 meter/sec
ZDOT = -3425
767533 ZDOT = -1044
173944
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 07152
02660547
00020000 00000-0 20000-3 0 9093
2 25544 51
6324 187
4158 0008361 265
6406 94
3804 15
78197289 8221
Satellite: ISS
Catalog Number: 25544
Epoch time: 07152
02660547 = yrday
fracday
Element set: 909
Inclination: 51
6324 deg
RA of node: 187
4158 deg
Eccentricity:
0008361
Arg of perigee: 265
6406 deg
Mean anomaly: 94
3804 deg
Mean motion: 15
78197289 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 822
Checksum: 306
Coasting Arc #11 (Orbit 837)
---------------------------------------
Vector Time (GMT): 2007/152/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5998644
79 A = 6717942
88 meter
Y = -1967901
12 meter E =
0006503
Z = 2284859
60 I = 51
63522
XDOT = 3459
816646 Wp = 49
27871
YDOT = -4219
145971 meter/sec RA = 181
51449 deg
ZDOT = 5443
620477 TA = 336
44518
MA = 336
47495
Ha = 180
582 n
mi
Hp = 180
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19680593
16 X = -5987293
15
Y = -6456368
49 feet Y = -2034918
32 meter
Z = 7496258
52 Z = 2255745
05
XDOT = 11351
104480 XDOT = 3480
294219
YDOT = -13842
342425 feet/sec YDOT = -4180
342972 meter/sec
ZDOT = 17859
647234 ZDOT = 5460
477326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14848046
85 X = 4525684
68
Y = -14497744
03 feet Y = -4418912
38 meter
Z = 7386152
96 Z = 2251299
42
XDOT = 6009
641337 XDOT = 1831
738680
YDOT = 15295
912936 feet/sec YDOT = 4662
194263 meter/sec
ZDOT = 17922
743008 ZDOT = 5462
852069
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 07153
03973126
00020000 00000-0 20000-3 0 9107
2 25544 51
6312 182
1784 0008459 269
7682 90
2514 15
78235561 8380
Satellite: ISS
Catalog Number: 25544
Epoch time: 07153
03973126 = yrday
fracday
Element set: 910
Inclination: 51
6312 deg
RA of node: 182
1784 deg
Eccentricity:
0008459
Arg of perigee: 269
7682 deg
Mean anomaly: 90
2514 deg
Mean motion: 15
78235561 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 838
Checksum: 299
Coasting Arc #12 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2007/153/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4212851
35 A = 6713150
74 meter
Y = 3411852
24 meter E =
0002388
Z = -3959356
53 I = 51
64747
XDOT = -5987
860148 Wp = 223
97432
YDOT = -2769
601985 meter/sec RA = 176
29915 deg
ZDOT = 3981
493561 TA = 87
25360
MA = 87
22626
Ha = 181
123 n
mi
Hp = 180
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13821690
79 X = -4231456
13
Y = 11193740
96 feet Y = 3364638
58 meter
Z = -12990014
85 Z = -3979867
16
XDOT = -19645
210460 XDOT = -5975
786502
YDOT = -9086
620686 feet/sec YDOT = -2836
494914 meter/sec
ZDOT = 13062
642916 ZDOT = 3952
433121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3861378
30 X = -1176948
11
Y = -17303829
08 feet Y = -5274207
10 meter
Z = -13067008
67 Z = -3982824
24
XDOT = 15685
195802 XDOT = 4780
847680
YDOT = -13289
047729 feet/sec YDOT = -4050
501748 meter/sec
ZDOT = 12952
628962 ZDOT = 3947
961308
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 07153
98951795
00020000 00000-0 20000-3 0 9110
2 25544 51
6302 177
2682 0008410 273
3140 86
7063 15
78257634 8539
Satellite: ISS
Catalog Number: 25544
Epoch time: 07153
98951795 = yrday
fracday
Element set: 911
Inclination: 51
6302 deg
RA of node: 177
2682 deg
Eccentricity:
0008410
Arg of perigee: 273
3140 deg
Mean anomaly: 86
7063 deg
Mean motion: 15
78257634 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 853
Checksum: 301
Coasting Arc #13 (Orbit 868)
---------------------------------------
Vector Time (GMT): 2007/154/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4165952
49 A = 6711622
51 meter
Y = 2879689
69 meter E =
0004359
Z = -4407075
57 I = 51
67001
XDOT = -5971
777499 Wp = 4
88197
YDOT = 3572
083797 meter/sec RA = 171
18250 deg
ZDOT = -3306
930999 TA = 231
92546
MA = 231
96479
Ha = 181
794 n
mi
Hp = 181
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13667823
12 X = 4154850
54
Y = 9447800
80 feet Y = 2926214
52 meter
Z = -14458909
34 Z = -4386863
73
XDOT = -19592
445863 XDOT = -5995
212743
YDOT = 11719
435031 feet/sec YDOT = 3505
173672 meter/sec
ZDOT = -10849
511152 ZDOT = -3335
998124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14458831
04 X = -4407051
70
Y = 8320035
93 feet Y = 2535946
95 meter
Z = -14382266
70 Z = -4383714
89
XDOT = -1528
579483 XDOT = -465
911026
YDOT = -21623
087465 feet/sec YDOT = -6590
717059 meter/sec
ZDOT = -10958
793681 ZDOT = -3340
240314
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 07155
00260227
00020000 00000-0 20000-3 0 9129
2 25544 51
6293 172
0316 0008394 277
3499 82
6712 15
78281357 8699
Satellite: ISS
Catalog Number: 25544
Epoch time: 07155
00260227 = yrday
fracday
Element set: 912
Inclination: 51
6293 deg
RA of node: 172
0316 deg
Eccentricity:
0008394
Arg of perigee: 277
3499 deg
Mean anomaly: 82
6712 deg
Mean motion: 15
78281357 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 869
Checksum: 300
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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